Regulation UN No. 10 (Rev.6)

Electromagnetic Compatibility

Consolidated up to Suppl. 1 to 06 dated: 25.09.2020

... Regulation a0c0
... 1. Scope a0c0
... 2. Definitions a0c0
... 3. Application for approval a0c0
... 4. Approval a0c0
... 5. Markings a0c0
... 6. Specification in configurations other than REESS charging mode coupled to the power grid a0c0
... 7. Additional specifications in the configuration "REESS charging mode coupled to the power grid" a0c0
... 8. Amendment or extension of a vehicle type approval following electrical/electronic sub-assembly (ESA) addition or substitution a0c0
...

9. Conformity of production

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... 10. Penalties for non-conformity of production a0c0
... 11. Production definitively discontinued a0c0
... 12. Modification and extension of type approval of a vehicle or ESA a0c0
... 13. Transitional provisions a0c0
... 14. Names and addresses of Technical Services conducting approval tests and of Type Approval Authorities a0c0
... Appendix 1 - List of standards referred to in this Regulation a0c0
... Appendix 2 - Vehicle broadband reference limits - Antenna-vehicle separation: 10 m a0c0
... Appendix 3 - Vehicle broadband reference limits - Antenna-vehicle separation: 3 m a0c0
... Appendix 4 - Vehicle narrowband reference limits - Antenna-vehicle separation: 10 m a0c0
... Appendix 5 - Vehicle narrowband reference limits - Antenna-vehicle separation: 3 m a0c0
... Appendix 6 - Electrical/electronic sub-assembly - Broadband reference limits a0c0
... Appendix 7 - Electrical/electronic sub-assembly - Narrowband reference limits a0c0
... Appendix 8 - Artificial networks (AN), High Voltage Artificial Networks (HV-AN), Direct Current charging Artificial Networks (DC-charging-AN), Artificial Mains Networks (AMN) and Asymmetric Artificial Networks (AAN) [#new] a0c0
... Annexes a0c0
... 1 Examples of approval marks a0c0
... 2A Information document for type approval of a vehicle with respect to electromagnetic compatibility a0c0
... 2B Information document for type approval of an electric/electronic sub-assembly with respect to electromagnetic compatibility a0c0
... 3A Communication concerning the approval or extension or refusal or withdrawal of approval or production definitively discontinued of a type of vehicle/component/separate technical unit with regard to Regulation No. 10 a0c0
... 3B Communication concerning the approval or extension or refusal or withdrawal of approval or production definitively discontinued of a type of electrical/electronic sub-assembly with regard to Regulation No. 10 a0c0
... 4 Method of measurement of radiated broadband electromagnetic emissions from vehicles a0c0
... Appendix 1 a0c0
... 5 Method of measurement of radiated narrowband electromagnetic emissions from vehicles a0c0
... Appendix 1 [#new] a0c0
... 6 Method of testing for immunity of vehicles to electromagnetic radiation a0c0
... Appendix 1 a0c0
... 7 Method of measurement of radiated broadband electromagnetic emissions from electrical/electronic sub assemblies (ESAs) a0c0
... Appendix 1 a0c0
... 8 Method of measurement of radiated narrowband electromagnetic emissions from electrical/electronic sub assemblies a0c0
... 9 Method(s) of testing for immunity of electrical/electronic sub-assemblies to electromagnetic radiation a0c0
... Appendix 1 a0c0
... Appendix 2 - Typical TEM cell dimensions a0c0
... Appendix 3 - Absorber chamber test a0c0
... Appendix 4 - BCI test a0c0
... 10 Method(s) of testing for immunity to and emission of transients of electrical/electronic sub-assemblies a0c0
... 11 Method(s) of testing for emission of harmonics generated on AC power lines from vehicle a0c0
... Appendix 1 a0c0
... 12 Method(s) of testing for emission of voltage changes, voltage fluctuations and flicker on AC power lines from vehicle a0c0
... Appendix 1 a0c0
... 13 Method(s) of testing for emission of radiofrequency conducted disturbances on AC or DC power lines from vehicles a0c0
... Appendix 1 a0c0
... 14 Method(s) of testing for emission of radiofrequency conducted disturbances on network and telecommunication access from vehicles a0c0
... Appendix 1 a0c0
... 15 Method of testing for immunity of vehicles to Electrical Fast Transient/Burst disturbances conducted along AC and DC power lines a0c0
... Appendix 1 a0c0
... 16 Method of testing for immunity of vehicles to surges conducted along AC and DC power lines a0c0
... Appendix 1 - Vehicle in configuration "REESS charging mode coupled to the power grid" a0c0
... 17 Method(s) of testing for emission of harmonics generated on AC power lines from an ESA a0c0
... Appendix 1 a0c0
... 18 Method(s) of testing for emission of voltage changes, voltage fluctuations and flicker on AC power lines from an ESA a0c0
... Appendix 1 a0c0
... 19 Method(s) of testing for emission of radiofrequency conducted disturbances on AC or DC power lines from an ESA a0c0
... Appendix 1 a0c0
... 20 Method(s) of testing for emission of radiofrequency conducted disturbances on network and telecommunication access from an ESA a0c0
... Appendix 1 [#new] a0c0
... 21 Method of testing for immunity of an ESA to Electrical Fast Transient/Burst disturbances conducted along AC and DC power lines a0c0
... Appendix 1 a0c0
... 22 Method of testing for immunity of ESAs to surges conducted along AC and DC power lines a0c0
...

Appendix 1 - ESA in configuration "REESS charging mode coupled to the power grid"

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1. Scope a0c0
... This Regulation applies to: a0c0
1.1. Vehicles of categories L, M, N and O[1] with regard to electromagnetic compatibility; a-1c0
1.2. Components and separate technical units intended to be fitted in these vehicles with the limitation given in paragraph 3.2.1. with regard to electromagnetic compatibility. a0c0
1.3. It covers: a0c0
... (a) Requirements regarding the immunity to radiated and conducted disturbances for functions related to direct control of the vehicle, related to driver, passenger and other road users' protection, related to disturbances, which would cause confusion to the driver or other road users, related to vehicle data bus functionality, related to disturbances, which would affect vehicle statutory data; a0c0
... (b) Requirements regarding the control of unwanted radiated and conducted emissions to protect the intended use of electrical or electronic equipment at own or adjacent vehicles or nearby, and the control of disturbances from accessories that may be retrofitted to the vehicle. a0c0
... (c) Additional requirements for vehicles and ESAs providing coupling systems for charging the REESS regarding the control of emissions and immunity from this connection between vehicle and power grid. a0c0
1 As defined in the Consolidated Resolution on the Construction of Vehicles (R.E.3), document ECE/TRANS/WP.29/78/Rev.3, para. 2. a0c0
2. Definitions a0c0
... For the purposes of this Regulation: a0c0
2.1. "Electromagnetic compatibility" means the ability of a vehicle or component(s) or separate technical unit(s) to function satisfactorily in its electromagnetic environment without introducing intolerable electromagnetic disturbances to anything in that environment. a0c0
2.2. "Electromagnetic disturbance" means any electromagnetic phenomenon which may degrade the performance of a vehicle or component(s) or separate technical unit(s), or of any other device, unit of equipment or system operated in vicinity of a vehicle. An electromagnetic disturbance may be electromagnetic noise, an unwanted signal or a change in the propagation medium itself. a0c0
2.3. "Electromagnetic immunity" means the ability of a vehicle or component(s) or separate technical unit(s) to operate without degradation of performance in the presence of (specified) electromagnetic disturbances which includes wanted radio frequency signals from radio transmitters or radiated in-band emissions of industrial-scientific-medical (ISM) apparatus, internal or external to the vehicle. a0c0
2.4. "Electromagnetic environment" means the totality of electromagnetic phenomena existing at a given location. a0c0
2.5. "Broadband emission" means an emission, which has a bandwidth greater than that of a particular measuring apparatus or receiver (International Special Committee on Radio Interference (CISPR) 25). a0c0
2.6. "Narrowband emission" means an emission which has a bandwidth less than that of a particular measuring apparatus or receiver (CISPR 25). a0c0
2.7. "Electrical/electronic system" means (an) electrical and/or electronic device(s) or set(s) of devices together with any associated electrical connections which form part of a vehicle but which are not intended to be type approved separately from the vehicle. a0c0
2.8. "Electrical/electronic sub-assembly" (ESA) means an electrical and/or electronic device or set(s) of devices intended to be part of a vehicle, together with any associated electrical connections and wiring, which performs one or more specialized functions. An ESA may be approved at the request of a manufacturer or his authorized representative as either a "component" or a "separate technical unit (STU)". a0c0
2.9. "Vehicle type" in relation to electromagnetic compatibility includes all vehicles, which do not differ essentially in such respects as: a0c0
2.9.1. The overall size and shape of the engine compartment; a0c0
2.9.2. The general arrangement of the electrical and/or electronic components and the general wiring arrangement; a0c0
2.9.3. The primary material of which the body or shell of the vehicle is constructed (for example, a steel, aluminium or fiberglass body shell). The presence of panels of different material does not change the vehicle type provided the primary material of the body is unchanged. However, such variations shall be notified. a0c0
2.10. An "ESA type" in relation to electromagnetic compatibility means ESAs, which do not differ in such essential respects as: a0c0
2.10.1. The function performed by the ESA; a0c0
2.10.2. The general arrangement of the electrical and/or electronic components, if applicable. a0c0
2.11. "Vehicle wiring harness" means supply voltage, bus system (e.g. CAN), signal or active antenna cables, which are installed by the vehicle manufacturer. a0c0
2.12. "Immunity related functions" are: a-1c0
... (a) Functions related to the direct control of the vehicle: a0c0
... (i) By degradation or change in: e.g. engine, gear, brake, suspension, active steering, speed limitation devices; a0c0
... (ii) By affecting drivers position: e.g. seat or steering wheel positioning; a0c0
... (iii) By affecting driver's visibility: e.g. dipped beam, windscreen wiper. a-1c0
... (b) Functions related to driver, passenger and other road user protection: a0c0
... (i) E.g. airbag and safety restraint systems. a-1c0
... (c) Functions which, when disturbed, cause confusion to the driver or other road users: a0c0
... (i) Optical disturbances: incorrect operation of e.g. direction indicators, stop lamps, end outline marker lamps, rear position lamp, light bars for emergency system, wrong information from warning indicators, lamps or displays related to functions in subparagraphs (a) or (b) which might be observed in the direct view of the driver; a0c0
... (ii) Acoustical disturbances: incorrect operation of e.g. anti-theft alarm, horn. a0c0
... (d) Functions related to vehicle data bus functionality: a0c0
... (i) By blocking data transmission on vehicle data bus-systems, which are used to transmit data, required to ensure the correct functioning of other immunity related functions. a0c0
... (e) Functions which when disturbed affect vehicle statutory data: e.g. tachograph, odometer. a0c0
... (f) Function related to charging mode when coupled to the power grid: a0c0
... (i) For vehicle test: by leading to unexpected vehicle motion; a0c0
... (ii) For ESA test: by leading to an incorrect charging condition (e.g. over-current, over-voltage). a0c0
2.13. "REESS" means the rechargeable energy storage system that provides electric energy for electric propulsion of the vehicle. a0c0
2.14. "Coupling system for charging the REESS" means the electrical circuit installed in the vehicle used for charging the REESS. a0c0
2.15. "REESS charging mode coupled to the power grid" means the normal charging operation mode of the vehicle and/or charging system. a0c0
2.16.

"Mode 1 Charging Mode" means charging mode as defined in IEC 61851-1 sub-clause 6.2.1 where the vehicle is connected directly to AC mains without any communication between the vehicle and the charging station and without any supplementary pilot or auxiliary contacts. In some countries Mode 1 charging may be prohibited or requires special pre-cautions. [#new]

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2.17.

"Mode 2 Charging Mode" means charging mode as defined in IEC 61851-1 sub-clause 6.2.2 where the vehicle is connected to AC mains using a charging harness including an Electric Vehicle Supply Equipment (EVSE) box providing control pilot signalling between the vehicle and the EVSE box and personal protection against electric shock. In some countries, special restrictions have to be applied for mode 2 charging. There is no communication between the vehicle and the AC supply network (mains). [#new]

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2.18.

"Mode 3 Charging Mode" means charging mode as defined in IEC 61851-1 sub-clause 6.2.3 where the vehicle is connected to an EVSE (e.g charging station, wallbox) providing AC power to the vehicle with communication between the vehicle and the charging station (through signal/control lines and/or through wired network lines). [#new]

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2.19.

"Mode 4 Charging Mode" means charging mode as defined in IEC 61851-1 sub-clause 6.2.4 where the vehicle is connected to an EVSE providing DC power to the vehicle (with an off-board charger) with communication between the vehicle and the charging station (through signal/control lines and/or through wired network lines) [#new]

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2.20.

"Signal/control port" means port intended for the interconnection of components of an ESA, or between an ESA and local AE (Ancillary Equipment) and used in accordance with relevant functional specifications (for example for the maximum length of cable connected to it). Examples include RS-232, Universal Serial Bus (USB), High-Definition Multimedia Interface (HDMI), IEEE Standard 1394 ("Fire Wire"). For vehicle in charging mode this includes Control Pilot signal, PLC technology used on Control Pilot signal line, CAN. [#new]

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2.21.

"Wired network port" means port for the connection of voice, data and signaling transfers intended to interconnect widely dispersed systems by direct connection to a single-user or multi-user communication network. Examples of these include CATV, PSTN, ISDN, xDSL, LAN and similar networks. These ports may support screened or unscreened cables and may also carry AC or DC power where this is an integral part of the telecommunication specification. [#new]

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2.22.

"Asymmetric artificial network (AAN)" means network used to measure (or inject) asymmetric (common mode) voltages on unshielded symmetric signal (e.g. telecommunication) lines while rejecting the symmetric (differential mode) signal. This network is inserted in the communication/signal lines of the vehicle in charging mode to provide a specific load impedance and/or a decoupling (e.g. between communication/signal lines and power mains). AAN is also used in this regulation for symmetric lines[#new]

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2.23. "Direct current charging artificial network (DC-charging-AN)" means network inserted in the high voltage DC lead of vehicle in charging mode which provides, in a given frequency range, a specified load impedance and which may isolate the vehicle from the HV DC charging station in that frequency range. [#new] a0c0
2.24.

"Artificial mains network (AMN)" means provides a defined impedance to the ESA at radio frequencies, couples the disturbance voltage to the measuring receiver and decouples the test circuit from the supply mains. There are two basic types of AMN, the V-network (V-AMN) that couples the unsymmetrical voltages, and the delta-network that couples the symmetric and the asymmetric voltages separately. The terms line impedance stabilization network (LISN) and V-AMN are used interchangeably. Network inserted in the power mains of the vehicle in charging mode which provides, in a given frequency range, a specified load impedance and which isolates the vehicle from the power mains in that frequency range. [#new]

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2.25.

"Outdoor Test Site (OTS)" measurement site similar to an open area test site as specified in CISPR 16, however a ground plane is not required and there are dimensional changes. [#new]

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3. Application for approval a0c0
3.1. Approval of a vehicle type a0c0
3.1.1. The application for approval of a vehicle type, with regard to its electromagnetic compatibility, shall be submitted by the vehicle manufacturer. a0c0
3.1.2. A model of information document is shown in Annex 2A. a0c0
3.1.3. The vehicle manufacturer shall draw up a schedule describing all relevant vehicle electrical/electronic systems or ESAs, body styles, variations in body material, general wiring arrangements, engine variations, left-hand/right-hand drive versions and wheelbase versions. Relevant vehicle electrical/electronic systems or ESAs are those which may emit significant broadband or narrowband radiation and/or those which are involved in immunity related functions of the vehicle (see paragraph 2.12.) and those which provide coupling systems for charging the REESS. a0c0
3.1.4. A vehicle representative of the type to be approved shall be selected from this schedule by mutual agreement between the manufacturer and the Type Approval Authority. The choice of vehicle shall be based on the electrical/electronic systems offered by the manufacturer. One or more vehicles may be selected from this schedule if it is considered by mutual agreement between the manufacturer and the Type Approval Authority that different electrical/electronic systems are included which are likely to have a significant effect on the vehicle's electromagnetic compatibility compared with the first representative vehicle. a0c0
3.1.5. The choice of the vehicle(s) in conformity with paragraph 3.1.4. above shall be limited to vehicle/electrical/electronic system combinations intended for actual production. a0c0
3.1.6. The manufacturer may supplement the application with a report on tests which have been carried out. Any such data provided may be used by the Type Approval Authority for the purpose of drawing up the communication form for type approval. a0c0
3.1.7. If the Technical Service responsible for the type approval test carries out the test itself, then a vehicle representative of the type to be approved according to paragraph 3.1.4. above shall be provided. a0c0
3.1.8. For vehicles of categories M, N, and O, the vehicle manufacturer shall provide a statement of frequency bands, power levels, antenna positions and installation provisions for the installation of radio frequency transmitters (RF-transmitters), even if the vehicle is not equipped with an RF transmitter at time of type approval. This should cover all mobile radio services normally used in vehicles. This information shall be made publicly available following the type approval. a-1c0
... Vehicle manufacturers shall provide evidence that vehicle performance is not adversely affected by such transmitter installations. a0c0
3.1.9. Vehicle type approval shall be applied for both REESS and coupling system for charging the REESS as they are considered as electrical/electronic systems. [#new] a0c0
3.2. ESA type approval a0c0
3.2.1. Applicability of this Regulation to ESA: a0c0
... a0c0
3.2.2. The application for approval of a type of ESA with regard to its electromagnetic compatibility shall be submitted by the vehicle manufacturer or by the manufacturer of the ESA. a0c0
3.2.3. A model of information document is shown in Annex 2B. a0c0
3.2.4. The manufacturer may supplement the application with a report on tests which have been carried out. Any such data provided may be used by the Type Approval Authority for the purpose of drawing up the communication form for type approval. a0c0
3.2.5. If the Technical Service responsible for the type approval test carries out the test itself, then a sample of the ESA system representative of the type to be approved shall be provided, if necessary, after discussion with the manufacturer on, e.g. possible variations in the layout, number of components, number of sensors. If the Technical Service deems it necessary, it may select a further sample. a0c0
3.2.6. The sample(s) shall be clearly and indelibly marked with the manufacturer's trade name or mark and the type designation. a0c0
3.2.7. Where applicable, any restrictions on use should be identified. Any such restrictions should be included in Annexes 2B and/or 3B. a0c0
3.2.8. ESA which are brought to the market as spare parts need no type approval if they are obviously marked as a spare part by an identification number and if they are identical and from the same manufacturer as the corresponding Original Equipment Manufacturer (OEM) part for an already type approved vehicle. a0c0
3.2.9. Components sold as aftermarket equipment and intended for the installation in motor vehicles need no type approval if they are not related to immunity related functions (see paragraph 2.12.). In this case a declaration shall be issued by the manufacturer that the ESA fulfils the requirements of this Regulation and in particular the limits defined in paragraphs 6.5., 6.6., 6.7., 6.8. and 6.9. of this Regulation. a0c0
3.2.10. In case of an ESA is (part of) a light source, the applicant shall: a0c0
... (a) Specify the approval number according to Regulation No. 37, Regulation No. 99 or Regulation No. 128, granted to this ESA; a0c0
... or a0c0
... (b) Provide a test report by a Technical Service designated by the Type Approval Authority, stating that this ESA is not mechanically interchangeable with any light source according to Regulation No. 37, Regulation No. 99 or Regulation No. 128. a0c0
4. Approval a0c0
4.1. Type approval procedures a0c0
4.1.1. Type approval of a vehicle a0c0
... The following alternative procedures for vehicle type approval may be used at the discretion of the vehicle manufacturer. a0c0
4.1.1.1. Approval of a vehicle installation a0c0
... A vehicle installation may be type approved directly by following the provisions laid down in paragraph 6. and, if applicable, in paragraph 7. of this Regulation. If this procedure is chosen by a vehicle manufacturer, no separate testing of electrical/electronic systems or ESAs is required. a0c0
4.1.1.2. Approval of vehicle type by testing of individual ESAs a0c0
... A vehicle manufacturer may obtain approval for the vehicle by demonstrating to the Type Approval Authority that all the relevant (see para. 3.1.3. of this Regulation) electrical/electronic systems or ESAs have been approved in accordance with this Regulation and have been installed in accordance with any conditions attached thereto. a0c0
4.1.1.3. A manufacturer may obtain approval according to this Regulation if the vehicle has no equipment of the type, which is subject to immunity or emission tests. Such approvals do not require testing. a0c0
4.1.2. Type approval of an ESA a0c0
... Type approval may be granted to an ESA to be fitted either to any vehicle type (component approval) or to a specific vehicle type or types requested by the ESA manufacturer (separate technical unit approval). a0c0
4.1.3. ESAs, which are intentional RF transmitters, which have not received type approval in conjunction with a vehicle manufacturer, shall be supplied with suitable installation guidelines. a0c0
4.2. Granting of type approval a0c0
4.2.1. Vehicle a0c0
4.2.1.1. If the representative vehicle fulfils the requirements of paragraph 6. and, if applicable, paragraph 7. of this Regulation, type approval shall be granted. a0c0
4.2.1.2. A model of communication form for type approval is contained in Annex 3A. a0c0
4.2.2. ESA a0c0
4.2.2.1. If the representative ESA system(s) fulfil(s) the requirements of paragraph 6. and, if applicable, paragraph 7. of this Regulation, type approval shall be granted. a0c0
4.2.2.2. A model of communication form for type approval is contained in Annex 3B. a0c0
4.2.3. In order to draw up the communication forms referred to in paragraph 4.2.1.2. or 4.2.2.2. above, the Type Approval Authority of the Contracting Party granting the approval may use a report prepared or approved by a recognized laboratory or in accordance with the provisions of this Regulation. a0c0
4.2.4. In case of an ESA is (part of) a light source and if the documentation as specified in paragraph 3.2.10. above is missing, approval of this ESA according to Regulation No. 10 shall not be granted. a0c0
4.3. Approval, or refusal of approval, of a type of vehicle or ESA in accordance with this Regulation shall be notified to the Parties to the Agreement applying this Regulation on a form conforming to the model in Annex 3A or 3B to this Regulation, accompanied by photographs and/or diagrams or drawings on an appropriate scale supplied by the applicant in a format not larger than A4 (210 x 297 mm) or folded to those dimensions. a0c0
5. Markings a0c0
5.1. An approval number shall be assigned to each vehicle or ESA type approved. The first two digits of this number (at present 05) shall indicate the series of amendments corresponding to the most recent essential technical amendments made to the Regulation at the date of approval. A Contracting Party may not assign the same approval number to another type of vehicle or ESA. a0c0
5.2. Presence of markings a0c0
5.2.1. Vehicle a0c0
... An approval mark described in paragraph 5.3. below shall be affixed to every vehicle conforming to a type approved under this Regulation. a0c0
5.2.2. Sub-assembly a0c0
... An approval mark described in paragraph 5.3. below shall be affixed to every ESA conforming to a type approved under this Regulation. a0c0
... No marking is required for electrical/electronic systems built into vehicles which are approved as units. a0c0
5.3. An international approval mark shall be affixed, in a conspicuous and easily accessible place specified on the approval communication form, on each vehicle conforming to the type approved under this Regulation. This mark shall comprise: a0c0
5.3.1. A circle containing the letter "E", followed by the distinguishing number of the country granting the approval.[2] a0c0
5.3.2. The number of this Regulation, followed by the letter "R", a dash and the approval number to the right of the circle specified in paragraph 5.3.1. above. a0c0
5.4. An example of the type approval mark is shown in Annex 1 to this Regulation. a0c0
5.5. Markings on ESAs in conformity with paragraph 5.3. above need not be visible when the ESA is installed in the vehicle. a0c0
[2] The distinguish numbers of the Contracting Parties to the 1958 Agreement are reproduced in Annex 3 to Consolidated Resolution on the Construction of Vehicles (R.E.3), document ECE/TRANS/WP.29/78/Rev.6, Annex 3. a0c0
6. Specification in configurations other than REESS charging mode coupled to the power grid a0c0
6.1. General specifications a0c0
6.1.1. A vehicle and its electrical/electronic system(s) or ESA(s) shall be so designed, constructed and fitted as to enable the vehicle, in normal conditions of use, to comply with the requirements of this Regulation. a0c0
6.1.1.1. A vehicle shall be tested for radiated emissions and for immunity to radiated disturbances. No tests for conducted emissions or immunity to conducted disturbances are required for vehicle type approval. a0c0
6.1.1.2. ESA(s) shall be tested for radiated and conducted emissions, for immunity to radiated and conducted disturbances. a0c0
6.1.2. Before testing, the Technical Service has to prepare a test plan in conjunction with the manufacturer, which contains at least mode of operation, stimulated function(s), monitored function(s), pass/fail criterion(criteria) and intended emissions. a0c0
6.2. Specifications concerning broadband electromagnetic radiation from vehicles a0c0
6.2.1. Method of measurement a0c0
... The electromagnetic radiation generated by the vehicle representative of its type shall be measured using the method described in Annex 4. The method of measurement shall be defined by the vehicle manufacturer in accordance with the Technical Service. a0c0
6.2.2. Vehicle broadband type approval limits a0c0
6.2.2.1.

If measurements are made using the method described in Annex 4 using a vehicle-to-antenna spacing of 10.0 ± 0.2 m, the limits shall be 32 dB microvolts/m in the 30 to 75 MHz frequency band and 32 to 43 dB microvolts/m in the 75 to 400 MHz frequency band, this limit increasing logarithmically with frequencies above 75 MHz as shown in Appendix 2 to this Regulation. In the 400 to 1,000 MHz frequency band the limit remains constant at 43 dB microvolts/m.

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6.2.2.2.

If measurements are made using the method described in Annex 4 using a vehicle-to-antenna spacing of 3.0 ± 0.05 m, the limits shall be 42 dB microvolts/m in the 30 to 75 MHz frequency band and 42 to 53 dB microvolts/m in the 75 to 400 MHz frequency band, this limit increasing logarithmically with frequencies above 75 MHz as shown in Appendix 3 to this Regulation. In the 400 to 1,000 MHz frequency band the limit remains constant at 53 dB microvolts/m.

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6.2.2.3. On the vehicle representative of its type, the measured values, expressed in dB microvolts/m shall be below the type approval limits. a0c0
6.3. Specifications concerning narrowband electromagnetic radiation from vehicles a0c0
6.3.1. Method of measurement a0c0
... The electromagnetic radiation generated by the vehicle representative of its type shall be measured using the method described in Annex 5. These shall be defined by the vehicle manufacturer in accordance with the Technical Service. a0c0
6.3.2. Vehicle narrowband type approval limits a0c0
6.3.2.1.

