BS EN 2355-1989 Specification for fork-ends threaded control cable in corrosion resisting steel Dimensions and loads《耐蚀钢操纵钢索带螺纹的叉型端头规范 尺寸和负荷》.pdf

《BS EN 2355-1989 Specification for fork-ends threaded control cable in corrosion resisting steel Dimensions and loads《耐蚀钢操纵钢索带螺纹的叉型端头规范 尺寸和负荷》.pdf》由会员分享，可在线阅读，更多相关《BS EN 2355-1989 Specification for fork-ends threaded control cable in corrosion resisting steel Dimensions and loads《耐蚀钢操纵钢索带螺纹的叉型端头规范 尺寸和负荷》.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、BRITISH STANDARD AEROSPACE SERIES BS EN 2355:1989 Specification for Fork-ends, threaded, control cable in corrosion resisting steel Dimensionsandloads This European StandardEN2355 has the status of a British Standard. UDC 629.7.05:621.854:621.52.053.004.1BSEN2355:1989 This British Standard, having b

2、een prepared under the directionof the Aerospace Standards Policy Committee, waspublished under the authorityof the Board of BSIandcomes into effect on 31October1989 BSI 01-2000 The following BSI references relate to the work on this standard: Committee reference ACE/14 Draft for comment88/70402 DC

3、ISBN 0 580 17723 8 Cooperating organizations The European Committee for Standardization, under whose supervision this European Standard was prepared, comprises the national standards organizations of the following Western European countries. Austria Oesterreichisches Normungsinstitut Belgium Institu

4、t belge de normalisation Denmark Dansk Standardiseringsraad Finland Suomen Standardisoimisliito, r.y. France Association franaise de normalisation Germany Deutsches Institut fr Normung e.V. Greece Hellenic Organization for Standardization Ireland National Standards Authority of Ireland Italy Ente Na

5、zionale Italiano di Unificazione Netherlands Nederlands Normalisatie-instituut Norway Norges Standardiseringsforbund Portugal Instituto Portugus da Qualidade Spain Instituto Espaol de Normalizacin Sweden Standardiseringskommissionen i Sverige Switzerland Association suisse de normalisation UnitedKin

6、gdom British Standards Institution Amendments issued since publication Amd. No. Date of issue CommentsBSEN2355:1989 BSI 01-2000 i Contents Page Cooperating organizations Inside front cover National foreword ii Brief history 2 Text of EN 2355 3 National appendix A Inside back cover National appendix

7、B Inside back coverBSEN2355:1989 ii BSI 01-2000 National foreword This British Standard has been prepared under the direction of the Aerospace Standards Policy Committee and is the English language version ofEN2355 “Aerospace series. Fork-ends, threaded, control cable in corrosion resisting steel. D

8、imensions and loads”, published by the European Committee for Standardization (CEN). EN2355 was produced as a result of international discussion in which the UK took an active part. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards

9、are responsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pages i and ii, theEN title page, pages 2 to 6, an inside back cover and a back

10、cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside front cover.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN2355 September 1988 UDC: 629.7.05:621.854:621.52.053.004.1 Key words: Aircr

11、aft industry, flight control, flexible cable, cable tensioner, cable-end, dimensions, breaking loads. English version Aerospace series Fork-ends, threaded, control cable in corrosion resisting steel Dimensions and loads Srie arospatiale Embouts chape pour tendeurs en acier rsistant la corrosion Dime

12、nsions et charges Luft- und Raumfahrt Spannschrauben mit Gabel aus korrosionsbestndigem Stahl Mae und Belastungen This European Standard was accepted by CEN on1988-03-17. CEN members are bound to comply with the requirements of CEN Internal Regulations which stipulate the conditions for giving this

13、European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN Central Secretariat or to any CEN member. This European Standard exists in three official versions

14、(English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to CEN Central Secretariat has the same status as the official versions. CEN members are the national standards organizations of Austria, Belgium

15、, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and UnitedKingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels

16、CEN1988 Copyright reserved to all CEN members Ref. No. EN 2355:1988 EEN2355:1988 BSI 01-2000 2 Brief history This draft European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After enquiries and votes carried out in accordance with the rules of this Assoc

17、iation, this draft has successively received the approval of the National Associations and the Official Services of the member countries of AECMA, prior to its presentation to CEN. In accordance with the Common CEN/CENELEC Rules, the following countries are bound to implement this European Standard:

18、 Austria, Belgium, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and UnitedKingdom. Contents Page Brief history 2 1 Scope and field of application 3 2 References 3 3 Required characteristics 3 4 Designation 6 5 Marking 6 6 Techni

