BS EN 2601-1996 Fork ends adjustable - Technical specification《可调节叉型端部 技术规范》.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS EN 2601:1996 Fork ends, adjustable Technical specification The European Standard EN 2601:1996 has the status of a British Standard ICS 49.040.30BS EN 2601:1996 This British Standard, having been prepared under the direction of the Engineering Sector Board, was pu
2、blished under the authority of the Standards Board and comes into effect on 15 December 1996 BSI 11-1998 The following BSI references relate to the work on this standard: Committee reference ACE/14 Draft for comment 90/73742 DC ISBN 0 580 26347 9 Committees responsible for this British Standard The
3、preparation of this British Standard was entrusted to Technical Committee ACE/14, Aerospace details and parts, upon which the following bodies were represented: British Iron and Steel Producers Association Civil Aviation Authority (Airworthiness Division) Federation of Wire Rope Manufacturers of Gre
4、at Britain Institute of Petroleum Ministry of Defence Society of British Aerospace Companies Amendments issued since publication Amd. No. Date CommentsBS EN 2601:1996 BSI 11-1998 i Contents Page Committees responsible Inside front cover National foreword ii Foreword 2 1 Scope 3 2 Normative reference
5、s 3 3 Definitions 3 4 Required characteristics, inspection and test methods 3 5 Quality assurance 6 6 Packaging 6 7 Certificate of conformity 7 Figure 1 Discontinuities on crest of thread 5 Figure 2 Discontinuities on thread flank 6 Table 1 Untitled 4 Table 2 Non-destructive inspections and tests to
6、 be carried out for qualification 7 Table 3 Destructive inspections and tests to be carried out for qualification 7 Table 4 Inspections and tests to be carried out for acceptance 7 List of references Inside back coverBS EN 2601:1996 ii BSI 11-1998 National foreword This British Standard has been pre
7、pared by Technical Committee ACE/14 and is the English language version of EN 2601:1996 Aerospace series Fork ends, adjustable Technical specification, published by the European Committee for Standardization (CEN). EN 2601:1996 was produced as a result of international discussions in which the Unite
8、d Kingdom took an active part. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are responsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Cross-refe
9、rences Publication referred to Corresponding British Standard BS 6293 Aerospace. MJ threads ISO 5855-1:1988 Part 1:1994 General requirements ISO 5855-2:1988 Part 2:1994 Limit dimensions for bolts and nuts EN 3042:1991 BS EN 3042:1992 Quality assurance. EN aerospace products. Qualification procedure
10、Summary of pages This document comprises a front cover, an inside front cover, pages i and ii, theEN title page, pages 2 to 8, an inside back cover and a back cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment
11、table on theinside front cover.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2601 July 1996 ICS 49.040.30 Descriptors: Aircraft, industry, aircraft control, rod fork-end, threaded shank, specification English version Aerospace series Fork ends, adjustable Technicalspecification Srie arospatia
12、le Embouts rglables chape Spcification technique Luft und Raumfahrt Einstellbare Gabelkpfe Technische Lieferbedingungen This European Standard was approved by CEN on 1995-12-27. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this E
13、uropean 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 Central Secretariat or to any CEN member. This European Standard exists in three official versions (Engl
14、ish, 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 the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Denmark, F
15、inland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050
16、 Brussels 1996 Copyright reserved to CEN members Ref. No. EN 2601:1996 EEN 2601:1996 BSI 11-1998 2 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries and votes carried out in accordance with the rules of this Association,
17、 this Standard has received the approval of the National Associations and the Official Services of the member countries of AECMA, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, a
18、t the latest by January 1997, and conflicting national standards shall be withdrawn at the latest by January 1997. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Denma
19、rk, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the United Kingdom.EN 2601:1996 BSI 11-1998 3 1 Scope This standard specifies the required characteristics, inspection and test methods, qualification and acceptan
20、ce conditions for single or double adjustable fork ends with threaded shank used with flight control rods. It is applicable whenever referenced. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are
21、 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 references the latest ed
22、ition of the publication referred to applies. ISO 5855-1, Aerospace MJ threads Part1:General requirements. ISO 5855-2, Aerospace MJ threads Part2:Limit dimensions for bolts and nuts. EN 2002-16, Aerospace series Test methods for metallic materials Part 16: Dye penetrant testing 1) . EN 3042, Aerospa
23、ce series Quality assurance EN aerospace products Qualification procedure. 3 Definitions For the purposes of this standard, the following definitions apply: 3.1 Surface discontinuities 3.1.1 crack break in the material which may extend in all directions and be intercrystalline or transcrystalline in
24、 character 3.1.2 score, scratch open surface defect 3.1.3 lap surface defect where particles of metal or sharp edges are folded over and then rolled or forged into the surface 3.1.4 seam unwelded fold which appears as an open defect in the material 3.2 production batch batch consisting of fork ends
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