If measurements are made using the method described in Annex 5 using a vehicle-to-antenna spacing of 10.0 ± 0.2 m, the limits shall be 22 dB microvolts/m in the 30 to 75 MHz frequency band and 22 to 33 dB microvolts/m in the 75 to 400 MHz frequency band, this limit increasing logarithmically with frequencies above 75 MHz as shown in Appendix 4 to this Regulation. In the 400 to 1,000 MHz frequency band the limit remains constant at 33 dB microvolts/m.

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6.3.2.2.

If measurements are made using the method described in Annex 5 using a vehicle-to-antenna spacing of 3.0 ± 0.05 m, the limit shall be 32 dB microvolts/m in the 30 to 75 MHz frequency band and 32 to 43 dB microvolts/m in the 75 to 400 MHz frequency band, this limit increasing logarithmically with frequencies above 75 MHz as shown in Appendix 5 to this Regulation. In the 400 to 1,000 MHz frequency band the limit remains constant at 43 dB microvolts/m.

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6.3.2.3. On the vehicle representative of its type, the measured values, expressed in dB microvolts/m, shall be below the type approval limit. a0c0
6.3.2.4. Notwithstanding the limits defined in paragraphs 6.3.2.1., 6.3.2.2. and 6.3.2.3. of this Regulation, if, during the initial step described in paragraph 1.3. of Annex 5, the signal strength measured at the vehicle broadcast radio antenna is less than 20 dB micro-volts over the frequency range 76 to 108 MHz measured with an average detector, then the vehicle shall be deemed to comply with the limits for narrowband emissions and no further testing will be required. a0c0
6.4. Specifications concerning immunity of vehicles to electromagnetic radiation a0c0
6.4.1. Method of testing a0c0
... The immunity to electromagnetic radiation of the vehicle representative of its type shall be tested by the method described in Annex 6. a0c0
6.4.2. Vehicle immunity type approval limits a0c0
6.4.2.1. If tests are made using the method described in Annex 6, the field strength shall be 30 volts/m rms (root mean squared) in over 90 per cent of the 20 to 2,000 MHz frequency band and a minimum of 25 volts/m rms over the whole 20 to 2,000 MHz frequency band. a0c0
6.4.2.2. The vehicle representative of its type shall be considered as complying with immunity requirements if, during the tests performed in accordance with Annex 6, there shall be no degradation of performance of "immunity related functions", according to paragraph 2.1. of Annex 6. a0c0
6.5. Specification concerning broadband electromagnetic interference generated by ESAs a0c0
6.5.1. Method of measurement a0c0
... The electromagnetic radiation generated by the ESA representative of its type shall be measured by the method described in Annex 7. a0c0
6.5.2. ESA broadband type approval limits a0c0
6.5.2.1. If measurements are made using the method described in Annex 7, the limits shall be 62 to 52 dB microvolts/m in the 30 to 75 MHz frequency band, this limit decreasing logarithmically with frequencies above 30 MHz, and 52 to 63 dB microvolts/m in the 75 to 400 MHz band, this limit increasing logarithmically with frequencies above 75 MHz as shown in Appendix 6 to this Regulation. In the 400 to 1,000 MHz frequency band the limit remains constant at 63 dB microvolts/m. a0c0
6.5.2.2. On the ESA representative of its type, the measured values, expressed in dB microvolts/m, shall be below the type approval limits. a0c0
6.6. Specifications concerning narrowband electromagnetic interference generated by ESAs a0c0
6.6.1. Method of measurement a0c0
... The electromagnetic radiation generated by the ESA representative of its type shall be measured by the method described in Annex 8. a0c0
6.6.2. ESA narrowband type approval limits a0c0
6.6.2.1. If measurements are made using the method described in Annex 8, the limits shall be 52 to 42 dB microvolts/m in the 30 to 75 MHz frequency band, this limit decreasing logarithmically with frequencies above 30 MHz, and 42 to 53 dB microvolts/m in the 75 to 400 MHz band, this limit increasing logarithmically with frequencies above 75 MHz as shown in Appendix 7. In the 400 to 1,000 MHz frequency band the limit remains constant at 53 dB microvolts/m. a0c0
6.6.2.2. On the ESA representative of its type, the measured value, expressed in dB microvolts/m shall be below the type approval limits. a0c0
6.7. Specifications concerning the emission of transient conducted disturbances generated by ESAs on 12/24 V supply lines a0c0
6.7.1. Method of testing
The emission of ESA representative of its type shall be tested by the method(s) according to ISO 7637-2 as described in Annex 10 for the levels given in Table 1.
a0c0
... Table 1
Maximum allowed pulse amplitude
a0c0
... a0c0
6.8. Specifications concerning immunity of ESAs to electromagnetic radiation a0c0
6.8.1. Method(s) of testing a0c0
... The immunity to electromagnetic radiation of the ESA representative of its type shall be tested by the method(s) chosen from those described in Annex 9. a0c0
6.8.2. ESA immunity type approval limits a0c0
6.8.2.1. If tests are made using the methods described in Annex 9, the immunity test levels shall be 60 volts/m root-mean-square (rms) for the 150 mm stripline testing method, 15 volts/m rms for the 800 mm stripline testing method, 75 volts/m rms for the Transverse Electromagnetic Mode (TEM) cell testing method, 60 mA rms for the bulk current injection (BCI) testing method and 30 volts/m rms for the free field testing method in over 90 per cent of the 20 to 2,000 MHz frequency band, and to a minimum of 50 volts/m rms for the 150 mm stripline testing method, 12.5 volts/m rms for the 800 mm stripline testing method, 62.5 volts/m rms, for the TEM cell testing method, 50 mA rms for the bulk current injection (BCI) testing method and 25 volts/m rms for the free field testing method over the whole 20 to 2,000 MHz frequency band. a0c0
6.8.2.2. The ESA representative of its type shall be considered as complying with immunity requirements if, during the tests performed in accordance with Annex 9, there shall be no degradation of performance of "immunity related functions". a0c0
6.9. Specifications concerning the immunity of ESAs to transient disturbances conducted along 12/24 V supply lines a0c0
6.9.1. Method of testing a0c0
... The immunity of ESA representative of this type shall be tested by the method(s) according to ISO 7637-2 as described in Annex 10 with the test levels given in Table 2. a0c0
... Table 2
Immunity of ESA
a0c0
...
Test pulse number Immunity test level Functional status for systems:
Related to immunity related functions Not related to immunity related functions
1 III C D
2a III B D
2b III C D
3a/3b III A D
4 III B
(for ESA which shall be operational during engine start phases)
C
(for other ESA)
D
a0c0
6.10. Exceptions a0c0
6.10.1. Where a vehicle or electrical/electronic system or ESA does not include an electronic oscillator with an operating frequency greater than 9 kHz, it shall be deemed to comply with paragraph 6.3.2. or 6.6.2. and with Annexes 5 and 8. a0c0
6.10.2. Vehicles which do not have electrical/electronic systems with "immunity related functions" need not be tested for immunity to radiated disturbances and shall be deemed to comply with paragraph 6.4. and with Annex 6 to this Regulation. a0c0
6.10.3. ESAs with no immunity related functions need not be tested for immunity to radiated disturbances and shall be deemed to comply with paragraph 6.8. and with Annex 9 to this Regulation. a0c0
6.10.4. Electrostatic discharge a0c0
... For vehicles fitted with tyres, the vehicle body/chassis can be considered to be an electrically isolated structure. Significant electrostatic forces in relation to the vehicle's external environment only occur at the moment of occupant entry into or exit from the vehicle. As the vehicle is stationary at these moments, no type approval test for electrostatic discharge is deemed necessary. a0c0
6.10.5. Emission of transient conducted disturbances generated by ESAs on 12/24 V supply lines. a0c0
... ESAs that are not switched, contain no switches or do not include inductive load need not be tested for transient conducted emission and shall be deemed to comply with paragraph 6.7. a0c0
6.10.6. The loss of function of receivers during the immunity test, when the test signal is within the receiver bandwidth (RF exclusion band) as specified for the specific radio service/product in the harmonized international EMC standard, does not necessarily lead to fail criteria. a0c0
6.10.7. RF transmitters shall be tested in the transmit mode. Wanted emissions (e.g. from RF transmitting systems) within the necessary bandwidth and out of band emissions are disregarded for the purpose of this Regulation. Spurious emissions are subject to this Regulation. a0c0
6.10.7.1. "Necessary bandwidth": For a given class of emission, the width of the frequency band which is just sufficient to ensure the transmission of information at the rate and with the quality required under specified conditions (Article 1, No. 1.152 of the International Telecommunication Union (ITU) Radio Regulations). a0c0
6.10.7.2. "Out-of-band Emissions": Emission on a frequency or frequencies immediately outside the necessary bandwidth which results from the modulation process, but excluding spurious emissions (Article 1, No. 1.144 of the ITU Radio Regulations). a0c0
6.10.7.3. "Spurious emission": In every modulation process additional undesired signals exist. They are summarized under the expression "spurious emissions". Spurious emissions are emissions on a frequency or frequencies, which are outside the necessary bandwidth and the level of which may be reduced without affecting the corresponding transmission of information. Spurious emissions include harmonic emissions, parasitic emissions, intermodulation products and frequency conversion products, but exclude out-of-band emissions (Article 1 No. 1.145 of the ITU Radio Regulations). a0c0
7. Additional specifications in the configuration "REESS charging mode coupled to the power grid" a0c0
7.1. General specifications a0c0
7.1.1. A vehicle and its electrical/electronic system(s) or ESA(s) shall be so designed, constructed and fitted as to enable the vehicle, in configuration "REESS charging mode coupled to the power grid", to comply with the requirements of this Regulation. a0c0
7.1.1.1. A vehicle in configuration "REESS charging mode coupled to the power grid" shall be tested for radiated emissions, immunity to radiated disturbances, conducted emissions and immunity to conducted disturbances. a0c0
7.1.1.2. ESAs in configuration "REESS charging mode coupled to the power grid" shall be tested for radiated and conducted emissions, for immunity to radiated and conducted disturbances. a0c0
7.1.2. Before testing the Technical Service has to prepare a test plan in conjunction with the manufacturer, for the configuration "REESS charging mode coupled to the power grid" configuration which contains at least mode of operation, stimulated function(s), monitored function(s), pass/fail criterion (criteria) and intended emissions. a0c0
7.1.3. A vehicle in configuration "REESS charging mode coupled to the power grid" should be tested with the charging cable delivered by the manufacturer. In this case, the cable shall be type approved as part of the vehicle. a-1c0
7.1.4. Artificial networks a0c0
...

AC Power mains shall be applied to the vehicle / ESA through 50 µH/50Ω AN(s) as defined in CISPR 16-1-2 paragraph 4.3.

a-1c0
...

DC Power mains shall be applied to the vehicle / ESA through 5 µH/50Ω DC-charging-AN(s) as defined in Appendix 8 clause 3 [#new]

a0c0
...

High voltage power line shall be applied to the ESA through a 5  µH/50Ω HV-AN(s) as defined in Appendix 8 clause 2. [#new]

a0c0
7.2. Specifications concerning broadband electromagnetic radiation from vehicles a0c0
7.2.1. Method of measurement a0c0
... The electromagnetic radiation generated by the vehicle representative of its type shall be measured using the method described in Annex 4. The method of measurement shall be defined by the vehicle manufacturer in accordance with the Technical Service. a0c0
7.2.2. Vehicle broadband type approval limits a0c0
7.2.2.1.

If measurements are made using the method described in Annex 4 using a vehicle-to-antenna spacing of 10.0 ± 0.2 m, the limits shall be 32 dB microvolts/m in the 30 to 75 MHz frequency band and 32 to 43 dB microvolts/m in the 75 to 400 MHz frequency band, this limit increasing logarithmically with frequencies above 75 MHz as shown in Appendix 2. In the 400 to 1,000 MHz frequency band the limit remains constant at 43 dB microvolts/m.

a0c0
7.2.2.2.

If measurements are made using the method described in Annex 4 using a vehicle-to-antenna spacing of 3.0 ± 0.05 m, the limits shall be 42 dB microvolts/m in the 30 to 75 MHz frequency band and 42 to 53 dB microvolts/m in the 75 to 400 MHz frequency band, this limit increasing logarithmically with frequencies above 75 MHz as shown in Appendix 3. In the 400 to 1,000 MHz frequency band the limit remains constant at 53 dB microvolts/m.

a0c0
... On the vehicle representative of its type, the measured values, expressed in dB microvolts/m shall be below the type approval limits. a0c0
7.3. Specifications concerning emission of harmonics on AC power lines from vehicles a0c0
7.3.1. Method of measurement a0c0
... The harmonics emission on AC power lines generated by the vehicle representative of its type shall be measured using the method described in Annex 11. The method of measurement shall be defined by the vehicle manufacturer in accordance with the Technical Service. a0c0
7.3.2. Vehicle type approval limit a0c0
7.3.2.1. If measurements are made using the method described in Annex 11, the limits for input current ≤ 16 A per phase are those defined in IEC 61000-3-2 and given in Table 3. a0c0
... Table 3
Maximum allowed harmonics (input current ≤ 16 A per phase)
a0c0
... a0c0
7.3.2.2. If measurements are made using the method described in Annex 11, the limits for input current > 16 A and ≤ 75 A per phase are those defined in IEC 61000-3-12, and given in given in Table 4, Table 5 and Table 6. a0c0
.

Table 4
Maximum allowed harmonics (input current > 16 A and ≤ 75 A per phase) for single phase or other than balanced three-phase equipment

a0c0
... a0c0
... [table 4]: Relative values of even harmonics lower or equal to 12 shall be lower than 16/n %. Even harmonics greater than 12 are taken into account in the Total Harmonic Distorsion (THD) and Partial Weighted Harmonic Distorsion (PWHD) the same way than odd harmonics. Linear interpolation between successive values of Short Circuit Ratio of an Equipment (Rsce) is authorized. a0c0
...

Table 5
Maximum allowed harmonics (input current > 16 A and 75 A per phase) for balanced three-phase equipment

a0c0
... a0c0
... [table 5] Relative values of even harmonics lower or equal to 12 shall be lower than 16/n %. Even harmonics greater than 12 are taken into account in the THD and PWHD the same way than odd harmonics. Linear interpolation between successive values of Rsce is authorized. a0c0
...

Table 6
Maximum allowed harmonics (input current > 16 A and ≤ 75 A per phase) for balanced three-phase equipment under specific conditions

a0c0
... a0c0
... Relative values of even harmonics lower or equal to 12 shall be lower than 16/n %. Even harmonics greater than 12 are taken into account in the THD and PWHD the same way than odd harmonics a0c0
7.4. Specifications concerning emission of voltage changes, voltage fluctuations and flicker on AC power lines from vehicles. a0c0
7.4.1. Method of measurement a0c0
... The emission of voltage changes, voltage fluctuations and flicker on AC power lines generated by the vehicle representative of its type shall be measured using the method described in Annex 12. The method of measurement shall be defined by the vehicle manufacturer in accordance with the Technical Service. a0c0
7.4.2. Vehicle type approval limit a0c0
7.4.2.1. If measurements are made using the method described in Annex 12, the limits for rated current ≤ 16 A per phase and not subjected to conditional connection are those defined in IEC 61000-3-3, paragraph 5. a-1c0
7.4.2.2. If measurements are made using the method described in Annex 12, the limits for rated current > 16 A and ≤ 75 A per phase and subjected to conditional connection are those defined in IEC 61000-3-11, paragraph 5. a-1c0
7.5. Specifications concerning emission of radiofrequency conducted disturbances on AC or DC power lines from vehicles a0c0
7.5.1. Method of measurement a0c0
... The emission of radiofrequency conducted disturbances on AC or DC power lines generated by the vehicle representative of its type shall be measured using the method described in Annex 13. The method of measurement shall be defined by the vehicle manufacturer in accordance with the Technical Service. a0c0
7.5.2. Vehicle type approval limit a0c0
7.5.2.1. If measurements are made using the method described in Annex 13, the limits on AC power lines are those defined in IEC 61000-6-3 and given in Table 7. a0c0
... Table 7
Maximum allowed radiofrequency conducted disturbances on AC power lines
a0c0
... a0c0
7.5.2.2. If measurements are made using the method described in Annex 13, the limits on DC power lines are those defined in IEC 61000-6-3 and given in Table 8. a0c0
... Table 8
Maximum allowed radiofrequency conducted disturbances on DC power lines
a0c0
... a0c0
7.6. Specifications concerning emission of radiofrequency conducted disturbances on wired network port from vehicles [#new] a0c0
7.6.1. Method of measurement a0c0
... The emission of radiofrequency conducted disturbances on wired network port generated by the vehicle representative of its type shall be measured using the method described in Annex 14. The method of measurement shall be defined by the vehicle manufacturer in accordance with the Technical Service. [#new] a0c0
7.6.2. Vehicle type approval limit a0c0
7.6.2.1. If measurements are made using the method described in Annex 14, the limits on wired network port are those defined in IEC 61000-6-3 and given in Table 9. a0c0
... Table 9
Maximum allowed radiofrequency conducted disturbances wired network port
a0c0
... a0c0
7.7. Specifications concerning immunity of vehicles to electromagnetic radiation a0c0
7.7.1. Method of testing a0c0
... The immunity to electromagnetic radiation of the vehicle representative of its type shall be tested by the method described in Annex 6. a0c0
7.7.2. Vehicle immunity type approval limits a0c0
7.7.2.1. If tests are made using the method described in Annex 6, the field strength shall be 30 volts/m rms (root mean squared) in over 90 per cent of the 20 to 2,000 MHz frequency band and a minimum of 25 volts/m rms over the whole 20 to 2,000 MHz frequency band. a0c0
7.7.2.2. The vehicle representative of its type shall be considered as complying with immunity requirements if, during the tests performed in accordance with Annex 6, there shall be no degradation of performance of "immunity related functions", according to paragraph 2.2. of Annex 6. a0c0
7.8. Specifications concerning the immunity of vehicles to Electrical Fast Transient/Burst disturbances conducted along AC and DC power lines. a0c0
7.8.1. Method of testing a0c0
7.8.1.1. The immunity to Electrical Fast Transient/Burst disturbances conducted along AC and DC power lines of the vehicle representative of its type shall be tested by the method described in Annex 15. a0c0
7.8.2. Vehicle immunity type approval limits a0c0
7.8.2.1.

If tests are made using the methods described in Annex 15, the immunity test levels, for AC or DC power lines, shall be: ±2 kV test voltage in open circuit, with a rise time (Tr) of 5 ns, and a hold time (Th) of 50 ns and a repetition rate of 5 kHz for at least 1 minute.

a0c0
7.8.2.2. The vehicle representative of its type shall be considered as complying with immunity requirements if, during the tests performed in accordance with Annex 15, there shall be no degradation of performance of "immunity related functions", according to paragraph 2.2. of Annex 6. a0c0
7.9. Specifications concerning the immunity of vehicles to surge conducted along AC or DC power lines. a0c0
7.9.1. Method of testing a0c0
7.9.1.1. The immunity to surge conducted along AC/DC power lines of the vehicle representative of its type shall be tested by the method described in Annex 16. a0c0
7.9.2. Vehicle immunity type approval limits a0c0
7.9.2.1. If tests are made using the methods described in Annex 16, the immunity test levels shall be: a0c0
...

(a) For AC power lines: ±2 kV test voltage in open circuit between line and earth and ±1 kV between lines (pulse 1.2 µs / 50 µs), with a rise time (Tr) of 1.2 µs, and a hold time (Th) of 50µs. Each surge shall be applied five times with a maximum delay of 1 minute between each pulse. This has to be applied for the following phases: 0, 90, 180 and 270 ,

a0c0
...

(b) For DC power lines: ±0.5 kV test voltage in open circuit between line and earth and ±0.5 kV between lines (pulse 1.2 µs / 50 µs) with a rise time (Tr) of 1.2 µs, and a hold time (Th) of 50µs. Each surge shall be applied five times with a maximum delay of 1 minute.

a0c0
7.9.2.2. The vehicle representative of its type shall be considered as complying with immunity requirements if, during the tests performed in accordance with Annex 16, there shall be no degradation of performance of "immunity related functions", according to paragraph 2.2. of Annex 6. a0c0
7.10. Specifications concerning broadband electromagnetic interference caused by ESAs a0c0
7.10.1. Method of measurement a0c0
... The electromagnetic radiation generated by the ESA representative of its type shall be measured by the method described in Annex 7. a0c0
7.10.2. ESA broadband type approval limits a0c0
7.10.2.1. If measurements are made using the method described in Annex 7, the limits shall be 62 to 52 dB V/m in the 30 to 75 MHz frequency band, this limit decreasing logarithmically with frequencies above 30 MHz, and 52 to 63 dB V/m in the 75 to 400 MHz band, this limit increasing logarithmically with frequencies above 75 MHz as shown in Appendix 6. In the 400 to 1,000 MHz frequency band the limit remains constant at 63 dB V/m. a0c0
7.10.2.2. On the ESA representative of its type, the measured values, expressed in dB V/m, shall be below the type approval limits. a0c0
7.11. Specifications concerning emission of harmonics on AC power lines from ESAs a0c0
7.11.1. Method of measurement a0c0
... The harmonics emission on AC power lines generated by the ESA representative of its type shall be measured using the method described in Annex 17. The method of measurement shall be defined by the manufacturer in accordance with the Technical Service. a0c0
7.11.2. ESA type approval limit a0c0
7.11.2.1. If measurements are made using the method described in Annex 17, the limits for input current ≤ 16 A per phase are those defined in IEC 61000-3-2 and given in Table 10. a0c0
...

Table 10
Maximum allowed harmonics (input current ≤ 16 A per phase)

a0c0
... a0c0
7.11.2.2. If measurements are made using the method described in Annex 17, the limits for input current > 16 A and ≤ 75 A per phase are those defined in IEC 61000-3-12 and given in Table 11, Table 12 and Table 13. a0c0
...

Table 11
Maximum allowed harmonics (input current > 16 A and ≤ 75 A per phase) for single phase or other than balanced three-phase equipment.

a0c0
... a0c0
... [table 11] Relative values of even harmonics lower or equal to 12 shall be lower than 16/n %. Even harmonics greater than 12 are taken into account in the THD and PWHD in the same way than odd harmonics.
Linear interpolation between successive values of Rsce is authorized.
a0c0
...

Table 12
Maximum allowed harmonics (input current > 16 A and ≤ 75 A per phase) for balanced three-phase equipment.

a0c0
... a0c0
... [table 12] Relative values of even harmonics lower or equal to 12 shall be lower than 16/n %. Even harmonics greater than 12 are taken into account in the THD and PWHD in the same way as odd harmonics.
Linear interpolation between successive values of Rsce is authorized.
a0c0
...

Table 13
Maximum allowed harmonics (input current > 16 A and ≤ 75 A per phase) for balanced three-phase equipment under specific conditions

a0c0
... a0c0
... [table 13] Relative values of even harmonics lower or equal to 12 shall be lower than 16/n %. Even harmonics greater than 12 are taken into account in the THD and PWHD in the same way as odd harmonics. a0c0
7.12. Specifications concerning emission of voltage changes, voltage fluctuations and flicker on AC power lines from ESAs a0c0
7.12.1. Method of measurement a0c0
... The emission of voltage changes, voltage fluctuations and flicker on AC power lines generated by the ESA representative of its type shall be measured using the method described in Annex 18. The method of measurement shall be defined by the ESA manufacturer in accordance with the Technical Service. a0c0
7.12.2. ESA type approval limit a0c0
7.12.2.1. If measurements are made using the method described in Annex 18, the limits for rated current ≤ 16 A per phase and not subjected to conditional connection are those defined in IEC 61000-3-3, paragraph 5. a0c0
7.12.2.2. If measurements are made using the method described in Annex 18, the limits for rated current > 16 A and ≤ 75 A per phase and subjected to conditional connection are those defined in IEC 61000-3-11, paragraph 5. a0c0
7.13. Specifications concerning emission of radiofrequency conducted disturbances on AC or DC power lines from ESA a0c0
7.13.1. Method of measurement a0c0
... The emission of radiofrequency conducted disturbances on AC or DC power lines generated by the ESA representative of its type shall be measured using the method described in Annex 19. The method of measurement shall be defined by the ESA manufacturer in accordance with the Technical Service. a0c0
7.13.2. ESA type approval limit a0c0
7.13.2.1. If measurements are made using the method described in Annex 19, the limits on AC power lines are those defined in IEC 61000-6-3 and given in Table 14. a0c0
... Table 14
Maximum allowed radiofrequency conducted disturbances on AC power lines
a0c0
... a0c0
7.13.2.2. If measurements are made using the method described in Annex 19, the limits on DC power lines are those defined in IEC 61000-6-3 and given in Table 15. a0c0
... Table 15
Maximum allowed radiofrequency conducted disturbances on DC power lines
a0c0
... a0c0
7.14. Specifications concerning emission of radiofrequency conducted disturbances wired network port from ESA a0c0
7.14.1. Method of measurement a0c0
... The emission of radiofrequency conducted disturbances wired network port generated by the ESA representative of its type shall be measured using the method described in Annex 20. The method of measurement shall be defined by the ESA manufacturer in accordance with the Technical Service. a0c0
7.14.2. ESA type approval limit a0c0
7.14.2.1. If measurements are made using the method described in Annex 20, the limits wired network port are those defined in IEC 61000-6-3 and given in Table 16. a0c0
... Table 16
Maximum allowed radiofrequency conducted disturbances wired network port
a0c0
... a0c0
7.15. Specifications concerning the immunity of ESAs to electrical fast transient/burst disturbances conducted along AC and DC power lines. a0c0
7.15.1. Method of testing a0c0
7.15.1.1. The immunity to Electrical Fast Transient/Burst disturbances conducted along AC and DC power lines of the ESA representative of its type shall be tested by the method described in Annex 21. a0c0
7.15.2. ESA immunity type approval limits a0c0
7.15.2.1.

If tests are made using the methods described in Annex 21, the immunity test levels, for AC or DC power lines, shall be: ± 2 kV test voltage in open circuit, with a rise time (Tr) of 5 ns, and a hold time (Th) of 50 ns and a repetition rate of 5 kHz for at least 1 minute.

a0c0
7.15.2.2. The ESA representative of its type shall be considered as complying with immunity requirements if, during the tests performed in accordance with Annex 21, there shall be no degradation of performance of "immunity related functions", according to paragraph 2.2. of Annex 9. a0c0
7.16. Specifications concerning the immunity of ESAs to surge conducted along AC or DC power lines a0c0
7.16.1. Method of testing a0c0
7.16.1.1. The immunity to surge conducted along AC / DC power lines of the ESA representative of its type shall be tested by the method described in Annex 22. a0c0
7.16.2. ESA immunity type approval limits a0c0
7.16.2.1. If tests are made using the methods described in Annex 22, the immunity test levels shall be: a0c0
...

