AECMA PREN 3645-001-2002 Aerospace Series Connectors Electrical Circular Scoop-Proof Triple Start Threaded Coupling Operating Temperature 175 Degrees Celcius or 200 Degrees Celsius.pdf

《AECMA PREN 3645-001-2002 Aerospace Series Connectors Electrical Circular Scoop-Proof Triple Start Threaded Coupling Operating Temperature 175 Degrees Celcius or 200 Degrees Celsius.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 3645-001-2002 Aerospace Series Connectors Electrical Circular Scoop-Proof Triple Start Threaded Coupling Operating Temperature 175 Degrees Celcius or 200 Degrees Celsius.pdf（64页珍藏版）》请在麦多课文档分享上搜索。

1、AECMA STANDARD NORME AECMA AECMA NORM This %Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is published on green paper for the needs of the European Aerospace Industry. It has been techni

2、cally approved 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. Afte

3、r examination and review by users and formal agreement of AECMA-STAN it will be submitted as a draf European Standard to CEN (European Committee for Standardization) for formal vote. prEN 3645-001 Edition P 1 January 2002 Edition approved for publication 2002-01-31 PUBLISHED BY THE EUROPEAN ASSOCIAT

4、ION OF AEROSPACE INDUSTRIES - STANDARDIZATION (AECMA-STAN) Gulledelle 94 - 6-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (t32) 2 775 81 11 Comments should be sent within six months after the date of publication to Gulledelle 94 Electrical Domain Mr Peuetta AECMA-STAN 6-1200 BRUXELLES I ICs: 49.0

5、60 Descriptors: Aeronautical industry, aicraft equipment, electrical connection equipment, electrical connector, characteristics, test, quality assurance ENGLISH VERSION Aerospace series Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 “C or 20

6、0 “C continuous Part 001: Technical specification Srie arospatiale Luft- und Raumfahrt Connecteurs lectriques circulaires, Elektrische Rundsteckverbinder, contacts protgs, kontaktgeschtzt, accouplement par filetage, pas rapide trois filets, temprature dutilisation 175 “C ou 200 “C continu Partie O01

7、 : Spcification technique Drei-gangige Gewinde-Schnelkupplung, Betriebstemperatur 175 “C oder 200 “C konstant Teil O01 : Technishe Lieferbedingungen Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or netw

8、orking permitted without license from IHS-,-,-Page 2 prEN 3645-001: 2002 Contents O 1 2 3 4 5 6 7 8 9 10 11 12 . Normative references Terminology Design Definition drawings and masses Quality assurance . Designation and marking Delivery conditions . . . . . Page 3 3 3 4 4 5 6 42 56 63 64 64 64 Copyr

9、ight Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 3645-001: 2002 O Introduction This family of connectors is derived from MIL-DTL-38999 series III

10、, with which it is intermateable and interchangeable. It is particularly suitable for use in zones of severe environmental conditions on board aircraft, applying EN 2282. I Scope This stadard specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, a

11、s well as the test programs and groups for threaded ring coupling circular connectors, fire- resistant, intended for use in a temperature range from - 65 “C to 175 “C continuous or 200 “C continuous according to the classes and models. 2 Normative references This European Standard incorporates by da

12、ted or undated reference, provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated and undated references, subsequent amendments to or revisions of any of these publications apply to this Europ

13、ean Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. IS0 68-1 IS0 261 IS0 262 IS0 965-2 IS0 4524-1 EN 2267-002 EN 2282 EN 2346-002 EN 2424 EN 2591 EN 2591-100 EN 2591-101 EN 2591-213 EN 2591-306 EN 3042

14、EN 3197 EN 3645-002 IS0 general purpose screw threads - Basic profile - Part 1 : Metric screw threads IS0 general purpose metric screw threads - General plan IS0 general purpose metric screw threads - Selected sizes for screws, bolts and nuts IS0 general purpose metric screw threads - Tolerances - P

15、art 2: Limit sizes for general purpose external and internal screw threads - Medium quality Metallic coatings - Test methods for electrodeposited gold and gold alloy coatings - Part 1 : Determination of coating thickness Aerospace series - Cables, electrical, for general purpose - Operating temperat

