AECMA PREN 3660-022-2007 Aerospace series Cable outlet accessories for circular and rectangular electrical and optical connectors Part 022 Cable outlet style A straight composite u.pdf

1、ASD STANDARD NORME ASD ASD NORM prEN 3660-022 Edition P 1 May 2007 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Avenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: 49.060 Descriptors: ENGLISH VERS

2、ION Aerospace series Cable outlet accessories for circular and rectangular electrical and optical connectors Part 022: Cable outlet, style A, straight, composite, unsealed, with cable tie strain relief Product standard Srie arospatiale Accessoires arrires pour connecteurs circulaires et rectangulair

3、es lectriques et optiques Partie 022 : Raccord, type A, droit, composite, non tanche, avec tenue du cble par frettage Norme de produit Luft- und Raumfahrt Endgehuse fr elektrische und optische Rund- und Rechtecksteckverbinder Teil 022: Endgehuse, Bauform A, gerade, Composite, nicht abgedichtet, mit

4、Arm fr Kabelbinder Produktnorm This “Aerospace Series“ Prestandard has been drawn 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

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

6、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 implement the EN at national level b

7、y giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 31 May 2007 Comments should be sent within six months after the date of publication to ASD-STAN Electrical Domain Copyright 2007 by ASD-STAN Copyright

8、 European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3660-022:20072 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Terms and definitions .3 4 Characteristics.3 5 De

9、signation 8 6 Marking .9 7 Technical specification .9 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

10、received approval 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 3660-022:20073 1 Scope This product standard defines a range of cable outlets, st

11、raight, composite, style A, for use under the following conditions: Associated electrical connector(s) : EN 3660-002 Temperature range, Class P : 55 C to 200 C 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only

12、 the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2591-*, Aerospace series Elements of electrical and optical connection Test methods. EN 3660-001, Aerospace series Cable outlet accessories for circular and rectan

13、gular electrical and optical connectors Part 001: Technical specification. 1)EN 3660-002, Aerospace series Cable outlet accessories for circular and rectangular electrical and optical connectors Part 002: Index of product standards. 1)AS85049, Connector accessories, electrical General specification.

14、2)3 Terms and definitions For the purposes of this document, the terms and definitions given in EN 3660-001 apply. 4 Characteristics 4.1 Dimensions and mass For dimensions and mass, see Figure 1, Figure 2 and Table 1. For interface dimensions, see 4.2. All its parts quoted. 1) Published as ASD Prest

15、andard at the date of publication of this standard. 2) Published by: Society of Automotive Engineers, Inc. (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001, USA. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or n

16、etworking permitted without license from IHS-,-,-prEN 3660-022:20074 All dimensions in millimetres Key Key 1 Thread A 2 Shell size relief marked this area 3 Cable tie or lacing cord 4 Teeth N (see Table 2) 5 Straight knurl 6 Marking (see Clause 6) 1 F Radius Figure 1 Figure 2 Table 1 B C D E aF Radi

17、us Mass Shell size A Thread Class 2B max. max. max. 0 0,56 max. max. inches mm mm mm mm mm g 08 0.500-20UNEF 15,55 6,80 2,23 3,1 10 0.625-24UNEF 18,52 9,49 28,20 3,03 3,7 12 0.750-20UNEF 21,67 12,87 29,65 3,93 4,4 14 0.875-20UNEF 24,87 14,72 4,93 5,3 16 1.000-20UNEF 28,13 18,03 32,25 5,83 6,2 18 1.0

18、625-18UNEF 30,30 19,90 36,05 7,26 6,9 20 1.1875-18UNEF 33,48 23,08 39,35 7,23 8,0 22 1.3125-18UNEF 36,65 26,31 42,35 8,07 9,0 24 1.4375-18UNEF 39,83 29,22 45,65 7,75 9,03 9,8 a“E” dimension is taken when the coupling nut is pulled in forward position. Copyright European Association of Aerospace Indu

19、stries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3660-022:20075 4.2 Interface dimensions 4.2.1 Associated connectors See EN 3660-002. 4.2.2 Standard AS85049 interface See Figure 3, Figure 4 and Table 2. All dimens

20、ions in millimetres Figure 3 Figure 4 Table 2 G H I 0 0,38 0 0,38 0 0,25 Shell size mm mm mm N Number of teeth 08 11,02 9,10 6,86 12 10 14,35 12,50 9,53 15 12 17,19 15,50 12,98 21 14 20,45 18,70 14,86 24 16 23,67 21,80 18,03 30 18 25,37 23,30 20,04 33 20 28,37 26,40 23,22 36 22 31,75 29,60 26,39 39

21、24 34,70 32,80 29,31 42 4.3 Material and finish Material Class P : Composite, natural colour, unplated 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 3660-022:2007

22、6 4.4 Assembly torque These torque values are intended for installation use only, see Table 3. Table 3 Shell size Torque Nm max. 08 2,2 10 2,8 12 14 3,4 16 3,9 18 20 5,0 22 24 9,0 4.5 Coupling thread strength torques These torque values are for test purposes, see EN 2591-420 and Table 4. Table 4 She

23、ll size Torque Nm max. 08 10 3,0 12 14 16 4,0 18 20 5,0 22 24 9,0 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 3660-022:2007 7 4.6 Tests Test details to be in ac

24、cordance with Table 5 and EN 3660-001. Qualification to be in accordance with EN 3660-001. Table 5 EN 2591 Test No. Title Not applicable Applicable see EN 3660-001 Particulars 101 Visual examination X 102 Examination of dimensions and mass X See 4.1. 205 Housing (shell) electrical continuity X 212 S

25、urface transfer impedance (from 100 MHz to 1 GHz) aX 301 Endurance at temperature X Method B. Temperature: 200 C Duration: 1 000 h 305 Rapid change of temperature X 306 Mould growth X See EN 3660-001. 307 Salt mist X 308 Sand and dust X 314 Immersion at low air pressure X 315 Fluid resistance X 316

26、Ozone resistance X 317 Flammability X Method A on standard test specimen not on product 318 Fire-resistance X 402 Shock X Method A. Severity 100 g Number of shocks: 4 One in each direction in 2 perpendicular axes 403 Sinusoidal and random vibration X Method B. Figure 3. Level J Duration: 8 h in each

27、 of two axes. Test performed: On one group 50 % of time at ( 55 2) C 50 % of time at ambient temperature On a 2ndgroup 100 % of time at max. temperature of class under test continued Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo repr

28、oduction or networking permitted without license from IHS-,-,-prEN 3660-022:20078 Table 5 (concluded) EN 2591 Test No. Title Not applicable Applicable see EN 3660-001 Particulars 406 Mechanical endurance X 30 cycles 408 Mating and unmating forces X Phase A Shell size Load N max. 08 21,2 10 31,7 12 3

29、9,1 14 50,0 16 73,5 18 89,0 20 96,6 22 124,4 24 140,4 420 Mechanical strength of rear accessories X Phase D and Table 4 422 Locking wire hole strength X 513 Magnetic permeability X 515 Hydrolytic stability X a1 GHz to 10 GHz under consideration. 5 Designation EXAMPLE EN3660-022P08 Cable outlet, styl

30、e A, composite, variant P, unplated, shell size 08. Description block CABLE OUTLET Identity block EN3660-022P08 Number of this standard Material/Finish class, see 4.3 Shell size NOTE 1 No gaps are required between sections in the part number when printed. NOTE 2 If necessary, the code I9005 shall be

31、 placed between the description block and the identity block. 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 3660-022:20079 6 Marking Refer to EN 3660-001 and Figure 1. 7 Technical specification Refer to EN 3660-001. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-