BS EN 3053-1994 Bearings airframe rolling - Single row self-aligning roller bearings in steel - Dimensions and loads《机体轴承 钢制的单列自调心滚子轴承 尺寸和负载》.pdf

1、BRITISH STANDARD AEROSPACE SERIES BS EN 3053:1994 Bearings, airframe rolling Single row self-aligning roller bearings in steel Dimensions and loads The European Standard EN3053:1994 has the status of a BritishStandard UDC629.7.02:621.822.8.004.1:621.828:669.14BSEN3053:1994 This BritishStandard, havi

2、ng been prepared under the directionof the Aerospace Standards Policy Committee, waspublished under the authorityof the Standards Boardand comes into effect on 15July1994 BSI01-2000 The following BSI references relate to the work on this standard: Committee reference MCE/7 Draft for comment88/72195

3、DC ISBN 0 580 22409 0 Cooperating organizations The European Committee for Standardization (CEN), under whose supervision this European Standard was prepared, comprises the national standards organizations of the following countries: Austria Oesterreichisches Normungsinstitut Belgium Institut belge

4、de normalisation Denmark Dansk Standard Finland Suomen Standardisoimisliito, r.y. France 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 o

5、f Ireland Italy Ente Nazionale Italiano di Unificazione Luxembourg Inspection du Travail et des Mines Netherlands Nederlands Normalisatie-instituut Norway Norges Standardiseringsforbund Portugal Instituto Portugus da Qualidade Spain Asociacin Espaola de Normalizacin y Certificacin Sweden Standardise

6、ringskommissionen i Sverige Switzerland Association suisse de normalisation United Kingdom BritishStandards Institution Amendments issued since publication Amd. No. Date CommentsBSEN3053:1994 BSI 01-2000 i Contents Page Cooperating organizations Inside front cover National foreword ii Foreword 2 1 S

7、cope 3 2 Normative references 3 3 Definition 3 4 Symbols 3 5 Required characteristics 4 6 Designation 6 7 Marking 6 8 Technical specification 6 National annex NA (informative) Committees responsible Inside back cover National annex NB (informative) Cross-references Inside back cover Figure 1 4 Table

8、 1 5BSEN3053:1994 ii BSI 01-2000 National foreword This BritishStandard has been prepared under the direction of the Aerospace Standards Policy Committee and is the English language version of EN3053:1994, Aerospace series Bearings, airframe rolling Single row self-aligning roller bearings in steel

9、Dimensions and loads, published by the European Committee for Standardization (CEN). EN3053 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 of Briti

10、sh 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, theEN title page, pages2 to6, an inside back cover an

11、d 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 EN 3053 April 1994 UDC 629.7.02:621.822.8.004.1:621.828:669.14 Descr

12、iptors: Aircraft industry, airframe bearings, self-aligning bearings, roller bearings, steel, dimensions, static loads English version Aerospace series Bearings, airframe rolling Singlerowself-aligning roller bearings in steel Dimensions and loads Srie arospatiale Roulements pour structures daronefs

13、 Roulements en acier, rotule, sur une range de rouleaux Dimensions et charges Luft- und Raumfahrt Flugwerklager Einreihige Tonnenlager aus Stahl Mae und Belastungen This European Standard was approved by CEN on1994-04-27. CEN members are bound to comply with the CEN/CENELEC International Regulations

14、 which 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 Central Secretariat or to any CEN member. This European

15、 Standard 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 the Central Secretariat has the same status as the official versions. CEN members are the national

16、 standards bodies of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and UnitedKingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung

17、 Central Secretariat: rue de Stassart 36, B-1050 Brussels CEN 1994 Copyright reserved to CEN members Ref.No.EN3053:1994EEN3053:1994 BSI 01-2000 2 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries and votes carried out in

18、 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 toCEN. This standard was submitted for Formal Vote, and the result was positive. Thi

19、s 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 October1994, and conflicting national standards shall be withdrawn at the latest by October1994. According to the CEN/CENELEC Internal Regulations, the

20、 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, Switzerland, UnitedKingdom.EN3053:1994 BSI 01-2000 3 1 Scope This standard specifies the

21、 characteristics of single row self-aligning roller bearings in steel 1)designed to withstand only slow rotations, oscillations and/or swivelling under load. They are intended for use in bell crank lever ends or at the end of rigid flight control rods for transmission purposes, before or after servo

22、 operation. The airframe rolling bearings defined in this standard are used from54 C to+150 C. However, being lubricated with the following greases: very high pressure grease, ester type (code A), operational range 73 C to+121 C or very high pressure grease, synthetic hydrocarbons, general purpose (

