ASD-STAN PREN 4708-101-2015 Aerospace series Sleeving heat-shrinkable for binding insulation and identification Part 101 Polyolefin sleeving Operating temperatures - 55 to 135 Prod.pdf
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1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 4708-101 Edition P 1 July 2015 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 VERSION
2、Aerospace series Sleeving, heat-shrinkable, for binding, insulation and identification Part 101: Polyolefin sleeving Operating temperatures 55 C to 135 C Product standard Srie arospatiale Manchons thermortractables, de jonction, isolement et identification Partie 101 : Gaine polyolfine Tempratures d
3、utilisation 55 C 135 C Norme de produit Luft- und Raumfahrt Wrmeschrumpfender Schlauch zur Befestigung, Isolierung und Identifizierung Teil 101: Polyolefin-Schlauch Temperaturbereich 55 C bis 135 C Produknorm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN
4、(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 following member comments. Subsequent to the publication of this Prestandard, the
5、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-STAN, it will be submitted as a draft European Standard (prEN) to CEN (Eur
6、opean 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 national standard and by withdrawing any national standards conflicting with the EN. Editi
7、on approved for publication 1st July 2015 Comments should be sent within six months after the date of publication to ASD-STAN Electrical Domain Copyright 2015 by ASD-STAN prEN 4708-101:2015 (E) 2 Contents Page Foreword 2 1 Scope 3 2 Normative references 3 3 Terms and definitions . 4 4 Required chara
8、cteristics . 4 5 Quality assurance 10 6 Designation 11 7 Labelling and packaging .11 8 Technical specification .11 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN de
9、fined in ASD-STANs General Process Manual, this standard has received approval for Publication. prEN 4708-101:2015 (E) 3 1 Scope This standard specifies the required characteristics for four types of heat-shrinkable polyolefin sleevings for use in aircraft electrical systems at operating temperature
10、s between 55 C and 135 C. Type A: Very flexible, flame retarded, shrink ratio 2:1 This sleeving has very good flexibility, is flame retarded and will shrink at low temperatures. It is suitable where sensitive components and delicate wiring need protection from excessive heat during shrinking. Type B
11、: Flexible, flame retarded, shrink ratio 2:1, 3:1 and 4:1 This sleeving is flexible and flame retarded. It is suitable for general purposes and is available with high shrink ratios. Type C: Flexible, not flame retarded, shrink ratio 2:1 and 3:1 This sleeving is flexible and not flame retarded and is
12、 available in two shrink ratios. Type D: Semi-rigid, flame retarded, shrink ratio 2:1 This sleeving is semi-rigid and flame retarded. It is suitable where strain relief and mechanical support are required These sleevings are normally supplied with internal diameters up to 102 mm for shrink ratios of
13、 2:1 and 4:1 and up to 39 mm for shrink ratios of 3:1 and in the following colours for type B, black, brown, red, yellow, green, blue, orange, violet, grey, white and green/yellow.Types A and D are black only. Type C is transparent, is not flame retarded and does not meet the flammability requiremen
14、ts of EN 4708-001. Sizes or colours other than those specifically listed in this standard may be available. These items shall be considered to comply with this standard if they comply with the property requirements listed in Tables 5, 6 and 7 except for dimensions and mass. 2 Normative references Th
15、e following documents, in whole or in part, 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 3909,
16、Aerospace series Test fluids and test methods for electric components and sub-assemblies EN 4708-001, Aerospace series Sleeving, heat-shrinkable, for binding, insulation and identification Part 001: Technical specification IEC 60684-1:2011, Specification for flexible insulating sleeving Part 1: Defi
17、nitions 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 Evaluation of the action of micro-organisms ISO 1817:2005, Rubber, vulcanized Determination of the effect of liquids
18、 1) Published by: IEC International Electrotechnical Commission. http:/www.iec.ch/ prEN 4708-101:2015 (E) 4 ISO 11075:2007, Aircraft De-icing/anti-icing fluids ISO type I ISO 11078:2007, Aircraft De-icing/anti-icing fluids ISO types II, III and IV MIL-PRF-87937, Performance specification: cleaning c
19、ompound, aerospace equipment 2) AMS 1428:2013, Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV 3) ASTM D740, Standard Specification for Methyl Ethyl Ketone 4) 3 Terms and definitions For the purposes of this document, the terms and definitions given in IE
20、C 60684-1 apply. 4 Required characteristics 4.1 Dimensions and mass See Tables 1, 2, 3 and 4. Table 1 Dimensional and mass requirements for Types A, B and C, shrink ratio 2:1 Size code Internal diameter mm Recovered wall thickness mm Mass per unit length g/m max. Expanded min. Recovered max. Type A
21、Type B Type C 1,2/0,6 1,2 0,6 0,45 0,10 2,8 2,7 2,0 1,6/0,8 1,6 0,8 0,45 0,10 3,3 3,2 2,3 2,4/1,2 2,4 1,2 0,50 0,10 4,7 4,6 3,4 3,2/1,6 3,2 1,6 0,50 0,10 5,8 5,6 4,1 4,8/2,4 4,8 2,4 0,50 0,10 7,8 7,6 5,7 6,4/3,2 6,4 3,2 0,65 0,15 14,0 13,6 10,0 9,5/4,8 9,5 4,8 0,65 0,15 19,6 19,0 14,1 12,7/6,4 12,7
22、6,4 0,65 0,15 25,0 24,4 18,1 19,0/9,5 19,0 9,5 0,75 0,15 40,1 39,4 29,4 25,4/12,7 25,4 12,7 0,90 0,15 63,0 61,2 45,3 38,0/19,0 38,0 19,0 1,00 0,20 106 103 76,1 51,0/25,4 51,0 25,4 1,15 0,25 164 159 118 76,0/38,0 76,0 38,0 1,25 0,25 259 252 186 102,0/51,0 102,0 51,0 1,40 0,25 380 369 273 2) Published
23、 by: Department of Defense (DoD). http:/www.defenselink.mil/ 3) Published by: SAE National (US) Society of Automotive Engineers. http:/www.sae.org/ 4) Published by: ASTM National (US) American Society for Testing and Materials. http:/www.astm.org/ prEN 4708-101:2015 (E) 5 Table 2 Dimensional and mas
24、s requirements for Types B and C, shrink ratio 3:1 Size code Internal diameter mm Recovered wall thickness mm Mass per unit length g/m max. Expanded min. Recovered max. Type B Type C 1,5/0,5 1,5 0,5 0,45 0,10 2,5 1,8 3,0/1,0 3,0 1,0 0,55 0,10 4,6 3,4 6,0/2,0 6,0 2,0 0,65 0,10 8,8 6,5 9,0/3,0 9,0 3,0
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