AECMA PREN 3545-008-2005 Aerospace Series Connectors electrical rectangular with sealed and non-sealed rear plastic housing locking device operating temperatures - 55 degrees C to .pdf

上传人:李朗 文档编号:420457 上传时间:2018-11-06 格式:PDF 页数:6 大小:62.94KB
下载 相关 举报
AECMA PREN 3545-008-2005 Aerospace Series Connectors electrical rectangular with sealed and non-sealed rear plastic housing locking device operating temperatures - 55 degrees C to .pdf_第1页
第1页 / 共6页
AECMA PREN 3545-008-2005 Aerospace Series Connectors electrical rectangular with sealed and non-sealed rear plastic housing locking device operating temperatures - 55 degrees C to .pdf_第2页
第2页 / 共6页
AECMA PREN 3545-008-2005 Aerospace Series Connectors electrical rectangular with sealed and non-sealed rear plastic housing locking device operating temperatures - 55 degrees C to .pdf_第3页
第3页 / 共6页
AECMA PREN 3545-008-2005 Aerospace Series Connectors electrical rectangular with sealed and non-sealed rear plastic housing locking device operating temperatures - 55 degrees C to .pdf_第4页
第4页 / 共6页
AECMA PREN 3545-008-2005 Aerospace Series Connectors electrical rectangular with sealed and non-sealed rear plastic housing locking device operating temperatures - 55 degrees C to .pdf_第5页
第5页 / 共6页
亲,该文档总共6页,到这儿已超出免费预览范围,如果喜欢就下载吧!
资源描述

1、AECMA STANDARD NORME AECMA AECMA NORM prEN 3545-008 Edition P 1 June 2005 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8110 - Fax. + 32 2 775 8111 - www.aecma-stan.orgICS: 49.060 Descriptors: ENGLISH VERSION Aerospa

2、ce series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 008: Tools for assembly/removal of coding and attachment system Product standard Srie arospatiale Connecteurs lectriques, rectangulaires, tanches

3、 et non tanches larrire, botier en plastique, verrouillage, tempratures dutilisation 55 C 175 C Partie 008 : Outils de serrage/dmontage de systme de codage et de fixation Norme de produit Luft- und Raumfahrt Elektrische Rechtecksteckverbinder mit und ohne hintere Abdichtung, Plastikgehuse, Verriegel

4、ungssystem, Betriebstemperaturen von 55 C bis 175 C Teil 008: Ein-und Ausbauwerkzeuge fr Befestigungs- und Kodierungssystem Produktnorm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). I

5、t is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is af

6、fected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of AECMA-STAN, it will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full

7、 European Standard (EN). The CEN national members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 30 June 2005 Comments should be sent within six mon

8、ths after the date of publication to AECMA-STAN Electrical Domain Copyright 2005 by AECMA-STAN 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-,-,-prEN 354

9、5-008:20052 Foreword This standard was reviewed by the Domain Technical Coordinator of AECMA-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of AECMA-STAN defined in AECMA-STANs General Process Manual, this standard has received approval for Publication. C

10、ontents Page 1 Scope . 3 2 Normative references 3 3 Terms and definitions . 3 4 Required characteristics 3 4.1 Description 3 4.2 Materials, treatments 4 4.3 Dimensions . 4 5 Designation. 6 6 Marking 6 7 Technical specification 6 Copyright Association Europeene des Constructeurs de Materiel Aerospati

11、al Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-008:20053 1 Scope This standard specifies the characteristics of tools for assembly/removal of coding and attachment systems in family of rectangular electrical con

12、nector with sealed and non-sealed version rear, plastic housing, locking device, for operating temperature from 55 C to 175 C for aerospace application. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the ed

13、ition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2424, Aerospace series Marking of aerospace products. EN 2591-100, Aerospace series Elements of electrical and optical connection Test methods Part 100: General.1)EN 3545

14、-005, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 005: Female coding and attachment system for mounting on free housing (plug) Product standard. 1)EN 3545-006, Aerospace series Conne

15、ctors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 006: Male coding and attachment system for mounting on free housing (receptacle) Product standard.1)3 Terms and definitions For the purposes of this document, t

16、he terms and definitions given in EN 2591-100 apply. 4 Required characteristics 4.1 Description 4.1.1 Tool allows the removal of coding and attachment system EN 3545-005 and EN 3545-006 (tool type A). 2 models are available: Model 01: Tool fitted with a spring piston system (see Figure 1). The remov

17、al operation is made by depressing the piston after insertion of tool in front face in the attachment and coding system housing of the connector. Model 02: Tool fitted with a spring system (see Figure 2). The removal operation is made by depressing the tool body after insertion of tool in front face

18、 in the attachment and coding system housing of the connector (side marked “M“ for male coding and attachment system EN 3545-006, and side marked “F“ for female coding and attachment system EN 3545-005). 1) Published as AECMA Prestandard at the date of publication of this standard. Copyright Associa

19、tion Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-008:20054 4.1.2 Tool for torquing male coding and attachment system EN 3545-006 for mounting on fixed housing

20、(receptacle). Tool serves to fit, to remove and to torque tighten the male coding and attachment system EN 3545-006 and to ensure the attachment of connector housing on panel (tool type B). 2 models are available: Model 01: Manual tool (see Figure 3). Model 02: Attachment for power or torquing tool

21、(see Figure 4). 4.2 Materials, treatments Not specified but shall be compatible with the required use. 4.3 Dimensions Dimensions are given in millimetres. See Figures 1 to 4. Key 1 Dimensions compatible with the required use (see EN 3545-005 and EN 3545-006) 2 Marking see clause 6 3 Optional form Fi

22、gure 1 Typical configuration of type A model 01 90 (Ref.) 2 1 3 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-,-,-prEN 3545-008:20055 Key 1 Dimensions co

23、mpatible with the required use (see EN 3545-005 and EN 3545-006) 2 Knurl 3 Marking see clause 6 Figure 2 Typical configuration of type A model 02 Key 1 Optional form 2 Dimensions compatible with the required use (see EN 3545-006) Figure 3 Typical configuration of type B model 01 Key 1 Hex form (6,35

24、 across flats) 2 Dimensions compatible with the required use (see EN 3545-006) Figure 4 Typical configuration of type B model 02 80 (Ref.) F M1 2 3 1110 (Ref.) 1 40 2 12 6,5 1 7,4 25 75 (Ref.) 21Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license w

25、ith AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-008:20056 5 Designation EXAMPLE Description block TOOL Identity block EN3545-008A01 Number of the standard Type of tool (see 4.1.1 and 4.1.2) Model code (see 4.1.1 and 4.1.2) NOTE If necessary, the

26、code I9005 shall be placed between the description block and the identity block. 6 Marking Marking shall be made as per EN 2424, category P. 7 Technical specification Not specified. 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-,-,-

展开阅读全文
相关资源
猜你喜欢
相关搜索

当前位置:首页 > 标准规范 > 国际标准 > 其他

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