AECMA PREN 4639-001-2006 Aerospace series Connectors optical rectangular modular multicontact 1 25 diameter ferrule with removable alignment sleeve holder Part 001 Technical specif.pdf

1、ASD STANDARD NORME ASD ASD NORM prEN 4639-001 Edition P 1 September 2006 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: 49.060 Descriptors: ENGLISH VERSION

2、Aerospace series Connectors, optical, rectangular, modular, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder Part 001: Technical specification Srie arospatiale Connecteurs optiques rectangulaires, modulaires multivoies, frule 1,25, quips dun porte sleeve dmontable Partie 0

3、01 : Spcification technique Luft- und Raumfahrt Optischer Rechtecksteckverbinder, modular, multipin, Ferrulendurchmesser 1,25 mm, demontierbarer Zentrierhlsenhalter Teil 001: Technische Lieferbedingungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The

4、AeroSpace and Defence Industries Association of Europe - Standardization). It 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 techn

5、ical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the 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

6、 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 giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition ap

7、proved for publication 30 September 2006 Comments should be sent within six months after the date of publication to ASD-STAN Electrical Domain Copyright 2006 by ASD-STAN Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleN

8、o reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:20062 Contents Page Foreword . 2 Introduction. 3 1 Scope 3 2 Normative references 3 3 Terms and definitions. 3 4 Description. 4 4.1 General . 4 4.2 Receptacle . 4 4.3 Plug. 4 4.4 Materials and surface treatment 4 5 Des

9、ign. 5 5.1 Housing 5 5.2 Modules 5 6 Definition drawings. 5 6.1 General . 5 6.2 Receptacle . 5 6.3 Plug. 5 6.4 Modules 5 6.5 Mating dimensions 8 7 Tests . 13 7.1 Tests according to EN 2591 series 13 7.2 Special tests 16 8 Quality assurance . 17 8.1 General . 17 8.2 Qualification. 17 8.3 Maintenance

10、of qualification 20 9 Designation and Marking 21 9.1 Fibre optic module 21 9.2 Fibre optic contact 21 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-

11、STANs General Process Manual, this standard has received approval for Publication. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:20063

12、 Introduction This family of fibre optic connectors is derived from EN EPX-xxx (GT3). It is suitable for use on aerospace onboard applications. It provides easy access for optical contact end face cleaning. The optical contacts are capable of accepting single cable sizes up to a maximum of 2 mm outs

13、ide diameter. 1 Scope This standard specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, as well as the test programs and groups for rectangular multipin fibre optic connectors. 2 Normative references The following referenced documents are indisp

14、ensable 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*, Aerospace series Elements of electrical and optical connection Test methods Part

15、 100: General. EN 3197, Aerospace series Installation of aircraft electrical and optical interconnection systems. 1) EN 3909, Aerospace series Test fluids for electric components and sub-assemblies. 1) EN 9133, Aerospace series Quality management systems Qualification Procedure for aerospace standar

16、d parts. EN EPX-xxx (GT3), Aerospace series (EPX standard). 2) MIL-I-81969/14, Installing and removal tools, connector electrical contact, type III, class 2, composition B. 3) 3 Terms and definitions For the purposes of this document, the terms and definitions given in EN 2591-100 apply. * And all p

17、arts quoted in this document. 1) Published as ASD Prestandard at the date of publication of this standard 2) In preparation at the date of publication of this standard 3) Published by : Department of Defence (DOD), the Pentagon, Washington, D.C. 20301 USA Copyright Association Europeene des Construc

18、teurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:20064 4 Description 4.1 General This document describes an optical connector module to be installed in plug and receptacle housings.

19、 Plug and receptacle housings conform to EN EPX-xxx (GT3). There are two sizes of connector housings Housing size 1 with 1 module cavity Housing size 2 with 2 module cavities The connectors use rear removable optical contacts with a ferrule diameter of 1,25 mm. The precise alignment of the optical c

20、ontacts is accomplished by alignment sleeves held in a removable sleeve holder. The receptacles and plugs contain either male or female module. The female module is characterised by its ability to receive the removable sleeve holder. The inserts can be installed and removed from the shell by mean of

21、 a tool as specified EN EPX-xxx (GT3). The modules are keyed to prevent mismating (“A” module for connector housing cavity “A” and “B” module for connector housing cavity “B.”) as specified EN EPX-xxx (GT3). The connectors are keyed as specified EN EPX-xxx (GT3). Connector type designation as specif

22、ied EN EPX-xxx (GT3). 4.2 Receptacle Receptacle description as specified EN EPX-xxx (GT3). 4.3 Plug Plug description as specified EN EPX-xxx (GT3). 4.4 Materials and surface treatment 4.4.1 General When dissimilar metals are in close contact, adequate protection against corrosion shall be used for t

23、he electromotive force of the cell not to exceed 0,25 V (see EN 3197). 4.4.2 Housings The connector housing description as specified in EN EPX-xxx (GT3). 4.4.3 Optical contacts and alignment sleeves The contacts shall be of suitable materials as specified in the product standard. The optical alignme

24、nt sleeves shall be of suitable materials as specified in the product standard. The optical contacts are sprung-loaded. The spring force is defined in the product standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for Resa

25、leNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:20065 4.4.4 Metallic or non-metallic materials The materials used for modules, seals and grommets shall have a hardness and mechanical characteristics consistent with the required use. 5 Design 5.1 Housing The conne

