EN 60952-1-2013 en Aircraft batteries - Part 1 General test requirements and performance levels.pdf

1、BSI Standards PublicationAircraft BatteriesPart 1: General test requirements and performance levelsBS EN 60952-1:2013National forewordThis British Standard is the UK implementation of EN 60952-1:2013. It isidentical to IEC 60952-1:2013. It supersedes BS EN 60952-1:2004, which willbe withdrawn on 13

2、August 2016.The UK participation in its preparation was entrusted to TechnicalCommittee PEL/21, Secondary cells and batteries.A list of organizations represented on this committee can be obtained onrequest to its secretary.This publication does not purport to include all the necessary provisions ofa

3、 contract. Users are responsible for its correct application. The British Standards Institution 2013Published by BSI Standards Limited 2013ISBN 978 0 580 74609 3ICS 29.220.20; 49.060Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published un

4、der the authority of theStandards Policy and Strategy Committee on 30 November 2013.Amendments/corrigenda issued since publicationDate Text affectedBRITISH STANDARDBS EN 60952-1:2013EUROPEAN STANDARD EN 60952-1 NORME EUROPENNE EUROPISCHE NORM October 2013 CENELEC European Committee for Electrotechni

5、cal Standardization Comit Europen de Normalisation Electrotechnique Europisches Komitee fr Elektrotechnische Normung CEN-CENELEC Management Centre: Avenue Marnix 17, B - 1000 Brussels 2013 CENELEC - All rights of exploitation in any form and by any means reserved worldwide for CENELEC members. Ref.

6、No. EN 60952-1:2013 E ICS 29.220.20; 49.060 Supersedes EN 60952-1:2004 English version Aircraft batteries - Part 1: General test requirements and performance levels (IEC 60952-1:2013) Batteries daronefs - Partie 1: Exigences gnrales dessais et niveaux de performances (CEI 60952-1:2013) Flugzeugbatte

7、rien - Teil 1: Allgemeine Prfverfahren und Leistungsmerkmale (IEC 60952-1:2013) This European Standard was approved by CENELEC on 2013-08-13. CENELEC members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a

8、 national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CENELEC member. This European Standard exists in three official versions (English, French, Germa

9、n). A version in any other language made by translation under the responsibility of a CENELEC member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CENELEC members are the national electrotechnical committees of Austria, Belgium,

10、 Bulgaria, Croatia, Cyprus, the Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, the Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Sw

11、itzerland, Turkey and the United Kingdom. BS EN 60952-1:2013EN 60952-1:2013 - 2 - Foreword The text of document 21/803/FDIS, future edition 3 of IEC 60952-1, prepared by IEC/TC 21 “Secondary cells and batteries“ was submitted to the IEC-CENELEC parallel vote and approved by CENELEC as EN 60952-1:201

12、3. The following dates are fixed: latest date by which the document has to be implemented at national level by publication of an identical national standard or by endorsement (dop) 2014-05-13 latest date by which the national standards conflicting with the document have to be withdrawn (dow) 2016-08

13、-13 This document supersedes EN 60952-1:2004. EN 60952-1:2013 includes the following significant technical changes with respect to EN 60952-1:2004: Additional test requirements to meet the needs of the regulatory airworthiness authorities for both product performance and qualification. Attention is

14、drawn to the possibility that some of the elements of this document may be the subject of patent rights. CENELEC and/or CEN shall not be held responsible for identifying any or all such patent rights. Endorsement notice The text of the International Standard IEC 60952-1:2013 was approved by CENELEC

15、as a European Standard without any modification. In the official version, for Bibliography, the following notes have to be added for the standards indicated: IEC 61434 NOTE Harmonised as EN 61434. ISO 266:1997 NOTE Harmonised as EN ISO 266:1997 (not modified). ISO 9000:2005 NOTE Harmonised as EN ISO

16、 9000:2005 (not modified). BS EN 60952-1:2013- 3 - EN 60952-1:2013 Annex ZA (normative) Normative references to international publications with their corresponding European publications The following documents, in whole or in part, are normatively referenced in this document and are indispensable fo

17、r its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. NOTE When an international publication has been modified by common modifications, indicated by (mod), the relevant EN/HD

18、applies. Publication Year Title EN/HD Year IEC 60051-1 - Direct acting indicating analogue electrical measuring instruments and their accessories - Part 1: Definitions and general requirements common to all parts EN 60051-1 - IEC 60051-2 - Direct acting indicating analogue electrical measuring instr

19、uments and their accessories - Part 2: Special requirements for ammeters and voltmeters EN 60051-2 - IEC 60485 - Digital electronic d.c. voltmeters and d.c. electronic analogue-to-digital converters - - IEC 60952-2 2013 Aircraft batteries - Part 2: Design and construction requirements EN 60952-2 201

