ImageVerifierCode 换一换
格式:PDF , 页数:14 ,大小:607.69KB ,
资源ID:549818      下载积分:10000 积分
快捷下载
登录下载
邮箱/手机:
温馨提示:
如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
如填写123,账号就是123,密码也是123。
特别说明:
请自助下载,系统不会自动发送文件的哦; 如果您已付费,想二次下载,请登录后访问:我的下载记录
支付方式: 支付宝扫码支付 微信扫码支付   
注意:如需开发票,请勿充值!
验证码:   换一换

加入VIP,免费下载
 

温馨提示:由于个人手机设置不同,如果发现不能下载,请复制以下地址【http://www.mydoc123.com/d-549818.html】到电脑端继续下载(重复下载不扣费)。

已注册用户请登录:
账号:
密码:
验证码:   换一换
  忘记密码?
三方登录: 微信登录  

下载须知

1: 本站所有资源如无特殊说明,都需要本地电脑安装OFFICE2007和PDF阅读器。
2: 试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。
3: 文件的所有权益归上传用户所有。
4. 未经权益所有人同意不得将文件中的内容挪作商业或盈利用途。
5. 本站仅提供交流平台,并不能对任何下载内容负责。
6. 下载文件中如有侵权或不适当内容,请与我们联系,我们立即纠正。
7. 本站不保证下载资源的准确性、安全性和完整性, 同时也不承担用户因使用这些下载资源对自己和他人造成任何形式的伤害或损失。

版权提示 | 免责声明

本文(BS EN 2283-2010 Aerospace series Testing of aircraft wiring《航空航天系列 航空布线试验》.pdf)为本站会员(arrownail386)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

BS EN 2283-2010 Aerospace series Testing of aircraft wiring《航空航天系列 航空布线试验》.pdf

1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS EN 2283:2010Aerospace series Testing ofaircraft wiringBS EN 2283:2010 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 2283:2010. Itsupers

2、edes BS EN 2283:1996 which is withdrawn.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/6, Aerospace avionic electrical and fibre optictechnology.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not

3、 purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. BSI 2010ISBN 978 0 580 63472 7ICS 49.060Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStand

4、ards Policy and Strategy Committee on 31 December 2010.Amendments issued since publicationDate Text affectedBS EN 2283:2010EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2283 December 2010 ICS 49.060 Supersedes EN 2283:1996English Version Aerospace series - Testing of aircraft wiring Srie aros

5、patiale - Vrification des cblages daronefs Luft- und Raumfahrt - Prfung der Verkabelung von Luftfahrzeugen This European Standard was approved by CEN on 4 March 2010. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Sta

6、ndard the status of a 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 CEN member. This European Standard exists in three official versions (Engli

7、sh, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, B

8、ulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE

9、FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2010 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2283:2010: EBS EN 2283:2010EN 2283:2010 (E)

10、 2 Contents Page Foreword 3Introduction .41 Scope 42 Normative references 43 Terms and definitions .54 Tests 54.1 General 54.2 Continuity .54.3 Dielectric strength .54.4 Insulation resistance .64.5 Test preparation .65 Procedures .65.1 General 65.2 Testing of wiring in production 85.2.1 Continuity .

11、85.2.2 Dielectric strength .85.3 Testing of assembled and installed bundles 86 Requirements .87 Test report 8BS EN 2283:2010EN 2283:2010 (E) 3 Foreword This document (EN 2283:2010) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enq

12、uiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a nation

13、al standard, either by publication of an identical text or by endorsement, at the latest by June 2011, and conflicting national standards shall be withdrawn at the latest by June 2011. This document supersedes EN 2283:1996. Attention is drawn to the possibility that some of the elements of this docu

14、ment may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard:

15、Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingd

16、om. BS EN 2283:2010EN 2283:2010 (E) 4 Introduction Due to the diversity of aircraft, manufacturing and installing methods for wiring, the tests defined in Clause 1 are carried out at different stages in the manufacturing programme: after assembly of cables into bundles before installation in the air

17、craft; after installation of bundles into the aircraft; after repairs or modifications. 1 Scope This European Standard specifies: the tests for finished wiring, including connectors and, if necessary, terminals, terminal ends, junction boxes, circuit breakers, etc.; these tests do not concern equipm