26、ctor housing design as specified in EN EPX-xxx (GT3). 5.2 Modules The modules carrying the optical contacts shall be in hard material and have a cross section and radii such that no cracks, flaking or breaks can occur in normal operation. The contact module is mechanically held in the connector hous

27、ing by retention clips, and removable with the use of an extraction tool. The mechanical contacts retention system shall be integrated in the hard module. The front face of the module shall be such that sealing is ensured when the connectors are coupled. The interfacial seal of the module of the mal

28、e contacts shall be permanently fastened on the hard module. Sealing of the rear face of the module is provided by a grommet adapted to the external diameter of the cable The design shall permit individual installation of the contacts without removal of the module. Fitting and removal of the contact

29、s shall be from the rear. For ease of operation, tools as per MIL-I-81969/14-03 standard (P/N for size 16) may be used. Contact position identification shall be permanent and contrasted on the rear face of the insert or grommet. 6 Definition drawings 6.1 General The general dimensions and the masses

30、 of receptacles, plugs and protective covers are given in the product standards. 6.2 Receptacle All housing dimensions are defined in EN EPX-xxx (GT3). 6.3 Plug All housing dimensions are defined in EN EPX-xxx (GT3). 6.4 Modules 6.4.1 Single rectangular connector interface insert See Figure 1. Copyr

31、ight Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:20066 Key 1 Receptacle connector 2 Pin cavity position A 3 Pin cavity position A 4 Plug conne

32、ctor 5 Front face of the module 6 Mechanical bottom of receptacle 7 Interfacial seal 8 Sleeve holder 9 Mechanical bottom of plug 10 Interfacial seal Figure 1 6.4.2 Dual rectangular connector interface insert See Figure 2. Receptacle Connector 4 1 2 3 5 10 9 8 7 6 5 0,30 Ar Pr 0,30 Ap Pp Copyright As

33、sociation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:2006 7 Key 1 Receptacle connector 2 Mechanical bottom of plug 3 Front face of the module 4 Interfaci

34、al seal 5 Sleeve holder 6 Pin cavity position A 7 Pin cavity position A 8 Mechanical bottom of the receptacle 9 Plug connector Figure 2 1 9 23 4 5 6 8 7 5 4 3 0,30 Ar Pr 0,30 Ap Pp Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not

35、for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:20068 6.5 Mating dimensions 6.5.1 Mating dimensions for single rectangular connector The mating dimensions of plug and receptacle for single rectangular connector are shown in Figure 3. Key 1 Single rectangu

36、lar receptacle 2 Single rectangular plug Figure 3 1 2 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:20069 6.5.2 Mating dimensions for

37、dual rectangular connector The mating dimensions of plug and receptacle for dual rectangular connector are shown in Figure 4. Key 1 Dual rectangular receptacle 2 Dual rectangular plug Figure 4 1 2 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license

38、 with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:200610 6.5.3 Receptacle with male module and plug with female module The displacement of the optical contact in the size 1 connector is shown on Figure 5. Dimensions and tolerances are in mil

39、limetres. Key 1 Receptacle connector 2 Plug connector Figure 5 6.5.4 Receptacle with female module and plug with male module The displacement of the optical contact in the size 2 is shown on Figure 6. Dimensions and tolerances are in millimetres. Key 1 Receptacle connector 2 Plug connector Figure 6

40、1 2 1 2 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:200611 6.5.5 Coupling contact condition See Figure 7. Key 1 Optical contact to s

41、leeve holder stop 2 D2 - Sleeve cavity inner diameter 3 Sleeve to sleeve holder cavity stop Condition: In every case, J 0 The different shapes and dimensions of the sleeve cavity must be defined to warranty this condition. Figure 7 6.5.6 Contact arrangements Identification of the contact position sh

42、all be permanently marked in contrasting colour on the rear face of the module. Contact arrangements: see Figure 8. 1 2 3 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without l

43、icense from IHS-,-,-prEN 4639-001:200612 Rear grommet face Female module (with sleeve holder) Rear grommet face Male module Key 1 “A“ keying 2 On ribs 3 “B“ keying 4 End of the optical contact 5 Cavity 6 Position of the optical contact polarization key 7 or “B“ marking (according to the connector ho

44、using cavity) Figure 8 1 5 4 2 2 5 3 7 6 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4639-001:200613 7 Tests 7.1 Tests according to EN 2591 s

45、eries The tests of EN 2591, applicable in the context of this standard as well as the details necessary for implementing them and for inspecting connector characteristics, are given in Table 1. Table 1 EN 2591- Test Details 6101 Visual examination No loosening of parts, cracks, excessive wear, or de

46、tached parts. Optical face undamaged and free from contamination when examined at 100 magnification minimum. 101 Visual examination Applicable to protective caps only. 102 Examination of dimensions and mass According optical contact product standard. NOTE In the case of a qualified inspection system

47、 the parts unrelated to a production batch, may be used. 6301 Endurance at temperature For performance and test method requirements refer to the applicable product standard for the component and cable under test. 302 Climatic sequence For performance and test method requirements refer to the applic

48、able product standard for the component and cable under test. 6303 Cold/low pressure and damp heat Not applicable 304 Damp heat steady state For performance and test method requirements refer to the applicable product standard for the component and cable under test. 6305 Rapid change of temperature For performance and test method requirements refer to the applicable product standard for the component and cable under test. 6306 Mould growth Not applicable 6307 Salt mist For performance and test method r