20、3 IEC 60952-3 2013 Aircraft batteries - Part 3: Product specification and declaration of design and performance (DDP) EN 60952-3 2013 ISO 2859 Series Sampling procedures for inspection by attributes - - ISO 7137 - Aircraft - Environmental conditions and test procedures for airborne equipment - - RTC

21、A DO-160 2010 Environmental Conditions and Test Procedures for Airborne Equipment - - SAE AIR 1377A-80 - Aerospace Information Report - Fire Test Equipment for Flexible Hose and Tube Assemblies - - SAE AS 1055B 1978 Aerospace Standard - Fire Testing of Flexible hose, Tube Assemblies, Coils, Fittings

22、 and Similar System Components - - U.S Federal Test Method, Standard N191A/Federal Test Method 5906 1978 Flammability (Horizontal Test) - - BS EN 60952-1:2013 2 60952-1 IEC:2013 CONTENTS INTRODUCTION . 7 1 Scope . 8 2 Normative references 8 3 Terms and definitions . 9 4 Test conditions and measuring

23、 apparatus . 10 4.1 General test conditions 10 4.2 Measuring apparatus . 10 4.2.1 General . 10 4.2.2 Voltage measurement 10 4.2.3 Current measurement 11 4.2.4 Temperature measurement 11 4.2.5 Time measurement 11 4.2.6 Additional test equipment . 11 4.2.7 Mass test equipment 11 4.3 Charging method .

24、11 4.4 Physical examination . 11 5 Electrical requirements and test procedures 11 5.1 Capacity tests at the 1 I1rate 11 5.1.1 Rated capacity C111 5.1.2 Initial capacity requirement for vented and valve regulated nickel-cadmium batteries . 12 5.1.3 Capacity at 1 I1 and 18 C 12 5.1.4 Capacity at 1 I1a

25、nd 30 C 12 5.1.5 Capacity at 1 I1and 50 C . 12 5.2 Constant voltage discharge 12 5.2.1 General . 12 5.2.2 Constant voltage 12 5.2.3 Constant voltage discharge (14 V) 13 5.3 Rapid discharge capacity . 14 5.3.1 Rapid discharge capacity at 23 C 14 5.3.2 Rapid discharge capacity at 30 C 14 5.4 Charge re

26、tention 14 5.5 Storage . 15 5.6 Charge stability 15 5.7 Short-circuit test 15 5.8 Charge acceptance 16 5.8.1 General . 16 5.8.2 Ambient temperature (23 C) 16 5.8.3 Low temperature (only for batteries fitted with heaters) . 16 5.9 Insulation resistance and dielectric strength . 17 5.9.1 General . 17

27、5.9.2 Insulation resistance 17 5.9.3 Dielectric strength 17 5.10 Duty cycle performance . 17 5.11 Water consumption test . 18 BS EN 60952-1:201360952-1 IEC:2013 3 5.12 Overcharge endurance 19 5.13 Cyclic endurance . 19 5.14 Deep discharge test . 19 5.15 Induced destructive overcharge . 20 5.16 Elect

28、rical emissions . 20 6 Environmental requirements 20 6.1 Vibration 20 6.1.1 General . 20 6.1.2 Battery mounting 21 6.1.3 Declaration 21 6.1.4 Vibration requirements . 21 6.2 Acceleration 22 6.3 Operational shock and crash safety . 23 6.3.1 Operational shock 23 6.3.2 Crash safety 23 6.3.3 Declaration

29、 23 6.4 Explosion containment . 23 6.5 Gas emission . 24 6.6 Altitude pressure . 24 6.7 Temperature variation (shock) . 25 6.8 Fungus resistance . 25 6.8.1 General . 25 6.8.2 General method . 25 6.9 Humidity 26 6.10 Fluid contamination 26 6.10.1 General . 26 6.10.2 Spray test 26 6.10.3 Immersion tes

30、t . 27 6.11 Salt spray 27 6.12 Physical integrity at high temperature (85 C) . 28 6.13 Flammability 28 6.13.1 General . 28 6.13.2 Flame resistant test . 28 6.13.3 Fire resistance . 29 6.13.4 Fire proof test 29 6.14 Electrolyte resistance . 29 6.15 Temperature sensors . 30 6.16 Component qualificatio

31、n tests 30 6.16.1 General . 30 6.16.2 Vent valve test . 30 6.16.3 Cell container test 31 6.16.4 Battery electrolyte containment test 32 6.17 Battery airtightness test (where applicable) 33 6.18 Strength of connector receptacle Connector types C and Q . 33 6.19 Handle strength test. 34 6.20 Hazardous

