1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 28 February 2003 prEN 41 65-01 O 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 Connecto
2、rs, electrical, rectangular, modular Operating temperature 175 OC continuous Part 010: Rack and panel rear mounted plug for 2 and 4 modules, series 2 Product standard Srie arospatiale Luft- und Raumfahrt modulaires in modularer Bauweise Connecteurs lectriques rectangulaires Elektrischer Rechteckstec
3、kverbinder Temprature dutilisation 175 OC continu Betriebstemperatur 175 OC konstant Partie O10 : Fiches de rack fixations inverses Teil 010: Freier rckseitiger Einschub- und 2 et 4 modules, srie 2 Gehusesteckverbinder mit 2 und 4 Modulen, Serie 2 Norme de produit Produktnorm This “Aerospace Series“
4、 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 technically approved by the experts of the concerned Domain followi
5、ng 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 and review by users and formal agreement of AEC
6、MA-STAN it will be submitted as a draft European Standard to CEN (European Committee for 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 l
7、icense from IHS-,-,-Page 2 prEN 4165-010: 2003 Foreword This standard was reviewed by the 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
8、received approval for Publication. Contents Page 1 Scope 2 Normative references . 3 Terminology 4 Required characteristics 5 Rack and panel rear plug . 6 Designation . 7 Marking . 8 Technical specification Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS unde
9、r license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 41 65-01 O: 2003 1 Scope This standard defines the rack and panel rear mounted plug 2 and 4 modules, series 2 used in the family of rectangular electrical connectors. The receptacles co
10、rresponding to those plugs are defined in EN 41 65-002. The protective covers corresponding to those plugs are defined in EN 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 a
11、t the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to 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
12、 the publication referred to apply. EN 2424, EN 41 65-001, EN 41 65-002, EN 41 65-01 9, Aerospace series - Marking of aerospace products Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature I75 “C continuous - Part 001: Technical specification - Product standard 1
13、) Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature I75 “C continuous - Part 002: Specification of performance and contact arrangements 1) Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature 175 “C continuous - Part 019: Prote
14、ctive cover for plug, for 2 and 4 modules, series 2 and series 3 - Product standard 2) EN 41 65-021, Aerospace series - Connectors, 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 41
15、65-001. 4 Required characteristics Dimensions are in millimetres. 1) Published as AECMA standard at the date of publication of 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 l
16、icense with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 4165-010: 2003 5 Rack and panel rear plug 5.1 See Figure 1. For 2 modules classes W, F and A Figure 1 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by
17、IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 41 65-01 O: 2003 Class W 5.2 See Figure 2. For 4 modules classes W, F and A Description Rack and panel plug with housing (shell) olive drab cadmium plated, aluminium alloy, cond
18、ucting finish, 500 hours resistance to salt mist, maximum operating temperature 175 “C continuous Figure 2 A Rack and panel plug with housing (shell) black anodised plated, aluminium alloy, no conducting finish, 48 hours resistance to salt mist, maximum operating temperature 175 “C continuous Rack a
19、nd panel plug with housing (shell) black nickel plated, aluminium alloy, 96 hours IFl resistance to salt mist, maximum operating temperature 175 “C continuous Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproducti
20、on or networking permitted without license from IHS-,-,-Page 6 prEN 4165-010: 2003 Type 9: Rack and panel plug (see EN 4165-002) A = series 2 6 Designation EXAMPLE: Shell type 4 = plug 4 modules 2 = plug 2 modules R = rear mounting Position of keying coupling O - Not fitted Fitted in the plug 4 5 6
21、State of delivery plug keying coupling (see EN 4165-021) 7 Marking Unless there are 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-,-,-
