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本文(AECMA PREN 3733-108-2005 Aerospace series Connector optical circular single channel coupled by self-locking ring operating temperature up to 150 continuous Part 108 Cable support.pdf)为本站会员(brainfellow396)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 3733-108-2005 Aerospace series Connector optical circular single channel coupled by self-locking ring operating temperature up to 150 continuous Part 108 Cable support.pdf

1、ASD STANDARD NORME ASD ASD NORM prEN 3733-108 Edition P 1 October 2005 PUBLISHED BY THE AEROSPACE AND DEFENSE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 775 8111 - www.asd-stan.orgICS: 49.060 Descriptors: Aerospace industry

2、, aircraft, aircraft equipment, optical connector, elements of opticalconnection, optical contact, characteristics, test, quality assurance ENGLISH VERSION Aerospace series Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous Part 1

3、08: Cable support boot Product standard Srie arospatiale Connecteur optique circulaire monovoie, accouplement par bague filete, temprature dutilisation 150 C continu Partie 108 : Manchon de protection Norme de produit Luft- und Raumfahrt Optischer Rundsteckverbinder einpolig Schraubkupplung, Betrieb

4、stemperatur 150 C konstant Teil 108: Kabelzugentlastung Produktnorm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The European Association of Aerospace Industries - Standardization). It is published for the needs of the European Aerospace Industry. It ha

5、s been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this pre-standard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the

6、standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implemen

7、t 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 31 October 2005 Comments should be sent within six months after the date of publication to ASD-STAN Electrical Domain Copy

8、right 2005 by ASD-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 3733-108:20052 Foreword This standard was reviewed by the Domain Technical

9、Coordinator of ASD-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. Contents Page 1 Scope . 3 2 Normative references 3 3 Terms and definitions . 3

10、4 Required characteristics 4 4.1 Dimensions and mass 4 4.2 Materials . 4 4.3 Application combinations 4 5 Designation. 5 6 Marking 5 7 Technical specification 5 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduc

11、tion or networking permitted without license from IHS-,-,-prEN 3733-108:20053 1 Scope This standard specifies the characteristics of cable support boots for single channel fibre optic plug and receptacle connectors for aerospace series single core optical cable in accordance with EN 4532, operating

12、temperature up to 150 C. Connector interface dimensions, table of tests and qualification approval requirements, are contained in the Technical Specification EN 3733-001. EN 3733-002, List of product standards, includes the listings of product types, codification and applicable combinations of produ

13、ct types. 2 Normative references The following referenced documents 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 2591-100, Aer

14、ospace series Elements of electrical and optical connection Test methods Part 100: General. EN 3733-001, Aerospace series Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous Part 001: Technical specification.1)EN 3733-002, Aerospac

15、e series Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous Part 002: List of product standards.1)EN 3733-003, Aerospace series Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up t

16、o 150 C continuous Part 003: Plug connector for cable to EN 4532 Product standard.1)EN 3733-004, Aerospace series Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous Part 004: Receptacle, connector, four hole fixing for cable to EN

17、 4532 Product standard.1)EN 3733-005, Aerospace series Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous Part 005: Receptacle, connector, two hole fixing for cable to EN 4532 Product standard.1)EN 3733-006, Aerospace series Conne

18、ctor, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous Part 006: Receptacle, connector, jam nut fixing for cable to EN 4532 Product standard.1)EN 4532, Aerospace series Cables, optical, single core 200 m/280 m, 2,5 mm diameter outer jacket

19、 Technical specification. 1)3 Terms and definitions For the purposes of this document, the terms and definitions given in EN 2591-100 apply. 1) Published as AECMA Prestandard at the date of publication of this standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provid

20、ed by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3733-108:20055 4 Required characteristics 4.1 Dimensions and mass Dimensions (in millimetres) shall be as shown in Figures 1 and 2 as applicable. Either cable support boot may be

21、 utilised. Figure 1 4 x-x 1 1,016Key 1 Typical Figure 2 Mass: 1,2 g max. 4.2 Materials Fluorosilicone. 4.3 Application combinations This component is supplied as an integral part of products conforming to ProduEN 3733-004, EN 3733-005 and EN 3733-006 and is a deliverable spare part. Copyright Associ

22、ation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHSct Standard EN 3733-003, -,-,-prEN 3733-108:20055 Designation EXAMPLE Description block CABLE SUPPORT BOOT Identity block EN

23、3733-108B 5 Number of the basic standard Product standard (see EN 3733-002) Class (see EN 3733-001, test fluids class B) NOTE 1 Part number spacing as shown is for clarity only. NOTE 2 If necessary, the code I9005 may be placed between the description block and the identity block. 6 Marking Not appl

24、icable. 7 Technical specification This component is qualified as part of a complete connector assembly when tested to the qualification requirements of EN 3733-001, EN 3733-003, EN 3733-004, EN 3733-005 and EN 3733-006. 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-,-,-

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