18、ent installed in the aircraft (see operation of systems and do not apply to the wiring used instrumentation; the requirements for verification of aircraft electrical wiring; continuity of circuits; dielectric strength; insulation resistance. 2 Normative references The following referenced documents

19、are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2282, Aerospace series Characteristics of aircraft electrical supplies EN 61557-2

20、, Electrical safety in low voltage distribution systems up to 1000 V a.c. and 1500 V d.c. Equipment for testing, measuring or monitoring of protective measures Part 2: Insulation resistance (IEC 61557-2:2007) EN 61557-4, Electrical safety in low voltage distribution systems up to 1000 V a.c. and 150

21、0 V d.c. Equipment for testing, measuring or monitoring of protective measures Part 4: Resistance of earth connection and equipotential bonding (IEC 61557-4:2007) ISO 2678, Environmental tests for aircraft equipment Insulation resistance and high voltage tests for electrical equipment BS EN 2283:201

22、0EN 2283:2010 (E) 5 IEC 50 (461), International Electrotechnical Vocabulary Chapter 461: Electric cables1)IEC 50 (581), International Electrotechnicla Vocabulary Chapter 581: Electromechanical components for electronic equipment1)3 Terms and definitions For the purposes of this document, the terms a

23、nd definitions given in IEC 50 (461) and IEC 50 (581) apply. 4 Tests 4.1 General For all the tests, the national safety regulations shall be observed. These tests may be carried out manually or on automatic equipment. In this case, the equipment operates with programmable sequences and trip threshol

24、ds. The test shall be stopped as soon as a fault is detected, or the fault shall be memorized. The voltage shall increase or decrease in a regular manner to each of the scheduled values and the measurements shall be made after stabilization. Test equipment is capable of performing the dielectric str

25、ength and the insulation resistance tests in a single operation, according to the requirements laid down in Table 2. 4.2 Continuity The test enables to verify the conformity of cables, bundles and their connections with the design documents. The direct current or alternating current voltage shall no

26、t exceed 28 V. The Test shall be carried out with equipment according to EN 61557-4. The value of the current passed shall not cause damage to any part of the circuits. 4.3 Dielectric strength The test enables to verify the insulation has the operating efficiency to withstand the voltage (limits) gi

27、ven in EN 2282. The maximum voltage rise or drop during test shall not exceed 500 V per second; this will avoid unintended insulation damage. When the permitted leakage current is exceeded, the warning or protection system shall operate to avoid damage to the components being tested. It should be no

28、ted that in alternating current tests, the capacitive leakage currents add (vectorially) to the fault currents detected. After each dielectric strength test, the measurement point shall be grounded in order to discharge the circuit (except when this circuit remains connected to the reference point).

29、 1) Published by: International Electrotechnical Commission (IEC), 3 rue de Varemb, 1211 Geneva 20, Switzerland. BS EN 2283:2010EN 2283:2010 (E) 6 4.4 Insulation resistance The test enables to verify the insulation resistance of the wiring is in a proper state to meet the operating efficiency. The v

30、oltages used for these measurements are between 50 V and 500 V direct current. The Test shall be carried out with equipment according to EN 61557-2. The fault current shall not exceed 5 mA (for a short-circuit). The reading shall not be made until voltage and current stabilization is achieved. 4.5 T

31、est preparation The conductors and screens of screened or coaxial cables shall be tested in the same way as single core cables, provided they are accessible at both ends. The screened cable test, with respect to the ground, shall be carried out before the screens are grounded. The connector shells c

32、overed with conducting protection or other conductive supports shall be grounded. Electronic components housed in junction boxes shall be short-circuited or disconnected. Connectors, switches, circuit breakers, etc. can be left in circuit provided that they can withstand the test. Otherwise the test

33、 voltage shall be decreased. No equipment shall be connected. The parts of circuits having already been brought into contact with flammable liquids or hydraulic fluids shall only be tested when the national safety regulations are observed, so as to avoid any risk of explosion or fire. 5 Procedures 5

34、.1 General The types of wiring, the systems to which they belong and their functions require several categories (see Table 1). Table 1 Categories Description A All wiring apart from specific cases dealt with under B or C B Specific circuits for each type of aircraft to be defined by mutual agreement

