ImageVerifierCode 换一换
格式:PDF , 页数:6 ,大小:230.08KB ,
资源ID:420602      下载积分:5000 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-420602.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(AECMA PREN 3708-004-1996 Aerospace Series Modular Interconnection Systems Terminal Junction Systems Part 004 Removable Feedback Modules Version Unsealed Product Standard Edition P.pdf)为本站会员(progressking105)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!

AECMA PREN 3708-004-1996 Aerospace Series Modular Interconnection Systems Terminal Junction Systems Part 004 Removable Feedback Modules Version Unsealed Product Standard Edition P.pdf

1、STD-AECMA PREN 3708-00LI-ENGL L97b U LO123Ll 0012219 9hb M Edition approved for publication 1996-1 1-29 AECMA STANDARD NORME AECMA AECMA NORM C2 Chairman Mr Pezzetta Comments should be sent within six months after the date of publication to AECMA Gulledelle 94 E-1 200 BRUXELLES prEN 3708-004 Edition

2、 P 2 November 1996 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 6-1200 BRUXELLES - Tel. (32) 2 775 81 10 - Fax. (32) 2 775 81 11 ICs : 49.060 Supersedes edition P 1 September 1995 Descriptors : Aircraft industry, connecting equipment, terminal strips, specifi

3、cations, dimensions, designation, marking, connecting diagrams ENGLISH VERSION Aerospace series Modular interconnection systems Terminal junction systems Part 004 : Removable feedback modules version, unsealed Product standard Srie arospatiale Luft- und Raumfahrt Systmes dinterconnexions modulaires

4、Partie 004 : Version modules amovibles Verteilersystsm in modularer Bauweise Teil 004 : Anreihbare Durchfhrungsmodule, nicht abgedichtet Barrettes de raccordement Verteilermodule retour, non tanches Norme de produit Produktnorm This “Aerospace Series“ Prestandard has been drawn up under the responsi

5、bility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Pre

6、standard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre INPS) and formal agreement of the Official Services of t

7、he Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitt

8、ed without license from IHS-,-,-STD-AECMA PREN 3708-0OLI-ENGL L77b LOL23LL 0032220 hb8 W Page 3 prEN 3708-004 : 1996 1 Scope This standard specifies a removable version of feedback unsealed modules, designed to operate at temperatures between - 55 OC and 775 OC and at a maximum altitude of 13 700 m,

9、 constituting a terminal junction system used in modular interconnection systems. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publicatio

10、ns are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 2591-101 Aeros

11、pace series - Elements of electrical and optical connection - Test methods - Part 101 : Visual examination Aerospace series - Elements of electrical and optical connection - Test methods - Part 317 : Flammability 1) Aerospace series - Modular interconnection systems - Terminal junction systems - Par

12、t O01 : Technical specification 1) EN 2591-317 EN 3708-001 3 Definitions For the purposes of this standard, the following definitions apply : See EN 3708-001. 1) Published as AECMA Prestandard at the date of publication of this standard Previous page is blank Copyright Association Europeene des Cons

13、tructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- - STD*AECMA PREN 3708-004-ENGL L97b 3OL23L3 O032223 5T4 W Code Page 4 prEN 3708-004 : 1996 Contact Mass without contacts max. size 9 4 Require

14、d characteristics A B 4.1 Dimensions and masses See figure 1 and table 1. The modules shall be coded A or B depending on their dimensions and the contacts with which they are used (see table 1). A recess shall be provided for coding labels, thickness : 0,5. Dimensions and tolerances are in millimetr

15、es. 22 6,l 20 8,1 See detail B - O +I 9 Detail B (4:Il Section A-A Contact I I Hard insulator Figure 1 Table 1 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from

16、IHS-,-,- STD-AECMA PREN 3708-004-ENGL 199b m 1012315 0032222 Li30 = Diagram number AO 1 Page 5 prEN 3708-004 : 1996 Feedback module, code A Definition of diagrams 10 groups, 9 of 2 contacts 1 of 3 contacts Number of contacts 4.2 Interconnection diagrams See figures 2 and 3 and tables 2 and 3. The fo

17、llowing shall be visible on the contact access surface : - lines delimiting each group of contacts; - the contact socket code for each group. The colour of these lines and codes shall contrast with that of the contact access surface. 02 03 04 Figure 2 : Interconnection diagrams for modules code A, c

18、ontact size 22 Table 2 I A02 I 1 A03 7 groups of 3 contacts 1 group of 21 contacts 1 of 6 contacts 1 of 3 contacts 1 group of 9 contacts 1 group of 12 contacts I I A06 13 groups of 7 contacts 06 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license w

19、ith AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Diagram Feedbc k module, code B I Page 6 I prEN 3708-004 : 1996 03 04 05 o1 o2 11 07 08 09 10 Figure 3 : Interconnection diagrams for modules code B, contact size 20 Table 3 5 aroum of 2 contacts 1 wouD of 10

20、 contacts 2 groups, 1 of 2 contacts 1 of 8 contacts 2 groups, 1 of 4 contacts 1 of 6 contacts 3 groups, 2 of 2 contacts 1 of 6 contacts 3 groups, 2 of 4 contacts 1 of 2 contacts 10 of size 20 4 groups, 2 groups of 5 contacts 4 groups, 3 of 2 contacts 1 of 4 contacts 2 of 2 contacts 2 of 3 contacts 3

21、 groups, 1 of 5 contacts 1 of 2 contacts 1 of 3 contacts 3 groups, 1 of 4 contacts 2 of 3 contacts Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- STD

22、*AECMA PREN 3708-004-ENGL L77b 101231L 0012224 203 D Page 7 prEN 3708-004 : 1996 4.3 Flammability Test EN 2591-317 - Method A 5 Designation EXAMPLE : Identity block I EN3708-004602 Description block FEEDBACK MODULE Number of this standard Diagram number, see tables 2 and 3 I NOTE : If necessary, the

23、 code 19005 shall be placed between the description block and the identity block. 6 Marking Unless otherwise indicated, the marking shall be shown on the modules. This marking shall include : - the manufacturers reference; - - the date of manufacture (year, week); the name or mark of the manufacture

24、r. 7 Delivery conditions The modules are supplied without contacts. 8 Packaging The modules shall be supplied in a package to protect them from damage. 9 Storage Every five years, an inspection shall be performed to test EN 2591-101. The date of inspection shall be noted and the modules repacked in accordance with 8. 1 O Technical specification See EN 3708-001. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

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