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本文(AECMA PREN 3733-009-2005 Aerospace Series Connector Optical Circular Single Channel Coupled by Self-Locking Ring Operating Temperature up to 150 Degrees C Continuous Part 009 Recep.pdf)为本站会员(tireattitude366)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 3733-009-2005 Aerospace Series Connector Optical Circular Single Channel Coupled by Self-Locking Ring Operating Temperature up to 150 Degrees C Continuous Part 009 Recep.pdf

1、AECMA STANDARD NORME AECMA AECMA NORM prEN 3733-009 Edition P 1 May 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 Aerospac

2、e series Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous Part 009: Receptacle sub-assembly for cable to EN 4532 (200 m/280 m fibre) Product standard Srie arospatiale Connecteur optique circulaire monovoie, accouplement par bagu

3、e filete, temprature dutilisation 150 C continu Partie 009 : Sous-ensemble embase pour cble EN 4532 (fibre 200 m/280 m) Norme de produit Luft- und Raumfahrt Optischer Rundsteckverbinder einpolig Schraubkupplung, Betriebstemperatur 150 C konstant Teil 009: Steckerunterbaugruppe fr Kabel nach EN 4532

4、(200 m/280 m fiber) Produktnorm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the

5、 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 affected, physically or functionally, without re-identification of the standard. After examination and rev

6、iew 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 European Standard (EN). The CEN national members have then to implement the EN at national level by giv

7、ing the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 31 May 2005 Comments should be sent within six months after the date of publication to AECMA-STAN Electrical Domain Copyright 2005 by AECMA-STAN Copyright

8、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 3733-009:20052 Foreword This standard was reviewed by the Domain Technical Coordinator of AECMA-STANs Electr

9、ical 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. Contents Page 1 Scope . 3 2 Normative references 3 3 Terms and definitions . 3 4 Required characteristics

10、4 5 Designation. 4 6 Marking 5 7 Technical specification 5 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 3733-009:20053 1 Scope This standard sp

11、ecifies the characteristics of receptacle sub-assemblies for single channel fibre optic receptacle connectors for aerospace series single core optical cable in accordance with EN 4532, operating temperature up to 150 C. Connector interface dimensions, table of tests and qualification approval requir

12、ements, 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 product types. 2 Normative references The following referenced documents are indispensable for the application

13、 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, Aerospace series Elements of electrical and optical connection Test methods Part 100: General.1)EN 3733-001,

14、 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, Aerospace series Connector, optical, circular, single channel, coupled by self-locking ring, operating temperat

15、ure up to 150 C continuous Part 002: List of products standards.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 4532 Product stan

16、dard.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: Receptable, connnector, two hole fixing for cable to EN 4532 Product standard.1)EN 3733-006, Aerospace series Connector, optical, ci

17、rcular, single channel, coupled by self-locking ring, operating temperature up to 150 C continuous Part 006: Receptable, connector, jam unt fixing for cable to EN 4532 Product standard.1)EN 4532, Aerospace series Cables, optical, single core 200 m/280 m fibre, 2,5 mm outer jacket Technical specifica

18、tion. 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 Provided by IHS under lice

19、nse with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3733-009:20054 4 Required characteristics 4.1 Dimensions and mass Dimensions (in millimetres) shall be as shown in Figure 1. Figure 1 NOTE Terminated overall length (when assembled within a receptac

20、le connector) assumes a maximum gap of 1 mm between crimp sleeve and rear nut. Mass: 4,0 g max. 4.2 Materials Zirconia ceramic, nickel-copper alloy metallic components. 4.3 Applicable combinations This component is supplied as an integral part of products conforming to Product Standards EN 3733-004

21、to EN 3733-006 and is a deliverable spare part. 5 Designation EXAMPLE Description block SUB-ASSEMBLY, RECEPTACLE Identity block EN3733-009B Number of the basic standard Product standard (see EN 3733-002) Class (see EN 3733-001, Test fluids Class B) NOTE If necessary, the code I9005 may be placed bet

22、ween the description block and the identity block. 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 3733-009:20055 6 Marking Not applicable. 7 Tech

23、nical specification This component is qualified as part of a complete receptacle connector assembly when tested to the qualification requirements of EN 3733-001 and the applicable Product Standards. 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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