(a) For AC power lines: ±2 kV test voltage in open circuit between line and earth and ±1 kV between lines (pulse 1.2 µs / 50 µs), with a rise time (Tr) of 1.2 µs, and a hold time (Th) of 50 µs. Each surge shall be applied five times with a maximum delay of 1 minute between each pulse. This has to be applied for the following phases: 0, 90, 180 and 270 ,

a0c0
...

(b) For DC power lines: ±0.5 kV test voltage in open circuit between line and earth and ±0.5 kV between lines (pulse 1.2 µs / 50 µs) with a rise time (Tr) of 1.2 µs, and a hold time (Th) of 50 µs. Each surge shall be applied five times with a maximum delay of 1 minute.

a0c0
7.16.2.2. The ESA representative of its type shall be considered as complying with immunity requirements if, during the tests performed in accordance with Annex 22, there shall be no degradation of performance of "immunity related functions", according to paragraph 2.2. of Annex 9. a0c0
7.17. Specifications concerning the emission of transient conducted disturbances generated by ESAs on 12 / 24 V supply lines a0c0
7.17.1. Method of testing a0c0
... The emission of ESA representative of its type shall be tested by the method(s) according to ISO 7637-2, as described in Annex 10 for the levels given in Table 17. a0c0
... Table 17
Maximum allowed pulse amplitude
a0c0
... a0c0
7.18. Specifications concerning immunity of ESAs to electromagnetic radiation a0c0
7.18.1. Method(s) of testing a0c0
... The immunity to electromagnetic radiation of the ESA representative of its type shall be tested by the method(s) chosen from those described in Annex 9. a0c0
7.18.2. ESA immunity type approval limits a0c0
7.18.2.1. If tests are made using the methods described in Annex 9, the immunity test levels shall be 60 volts/m rms for the 150 mm stripline testing method, 15 volts/m rms for the 800 mm stripline testing method, 75 volts/m rms for the Transverse Electromagnetic Mode (TEM) cell testing method, 60 mA rms for the Bulk Current Injection (BCI) testing method and 30 volts/m rms for the free field testing method in over 90 per cent of the 20 to 2,000 MHz frequency band, and to a minimum of 50 volts/m rms for the 150 mm stripline testing method, 12.5 volts/m rms for the 800 mm stripline testing method, 62.5 volts/m rms, for the TEM cell testing method, 50 mA rms for the bulk current injection (BCI) testing method and 25 volts/m rms for the free field testing method over the whole 20 to 2,000 MHz frequency band. a0c0
7.18.2.2. The ESA representative of its type shall be considered as complying with immunity requirements if, during the tests performed in accordance with Annex 9, there shall be no degradation of performance of "immunity related functions". a0c0
7.19. Specifications concerning the immunity of ESAs to transient disturbances conducted along 12 / 24 V supply lines. a0c0
7.19.1 Method of testing a0c0
... The immunity of ESA representative of its type shall be tested by the method(s) according to ISO 7637-2, as described in Annex 10 with the test levels given in Table 18. a0c0
... Table 18
Immunity of ESA [#new: Impulse 4 deleted]
a0c0
... a0c0
7.20. Exceptions a0c0
7.20.1. When there is no direct connection to a wired network which includes telecommunication service additional to the charging communication service, Annex 14 and Annex 20 shall not apply. a0c0
7.20.2. When wired network port of the vehicle uses power line Transmission (PLT) on its AC/DC power lines, Annex 14 shall not apply. a0c0
7.20.3. When wired network port of the ESA uses Power Line Transmission (PLT) on its AC/DC power lines, Annex 20 shall not apply. a0c0
7.20.4. Vehicles and / or ESA which are intended to be used in "REESS charging mode coupled to the power grid" in the configuration connected to a DC-charging station with a length of a DC network cable shorter than 30 m do not have to fulfil the requirements of Annex 13, Annex 15, Annex 16, Annex 19, Annex 21 and Annex 22. a-1c0
... In this case, the manufacturer shall provide a statement that the vehicle and/or ESA can be used in "REESS charging mode coupled to the power grid" only with cables shorter than 30 m. This information shall be made publicly available following the type approval. a0c0
7.20.5. Vehicles and / or ESA which are intended to be used in "REESS charging mode coupled to the power grid" in the configuration connected to a local / private DC-charging station without additional participants do not have to fulfil requirements of paragraphs 7.5., 7.8., 7.9., 7.13., 7.15., 7.16. [#new] a0c0
... In this case, the manufacturer shall provide a statement that the vehicle and / or ESA can be used in "REESS charging mode coupled to the power grid" only with a local/private DC charging station without additional participants. This information shall be made publicly available following the type approval. a0c0
8. Amendment or extension of a vehicle type approval following electrical/electronic sub-assembly (ESA) addition or substitution a0c0
8.1. Where a vehicle manufacturer has obtained type approval for a vehicle installation and wishes to fit an additional or substitutional electrical/electronic system or ESA which has already received approval under this Regulation, and which will be installed in accordance with any conditions attached thereto, the vehicle approval may be extended without further testing. The additional or substitutional electrical/electronic system or ESA shall be considered as part of the vehicle for conformity of production purposes. a0c0
8.2. Where the additional or substitution part(s) has (have) not received approval pursuant to this Regulation, and if testing is considered necessary, the whole vehicle shall be deemed to conform if the new or revised part(s) can be shown to conform to the relevant requirements of paragraph 6. and, if applicable, of paragraph 7. or if, in a comparative test, the new part can be shown not to be likely to adversely affect the conformity of the vehicle type. a0c0
8.3. The addition by a vehicle manufacturer to an approved vehicle of standard domestic or business equipment, other than mobile communication equipment, which conforms to other Regulations, and the installation, substitution or removal of which is according to the recommendations of the equipment and vehicle manufacturers, shall not invalidate the vehicle approval. This shall not preclude vehicle manufacturers fitting communication equipment in accordance with suitable installation guidelines developed by the vehicle manufacturer and/or manufacturer(s) of such communication equipment. The vehicle manufacturer shall provide evidence (if requested by the test authority) that vehicle performance is not adversely affected by such transmitters. This can be a statement that the power levels and installation are such that the immunity levels of this Regulation offer sufficient protection when subject to transmission alone i.e. excluding transmission in conjunction with the tests specified in paragraph 6. This Regulation does not authorize the use of a communication transmitter when other requirements on such equipment or its use apply. a0c0
9. Conformity of production a0c0
... The conformity of production procedures shall comply with those set out in the Agreement, Appendix 2 (E/ECE/324-E/ECE/TRANS/505/Rev.2), with the following requirements: a0c0
9.1. Vehicles or components or ESAs approved under this Regulation shall be so manufactured as to conform to the type approved by meeting the requirements set forth in paragraph 6. and, if applicable, in paragraph 7. above. a0c0
9.2. Conformity of production of the vehicle or component or separate technical unit shall be checked on the basis of the data contained in the communication form(s) for type approval set out in Annex 3A and/or 3B to this Regulation. a0c0
9.3. If the Type Approval Authority is not satisfied with the checking procedure of the manufacturer, then paragraphs 9.3.1., 9.3.2. and 9.3.3. below shall apply. a0c0
9.3.1. When the conformity of a vehicle, component or ESA taken from the series is being verified, production shall be deemed to conform to the requirements of this Regulation in relation to broadband electromagnetic disturbances and narrowband electromagnetic disturbances if the levels measured do not exceed by more than 4 dB (60 per cent) the reference limits prescribed in paragraphs 6.2.2.1., 6.2.2.2., 6.3.2.1., 6.3.2.2. and, if applicable, paragraphs 7.2.2.1. and 7.2.2.2. for vehicles and paragraphs 6.5.2.1., 6.6.2.1., and, if applicable, paragraph 7.10.2.1. above for ESAs (as appropriate). a0c0
9.3.2. When the conformity of a vehicle, component or ESA taken from the series is being verified, production shall be deemed to conform to the requirements of this Regulation in relation to immunity to electromagnetic radiation if the vehicle ESA does not exhibit any degradation relating to the direct control of the vehicle which could be observed by the driver or other road user when the vehicle is in the state defined in Annex 6, paragraph 4., and is subjected to a field strength, expressed in Volts/m, up to 80 per cent of the reference limits prescribed in paragraph 6.4.2.1., and, if applicable, paragraph 7.7.2.1. for vehicles and paragraph 6.8.2.1. and, if applicable, paragraph 7.18.2.1. for ESAs above. a0c0
9.3.3. If the conformity of a component, or Separate Technical Unit (STU) taken from the series is being verified, production shall be deemed to conform to the requirements of this Regulation in relation to immunity to conducted disturbances and emission if the component or STU shows no degradation of performance of "immunity related functions" up to levels given in paragraph 6.9.1. and, if applicable, paragraph 7.19.1., and does not exceed the levels given in paragraph 6.7.1. and, if applicable, paragraph 7.17.1. above. a0c0
10. Penalties for non-conformity of production a0c0
10.1. The approval granted in respect of a type of vehicle, component or separate technical unit pursuant to this Regulation may be withdrawn if the requirements laid down in paragraph 6. and, if applicable, paragraph 7. above are not complied with or if the selected vehicles fail to pass the tests provided for in paragraph 6. and, if applicable, paragraph 7. above. a0c0
10.2. If a Party to the Agreement which applies this Regulation withdraws an approval it has previously granted, it shall forthwith notify the other Contracting Parties applying this Regulation thereof by means of a communication form conforming to the model in Annexes 3A and 3B to this Regulation. a0c0
11. Production definitively discontinued a0c0
... If the holder of an approval permanently ceases to manufacture a type of vehicle or ESA approved in accordance with this Regulation, he shall so inform the Type Approval Authority which granted the approval, which shall in turn notify the other Parties to the 1958 Agreement which apply this Regulation, by means of a communication form conforming to the model in Annexes 3A and 3B to this Regulation. a0c0
12. Modification and extension of type approval of a vehicle or ESA a0c0
12.1. Every modification of the vehicle or ESA type shall be notified to the Type Approval Authority which granted approval of the vehicle type. This Authority may then either: a0c0
12.1.1. Consider that the modifications made are unlikely to have an appreciable adverse effect and that in any case the vehicle or ESA still meets the requirements; or a0c0
12.1.2. Require a further test report from the Technical Service responsible for conducting the tests. a0c0
12.2. Notice of conformation of approval or of refusal of approval, accompanied by particulars of the modifications, shall be communicated by the procedure indicated in paragraph 4. of this Regulation above to the Parties to the Agreement applying this Regulation. a0c0
12.3. The Type Approval Authority granting the approval extension shall assign a serial number to the extension and so notify the other Parties to the 1958 Agreement applying this Regulation by means of a communication form conforming to the models in Annexes 3A and 3B to this Regulation. a0c0
13. Transitional provisions a0c0
13.1. Transitional provisions applicable to the 05 series of amendments a0c0
13.1.1. As from 9 October 2014, no Contracting Party applying this UN Regulation shall refuse to grant or refuse to accept UN type-approvals under this UN Regulation as amended by the 05 series of amendments. a0c0
13.1.2. As from 9 October 2017, Contracting Parties applying this UN Regulation shall not be obliged to accept UN type-approvals to the preceding series of amendments, first issued after 9 October 2017 or extensions thereof. a0c0
13.1.3.

Notwithstanding paragraph 13.1.2., Contracting Parties applying the UN Regulation shall continue to accept UN type-approvals issued according to the preceding series of amendments to the UN Regulation, for the vehicle type which are not equipped with a coupling system to charge the REESS, or for component or separate technical unit which doesn't include a coupling part to charge the REESS which are not affected by the changes introduced by the 05 series of amendments

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13.1.4. Contracting Parties applying this UN Regulation shall not refuse to grant UN type-approvals according to any preceding series of amendments to this UN Regulation or extensions thereof. a0c0
13.2. Transitional provisions applicable to the 06 series of amendments a0c0
13.2.1. As from the official date of entry into force of the 06 series of amendments, no Contracting Party applying this UN Regulation shall refuse to grant or refuse to accept UN type-approvals under this UN Regulation as amended by the 06 series of amendments. a0c0
13.2.2. As from 1 September 2022, Contracting Parties applying this UN Regulation shall not be obliged to accept UN type-approvals to the preceding series of amendments, first issued after 1 September 2022 or extensions thereof. a0c0
13.2.3.

Notwithstanding paragraph 13.2.2., Contracting Parties applying the UN Regulation shall continue to accept UN type-approvals issued according to the preceding series of amendments to the UN Regulation, for the vehicle type which are not equipped with a coupling system to charge the REESS, or for component or separate technical unit which doesn't include a coupling part to charge the REESS which are not affected by the changes introduced by the 05 or 06 series of amendments

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13.2.4. Contracting Parties applying this UN Regulation shall not refuse to grant UN type-approvals according to any preceding series of amendments to this UN Regulation or extensions thereof. a0c0
14. Names and addresses of Technical Services conducting approval tests and of Type Approval Authorities a0c0
... The Parties to the 1958 Agreement applying this Regulation shall communicate to the United Nations Secretariat the names and addresses of the Technical Services conducting approval tests and of the Type Approval Authorities which grant approvals and to which forms certifying approval or extension, refusal or withdrawal of approval, issued in other countries, are to be sent. a0c0
... Appendix 1 a0c0
... List of standards referred to in this Regulation a0c0
1. CISPR 12 "Vehicles', motorboats' and spark-ignited engine-driven devices' radio disturbance characteristics - Limits and methods of measurement", fifth edition 2001 and Amd1: 2005. a0c0
2. CISPR 16-1-4 "Specifications for radio disturbance and immunity measuring apparatus and methods - Part 1: Radio disturbance and immunity measuring apparatus apparatus - Antennas and test sites for radiated disturbances mesaurements", third edition 2010. a0c0
3. CISPR 25 "Limits and methods of measurement of radio disturbance characteristics for the protection of receivers used on board vehicles", second edition 2002 and corrigendum 2004. a0c0
4. ISO 7637-2 "Road vehicles - Electrical disturbance from conduction and coupling - Part 2: Electrical transient conduction along supply lines only on vehicles with nominal 12 V or 24 V supply voltage", second edition 2004. a0c0
5. ISO-EN 17025 "General requirements for the competence of testing and calibration laboratories", second edition 2005 and Corrigendum: 2006. a0c0
6. ISO 11451 "Road vehicles - Electrical disturbances by narrowband radiated electromagnetic energy - Vehicle test methods": a0c0
... Part 1:General and definitions (ISO 11451-1, third edition 2005 and Amd1: 2008); a0c0
... Part 2: Off-vehicle radiation source (ISO 11451-2, fourth edition 2015); [#new] a0c0
... Part 4: Bulk current injection (BCI) (ISO 11451-4, third edition 2013). [#new] a0c0
7. ISO 11452 "Road vehicles - Electrical disturbances by narrowband radiated electromagnetic energy - Component test methods": a0c0
... Part 1: General and definitions (ISO 11452-1, third edition 2005 and Amd1: 2008); a0c0
... Part 2: Absorber-lined chamber (ISO 11452-2, second edition 2004); a0c0
... Part 3: Transverse electromagnetic mode (TEM) cell (ISO 11452-3, third edition 2016); [#new] a0c0
... Part 4: Bulk current injection (BCI) (ISO 11452-4, fourth edition 2011); a0c0
... Part 5: Stripline (ISO 11452-5, second edition 2002). a0c0
8. ITU Radio Regulations, edition 2008. a0c0
9.

IEC 61000-3-2 "Electromagnetic Compatibility (EMC) - Part 3-2 - Limits for harmonic current emissions (equipment input current ≤ 16 A per phase)", edition 3.2 - 2005 + A1: 2008 + A2: 2009.

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10.

IEC 61000-3-3 "Electromagnetic Compatibility (EMC) - Part 3-3 - Limits - Limitation of voltage changes, voltage fluctuations and flicker in public low-voltage systems for equipment with rated current ≤ 16 A per phase and not subjected to conditional connection", edition 2.0 - 2008.

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11.

IEC 61000-3-11 "Electromagnetic Compatibility (EMC) - Part 3-11 - Limits - Limitation of voltage changes, voltage fluctuations and flicker in public low-voltage systems - Equipment with rated current ≤ 75 A per phase and subjected to conditional connection", edition 1.0 - 2000.

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12.

IEC 61000-3-12 "Electromagnetic Compatibility (EMC) - Part 3-12 - Limits for harmonic current emissions produced by equipment connected to public low-voltage systems with input current > 16 A and ≤ 75 A per phase", edition 1.0 - 2004.

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13. IEC 61000-4-4 "Electromagnetic Compatibility (EMC) - Part 4-4 - Testing and measurement techniques - Electrical fast transients/burst immunity test", edition 2.0 - 2004. a0c0
14. IEC 61000-4-5 "Electromagnetic Compatibility (EMC) - Part 4-5 - Testing and measurement techniques - Surge immunity test", edition 2.0 - 2005. a0c0
15. IEC 61000-6-3 "Electromagnetic Compatibility (EMC) - Part 6-3 - Generic standards Emission standard for residential, commercial and light-industrial environments", edition 2.0 - 2006. a0c0
16. CISPR 16-2-1 "Specification for radio disturbances and immunity measuring apparatus and methods - Part 2-1 - Methods of measurement of disturbances and immunity - Conducted disturbances measurement", edition 2.0 - 2008. a0c0
17. CISPR 22 "Information Technology Equipment - Radio disturbances characteristics - Limits and methods of measurement", edition 6.0 - 2008. a0c0
18. CISPR 16-1-2 "Specification for radio disturbance and immunity measuring apparatus and methods - Part 1-2: Radio disturbance and immunity measuring apparatus - Ancillary equipment - Conducted disturbances", edition 1.2: 2006. a0c0
19.

IEC 61851-1 "Electric vehicle conductive charging system - Part 1: General requirements ", edition 3.0 - 2017.

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20.

CISPR 32 "Electromagnetic compatibility of multimedia equipment - Emission requirements", edition 2.0 - 2015. [#new]

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... Appendix 2 a0c0
... Vehicle broadband reference limits - Antenna-vehicle separation: 10 m a0c0
... a0c0
... Appendix 3 a0c0
... Vehicle broadband reference limits - Antenna-vehicle separation: 3 m a0c0
... a0c0
... Appendix 4 a0c0
... Vehicle narrowband reference limits - Antenna-vehicle separation: 10 m a0c0
...

Limit E (dBµV/m) at frequency F (MHz)

30-230 MHz [#new]

230-1,000 MHz [#new]

E = 28 [#new]

E = 35 [#new]

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... a0c0
... Appendix 5 a0c0
... Vehicle narrowband reference limits - Antenna-vehicle separation: 3 m a0c0
...

Limit E (dBµV/m) at frequency F (MHz)

30-230 MHz [#new]

230-1,000 MHz [#new]

E = 38 [#new]

E = 45 [#new]

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... a0c0
... Appendix 6 a0c0
... Electrical/electronic sub-assembly - Broadband reference limits a0c0
... a0c0
... Appendix 7 a0c0
... Electrical/electronic sub-assembly a0c0
... a0c0
... Appendix 8 a0c0
... Artificial networks (AN), High Voltage Artificial Networks (HV-AN), Direct Current charging Artificial Networks (DC-charging-AN), Artificial Mains Networks (AMN) and Asymmetric Artificial Networks (AAN) [#new] a0c0
... This appendix defines the artificial networks for vehicle in charging mode:
-     Artificial networks (AN): used for low voltage power supplies;
-     High Voltage Artificial networks (HV-AN) : used for DC power supplies;
-     Direct Current charging Artificial Networks (DC-charging-AN): used for DC power supplies;
-     Artificial Mains Networks (AMN) : used for AC power mains;
-     Asymmetric artificial network (AAN): used for signal/control port lines and/or wired network port lines.
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1.

Artificial networks (AN)
For an ESA powered by LV, a 5 µH / 50 Ω AN as defined in Figure 1 shall be used.
The AN(s) shall be mounted directly on the ground plane. The grounding connection of the AN(s) shall be bonded to the ground plane.
Measurement ports of AN(s) shall be terminated with a 50 Ω load.
The AN impedance ZPB (tolerance ± 20 %) in the measurement frequency range of 0,1 MHz to 100 MHz is shown in Figure 2. It is measured between the terminals P and B (of Figure 1) with a 50 Ω load on the measurement port with terminals A and B (of Figure 1) short circuited.

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...

Figure 1
Example of 5 mH AN schematic

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... a0c0
... Figure 2
Characteristics of the AN impedance ZPB
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... a0c0
2.

High Voltage Artificial networks (HV-AN)
For an ESA powered by HV, a 5 µH / 50 Ω HV-AN as defined in Figure 3 shall be used.
The HV-AN(s) shall be mounted directly on the ground plane. The grounding connection of the HV-AN(s) shall be bonded to the ground plane.
Measurement ports of HV-AN(s) shall be terminated with a 50 Ω load.
The HV-AN impedance ZPB (tolerance ± 20 %) in the measurement frequency range of 0,1 MHz to 100 MHz is shown in Figure 2. It is measured between the “Vehicle/ESA HV” and “GND” terminals (of Figure 3) with a 50 Ω load on the measurement port and with the “HV supply” and “GND” terminals short circuited

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...

Figure 3
Example of 5 mH HV AN schematic

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... a0c0
...

Figure 4
Example of 5 mH HV AN combination in a single shielded box

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... a0c0
... Figure 5
Impedance matching network attached between HV ANs and ESA
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... a0c0
3.

Direct Current charging Artificial Networks (DC-charging-AN)

For a vehicle in charging mode connected to a DC power supply, a 5 µH / 50 Ω DC-charging-AN as defined in Figure 6 shall be used.
Measurement ports of DC-charging-AN(s) shall be terminated with 50 Ω loads.
The DC-charging-AN impedance ZPB (tolerance ± 20 %) in the measurement frequency range of 0,1 MHz to 100 MHz is shown in Figure 7. It is measured between the terminals “Vehicle/ESA HV” and “GND” (of Figure 6) with a 50 Ω load on the measurement port and with terminals “HV Supply” and “GND” (of Figure 6) short circuited.

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...

Figure 6
Example of 5 mH DC-charging-AN schematic

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... a0c0
... Figure 7
Characteristics of the DC-charging-AN impedance
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... a0c0
4.

Artificial Mains networks (AMN)

For a vehicle in charging mode connected to an AC power mains, a 50 µH / 50 Ω-AMN as defined in CISPR 16-1-2 clause 4.4 shall be used. Measurement ports of AMN(s) shall be terminated with 50 Ω loads.

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5.

Asymmetric artificial network (AAN)

Currently, different technologies for signal/control port lines and/or wired network port lines are used for the communication between charging station and vehicle. Therefore, a distinction between some specific signal/control port lines and/or wired network port lines (for example, control pilot line, CAN lines) is necessary.

Measurement ports of AAN(s) shall be terminated with 50 Ω loads.
AANs that are defined in 5.1., 5.2., 5.3. and 5.4. are used for unshielded signal/control port lines and/or wired network port lines.
If shielded signal/control port lines are used, then shielded AANs defined in CISPR 32:2015 Annex G, Figures G.10 and G.11 should be used.

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5.1.

Signal/Control port with symmetric lines

An asymmetric artificial network (AAN) to be connected between the vehicle and the charging station or any associated equipment (AE) used to simulate communication is defined in CISPR 16-1-2 Annex E clause E.2 (T network circuit) (see example in Figure 8).
The AAN has a common mode impedance of 150 Ω. The impedance Zcat adjusts the symmetry of the cabling and attached periphery typically expressed as longitudinal conversion loss (LCL). The value of LCL should be predetermined by measurements or be defined by the manufacturer of the charging station/charging harness. The selected value for LCL and its origin shall be stated in the test report.
CAN communication is an example of symmetric lines used for vehicle DC charging mode.
If an original charging station can be used for the test, an AAN is not required for CAN communication.
If the CAN communication is emulated and if the presence of the AAN prevents proper CAN communication, then no AAN should be used.

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... Figure 8
Example of an AAN for Signal/Control port with symmetric lines (e.g. CAN)
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... a0c0
5.2. Wired network port with PLC on power lines

If an original charging station can be used for the test, an AAN and/or AMN/DC-charging-AN might not be required for PLC communication.
If the presence of the AMN/DC-charging-AN prevents proper PLC communication with the original charging station or if the PLC communication needs to be simulated by means of a piece of associated equipment (e.g. a PLC modem) instead of the original charging station, it is necessary to add an AAN between the AE (e.g. the PLC modem) and the AMN/DC-charging-AN output (vehicle side), as shown in Figure 9.
The circuit in Figure 9 provides a common mode termination by the AMN / DC-charging-AN HV-AN. In order to minimize emission from the PLC modem of the vehicle, an attenuator is located between the powerline and the PLC modem at the AE side in the circuit for emission tests. This attenuator consists of two resistors in combination with the input/output impedance of the PLC modem. The value of the resistors depends on the design impedance of the PLC modems and the allowed attenuation for the PLC system.
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... a0c0
5.3.

Signal/Control port with PLC (technology) on control pilot

Some communication systems use the control pilot line (versus PE) with a superimposed (high frequency) communication. Typically the technology developed for powerline communication (PLC) is used for that purpose. On one hand the communication lines are operated unsymmetrically, on the other hand two different communication systems operate on the same line. Therefore, a special AAN must be used as defined in Figure 10.
It provides a common mode impedance of 150 Ω ± 20 Ω (150 kHz to 30 MHz) on the control pilot line (assuming a design impedance of the modem of 100 Ω). Both types of communications (control pilot, PLC) are separated by the network. Therefore, typically a communication simulation is used in combination with this network.
The attenuator built by the resistors and the design impedance of the PLC modem makes sure that the signal on the charging harness is dominated by the vehicle’s communication signals rather than the AE PLC modem.
The values of inductance and capacitance in the networks added for PLC on control pilot shown in Figure 10 shall not induce any malfunction of communication between vehicle and AE or charging station. It may therefore be necessary to adapt these values to ensure proper communication.
If PLC communication is emulated and if the presence of the AAN prevents proper PLC communication then no AAN should be used.

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... Figure 10
Example of AAN circuit for Signal/Control port with PLC on control pilot
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... a0c0
5.4.

Signal/Control port with control pilot

Some communication systems use the control pilot line (versus PE). On one hand the communication lines are operated unsymmetrically, on the other hand two different communication systems operate on the same line. Therefore, a special AAN must be used as defined in Figure 11.
It provides a common mode impedance of 150 Ω ± 20 Ω (150 kHz to 30 MHz) on the control pilot line (between A and B/D).
Therefore, typically a communication simulation is used in combination with this network.
The values of inductance and capacitance in the networks on control pilot shown in Figure 11 shall not induce any malfunction of communication between vehicle and charging station. It may therefore be necessary to adapt these values to ensure proper communication.
If Control pilot communication is emulated and if the presence of the AAN prevents proper Control pilot communication then no AAN should be used.

