EN 4536-2-2009 en Aerospace series - Bushes plain in corrosion resisting steel with self-lubricating liner elevated load - Part 2 Dimensions and loads - Inch series《航空航天系列 带有高负荷自润滑.pdf
《EN 4536-2-2009 en Aerospace series - Bushes plain in corrosion resisting steel with self-lubricating liner elevated load - Part 2 Dimensions and loads - Inch series《航空航天系列 带有高负荷自润滑.pdf》由会员分享,可在线阅读,更多相关《EN 4536-2-2009 en Aerospace series - Bushes plain in corrosion resisting steel with self-lubricating liner elevated load - Part 2 Dimensions and loads - Inch series《航空航天系列 带有高负荷自润滑.pdf(16页珍藏版)》请在麦多课文档分享上搜索。
1、BS EN 4536-2:2009ICS 49.035NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Bushes, plain in corrosion-resisting steel with self-lubricating liner, elevated load Part 2: Dimensions and loads Inch seriesThis British Standardwas published under the
2、authority of the StandardsPolicy and StrategyCommittee on 31 July2009. BSI 2009ISBN 978 0 580 57132 9Amendments/corrigenda issued since publicationDate CommentsBS EN 4536-2:2009National forewordThis British Standard is the UK implementation of EN 4536-2:2009.The UK participation in its preparation w
3、as entrusted to TechnicalCommittee ACE/12, Aerospace fasteners and fastening systems.A list of organizations represented on this committee can be obtained onrequest to its secretary.This publication does not purport to include all the necessary provisionsof a contract. Users are responsible for its
4、correct application.Compliance with a British Standard cannot confer immunityfrom legal obligations.BS EN 4536-2:2009EUROPEAN STANDARDNORME EUROPENNEEUROPISCHE NORMEN 4536-2July 2009ICS 49.035English VersionAerospace series - Bushes, plain in corrosion resisting steel withself-lubricating liner, ele
5、vated load - Part 2: Dimensions andloads - Inch seriesSrie arospatiale - Bagues en acier rsistant lacorrosion garniture autolubrifiante, charge leve - Partie2: Dimensions et charges - Srie en inchesLuft- und Raumfahrt - Buchsen aus korrosionsbestndigemStahl, mit selbstschmierender Beschichtung, erhh
6、teBelastung - Teil 2: Mae und Belastungen - Inch ReiheThis European Standard was approved by CEN on 23 April 2009.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any al
7、teration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the CEN Management Centre or to any CEN member.This European Standard exists in three official versions (English, French, German). A version in any other language made by tra
8、nslationunder the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as theofficial versions.CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland,France, Germany,
9、 Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMIT EUROPEN DE NORMALISATIONEUROPISCHES KOMITEE FR NORMUNGManageme
10、nt Centre: Avenue Marnix 17, B-1000 Brussels 2009 CEN All rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4536-2:2009: EBS EN 4536-2:2009EN 4536-2:2009 (E) 2 Contents Page Foreword 31 Scope 42 Normative references 43 Terms and definitions .4
11、4 Requirements .44.1 Configuration, dimensions, tolerances and mass .44.2 Surface roughness 44.3 Materials .54.4 Surface treatment 55 Designation . 126 Marking 127 Technical specification 128 Design recommendation 12BS EN 4536-2:2009EN 4536-2:2009 (E) 3 Foreword This document (EN 4536-2:2009) has be
12、en prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member
13、 countries of ASD, 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 January 2010, and conflicting national standards shall be withdrawn at the latest by January 20
14、10. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organiza
15、tions of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Roman
16、ia, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4536-2:2009EN 4536-2:2009 (E) 4 1 Scope This standard specifies the characteristics of plain bushes in corrosion resisting steel with self-lubricating liner, elevated load for aerospace applications. The bushes are inte
17、nded for use in fixed or moving parts of the aircraft structure and control mechanisms. They shall be used in the temperature range 55 C to 163 C. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition
18、cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2311, Aerospace series Bushes with self-lubricating liner Technical specification EN 2424, Aerospace series Marking of aerospace products EN 3161, Aerospace series Steel FE-PM3
19、801 (X5CrNiCu17-4) Air melted, solution treated and precipitation treated, bar a or D 200 mm, Rm 930 MPa TR 4475, Aerospace series Bearings and mechanical transmissions for airframe applications Vocabulary 1) ISO 2768-1, General tolerances Part 1: Tolerances for linear and angular dimensions without
20、 individual tolerance indications ISO 8075, Aerospace Surface treatment of hardenable stainless steel parts 3 Terms and definitions For the purposes of this document, the terms and definitions given in TR 4475 apply. 4 Requirements 4.1 Configuration, dimensions, tolerances and mass According to Figu
21、re 1 and Tables 1 and 2. Dimensions apply after surface treatment. Dimensions and tolerances are expressed in millimetres (inches). General tolerances shall be ISO 2768-m in accordance with ISO 2768-1. 4.2 Surface roughness According to Figure 1. 1) Published as ASD Technical Report at the date of p
22、ublication of this standard. BS EN 4536-2:2009EN 4536-2:2009 (E) 5 4.3 Materials Bush: Stainless steel according to EN 3161 Liner: Self-lubricating wear resistant material consistent with the requirements of EN 2311 4.4 Surface treatment Code T: Passivation according to ISO 8075. Key aChamfer machin
23、ed before bonding bChamfer or radius at manufacturers option cChamfer machined after bonding Figure 1 Configuration BS EN 4536-2:2009EN 4536-2:2009 (E) 6 Table 1 Dimensions and tolerances Diameter code a d D a Nominal diameter 0 0,025 0 0,013 2 (0 0.0010) (0 0.0005) 04 6,350 (0.2500) 6,388 (0.2515)
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