AECMA PREN 2591-420-2005 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part 420 Michanical Strength of Rear Accessories Edition P 1《航空航天系列.光电连接元件　试验方法.pdf

《AECMA PREN 2591-420-2005 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part 420 Michanical Strength of Rear Accessories Edition P 1《航空航天系列.光电连接元件　试验方法.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 2591-420-2005 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part 420 Michanical Strength of Rear Accessories Edition P 1《航空航天系列.光电连接元件　试验方法.pdf（6页珍藏版）》请在麦多课文档分享上搜索。

1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication Comments should be sent within six months prEN 2591 -420 Edition P 1 February 2005 Electrical Domain PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION 4 $fqpb 7 Lg -_ - $fib,* k6-d Gulledelle 94 - 8-

2、1200 Brussels -Tel + 32 2 775 8110 - Fax + 32 2 775 811 1 - www aecma-stan org ICs: 49.060 Will supersede EN 2591-420:2001 Descriptors: ENGLISH VERSION Aerospace series Elements of electrical and optical connection Test methods Part 420: Mechanical strength of rear accessories Organes Srie arospatia

3、le Luft- und Raumfahrt Mthodes dessais Partie 420 : Tenue mcanique des accessoires arrire de connexion lectrique et optique Elektrische und optische Verbindungselemente P rfve rfa h ren Teil 420: Mechanische Festigkeit der rckseitigen Zubehrteile This %Aerospace Series“ Prestandard has been drawn up

4、 under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is published 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 Euro

6、pean Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any national standard

7、s conflicting with the EN. 28 February 2005 after the date of publication to AECMA-STAN I I Copyright 2005 O by AECMA-STA1 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without l

8、icense from IHS-,-,-Page 2 prEN 2591-420:2005 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 re

9、ceived approval for Publication. Contents Page 1 Scope 3 2 Normative referen ces 3 3 Preparation of specimens 3 4 Apparatus 3 5 Method 3 6 Requirements 6 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or

10、 networking permitted without license from IHS-,-,-Page 3 prEN 2591-420:2005 1 Scope This standard specifies a method of determining the mechanical strength of rear accessories used on elements of electrical and optical connection subjected to bending, tensile and torsional forces. It shall be used

11、together with EN 2591-100. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies.

12、 EN 2591-100, Aerospace series - Elements of electrical and optical connection - Test methods - Part 100: General. EN 2591 -1 01, Aerospace series - Elements of electrical and optical connection - Test methods - Part 101: Visual examination. 3 Preparation of specimens Unless specified in the technic

13、al specification, the following details shall be stated: - mounting and locking of specimens; - for phase A, bending moment; - for phase B, tensile force; - for phase C, torsional moment; - for phase D, tightening torque; - requirements. 4 Apparatus - Equipment for applying and measuring the bending

14、, tensile, torsional forces and torques - Fixture simulating the rear part of a connector 5 Method The mounted specimens shall be subjected to the following test sequence unless otherwise stated. Dummy shells may be used. 1) Published as AECMA Prestandard at the date of publication of this standard.

15、 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 2591-420:2005 a) Phase A: bending test With the specimens placed horizontally in the test

16、fixture, bending moments shall be applied successively to the end of the accessory, see Figures 1, 2 and 3. The forces f, and f2 and f3 shall be increased at a rate not exceeding 20 N/s until the specified value is reached and maintained for 1 min. Figure 1 - Bending moment (straight accessory) Figu

17、re 2 - Bending moment (90 accessory) Figure 3 - Bending moment (90 accessory) 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 2591-420:2005

18、 b) Phase B: tensile test With the specimens placed horizontally in the test fixture, tensile force f shall be applied to the end of the accessory, see Figure 4 or Figure 5. It shall be increased at a rate not exceeding 20 N/s until the specified value is reached and maintained for 1 min. Figure 4 -

19、 Tensile force (straight accessory) Figure 5 - Tensile force (90 accessory) c) Phase C: torsion test With the specimens placed horizontally in the test fixture, the torsional moment C shall be applied to the end of the accesory, see Figure 6 or Figure 7. This force shall be increased at a rate not e

20、xceeding 20 N/s until the specified value is reached and maintained for one minute. Figure 6 -Torsional moment (straight accessory) Figure 7 -Torsional moment (90 accessory) Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for Resa

21、leNo reproduction or networking permitted without license from IHS-,-,-Page 6 prEN 2591-420:2005 d) Phase D: torsion test on the mating thread With the specimens placed in the test fixture, a torque shall be applied to the coupling nut at a rate of 1 f 0,1 Nm/s until the specified value is reached a

22、nd maintained for one minute. 6 Requirements At the end of phase D, prior to removal, there shall be no play between the accessory and the test fixture. The untightening torque shall comply with the specified value. After removal, the specimens shall be examined visually according to EN 2591-1 01. No deformation shall be observed. 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-,-,-