AECMA PREN 4056-001-2002 Aerospace Series Cable Ties for Harnesses Part 001 Technical Specification Edition P 1《航空航天系列铠装用绳索系材.第001部分 技术规范.P1版》.pdf

《AECMA PREN 4056-001-2002 Aerospace Series Cable Ties for Harnesses Part 001 Technical Specification Edition P 1《航空航天系列铠装用绳索系材.第001部分 技术规范.P1版》.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 4056-001-2002 Aerospace Series Cable Ties for Harnesses Part 001 Technical Specification Edition P 1《航空航天系列铠装用绳索系材.第001部分 技术规范.P1版》.pdf（9页珍藏版）》请在麦多课文档分享上搜索。

1、AECMA STANDARD prEN 4056-001 NORME AECMA Edition P 1 AECMA NORM June 2002 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION L%dDsTAm Gulledelle 94 - 6-1200 Brussels - Tel. + 32 2 775 81 10 - Fax. + 32 2 775 81 11 - www.aecma-stan.org ICs: 49.060 Descriptors: ENGLISH VER

2、SION Aerospace series Cable ties for harnesses Part O01 : Technical specification Srie arospatiale Frettes de cblage pour harnais Partie O01 : Spcification technique Luft- und Raumfahrt Befestigungsbnder fr Leitungsbndel Teil 001: Technische Lieferbedingungen This “Aerospace Series“ Prestandard has

3、been drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is published on green paper for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comment

4、s. 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 agreemenf of AECMA-STAN it will b

5、e submitfed as a draff European Standard to CEN (European Committee for standardization) for formal vote. Nota -Extra copies can be supplied by B.N.A.E. - Technopolic 54 - 199. rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX I I I Edition approved for publication Comments should be sent

6、within six months after the date of Dublication to 28 June 2002 AECMA-STAN Gulledelle 94 Electrical Domain 0-1200 BRUXELLES Copyright 2002 O by AECMA-STA Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or

7、 networking permitted without license from IHS-,-,-Page 2 prEN 4056-001 : 2002 Contents Scope Terms and defini Conditions of us . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . Descriptions and Tests . . . . . . . . . . . . . . . , . . . . . . . . . . . . . . . . . . . . . . . . . . . .

8、 . . . . . . , . . . , . , . . . . . . . . . . . Quality assurance . . . Designation and marking Packaging and st Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license fr

9、om IHS-,-,-Page 3 prEN 4056-001: 2002 I Scope This standard specifies the characteristics, test methods, qualification and acceptance conditions of plastic cable ties, used for the bundling, fixing andlor marking of cable harnesses in aircraft. The cable ties should be installedwith a qualified appl

10、ication tool, which controls the application force thus avoiding damage tothe cable insulation. It defines the aerospace requirements not specified in EN 501 46. 2 Normative references This European Standard incorporates by dated or undated reference, provisions from other publications. These normat

11、ive 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 Standard only when incorporated in it by amendment or revision. For undated refere

12、nces the latest edition of the publication referred to applies. IS0 8815 EN 2424 EN 2825 EN 2826 EN 3042 EN 3475-100 EN 4057 EN 4057-407 EN 50146 MS 90387 Aircraft - Electrical Cables and Cable Harnesses - Vocabulary Aerospace series - Marking of aerospace products Aerospace series - Burning behavio

13、ur of non metallic materials under the influence of radiating heat and flames - Determination of smoke density 1) Aerospace series - Burning behaviour of non metallic materials under the influence of radiating heat and flames - Determination of gas components in the smoke 1) Aerospace series - Quali

14、ty assurance - EN aerospace products - Qualification procedure Aerospace series - Cables, electrical, aircraft use - Test methods - Part 100: General 1) Aerospace series - Cable ties for harnesses -Test methods Aerospace series - Cable ties for harnesses - Test methods - Part 407: Verification of ap

15、plication tool settings 1) Cable Ties for Electrical Installations Tool, Hand, adjustable for plastic and metal tiedown straps 3 Terms and definitions For the purposes of this standard, the terms and definitions given in EN 3475-100 and IS0 8815 and the following apply: 3.1 cable loom or cable harne