35、 between manufacturers and authorities C Screened wiring, in principle isolated from the ground for tests, before being connected to the ground Aircraft wiring presenting installation difficulties and wiring that are not complete and require to be finished in the aircraft shall be subject to test an

36、d inspection after installation (Table 2, Part II). BS EN 2283:2010EN 2283:2010 (E) 7 Table 2 Tests Characteristics Categories (see Table 1) A B C Part I : Tests after manufacture (prior to installation in aircraft) Voltage strength 1 000 V a.c.aor 1 300 V d.c. 380 V a.c. aor 500 V d.c. 40 V a.c. ao

37、r 50 Vd.c. Minimum application time 1 s 0,1 s 0,1 s Minimum insulation resistance Measuring voltage ( 10 %) 500 V d.c. 500 V d.c. 50 V d.c. RH b = 70 % 20 M 50 M 10 M Part II : Tests of assembled bundles (after installation in aircraft) Voltage strength 1 000 V a.c. aor 1 300 V d.c. 380 V a.c. aor 5

38、00 V d.c 40 V a.c aor 50 V d.c. Application time 0,1 s to 1 min 0,1 s to 1 min 0,1 s to 1 min Minimum insulation resistance Measuring voltage ( 10 %) 500 V d.c. 500 V d.c. 50 V d.c. RH b= 70 % 10 M 20 M 2 M RH b 70 % to 80 % 5 M 10 M 1 M aRoot mean square, frequency 50 Hz to 60 Hz. bRelative humidit

39、y. All the tests for wiring shall take place before the connection of equipment. Electrical and electronic components connected within the wiring shall not be exposed to voltages and currents, which could damage them (see 4.5). Dielectric strength and insulation resistance tests shall be carried out

40、 between each conductor and any other conductor, and between each conductor and earth (structure). See Table 2 for conditions and requirements. Tests on pre-assembled wiring shall comply with the requirements in 5.2 and the requirements of Table 2, Part I. Tests on finished wiring (assembled and ins

41、talled) shall comply with the requirements of 5.3 and the requirements of Table 2, Part II. BS EN 2283:2010EN 2283:2010 (E) 8 5.2 Testing of wiring in production 5.2.1 Continuity The test shall be carried out successively on each section of the circuit, suitably established by the control units (swi

42、tches, isolators, etc.). The purpose of the test is not to measure possible voltage drop on line, since this is covered by the functional tests (see EN 2282). 5.2.2 Dielectric strength See Table 2, Part I. The aircraft test specification shall state the value to be applied or the specific circuits t

43、o be subjected to the relevant requirements. The choice of direct current or alternating current can depend on the test devices or national requirements. The use of direct current is recommended and is necessary where the circuit capacity causes leakage currents affecting measurements. 5.3 Testing o

44、f assembled and installed bundles Perform the tests of 5.2. The applicability of these tests, either on the complete aircraft or sub-assemblies, and the specific circuits is defined in the aircraft test specification. The tests are usually carried out by automatic test equipment which, combines the

45、dielectric strength test and insulation resistance measurements. For tests, which are to be repeated, in-service inspection, repair, etc., the voltage values in Part II of Table 2 shall apply with a possible coefficient of reduction (for example 0,8). All the conductors affected by modifications or

46、repairs on a wiring shall be tested. When screens and certain return conductors are finally connected to the aircraft structure, they shall be considered as earth and shall no longer be disconnected. Then they will only be subject to continuity tests. 6 Requirements No deterioration due to breakdown

47、 caused by the insulation material damage or by ionisation shall appear or be detected. If, because of too high wiring capacity the alternating current dielectric strength test results are not satisfactory, the direct current test is valid. The insulation resistance values shall be complied with. 7

48、Test report It shall include the following data: Degree of relative humidity of the environment; The values obtained; BS EN 2283:2010EN 2283:2010 (E) 9 The procedure; The test means; Defects; Possible deviations. This page deliberately left blankThis page deliberately left blankBSI is the independen

49、t national body responsible for preparing British Standardsand other standards-related publications, information and services. It presents the UK view on standards in Europe and at the international level. It is incorporated by Royal Charter.British Standards Institution (BSI)raising standards worldwideBSI Group Headquarters389 Chiswick High Road London W4 4AL UKTel +44 (0)20 8996 9001Fax +44 (0)20 8996 Standards are updated by

copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
备案/许可证编号:苏ICP备17064731号-1