19、cal specification 6 Figure 4 Table 5EN2355:1988 BSI 01-2000 3 1 Scope and field of application This standard specifies the characteristics of threaded fork-ends in corrosion resisting steel intended for the turnbuckles of aircraft control cables. 2 References ISO 2020, Aerospace Mechanical system pa

20、rts Preformed flexible steel wire rope for aircraft controls Technical specification. ISO 5855-1, Aerospace construction MJ threads Part1: Basic profile. ISO 5855-2, Aerospace construction MJ threads Part2: Dimensions for bolts and nuts. EN 2363, Aerospace series Locking clips for turnbuckles of con

21、trol cables Dimensions . EN 2462, Steel FE-PA13 Softened Bars D e 100mm Aerospace series. EN 2516, Aerospace series Passivation of corrosion resistant steels 1) . EN 2569, Aerospace series Control cable fittings and turnbarrels Technical specification 1) . 3 Required characteristics 3.1 Dimensions T

22、olerances Loads Mass The configuration shall correspond to theFigure and the dimensions shall conform to the values given in theFigure and theTable. 3.2 Surface roughness SeeFigure. 3.3 Material Steel EN2462. 3.4 Surface treatment Passivation EN2516. 1) In preparation.EN 2355:1988 4 BSI 01-2000 Figu

23、re EN 2355:1988 BSI 01-2000 5 Table Dimensionsinmillimetres Thread a A B C D E F G H K L M N t Mass Minimum breaking load kN b Nominal diameter of cable used Code Designation H 11 0,1 H 8 0,5 0,5 Code Dimensions 0,5 min. max. 0,5 g 04 MJ 4 0,70 4h6h 2,5 5,5 5 10 1 9,5 15 2,9 8 S 37 3,25 3,36 24,5 0,

24、8 4 2,15 1,6 05 MJ 5 0,80 4h6h 3 6,5 12 11 23 3,8 10 S 50 4,16 4,33 30,5 0,10 9,2 4,45 2,4 L 63 43,5 10,3 06 MJ 6 1,00 4h6h 5 9,5 6 14 13 4,6 12 S 55 5,08 5,27 35 13,1 8,90 3,2 L 71 51 15,4 07 MJ 7 1,00 4h6h 6 10,5 17 14,5 25 5,6 14 S 62 6,08 6,27 39,5 0,15 20,2 12,45 4 L 80 57,5 23,7 08 MJ 8 1,00 4

25、h6h 6,5 13,5 8 20 1,5 18 28 6,6 16 S 70 7,08 7,27 44,5 0,20 34 18,60 4,8 10 MJ10 1,25 4h6h 7,5 15,5 23 20 31 7,8 20 S 84 8,98 9,19 56,5 56,3 24,90 5,6 12 MJ12 1,25 4h6h 8 17,5 10 25 22 35 9,8 24 S 88 10,98 11,19 57 82,4 31,20 6,4 a Conforming to ISO5855-1 andISO5855-2, rolled. b Equal to the one of

26、the cable used according to ISO2020. +0,60 0,25 +0,25 0 0 0,25 0 0,1 0 0,15EN2355:1988 6 BSI 01-2000 4 Designation Each threaded fork-end shall only be designated as in the following example: Where the following codes are applied for the thread direction: R = right-hand thread L = left-hand thread N

27、OTEIf necessary, originator codeS9005 may be intended between the description block and identity block. 5 Marking In addition to the manufacturers own marking, each threaded fork-end shall be marked (seeFigure) using the identity block as defined inclause4 of this standard. The marking method is to

28、the manufacturers option. 6 Technical specification The threaded fork-ends supplied according to this standard shall conform with the requirements ofEN2569.BSEN2355:1989 BSI 01-2000 National appendix A The UnitedKingdom participation in the preparation of this European Standard was entrusted by the

29、Aerospace Standards Policy Committee (ACE/-) to Technical Committee ACE/14 upon which the following bodies were represented: British Independent Steel Producers Association Civil Aviation Authority (Airworthiness Division) Federation of Wire Rope Manufacturers of GreatBritain Ministry of Defence Soc

30、iety of British Aerospace Companies Ltd. Stainless Steel Wire Export Group National appendix B The British Standards corresponding to the European and International Standards referred to in the text are identical in number and title to those given inclause2 with the exception ofISO2020, ISO5855-1 an

31、dISO5855-2 for which the corresponding British Standards are British Standard W13 (related), BS6293-1 (identical) andBS6293-2 (identical) respectively.BS EN 2355:1989 BSI 389 Chiswick High Road London W4 4AL BSIBritishStandardsInstitution BSI is the independent national body responsible for preparin

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