16、ss any assembly of cables, complete with end terminals, which may be manufactured and formed on or off the aircraft, with two or more end destinations 3.2 cable bundle any group of cables which are tied together - 1) Published as AECMA Prestandard at the date of publication of this standard. And all

17、 its parts quoted in tables 3, 4 and 5 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-,-,-Page 4 prEN 4056-001 : 2002 4 Conditions of use 4.1 Temperature

18、ratings (type) The ties shall be capable of use within the following temperature ranges: - Type I : - 65 OC to 105 OC - Type 2: - 65 OC to 150 OC Temperature ratings shall be defined by the material code in table 1. 4.2 Flammability class Ties shall meet either class I or class 2 flammability requir

19、ements as defined in the appropriate product standard: - Class 1 has the highest degree of flame retardant properties; - Class 2 has a lower degree of flame retardant properties. 5 Descriptions and design 5.1 Description Ties, see figure 1, shall be designed for installation “y a tool providing cont

20、rolled tenv.m in accordance with MS 90387. The head design, locking system and strap cross sectional dimensions shall be such that the requirements of the tests given in clause 6 are met. Ties are available with plastic or metallic locking mechanisms and those with plastic locking mechanisms may hav

21、e either internal or external serrations on the strap. A . 1 l B I E I Figure I 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-,-,-Page 5 prEN 4056-001: 2

22、002 A B 5.2 Design and manufacture The finish shall prevent abrasion to the harness and to adjacent harnesses or breakouts. In completing the joint, no sharp or abrasive edges shall be formed that could damage the cable insulation of the loom or any adjacent looms, or that could cause injury to an o

23、perator. 1 Non UV resistant 1 UV resistant a 5.3 Materials C D Ties shall be made from virgin materials which may be formulated to be UV resistant. The use of in process reground material to a maximum of 25 % by mass is permissible but is limited to the percentage used in the qualification sample. M

24、aterials shall be identified by the codes in table 1. 2 Non UV resistant 2 UV resistant a Table 1 - Material codes Material description Temperature rating type Material code I 5.4 Colour Ties shall be either natural or unpigmented material finish or a colour according to the codes shown in table 2.

25、Table 2 - Colour codes The colour shall be uniform throughout any coloured tie. 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-,-,-Page 6 prEN 4056-001 :

26、2002 6 Tests All non-metallic materials used for the manufacture of cable ties shall be tested for their smoke and toxicity properties in accordance with EN 2825 and EN 2826 as defined in the product standard. Finished products shall be tested as detailed in table 3 and the product standard. Before

27、commencement of these tests the calibration of the application tools to be used shall be verified in accordance with Table 3 -Tests EN 4057-407. EN 4057- Designation of the test Number of specimens All test Specimens to be examined All test Specimens to be tested Details 201 ai Visual examination Th

28、ere shall be no sharp or abrasive edges. Examination of mass and dimensions The mass and dimensions shall be in accordance with the product standard. 202 a Salt mist test (applicable to ties containing metallic locking barbs) 3 specimens for each cross section grouping (.e. loop tensile strength gro

29、up) The minimum loop tensile strength shall be in accordance with the product standard. The locking device shall show no sign of corrosion. After removal of the burner from the specimen, any flame shall extinguish within 5 s. If there are no flaming droplets (or particles) during the test, and the f

30、lame extinguishes within 5 s, the specimen will be classified as Class 1. If there are flaming droplets (or particles) but all the flames extinguish within 5 s, the specimen will be classified as Class 2. The minimum loop tensile strength should be in accordance with the product standard 301 a 3 spe

31、cimens (see table 5) of the largest cross-section each material code. (.e. loop tensile strength group) 302 a Flammability 3 specimens for each material type and or class for each of the test solutions. 303 a Resistance to fluids 304 a Loop tensile strength at maximum working temperature 3 specimens

32、 for each cross section grouping (see table 5) (.e. loop tensile strength group) 1 specimen per colour, material type and material class The minimum loop tensile strength should be in accordance with the product standard. The colour fastness of the specimen should be in accordance with the product s