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... Figure 11
Example of AAN circuit for pilot line
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... a0c0
A1 

Annex 1

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A1  Examples of approval marks a0c0
A1 

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A1 

The above approval mark affixed to a vehicle or ESA shows that the vehicle type concerned has, with regard to electromagnetic compatibility, been approved in the Netherlands (E 4) pursuant to Regulation No. 10 under approval No. 06 2439. The approval number indicates that the approval was granted according to the requirements of Regulation No. 10 as amended by the 06 series of amendments.

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A1 

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A1 

The above approval mark affixed to a vehicle or ESA shows that the vehicle type concerned has, with regard to electromagnetic compatibility, been approved in the Netherlands (E 4) pursuant to Regulations Nos. 10 and 33.[1] The approval numbers indicate that, at the date when the respective approvals were given, Regulation No. 10 included the 06 series of amendments and Regulation No. 33 was still in its original form.

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A1 [1] The second number is given merely as an example. a0c0
A2  Annex 2A a0c0
A2  Information document for type approval of a vehicle with respect to electromagnetic compatibility a0c0
A2  The following information shall be supplied in triplicate and shall include a list of contents. a0c0
A2 

Any drawings shall be supplied in appropriate scale and in sufficient detail. If submission is paper based, documents shall be on size A4 or in a folder of A4 format. Electronic submissions may be of any standard size.

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A2  Photographs, if any, shall show sufficient detail. a0c0
A2  If the systems, components or separate technical units have electronic controls, information concerning their performance shall be supplied. a0c0
A2  General a0c0
A2 1. Make (trade name of manufacturer): a0c0
A2 2. Type: a0c0
A2 3. Category of vehicle: a0c0
A2 4. Name and address of manufacturer: a0c0
A2  Name and address of authorised representative, if any: a0c0
A2 5. Address(es) of assembly plant(s): a0c0
A2  General construction characteristics of the vehicle a0c0
A2 6. Photograph(s) and/or drawing(s) of a representative vehicle: a0c0
A2 7. Position and arrangement of the engine: a0c0
A2  Power plant a0c0
A2 8. Manufacturer: a0c0
A2 9. Manufacturer's engine code as marked on the engine: a0c0
A2 10. Internal combustion engine: a0c0
A2 11. Working principle: positive ignition/compression ignition, four-stroke/two stroke[1] a0c0
A2 12. Number and arrangement of cylinders: a0c0
A2 13. Fuel feed: a0c0
A2 14. By fuel injection (compression ignition only): yes/no[1] a0c0
A2 15. Electronic control unit: a0c0
A2 16. Make(s): a0c0
A2 17. Description of the system: a0c0
A2 18. By fuel injection (positive ignition only): yes/no[1] a0c0
A2 19. Electrical system: a0c0
A2 20. Rated voltage: __________________________ V, positive/negative ground[1] a0c0
A2 21. Generator: a0c0
A2 22. Type: a0c0
A2 23. Ignition: a0c0
A2 24. Make(s): a0c0
A2 25. Type(s): a0c0
A2 26. Working principle: a0c0
A2 27. LPG fuelling system: yes/no[1] a0c0
A2 28. Electronic engine management control unit for LPG fuelling: a0c0
A2 29. Make(s): a0c0
A2 30. Type(s): a0c0
A2 31. NG fuelling system: yes/no[1] a0c0
A2 32. Electronic engine management control unit for NG fuelling: a0c0
A2 33. Make(s): a0c0
A2 34. Type(s): a0c0
A2 35. Electric motor: a0c0
A2 36. Type (winding, excitation): a0c0
A2 37. Operating voltage: a0c0
A2  Gas fuelled engines (in the case of systems laid-out in a different manner, supply equivalent information) a0c0
A2 38. Electronic control unit (ECU): a0c0
A2 39. Make(s): a0c0
A2 40. Type(s): a0c0
A2  Transmission a0c0
A2 41. Type (mechanical, hydraulic, electric, etc.): a0c0
A2 42. A brief description of the electrical/electronic components (if any): a0c0
A2  Suspension a0c0
A2 43. A brief description of the electrical/electronic components (if any): a0c0
A2 44. A brief description of the electrical/electronic components (if any): a0c0
A2  Brakes a0c0
A2 45. Anti-lock braking system: yes/no/optional[1] a0c0
A2 46. For vehicles with anti-lock systems, description of system operation (including any electronic parts), electric block diagram, hydraulic or pneumatic circuit plan: a0c0
A2  Bodywork a0c0
A2 47. Type of bodywork: a0c0
A2 48. Materials used and methods of construction: a0c0
A2 49. Windscreen and other windows: a0c0
A2 50. A brief description of the electrical/electronic components (if any) of the window lifting mechanism: a0c0
A2 51.

Devices for indirect vision in the scope of Regulation No. 46:

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A2 52.

A brief description of the electrical/electronic components (if any):

a0c0
A2 53. Safety belts and/or other restraint systems: a0c0
A2 54. A brief description of the electrical/electronic components (if any): a0c0
A2 55. Suppression of radio interference: a0c0
A2 56. Description and drawings/photographs of the shapes and constituent materials of the part of the body forming the engine compartment and the part of the passenger compartment nearest to it: a0c0
A2 57. Drawings or photographs of the position of the metal components housed in the engine compartment (e.g. heating appliances, spare wheel, air filter, steering mechanism, etc.): a0c0
A2 58. Table and drawing of radio interference control equipment: a0c0
A2 59. Particulars of the nominal value of the direct current resistance and, in the case of resistive ignition cables, of their nominal resistance per metre: a0c0
A2  Lighting and light signalling devices a0c0
A2 60. A brief description of electrical/electronic components other than lamps (if any): a0c0
A2  Miscellaneous a0c0
A2 61. Devices to prevent unauthorised use of the vehicle: a0c0
A2 62. A brief description of the electrical/electronic components (if any): a0c0
A2 63. Table of installation and use of RF transmitters in the vehicle(s), if applicable (see paragraph 3.1.8. of this Regulation): a0c0
A2  a0c0
A2 64. Vehicle equipped with 24 GHz short-range radar equipment: yes/no/optional.[1] a0c0
A2  The applicant for type approval shall also supply, where appropriate: a0c0
A2 Appendix 1 A list with make(s) and type(s) of all electrical and/or electronic components concerned by this Regulation (see paragraphs 2.9. and 2.10. of this Regulation) and not previously listed. a0c0
A2 Appendix 2: Schematics or drawing of the general arrangement of electrical and/or electronic components (concerned by this Regulation) and the general wiring harness arrangement. a0c0
A2 Appendix 3: Description of vehicle chosen to represent the type: a0c0
A2  Body style: a0c0
A2  Left or right hand drive: a0c0
A2  Wheelbase: a0c0
A2 Appendix 4: Relevant test report(s) supplied by the manufacturer from a test laboratory accredited to ISO 17025 and recognized by the Type Approval Authority for the purpose of drawing up the type approval certificate. a0c0
A2 65. Charger: on board/external/without:[1] a0c0
A2 66. Charging current: direct current / alternating current (number of phases/frequency):[1] a0c0
A2 67. Maximal nominal current (in each mode if necessary): a0c0
A2 68. Nominal charging voltage: a0c0
A2 69. Basic vehicle interface functions: ex: L1/L2/L3/N/E/control pilot: a0c0
A2 70. Minimum Rsce value (see paragraph 7.3.) a0c0
A2 71.

Charging harness delivered with the vehicle: yes/no[1]

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A2 72.

If charging harness delivered with the vehicle:

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A2  Length (m) a0c0
A2  Cross sectional area (mm2) a0c0
A2 [1] Strike out what does not apply. a0c0
A2  Annex 2B a0c0
A2  Information document for type approval of an electric/electronic sub-assembly with respect to electromagnetic compatibility a0c0
A2  The following information, if applicable, shall be supplied in triplicate and shall include a list of contents. Any drawings shall be supplied in appropriate scale and in sufficient detail on size A4 or on a folder of A4 format. Photographs, if any, shall show sufficient detail. a0c0
A2  If the systems, components or separate technical units have electronic controls, information concerning their performance shall be supplied. a0c0
A2 1. Make (trade name of manufacturer): a0c0
A2 2. Type: a0c0
A2 3. Means of identification of type, if marked on the component/separate technical unit:[1] a0c0
A2 3.1. Location of that marking: a0c0
A2 4. Name and address of manufacturer: a0c0
A2  Name and address of authorized representative, if any: a0c0
A2 5. In the case of components and separate technical units, location and method of affixing of the approval mark: a0c0
A2 6. Address(es) of assembly plant(s): a0c0
A2 7. This ESA shall be approved as a component/STU[2] a0c0
A2 8. Any restrictions of use and conditions for fitting: a0c0
A2 9. Electrical system rated voltage: V, positive/negative[2] ground. a0c0
A2 Appendix 1: Description of the ESA chosen to represent the type (electronic block diagram and list of main component constituting the ESA (e.g. make and type of microprocessor, crystal, etc.). a0c0
A2 Appendix 2: Relevant test report(s) supplied by the manufacturer from a test laboratory accredited to ISO 17025 and recognized by the Type Approval Authority for the purpose of drawing up the type approval certificate. a0c0
A2  Only applicable for charging systems: a0c0
A2 10. Charger: on board/external[2] a0c0
A2 11. Charging current: direct current/alternating current (number of phases/frequency)[2] a0c0
A2 12. Maximal nominal current (in each mode if necessary) a0c0
A2 13. Nominal charging voltage a0c0
A2 14. Basic ESA interface functions: ex. L1/L2/L3/N/PE/control pilot a0c0
A2 15. Minimum Rsce value (see paragraph 7.11. of this Regulation) a0c0
A2 [1] If the means of identification of type contains characters not relevant to describe the component or separate technical unit types covered by this information document, such characters shall be represented in the documentation by the symbol "?" (e.g. ABC??123??). a0c0
A2 [2] Delete where not applicable. a0c0
A3  Annex 3A a0c0
A3  Communication a0c0
A3  (Maximum format: A4 (210 x 297 mm)) a0c0
A3  a0c0
A3  of a type of vehicle/component/separate technical unit[2] with regard to Regulation No. 10. a0c0
A3  Approval No.:....................Extension No.:.................... a0c0
A3 1. Make (trade name of manufacturer): a0c0
A3 2. Type: a0c0
A3 3. Means of identification of type, if marked on the vehicle/component/separate technical unit[2] a0c0
A3 3.1. Location of that marking: a0c0
A3 4. Category of vehicle: a0c0
A3 5. Name and address of manufacturer: a0c0
A3 6. In the case of components and separate technical units, location and method of affixing of the approval mark: a0c0
A3 7. Address(es) of assembly plant(s): a0c0
A3 8. Additional information (where applicable): See appendix below a0c0
A3 9. Technical Service responsible for carrying out the tests: a0c0
A3 10. Date of test report: a0c0
A3 11. Number of test report: a0c0
A3 12. Remarks (if any): See appendix below a0c0
A3 13. Place: a0c0
A3 14. Date: a0c0
A3 15. Signature: a0c0
A3 16. The index to the information package lodged with the Approval Authority, which may be obtained on request is attached: a0c0
A3 17. Reasons for extension: a0c0
A3  Appendix to type approval communication form No......... a0c0
A3  concerning the type approval of a vehicle under Regulation No. 10 a0c0
A3 1. Additional information: a0c0
A3 2. Electrical system rated voltage: ..............................................V. pos/neg ground[2] a0c0
A3 3. Type of bodywork: a0c0
A3 4. List of electronic systems installed in the tested vehicle(s) not limited to the items in the information document: a0c0
A3 4.1. Vehicle equipped with 24 GHz short-range radar equipment: yes/no/optional[2] a0c0
A3 5. Laboratory accredited to ISO 17025 and recognized by the Approval Authority responsible for carrying out the tests: a0c0
A3 6. Remarks: (e.g. valid for both left-hand drive and right-hand drive vehicles): a0c0
A3 [1] Distinguishing number of the country which has granted/extended/ refused/withdrawn approval (see approval provisions in the Regulation). a0c0
A3 [2] Strike out what does not apply. a0c0
A3  Annex 3B a0c0
A3  Communication a0c0
A3  (Maximum format: A4 (210 x 297 mm)) a0c0
A3  a0c0
A3  of a type of electrical/electronic sub-assembly[2] with regard to Regulation No. 10. a0c0
A3 1. Make (trade name of manufacturer): a0c0
A3 2. Type and general commercial description(s): a0c0
A3 3. Means of identification of type, if marked on the vehicle/component/separate/technical unit[2] a0c0
A3 3.1. Location of that marking: a0c0
A3 4. Category of vehicle: a0c0
A3 5. Name and address of manufacturer: a0c0
A3 6. In the case of components and separate technical units, location and method of affixing of the approval mark: a0c0
A3 7. Address(es) of assembly plant(s): a0c0
A3 8. Additional information (where applicable): See appendix below a0c0
A3 9. Technical Service responsible for carrying out the tests: a0c0
A3 10. Date of test report: a0c0
A3 11. No. of test report: a0c0
A3 12. Remarks (if any): See appendix below a0c0
A3 13. Place: a0c0
A3 14. Date: a0c0
A3 15. Signature: a0c0
A3 16. The index to the information package lodged with the Approval Authority, which may be obtained on request, is attached: . a0c0
A3 17. Reasons for extension: a0c0
A3  Appendix to type approval communication form No........ a0c0
A3  concerning the type approval of an electrical/electronic a0c0
A3 

sub-assembly under UN Regulation No. 10

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A3 1. Additional information: a0c0
A3 1.1. Electrical system rated voltage: ...................................................V. pos/neg ground[2] a0c0
A3 1.2. This ESA can be used on any vehicle type with the following restrictions: a0c0
A3 1.2.1. Installation conditions, if any: a0c0
A3 1.3. This ESA can be used only on the following vehicle types: a0c0
A3 1.3.1. Installation conditions, if any: a0c0
A3 1.4. The specific test method(s) used and the frequency ranges covered to determine immunity were: (Please specify precise method used from Annex 9): a0c0
A3 1.5. Laboratory accredited to ISO 17025 and recognized by the Approval Authority responsible for carrying out the tests: a0c0
A3 2. Remarks: a0c0
A4  Annex 4 a0c0
A4  Method of measurement of radiated broadband electromagnetic emissions from vehicles a0c0
A4 1. General a0c0
A4 1.1. The test method described in this annex shall only be applied to vehicles. This method concerns both configurations of the vehicle: a0c0
A4  (a) Other than "REESS charging mode coupled to the power grid". a0c0
A4  (b) "REESS charging mode coupled to the power grid" a0c0
A4 1.2. Test method a0c0
A4  This test is intended to measure the broadband emissions generated by electrical or electronic systems fitted to the vehicle (e.g. ignition system or electric motors). a0c0
A4  If not otherwise stated in this annex the test shall be performed according to CISPR 12. a0c0
A4 2. Vehicle state during tests a0c0
A4 2.1. Vehicle in configuration other than "REESS charging mode coupled to the power grid". a0c0
A4 2.1.1. Engine a0c0
A4 

The engine shall be in operation according to CISPR 12.

For vehicle with an electric propulsion motor or hybrid propulsion system, if this is not appropriate (e.g. in case of busses, trucks, two- and three wheel vehicles), transmission shafts, belts or chains may be disconnected to achieve the same operation condition for the propulsion. [#new]

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A4 2.1.2. Other vehicle systems a0c0
A4  All equipment capable of generating broadband emissions which can be switched on permanently by the driver or passenger should be in operation in maximum load, e.g. wiper motors or fans. The horn and electric window motors are excluded because they are not used continuously. a0c0
A4 2.2. Vehicle in configuration "REESS charging mode coupled to the power grid". a0c0
A4 

The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole frequency range measurement (this may lead to split the measurement into different sub-bands with the need to discharge the vehicle's traction battery before starting the next sub-bands). 

If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging.
If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for DC charging unless another value is agreed with the type approval authorities.
In case of multiple batteries the average state of charge must be considered.
The vehicle shall be immobilized, the engine(s) (ICE and / or electrical engine) shall be OFF and in charging mode. All other equipment which can be switched ON by the driver or passengers shall be OFF. [#new]

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A4 2.3.

Vehicle in charging mode 1 or mode 2 (AC power charging without communication).

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A4 2.3.1.

Charging station / Power mains

The power mains socket can be placed anywhere in the test site with the following conditions:
-           The socket(s) shall be placed on the ground plane (ALSE) or floor (OTS);
-           The length of the harness between the power mains socket and the AMN(s) shall be kept as short as possible, but not necessarily aligned with the charging harness;
-           The harness shall be placed as close as possible to the ground plane (ALSE) or floor (OTS).

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A4 2.3.2.

Artificial network

Power mains shall be applied to the vehicle through 50 µH/50 W artificial networks (AMN(s)) (see appendix 8 clause 4).
The AMN(s) shall be mounted directly on the ground plane (ALSE) or floor (OTS). The case of the AMN(s) shall be bonded to the ground plane (ALSE) or connected to the protective earth (OTS, e.g. an earth rod).
The measuring port of each AMN shall be terminated with a
50 W load.

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A4 2.3.3.

Power charging harness

The power charging harness shall be placed in a straight line between the AMN(s) and the vehicle charging plug and shall be routed perpendicularly to the vehicle longitudinal axis (see Figure 3d and Figure 3c). The projected harness length from the side of the AMN(s) to the side of the vehicle shall be 0,8 (+0,2 / -0) m as shown in Figure 3d and Figure 3e.
For a longer harness the extraneous length shall be “Z-folded” in a less than 0,5 m width approximately around the middle of the AMN to vehicle distance. If it is impractical to do so because of harness bulk or stiffness, or because the testing is being done at a user’s installation, the disposition of the excess harness shall be precisely noted in the test report.
The charging harness at the vehicle side shall hang vertically at a distance of 100 (+200 / -0) mm from the vehicle body.
The whole harness shall be placed on a non-conductive, low relative permittivity (dielectric-constant) material (er ≤ 1,4), at (100 ± 25) mm above the ground plane (ALSE) or floor (OTS).

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A4 2.4.

Vehicle in charging mode 3 (AC power charging with communication) or mode 4 (DC power charging with communication).

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A4 2.4.1.

Charging station / Power mains

The charging station may be placed either in the test site or outside the test site.
If the local/private communication between the vehicle and the charging station can be simulated, the charging station may be replaced by a supply from the AC power mains network.
In both cases power mains and communication or signal lines socket(s) shall be placed in the test site with the following conditions:
-    The socket(s) shall be placed on the ground plane (ALSE) or floor (OTS);
-   The length of the harness between the power mains / local/private communication socket and the AMN(s) / DC-charging-AN(s) / AAN(s) shall be kept as short as possible, but not necessarily aligned with the charging harness; 
-    The harness between the power mains / local/private communication socket and the AMN(s) / DC-charging-AN(s) / AAN(s) shall be placed as close as possible of the ground plane (ALSE) or floor (OTS).

If the charging station is placed inside the test site, then the harness between the charging station and the power mains / local/private communication socket shall satisfy the following conditions:
-   The harness at charging station side shall hang vertically down to the ground plane (ALSE) or floor (OTS);
-   The extraneous length shall be placed as close as possible to the ground plane (ALSE) or floor (OTS) and “Z-folded” if necessary. If it is impractical to do so because of cable bulk or stiffness, or because the testing is being done at a user installation, the disposition of the excess cable shall be precisely noted in the test report.

The charging station should be placed outside of the 3 dB beamwidth of the receiving antenna. If this is not technically feasible, the charging station can be placed behind a panel of absorbers but not between the antenna and the vehicle.

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A4 2.4.2.

Artificial network

AC power mains shall be applied to the vehicle through 50 µH/50 Ω AMN(s) (see Appendix 8, clause 4).
DC power mains shall be applied to the vehicle through 5 µH/50 Ω High Voltage Artificial Networks (DC-charging-AN(s)) (see Appendix 8, clause 3).
The AMN(s) / DC-charging-AN(s) shall be mounted directly on the ground plane (ALSE) or floor (OTS). The cases of the AMN(s) / DC-charging-AN(s) shall be bonded to the ground plane (ALSE) or connected to the protective earth (OTS, e.g. an earth rod).
The measuring port of each AMN / DC-charging-AN shall be terminated with a 50 Ω load.

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A4 2.4.3.

Asymmetric artificial network

Local/private communication lines connected to signal/control ports and lines connected to wired network ports shall be applied to the vehicle through AAN(s).

The various AAN(s) to be used are defined in Appendix 8, clause 5:
-    Clause 5.1 for signal/control port with symmetric lines;
-    Clause 5.2 for wired network port with PLC on power lines;
-    Clause 5.3 for signal/control port with PLC (technology) on control pilot; and
-    Clause 5.4 for signal/control port with control pilot.

The AAN(s) shall be mounted directly on the ground plane. The case of the AAN(s) shall be bonded to the ground plane (ALSE) or connected to the protective earth (OTS, e.g. an earth rod).

The measuring port of each AAN shall be terminated with a 50 Ω load.

If a charging station is used, AAN(s) are not required for the signal/control ports and/or for the wired network ports. The local/private communication lines between the vehicle and the charging station shall be connected to the associated equipment on the charging station side to work as designed. If communication is emulated and if the presence of the AAN prevents proper communication then no AAN should be used

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A4 2.4.4.

Power charging / local/private communication harness
 
The power charging local/private communication harness shall be laid out in a straight line between the AMN(s) / DC-charging-AN(s) / AAN(s) and the vehicle charging socket and shall be routed perpendicularly to the vehicle’s longitudinal axis (see Figure 3f and Figure 3g). The projected harness length from the side of the AMN(s) to the side of the vehicle shall be 0,8 (+0,2 / -0) m.

For a longer harness the extraneous length shall be “Z-folded” in less than 0,5 m width. If it is impractical to do so because of harness bulk or stiffness, or because the testing is being done at a user installation, the disposition of the excess harness shall be precisely noted in the test report.

The power charging local/private communication harness at vehicle side shall hang vertically at a distance of 100 (+200 / -0) mm from the vehicle body.

The whole harness shall be placed on a non-conductive, low relative permittivity (dielectric-constant) material (εr ≤ 1,4), at (100 ± 25) mm above the ground plane (ALSE) or floor (OTS).

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A4 3. Measuring location a0c0
A4 3.1. As an alternative to the requirements of CISPR 12 for vehicles of category L, the test surface may be any location that fulfils the conditions shown in the Figure of the appendix to this annex. In this case the measuring equipment shall lie outside the part shown in Figure 1 of Appendix 1 to this annex. a0c0
A4 3.2.

Enclosed test facilities may be used if correlation can be shown between the results obtained in the enclosed test facility and those obtained at an outdoor site. Enclosed test facilities do not need to meet the dimensional requirements of the outdoor site other than the distance from the antenna to the vehicle and the height of the antenna.

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A4 4. Test requirements a0c0
A4 4.1.

The limits apply throughout the frequency range 30 to 1,000 MHz for measurements performed in chamber an absorber lined shielded enclosure (ALSE) or an outdoor test site (OTS).

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A4 4.2.

Measurements can be performed with either quasi-peak or peak detectors. The limits given in paragraphs 6.2. and 7.2. of this Regulation are for quasi-peak detectors. If peak detectors are used a correction factor of 20 dB as defined in CISPR 12 shall be applied.

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A4 4.3. The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in Table 1 and Table 2. a0c0
A4 

Table 1
Spectrum analyser parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz RBW at Minimum scan RBW at Minimum scan RBW at Minimum scan
  -3 dB time -6 dB time -3 dB time
30 to 100/120 kHz 100 ms/MHz 120 20 100/120 kHz 100 ms/MHz
1,000 kHz s/MHz

Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth (RBW). 

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A4 

Table 2
Scanning receiver parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz BW at Step Minimum scan time BW at Step Minimum Dwell time BW at Step Minimum scan time
  -6 dB size a -6 dB size a -6 dB size a
30 to 1000 120 kHz 50 kHz 5 ms 120 kHz 50 kHz 1 s 120 kHz 50 kHz 5 ms

a  For purely broadband disturbances, the maximum frequency step size may be increased up to a value not greater than the bandwidth value. 

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A4 4.4. Measurements a0c0
A4  The Technical Service shall perform the test at the intervals specified in the CISPR 12 standard throughout the frequency range 30 to 1,000 MHz. a0c0
A4  Alternatively, if the manufacturer provides measurement data for the whole frequency band from a test laboratory accredited to the applicable parts of ISO 17025 and recognized by the Type Approval Authority, the Technical Service may divide the frequency range in 14 frequency bands 30-34, 34-45, 45-60, 60-80, 80-100, 100-130, 130-170, 170-225, 225-300, 300-400, 400-525, 525-700, 700-850 and 850-1,000 MHz and perform tests at the 14 frequencies giving the highest emission levels within each band to confirm that the vehicle meets the requirements of this annex. a0c0
A4  In the event that the limit is exceeded during the test, investigations shall be made to ensure that this is due to the vehicle and not to background radiation. a0c0
A4 4.5 Readings a0c0
A4  The maximum of the readings relative to the limit (horizontal and vertical polarization and antenna location on the left and right-hand sides of the vehicle) in each of the 14 frequency bands shall be taken as the characteristic reading at the frequency at which the measurements were made. a0c0
A4 4.6.

Antenna position

Measurements shall be made on the left and right sides of the vehicle.

The horizontal distance is from the reference point of the antenna to the nearest part of the vehicle body.

Multiple antenna positions may be required (both for 10 m and 3 m antenna distance) depending on the vehicle length. The same positions shall be used for both horizontal and vertical polarization measurements. The number of antenna positions and the position of the antenna with respect to the vehicle shall be documented in the test report.

- If the length of the vehicle is smaller than the 3 dB beamwidth of the antenna, only one antenna position is necessary. The antenna shall be aligned with the middle of the total vehicle (see Figure 4);

- If the length of the vehicle is greater than the 3 dB beamwidth of the antenna, multiple antenna positions are necessary in order to cover the total length of the vehicle (see Figure 5). The number of antenna positions shall allow to meet the following condition:


With:

N: Number of antenna positions;

D: Measurement distance (3 m or 10 m);

2×β: 3 dB antenna beamwidth angle in the plane parallel to ground (i.e. the E-plane beamwidth angle when the antenna is used in horizontal polarization, and the H-plane beamwidth angle when the antenna is used in vertical polarization);

L: Total vehicle length;

Depending of the chosen values of N (number of antenna positions) different set-up shall be used:

if N=1 (only one antenna position is necessary) and the antenna shall be aligned with the middle of the total vehicle length (see Figure 4).

if N>1 (more than one antenna position is necessary) and multiple antenna positions are necessary in order to cover the total length of the vehicle (see Figure 5). The antenna positions shall be symmetric in regard to the vehicle perpendicular axis.