16、ures between - 55 “C and 260 “C - Part 002: General 1) Aerospace series - Characteristics of aircraft electrical supplies Aerospace series - Cable, electrical, fire resistant - Operating temperatures between - 65 “C and 260 “C - Part 002: General 1) Aerospace series - Marking of aerospace products A

17、erospace series - Elements of electrical and optical connection - Test methods Aerospace series - Elements of electrical and optical connection - Test methods - Part 100: General 1) Aerospace series - Elements of electrical and optical connection - Test methods - Part 1 O1 : Visual examination Aeros

18、pace series - Elements of electrical and optical connection - Test methods - Pari 213: Shielding effectiveness from 100 MHz to 1 GHz Aerospace series - Elements of electrical and optical connection - Test methods - Part 100: Mould growth Aerospace series - Quality assurance - EN aerospace products -

19、 Qualification procedure Aerospace series - Installation of aircraft electrical and optical interconnection systems 1) Aerospace series - Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 “C or 200 “C continuous - Part 002: Specification of perf

20、ormance and contact arrangements 1) - All parts quoted in tables 10 and 17 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 license with AECMANot for ResaleNo reproduction or

21、networking permitted without license from IHS-,-,-Page 4 prEN 3645-001: 2002 AS 1241C MIL-A-8243D MIL-C-25769J MIL-DTL-38999K M IL-H DBK-454A MIL-H-5606G MIL-PRF-7808L MIL-PRF-23699F MIL-PRF-7870C MIL-STD-1373 TR 4257 Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft 2) Anti-icing and Deic

22、ing-Defrosting Fluids 3) Cleaning Compound, Aircraft Surface, alkaline Water Base 3) Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded, and Breech Coupling), Environment Resistant, Removable Crimp and Hermetic Solder Contacts, General Specification for 3)

23、 General Guidelines for Electronic Equipment 3) Hydraulic Fluid, Petroleum Base; Aircraft; Missile and Ordnance 3) Lubricating Oil, Aircraft Turbine Engine, Synthetic Base 3) Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Number 0-156 3) Lubricating Oil: General Purpose, Low Tem

24、perature 3) Screw-Thread, Modified, 60“, Stub, Double 3) Aerospace series - Elements of electrical and optical connection - Relationship between the numbering systems for parts of EN 2591 4) 3 Terminology see Eh! 25S?-?GG. 4 Description 4.1 General Different variants of materials, housings and conta

25、ct arrangements are provided according to the models depending on the service conditions. The pair of connectors is characterized: - by the mechanical stop of the shells on the coupling; - by its triple threaded and self-locking coupling system; - by plugs with shielding ring providing protection ag

26、ainst radioelectrical interference; - by the scoop-proof shells. These connectors use the following contacts: - crimped sizes 22, 20, 16, 12 and 10, - soldered (model Y) sizes 22, 20, 16 and 12, For arrangements comprising the letter GI all contacts are grounded to the receptacle ho us in g - coaxia

27、l crimped or soldered sizes 16, 12 and 8, - triaxial crimped or soldered size 8. The receptacles and plugs contain either male contacts or female contacts. The contacts fitted in the model Y receptacles are exclusively of the male solder type. The connectors are polarized by means of keyways and key

28、s; polarization shall be obtained before the male contacts enter the insert of the female contacts and before the coupling ring is engaged. The position of the keying arrangement is given in table 5. The visual check of coupling is obtained by masking of a red colour band on the receptacle. 2) Publi

29、shed by: Society of Automotive Engineers, Inc. (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001, USA 3) Published by: Department of Defense (DOD), the Pentagon, Washington, DC 20301, USA 4) Published as AECMA Technical Report at the date of publication of this standard Copyright Association

30、Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 3645-001: 2002 4.2 Receptacle The receptacle fixing may be attached: - square flange; - nut, with sealing by O-ri

31、ng at the attachment; - round soldered or brazed flange for model Y connectors. 4.3 Plug The coupling ring is permanently fitted to the plug and allows coupling and uncoupling of the connectors. The lanyard release version may also be uncoupled by pulling on the lanyard. The plug is fitted with a se

32、lf-locking mechanism and a grounding spring device ensuring electrical continuity between the coupled connector housings. 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

