ASD-STAN PREN 4838-004-2016 Aerospace series Arc Fault Circuit breakers single-pole temperature compensated rated current 3 A to 25 A 115 V a c 400 Hz constant frequency Part 004 W.pdf
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1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM ASD-STAN prEN 4838-004 Edition P 1 September 2016 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Rue Montoyer 10 - 1000 Brussels - Tel. 32 2 775 8126 - Fax. 32 2 775 8131 - www.asd-stan.org ICS: Descriptors: EN
2、GLISH VERSION Aerospace series Arc Fault Circuit breakers, single-pole, temperature compensated, rated current 3 A to 25 A 115 V a.c. 400 Hz constant frequency Part 004: With signal contact Product standard Luft- und Raumfahrt Arc Fault Schutzschalter, einpolig, Temperaturkompensiert, Nennstrme von
3、3 A bis 25 A 115 V a.c. 400 Hz Konstantfrequenz Teil 004: Mit Signalkontakt Produktnorm Srie arospatiale Disjoncteurs unipolaires dtection darc compenss en temprature, intensits nominales 3 A 25 A 115 V a.c. 400 Hz frquence fixe Partie 004 : Avec contact de signalisation Norme de produit This “Aeros
4、pace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain fo
5、llowing member comments. Subsequent to the publication 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 o
6、f ASD-STAN, the ASD-STAN prEN will be submitted as a draft European 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
7、of a national standard and by withdrawing any national standards conflicting with the EN. ASD-STAN Technical Committee approves that: “This document is published by ASD-STAN for the needs of the European Aerospace Industry. The use of this standard is entirely voluntary, and its applicability and su
8、itability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” ASD-STAN reviews each standard and technical report at least every five years at which time it may be revised, reaffirmed, stabilized or cancelled. ASD-STAN invites you to
9、send your written comments or any suggestions that may arise. All rights reserved. No parts of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without prior written permission
10、 of ASD-STAN. Order details: E-mail: salesasd-stan.org Web address: http:/www.asd-stan.org/ Edition approved for publication 1st September 2016 Comments should be sent within six months after the date of publication to ASD-STAN Electrical Domain Copyright 2016 ASD-STAN prEN 4838-004:2016 (E) 2 Conte
11、nts Page Foreword 2 1 Scope 3 2 Normative references 3 3 Terms and definitions . 3 4 Dimension and mass 3 5 Characteristics . 6 6 Designation. 10 7 Rated current code 10 8 Delivery hardware codes 10 9 Marking 11 10 Technical Specification 11 Foreword This standard was reviewed by the Domain Technica
12、l Coordinator of ASD-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. prEN 4838-004:2016 (E) 3 1 Scope This standard specifies the required charact
13、eristics for single-pole, arc fault circuit breakers rated currents from 3 A to 25 A, switching capacity 65 In, for use in aircraft electrical systems. Their operating temperatures are between 40 C to 85 C at a maximum altitude of Z = 15 000 m. The thermal protection is temperature compensated and o
14、perates between 55 C and 125 C. These arc fault circuit breakers are operated by a push-pull type single pushbutton (actuator), with delayed action “trip-free“ tripping. They will continue to function up to the short-circuit current. 2 Normative references The following documents, in whole or in par
15、t, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 3155-016, Aerospace series Electrical contacts
16、used in elements of connection Part 016: Contacts, electrical, male, type A, crimp, class S Product standard EN 3841-100, Aerospace series Circuit breakers Test Methods Part 100: General EN 4838-001, Aerospace series Arc Fault Circuit breakers, single-pole, temperature compensated, rated current 3 A
17、 to 25 A 115 V a.c. 400 Hz constant frequency Part 001: Technical specification EN 6113, Aerospace series Circuit breaker, connecting and attachment hardware TR 6083, Aerospace series Cut-outs for installation of electrical components 1) MIL-I-81969/1-02, Installing and removal tools, connector elec
18、trical contact, Type III, Class 2, composition C 2) MIL-I-81969/14-11, Installing and removal tools, connector electrical contact, Type III, Class 2, composition B 2) FED-STD-595B, Colours used in Government Procurement 3 Terms and definitions For the purposes of this document, the terms and definit
19、ions given in EN 3841-100 apply. 4 Dimension and mass 4.1 Dimensional characteristics The circuit breakers do not have to correspond to the pictorial illustration, only the dimensions given shall be adhered to. See Figure 1. Dimensions are in millimetres with exception terminal thread 8-32 UNC. 1) P
20、ublished as ASD-STAN Technical Report at the date of publication of this standard by Aerospace and Defense industries Association of European-Standardization (ASD-STAN) (www.asd-stan.org) 2) Published by: DoD National (US) Mil. Department of Defense http:/www.defenselink.mil/ prEN 4838-004:2016 (E)
21、4 Key 1 Push button released 9 Gauge 20 connection pins according to EN 3155-016M2018 (terminals 3 and 4) 2 Green colour according to FED-STD-595B No. 34090 10 Indicative value 25 (see Note) 3 White 11 Positioning lug in accordance with the panel cut-out, as per TR 6083C202. Neutral connection 4 Mar
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