BS EN 2791-1991 Rod ends adjustable single fork and threaded shank with engagement 1 5 thread diameter Dimensions and loads《啮合量为1 5螺纹直径的单叉螺纹柄可调节的连杆端头 尺寸和负荷》.pdf
《BS EN 2791-1991 Rod ends adjustable single fork and threaded shank with engagement 1 5 thread diameter Dimensions and loads《啮合量为1 5螺纹直径的单叉螺纹柄可调节的连杆端头 尺寸和负荷》.pdf》由会员分享,可在线阅读,更多相关《BS EN 2791-1991 Rod ends adjustable single fork and threaded shank with engagement 1 5 thread diameter Dimensions and loads《啮合量为1 5螺纹直径的单叉螺纹柄可调节的连杆端头 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 2791:1991 Rod ends, adjustable, single fork and threaded shank with engagement: 1.5 thread diameter Dimensions and loads This European Standard EN2791:1991 has the status of a BritishStandardBSEN 2791:1991 This BritishStandard was published under the authority
2、 ofthe Standards Board and comesinto effect on 30August1991 BSI12-1999 The following BSI references relate to the work on this standard: Committee reference ACE/14 Draft for comment88/76837 DC ISBN 0 580 19887 1 Cooperating organizations The European Committee for Standardization, under whose superv
3、ision this European Standard was prepared, comprises the national standards organizations of the following Western European countries. Austria Oesterreichisches Normungsinstitut Belgium Institut belge de normalisation Denmark Dansk Standardiseringsraad Finland Suomen Standardisoimisliito, r.y. Franc
4、e Association franaise de normalisation Germany Deutsches Institut fr Normung e.V. Greece Hellenic Organization for Standardization Iceland Technological Institute of Iceland Ireland National Standards Authority of Ireland Italy Ente Nazionale Italiano di Unificazione Luxemburg Inspection du Travail
5、 et des Mines Netherlands Nederlands Normalisatie-instituut Norway Norges Standardiseringsforbund Portugal Instituto Portugus da Qualidade Spain Asociacin Espaola de Normalizacin y Certificacin Sweden Standardiseringskommissionen i Sverige Switzerland Association suisse de normalisation United Kingd
6、om BritishStandards Institution Amendments issued since publication Amd. No. Date CommentsBSEN 2791:1991 BSI 12-1999 i Contents Page Cooperating organizations Inside front cover National foreword ii Foreword 2 Text of EN2791 3 National appendix NA Inside back cover National appendix NB Inside back c
7、overBSEN 2791:1991 ii BSI 12-1999 National foreword This BritishStandard has been prepared under the direction of the Aerospace Standards Policy Committee and is the English language version of EN2791 “Aerospace series Rod ends, adjustable, single fork and threaded shank with engagement:1.5 thread d
8、iameter Dimensions and loads” published by the European Committee for Standardization (CEN). EN2791 was produced as a result of international discussions in which the United Kingdom took an active part. A British Standard does not purport to include all the necessary provisions of a contract. Users
9、of British Standards 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, pagesi andii, the EN title page, pages2 to6, an inside back
10、 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 table on the inside front cover.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN2791 UDC629.7.02:621.827.1:621.85.053.004.1 Key words: Ai
11、rcraft industry, flight control, rod ends, threaded shanks, dimensions, static loads English version Aerospace series Rod ends, adjustable, single fork and threaded shank withengagement:1,5 thread Dimensions and loads Srie arospatiale Embouts rglables chape simple et tige filete implantation:1,5 fil
12、etage Dimensions et charges Luft- und Raumfahrt Einstellbare Gabelkpfe einfach, mit Gewindeschaft mit Einschraubtiefe von1,5 Gewinde- Mae und Belastungen This European Standard was accepted by CEN on12 June1990. CEN members are bound to comply with the requirements of CEN Internal Regulations which
13、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 CEN Central Secretariat or to any CEN member. This European St
14、andard 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 CEN Central Secretariat has the same status as the official versions. CEN members are the national st
15、andards organizations 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 Nor
16、mung Central Secretariat: rue de Stassart 36, B-1050 Brussels CEN1991 Copyright reserved to all CEN members Ref. No. EN2791:1991 EEN 2791:1991 BSI 12-1999 2 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries and votes car
17、ried 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 AECMA, prior to its presentation to CEN. According to the Common CEN/CENELEC Rules, the following countrie
18、s are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom. Contents Page Foreword 2 1 Scope and field of application 3 2 References 3
19、3 Required characteristics 3 4 Designation 6 5 Marking 6 6 Technical specification 6 Figure 4 Table 5EN 2791:1991 BSI 12-1999 3 1 Scope and field of application This standard specifies the characteristics of adjustable rod-ends consisting of: a single fork; a threaded shank comprising: a circumferen
20、tial groove to identify engagement; an optional longitudinal groove for locking purposes. These rod ends are intended for use with flight control rods or rods for aircraft structures. The cadmium plating restricts the application to a temperature not exceeding235 C. 2 References ISO3353, Aerospace c
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