EN 3061-2007 en Aerospace series - Bearings airframe rolling - Rigid single row ball bearings in corrosion resisting steel with flanged alignment housing - Dimensions and loads《航空航.pdf
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1、BRITISH STANDARDBS EN 3061:2007Aerospace series Bearings, airframe rolling Rigid single row ball bearings in corrosion resisting steel, with flanged alignment housing Dimensions and loadsThe European Standard EN 3061:2007 has the status of a British StandardICS 49.035g49g50g3g38g50g51g60g44g49g42g3g
2、58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 3061:2007This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 July 200
3、7 BSI 2007ISBN 978 0 580 58103 8National forewordThis British Standard is the UK implementation of EN 3061:2007. The UK participation in its preparation was entrusted to Technical Committee MCE/7, Rolling bearings.A list of organizations represented on this committee can be obtained on request to it
4、s secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunity from legal obligations.Amendments issued since publicationAmd. No. Date CommentsEUROPEAN ST
5、ANDARDNORME EUROPENNEEUROPISCHE NORMEN 3061June 2007ICS 49.035English VersionAerospace series - Bearings, airframe rolling - Rigid single rowball bearings in corrosion resisting steel, with flanged alignmenthousing - Dimensions and loadsSrie arospatiale - Roulements pour structures daronefs- Rouleme
6、nts en acier rsistant la corrosion, rigides, une range de billes, avec bague dalignement collerette -Dimensions et chargesLuft- und Raumfahrt - Flugwerklager - EinreihigeRillenkugellager aus korrosionsbestndigem Stahl mitselbsteinstellendem Flansch - Mae und BelastungenThis European Standard was app
7、roved by CEN on 16 March 2006.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 alteration. Up-to-date lists and bibliographical references concerning such nationalst
8、andards 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 translationunder the responsibility of a CEN member into its own language and notified
9、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, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Net
10、herlands, Norway, Poland, Portugal,Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMIT EUROPEN DE NORMALISATIONEUROPISCHES KOMITEE FR NORMUNGManagement Centre: rue de Stassart, 36 B-1050 Brussels 2007 CEN All rights of exploitation i
11、n any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 3061:2007: E2 Contents Page Foreword3 1 Scope 4 2 Normative references 4 3 Terms and definitions .5 4 Symbols and abbreviations 5 5 Required characteristics.5 6 Designation 10 7 Marking .10 8 Technical specification .
12、10 EN 3061:20073 Foreword This document (EN 3061:2007) has been 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
13、National Associations and the Official Services of the member 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 December 2007, and conflicting nat
14、ional standards shall be withdrawn at the latest by December 2007. 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 CE
15、N/CENELEC Internal Regulations, the national standards organizations 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,
16、Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 3061:20074 1 Scope This standard specifies the characteristics of rigid single row ball bearings in corrosion resisting steel with a solid or lightweight flang
17、ed alignment housing, designed to withstand only slow rotations and slight oscillations under load. They are intended for use in the hubs of torsion lever and in separated supports for airframe/aerospace applications. The airframe rolling bearings defined in this standard may be used in the temperat
18、ure range from 54 C to 150 C. However, being lubricated with the following greases (see EN 3727): ester type very high pressure grease (code letter A), operating range from 73 C to 121 C or, synthetic hydrocarbons type very high pressure grease general purpose (code letter B) operating range from 54
19、 C to 177 C. Their field of application when lubricated with code letter A grease is limited to 121 C. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the l
20、atest edition of the referenced document (including any amendments) applies. ISO 1132-1, Rolling bearings Tolerances Part 1: Terms and definitions. ISO 8075, Aerospace Surface treatment of hardenable stainless steel parts. EN 2030, Steel FE-PM43 Hardened and tempered Bars D 150 mm Aerospace series.1
21、)EN 2226, Steel FE-PM43 Hardened and tempered Hand and die forgings De 150 mm Aerospace series. 1)EN 2424, Aerospace series Marking of aerospace products. EN 2502, Steel FE-PM66 930 Rm 1 080 MPa Bars De 150 mm Aerospace series. 1)EN 2503, Steel FE-PM66 930 Rm 1 080 MPa Forgings De 150 mm Aerospace s
22、eries. 1)EN 25392), Aerospace series Steel FE-PM3801(X5CrNiCu17-4) Air melted Solution treated and precipitation treated Bar a or D 200 mm Rm 965 MPa.3)EN 3161, Aerospace series Steel FE-PM3801 (X5CrNiCu17-4) Air melted Solution treated and precipitation treated Bar a or D 200 mm Rm 930 MPa. 3)EN 37
23、27, Aerospace series Bearings, airframe rolling rigid with flanged alignment housing Technical specification. 1) Published as ASD Standard at the date of publication of this standard. 2) Inactive for new design, see EN 3161. 3) Published as ASD Prestandard at the date of publication of this standard
24、. EN 3061:20075 3 Terms and definitions For the purposes of this document, the terms and definitions given in ISO 1132-1 and the following apply. 3.1 bearing full complement of balls (without retainer), with filling slot 4 Symbols and abbreviations dmp= single plane mean bore diameter deviation ds=
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