33、tandard. Colour fastness (applicable only to coloured ties) 305 a 306 a 307 a Heat ageing test 3 specimens for each material code and cross section group The tensile strength shall not be lower than that specified in the appropriate product standard Resistance to Ultra Violet radiation As detailed T

34、he average elongation at break of the exposed samples shall be not less than 60 % of the figure for the unexposed samples continued Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted

35、without license from IHS-,-,-Page 7 prEN 4056-001 : 2002 Table 3 -Tests (concluded) EN 4057- 401 402 a 404 a 405 a 406 a 407 a Designation of the test Loop tensile strength Life cycle Low temperature installation Compass safe distance (applicable to ties containing metallic locking barbs) Locking de

36、vice retention (applicable to ties containing metallic locking barbs) Verification of application tool settings _ - _ Number of specimens 3 specimens per cross section grouping (see table 5) Specimens for each cross section grouping (see table 5) (Le. loop tensile strength group) 3 specimens for eac

37、h cross section grouping (see table 5) (.e. loop tensile strength group) 1 specimen 3 specimens 5 specimens Details The minimum loop tensile strength shall be in accordance Mith the product standard 1. There shall be no damage to the cable insulation when viewed with a 10 times magnification aid. 2.

38、 The specimens shall be examined for cracks, breaking and/or release of the locking device during removal from the vibration test harness. 3. The minimum loop tensile strength shall be in accordance with the product standard. The minimum loop tensile strength shall be in accordance with the product

39、standard. The compass safe distance shall not exceed 125 mm. The force to pull out the barb from the tie head shall meet the requirement of the appropriate product standard. At the appropriate setting the reading for all 5 specimens shall be as detailed in the product standard -,o %. a Published as

40、AECMA Prestandard at the date of publication of this standard Small sizes may contain insufficient mass for these tests to be performed satisfactorily In preparaion at the date of publication of this standard 7 Quality assurance 7.1 General conditions Quality assurance conditions shall conform to EN

41、 3042. 7.2 Qualification testing All the applicable tests in table 3 shall be performed on all types, classes and colours of product at the commencement of manufacture, the use of new manufacturing tooling or change of raw material. These tests shall also be carried out at the re-commencement of pro

42、duction in the event of a stoppage longer than three years. 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-,-,-Page 8 prEN 4056-001 : 2002 EN 4057- Design

43、ation of the test 20 1 Visual examination 202 306 Heat ageing 401 Loop tensile strength 406 Locking device retention a Examination of mass and dimensions Number of specimens 6 specimens to be tested 3 specimens to be tested 3 specimens to be tested 3 specimens to be tested 3 specimens to be tested E

44、N 4057- Designation of the test 20 1 Visual examination 202 40 1 Loop tensile strength Examinations of mass and dimensions 8 Designation and marking Number of specimens 6 specimens to be tested 3 specimens to be tested. Dimensions only. 3 specimens per batch 8.1 Marking The manufacturers monogram in

45、 accordance with EN 2424 Style F shall be marked on the strap of the tie as close to the head as possible such that it is on the outside of the cable bundle after installation. 8.2 Designation EXAMPLE: Description block Identity block EN4056-001AlP1 Product standard number Material code (see table 1

46、) Flammability class (see 4.2) Size code (see table 6) Colour code (see table 2) Variant code (see table 7) ! Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from I

47、HS-,-,-Page 9 prEN 4056-001: 2002 Size code P R S T U V Table 6 - Size code Recommended bundle diameter mm min. max. 176 20 1,6 50 1,6 80 10 1 O0 1,6 110 10 130 Table 7 -Variant of cable tie (serration position) 9 Packaging and storage 9.1 Packaging Each packet shall be identified with the following

48、 information: a) Product designation; b) Manufacturers name; c) Manufacturers part number; d) Quantity; e) Batch number and date of manufacture. 9.2 Storage Until required for use, it is recommended that the product is protected from exposure to direct sunlight. 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-,-,-