AECMA PREN 2349-413-2000 Aerospace Series Requirements and Test Procedures for Relays and Contactors Part 413 Vibration Sinusoidal and Random Edition P 1《航空航天系列继电器和接触器要求和试验程序.第413部.pdf

《AECMA PREN 2349-413-2000 Aerospace Series Requirements and Test Procedures for Relays and Contactors Part 413 Vibration Sinusoidal and Random Edition P 1《航空航天系列继电器和接触器要求和试验程序.第413部.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 2349-413-2000 Aerospace Series Requirements and Test Procedures for Relays and Contactors Part 413 Vibration Sinusoidal and Random Edition P 1《航空航天系列继电器和接触器要求和试验程序.第413部.pdf（4页珍藏版）》请在麦多课文档分享上搜索。

1、STD-AECMA PREN 23q7-413-ENGL Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX Comments should be sent within six months after the date of publication to Gulledelle 94 Edition approved for publication C2 Chairman Mr Pe

2、uetta 2000-01-31 AECMA 8-1200 BRUXELLES 0 aecma 201 AECMA STANDARD NORME AECMA AECMA NORM 2000 H 101Z311 0017592 053 H prEN 2349-413 Edition P 1 January 2000 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 8-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2

3、 775 81 11 ICs: Descriptors: ENGLISH VERSION Aerospace series Requirements and test procedures for relays and contactors Part 413: Vibration, sinusoidal and random Srie arospatiale Luft- und Raumfahrt Exigences et mthodes dessais des relais et contacteurs Partie 413: Vibration sinusodale et alatoire

4、 An for de ru ngen u nd P r fve ra h ren fr Relais und Schaltschtze Teil 413: Sinus Schwingungen und Rauschfrmigc This “Aerospace Series” Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs o

5、f 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 an extent that inferchangeability is affected, physically

6、 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 submiffed as a draft European Standard to CEN (European Committee for Standardizat

7、ion) 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-AECMA PREN 2349-413-ENGL 2000 lDL23Ll 0017593 TqT M Page 2 prEN 2349-41 3: 2

8、000 Con tents Scope . 3 Normative references 3 Method . 3 Requirements . 4 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 2347-413-ENG

9、L 2000 LOL23LL OOL7574 72b page3 prEN 2349-413: 2000 I Scope This standard specifies a method for checking the capability of relays and contactors to withstand sinusoidal and random vibrations. It shall be used together with EN 2349-100. 2 Normative references This European Standard incorporates by

10、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 references, subsequent amendments to or revisions of any of these publications apply to this European Standar

11、d only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 2349-1 O0 EN 2349-301 EN 2349-303 EN 2349-304 EN 2349-305 EN 2349-307 EN 2349-309 EN 2349-412 Aerospace series - Requirements and test procedures for relays a

12、nd contactors - Part 100: General requirements 1) Aerospace series - Requirements and test procedures for relays and contactors - Part 301: Pick-up and drop-out voltage 2) Aerospace series - Requirements and test procedures for relays and contactors - Part 303: Dielectric strength 2) Aerospace serie

13、s - Requirements and test procedures for relays and contactors - Part 304: Operate and release time 2) Aerospace series - Requirements and test procedures for relays and contactors - Part 305: Bounce time 2) Aerospace series - Requirements and test procedures for relays and contactors - Part 307: Co

14、ntact voltage drop 2) Aerospace series - Requirements and test procedures for relays and contactors - Part 309: Exported spikes 2) Aerospace series - Requirements and test procedures for relays and contactors - Part 41 2: Seal 2) IS0 71 37: 1995 Aircraft - Environmental conditions and test procedure

15、s for airborne equipment 3) 3 Method 3.1 Mounting of the relay or contactor on the vibrator table shall be rigid, so that the vibrations produced can be transmitted directly to the test sample without absorption or resonance. The electrical connections shall be wired in accordance with the product s

16、tandard. The wires shall be secured to the vibrator as close as possible to the point of electrical connection. Mo un t i n g I) in preparation at the date of publication of this standard 2) Published as AECMA Prestandard at the date of publication of this standard 3) Endorsement of publications EUR

17、OCAEIED-I4 and RTCAfDO-I60 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 23q9-413-ENGL 2000 LOL2333 0037595 Bb2 Page 4 prEN 2349-41 3:

18、 2000 3.2 Procedures The relay or contactor shall be subjected to a sinusoidal vibration test in accordance with IS0 71 37. For test conditions, see product standard. The relay or contactor shall be subjected to a random vibration test in accordance with IS0 7137. For test conditions, see product st

19、andard. 4 Requirements The torque for the connections and attachments shall not be less than 80 % of the rated value. No opening of closed contacts for longer than 1 O ps. No closing of open contacts for longer than 1 ps. Test in accordance with EN 2349-301,303, 304,305,307,309, and 412. 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-,-,-