AECMA PREN 4640-001-2007 Aerospace series Connectors optical rectangular rack and panel multicontact 1 25 diameter ferrule with removable alignment sleeve holder Part 001 Technical.pdf

1、ASD STANDARD NORME ASD ASD NORM prEN 4640-001 Edition P 1 February 2007 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 A

2、erospace series Connectors, optical, rectangular, rack and panel, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder Part 001: Technical specification Srie arospatiale Connecteurs, optiques, rectangulaires, contacts multiples, rackables, frule diamtre 1,25, quips dun porte s

3、leeve dmontable Partie 001 : Spcification technique Luft- und Raumfahrt Optischer Rechtecksteckverbinder, Gehuse, Einschub, Steckverbinder, Multipin, Ferrulendurchmesser 1,25 mm, demontierbarer Zentrierhlsenhalter Teil 001: Technische Lieferbedingungen This “Aerospace Series“ Prestandard has been dr

4、awn up under the responsibility of ASD-STAN (The 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

5、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 review by users and formal agreement of ASD-STAN, it will be submitted as

6、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 giving the EN the status of a national standard and by withdrawing any natio

7、nal standards conflicting with the EN. Edition approved for publication 28 February 2007 Comments should be sent within six months after the date of publication to ASD-STAN Electrical Domain Copyright 2007 by ASD-STAN Copyright European Association of Aerospace Industries Provided by IHS under licen

8、se with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001:20072 Contents Page Foreword2 Introduction .3 1 Scope 3 2 Normative references 3 3 Terms and definitions .4 4 Description .4 5 Design .5 6 Definition drawings5 7 Tests. 15 8 Quality assuran

9、ce. 18 9 Designation and marking. 22 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-STANs General Process Manual, this standard has received approval

10、 for Publication. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001:20073 Introduction This family of fibre optic connectors is derived from ARINC Specificat

11、ion 600 connectors. 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 outside diameter. 1 Scope This standard specifies the general characte

12、ristics, 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 indispensable for the application of this document. For dated references

13、, 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. EN 3197, Aerospace series Installation of aircraft

14、electrical and optical interconnection systems. 1)EN 3909, Aerospace series Test fluids for electric components and sub-assemblies. 1)EN 4639-101, Aerospace series Connectors, optical, rectangular, modular, multicontact, 1,25 mm diameter ferrule, with removable alignment sleeve holder Part 101: Opti

15、cal contact for cable EN 4641-100 Operating temperature between 65 C and 152 C Product standard. 1)EN 4640-002, Aerospace series Connectors, optical, rectangular, rack and panel, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder Part 002: List of product standards. 1)EN 464

16、0-003, Aerospace series Connectors, optical, rectangular, rack and panel, multicontact, 1,25 diameter ferrule, with removable alignment sleeve holder Part 003: Plug optical connector Product standard. 1)EN 4640-004, Aerospace series Connectors, optical, rectangular, rack and panel, multicontact, 1,2

17、5 diameter ferrule, with removable alignment sleeve holder Part 004: Receptacle optical connector Product standard. 1)EN 9133, Aerospace series Quality management systems Qualification Procedure for aerospace standard parts. ARINC Specification 600, Air Transport Avionics Equipment Interfaces. 2)MIL

18、-I-81969/14, Installing and removal tools, connector electrical contact, type III, class 2, composition B. 3)*And all parts quoted in this standard. 1) Published as ASD Prestandard at the date of publication of this standard. 2) Published by: AERONAUTICAL RADIO, INC. 2551 Riva road, Annapolis, Maryl

19、and 21401-7435 USA. 3) Published by: Department of Defence (DOD), the Pentagon, Washington, D.C. 20301 USA. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001

20、:20074 3 Terms and definitions For the purposes of this document, the terms and definitions given in EN 2591-100 apply. 4 Description 4.1 General This document describes an optical connector insert to be installed in plug and receptacle housings. Plug and receptacle housings conform to ARINC Specifi

21、cation 600. The precise alignment of the optical contacts is accomplished by alignment sleeves held in a removable sleeve holder. The plug connector contain male insert as specified in EN 4640-003. The receptacles connector contain female insert as specified in EN 4640-004. The female insert is comp

22、osed of an insert and a removable sleeve holder as specified in EN 4640-004. The sleeve holder is delivered with the female insert. It is considered as a part of the female insert (specific design per manufacturer). The sleeve holder can be supplied separately only for repair purpose. The optical co

23、ntact is in accordance with EN 4639-101. The connectors are keyed as specified in ARINC Specification 600. Connector type designation as specified in ARINC Specification 600. 4.2 Receptacle Receptacle description as specified in ARINC Specification 600. 4.3 Plug Plug description as specified in ARIN

24、C Specification 600. 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 the electromotive force of the cell not to exceed 0,25 V (see EN 3197). 4.4.2 Housings The connector housing description as spec

25、ified in ARINC Specification 600. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001:20075 4.4.3 Optical contacts and alignment sleeves The contacts shall be

26、of suitable materials as specified in EN 4639-101. The optical alignment sleeves shall be of suitable materials as specified in EN 4640-002. The optical contacts are sprung-loaded. The spring force is defined in the product standard (EN 4639-101). 4.4.4 Metallic or non-metallic materials The materia

27、ls used for inserts, seals and grommets shall have a hardness and mechanical characteristics consistent with the required use. 5 Design 5.1 Housing The connector housing design as specified in ARINC Specification 600. 5.2 Connector inserts The connector insert carrying the optical contacts shall be

