1、CEN PREN*25L (PARTSE61 92 3404589 0027072 T - Edition approved for publication Comments should be sent within six months after the date of publication decision Technopolis - 175, rue Jean-Jacques Rousseau 92138 Issy-les-Moulineaux Cdex - FRANCE 1992-06-05 A.E.C.M.A. A. E. C. M. A. STAN DARD NORME A.
2、E.C.M.A. A.E.C.M.A. NORM C2 Chairman M. J. LE CUNFF prEN 2591 Part E6 Issue P 1 June 1992 $DITE PAR LASSOCIATION EUROPENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cdex -Tl. (1) 47.36.98.76 UDC : Key words ENGLISH VERSION Aero
3、space series Elements of electrical and optical connection Test methods Part E6 - Use of tools . Srie arospatiale Luft- und Raumfahrt Mthodes dessais Prfverfahren Organes de connexion lectrique et optique Partie E6 - Utilisation des outils Elektrische und optische Verbindungselemente Teil E6 - Anwen
4、dung der Werkzeuge This (Aerospace Series9 pre-standard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs 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
5、 Commission following comment by the Member countries. Subsequent to the publication of this pre-standard, 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 signatu
6、re of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for final vote. aecrna 1992 Copyright Association Europeene des Constructeurs de Mate
7、riel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Q prEN 2591-E6 Page 3 1 Scope and field of application This standard specifies a method of checking the ability of the elements of connection to withstand the u
8、se of the standardized tooling for insertion and extraction of electrical contacts. It shall be used together with EN 2591. 2 References EN 2591 Aerospace series - Elements of electrical and optical connection - Test methods = General EN 2591-Al Aerospace series - Elements of electrical and optical
9、connection - Test methods - Part Al - Visual examination 1) EN 2591-09 Aerospace series - Elements of electrical and optical connection - Test methods - Part D9 - Contact retention in insert 2) 3 - Preparation of specimens 3.1 The specimens are fitted with all their contacts wired in accordance with
10、 the technical specification. 3.2 Unless indicated in the technical specification, the following details shall be specified : - type of cable, - tool or tools for insertion of contacts, - tool or tools for extraction of contacts, - forces to be applied on the tool for phases 1 and 2, - value of the
11、contact retention force. 4 Method 4.1 Number of contacts to be tested per size of contact . For each phase five contact cavities shall be tested. The contact cavity which has been used for the tests in one phase shall not undergo another test. 1) In preparation at the date of publication of the pres
12、ent standard. 2) Published as AECMA pre-standard at the date of publication of the present standard. -. 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 witho
13、ut license from IHS-,-,-CEN PREN*Z59L (PARTxEb) 92 m 3404589 0027074 3 I prEN 2591-E6 Page 4 4.2 Procedure Phase 1 - Rotation of the extraction tool The specified extraction tool having been introduced into a cavity containing the contact, an axial load as defined by the technical specification shal
14、l be applied to it. This load being maintained, an alternating rotation shall be carried out as shown in figure 1 ; the tool shall then be extracted with the contact. The contact shall be reintroduced. This operation shall be carried out four times on each of five contacts. Phase 2 - Rotation of the
15、 insertion tool The contact shall first of all be withdrawn and then re-inserted into its cavity using the insertion tool, on which an axial load as defined in the technical specification shall be applied. With this load maintained, an alternating rotation shall be carried out as indicated in the fi
16、gure 1. The tool shall then be extracted and then the contact shall be withdrawn. This operation shall be carried out four times on each of the five contacts. Figure 1 If a tool is damaged during the test, it shall be replaced. 4.3 Final measurements (if applicable) - EN 2591-A1 - Visual examination. - EN 2591-D9 - Contact retention in insert. 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-,-,-