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A4 

Annex 4 - Appendix 1

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A4 

Figure 1
Clear horizontal surface free of electromagnetic reflection delimitation of the surface defined by an ellipse

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A4 

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A4 

Figure 2
Position of antenna in relation to the vehicle:

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A4 

Figure 2a
Dipole antenna in position to measure the vertical radiation components

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A4 

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A4 

Figure 2b
Dipole antenna in position to measure the horizontal radiation components

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A4 

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A4 

Figure 3
Vehicle in configuration "REESS charging mode" coupled to the power grid:

Example of test set-up for vehicle with plug located on vehicle side (AC powered without communication)

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A4 

Figure 3a

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A4 

Figure 3b

Legend:

1:   Vehicle under test.
2:   Insulating support.
3:   Charging harness (including EVSE for charging mode 2).
4:   AMN(s) or DC-charging-AN(s) grounded.
5:   Power mains socket.

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A4 

Example of test setup for vehicle with socket located front / rear of vehicle (charging mode 1 or 2, AC powered, without communication).

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A4 

Figure 3c

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A4 

Figure 3d

Legend:
1:    Vehicle under test.
2:    Insulating support.
3:    Charging harness (including EVSE for charging mode 2).
4:    AMN(s) or DC-charging-AN(s) grounded.
5:    Power mains socket.

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A4 

Example of test setup for vehicle with socket located on vehicle side (charging mode 3 or mode 4, with communication)

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A4 

Figure 3e

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A4 

Figure 3f

Legend:
1:    Vehicle under test.
2:    Insulating support.
3:    Charging harness with local/private communication lines.
4:    AMN(s) or DC-charging-AN(s) grounded.
5:    Power mains socket.
6:    AAN(s) grounded (optional).
7:    Charging station.

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A4 

Example of test setup for vehicle with socket located front / rear of vehicle (charging mode 3 or mode 4, with communication) 

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A4 

Figure 3g

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A4 

Figure 3h

Legend:
1:    Vehicle under test.
2:    Insulating support.
3:    Charging harness with local/private communication lines.
4:    AMN(s) or DC-charging-AN(s) grounded.
5:    Power mains socket.
6:    AAN(s) grounded (optional).
7:    Charging station.

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A4 

Antenna position

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A4 

Figure 4
Antenna position for N = 1 (one antenna position to be used) – Horizontal polarization shown

Legend 
1:    Vehicle under test.
2:    Antenna

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A4 

Figure 5
Antenna positions for N = 2 (multiple antenna positions to be used) – Horizontal polarization shown

Key 
1:    Vehicle under test.
2:    Antenna (two position)

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A5  Annex 5 a0c0
A5  Method of measurement of radiated narrowband electromagnetic emissions from vehicles a0c0
A5 1. General a0c0
A5 1.1. The test method described in this annex shall only be applied to vehicles. This method concerns only the configuration of the vehicle other than "REESS charging mode coupled to the power grid". a0c0
A5 1.2. Test method a0c0
A5  This test is intended to measure the narrowband electromagnetic emissions that may emanate from microprocessor-based systems or other narrowband source. a0c0
A5  If not otherwise stated in this annex the test shall be performed according to CISPR 12 or CISPR 25. a0c0
A5 1.3. As an initial step the levels of emissions in the Frequency Modulation (FM) band (76 to 108 MHz) shall be measured at the vehicle broadcast radio antenna with an average detector. If the level specified in paragraph 6.3.2.4. of this Regulation is not exceeded, then the vehicle shall be deemed to comply with the requirements of this annex in respect of that frequency band and the full test shall not be carried out. a0c0
A5 1.4. As an alternative for vehicles of category L the measurement location can be chosen according to Annex 4, paragraphs 3.1. and 3.2. a0c0
A5 2. Vehicle state during tests a0c0
A5 2.1. The ignition switch shall be switched on. The engine shall not be operating. a0c0
A5 2.2. The vehicle's electronic systems shall all be in normal operating mode with the vehicle stationary. a0c0
A5 2.3. All equipment which can be switched on permanently by the driver or passenger with internal oscillators > 9 kHz or repetitive signals should be in normal operation. a0c0
A5 3.

Measuring location

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A5 3.1.

Absorber lined shielded enclosures (ALSE) and outdoor test site (OTS) may be used. An ALSE has the advantage of all all-weather testing, a controlled environment and improved repeatability because of the stable chamber electrical characteristics. 

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A5 4.

Test requirements

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A5 4.1.

The limits apply throughout the frequency range 30 to 1,000 MHz for measurements performed in an absorber lined shielded enclosure (ALSE) or an outdoor test site (OTS).

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A5 4.2.

Measurements shall be performed with an average detector.

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A5 4.3.

The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in Table 1 and Table 2.

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A5 

Table 1
Spectrum analyser parameters

Frequency range Peak detector Average detector
MHz RBW at Minimum scan time RBW at Minimum scan time
  -3 dB -3 dB
30 to 1,000 100/120 kHz 100 ms/MHz 100/120 kHz 100 ms/MHz

Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth (RBW). 

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A5 

Table 2
Scanning receiver parameters

Frequency range Peak detector Average detector
MHz BW at Step Minimum scan time BW at Step Minimum scan time
  -6 dB size  -6 dB size 
30 to 1,000 120 kHz 50 kHz 5 ms 120 kHz 50 kHz 5 ms
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A5 4.4.

Measurements

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A5  The Technical Service shall perform the test at the intervals specified in the CISPR 12 standard throughout the frequency range 30 to 1,000 MHz. a0c0
A5  Alternatively, if the manufacturer provides measurement data for the whole frequency band from a test laboratory accredited to the applicable parts of ISO 17025 and recognized by the Type Approval Authority, the Technical Service may divide the frequency range in 14 frequency bands 30-34, 34-45, 45-60, 60-80, 80-100, 100-130, 130-170, 170-225, 225-300, 300-400, 400-525, 525-700, 700-850 and 850-1,000 MHz and perform tests at the 14 frequencies giving the highest emission levels within each band to confirm that the vehicle meets the requirements of this Annex. a0c0
A5  In the event that the limit is exceeded during the test, investigations shall be made to ensure that this is due to the vehicle and not to background radiation including broadband radiation from any ESA. a0c0
A5 4.5.

Readings

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A5  The maximum of the readings relative to the limit (horizontal and vertical polarization and antenna location on the left and right-hand sides of the vehicle) in each of the 14 frequency bands shall be taken as the characteristic reading at the frequency at which the measurements were made. a0c0
A5 

Antenna position

Measurements shall be made on the left and right sides of the vehicle.

The horizontal distance is from the reference point of the antenna to the nearest part of the vehicle body.

Multiple antenna positions may be required (both for 10 m and 3 m antenna distance) depending on the vehicle length. The same positions shall be used for both horizontal and vertical polarization measurements. The number of antenna positions and the position of the antenna with respect to the vehicle shall be documented in the test report.

- if the length of the vehicle is smaller than the 3 dB beamwidth of the antenna, only one antenna position is necessary. The antenna shall be aligned with the middle of the total vehicle (see Figure 1)

- If the length of the vehicle is greater than the 3 dB beamwidth of the antenna, multiple antenna positions are necessary in order to cover the total length of the vehicle (see Figure 2). The number of antenna positions shall allow to meet the following condition :

With:
N: number of antenna positions.
D: measurement distance (3 m or 10 m).

2×β: 3 dB antenna beamwidth angle in the plane parallel to ground (i.e. the E-plane beamwidth angle when the antenna is used in horizontal polarization, and the H-plane beamwidth angle when the antenna is used in vertical polarization).
L: total vehicle length.

Depending of the chosen values of N (number of antenna positions) different set-up shall be used:
if N=1 (only one antenna position is necessary) and the antenna shall be aligned with the middle of the total vehicle length (see Figure 1).
if N>1 (more than one antenna position is necessary) and multiple antenna positions are necessary in order to cover the total length of the vehicle (see Figure 2). The antenna positions shall be symmetric in regard to the vehicle perpendicular axis.

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A5 

Annex 5 - Appendix 1

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A5 

Antenna position

Figure 1
Antenna position for N = 1 (one antenna position to be used) – 
Horizontal polarization shown

Legend:
1:    Vehicle under test
2:    Antenna

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A5 

Figure 2
Antenna positions for N = 2 (multiple antenna positions to be used) – 
Horizontal polarization shown

Legend:
1:    Vehicle under test
2:    Antenna (two positions)

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A6 

Annex 6

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A6  Method of testing for immunity of vehicles to electromagnetic radiation a0c0
A6 1. General a0c0
A6 1.1. The test method described in this annex shall only be applied to vehicles. This method concerns both configurations of vehicle: a0c0
A6  (a) Other than "REESS charging mode coupled to the power grid". a0c0
A6  (b) "REESS charging mode coupled to the power grid". a0c0
A6 1.2. Test method a0c0
A6  This test is intended to demonstrate the immunity of the vehicle electronic systems. The vehicle shall be subject to electromagnetic fields as described in this annex. The vehicle shall be monitored during the tests. a0c0
A6  If not otherwise stated in this annex the test shall be performed according to ISO 11451-2. a0c0
A6 1.3. Alternative test methods a0c0
A6  The test may be alternatively performed in an outdoor test site for all vehicles. The test facility shall comply with (national) legal requirements regarding the emission of electromagnetic fields. a0c0
A6  If a vehicle is longer than 12 m and/or wider than 2.60 m and/or higher than 4.00 m, BCI (bulk current injection) method according to ISO 11451-4 shall be used in the frequency range 20 to 2,000 MHz with levels defined in paragraph 6.8.2.1. of this Regulation. a0c0
A6 2. Vehicle state during tests a0c0
A6 2.1. Vehicle in configuration other than "REESS charging mode coupled to the power grid. a0c0
A6 2.1.1. The vehicle shall be in an unladen condition except for necessary test equipment. a0c0
A6 2.1.1.1. The engine shall normally turn the driving wheels at a steady speed of 50 km/h if there is no technical reason due to the vehicle to define a different condition. For vehicles of categories L1 and L2 the steady speed shall normally be turned at 25 km/h. The vehicle shall be on an appropriately loaded dynamometer or alternatively supported on insulated axle stands with minimum ground clearance if no dynamometer is available. Where appropriate, transmission shafts, belts or chains may be disconnected (e.g. trucks, two- and three-wheel vehicles). a0c0
A6 2.1.1.2. Basic vehicle conditions a0c0
A6  The paragraph defines minimum test conditions (as far as applicable) and failures criteria for vehicle immunity tests. Other vehicle systems, which can affect immunity related functions, shall be tested in a way to be agreed between manufacturer and Technical Service. a0c0
A6 
"50 km/h mode" vehicle test conditions Failure criteria
Vehicle speed 50 km/h (respectively 25 km/h for L1, L2 vehicles) ±20 per cent (vehicle driving the rollers). If the vehicle is equipped with a cruise control system, it shall be used to maintain the required constant vehicle speed and maintained without any deactivation. Speed variation greater than ±10 per cent of the nominal speed. In case of automatic gearbox: change of gear ratio inducing a speed variation greater than ±10 per cent of the nominal speed.
Dipped beams ON (manual mode) Lighting OFF (front light and rear light) 
Specific warning (e.g Rotating/flashing light, signaling bar, siren…) ON Specific warning OFF
Cluster operate in normal mode Unexpected warning
Inconsistent variation of the odometer
Rear view system Unexpected movement of rear view mirror
Loss or freezing of the display (CMS)
Front wiper ON (manual mode) maximum speed Complete stop of front wiper
Direction indicator on driver's side ON Frequency change (lower than 0.75 Hz or greater than 2.25 Hz). Duty cycle change (lower than 25 per cent or greater than 75 per cent).
Adjustable suspension in normal position  Unexpected significant variation 
Driver's seat and steering wheel in medium position Unexpected variation greater than 10 per cent of total range
Alarm unset Unexpected activation of alarm
Horn OFF Unexpected activation of horn
Airbag and safety restraint systems operational with inhibited passenger airbag if this function exists Unexpected activation
Automatic doors closed Unexpected opening
Adjustable endurance brake lever in normal position Unexpected activation
Brake pedal not depressed Unexpected activation of brake and unexpected activation of stop lights
Vehicle in a state that allows the braking system to operate normally, parking brake released, vehicle speed 0 km/h. Stop lights inactivated during mode
Brake pedal depressed to activate the brake function and the stop lights without any dynamic cycle. Brake warning light ON with loss of brake function.
Day running light (DRL) ON DRL inactivated during mode
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A6 2.1.1.3. All equipment which can be switched on permanently by the driver or passenger should be in normal operation. a0c0
A6 2.1.1.4. All other systems which affect the driver's control of the vehicle shall be (on) as in normal operation of the vehicle. a0c0
A6 2.1.2.

If there are vehicle electrical/electronic systems which form an integral part of the immunity related functions, which will not operate under the conditions described in paragraph 2.1., it will be permissible for the manufacturer to provide a report or additional evidence to the Technical Service that the vehicle electrical/electronic system meets the requirements of this Regulation. Such evidence shall be retained in the type approval documentation.

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A6 2.1.3. Only non-perturbing equipment shall be used while monitoring the vehicle. The vehicle exterior and the passenger compartment shall be monitored to determine whether the requirements of this annex are met (e.g. by using (a) video camera(s), a microphone, etc.). a0c0
A6 2.2. Vehicle in configuration "REESS charging mode coupled to the power grid". a0c0
A6 2.2.1. The vehicle shall be in an unladen condition except for necessary test equipment. a0c0
A6 2.2.1.1.

The vehicle shall be immobilized, the engine(s) (ICE and / or electrical engine) shall be OFF and in charging mode.

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A6 2.2.1.2. Basic vehicle conditions a0c0
A6  The paragraph defines minimum test conditions (as far as applicable) and failures criteria for vehicle immunity tests. Other vehicle systems, which can affect immunity related functions, shall be tested in a way to be agreed between manufacturer and Technical Service. a0c0
A6 
"REESS charging mode" vehicle test conditions Failure criteria
The REESS shall be in charging mode. The REESS State of charge (SOC) shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole frequency range measurement (this may lead to split the measurement in different sub-bands with the need to discharge the vehicle's traction battery before starting the next sub-bands). If the current consumption can be adjusted, then the current shall be set to at least 20 per cent of its nominal value.
In case of multiple batteries the average state of charge must be considered.
Vehicle sets in motion.
Unexpected release of the parking brake.
Loss of  Parking position for automatic transmission.
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A6 2.2.1.3.

All other equipment which can be switched ON by the driver or passengers shall be OFF.

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A6 2.2.2. Only non-perturbing equipment shall be used while monitoring the vehicle. The vehicle exterior and the passenger compartment shall be monitored to determine whether the requirements of this annex are met (e.g. by using (a) video camera(s), a microphone, etc.). a0c0
A6 2.2.3. The test set-up for the connection of the vehicle in configuration "REESS charging mode coupled to the power grid" is shown in Figures 4a to 4h (depending of AC or DC power charging mode, location of charging plug and charging with or without communication) of Appendix 1 to this annex. a0c0
A6 2.3.

Vehicle in charging mode 1 or mode 2 (AC power charging without communication)

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A6 2.3.1.

Charging station / Power mains
The power mains socket can be placed anywhere in the test site with the following conditions:

  • The socket(s) shall be placed on the ground plane (ALSE) or floor (OTS);
  • The length of the harness between the power mains socket and the AMN(s) shall be kept as short as possible, but not necessarily aligned with the charging harness;
  • The harness shall be placed as close as possible to the ground plane (ALSE) or floor (OTS).
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A6 2.3.2.

Artificial network

Power mains shall be applied to the vehicle through 50 µH/50 W artificial networks (AMN(s)) (see appendix 8 clause 4).

The AMN(s) shall be mounted directly on the ground plane (ALSE) or floor (OTS). The case of the AMN(s) shall be bonded to the ground plane (ALSE) or connected to the protective earth (OTS, e.g. an earth rod).

The measuring port of each AMN shall be terminated with a 50 W load.

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A6 2.3.3.

Power charging harness
The power charging harness shall be placed in a straight line between the AMN(s) and the vehicle charging plug and shall be routed perpendicularly to the vehicle longitudinal axis (see Figure 3d and Figure 3e). The projected harness length from the side of the AMN(s) to the side of the vehicle shall be 0,8 (+0,2 / -0) m as shown in Figure 3d and Figure 3e.
For a longer harness the extraneous length shall be “Z-folded” in a less than 0,5 m width approximately around the middle of the AMN to vehicle distance. If it is impractical to do so because of harness bulk or stiffness, or because the testing is being done at a user’s installation, the disposition of the excess harness shall be precisely noted in the test report.
The charging harness at the vehicle side shall hang vertically at a distance of 100 (+200 /  0) mm from the vehicle body.
The whole harness shall be placed on a non-conductive, low relative permittivity (dielectric-constant) material (er ≤ 1,4), at (100 ± 25) mm above the ground plane (ALSE) or floor (OTS).

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A6 2.4.

Vehicle in charging mode 3 (AC power charging with communication) or mode 4 (DC power charging with communication)

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A6 2.4.1.

Charging station / Power mains

The charging station may be placed either in the test site or outside the test site.
If the local/private communication between the vehicle and the charging station can be simulated, the charging station may be replaced by a supply from the AC power mains network.
In both cases power mains and communication or signal lines socket(s) shall be placed in the test site with the following conditions:
-    The socket(s) shall be placed on the ground plane (ALSE) or floor (OTS);
-   The length of the harness between the power mains / local/private communication socket and the AMN(s) / DC-charging-AN(s) / AAN(s) shall be kept as short as possible, but not necessarily aligned with the charging harness;
-    The harness between the power mains / local/private communication socket and the AMN(s) / DC-charging-AN(s) / AAN(s) shall be placed as close as possible of the ground plane (ALSE) or floor (OTS).
If the charging station is placed inside the test site then the harness between the charging station and the power mains / local/private communication socket shall satisfy the following conditions:
-    The harness at charging station side shall hang vertically down to the ground plane (ALSE) or floor (OTS);
-   The extraneous length shall be placed as close as possible to the ground plane (ALSE) or floor (OTS) and “Z-folded” if necessary. If it is impractical to do so because of cable bulk or stiffness, or because the testing is being done at a user installation, the disposition of the excess cable shall be precisely noted in the test report;

The charging station should be placed outside the beamwidth of the receiving antenna.

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A6 2.4.3.

Asymmetric artificial network
Local/private communication lines connected to signal/control ports and lines connected to wired network ports shall be applied to the vehicle through AAN(s).
The various AAN(s) to be used are defined in Appendix 8, clause 5:
-    Clause 5.1. for signal/control port with symmetric lines;
-    Clause 5.2. for wired network port with PLC on power lines;
-    Clause 5.3. for signal/control port with PLC (technology) on control pilot; and
-    Clause 5.4. for signal/control port with control pilot.
The AAN(s) shall be mounted directly on the ground plane. The case of the AAN(s) shall be bonded to the ground plane (ALSE) or connected to the protective earth (OTS, e.g. an earth rod).
The measuring port of each AAN shall be terminated with a 50 W load.
If a charging station is used, AAN(s) are not required for the signal/control ports and/or for the wired network ports. The local/private communication lines between the vehicle and the charging station shall be connected to the associated equipment on the charging station side to work as designed. If communication is emulated and if the presence of the AAN prevents proper communication then no AAN should be used

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A6 2.4.4.

Power charging / local/private communication harness 
The power charging local/private communication harness shall be laid out in a straight line between the AMN(s) / DC-charging-AN(s) / AAN(s) and the vehicle charging socket and shall be routed perpendicularly to the vehicle’s longitudinal axis (see Figure 3f and Figure 3g). The projected harness length from the side of the AMN(s) to the side of the vehicle shall be 0,8 
(+0,2 / - 0) m.
For a longer harness the extraneous length shall be “Z-folded” in less than 0,5 m width. If it is impractical to do so because of harness bulk or stiffness, or because the testing is being done at a user installation, the disposition of the excess harness shall be precisely noted in the test report.
The power charging local/private communication harness at vehicle side shall hang vertically at a distance of 100 (+200 /  0) mm from the vehicle body.
The whole harness shall be placed on a non-conductive, low relative permittivity (dielectric-constant) material (er ≤ 1,4), at (100 ± 25) mm above the ground plane (ALSE) or floor (OTS).

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A6 3. Reference point a0c0
A6 3.1. For the purposes of this annex, the reference point is the point at which the field strength shall be established and shall be defined as follows: a0c0
A6 3.2.

For categories M, N, O, T, R and S vehicles according to ISO 11451-2.

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A6 3.3. For category L vehicles: a0c0
A6 3.3.1. At least 2 m horizontally from the antenna phase centre or at least 1 m vertically from the radiating elements of a transmission-line-system (TLS); a0c0
A6 3.3.2.

On the vehicle's centre line (plane of longitudinal symmetry).

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A6 3.3.3.

At a height of 1.0 ± 0.05 m above the plane on which the vehicle rests or 2.0 ± 0.05 m if the minimum height of the roof of any vehicle in the model range exceeds 3.0 m,

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A6 3.3.4.

Either at 1.0 ± 0.2 m behind the vertical centreline of the vehicle's front wheel (point C in Figure 1 of Appendix 1 to this annex) in the case of three-wheeled vehicles,

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A6 

Or at 0.2 ± 0.2 m behind the vertical centreline of the vehicle's front wheel (point D in Figure 2 of Appendix 1 to this annex) in the case of two-wheeled vehicles.

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A6 3.3.5. If it is decided to radiate the rear of the vehicle, the reference point shall be established as in paragraphs 3.3.1. to 3.3.4. above. The vehicle shall then be installed facing away from the antenna and positioned as if it had been horizontally rotated 180 around its centre point, i.e. such that the distance from the antenna to the nearest part of the outer body of the vehicle remains the same. This is illustrated in Figure 3 of Appendix 1 to this annex. a0c0
A6 4. Test requirements a0c0
A6 4.1. Frequency range, dwell times, polarization a0c0
A6  The vehicle shall be exposed to electromagnetic radiation in the 20 to 2,000 MHz frequency ranges in vertical polarization. a0c0
A6  The test signal modulation shall be: a0c0
A6  (a) AM (amplitude modulation), with 1 kHz modulation and 80 per cent modulation depth in the 20 to 800 MHz frequency range, and a0c0
A6  (b) PM (pulse modulation), Ton 577 µs, period 4,600 µs in the 800 to 2,000 MHz frequency range, a0c0
A6  If not otherwise agreed between Technical Service and vehicle manufacturer. a0c0
A6  Frequency step size and dwell time shall be chosen according to ISO 11451-1. a0c0
A6 4.1.1. The Technical Service shall perform the test at the intervals specified in ISO 11451-1 throughout the frequency range 20 to 2,000 MHz. a0c0
A6  Alternatively, if the manufacturer provides measurement to data for the whole frequency band from a test laboratory accredited to the applicable parts of ISO 17025 and recognized by the Type Approval Authority, the Technical Service may choose a reduced number of spot frequencies in the range, e.g. 27, 45, 65, 90, 120, 150, 190, 230, 280, 380, 450, 600, 750, 900, 1,300 and 1,800 MHz to confirm that the vehicle meets the requirements of this annex. a0c0
A6  If a vehicle fails the test defined in this annex, it shall be verified as having failed under the relevant test conditions and not as a result of the generation of uncontrolled fields. a0c0
A6 5. Generation of required field strength a0c0
A6 5.1. Test methodology a0c0
A6 5.1.1. The substitution method according to ISO 11451-1, shall be used to establish the test field conditions. a0c0
A6 5.1.2.

Calibration

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A6 

For TLS one field probe at the vehicle reference point shall be used.

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A6 

For antennas four field probes at the vehicle reference line shall be used.

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A6 5.1.3.

Test phase
   The vehicle shall be positioned with the centre line of the vehicle on the vehicle reference point or line. The vehicle shall normally face a fixed antenna. However, where electronic control units with immunity related functions and the associated wiring harness are predominantly in the rear half of the vehicle, the test should normally be carried out with the vehicle facing away from the antenna and positioned as if it had been horizontally rotated 180° around its centre point, i.e. such that the distance from the antenna to the nearest part of the outer body of the vehicle remains the same. In the case of long vehicles (i.e. excluding vehicles of categories L, M1 and N1), which have electronic control units with immunity related functions and associated wiring harness predominantly towards the middle of the vehicle, a reference point may be established based on either the right side surface or the left side surface of the vehicle. This reference point shall be at the midpoint of the vehicle's length or at one point along the side of the vehicle chosen by the manufacturer in conjunction with the Type Approval Authority after considering the distribution of electronic systems and the layout of any wiring harness.
    Such testing may only take place if the physical construction of the chamber permits. The antenna location shall be noted in the test report.

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A6  Appendix 1 a0c0
A6  Figure 1 a0c0
A6 

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A6  Figure 2 a0c0
A6 

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A6  Figure 3 a0c0
A6 

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A6  Figure 4 a0c0
A6  Vehicle in configuration "REESS charging mode coupled to the power grid" a0c0
A6 

Example of test setup for vehicle with socket located on vehicle side 
(charging mode 1 or 2, AC powered, without communication)

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A6  Figure 4a a0c0
A6 

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A6  Figure 4b a0c0
A6 

Legend:
1    Vehicle under test
2    Insulating support
3    Charging harness (including EVSE for charging mode 2)
4    AMN(s) or DC-charging-AN(s) grounded
5    Power mains socket

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A6 

Example of test setup for vehicle with socket located front / rear of vehicle side 
(charging mode 1 or 2, AC powered, without communication)

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A6  Figure 4c a0c0
A6 

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A6  Figure 4d a0c0
A6 

Legend:
1    Vehicle under test
2    Insulating support
3    Charging harness (including EVSE for charging mode 2)
4    AMN(s) or DC-charging-AN(s) grounded
5    Power mains socket

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A6 

Example of test setup for vehicle with socket located on vehicle side 
(charging mode 3 or mode 4, with communication)

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A6  Figure 4e a0c0
A6 

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A6  Figure 4f a0c0
A6 


Legend:
1    Vehicle under test
2    Insulating support
3    Charging harness with local/private communication lines
4    AMN(s) or DC-charging-AN(s) grounded
5    Power mains socket 
6    AAN(s) grounded (optional)
7    Charging station

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A6 

Example of test setup for vehicle with socket located front / rear of the vehicle side 
(charging mode 3 or mode 4, with communication)

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A6  Figure 4g a0c0
A6 

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A6  Figure 4h a0c0
A6 


Legend:
1    Vehicle under test
2    Insulating support
3    Charging harness with local/private communication lines 
4    AMN(s) or DC-charging-AN(s) grounded
5    Power mains socket 
6    AAN(s) grounded (optional)
7    Charging station

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A7  Annex 7 a0c0
A7  Method of measurement of radiated broadband electromagnetic emissions from electrical/electronic sub-assemblies (ESAs) a0c0
A7 1. General a0c0
A7 1.1. The test method described in this annex may be applied to ESAs, which may be subsequently fitted to vehicles, which comply with Annex 4. a0c0
A7  This method concerns both kinds of ESA: a0c0
A7  (a) Other ESAs than involved in "REESS charging mode coupled to the power grid". a0c0
A7  (b) ESAs involved in "REESS charging mode coupled to the power grid". a0c0
A7 1.2. Test method a0c0
A7  This test is intended to measure broadband electromagnetic emissions from ESAs (e.g. ignition systems, electric motor, onboard battery charging unit, etc.) a0c0
A7  If not otherwise stated in this annex the test shall be performed according CISPR 25. a0c0
A7 2. ESA state during tests a0c0
A7 2.1. The ESA under test shall be in normal operation mode, preferably in maximum load. a0c0
A7  ESAs involved in "REESS charging mode coupled to the power grid" shall be in charging mode. a0c0
A7  The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole frequency range measurement (this may lead to split the measurement in different sub-bands with the need to discharge the vehicle's traction battery before starting the next sub-bands) a0c0
A7 

If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging.
If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for DC charging unless another value is agreed with the type approval authorities [#new]

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A7 3. Test arrangements a0c0
A7 3.1. For ESA other than involved in "REESS charging mode coupled to the power grid" the test shall be performed according to the ALSE method described in paragraph 6.4. of CISPR 25. a0c0
A7 3.2. For ESAs in configuration "REESS charging mode coupled to the power grid" the test arrangement shall be according to Figure 2 of the appendix to this annex. a0c0
A7 3.2.1. The shielding configuration shall be according to the vehicle series configuration. Generally all shielded High Voltage (HV) parts shall be properly connected with low impedance to ground (e. g. AN, cables, connectors etc.). ESAs and loads shall be connected to ground. The external HV power supply shall be connected via feed-through-filtering. a0c0
A7 3.2.2.

