EN 3059-2007 en Aerospace series - Bearings airframe rolling - Rigid single row ball bearings in steel with flanged alignment housing cadmium plated - Dimensions and loads《航空航天系列 飞.pdf
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1、BRITISH STANDARDBS EN 3059:2007Aerospace series Bearings, airframe rolling Rigid single row ball bearings in steel with flanged alignment housing, cadmium plated Dimensions and loadsThe European Standard EN 3059:2007 has the status of a British StandardICS 49.035g49g50g3g38g50g51g60g44g49g42g3g58g44
2、g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 3059:2007This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 July 2007 BSI
3、 2007ISBN 978 0 580 56298 3National forewordThis British Standard is the UK implementation of EN 3059:2007.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 its secr
4、etary.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 STANDARD
5、NORME EUROPENNEEUROPISCHE NORMEN 3059June 2007ICS 49.035English VersionAerospace series - Bearings, airframe rolling - Rigid single rowball bearings in steel with flanged alignment housing, cadmiumplated - Dimensions and loadsSrie arospatiale - Roulements pour structures daronefs- Roulements en acie
6、r, rigides, une range de billes, avecbague dalignement collerette cadmie - Dimensions etchargesLuft- und Raumfahrt - Flugwerklager - EinreihigeRillenkugellager aus Stahl mit selbsteinstellendem Flansch,verkadmet - Mae und BelastungenThis European Standard was approved by CEN on 16 March 2006.CEN mem
7、bers 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 nationalstandards may be obtained on applicatio
8、n 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 to the CEN Management Centre has the
9、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, Netherlands, Norway, Poland, Portugal,Ro
10、mania, 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 in any form and by any means reservedw
11、orldwide for CEN national Members.Ref. No. EN 3059:2007: 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 .10 EN 3059:20073 Foreword This docume
12、nt (EN 3059:2007) 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 National Associations and the Officia
13、l 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 national standards shall be withdrawn at
14、 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 CEN/CENELEC Internal Regulations, the n
15、ational 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, Luxembourg, Malta, Netherlands, Norwa
16、y, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 3059:20074 1 Scope This standard specifies the characteristics of rigid single row ball bearings in steel, with cadmium-plated flanged alignment housing designed to withstand only slow rotations a
17、nd 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 temperature range from 54 C to 150 C. However, being lubricated with the followi
18、ng 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 C to 177 C. Their field of application when lubricated with code letter
19、 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 latest edition of the referenced document (including any amendments) appl
20、ies. ISO 1132-1, Rolling bearings Tolerances Part 1: Terms and Definitions. EN 2031, Steel FE-PL31 Hardened and tempered Bars Aerospace series. 1)EN 2133, Aerospace series Cadmium plating of steels with specified tensile strength 1 450 MPa, copper, copper alloys and nickel alloys. EN 2221, Steel FE-
21、PL31 Hardened and tempered Hollow bars 3,5 mm a 55 mm Aerospace series. 1)EN 2222, Steel FE-PL31 Hardened and tempered Hand and die forgings Aerospace series. 1)EN 2249, Aerospace series Steel FE-PL52S Rm 690 MPa Bars De 250 mm. 2)EN 2424, Aerospace series Marking of aerospace products. EN 3727, Aer
22、ospace series Bearings, airframe rolling rigid with flanged alignment housing Technical specification. TR 4475, Aerospace series Bearings and mechanical transmissions for airframe applications Vocabulary. 3)1) Published as ASD Standard at the date of publication of this standard. 2) In preparation a
23、t the date of publication of this standard. 3) Published as ASDTechnical report at the date of publication of this standard. EN 3059:20075 3 Terms and definitions For the purposes of this document, the terms and definitions given in ISO 1132-1 and TR 4475 apply. 4 Symbols and abbreviations dmp= sing
24、le plane mean bore diameter deviation ds= deviation of a single bore diameter Cs= permissible static radial load Famax.= permissible static axial load Ga= axial internal clearance Gr= radial internal clearance Sia= assembled bearing inner ring face runout with raceway Sea= assembled bearing outer ri
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