33、the cell not to exceed 0,25 V (see EN 3197). 4.4.2 Housings The material of the housings for the connectors and fittings may be either aluminium alloy, passivated stainless steel or composite. Aluminium alloy and composite shall be plated as defined by the model (composite coupling rings may be unpl

34、ated) (see EN 3645-002). 4.4.3 Contacts Unless otherwise specified, the non-removable contacts shall be in ferrous alloy for models Y and in copper alloy for the other models. They shall be gold-plated on an appropriate undercoat. Selective protection is authorized provided that it is sufficient to

35、ensure that the specified performance is achieved. Measurement of the thickness of the protective plating shall be effected in accordance with IS0 4524-1, For removable contacts see EN 3645-002. 4.4.4 Non-metallic materials The materials used for insert, seals and grommets shall have a hardness and

36、mechanical and electrical characteristics consistent with the required use. 5 Design 5.1 The connector housings shall be one-piece. They shall contain teeth at the rear over their entire periphery and shall accomodate the rear accessories. The receptacle shall be fitted with a seal for sealing the c

37、oupled housings. Jam nut receptacles shall contain an O-ring seal. The nut shall have holes for the passage of locking wire. During coupling the grounding spring shall be engaged a minimum of 1,02 mm in the receptacle before the contacts engage. Except for the triple start threads, which shall confo

38、rm to standard MIL-STD-1373, threads shall conform to standards IS0 68-1, IS0 261, IS0 262 and IS0 965-2. Ho us in g s Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without licen

39、se from IHS-,-,-Page 6 prEN 3645-001: 2002 The coupling ring shall be designed so that the male and female contacts engage when it is turned in a clockwise direction and disengage when turned anticlockwise. The coupling threads may have a lubricant applied during manufacture. Full locking of the con

40、nectors shall occur at about 360“. On completion of tightening of the coupling ring, mechanical contact shall exist between the receptacle and plug housings. Masking of a red colour band on the receptacle by the coupling nut shall show that the connectors are correctly coupled. The receptacle has fi

41、ve keyways which engage with corresponding keys on the plug. The major key is fixed and is wider than the others. Polarization is ensured by the different positions which the minor keys may take. The position of the insert is fixed relative to the major key. A blue-coloured band indicating that the

42、crimped contacts of the connectors are rear-releasable shall be provided: - in front of the flange on square flange receptacles; - on the flange of jam nut receptacles; - on the coupling ring of plugs. This band shall be positioned so that at least one is visible when the connectors are fitted and w

43、hen they are mated or unmated. 5.2 Inserts The insert carrying the male and female 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. provided between the housing and insert. The front face of the insert shall b

44、e such that sealing is ensured when the connectors are coupled. The interfacial seal of the insert of the male contacts shall be bonded on the hard insert. The grommet shall permit sealing for all cable diameters indicated in EN 3645-002 and shall not be removable. The mechanical contacts retention

45、system shall be integrated in the hard insert. The design of non-hermetic connectors shall permit individual installation of the contacts without removal of the insert or grommet. Fitting and removal of the contacts shall be from the rear with the tools specified in the contact product standards. Co

46、ntact position identification shall be permanent and contrasted on the front face of the insert or the interfacial seal and on the rear face of the grommet as indicated in 6.5. The marking shall not be recessed or raised on the surfaces providing a seal. The incer! fer contacts sha! he nO!?-rem.lh!E

47、!; it Sh=i! be mechanica!y he!d in the ho!iing: Sealing shall be 6 Definition drawings and masses The general dimensions and the masses of receptacles, plugs and protective covers are given in the product standards. 6.1 Receptacle mating dimensions The mating dimensions of receptacles are shown in f

48、igure 1 and details V and W as well as in tables 1, 2 and 3. 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-,-,-Page 7 prEN 3645-001: 2002 Dimensions and

49、tolerances are in millimetres. 10.54 V (4:l) I 1 1.32 * 0.13 I a the nominal diameter of a male contact comes into contact with the elastic part of the female contact. The distance between the front face of the shell and the point where the right end of a gauge with a diameter equal to Figure I - Receptacle - Coupling dimensions Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot