1、STD-AECMA PREN 35q5-00b-ENGL 1775 W 10L23LL 0012b21 128 = 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 C 2 Chairman M. Pezzetta prEN 3545-006 Edition P 1 April 1995 DIT PAR LASSOCIATION EUROPENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cedex - Tl. (1) 47.36.98.76 ICs : Descriptors : ENGLISH VERSION Aerospace series Con
3、nectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 OC to 175 OC Part 006 : Male coding and attachment system for mounting on fixed housing (receptacle) Product standard Srie arospatiale Connecteurs lectriques, rectangulaire
4、s, tanches et non tanches larrire, botier en plastique, verrouillage, tempratures dutilisation - 55 OC 175 OC Partie 006 : Systme de fixation et de codage mle pour montage sur botier fixe (embase) Norme de produit Luft- und Raumfahrt Elektrische Rechtecksteckverbinder mit und ohne hintere Abdichtung
5、, Plastikgehuse, Verriegelungssystem, Betriebstemperaturen von - 55 OC bis 175 OC Teil 006 : Buchsenkodierung und Befestigungszubehr fr ein festes Gehuse (Steckdose) Produ ktnorm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (Association Europenne des Constr
6、ucteurs de Matriel Arospatial). 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 shal
7、l not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submi
8、tted 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 license from IHS-,-,- STD
9、-AECMA PREN 3545-00b-ENGL 1775 1012311 0012b22 Ob4 Page 3 prEN 3545-006: 1995 1 Scope This standard specifies the male coding and attachment system for mounting on a fixed housing in the family of rectangular electrical connectors with sealed and non-sealed rear, plastic housing, locking device, for
10、 operating temperatures from -55 OC to 175 OC. 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
11、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 applies. EN 3545-001 EN 3545-002 FED-STD-H28: 1978 Aerospace
12、series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 OC to 175 OC - Part O01 : Technical specification Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locki
13、ng device, operating temperatures -55 OC to 175 OC - Part 002 : Specification of performance and contact arrangements 1) Screw threads standards for federal services *) 3 Definitions See EN 3545-001 4 Required characteristics 4.1 Dimensions, mass The dimensions of attachment system are given in figu
14、res 1, 2 and 3. Dimensions and tolerances are in millimetres. Mass : 6 g max. 1) Published as AECMA Prestandard at the date of publication of this standard 2) Published by : Department of Defense (DODI, the Pentagon, Washington, D.C. 20301 USA. Previous page is blank Copyright Association Europeene
15、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 3545-006:1995 ml General concentricity Position indicator (recessed circle1 I 0.1120 inch - 40 UNC-36 according to FEO-STO-
16、H28 I 0.2500 inch - 28 UNF-3A occording to FEO-STO-H28 Figure 1 - Male body Washer and nut are fitted on the mole body B-B - “1 - Washer with two corrugations in dichromate-sealed cadmium Dlated steel I 1.7 max. 0.3 at I 0.2500 inch - 28 UNF-3B according to FEO-STO-H28 A-A R 2,250 0,025 T- c-c O 2s
17、- 0.2 Figure 2 - Washer and nut 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 5 prEN 3545-006: 1995 R 0.05 max. I I 0,025 I General concentricit
18、y O 6,34 - 0.10 Retaining ring Detail X I View on F Figure 3 - Retaining ring 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
19、 panel mounting nut : O, 125 daN.m to 0,150 daN.m 5 Designation EXAMPLE : Description block Identity block CONNECTOR, CODING SYSTEM EN3545-0066 B : male attachment system for mounting on fixed housing (receptacle) Number of this standard 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-,-,-
