BS EN 2644-1998 Rod assemblies for flight controls - Technical specification《飞行控制杆组件 技术规范》.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS EN 2644:1998 Rod assemblies for flight controls Technical specification The European Standard EN 2644:1998 has the status of a British Standard ICS 49.035BSEN2644:1998 This British Standard, having been prepared under the directionof the Engineering SectorBoard,
2、was published underthe authority of the Standards Board and comes into effect on 15 July 1998 BSI 05-1999 ISBN 0 580 31024 9 National foreword This British Standard is the English language version of EN2644:1998. The UK participation in its preparation was entrusted to Technical Committee ACE/14, Ae
3、rospace details and parts, which has the responsibility to: aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep the UK interests informed; monitor related international and European d
4、evelopments and promulgate them in the UK. A list of organizations represented on this committee can be obtained on request to its secretary. Cross-references The British Standards which implement international or European publications referred to in this document may be found in the BSI Standards C
5、atalogue under the section entitled “International Standards Correspondence Index”, or by using the “Find” facility of the BSI Standards Electronic Catalogue. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are responsible for the
6、ir 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, pagesi andii, the EN title page, pages2to9 and a back cover. This standard has been updated (see copyri
7、ght date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside front cover. Amendments issued since publication Amd. No. Date CommentsBSEN2644:1998 BSI 05-1999 i Contents Page National foreword Inside front cover Foreword 2 Text of EN 2644 3ii blankEU
8、ROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2644 April 1998 ICS 49.035 Descriptors: Aircraft industry, flight control, connecting rods, characteristics, inspection, tests qualification, quality assurance, acceptance testing, marking, packing English version Aerospace series Rod assemblies for
9、 flight controls Technical specification Srie arospatiale Bielles quipes pour commandes de vol Spcification technique Luft- und Raumfahrt Bediengestnge fr Flugsteuerungen Technische Lieferbedingungen This European Standard was approved by CEN on 17 October 1997. CEN members are bound to comply with
10、the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this 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 Central Secretariat
11、 or to any CEN member. This European Standard exists in three official versions (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 the Central Secretariat has the same status as the official ve
12、rsions. CEN members are the national standards bodies of Austria, Belgium, CzechRepublic, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and UnitedKingdom. CEN European Committee for Standardization Comit Euro
13、pen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1998 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2644:1998 EEN2644:1998 BSI 05-1999 2 Foreword This European Standard
14、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, this Standard has successively received the approval of the National Associations and the Official Services of the member countrie
15、s 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, at the latest by October1998, and conflicting national standards shall be withdrawn at the latest by October1998. Accor
16、ding to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, CzechRepublic, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, the Netherlands, Norway, Portu
17、gal, Spain, Sweden, Switzerland and the UnitedKingdom. Contents Page Foreword 2 1 Scope 3 2 Normative references 3 3 Description 4 4 Required characteristics, inspection and test methods 7 5 Quality assurance 9 6 Identification marking 9 7 Packaging 9 9 Certificate of compliance 9 Figure 1 4 Figure
18、2 5 Figure 3 6 Figure 4 8 Figure 5 Adjustment range 8 Table 1 4 Table 2 5 Table 3 6 Table 4 7 Table 5 Torsion resistance end fitting/rod body 8 Table 6 Adjustment range for length L related to theoretical length L 8 Table 7 Non-destructive tests 9 Table 8 Destructive tests 9EN2644:1998 BSI 05-1999 3
19、 1 Scope This standard specifies the required characteristics, inspections and tests, quality assurance, qualification, acceptance and delivery conditions for rod assemblies for flight controls, consisting of an aluminium alloy rod body and fixed or adjustable rod end fittings. It is applicable when
20、ever referenced. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendme
21、nts 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 edition of the publication referred to applies. EN 2290-1, Aerospace series Rod bodies for flight control, in aluminium alloys, fo
22、r adjustable end fittings Dimensions 1) . EN 2291, Aerospace series Rod assemblies for flight control in aluminium alloys, with one extremity for an adjustable end and one extremity fitted with a fixed single fork end fittings Dimensions 1) . EN 2292, Aerospace series Rod assemblies for flight contr
23、ol in aluminium alloys with fixed single fork end fittings Dimensions 1) . EN 2327, Aerospace series Washers, lock with radial serrations in alloy steel Dimensions. EN 2424, Aerospace series Marking of aerospace products. EN 2492, Aerospace series Rod ends, self-aligning ball bearing with threaded s
24、hank Dimensions and loads 2) . EN 2515, Aerospace series Rod ends, adjustable, single fork and threaded shank Dimensions and loads. EN 2546, Aerospace series Washers, lock with radial serrations in corrosion resisting steel Dimensions. EN 2586, Aerospace series Washers, lock for flight control rods
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