The ESA power supply lead shall be connected to the power supply through an HV-AN (for ESA with DC HV supply) and/or AMN (for ESA with AC supply). 
DC HV supply shall be applied to the ESA via a 5 μH/50 Ω HV-AN (see Appendix 8 clause 2). 
AC supply shall be applied to the ESA via a 50 μH/50 Ω AMN (see Appendix 8 clause 4). [#new]

a0c0
A7 3.2.3.

Unless otherwise specified the length of the Low Voltage (LV) harness and the HV harness parallel to the front edge of the ground plane shall be 1,500 mm (±75 mm). The total length of the test harness including the connector shall be 1,700 mm (+300/-0 mm). The distance between the LV harness and the HV harness shall be 100 mm (+100/-0 mm).

a0c0
A7 3.2.4.

All of the harnesses shall be placed on a non-conductive, low relative permittivity material (εr ≤ 1.4), at 50 mm (±5 mm) above the ground plane.

a0c0
A7 3.2.5.

Shielded supply lines for HV+ and HV- line and three phase lines may be coaxial cables or in a common shield depending on the used plug system. The original HV-harness from the vehicle may be used optionally.

a0c0
A7 3.2.6.

Unless otherwise specified, the ESA case shall be connected to the ground plane either directly or via defined impedance.

a0c0
A7 3.2.7.

For onboard chargers, the AC/DC power lines shall be placed the furthest from the antenna (behind LV and HV harness). The distance between the AC/DC power lines and the closest harness (LV or HV) shall be 100 mm (+100/-0 mm).

a0c0
A7 3.3. Alternative measuring location a0c0
A7 

As an alternative to an absorber lined shielded enclosure (ALSE) an open area test site (OATS), which complies with the requirements of CISPR 16-1-4 may be used (see Figure 1 of the appendix to this annex).

a0c0
A7 3.4. Ambient a0c0
A7  To ensure that there is no extraneous noise or signal of a magnitude sufficient to affect materially the measurement, measurements shall be taken before or after the main test. In this measurement, the extraneous noise or signal shall be at least 6 dB below the limits of interference given in paragraph 6.5.2.1. of this Regulation, except for intentional narrowband ambient transmissions. a0c0
A7 4. Test requirements a0c0
A7 4.1.

The limits apply throughout the frequency range 30 to 1,000 MHz for measurements performed in an absorber lined shielded enclosure (ALSE) or open area test site (OATS).

a0c0
A7 4.2.

Measurements can be performed with either quasi-peak or peak detectors. The limits given in paragraphs 6.5. and 7.10. of this Regulation are for quasi-peak detectors. If peak detectors are used a correction factor of 20 dB as defined in CISPR 12 shall be applied.

a0c0
A7 4.3. The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in Table 1 and Table 2. a0c0
A7  Table 1 a0c0
A7  Spectrum analyser parameters a0c0
A7 
  Peak detector Quasi-peak detector Average detector
Frequency range MHz RBW at -3 dB  Minimum  scan  time RBW at -6 dB  Minimum  scan  time RBW at -3 dB Minimum scan  time
30 to 1,000 100/120 100 120 20 100/120 kHz 100
 kHz  ms/MHz  kHz  s/MHz  ms/MHz
a0c0
A7  Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth (RBW). a0c0
A7  Table 2 a0c0
A7  Scanning receiver parameters a0c0
A7 
Frequency range Peak detector Quasi-peak detector Average detector
MHz BW at Step Minimum dwell time BW at Step Minimum dwell time BW at Step Minimum dwell time
  -6 dB sizea -6 dB sizea -6 dB sizea
30 to 1,000 120 kHz 50 5 120 kHz 50 1 120 50 5
 kHz  ms  kHz  s  kHz  kHz  ms
a0c0
A7  a For purely broadband disturbances, the maximum frequency step size may be increased up to a value not greater than the bandwidth value. a0c0
A7  Note: For emissions generated by brush commutator motors without an electronic control unit, the maximum step size may be increased up to five times the bandwidth. a0c0
A7 4.4. Measurements a0c0
A7  Unless otherwise specified the configuration with the LV harness closer to the antenna shall be tested. a0c0
A7  The phase centre of the antenna shall be in line with the centre of the longitudinal part of the wiring harnesses for frequencies up to 1,000 MHz. a0c0
A7  The Technical Service shall perform the test at the intervals specified in the CISPR 12 standard throughout the frequency range 30 to 1,000 MHz. a0c0
A7  Alternatively, if the manufacturer provides measurement to data for the whole frequency band from a test laboratory accredited to the applicable parts of ISO 17025 and recognized by the Type Approval Authority, the Technical Service may divide the frequency range in 14 frequency bands 30-34, 34-45, 45-60, 60-80, 80-100, 100-130, 130-170, 170-225, 225-300, 300-400, 400-525, 525-700, 700-850 and 850- 1,000 MHz and perform tests at the 14 frequencies giving the highest emission levels within each band to confirm that the ESA meets the requirements of this annex. a0c0
A7  In the event that the limit is exceeded during the test, investigations shall be made to ensure that this is due to the ESA and not to background radiation. a0c0
A7 4.5. Readings a0c0
A7  The maximum of the readings relative to the limit (horizontal/vertical polarization) in each of the 14 frequency bands shall be taken as the characteristic reading at the frequency at which the measurements were made. a0c0
A7  Appendix a0c0
A7  Figure 1 a0c0
A7  Open area test site: Electrical/electronic sub-assembly test area boundary a0c0
A7  Level clear area free from electromagnetic reflecting surfaces a0c0
A7 

a0c0
A7  Figure 2 a0c0
A7  Test configuration for ESAs involved in "REESS charging mode coupled to the power grid" (example for biconical antenna) a0c0
A7 

Dimensions in millimetres

Legend:
1     ESA (grounded locally if required in test plan)
2     LV Test harness
3     LV Load simulator (placement and ground connection according to CISPR 25 paragraph 6.4.2.5)
4     Power supply (location optional)
5     LV Artificial network (AN)
6     Ground plane (bonded to shielded enclosure)
7     Low relative permittivity support (εr ≤ 1.4)
8     Biconical antenna
10     High-quality coaxial cable e.g. double-shielded (50 Ω) 
11     Bulkhead connector
12     Measuring instrument
13     RF absorber material
14     Stimulation and monitoring system 
15     HV harness
16     HV load simulator
17     HV AN
18     HV power supply
19     HV feed-through
25     AC/DC charger harness
26     AC/DC load simulator (e.g. Programmable Logic Controller (PLC))
27     AMN(s) or DC-charging-AN(s)
28     AC/DC power supply
29     AC/DC feed-through

a0c0
A8  Annex 8 a0c0
A8  Method of measurement of radiated narrowband electromagnetic emissions from electrical/electronic sub assemblies a0c0
A8 1. General a0c0
A8 1.1. The test method described in this annex may be applied to ESAs, which may be subsequently fitted to vehicles, which comply, with Annex 5. a0c0
A8  This method concerns only ESA other than those involved in "REESS charging mode coupled to the power grid". a0c0
A8 1.2. Test method a0c0
A8  This test is intended to measure the narrowband electromagnetic emissions such as might emanate from a microprocessor-based system. a0c0
A8  If not otherwise stated in this annex the test shall be performed according to CISPR 25. a0c0
A8 2. ESA state during tests a0c0
A8  The ESA under test shall be in normal operation mode, preferably in maximum load. a0c0
A8 3. Test arrangements a0c0
A8 3.1. The test shall be performed according to ALSE method described in paragraph 6.4. of CISPR 25. a0c0
A8 3.2. Alternative measuring location a0c0
A8  As an alternative to an absorber lined shielded enclosure (ALSE) an open area test site (OATS) which complies with the requirements of CISPR 16-1-4 may be used (see Figure 1 of the appendix to Annex 7). a0c0
A8 3.3. Ambient a0c0
A8  To ensure that there is no extraneous noise or signal of a magnitude sufficient to affect materially the measurement; measurements shall be taken before or after the main test. In this measurement, the extraneous noise or signal shall be at least 6 dB below the limits of interference given in paragraph 6.6.2.1. of this Regulation, except for intentional narrowband ambient transmissions. a0c0
A8 4. Test requirements a0c0
A8 4.1.

The limits apply throughout the frequency range 30 to 1,000 MHz for measurements performed in an absorber lined shielded enclosure (ALSE) or open area test site (OATS).

a0c0
A8 4.2. Measurements shall be performed with an average detector. a0c0
A8 4.3. The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in Tables 1 and 2. a0c0
A8  Table 1 a0c0
A8  Spectrum analyser parameters a0c0
A8 
Frequency range Peak detector Average detector
MHz RBW at Minimum scan time RBW at Minimum scan time
  -3 dB -3 dB
30 to 1,000 100/120 kHz 100  ms/MHz 100/120 kHz 100 ms/MHz
a0c0
A8  Note: If a spectrum analyser is used for peak measurements, the video band width shall be at least three times the resolution band width (RBW) a0c0
A8  Table 2 a0c0
A8  Scanning receiver parameters a0c0
A8 
Frequency range Peak detector Average detector
MHz BW at Step Minimum dwell time BW at Step Minimum dwell time
  -6 dB size -6 dB size
30 to 1,000 120 kHz 50 kHz 5 ms 120 kHz 50 kHz 5 ms
a0c0
A8 4.4. Measurements a0c0
A8  The Technical Service shall perform the test at the intervals specified in the CISPR 12 standard throughout the frequency range 30 to 1,000 MHz. a0c0
A8  Alternatively, if the manufacturer provides measurement to data for the whole frequency band from a test laboratory accredited to the applicable parts of ISO 17025 and recognized by the Type Approval Authority, the Technical Service may divide the frequency range in 14 frequency bands 30-34, 34-45, 45-60, 60-80, 80-100, 100-130, 130-170, 170-225, 225-300, 300-400, 400-525, 525-700, 700-850 and 850-1,000 MHz and perform tests at the 14 frequencies giving the highest emission levels within each band to confirm that the ESA meets the requirements of this annex. In the event that the limit is exceeded during the test, investigations shall be made to ensure that this is due to the ESA and not to background radiation including broadband radiation from the ESA. a0c0
A8 4.5. Readings a0c0
A8  The maximum of the readings relative to the limit (horizontal/vertical polarisation) in each of the 14 frequency bands shall be taken as the characteristic reading at the frequency at which the measurements were made. a0c0
A9  Annex 9 a0c0
A9  Method(s) of testing for immunity of electrical/electronic sub-assemblies to electromagnetic radiation a0c0
A9 1. General a0c0
A9 1.1. The test method(s) described in this annex applies to ESAs. a0c0
A9 1.2. Test methods a0c0
A9  This method concerns both kinds of ESA: a0c0
A9  (a) Other ESAs than involved in "REESS charging mode coupled to the power grid"; a0c0
A9  (b) ESAs involved in "REESS charging mode coupled to the power grid". a0c0
A9 1.2.1. ESAs may comply with the requirements of any combination of the following test methods at the manufacturer's discretion provided that these results in the full frequency range specified in paragraph 3.1. of this annex being covered: a0c0
A9  (a) Absorber chamber test according to ISO 11452-2; a0c0
A9  (b) TEM cell testing according to ISO 11452-3; a0c0
A9  (c) Bulk current injection testing according to ISO 11452-4; a0c0
A9  (d) Stripline testing according to ISO 11452-5; a0c0
A9  (e) 800 mm stripline according to paragraph 4.5. of this annex. a0c0
A9  ESAs in configuration "REESS charging mode coupled to the power grid" shall comply with the requirements of the combination of the Absorber chamber test according to ISO 11452-2 and Bulk current injection testing according to ISO 11452-4 at the manufacturer's discretion provided that these results in the full frequency range specified in paragraph 3.1. of this annex being covered. a0c0
A9  (Frequency range and general test conditions shall be based on ISO 11452-1). a0c0
A9 2. State of ESA during tests a0c0
A9 2.1. The test conditions shall be according ISO 11452-1. a0c0
A9 2.2. The ESA under test shall be switched on and shall be stimulated to be in normal operation condition. It shall be arranged as defined in this annex unless individual test methods dictate otherwise. a0c0
A9  ESAs involved in "REESS charging mode coupled to the power grid" shall be in charging mode. a0c0
A9  The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole frequency range measurement (this may lead to split the measurement in different sub-bands with the need to discharge the vehicle's traction battery before starting the next sub-bands). a0c0
A9  If the test is not performed with a REESS the ESA should be tested at rated current. If the current consumption can be adjusted, then the current shall be set to at least 20 per cent of its nominal value. a0c0
A9 2.3. Any extraneous equipment required to operate the ESA under test shall not be in place during the calibration phase. No extraneous equipment shall be closer than 1 m from the reference point during calibration. a0c0
A9 2.4. To ensure reproducible measurement results are obtained when tests and measurements are repeated, the test signal generating equipment and its layout shall be to the same specification as that used during each appropriate calibration phase. a0c0
A9 2.5. If the ESA under test consists of more than one unit, the interconnecting cables should ideally be the wiring harnesses as intended for use in the vehicle. If these are not available, the length between the electronic control unit and the AN shall be as defined in the standard. All cables in the wiring harness should be terminated as realistically as possible and preferably with real loads and actuators. a0c0
A9 3. General test requirements a0c0
A9 3.1. Frequency range, dwell times a0c0
A9  Measurements shall be made in the 20 to 2,000 MHz frequency range with frequency steps according to ISO 11452-1. a0c0
A9  The test signal modulation shall be: a0c0
A9  (a) AM (amplitude modulation), with 1 kHz modulation and 80 per cent modulation depth in the 20 to 800 MHz frequency range, and a0c0
A9  (b) PM (pulse modulation), Ton 577 µs, period 4,600 µs in the 800 to 2,000 MHz frequency range, a0c0
A9  If not otherwise agreed between Technical Service and ESA manufacturer. a0c0
A9  Frequency step size and dwell time shall be chosen according to ISO 11452-1. a0c0
A9 3.2. The Technical Service shall perform the test at the intervals specified in a0c0
A9  ISO 11452-1, throughout the frequency range 20 to 2,000 MHz. a0c0
A9  Alternatively, if the manufacturer provides measurement to data for the whole frequency band from a test laboratory accredited to the applicable parts of ISO 17025, and recognized by the Type Approval Authority, the Technical Service may choose a reduced number of spot frequencies in the range, e.g. 27, 45, 65, 90, 120, 150, 190, 230, 280, 380, 450, 600, 750, 900, 1,300, and 1,800 MHz to confirm that the ESA meets the requirements of this annex. a0c0
A9 3.3. If an ESA fails the tests defined in this annex, it shall be verified as having failed under the relevant test conditions and not as a result of the generation of uncontrolled fields. a0c0
A9 4. Specific test requirements a0c0
A9 4.1. Absorber chamber test a0c0
A9 4.1.1. Test method a0c0
A9  This test method allows the testing of vehicle electrical/electronic systems by exposing an ESA to electromagnetic radiation generated by an antenna. a0c0
A9 4.1.2. Test methodology a0c0
A9  The "substitution method" shall be used to establish the test field conditions according ISO 11452-2. a0c0
A9  The test shall be performed with vertical polarization. a0c0
A9 4.1.2.1. For ESAs in configuration "REESS charging mode coupled to the power grid" the test arrangement shall be according to Appendix 3 to this annex. a0c0
A9 4.1.2.1.1. The shielding configuration shall be according to the vehicle series configuration. Generally all shielded HV parts shall be properly connected with low impedance to ground (e. g. AN, cables, connectors etc.). ESAs and loads shall be connected to ground. The external HV power supply shall be connected via feed-through-filtering. a0c0
A9 4.1.2.1.2.

Unless otherwise specified the length of the LV harness and the HV harness parallel to the front edge of the ground plane shall be 1,500 mm (±75 mm). The total length of the test harness including the connector shall be 1,700 mm (+300/-0 mm). The distance between the LV harness and the HV harness shall be 100 mm (+100/-0 mm).

a0c0
A9 4.1.2.1.3.

All of the harnesses shall be placed on a non-conductive, low relative permittivity material (εr ≤ 1,4), at 50 mm (±5 mm) above the ground plane.

a0c0
A9 4.1.2.1.4. Shielded supply lines for HV+ and HV- line and three phase lines may be coaxial cables or in a common shield depending on the used plug system. The original HV-harness from the vehicle may be used optionally. a0c0
A9 4.1.2.1.5. Unless otherwise specified, the ESA case shall be connected to the ground plane either directly or via defined impedance. a0c0
A9 4.1.2.1.6. For onboard chargers, the AC/DC power lines shall be placed the furthest from the antenna (behind LV and HV harness). The distance between the AC/DC power lines and the closest harness (LV or HV) shall be 100 mm (+100/-0 mm). a0c0
A9 4.1.2.1.7. Unless otherwise specified, the configuration with the LV harness closer to the antenna shall be tested. a0c0
A9 4.2. TEM cell testing (see Appendix 2 to this annex) a0c0
A9 4.2.1. Test method a0c0
A9  The TEM (transverse electromagnetic mode) cell generates homogeneous fields between the internal conductor (septum) and housing (ground plane). a0c0
A9 4.2.2. Test methodology a0c0
A9  The test shall be performed according ISO 11452-3. a0c0
A9  Depending on the ESA to be tested the Technical Service shall chose the method of maximum field coupling to the ESA or to the wiring harness inside the TEM-cell. a0c0
A9 4.3. Bulk current injection testing a0c0
A9 4.3.1. Test method a0c0
A9  This is a method of carrying out immunity tests by inducing currents directly into a wiring harness using a current injection probe. a0c0
A9 4.3.2. Test methodology a0c0
A9 

The test shall be performed according to ISO 11452-4 on a test bench with the following characteristics:
-    BCI test method with substitution method and injection probe positioned at 150 mm distance to the ESA;
-    Or BCI test method with closed loop method and injection probe positioned at 900 mm distance to the ESA.
As an alternative the ESA may be tested while installed in the vehicle according to ISO 11451-4 with the following characteristics:
-    BCI test method with substitution method and injection probe positioned at 150 mm distance to the ESA. [#new]

a0c0
A9 4.3.2.1.

For ESAs in configuration "REESS charging mode coupled to the power grid", an example of test arrangement (for substitution method) is given in Appendix 4 to this annex (figure 1 for substitution method and figure 2 for closed loop method). [#new]

a0c0
A9 4.3.2.1.1. The shielding configuration shall be according to the vehicle series configuration. Generally all shielded HV parts shall be properly connected with low impedance to ground (e. g. AN, cables, connectors, etc.). ESAs and loads shall be connected to ground. The external HV power supply shall be connected via feed-through-filtering. a0c0
A9 4.3.2.1.2.

When using substitution method, unless otherwise specified the length of the LV harness and the HV harness shall be 1,700 mm (+300/-0 mm). The distance between the LV harness and the HV harness shall be 100 mm (+100/-0 mm). The HV/LV wiring harness shall be straight over at least 1,400 mm starting at the ESA for all test methods defined in part 4 of ISO 11452 except for the BCI test method using the closed-loop method with power limitation.
When using closed loop method, unless otherwise specified the length of the LV harness and the HV harness shall be 1,000 mm (+200/-0 mm). The distance between the LV harness and the HV harness shall be 100 mm (+100/-0 mm). The HV/LV wiring harness shall be straight over its entire length for the BCI test method using the closed-loop method with power limitation. [#new]

a0c0
A9 4.3.2.1.3.

All of the harnesses shall be placed on a non-conductive, low relative permittivity material (εr≤.4), at (50 ± 5) mm above the ground plane.

a0c0
A9 4.3.2.1.4. Shielded supply lines for HV+ and HV- line and three phase lines may be coaxial cables or in a common shield depending on the used plug system. The original HV-harness from the vehicle may be used optionally. a0c0
A9 4.3.2.1.5. Unless otherwise specified, the ESA case shall be connected to the ground plane either directly or via defined impedance. a0c0
A9 4.3.2.1.6. Unless otherwise specified the test shall be performed with the injection probe placed around each of the following harnesses: a0c0
A9  (a) Low voltage harness; a0c0
A9  (b) High voltage harness; a0c0
A9  (c) AC power lines if applicable; a0c0
A9  (d) DC power lines if applicable. a0c0
A9 4.4. Stripline testing a0c0
A9 4.4.1. Test method a0c0
A9  This test method consists of subjecting the wiring harness connecting the components in an ESA to specified field strengths. a0c0
A9 4.4.2. Test methodology a0c0
A9  The test shall be performed according to ISO 11452-5. a0c0
A9 4.5. 800 mm stripling testing a0c0
A9 4.5.1. Test method a0c0
A9  The stripline consists of two parallel metallic plates separated by 800 mm. Equipment under test is positioned centrally between the plates and subjected to an electromagnetic field (see Appendix 1 to this annex). a0c0
A9  This method can test complete electronic systems including sensors and actuators as well as the controller and wiring loom. It is suitable for apparatus whose largest dimension is less than one-third of the plate separation. a0c0
A9 4.5.2. Test methodology a0c0
A9 4.5.2.1. Positioning of stripline a0c0
A9  The stripline shall be housed in a screened room (to prevent external emissions) and positioned 2 m away from walls and any metallic enclosure to prevent electromagnetic reflections. RF absorber material may be used to damp these reflections. The stripline shall be placed on non-conducting supports at least 0.4 m above the floor. a0c0
A9 4.5.2.2. Calibration of the stripline a0c0
A9  A field-measuring probe shall be positioned within the central one-third of the longitudinal, vertical and transverse dimensions of the space between the parallel plates with the system under test absent. a0c0
A9  The associated measuring equipment shall be sited outside the screen room. At each desired test frequency, a level of power shall be fed into the stripline to produce the required field strength at the antenna. This level of forward power, or another parameter directly related to the forward power required to define the field, shall be used for type approval tests unless changes occur in the facilities or equipment, which necessitate this procedure being repeated. a0c0
A9 4.5.2.3. Installation of the ESA under test a0c0
A9  The main control unit shall be positioned within the central one third of the longitudinal, vertical and transverse dimensions of the space between the parallel plates. It shall be supported on a stand made from non-conducting material. a0c0
A9 4.5.2.4. Main wiring loom and sensor/actuator cables a0c0
A9  The main wiring loom and any sensor/actuator cables shall rise vertically from the control unit to the top ground plate (this helps to maximize coupling with the electromagnetic field). Then they shall follow the underside of the plate to one of its free edges where they shall loop over and follow the top of the ground plate as far as the connections to the stripline feed. The cables shall then be routed to the associated equipment, which shall be sited in an area outside the influence of the electromagnetic field, e.g. on the floor of the screened room 1 m longitudinally away from the stripline. a0c0
A9  Appendix 1 a0c0
A9  Figure 1 a0c0
A9  800-mm Stripline testing a0c0
A9 

a0c0
A9  Figure 2 a0c0
A9  800-mm stripline dimensions a0c0
A9 

a0c0
A9  Appendix 2 a0c0
A9  Typical TEM cell dimensions a0c0
A9  The following table shows the dimensions for constructing a cell with specified upper frequency limits: a0c0
A9 
Upper frequency Cell form factor Cell form factor Plate separation Septum
(MHz) W: b L/W b (cm) S (cm)
200 1.69 0.66 56 70
200 1.00 1 60 50
a0c0
A9  Appendix 3 a0c0
A9  Absorber chamber test a0c0
A9  Test configuration for ESA's involved in "REESS charging mode coupled to the power grid". The test shall be performed according to ISO 11452-2. a0c0
A9 

Figure 1
Example of test set-up for log-periodic antenna
         Top view                                                                                                 Dimensions in millimetres

Legend:        
1    ESA (grounded locally if required in test plan)    16    power line filter
2    ground plane    17    fibre optic feed through
3    low relative permittivity support (er ≤ 1.4); thickness 50 mm    18    bulk head connector
4    ground straps    19    stimulating and monitoring system
5    LV harness    20    RF signal generator and amplifier
6    HV lines (HV+, HV-)    21    high quality coaxial cable e.g. double shielded (50 Ω)
7    LV load simulator    22    optical fibre
8    impedance matching network (optional)    23    log-periodic antenna
9    LV AN    24    RF absorber material
10    HV AN    25    AC power mains
11    LV supply lines    26    AMN for AC power mains
12    HV supply lines    27    AC charging load simulator
13    LV power supply 12 V / 24 V / 48 V (placed on the bench)    28    50 Ω load
14    additional shielded box (optional)    29    AC lines
15    HV power supply (should be shielded if placed inside ALSE)        

a0c0
A9 

Figure 2
Example of test set-up for horn antenna
     Top view                                                                                                 Dimensions in millimetres

