1、STD-AECMA PREN 35LI5-005-ENGL 1775 = 1012311 0032577 290 Edition approved for publication 1995-04-28 AECMA STANDARD NORME AECMA AECMA NORM Comments should be sent within six months after the date of publication to AECMA Technopolis - 175, rue Jean-Jacques Rousseau 921 38 Issy-les-Moulineaux Cedex -
2、FRANCE prEN 3545-005 Edition P 1 April 1995 DIT PAR LASSOCIATION EUROPtENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cedex - Tl. (1 1 47.36.98.76 ICs : Descriptors : ENGLISH VERSION Aerospace series Connectors, electrical, rec
3、tangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 OC to 175 OC Part 005 : Female coding and attachment system for mounting on free housing (plug) Product standard Srie arospatiale Connecteurs lectriques, rectangulaires, tanches et non tanches lar
4、rire, botier en plastique, verrouillage, tempratures dutilisation - 55 OC 175 OC Partie 005 : Systme de fixation et de codage femelle pour montage sur botier mobile (fiche) Norme de produit Luft- und Raumfahrt Elektrische Rechtecksteckverbinder mit und ohne hintere Abdichtung, Plastikgehuse, Verrieg
5、elungssystem, Betriebstemperaturen von - 55 OC bis 175 OC Teil 005 : Buchsenkodierung und Befestigungszubehr fr ein bewegliches Gehuse (Stecker) Produ ktnorm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matriel Ar
6、ospatial). It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to a
7、n extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre INPSI and formal agreement of the Official Services of the Member countries it will be submitted as a draft Europ
8、ean Standard to CEN (European Committee for Standardization) for formal vote. Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 921 38 ISSY-LEC-MOULINEAUX CEDEX - aecma 1995 C 2 Chairman M. Pezzetta Copyright Association Europeene des Constructeurs d
9、e Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN 3545-005-ENGL 1775 1012311 0012578 127 Page 3 prEN 3545-005: 1995 1 Scope This standard specifies the female coding and attachment system f
10、or mounting on a free housing in the family of rectangular electrical connectors with sealed and non-sealed rear, plastic housing, locking device, for operating temperatures from -55 OC to 175 OC. 2 Normative references This European Standard incorporates by dated or undated reference provisions fro
11、m 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 to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendme
12、nt or revision. For undated references the latest edition of the publication referred to applies. EN 3545-002 EN 3545-001 Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 OC to 175 OC - Part O01 : Tec
13、hnical specification 1) Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 OC to 175 OC - Part 002 : Specification of performance and contact arrangements FED-STD-H28/2A: 1978 Screw thread standards for
14、 federal services *) 3 Definitions See EN 3545-001 4 Required characteristics 4.1 Dimensions, mass The dimensions of attachment system are given in figure 1. Dimensions and tolerances are in millimetres. Mass : 3 g max. 1) Published as AECMA Prestandard at the date of publication of this standard 2)
15、 Published by : Department of Defense (DOD), the Pentagon, Washington, D.C. 20301 USA. Previous page is blank Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from I
16、HS-,-,-Page 4 prEN 3545-005: 1995 1 I (#I 0,025 I General concentricity Female body Op tionai -? knurlingl R 2.425 +:Os0 1 View on F 15 I0.2 L screw i O - 0.2 8.2 + t2 2,5* 0.1 Retaining ring Detail X 9 0.1120 inch - 40 UNC-35 ccording to FED-STO-H28 I F O R 0.05 max. 6*34 - 0.10 - - r I _ -1- - - !
17、 I I I I +I O Ln N “ o. 4- I 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 from IHS-,-,-_ STD-AECMA PREN 35Li5-005-ENGL 1775 LOL23LL 0032580 885 Page 5 p
18、rEN 3545-005: 1 995 4.2 Material, surface treatment Body : steel, cadmium-plated, dichromate sealed Retaining ring : beryllium copper, cadmium-plated, dichromate sealed 4.3 Main general characteristics See EN 3545-002 Tightening torque of the locking screw : 0,06 mN.m to 0,lO daN.m 5 Designation EXA
19、MPLE : Description block I Identity block CONNECTOR. CODING SYSTEM EN3545-005A 1-7-T Number of this standard A : female attachment system for mounting on free housing (plug) NOTE : If necessary, the code 19005 shall be placed between the description block and the identity block. 6 Technical specification See EN 3545-001 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-,-,-
