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    AECMA PREN 2591-D17-1992 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part D17 - Tensile Strength (Crimped Connection) Issue P 1《航空航天系列.光电连接元件 试验方法 D.pdf

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    AECMA PREN 2591-D17-1992 Aerospace Series Elements of Electrical and Optical Connection Test Methods Part D17 - Tensile Strength (Crimped Connection) Issue P 1《航空航天系列.光电连接元件 试验方法 D.pdf

    1、CEN PREN*259L (PART*DL7) 92 W 3404589 0027003 2 I Edition approved for publication 1992-06-05 A.E.C.M.A. STANDARD NORME A.E.C.M.A. A.E.C.M.A. NORM Comments should be sent within six months C2 Chairman after the date of publication decision A E.C.M A. Technopolis 175. rue Jean-Jacques Rousseau 921 38

    2、 Issy-les-Moulineaux Cdex - FRANCE M. J. LE CUNFF prEN 2591 Part Di7 Issue P 1 June 1992 EDIT PAR LASSOCIATION EUROPEENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cdex - T1 (1) 47 36.98.76 UDC : Key words ENGLISH VERSION Aeros

    3、pace series Elements of electrical and optical connection Test methods Part DI 7 - Tensile strength (crimped connection) Orga Srie arospatiale Luft- und Raumfahrt Mthodes dessais Prfverfahren Partie DI 7 - Rsistance la traction (connexion sertie) es d connexion lectrique et optique Elektrische und o

    4、ptische Verbindungselemente Teil Dl7 - Zugfestigkeit (Cri m pver bind ung ) This .Aerospace Series 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 b

    5、een technically approved by the experts of the concerned 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-ident

    6、ification 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 willbe submitted as a draft European Standard to CEN (European Committee for Standardization) for final vote. (c;) aecma 199

    7、2 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-,-,- CEN PREN82591 (PARTrD17) 92 m 3404589 002700Ll 4 m prEN 2591-D17 Page 3 1 Scope and field of applica

    8、tion This standard specifies a method of assessing the mechanical strength of crimped wire terminations for 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 3 Preparation of sp

    9、ecimens 3.1 The specimens shall be crimped with a tool as defined by the technical specification and wired : - for 50 % with conductors having the maximum section allowed by contact, - for 50 % with conductors having the minimum section allowed by contact. The length of the wire shall be as appropri

    10、ate for the tensile tester used. 3.2 Unless indicated in the technical specification, the following details shall be specified : - minimum and maximum sections of conductor for each contact size, - minimum tensile force to be applied for each contact size, - crimping tool. 4 Method 4.1 Number of con

    11、tacts to be measured per size Table 1 - Number of contacts of the same size in an element of connection : N Minimum percentage to be measured % NS 5 1 O0 5cNS 60 50 1) 25 1) N 130 10 1) 60 N I 130 1) The result shall be, if necessary, rounded up to the next full number Previous page is blank Copyrig

    12、ht Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-CEN PREN*Z591 (PART*D17) 72 I 3404589 0027085 b prEN 2591-DI7 Page 4 4.2 Procedure Crimped contacts shall be t

    13、ested individually in a tensile machine. The load shall be applied at a uniform speed of 25 mm/min to 50 mm/min along the contact axis. The tensile force shall be increased until the conductor or the joint breaks. 4 Requirement While the minimum force is applied no slip or pull out of the wire 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-,-,-


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