Legend:        
1    ESA (grounded locally if required in test plan)    16    power line filter
2    ground plane    17    fibre optic feed through
3    low relative permittivity support (er ≤ 1.4); thickness 50 mm    18    bulk head connector
4    ground straps    19    stimulating and monitoring system
5    LV harness    20    RF signal generator and amplifier
6    HV lines (HV+, HV-)    21    high quality coaxial cable e.g. double shielded (50 Ω)
7    LV load simulator    22    optical fibre
8    impedance matching network (optional)    23    horn antenna
9    LV AN    24    RF absorber material
10    HV AN    25    AC power mains
11    LV supply lines    26    AMN for AC power mains
12    HV supply lines    27    AC charging load simulator
13    LV power supply 12 V / 24 V / 48 V (placed on the bench)    28    50 Ω load
14    additional shielded box (optional)    29    AC lines
15    HV power supply (should be shielded if placed inside ALSE)        

a0c0
A9  Appendix 4 a0c0
A9  BCI test a0c0
A9  Test configuration for ESAs involved in "REESS charging mode coupled to the power grid". The test shall be performed according to ISO 11452-4. a0c0
A9 

Figure 1 
Example of test set-up for substitution method - Injection on LV (or HV or AC) lines for ESAs with shielded power supply systems and inverter/charger device (dimensions in millimetres)

    Legend:        
1    ESA    
2    ground plane    
3    low relative permittivity support (er ≤ 1,4); thickness 50 mm    
4    ground straps    
5    LV harness    
6    HV lines (HV+, HV-)    
7    LV load simulator    
8    impedance matching network (optional) (see ISO 11452-1)  
9    LV AN    
10    HV AN  
11    LV supply lines    
12    HV supply lines  
13    LV power supply 12 V / 24 V / 48 V (should be placed on the bench)    
14    additional shielded box       
15    HV power supply (should be shielded if placed inside ALSE)
16    power line filter
17    fibre optic feed through
18    bulk head connector
19    stimulating and monitoring system
20    injection probe
21    high frequency equipment (generator and amplifier)
22    optical fibre
23    50 Ω load
24    AC lines
25    AMN for AC power mains
26    AC charging load simulator
27    AC power mains

a0c0
A9 

Figure 2
Example of test set-up for closed loop method - Injection on LV (or HV or AC) lines for ESAs with shielded power supply systems and inverter/charger device (dimensions in millimetres)

    Legend:        
1    ESA    
2    ground plane    
3    low relative permittivity support (er ≤ 1,4); thickness 50 mm    
4    ground straps    
5    LV harness    
6    HV lines (HV+, HV-)    
7    LV load simulator    
8    impedance matching network (optional) (see ISO 11452-1)    
9    LV AN    
10    HV AN    
11    LV supply lines    
12    HV supply lines    
13    LV power supply 12 V / 24 V / 48 V (should be placed on the bench)    
14    additional shielded box    28    injection probe
15    HV power supply (should be shielded if placed inside ALSE)
16    power line filter
17    fibre optic feed through
18    bulk head connector
19    stimulating and monitoring system
20    measuring probe
21    high frequency equipment (generator, amplifier and spectrum analyser)
22    optical fibre
23    50 Ω load 
24    AC lines
25    AMN for AC power mains
26    AC charging load simulator
27    AC power mains

a0c0
A10  Annex 10 a0c0
A10  Method(s) of testing for immunity to and emission of transients of electrical/electronic sub-assemblies a0c0
A10 1. General a0c0
A10  This test method shall ensure the immunity of ESAs to conducted transients on the vehicle power supply and limit conducted transients from ESAs to the vehicle power supply. a0c0
A10 2. Immunity against transient disturbances conducted along 12/24 V supply lines. a0c0
A10  Apply the test pulses 1, 2a, 2b, 3a, 3b and 4 according to the International Standard ISO 7637-2 to the supply lines as well as to other connections of ESAs which may be operationally connected to supply lines. a0c0
A10 3. Emission of transient conducted disturbances generated by ESAs on 12/24 V supply lines a0c0
A10  Measurement according to the International Standard ISO 7637-2 on supply lines as well as to other connections of ESAs which may be operationally connected to supply lines. a0c0
A11 

Annex 11

a0c0
A11  Method(s) of testing for emission of harmonics generated on AC power lines from vehicle a0c0
A11 1. General a0c0
A11 1.1. The test method described in this annex shall be applied to vehicles in configuration "REESS charging mode coupled to the power grid" a0c0
A11 1.2. Test method a0c0
A11  This test is intended to measure the level of harmonics generated by vehicle in configuration "REESS charging mode coupled to the power grid" through its AC power lines in order to ensure it is compatible with residential, commercial and light industrial environments. a0c0
A11  If not otherwise stated in this annex the test shall be performed according to: a0c0
A11  (a) IEC 61000-3-2 for input current in charging mode ≤ 16 A per phase for class A equipment; a0c0
A11  (b) IEC 61000-3-12 for input current in charging mode-> 16 A and ≤ 75 A per phase. a0c0
A11 2. Vehicle state during tests a0c0
A11 2.1. The vehicle shall be in configuration "REESS charging mode coupled to the power grid". a0c0
A11 

The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole time duration of the measurement (this may lead to the measurement being splitting into different time slots with the need to discharge the vehicle’s traction battery before starting the next time slot). If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging.
In case of multiple batteries the average state of charge must be considered.

The vehicle shall be immobilized, the engine(s) (ICE and / or electrical engine) shall be OFF and in charging mode.

All other equipment which can be switched ON by the driver or passengers shall be OFF.

a0c0
A11 3. Test arrangements a0c0
A11 3.1.

The observation time to be used for the measurements shall be as for quasi-stationary equipment as defined in IEC 61000-3-2, Table 4.

a0c0
A11 3.2.

The test set-up for single phase / three-phase vehicle in configuration "REESS charging mode coupled to the power grid" is shown in Figure 1a to 1d of Appendix 1 to this annex.

a0c0
A11 4. Test requirements a0c0
A11 4.1. The measurements of even and odd current harmonics shall be performed up to the 40th harmonic. a0c0
A11 4.2. The limits for single phase or three-phase "REESS charging mode coupled to the power grid" with input current ≤ 16 A per phase are given in Table 3 of paragraph 7.3.2.1. of this Regulation. a0c0
A11 4.3.

The limits for single phase or other than balanced three-phase "REESS charging mode coupled to the power grid" with input current > 16 A and ≤ 75 A per phase are given in Table 4 of paragraph 7.3.2.2. of this Regulation.

a0c0
A11 4.4.

The limits for balanced three-phase "REESS charging mode coupled to the power grid" with input current > 16 A and ≤ 75 A per phase are given in Table 5 of paragraph 7.3.2.2. of this Regulation.

a0c0
A11 4.5. For three-phase "REESS charging mode coupled to the power grid" with input current > 16 A and ≤ 75 A per phase, when at least one of the three conditions a), b) or c) described in paragraph 5.2. of IEC 61000-3-12 is fulfilled, then the limits given in Table 6 of paragraph 7.3.2.2. of this Regulation can be applied. a0c0
A11  Appendix 1 a0c0
A11 

Figure 1
Vehicle in configuration "REESS charging mode coupled to the power grid"

a0c0
A11 

Example of test setup for vehicle with plug located on vehicle side
Figure 1a

a0c0
A11 

Figure 1b

Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     Harmonic analyzer
5     Power supply

a0c0
A11 

Example of test setup for vehicle with plug located front/rear of vehicle
Figure 1c

a0c0
A11 

Figure 1d

Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     Harmonic analyzer
5     Power supply

a0c0
A12  Annex 12 a0c0
A12  Method(s) of testing for emission of voltage changes, voltage fluctuations and flicker on AC power lines from vehicle a0c0
A12 1. General a0c0
A12 1.1. The test method described in this annex shall be applied to vehicles in configuration "REESS charging mode coupled to the power grid" a0c0
A12 1.2. Test method a0c0
A12  This test is intended to measure the level of voltage changes, voltage fluctuations and flicker generated by vehicle in configuration "REESS charging mode coupled to the power grid" through its AC power lines in order to ensure it is compatible with residential, commercial and light industrial environments. a0c0
A12  If not otherwise stated in this annex the test shall be performed according to: a0c0
A12  (a) IEC 61000-3-3 for rated current in "REESS charging mode" ≤ 16 A per phase and not subjected to conditional connection; a0c0
A12  (b) IEC 61000-3-11 for rated current in "REESS charging mode" > 16 A and ≤ 75 A per phase and subjected to conditional connection. a0c0
A12 2. Vehicle state during tests a0c0
A12 2.1. The vehicle shall be in configuration "REESS charging mode coupled to the power grid". a0c0
A12 

The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole time duration of the measurement (this may lead to the measurement being splitting into different time slots with the need to discharge the vehicle’s traction battery before starting the next time slot). If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging.
In case of multiple batteries the average state of charge must be considered.
The vehicle shall be immobilized, the engine(s) (ICE and / or electrical engine) shall be OFF and in charging mode.
All other equipment which can be switched ON by the driver or passengers shall be OFF.

a0c0
A12 3. Test arrangements a0c0
A12 3.1.

The tests for vehicle in configuration "REESS charging mode coupled to the power grid" with rated current ≤ 16 A per phase and not subjected to conditional connection shall be performed according to paragraph 6. of IEC 61000-3-3.

a0c0
A12 3.2. The tests for vehicle in configuration "REESS charging mode coupled to the power grid" with rated current > 16 A and ≤ 75 A per phase and subjected to conditional connection shall be performed according to paragraph 6. of IEC 61000-3-11. a0c0
A12 3.3.

The test set-up for vehicle in configuration "REESS charging mode coupled to the power grid" is shown in Figures 1a and 1d of Appendix 1 to this annex.

a0c0
A12 4. Test requirements a0c0
A12 4.1. The parameters to be determined in the time-domain are "short duration flicker value", "long duration flicker value" and "voltage relative variation". a0c0
A12 4.2. The limits for vehicle in configuration "REESS charging mode coupled to the power grid" with input current ≤ 16 A per phase and not subjected to conditional connection are given in paragraph 7.4.2.1. of this Regulation. a0c0
A12 4.3. The limits for vehicle in configuration "REESS charging mode coupled to the power grid" with input current > 16 A and ≤ 75 A per phase and subjected to conditional connection are given in paragraph 7.4.2.2. of this Regulation. a0c0
A12 

Annex 12 - Appendix 1

a0c0
A12 

Figure 1 
Vehicle in configuration "REESS charging mode coupled to the power grid"

a0c0
A12 

Example of test setup for vehicle with plug located on vehicle side
Figure 1a

a0c0
A12 

Figure 1b

Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     Flicker analyzer
5     Impedance simulator
6    Power supply

a0c0
A12 

Example of test setup for vehicle with plug located front/rear of vehicle
Figure 1c

a0c0
A12 

Figure 1d

Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     Flicker analyzer
5     Impedance simulator
6    Power supply

a0c0
A13  Annex 13 a0c0
A13  Method(s) of testing for emission of radiofrequency conducted disturbances on AC or DC power lines from vehicles a0c0
A13 1. General a0c0
A13 1.1. The test method described in this annex shall be applied to vehicles in configuration "REESS charging mode coupled to the power grid". a0c0
A13 1.2. Test method a0c0
A13  This test is intended to measure the level of radio frequency conducted disturbances generated by vehicle in configuration "REESS charging mode coupled to the power grid" through its AC or DC power lines in order to ensure it is compatible with residential, commercial and light industrial environments. a0c0
A13  If not otherwise stated in this annex the test shall be performed according to CISPR 16-2-1. a0c0
A13 2. Vehicle state during tests a0c0
A13 2.1. The vehicle shall be in configuration "REESS charging mode coupled to the power grid". a0c0
A13 

The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole frequency range measurement (this may lead to splitting the measurement in different sub-bands with the need to discharge the vehicle's traction battery before starting the next sub-bands).
If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging.
If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for DC charging unless another value is agreed with the type approval authorities.
In case of multiple batteries the average state of charge must be considered.
The vehicle shall be immobilized, the engine(s) (ICE and / or electrical engine) shall be OFF and in charging mode.
All other equipment which can be switched ON by the driver or passengers shall be OFF.

a0c0
A13 3. Test arrangements a0c0
A13 3.1. The test shall be performed according to paragraph 7.4.1. of CISPR 16-2-1 as floor-standing equipment. a0c0
A13 3.2.

Measuring location
A shielded enclosure or an absorber lined shielded enclosure (ALSE) or an open area test site (OATS) which complies with the requirements of CISPR 16-1-4 may be used.

a0c0
A13 3.3.

The artificial network(s) to be used for the measurement on vehicle are 
(a)    The AMN(s) defined in Appendix 8 clause 4 for AC power lines;
(b)    The DC-charging-AN(s) defined in Appendix 8 clause 3 for DC power lines.
Artificial networks
The AMN(s)/DC-charging-AN(s) shall be mounted directly on the ground plane. The cases of the AMN(s)/DC-charging-AN(s) shall be bonded to the ground plane.
The conducted emissions on AC and DC power lines are measured successively on each power line by connecting the measuring receiver on the measuring port of the related AMN/DC-charging-AN. The measuring port of the AMN/DC-charging-AN inserted in the other power line shall be terminated with a 50 Ω load.
The AMN(s)/DC-charging-AN(s) shall be placed as defined in Figures 1a to 1d. of Appendix 1 to this annex.

a0c0
A13 3.4.

The test set-up for the connection of the vehicle in configuration "REESS charging mode coupled to the power grid" is shown in Figure 1a to 1d of Appendix 1 to this annex.

a0c0
A13 3.5.

The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in Table 1 and Table 2.

a0c0
A13 

Table 1 
Spectrum analyser parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz RBW at Minimum scan RBW at Minimum scan RBW at Minimum scan
  -3 dB  time -6 dB  time -3 dB  time
0.15 to 30 09-ott 10 9 200 09-ott 10
 kHz  s/MHz  kHz  s/MHz  kHz  s/MHz

Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth (RBW) 

a0c0
A13 

Table 2 
Scanning receiver parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz BW at Step Minimum dwell BW at Step Minimum dwell BW at Step Minimum dwell
  -6 dB size   time -6 dB size  time -6 dB size  time
0.15 to 30 9  kHz 5 kHz 50  ms 9 kHz 5  kHz 1  s 9  kHz 5 kHz 50  ms

 

a0c0
A13 4. Test requirements a0c0
A13 4.1.

The limits apply throughout the frequency range 0.15 to 30 MHz for measurements performed in a shielded enclosure or an absorber lined shielded enclosure (ALSE) or an open area test site (OATS).

a0c0
A13 4.2. Measurements shall be performed with average and either quasi-peak or peak detectors. The limits are given in paragraph 7.5. of this Regulation. a0c0
A13  Table 7 for AC lines and Table 8 for DC lines. If peak detectors are used a correction factor of 20 dB as defined in CISPR 12 shall be applied. a0c0
A13 

Annex 13 - Appendix 1

a0c0
A13  Figure 1 a0c0
A13  Vehicle in configuration "REESS charging mode coupled to the power grid" a0c0
A13  Example of test setup for vehicle with plug located on vehicle side (AC powered without communication) a0c0
A13  Figure 1a a0c0
A13 

a0c0
A13  Figure1b a0c0
A13 


Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     AMN(s) or DC-charging-AN(s) grounded
5     Power mains socket
6     Measuring receiver

a0c0
A13  Vehicle in configuration "REESS charging mode coupled to the power grid" a0c0
A13  Example of test setup for vehicle with plug located front / rear of vehicle (AC powered without communication) a0c0
A13  Figure 1c a0c0
A13 

a0c0
A13  Figure 1d a0c0
A13 


Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     AMN(s) or DC-charging-AN(s) grounded 
5     Power mains socket 
6     Measuring receiver

a0c0
A14  Annex 14 a0c0
A14 

Method(s) of testing for emission of radiofrequency conducted disturbances on wired network port from vehicles

a0c0
A14 1. General a0c0
A14 1.1. The test method described in this annex shall be applied to vehicles in configuration "REESS charging mode coupled to the power grid". a0c0
A14 1.2. Test method a0c0
A14 

This test is intended to measure the level of radio frequency conducted disturbances generated by vehicle in configuration "REESS charging mode coupled to the power grid" through its wired network port in order to ensure it is compatible with residential, commercial and light industrial environments.

a0c0
A14  If not otherwise stated in this annex the test shall be performed according to CISPR 22. a0c0
A14 2. Vehicle/ state during tests a0c0
A14 2.1.

The vehicle shall be in configuration "REESS charging mode coupled to the power grid". The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole frequency range measurement (this may lead to splitting the measurement in different sub-bands with the need to discharge the vehicle's traction battery before starting the next sub-bands).
If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging.
If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for DC charging unless another value is agreed with the type approval authorities.
In case of multiple batteries the average state of charge must be considered.
The vehicle shall be immobilized, the engine(s) (ICE and / or electrical engine) shall be OFF and in charging mode.
All other equipment which can be switched ON by the driver or passengers shall be OFF.

a0c0
A14 3. Test arrangements a0c0
A14 3.1. The test set-up shall be performed according to paragraph 5. of CISPR 22 for conducted emissions. a0c0
A14 3.2.

Measuring location

A shielded enclosure or an absorber lined shielded enclosure (ALSE) or an open area test site (OATS) which complies with the requirements of CISPR 16-1-4 may be used.

a0c0
A14 3.3.

Local/private communication lines connected to signal/control ports and lines connected to wired network ports shall be applied to the vehicle through AAN(s).
The various AAN(s) to be used are defined in Appendix 8, clause 5:
-    Clause 5.1. for signal/control port with symmetric lines;
-    Clause 5.2. for wired network port with PLC on power lines;
-    Clause 5.3. for signal/control port with PLC (technology) on control pilot; and
-    Clause 5.4. for signal/control port with control pilot.
The AAN(s) shall be mounted directly on the ground plane. The case of the AAN(s) shall be bonded to the ground plane (ALSE) or connected to the protective earth (OTS, e.g. an earth rod).
The measuring port of each AAN shall be terminated with a 50 W load.
If a charging station is used, AAN(s) are not required for the signal/control ports and/or for the wired network ports. The local/private communication lines between the vehicle and the charging station shall be connected to the associated equipment on the charging station side to work as designed. If communication is emulated and if the presence of the AAN prevents proper communication then no AAN should be used.

a0c0
A14 3.4.

The test set-up for the connection of the vehicle in configuration "REESS charging mode coupled to the power grid" is shown in Figures 1a to 1d of Appendix 1 to this annex.
If it is impossible to guarantee the functionality of vehicle, due to introduction of AAN, an alternate method described in CISPR 22 (according to Figures 2a to 2d of Appendix 1 to this annex) shall be applied.

a0c0
A14 3.5.

The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in Table 1 and Table 2.

a0c0
A14 

Table 1
Spectrum analyser parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz RBW at Minimum scan RBW at Minimum scan RBW at Minimum scan
  -3 dB  time -6 dB  time -3 dB  time
0.15 to 30 9/10 kHz 10 s/MHz 9 kHz 200 s/MHz 9/10 kHz 10 s/MHz

Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth (RBW)

a0c0
A14 

Table 2 
Scanning receiver parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz BW at Step Minimum dwell BW at Step Minimum dwell BW at Step Minimum dwell
  -6 dB size  time -6 dB size  time -6 dB size a  time
0.15 to 30 9  kHz 5 kHz 50  ms 9 kHz 5  kHz 1 s 9 kHz 5 kHz 50 ms
a0c0
A14 4. Test requirements a0c0
A14 4.1.

The limits apply throughout the frequency range 0.15 to 30 MHz for measurements performed in a shielded enclosure or an absorber lined shielded enclosure (ALSE) or an open area test site (OATS).

a0c0
A14 4.2. Measurements shall be performed with average and either quasi-peak or peak detectors. The limits are given in Table 9 of paragraph 7.6. If peak detectors are used a correction factor of 20 dB as defined in CISPR 12 shall be applied. a0c0
A14 

Annex 14 - Appendix 1

a0c0
A14  Figure 1 a0c0
A14  Vehicle in configuration "REESS charging mode coupled to the power grid" a0c0
A14  Example of test setup for vehicle with plug located on vehicle side (AC or DC powered with communication) a0c0
A14  Figure 1a a0c0
A14 

a0c0
A14  Figure 1b a0c0
A14 

Legend:
1     Vehicle under test
2     Insulating support
3     Charging / communication harness
4     AMN(s) or DC-charging-AN(s) grounded    
5     Power mains socket 
6     AAN(s) grounded (for communication lines)
7     Charging station
8     Measuring receiver 

a0c0
A14  Vehicle in configuration "REESS charging mode coupled to the power grid" a0c0
A14  Example of test set-up for vehicle with plug located front/rear of vehicle (AC or DC powered with communication) a0c0
A14  Figure 1c a0c0
A14 

a0c0
A14  Figure 1d a0c0
A14 

Legend:
1     Vehicle under test
2     Insulating support
3     Charging / communication harness
4     AMN(s) or DC-charging-AN(s) grounded    
5     Power mains socket 
6     AAN(s) grounded (for communication lines)
7     Charging station
8     Measuring receiver 

a0c0
A14  Figure 2 a0c0
A14  Alternative measurement for vehicle in configuration "REESS charging mode coupled in the power grid" a0c0
A14  Example of test setup for vehicle with plug located on vehicle side (AC or DC powered with communication) a0c0
A14  Figure 2a a0c0
A14 

a0c0
A14  Figure 2b a0c0
A14 

Legend:
1     Vehicle under test
2     Insulating support
3     Charging / communication harness 
4     AMN(s) or DC-charging-AN(s) grounded 
5     Power mains socket     
7     Charging station
8     Current probe
9     Communication lines
10     Measuring receiver
11     Capacitive voltage probe

a0c0
A14  Alternative measurement for vehicle in configuration "REESS charging mode coupled in the power grid" a0c0
A14  Example of test setup for vehicle with plug located front / rear of vehicle (AC or DC powered with communication) a0c0
A14  Figure 2c a0c0
A14 

a0c0
A14  Figure 2d a0c0
A14 

Legend:
1     Vehicle under test
2     Insulating support
3     Charging / communication harness
4     AMN(s) or DC-charging-AN(s) grounded 
5     Power mains socket     
7     Charging station
8     Current probe (or capacitive voltage probe)
9     Communication lines
10     Measuring receiver
11     Capacitive voltage probe

a0c0
A15  Annex 15 a0c0
A15  Method of testing for immunity of vehicles to electrical fast transient/burst disturbances conducted along AC and DC power lines a0c0
A15 1. General a0c0
A15 1.1. The test method described in this annex shall only be applied to vehicles. This method concerns only the configuration of the vehicle with "REESS charging mode coupled to the power grid". a0c0
A15 1.2. Test method a0c0
A15  This test is intended to demonstrate the immunity of the vehicle electronic systems. The vehicle shall be subject to electrical fast transient/burst disturbances conducted along AC and DC power lines of the vehicle as described in this annex. The vehicle shall be monitored during the tests. a0c0
A15  If not otherwise stated in this annex the test shall be performed according to IEC 61000-4-4. a0c0
A15 2. Vehicle state during tests in configuration "REESS in charging mode coupled to the power grid" a0c0
A15 2.1. The vehicle shall be in an unladen condition except for necessary test equipment. a0c0
A15 2.1.1.

The vehicle shall be immobilized, the engine(s) (ICE and / or electrical engine) shall be OFF and in charging mode.

a0c0
A15 2.1.2. Basic vehicle conditions a0c0
A15  The paragraph defines minimum test conditions (as far as applicable) and failures criteria for vehicle immunity tests. Other vehicle systems, which can affect immunity related functions, shall be tested in a way to be agreed between manufacturer and Technical Service. a0c0
A15 
"REESS charging mode" vehicle test conditions Failure criteria
The REESS shall be in charging mode. The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole time duration of the measurement (this may lead to the measurement being split into different time slots with the need to discharge the vehicle’s traction battery before starting the next time slot). If the current consumption can be adjusted, then the current shall be set to at least 20 per cent of its nominal value. In case of multiple batteries the average state of charge must be considered. Vehicle sets in motion.
Unexpected release of the parking brake.
Loss of Parking position for automatic transmission.
a0c0
A15 2.1.3.

All other equipment which can be switched ON by the driver or passengers shall be OFF.

a0c0
A15 2.2. Only non-perturbing equipment shall be used while monitoring the vehicle. The vehicle exterior and the passenger compartment shall be monitored to determine whether the requirements of this annex are met (e.g. by using (a) video camera(s), a microphone, etc.). a0c0
A15 3. Test equipment a0c0
A15 3.1. The test equipment is composed of a reference ground plane (a shielded room is not required), a transient/burst generator, Coupling/Decoupling Network (CDN) and capacitive coupling clamp. a0c0
A15 3.2. The transient/burst generator shall meet the condition defined in paragraph 6.1. of IEC 61000-4-4. a0c0
A15 3.3. The Coupling/Decoupling Network shall meet the condition defined in paragraph 6.2. of IEC 61000-4-4. When the Coupling/Decoupling Network cannot be used on AC or DC power lines, the capacitive coupling clamp defined in paragraph 6.3. of IEC 61000-4-4 can be used. a0c0
A15 4. Test setup a0c0
A15 4.1. The vehicle test setup is based on the laboratory type setup as described in paragraph 7.2. of IEC 61000-4-4. a0c0
A15 4.2. The vehicle shall be placed directly on the ground plane. a0c0
A15 4.3.

The Technical Service shall perform the test as specified in paragraph 7.8.2.1. of this Regulation.

a0c0
A15  Alternatively, if the manufacturer provides measurement from a test laboratory accredited to the applicable parts of ISO 17025 and recognized by the Type Approval Authority, the Technical Service may choose not to perform the test to confirm that the vehicle meets the requirements of this annex. a0c0
A15 5. Generation of required test level a0c0
A15 5.1. Test methodology a0c0
A15 5.1.1. The test method according to IEC 61000-4-4 shall be used to establish the test level requirements. a0c0
A15 5.1.2. Test phase a0c0
A15 

The vehicle shall be positioned on the ground plane. The electrical fast transient/burst (EFT/B) shall be applied on the vehicle on the AC/DC power lines in common modes by using CDN as described in Figure 1a to 1d of Appendix 1 to this annex.

a0c0
A15  The test set-up shall be noted in the test report. a0c0
A15 

Annex 15 - Appendix 1

a0c0
A15  Figure 1 a0c0
A15 

Vehicle in configuration "REESS charging mode coupled to the power grid"
Example of test setup for vehicle with plug located on vehicle side

a0c0
A15 

Figure 1a

a0c0
A15 

Figure 1b

Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     CDN 
5     Fast Transients / Burst generator
6    Power supply

a0c0
A15 

Example of test setup for vehicle with plug located front/rear of vehicle
Figure 1c

a0c0
A15 

Figure 1d

Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     CDN 
5     Fast Transients / Burst generator
6    Power supply

a0c0
A16  Annex 16 a0c0
A16  Method of testing for immunity of vehicles to surges conducted along AC and DC power lines a0c0
A16 1. General a0c0
A16 1.1. The test method described in this annex shall only be applied to vehicles. This method concerns only the configuration of the vehicle with "REESS charging mode coupled to the power grid". a0c0
A16 1.2. Test method a0c0
A16  This test is intended to demonstrate the immunity of the vehicle electronic systems. The vehicle shall be subject to surges conducted along AC and DC power lines of the vehicle as described in this annex. The vehicle shall be monitored during the tests. a0c0
A16 

If not otherwise stated in this annex the test shall be performed according to IEC 61000-4-5 for lightning transients (clause 4.2)

a0c0
A16 2. Vehicle state during tests in configuration "REESS in charging mode coupled to the power grid" a0c0
A16 2.1. The vehicle shall be in an unladen condition except for necessary test equipment. a0c0
A16 2.1.1.

