1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 28 February 2003 prEN 41 65-009 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 009: Rack and panel plug for 2 and 4 modules, series 3 Product standard Srie arospatiale Luft- und Raumfahrt Connecteurs lectriques rectangulaires Elektrischer Rechtecksteckverbinder Temprature dutilisation 175 OC conti
3、nu Partie O09 : Fiches de rack 2 et 4 modules, srie 3 modulaires in modularer Bauweise Betriebstemperatur 175 OC konstant Teil 009: Freier Einschub- und Gehusesteckverbinder mit 2 und 4 Modulen, Serie 3 Norme de produit Produktnorm This “Aerospace Series“ Prestandard has been drawn up under the resp
4、onsibility 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 following member comments. Subsequent to the publica
5、tion 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 AECMA-STAN it will be submitted as a draft Europ
6、ean 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 license from IHS-,-,-Page 2 prEN 4165-009: 200
7、3 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 received approval for Publication. Contents P
8、age 1 Scope 3 2 Normative references . 3 3 Terminology 3 4 Required characteristics 3 5 Rack plug . 4 6 Designation . 6 7 Marking . 6 8 Technical specification 6 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reprodu
9、ction or networking permitted without license from IHS-,-,-Page 3 prEN 4165-009: 2003 1 Scope This standard defines the rack and panel plug for 2 and 4 modules, series 3 used in the family of rectangular electrical connectors. The receptacles corresponding to those plugs are defined in EN 41 65-002.
10、 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 at the appropriate places in the text and the publicatio
11、ns 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 the publication referred to apply. EN 2424, EN 41 65-0
12、01, 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 ) Aerospace series - Connectors, electrical, rectangula
13、r, 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: Protective cover for plug, for 2 or 4 modules, series 2 and
14、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 4165-001. 4 Required characteristics Dimensions are in mil
15、limetres. 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 license with AECMANot for ResaleNo reproduction or networ
16、king permitted without license from IHS-,-,-Page 4 prEN 4165-009: 2003 5 Rack 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 IHS under license with AECMANot for ResaleNo reproduction or networking
17、 permitted without license from IHS-,-,-Page 5 prEN 4165-009: 2003 W 5.2 See Figure 2. For 4 modules classes W, F and A Rack and panel plug with housing (shell) olive drab cadmium plated, aluminium alloy, conducting finish, 500 hours resistance to salt mist, maximum operating temperature 175 “C cont
18、inuous. Figure 2 Table 1 - Rack and panel plug class A I Class I Description 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 and panel plug with housing (she
19、ll) black nickel plated, aluminium alloy, 96 hours IFI 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 reproduction or networking permitted wit
20、hout license from IHS-,-,-Page 6 prEN 4165-009: 2003 Type 9: Rack and panel plug (see EN 4165-002) B = series 3 6 Designation EXAMPLE: Shell type 4 = plug 4 modules 2 = plug 2 modules State of delivery plug keying coupling (see EN 4165-021) Position of keying coupling O - Not fitted Fitted in the pl
21、ug 4 5 6 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-,-,-
