1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 28 February 2003 prEN 41 65-007 Edition P 1 February 2003 Comments should be sent within six months after the date of publication to Electrical Domain AECMA-STAN ICs: 49.060 Descriptors: ENGLISH VERSION Aerospace series Connector
2、s, electrical, rectangular, modular Operating temperature 175 OC continuous Part 007: Plug for 2 and 4 modules, series 3 Product standard Srie arospatiale Luft- und Raumfahrt Connecteurs lectriques rectangulaires Elektrischer Rechtecksteckverbinder Temprature dutilisation 175 OC continu Betriebstemp
3、eratur 175 OC konstant Partie 007 : Fiches 2 et 4 modules, Teil 007: Freier Steckverbinder mit 2 und 4 Modulen, modulaires in modularer Bauweise srie 3 Norme de produit Serie 3 Produktnorm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA-STAN (The European Asso
4、ciation of Aerospace Industries - Standardization). It is published on green paper 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 technical con
5、tent 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 AECMA-STAN it will be submitted as a draft European Standard to CEN (European Committee for
6、 Standardization) for formal vote. 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 2 prEN 4165-007: 2003 Foreword This standard was reviewed by th
7、e Domain Technical Coordinator of AECMA-STANS Electrical 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 2 Normative references . 3 Term
8、inology 4 Required characteristics 5 Clicker-nut plug 6 Designation . 7 Marking . 8 Technical specification 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
9、-,-,-Page 3 prEN 4165-007: 2003 1 Scope This standard defines the plug series 3, for 2 and 4 modules used in the family of rectangular electrical connectors. The receptacles corresponding to those plugs are defined in EN 4165-002. The protective covers corresponding to those plugs are defined in EN
10、41 65-01 9. 2 Normative references This European Standard incorporates by dated 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 references, subsequent amendments t
11、o or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to apply. EN 2424, EN 41 65-001, EN 41 65-002, EN 41 65-01 9, Aerospace series - Marking of aerospa
12、ce products Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature I75 “C continuous - Part 001: Technical specification - Product standard 1 ) Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature I75 “C continuous - Part 002: Speci
13、fication of performance and contact arrangements 1) Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature 175 “C continuous - Part 019: Protective cover for plug, for 2 or 4 modules, series 2 and series 3 - Product standard 2) EN 41 65-021, Aerospace series - Connec
14、tors, electrical, rectangular, modular - Operating temperature I75 “C continuous - Part 021: Coupling system keyway for plug - Product standard 1 ) 3 Term in ol ogy See EN 4165-001. 4 Required characteristics Dimensions are in millimetres. 1) Published as AECMA standard at the date of publication of
15、 this standard 2) In preparation 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 networking permitted without license from IHS-,-,-Page 4 prEN 4165-007: 2003
16、 5 Clicker-nut plug 5.1 See Figure 1. For 2 modules classes W, F and A a active thread hexagonal groove Figure 1 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license fro
17、m IHS-,-,-Page 5 prEN 4165-007: 2003 Class 5.2 See Figure 2. For 4 modules classes W, F and A Description Plug with housing (shell) olive drab cadmium plated, aluminium alloy, conducting finish, 500 hours resistance to salt mist, maximum operating temperature 175 “C continuous a active thread hexago
18、nal groove A Figure 2 Plug with housing (shell) black anodised plated, aluminium alloy, no conducting finish, 48 hours resistance to salt mist, maximum operating temperature 175 “C continuous Plug with housing (shell) black nickel plated, aluminium alloy, 96 hours resistance to salt IFI mist, maximu
19、m operating temperature 175 “C continuous 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 6 prEN 4165-007: 2003 Type 6: Plug (see EN 4165-002) B =
20、 series 3 6 Designation EXAMPLE: Shell type 4 = plug 4 modules 2 = plug 2 modules Plug keying coupling (number not marked on the connector) State of delivery plug keying coupling (see EN 4165-021) (Not marked on the connector) O - Not fitted Fitted in the receptacle 4 5 6 7 Marking Unless there are
21、other specific contractual requirements, the marking shall be in accordance with EN 2424, category P. 8 See EN 4165-001. Tech n i cal specification 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-,-,-