28、in hard material and have a cross section and radii such that no cracks, flaking or breaks can occur in normal operation. The mechanical contacts retention system shall be integrated in the connector insert. Sealing of the rear face of the connector insert can be provided by a grommet adapted to the

29、 external diameter of the cable The design shall permit individual installation of the contacts without removal of the connector insert. Fitting and removal of the contacts shall be from the rear. For ease of operation, tools as per MIL-I-81969/14-03 (P/N for size 16) may be used. Contact position i

30、dentification 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 of receptacles, plugs and protective covers are given in the product standards. 6.2 Receptacle All housing dimensions are defined in ARIN

31、C Specification 600. 6.3 Plug All housing dimensions are defined in ARINC Specification 600. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001:20076 6.4 Conn

32、ector inserts 6.4.1 Connector interface insert See Figure 1. Key 1 Receptacle connector 5 Mechanical bottom of receptacle 2 Mechanical bottom of plug 6 Plug connector 3 Front face of the insert 7 Pin cavity position A 4 Sleeve holder Figure 1 Copyright European Association of Aerospace Industries Pr

33、ovided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001:20077 6.5 Mating dimensions The mating dimensions receptacle (free position) are shown in Figure 2. Sleeve-holder screw cavity (Sleeve-holder not show) Optical cont

34、act position Key 1 Limit stop of the alignment sleeve holder screw 2 (unmated position) 3 Mechanical bottom of the receptacle NOTE Other dimensions in accordance with ARINC Specification 600. Figure 2 max.Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA

35、 Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001:20078 The mating dimensions of plug (free position) are shown in Figure 3. Key 1 (unmated position) 2 Mechanical bottom of the plug NOTE Other dimensions in accordance with ARINC Specification 600. Figu

36、re 3 6.5.1 Receptacle with female insert and plug with male insert The displacement of the optical contact in the connector is shown in Figure 4. Dimensions and tolerances are in millimetres. Mating position Key 1 Mechanical bottom 2 Receptacle connector 3 Plug connector Figure 4 1 2 min.7,01 5,92 1

37、 2 3 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001:20079 6.5.2 Receptacle connector Contact entering mating sleeve holder Contact optically mated Key 1 #

38、22 Electrical contact 6 Bloc side 2 Sleeve holder 7 Rack side 3 #12 Electrical contact 8 Plug 4 #16 Electrical contact 9 Optical contact 5 Receptacle X1 contact entering mating sleeve holder X2 contact optically mated Optical contact 18,68 mm .735 16,53 mm .650 #22 16,30 mm .642 b13,89 mm .547 #22 2

39、0,32 mm .800 a18,99 mm .748 Optical contact 16,25 mm .634 13,28 mm .523 #20 20,54 mm .809 a18,82 mm .741 #20 16,48 mm .649 b14,04 mm .553 #16 25,70 mm 1.012 a24,10 mm .949 #16 18,42 mm .725 b20,77 mm .818 #12 25,60 mm 1.008 a24,20 mm .953 #12 19,60 mm .772 b17,57 mm .692 aValues for #22,#20,#16,#12

40、electrical contacts are for contact entering mating insulator extracted from ARINC Specification 600. These values are given for information only. Refer to ARINC Specification 600 for more information. bValues for #22,#20,#16,#12 electrical contacts are for contact electrically engaged extracted fro

41、m ARINC Specification 600. These values are given for information only. Refer to ARINC Specification 600 for more information. Figure 5 11223344556 7 76 8 9 89Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking p

42、ermitted without license from IHS-,-,-prEN 4640-001:200710 6.5.3 Coupling contact condition Key 1 D2 - Sleeve cavity inner diameter 2 Sleeve to sleeve-holder cavity stop 3 Optical contact to sleeve-holder stop Condition: in every case, J 0 The different shapes and dimensions of the sleeve cavity mus

43、t be defined to warranty this condition. Figure 6 6.5.4 Contact arrangements Identification of the contact position shall be permanently marked in contrasting colour on the rear face of the module. Contact arrangements 20F12Q8 for shell size 2 or 3: see Figure 7. D1 J Copyright European Association

44、of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001:200711 Receptacle rear face Plug rear face Plug front face Key 1 Ref on ribs 2 Sleeve-holder screw hole (on receptacle side) 3 12 optical

45、cavities 4 End of the optical contacts 5 Keyway 6 8 cavities for #8 quadrax contacts. Contact body is grounded to the connector shell 7 Angular position of the optical contact polarization key 8 Step Number of contacts Contact size Insert cavity location 12 Optical contact RR/RR 1 thru 12 8 8 (Quadr

46、ax) FR/FR (Receptacle side) RR/RR (Plug side) AA thru HH NOTE RR/RR = Contacts are REAR RELEASE / REAR REMOVABLE FR/FR = Contacts are FRONT RELEASE / FRONT REMOVABLE Figure 7 Receptacle front face (without sleeve holder) Copyright European Association of Aerospace Industries Provided by IHS under li

47、cense with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4640-001:200712 Contact arrangements 36F36 for shell size 2 or 3: see Figure 8. Receptacle rear face Plug rear face Plug front face Key 1 Ref on ribs 2 3 cavities for sleeve-holder screw (on rece

48、ptacle side) 3 Keyway 4 36 optical cavities 5 End of the optical contacts 6 Angular position of the optical contact polarization key Number of contacts Contact size Insert cavity location 36 Optical contact RR/RR 1 thru 36 NOTE RR/RR = Contacts are REAR RELEASE / REAR REMOVABLE FR/FR = Contacts are FRONT RELEASE / FRONT REMOVABLE Figure 8 Receptacle front face (without sleeve holder) Copyright European Association of Aerospace Industries Provided by IHS un