32、 materials 34 6.21 Instructions for continued airworthiness . 34 6.22 Limitations . 34 6.23 Electronics 34 BS EN 60952-1:2013 4 60952-1 IEC:2013 6.24 Impact resistance (non-metallic battery container) 34 6.25 Special test requirements 35 7 Quality assurance requirements 35 7.1 General quality assura

33、nce requirements 35 7.2 Approval requirements . 35 7.2.1 General requirements 35 7.2.2 Order of testing 35 7.2.3 Maintenance of approval 36 7.2.4 Declaration of design and performance 36 7.2.5 Qualification approval 36 7.2.6 Quality conformance 36 Bibliography 39 Figure 1 Vibration orientation 21 Ta

34、ble 1 Acceleration conditions 22 Table 2 Impact resistance requirements . 35 Table 3 Approval test schedule . 38 BS EN 60952-1:201360952-1 IEC:2013 7 INTRODUCTION The IEC 60952 series defines minimum environmental and performance requirements for establishing a qualification standard for airworthine

35、ss of lead-acid and nickel-cadmium aircraft batteries, which contain corrosive electrolytes. The series defines test procedures for determining battery performance. The electrical test results may be used to establish airworthiness in a particular application. For all tests, the manufacturer declare

36、s the minimum performance for each battery type. The requirements of IEC 60952 for aircraft batteries are divided into three parts: Part 1 defines test procedures for the evaluation, comparison and qualification of batteries and states minimum environmental performance levels for airworthiness. Part

37、 2 defines the design requirements for aircraft batteries as well as their format (shape and size) and the range of aircraft interface connectors that are used. Part 3 defines the product specification which is used to define specific requirements for an application and a declaration of design and p

38、erformance (DDP), which details the performance of a battery format when tested to Part 1. BS EN 60952-1:2013 8 60952-1 IEC:2013 AIRCRAFT BATTERIES Part 1: General test requirements and performance levels 1 Scope This part of the IEC 60952 series defines test procedures for the evaluation, compariso

39、n and qualification of batteries and states minimum performance and environmental levels for airworthiness. Where specific tests are defined with no pass/fail requirement (to establish performance capability), the manufacturers declared values, from qualification testing, will be used to establish m

40、inimum requirements for ongoing maintenance of approval for that design of battery. To provide representative examples, this standard utilises voltage and current values based upon an aircraft electrical system nominally rated at 28 V d.c. Additionally, the nominal values for cell voltage are assume

41、d to be 1,2 V per cell for nickel-cadmium batteries and 2,0 V per cell for lead-acid batteries. The specific topics addressed in this part of IEC 60952 serve to establish acceptable quality standards required to qualify a battery as airworthy. In cases where the requirements for a specific applicati

42、on exceed those detailed in this standard, the purchaser will detail said requirements in the product specification and the method of establishing compliance. It is recognised that additional data may be required by other organisations (national standards bodies, AECMA, SAE etc.). The present standa

43、rd can be used as a framework to devise tests for generation of the required data. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For und

44、ated references, the latest edition of the referenced document (including any amendments) applies. IEC 60051-1, Direct acting indicating analogue electrical measuring instruments and their accessories Part 1: Definitions and general requirements common to all parts IEC 60051-2, Direct acting indicat

45、ing analogue electrical measuring instruments and their accessories Part 2: Special requirements for ammeters and voltmeters IEC 60485, Digital electronic d.c. voltmeters and d.c. electronic analogue-to-digital convertors1IEC 60952-2:2013, Aircraft batteries Part 2: Design and construction requireme

46、nts IEC 60952-3:2013, Aircraft batteries Part 3: Product specification and declaration of design and performance (DDP)2_ 1Withdrawn. 2The first edition (1993) was published under the title Aircraft batteries Part 3: External electric connectors BS EN 60952-1:201360952-1 IEC:2013 9 ISO 2859 (all part

47、s), Sampling procedures for inspection by attributes ISO 7137, Aircraft Environmental conditions and test procedures for airborne equipment RTCA DO-160:2010, Environmental Conditions and Test Procedures for Airborne Equipment U.S. Federal Test Method, Standard No. 191A / Federal Test Method 5906: 19

48、78, Flammability (Horizontal Test) SAE AIR 1377A-80, Aerospace Information Report Fire Test Equipment for Flexible Hose and Tube Assemblies SAE AS 1055B:1978, Aerospace Standard Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings and Similar System Components 3 Terms and definitions For

49、the purposes of this document, the following terms and definitions apply. 3.1 current value value of current in ampere (A) used to charge and discharge cells and batteries, expressed as a multiple of the capacity EXAMPLE For example, a current of 20 A used to charge a cell with a rated capacity C (Ah) of 100 Ah would be expressed as C/5 or 0,2 C (A). Note 1 to entry: IEC 61434 is equally applicable to both nickel-cadmium and lead-acid and therefore the reference current (