ASD-STAN PREN 4708-104-2016 Aerospace series Sleeving heat-shrinkable for binding insulation and identification Part 104 Semi-rigid polyvinylidene fluoride (PDVF) Operating tempera.pdf
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1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM ASD-STAN prEN 4708-104 Edition P 1 July 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: ENGLISH
2、 VERSION Aerospace series Sleeving, heat-shrinkable, for binding, insulation and identification Part 104: Semi-rigid polyvinylidene fluoride (PDVF) Operating temperature 55 C to 175 C Product standard Luft- und Raumfahrt Wrmeschrumpfender Schlauch zur Befestigung, Isolierung und Identifizierung Teil
3、 104: Halbsteif, Polyvenylidenfluorid (PVDF) Temperaturbereich 55 C bis 175 C Produktnorm Srie arospatiale Manchons thermortractables, de jonction, isolement et identification Partie 104 : Semi-rigide polyvinylidene fluoride (PVDF) Temprature dutilisation 55 C 175 C Norme de produit This “Aerospace
4、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 followi
5、ng 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 of ASD
6、-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 of a
7、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 suitabi
8、lity 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 send
9、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 of A
10、SD-STAN. Order details: E-mail: salesasd-stan.org Web address: http:/www.asd-stan.org/ Edition approved for publication 1st July 2016 Comments should be sent within six months after the date of publication to ASD-STAN Electrical Domain Copyright 2016 ASD-STAN prEN 4708-104:2016 (E) 2 Contents Page F
11、oreword 2 1 Scope 3 2 Normative references 3 3 Terms and definitions . 3 4 Required characteristics 4 5 Quality assurance 8 6 Designation . 9 7 Labelling and packaging . 9 8 Technical specification . 9 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Electrical Do
12、main. 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 4708-104:2016 (E) 3 1 Scope This standard specifies the required characteristics for a heat-shrinkable, semi-rig
13、id polyvinylidene sleeving for use in aircraft electrical systems at operating temperatures between 55 C and 175 C. This sleeving is basically transparent, but may be tinted. It is semi-rigid, tough and abrasion resistant, and is suitable for use where strain relief and mechanical protection are req
14、uired, or where their transparent properties are desirable. These sleevings are normally supplied with internal diameters up to 25,4 mm for shrink ratios of 2:1. Sizes other than those specifically listed in this standard may be available. These items shall be considered to comply with this standard
15、 if they comply with the property requirements listed in tables 2, 3 and 4 except for dimensions and mass. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the editio
16、n cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 3909, Aerospace series Test fluids for electrical and optical components and sub-assemblies EN 4708-001, Aerospace series Sleeving, heat-shrinkable, for binding, insulation a
17、nd identification Part 001: Technical specification IEC 60684-1:2011, Flexible insulating sleeving Part 1: Definitions and general requirements 1) IEC 60684-2:2005, Flexible insulating sleeving Part 2: Methods of test 1) IEC 60757:1983, Code for designation of colours 1) ISO 846:1997, Plastics Evalu
18、ation of the action of micro-organisms ISO 1817:2005, Rubber, vulcanized Determination of the effect of liquids MIL-PRF-87937, Performance specification: cleaning compound, aerospace equipment 2) AMS 1476B:2004, Deodorant, Aircraft Toilet 3) 3 Terms and definitions For the purposes of this document,
19、 the terms and definitions given in IEC 60684-1 apply. 1) Published by: IEC International Commission Electrotechnique Internationale. http:/www.iec.ch/ 2) Published by: Department of Defense (DoD). http:/www.defenselink.mil/ 3) Published by: SAE National (US) Society of Automotive Engineers. http:/w
20、ww.sae.org/ prEN 4708-104:2016 (E) 4 4 Required characteristics 4.1 Dimension and mass See Table 1. Table 1 Dimensional and mass requirements Size code Internal diameter mm Recovered wall thickness mm Mass per unit length max. g/m Expanded min. Recovered max. 1,2/0,6 1,2 0,6 0,25 0,05 1,5 1,6/0,8 1,
21、6 0,8 0,25 0,05 1,9 2,4/1,2 2,4 1,2 0,25 0,05 2,5 3,2/1,6 3,2 1,6 0,25 0,05 3,2 4,8/2,4 4,8 2,4 0,25 0,05 4,6 6,4/3,2 6,4 3,2 0,30 0,10 8,1 9,5/4,8 9,5 4,8 0,30 0,10 11,8 12,7/6,4 12,7 6,4 0,30 0,10 15,4 19,0/9,5 19,0 9,5 0,45 0,10 31,2 25,4/12,7 25,4 12,7 0,50 0,10 45,1 4.2 Conditions of test Unles
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