BS-EN-2515-1990.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS EN 2515:1990 Specification for Rod ends, adjustable single fork and threaded shank Dimensions and loads This European Standard EN 2515 has the status of a British Standard. Licensed Copy: sheffieldun sheffieldun, na, Fri Nov 03 02:05:55 GMT+00:00 2006, Uncontroll
2、ed Copy, (c) BSI BS EN 2515:1990 This British Standard was published under the authority of the Board of BSI and comes into effect on 31 December 1990 BSI 12-1999 The following BSI references relate to the work on this standard: Committee reference ACE/14 Draft for comment 89/79499 DC ISBN 0 580 190
3、70 6 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. AustriaOesterreichisches Normungsinstitut BelgiumInstitut belge de norma
4、lisation DenmarkDansk Standardiseringsraad FinlandSuomen Standardisoimisliito, r.y. FranceAssociation franaise de normalisation GermanyDeutsches Institut fr Normung e.V. GreeceHellenic Organization for Standardization IcelandTechnological Institute of Iceland IrelandNational Standards Authority of I
5、reland ItalyEnte Nazionale Italiano di Unificazione LuxemburgInspection du Travail et des Mines NetherlandsNederlands Normalisatie-instituut NorwayNorges Standardiseringsforbund PortugalInstituto Portugus de Qualidade SpainAsociacin Espaola de Normalizacin y Certificacin SwedenStandardiseringskommis
6、sionen i Sverige SwitzerlandAssociation suisse de normalisation United KingdomBritish Standards Institution Amendments issued since publication Amd. No.Date of issueComments Licensed Copy: sheffieldun sheffieldun, na, Fri Nov 03 02:05:55 GMT+00:00 2006, Uncontrolled Copy, (c) BSI BS EN 2515:1990 BSI
7、 12-1999i Contents Page Cooperating organizationsInside front cover National forewordii Brief history2 Text of EN 25153 National appendix AInside back cover National appendix BInside back cover Licensed Copy: sheffieldun sheffieldun, na, Fri Nov 03 02:05:55 GMT+00:00 2006, Uncontrolled Copy, (c) BSI
8、 BS EN 2515:1990 ii BSI 12-1999 National foreword This British Standard has been prepared under the direction of the Aerospace Standards Policy Committee and is the English language version of EN 2515 “Aerospace series. Rod ends, adjustable single fork and threaded shank. Dimensions and loads”, publ
9、ished by the European Committee for Standardization (CEN). EN 2515 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 are responsible for their
10、 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, the EN title page, pages 2 to 6, an inside back cover and a back cover. This standard has
11、 been updated (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside front cover. Licensed Copy: sheffieldun sheffieldun, na, Fri Nov 03 02:05:55 GMT+00:00 2006, Uncontrolled Copy, (c) BSI EUROPEAN STANDARD NORME EUROPENNE EUROPISCH
12、E NORM EN 2515 June 1990 UDC: 629.7.02:621.827.1:621.85.053.004.1 Key words: Aircraft industry, flight control, rod ends, threated ends, dimensions, static loads English version Aerospace series Rod ends, adjustable single fork and threaded shank Dimensions and loads Srie arospatiale Embouts rglable
13、s chape simple et tige filete Dimensions et charges Luft- und Raumfahrt Einstellbare Gabelkpfe einfach, mit Gewindeschaft Mae und Belastungen This European Standard was accepted by CEN on 1990-01-10. CEN members are bound to comply with the requirements of CEN Internal Regulations which stipulate th
14、e 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 CEN Central Secretariat or to any CEN member. This European Standard exist
15、s 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 CEN Central Secretariat has the same status as the official versions. CEN members are the national standards orga
16、nizations of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxemburg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central
17、 Secretariat: rue de Stassart 36, B-1050 Brussels CEN 1990 Copyright reserved to all CEN members Ref. No. EN 2515:1990 E Licensed Copy: sheffieldun sheffieldun, na, Fri Nov 03 02:05:55 GMT+00:00 2006, Uncontrolled Copy, (c) BSI EN 2515:1990 BSI 12-1999 2 Brief history This European Standard has been
18、 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 countries of AEC
19、MA, prior to its presentation to CEN. According to the Common CEN/CENELEC Rules, the following countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Swit
20、zerland and United Kingdom. Contents Page Brief history2 1Scope and field of application3 2References3 3Required characteristics3 4Designation6 5Marking6 6Technical specification6 Figure4 Table5 Licensed Copy: sheffieldun sheffieldun, na, Fri Nov 03 02:05:55 GMT+00:00 2006, Uncontrolled Copy, (c) BS
21、I EN 2515:1990 BSI 12-19993 1 Scope and field of application This standard specifies the characteristics of adjustable rod ends consisting of a rod end body with threaded shank consisting of: a single fork; a circumferential groove to identify location; an optional longitudinal groove for locking pu
22、rposes. These rod ends are intended for flight control rods or rods for aerospace structures. The cadmium plating restricts the application to temperature not exceeding 235 C. 2 References ISO 3353, Aerospace construction Rolled threads Runout and lead threads. ISO 5855-1, Aerospace MJ Threads Part
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