The vehicle shall be immobilized, the engine(s) (ICE and / or electrical engine) shall be OFF and in charging mode.

a0c0
A16 2.1.2. Basic vehicle conditions a0c0
A16  The paragraph defines minimum test conditions (as far as applicable) and failures criteria for vehicle immunity tests. Other vehicle systems, which can affect immunity related functions, shall be tested in a way to be agreed between manufacturer and Technical Service. a0c0
A16 
"REESS charging mode" vehicle test conditions Failure criteria
The REESS shall be in charging mode. The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole time duration of the measurement (this may lead to the measurement being split into different time slots with the need to discharge the vehicle’s traction battery before starting the next time slot).. If the current consumption can be adjusted, then the current shall be set to at least 20 per cent of its nominal value.
In case of multiple batteries the average state of charge must be considered.
Vehicle sets in motion.
Unexpected release of the parking brake.
Loss of  Parking position for automatic transmission.
a0c0
A16 2.1.3.

All other equipment which can be switched ON by the driver or passengers shall be OFF.

a0c0
A16 2.2. Only non-perturbing equipment shall be used while monitoring the vehicle. The vehicle exterior and the passenger compartment shall be monitored to determine whether the requirements of this annex are met (e.g. by using (a) video camera(s), a microphone, etc.). a0c0
A16 3. Test equipment a0c0
A16 3.1. The test equipment is composed of a reference ground plane (a shielded room is not required), a surge generator and a Coupling/Decoupling Network (CDN). a0c0
A16 3.2. The surge generator shall meet the condition defined in paragraph 6.1. of IEC 61000-4-5. a0c0
A16 3.3. The Coupling/Decoupling Network shall meet the condition defined in paragraph 6.3. of IEC 61000-4-5. a0c0
A16 4. Test setup a0c0
A16 4.1. The vehicle test setup is based on the setup described in paragraph 7.2. of IEC 61000-4-5. a0c0
A16 4.2. The vehicle shall be placed directly on the ground plane. a0c0
A16 4.3.

The Technical Service shall perform the test as specified in paragraph 7.9.2.1. of this Regulation.

a0c0
A16  Alternatively, if the manufacturer provides measurement from a test laboratory accredited to the applicable parts of ISO 17025 and recognized by the Type Approval Authority, the Technical Service may choose not to perform the test to confirm that the vehicle meets the requirements of this annex. a0c0
A16 5. Generation of required test level a0c0
A16 5.1. Test methodology a0c0
A16 5.1.1. The test method according to IEC 61000-4-5 shall be used to establish the test level requirements. a0c0
A16 5.1.2. Test phase a0c0
A16 

The vehicle shall be positioned on the ground plane. The electrical surge shall be applied on the vehicle on the AC/DC power lines between each line and earth and between lines by using CDN as described in Figures 1a to 1d of Appendix 1 to this annex,

a0c0
A16  The test setup shall be noted in the test report. a0c0
A16 

Annex 16 - Appendix 1

a0c0
A16  Vehicle in configuration "REESS charging mode coupled to the power grid" a0c0
A16  Figure 1 a0c0
A16 

Vehicle in configuration "REESS charging mode coupled to the power grid"

a0c0
A16 

Example of test setup for vehicle with plug located on vehicle side
Figure 1a

a0c0
A16 

 

Figure 1b

Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     CDN
5     Surge generator
6     Power supply
Example of test setup for vehicle with plug located front/rear of vehicle

a0c0
A16 

Figure 1c

a0c0
A16 

Figure 1d

Legend:
1     Vehicle under test
2     Insulating support
3     Charging harness
4     CDN
5     Surge generator
6     Power supply

a0c0
A17  Annex 17 a0c0
A17  Method(s) of testing for emission of harmonics generated on AC power lines from an ESA a0c0
A17 1. General a0c0
A17 1.1. The test method described in this annex shall be applied to ESAs in configuration "REESS charging mode coupled to the power grid" a0c0
A17 1.2. Test method a0c0
A17  This test is intended to measure the level of harmonics generated by an ESA in configuration "REESS charging mode coupled to the power grid" through its AC power lines in order to ensure it is compatible with residential, commercial and light industrial environments. a0c0
A17  If not otherwise stated in this annex the test shall be performed according to: a0c0
A17  (a) IEC 61000-3-2 for input current in charging mode ≤ 16 A per phase for class A equipment; a0c0
A17  (b) IEC 61000-3-12 for input current in charging mode > 16 A and ≤ 75 A per phase. a0c0
A17 2. ESA state during tests a0c0
A17 2.1. The ESA shall be in configuration "REESS charging mode coupled to the power grid". a0c0
A17  The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole time duration of the measurement (this may lead to the measurement being split into different time slots with the need to discharge the vehicle's traction battery before starting the next time slot). a0c0
A17 

If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging. 

a0c0
A17 3. Test arrangements a0c0
A17 3.1. The observation time to be used for the measurements shall be as for quasi-stationary equipment as defined in Table 4 of IEC 61000-3-2. a0c0
A17 3.2. The test set-up for single phase ESA in configuration "REESS charging mode coupled to the power grid" is shown in Figure 1 of Appendix 1 to this annex. a0c0
A17 3.3. The test set-up for three-phase ESA in configuration "REESS charging mode coupled to the power grid" is shown in Figure 2 of Appendix 1 to this annex. a0c0
A17 4. Test requirements a0c0
A17 4.1. The measurements of even and odd current harmonics shall be performed up to the 40th harmonic. a0c0
A17 4.2. The limits for single phase or three-phase ESAs in configuration "REESS charging mode coupled to the power grid" with input current ≤ 16 A per phase are given in Table 10 of paragraph 7.11.2.1. of this Regulation. a0c0
A17 4.3.

The limits for single phase or other than balanced three-phase ESAs in configuration "REESS charging mode coupled to the power grid" with input current > 16 A and ≤ 75 A per phase are given in Table 11 of paragraph 7.11.2.2. of this Regulation.

a0c0
A17 4.4.

The limits for balanced three-phase ESAs in configuration "REESS charging mode coupled to the power grid" with input current > 16 A and ≤ 75 A per phase are given in paragraph Table 12 of 7.11.2.2. of this Regulation.

a0c0
A17 4.5. For three-phase ESAs in configuration "REESS charging mode coupled to the power grid" with input current > 16 A and ≤ 75 A per phase, when at least one of the three conditions a), b) or c) described in paragraph 5.2. of a0c0
A17  IEC 61000-3-12 is fulfilled, then the limits given in Table 13 of paragraph 7.11.2.2. of this Regulation can be applied. a0c0
A17 

Annex 17 - Appendix 1

a0c0
A17  Figure 1 a0c0
A17  ESA in configuration "REESS charging mode coupled to the power grid" - Single phase test set-up a0c0
A17 

a0c0
A17  Figure 2 a0c0
A17  ESA in configuration "REESS charging mode coupled to the power grid" -Three-phase test set-up a0c0
A17 

a0c0
A18  Annex 18 a0c0
A18  Method(s) of testing for emission of voltage changes, voltage fluctuations and flicker on AC power lines from an ESA a0c0
A18 1. General a0c0
A18 1.1. The test method described in this annex shall be applied to ESAs in configuration "REESS charging mode coupled to the power grid" a0c0
A18 1.2. Test method a0c0
A18  This test is intended to measure the level of voltage changes, voltage fluctuations and flicker generated by ESA in configuration "REESS charging mode coupled to the power grid" through its AC power lines in order to ensure it is compatible with residential, commercial and light industrial environments. a0c0
A18  If not otherwise stated in this annex the test shall be performed according to: a0c0
A18  (a) IEC 61000-3-3 for rated current in "REESS charging mode" ≤ 16 A per phase and not subjected to conditional connection; a0c0
A18  (b) IEC 61000-3-11 for rated current in "REESS charging mode" > 16 A and ≤ 75 A per phase and subjected to conditional connection a0c0
A18 2. ESA state during tests a0c0
A18 2.1. The ESA shall be in configuration "REESS charging mode coupled to the power grid" a0c0
A18  The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole time duration of the measurement (this may lead to the measurement being split into different time slots with the need to discharge the vehicle's traction battery before starting the next time slot). a0c0
A18 

If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging. 

a0c0
A18 3. Test Arrangements a0c0
A18 3.1. The tests for ESA in configuration "REESS charging mode coupled to the power grid" with rated current ≤ 16 A per phase and not subjected to conditional connection shall be performed according to paragraph 4. of IEC 61000-3-3. a0c0
A18 3.2. The tests for ESA in configuration "REESS charging mode coupled to the power grid" with rated current > 16 A and ≤ 75 A per phase and subjected to conditional connection shall be performed according to paragraph 6. of IEC 61000-3-11. a0c0
A18 3.3. The test set-up for ESA in configuration "REESS charging mode coupled to the power grid" is shown in Figures 1a and 1b of Appendix 1 to this annex. a0c0
A18 4. Test requirements a0c0
A18 4.1. The parameters to be determined in the time-domain are "short duration flicker value", "long duration flicker value" and "voltage relative variation". a0c0
A18 4.2. The limits for ESA in configuration "REESS charging mode coupled to the power grid" with input current ≤ 16 A per phase and not subjected to conditional connection are given in paragraph 7.12.2.1. of this Regulation. a0c0
A18 4.3. The limits for ESA in configuration "REESS charging mode coupled to the power grid" with input current > 16 A and ≤ 75 A per phase and subjected to conditional connection are given in paragraph 7.12.2.2. of this Regulation. a0c0
A18  Appendix 1 a0c0
A18  Figure 1a a0c0
A18  ESA in configuration "REESS charging mode coupled to the power grid"- Single phase test set-up a0c0
A18 

a0c0
A18  Figure 1b a0c0
A18  ESA in configuration "REESS charging mode coupled to the power grid" - Three-phase test set-up a0c0
A18 

a0c0
A19  Annex 19 a0c0
A19  Method(s) of testing for emission of radiofrequency conducted disturbances on AC or DC power lines from an ESA a0c0
A19 1. General a0c0
A19 1.1. The test method described in this annex shall be applied to ESAs in configuration "REESS charging mode coupled to the power grid". a0c0
A19 1.2. Test method a0c0
A19  This test is intended to measure the level of radio frequency conducted disturbances generated by ESA in configuration "REESS charging mode coupled to the power grid" through its AC or DC power lines in order to ensure it is compatible with residential, commercial and light industrial environments. a0c0
A19  If not otherwise stated in this annex the test shall be performed according to CISPR 16-2-1. a0c0
A19 2. ESA state during tests a0c0
A19 2.1. The ESA shall be in configuration "REESS charging mode coupled to the power grid". a0c0
A19  The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole frequency range measurement (this may lead to split the measurement in different sub-bands with the need to discharge the vehicle's traction battery before starting the next sub-bands). a0c0
A19 

If the test is not performed with a REESS the ESA should be tested at rated current. 
If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging.
If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for DC charging unless another value is  agreed with the type approval authorities.

a0c0
A19 3.1.

The artificial network(s) to be used for the measurement on vehicle are 
(a)    The AMN(s) defined in Appendix 8 clause 4 for AC power lines;
(b)    The DC-charging-AN(s) defined in Appendix 8 clause 3 for DC power lines.
Artificial networks
The AMN(s)/DC-charging-AN(s) shall be mounted directly on the ground plane. The cases of the AMN(s)/DC-charging-AN(s) shall be bonded to the ground plane.
The conducted emissions on AC and DC power lines are measured successively on each power line by connecting the measuring receiver on the measuring port of the related AMN/DC-charging-AN. The measuring port of the AMN/DC-charging-AN inserted in the other power lines shall be terminated with a 50 Ω load.
The AMN(s)/DC-charging-AN(s) shall be placed in front, aligned and on the same side of the vehicle power charging plug.
16-1-4 may be used.

a0c0
A19 3.2.

Measuring location
A shielded enclosure or an absorber lined shielded enclosure (ALSE) or an open area test site (OATS) which complies with the requirements of CISPR 16-1-4 may be used.

a0c0
A19 3.3.

The test set-up (floor-standing equipment) for the connection of the ESAs in configuration "REESS charging mode coupled to the power grid" is shown in Figure 1 of Appendix 1 to this annex.

a0c0
A19 3.4.

The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in Table 1 and Table 2.

a0c0
A19 

Table 1 
Spectrum analyser parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz RBW at Minimum scan RBW at Minimum scan RBW at Minimum scan
  -3 dB time -6 dB time -3 dB time
0.15 to 30 09/10 kHz 10 s/MHz 9 kHz 200 s/MHz 09/10 kHz 10 s/MHz

Note: If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth (RBW) 

a0c0
A19 

Table 2 
Scanning receiver parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz BW at Step Minimum dwell BW at Step Minimum dwell BW at Step Minimum dwell
  -6 dB size time -6 dB size time -6 dB size time
0.15 to 30 9 5 50 9 5 1 9 5 50
 kHz  kHz  ms  kHz  kHz  s  kHz  kHz  ms
a0c0
A19 4. Test Requirements a0c0
A19 4.1

The limits apply throughout the frequency range 0.15 to 30 MHz for measurements performed in a shielded enclosure or an absorber lined shielded enclosure (ALSE) or an open area test site (OATS). 

a0c0
A19 4.2 Measurements shall be performed with average and either quasi-peak or peak detectors. The limits are given in Table 14 of paragraph 7.13.2.1. of this Regulation for AC lines and in Table 15 of paragraph 7.13.2.2. of this Regulation for DC lines. If peak detectors are used a correction factor of 20 dB as defined in CISPR 12 shall be applied. a0c0
A19  Appendix 1 a0c0
A19  Figure 1 a0c0
A19 

ESA in configuration "REESS charging mode coupled to the power grid" (floor-standing equipment)

a0c0
A19 

Legend:
1     ESA under test
2     Insulating support
3     Charging harness
4     AMN(s) or DC-charging-AN(s) grounded
5     Power mains socket 
6     Measuring receiver
7     Ground plane

a0c0
A20  Annex 20 a0c0
A20 

Method(s) of testing for emission of radiofrequency conducted disturbances on wired network port from an ESA

a0c0
A20 1. General a0c0
A20 1.1. The test method described in this annex shall be applied to ESAs in configuration "REESS charging mode coupled to the power grid". a0c0
A20 1.2. Test method a0c0
A20 

This test is intended to measure the level of radio frequency conducted disturbances generated by ESA in configuration "REESS charging mode coupled to the power grid" through its wired network port in order to ensure it is compatible with residential, commercial and light industrial environments.

a0c0
A20  If not otherwise stated in this annex the test shall be performed according to CISPR 22. a0c0
A20 2. ESA state during tests a0c0
A20 2.1. The ESA shall be in configuration "REESS charging mode coupled to the power grid". a0c0
A20  The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole frequency range measurement (this may lead to split the measurement in different sub-bands with the need to discharge the vehicle's traction battery before starting the next sub-bands). a0c0
A20 

If the test is not performed with a REESS the ESA should be tested at rated current.

If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for AC charging.
If the current consumption can be adjusted, then the current shall be set to at least 80 per cent of its nominal value for DC charging unless another value is  agreed with the type approval authorities.

a0c0
A20 3. Test arrangements a0c0
A20 3.1.

Local/private communication lines connected to signal/control ports and lines connected to wired network ports shall be applied to the vehicle through AAN(s).
The various AAN(s) to be used are defined in Appendix 8, clause 5:
-    Clause 5.1. for signal/control port with symmetric lines;
-    Clause 5.2. for wired network port with PLC on power lines;
-    Clause 5.3. for signal/control port with PLC (technology) on control pilot; and
-    Clause 5.4. for signal/control port with control pilot.
The AAN(s) shall be mounted directly on the ground plane. The case of the AAN(s) shall be bonded to the ground plane (ALSE) or connected to the protective earth (OTS, e.g. an earth rod).
The measuring port of each AAN shall be terminated with a 50 W load.
If a charging station is used, AAN(s) are not required for the signal/control ports and/or for the wired network ports. The local/private communication lines between the vehicle and the charging station shall be connected to the associated equipment on the charging station side to work as designed. If communication is emulated and if the presence of the AAN prevents proper communication then no AAN should be used

a0c0
A20 3.2.

Measuring location
A shielded enclosure or an absorber lined shielded enclosure (ALSE) or an open area test site (OATS) which complies with the requirements of CISPR 16-1-4 may be used.

a0c0
A20 3.3.

The test set-up (floor-standing equipment) for the connection of the ESA in configuration "REESS charging mode coupled to the power grid" is shown in Figure 1 of Appendix 1 to this annex.

a0c0
A20 3.4.

The measurements shall be performed with a spectrum analyser or a scanning receiver. The parameters to be used are defined in Table 1 and Table 2.

a0c0
A20 

Table 1 
Spectrum analyser parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz RBW at Minimum scan RBW at Minimum scan RBW at Minimum scan
  -3 dB time -6 dB time -3 dB time
0.15 to 30 09/10 kHz 10 s/MHz 9 kHz 200 s/MHz 09/10 kHz 10 s/MHz

Note: 
If a spectrum analyser is used for peak measurements, the video bandwidth shall be at least three times the resolution bandwidth (RBW).

a0c0
A20 

Table 2 
Scanning receiver parameters

Frequency range Peak detector Quasi-peak detector Average detector
MHz BW at Step Minimum dwell BW at Step Minimum dwell BW at Step Minimum dwell
  -6 dB size time -6 dB size time -6 dB size time
0.15 to 30 9 5 50 9 5 1 9 5 50
 kHz  kHz  ms  kHz  kHz  s  kHz  kHz  ms
a0c0
A20 4. Test requirements a0c0
A20 4.1.

The limits apply throughout the frequency range 0.15 to 30 MHz for measurements performed in a shielded enclosure or an absorber lined shielded enclosure (ALSE) or an open area test site (OATS).

a0c0
A20 4.2. Measurements shall be performed with average and either quasi-peak or peak detectors. The limits are given in Table 16 of paragraph 7.14.2.1. of this Regulation. If peak detectors are used a correction factor of 20 dB as defined in CISPR 12 shall be applied. a0c0
A20  Appendix 1 a0c0
A20  Figure 1 a0c0
A20 

ESA in configuration "REESS charging mode coupled to the power grid"
(floor-standing equipment)

a0c0
A20 


Legend:
1     ESA under test
2     Insulating support
3     Charging / communication harness
4     AMN(s) or DC-charging-AN(s) grounded
5     Power mains socket 
6     AAN(s)
7     Charging station
8    Measuring receiver
9    Ground plane

a0c0
A21  Annex 21 a0c0
A21  Method of testing for immunity of an ESA to Electrical Fast Transient/Burst disturbances conducted along AC and DC power lines a0c0
A21 1. General a0c0
A21 1.1. The test method described in this annex shall only be applied to ESAs. This method applies only to ESA in configuration "REESS charging mode coupled to the power grid". a0c0
A21 1.2. Test method a0c0
A21  This test is intended to demonstrate the immunity of the ESA. The ESA shall be subject to Electrical Fast Transient/Burst disturbances conducted along AC and DC power lines of the ESA as described in this annex. The ESA shall be monitored during the tests. a0c0
A21  If not otherwise stated in this annex the test shall be performed according to IEC 61000-4-4. a0c0
A21 2. ESA state during tests in configuration "REESS in charging mode coupled to the power grid" a0c0
A21 2.1. Basic ESA conditions a0c0
A21  The paragraph defines minimum test conditions (as far as applicable) and failures criteria for ESA immunity tests. a0c0
A21 
"REESS charging mode" ESA test conditions Failure criteria
ESA shall be in configuration "REESS charging mode coupled to the power grid".
The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole time duration of the measurement (this may lead to the measurement being split into different time slots with the need to discharge the vehicle’s traction battery before starting the next time slot).
If the current consumption can be adjusted, then the current shall be set to at least 20 per cent of its nominal value. 
Incorrect charging condition
(e.g. over-current, overvoltage)
a0c0
A21 2.2. Only non-perturbing equipment shall be used while monitoring the ESA. The ESA shall be monitored to determine whether the requirements of this annex are met (e.g. by using (a) video camera(s), a microphone, etc.). a0c0
A21 3. Test equipment a0c0
A21 3.1.

The test equipment is composed of a reference ground plane (a shielded room is not required), a transient / burst generator, Coupling/Decoupling Network (CDN) and capacitive coupling clamp.

a0c0
A21 3.2. The transient/burst generator shall meet the condition defined in paragraph 6.1. of IEC 61000-4-4. a0c0
A21 3.3. The Coupling/Decoupling Network shall meet the condition defined in paragraph 6.2. of IEC 61000-4-4. When the Coupling/Decoupling Network cannot be used on AC or DC power lines, the capacitive coupling clamp defined in paragraph 6.3. of IEC 61000-4-4 can be used. a0c0
A21 4. Test set-up a0c0
A21 4.1. The ESA test setup is based on the laboratory type set-up as described in paragraph 7.2. of IEC 61000-4-4. a0c0
A21 4.2. The ESA shall be placed directly on the ground plane. a0c0
A21 4.3. The Technical Service shall perform the test as specified in paragraph 7.15.2.1. of this Regulation. a0c0
A21  Alternatively, if the manufacturer provides measurement from a test laboratory accredited to the applicable parts of ISO 17025 and recognized by the Type Approval Authority, the Technical Service may choose not to perform the test to confirm that the ESA meets the requirements of this annex. a0c0
A21 5. Generation of required test level a0c0
A21 5.1. Test methodology a0c0
A21 5.1.1. The test method according to IEC 61000-4-4 shall be used to establish the test level requirements. a0c0
A21 5.1.2. Test phase a0c0
A21  The ESA shall be positioned on the ground plane. The Electrical Fast Transient/Burst (EFT/B) shall be applied on the ESA on the AC/DC power lines in common modes by using CDN as described in Figure 1 of Appendix 1 to this annex. a0c0
A21  The test setup shall be noted in the test report. a0c0
A21  Appendix 1 a0c0
A21  Figure 1 a0c0
A21  ESA in configuration "REESS charging mode coupled to the power grid" a0c0
A21 

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A22  Annex 22 a0c0
A22  Method of testing for immunity of ESAs to surges conducted along AC and DC power lines a0c0
A22 1. General a0c0
A22 1.1. The test method described in this annex shall only be applied to ESAs. This method applies only to ESAs in configuration "REESS charging mode coupled to the power grid". a0c0
A22 1.2. Test method a0c0
A22  This test is intended to demonstrate the immunity of the ESA. The ESA shall be subject to surges conducted along AC and DC power lines of the ESA as described in this annex. The ESA shall be monitored during the tests. a0c0
A22  If not otherwise stated in this annex the test shall be performed according to IEC 61000-4-5. a0c0
A22 2. ESA state during tests in configuration "REESS in charging mode coupled to the power grid" a0c0
A22 2.1. The ESA shall be in charging mode. a0c0
A22 2.1.2. Basic ESA conditions a0c0
A22  The paragraph defines minimum test conditions (as far as applicable) and failures criteria for ESA immunity tests. a0c0
A22 
"REESS charging mode" ESA test conditions Failure criteria
ESA shall be in configuration "REESS charging mode coupled to the power grid".
The state of charge (SOC) of the traction battery shall be kept between 20 per cent and 80 per cent of the maximum SOC during the whole frequency range measurement (this may lead to split the measurement in different sub-bands with the need to discharge the vehicle's traction battery before starting the next sub-bands).
If the test is not performed with a REESS the ESA should be tested at rated current. If the current consumption can be adjusted, then the current shall be set to at least 20 per cent of its nominal value. 
Incorrect charging condition
(e.g. over-current, overvoltage)
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A22 2.2. Only non-perturbing equipment shall be used while monitoring the ESA. The ESA shall be monitored to determine whether the requirements of this annex are met (e.g. by using (a) video camera(s), a microphone, etc.). a0c0
A22 3. Test equipment a0c0
A22 3.1. The test equipment is composed of a reference ground plane (a shielded room is not required), a surge generator and a Coupling/Decoupling Network (CDN). a0c0
A22 3.2. The surge generator shall meet the condition defined in paragraph 6.1. of IEC 61000-4-5. a0c0
A22 3.3. The Coupling/Decoupling Network shall meet the condition defined in paragraph 6.3. of IEC 61000-4-5. a0c0
A22 4. Test set-up a0c0
A22 4.1. The ESA test set-up is based on the set-up described in paragraph 7.2. of IEC 61000-4-5. a0c0
A22 4.2. The ESA shall be placed directly on the ground plane. a0c0
A22 4.3. The Technical Service shall perform the test as specified in paragraph 7.16.2.1. of this Regulation. a0c0
A22  Alternatively, if the manufacturer provides measurement from a test laboratory accredited to the applicable parts of ISO 17025 and recognized by the Type Approval Authority, the Technical Service may choose not to perform the test to confirm that the ESA meets the requirements of this annex. a0c0
A22 5. Generation of required test level a0c0
A22 5.1. Test methodology a0c0
A22 5.1.1. The test method according to IEC 61000-4-5 shall be used to establish the test level requirements. a0c0
A22 5.1.2. Test phase a0c0
A22  The ESA shall be positioned on the ground plane. The electrical surge shall be applied on the ESA on the AC/DC power lines between each line and earth and between lines by using CDN as described in Figures 1 to 4 of Appendix 1 to this annex. a0c0
A22  The test set-up shall be noted in the test report a0c0
A22  Appendix 1 a0c0
A22  ESA in configuration "REESS charging mode coupled to the power grid" a0c0
A22  Figure 1 a0c0
A22  ESA in configuration "REESS charging mode coupled to the power grid" - Coupling between lines for DC or AC (single phase) power lines a0c0
A22 

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A22  Figure 2 a0c0
A22  ESA in configuration "REESS charging mode coupled to the power grid" - Coupling between each line and earth for DC or AC (single phase) power lines a0c0
A22 

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A22  Figure 3 a0c0
A22  ESA in configuration "REESS charging mode coupled to the power grid" - Coupling between lines for AC (three phases) power lines a0c0
A22 

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A22  Figure 4 a0c0
A22  ESA in configuration "REESS charging mode coupled to the power grid" - Coupling between each line and earth for AC (three phases) power lines a0c0
A22 

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