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    ISO 2635 AMD 1-2017 Aircraft - Conductors for general purpose aircraft electrical cables and aerospace applications - Dimensions and characteristics - Amendment.pdf

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    ISO 2635 AMD 1-2017 Aircraft - Conductors for general purpose aircraft electrical cables and aerospace applications - Dimensions and characteristics - Amendment.pdf

    1、 ISO 2017 Aircraft Conductors for general purpose aircraft electrical cables and aerospace applications Dimensions and characteristics AMENDMENT 1: Correction of table 1 Aronefs Conducteurs pour cbles lectriques pour usage gnral aronautique et pour applications arospatiales Dimensions et caractristi

    2、ques AMENDEMENT 1: Correction du tableau 1 INTERNATIONAL STANDARD ISO 2635 Second edition 2003-11-15 Reference number ISO 2635:2003/Amd.1:2017(E) AMENDMENT 1 2017-06 ISO 2635:2003/Amd.1:2017(E)ii ISO 2017 All rights reserved COPYRIGHT PROTECTED DOCUMENT ISO 2017, Published in Switzerland All rights

    3、reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized otherwise in any form or by any means, electronic or mechanical, including photocopying, or posting on the internet or an intranet, without prior written permission. Permission can be requested from eithe

    4、r ISO at the address below or ISOs member body in the country of the requester. ISO copyright office Ch. de Blandonnet 8 CP 401 CH-1214 Vernier, Geneva, Switzerland Tel. +41 22 749 01 11 Fax +41 22 749 09 47 copyrightiso.org www.iso.org ISO 2635:2003/Amd.1:2017(E) Foreword ISO (the International Org

    5、anization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing International Standards is normally carried out through ISO technical committees. Each member body interested in a subject for which a technical committee has been establi

    6、shed has the right to be represented on that committee. International organizations, governmental and non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardizatio

    7、n. The procedures used to develop this document and those intended for its further maintenance are described in the ISO/IEC Directives, Part 1. In particular, the different approval criteria needed for the different types of ISO documents should be noted. This document was drafted in accordance with

    8、 the editorial rules of the ISO/IEC Directives, Part 2 (see www .iso .org/ directives). Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights. Details of an

    9、y patent rights identified during the development of the document will be in the Introduction and/or on the ISO list of patent declarations received (see www .iso .org/ patents). Any trade name used in this document is information given for the convenience of users and does not constitute an endorse

    10、ment. For an explanation on the voluntary nature of standards, the meaning of ISO specific terms and expressions related to conformity assessment, as well as information about ISOs adherence to the World Trade Organization (WTO) principles in the Technical Barriers to Trade (TBT), see the following

    11、URL: w w w . i s o .org/ iso/ foreword .html. This document was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 1, Aerospace electrical requirements. ISO 2017 All rights reserved iii Aircraft Conductors for general purpose aircraft electrical cables and aerosp

    12、ace applications Dimensions and characteristics AMENDMENT 1: Correction of table 1 7.2, Table 1 Replace Table 1 with the following: Table 1 Conductor, electric cable, in copper and copper alloy Con- ductor code Nominal cross-sec- tional area Approxi- mate wire gauge with reference to AWG Number of s

    13、trands in con- ductor Nomi- nal strand size Conductor diameter Electrical resistance at 20 C Max. Mechanical properties Types A and C Types B and D Elonga- tion Mass per unit length Ulti- mate break- ing load Min. Max. Min. Max. Min. mm 2 mm mm mm /km /km % kg/km N 001 a 0,15 26 19 0,10 0,46 0,53 14

    14、9 160 6 1,6 46 002 a 0,25 24 19 0,12 0,55 0,62 106 114 6 2,18 67 004 0,4 22 19 0,15 0,70 0,80 55,3 60 10 3,43 71 006 0,6 20 19 0,20 0,94 1,04 31 33,2 10 5,95 127 010 1 18 19 0,25 1,18 1,29 19,6 21,1 10 9,16 198 012 1,2 16 19 0,30 1,39 1,53 13,6 14,5 10 13,2 285 020 2 14 37 0,25 1,68 1,82 10,2 10,9 1

    15、0 18 385 030 3 12 37 0,32 2,12 2,28 6,4 6,8 10 28,5 645 050 5 10 37 0,40 2,69 2,88 4 4,2 10 46 1 000 090 9 8 127 0,30 4,40 2,3 2,4 10 87 140 14 6 27 7 0,30 5,50 1,5 1,55 10 133 220 22 4 37 12 0,25 6,80 0,91 0,94 10 216 340 34 2 37 19 0,25 8,60 0,585 0,62 10 342 420 42 1 37 23 0,25 9,50 0,48 0,5 10 4

    16、14 530 53 0 37 29 0,25 10,70 0,375 0,39 10 526 680 68 00 37 37 0,25 12,10 0,295 0,305 10 685 850 85 000 48 36 0,25 13,60 0,233 0,24 10 849 107 107 0 000 61 36 0,25 15,20 0,183 0,19 10 1 090 aHigh-strength copper alloy ISO 2635:2003/Amd.1:2017(E) ISO 2017 All rights reserved 1 ISO 2635:2003/Amd.1:2017(E) ISO 2017 All rights reserved IC S 49.060 Price based on 1 page


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