23、code B), operational range54 C to+177 C (seeEN3280), their field of application when lubricated with code A grease is limited to+121 C. 2 Normative references This European Standard incorporates by dated or undated reference, provisions from other publications. These normative references are cited a

24、t the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of

25、 the publication referred to applies. ISO1132, Rolling bearings Tolerances Definitions. EN2031, Steel FE-PL31 Hardened and tempered Bars Aerospace series 2) . EN2221, SteelFE-PL31 Hardened and tempered Hollow bars3,5mmk ak 55mm Aerospace series 2) . EN2222, SteelFE-PL31 Hardened and tempered Hand an

26、d die forgings Aerospace series 2) . EN3055, Aerospace series Bearings, airframe rolling Single row self-aligning roller bearings in corrosion resisting steel Dimensions and loads. EN3280, Aerospace series Bearings, airframe rolling, rigid or self-aligning Technical specification. 3 Definition For t

27、he purposes of this standard, the following definition applies: shielded bearing full complement of rollers (without cage) EN3280 4 Symbols The definitions of tolerances and clearances are given in ISO1132. 1) For new design, use preferably bearings in corrosion resisting steel, seeEN3055. 2) Publis

28、hed as AECMA Standard at the date of publication of this standard. % dmp = single plane mean bore diameter deviation % Dmp = single plane mean outside diameter deviation % ds = deviation of a single bore diameter % Ds = deviation of a single outside diameter G a = axial internal clearance G r = radi

29、al internal clearance K ia = radial runout of assembled bearing inner ring K ea = radial runout of assembled bearing outer ring F amax. = permissible static axial load C s = permissible static radial load P or = static equivalent radial load F a = bearing axial load, axial component of actual bearin

30、g load F r = bearing radial load, radial component of actual bearing load.EN3053:1994 4 BSI 01-2000 5 Required characteristics 5.1 Dimensions Tolerances Clearances Loads Mass Configuration: seeFigure 1; the bearings are fitted with shields (code P). Values: seeTable 1. 5.2 Surface roughness Raceways

31、 and rolling elements: R a =0,24m Bore, side faces and cylindrical outer surface: R a =0,84m. 5.3 Materials Inner ring : EN2031 or EN2221 or EN2222, 59HRC to64HRC Outer ring : EN2031 or EN2221 or EN2222, 59HRC to64HRC Rollers : EN2031, 59HRC to64HRC Shields : Corrosion resisting material. NOTEThe in

32、stallation of shields is at the manufacturers option. Figure 1 EN3053:1994 BSI 01-2000 5 Table 1 Table 1 Dimensions in millimetres d B C D d1 min. F max. b G max. b Tolerances 4m r Mass Kg/1000 parts Code Nominal % dmp % Dmp % ds % Ds 06 6 12 8 24 11,9 10 20,5 0,3 to 0,8 21 08 8 15 10 26 12,3 13 22

33、37 08 a 8 30 14,3 12 25 49 10 10 16 12 35 16,9 13 29 70 10 a 10 20 17 72 12 12 13 40 19,9 33,5 108 15 15 24 14 47 23,9 20 40 153 17 17 15 25,9 41 163 d Code Internal clearances 4m Radial runout tolerances max.4m Starting torque cin mN.m Permissible static loads dkN Axial max. G a Radial G r K ia K e

34、a Axial F amax. Radial C s 06 180 2 to6 25 40 6 4,8 15,9 08 210 2 to7 8 6,9 22,8 08 a 12 8,4 27,8 10 16 10 32,9 10 a 12 20 13,6 45 15 3 to9 25 16,4 54,2 17 30 21 69,4 a In the designation add code1 to the end of the identity block. b Dimensions of the shields are at the manufacturers option within t

35、he limits of F and G. c Definition,seeEN3280. d F r +3,3F a = P or ; P orshall bek C s . For ultimate static loads, seeEN3280. 0 0,12 0 0,12 0 8 0 9 +2 10 +2 11 0 11 +3 14 +3 11EN3053:1994 6 BSI 01-2000 6 Designation EXAMPLE: NOTEIf necessary, the codeI9005 shall be placed between the description bl

36、ock and the identity block. 7 Marking In addition to the manufacturers own marking, each bearing shall be marked, on one side face only, using the identity block, see6. Marking position and method are at the manufacturers option. 8 Technical specification SeeEN3280.BSEN3053:1994 BSI 01-2000 National

37、 annex NA (informative) Committees responsible The United Kingdom participation in the preparation of this European Standard was entrusted by the Aerospace Standards Policy Committee (ACE/-) to Technical Committee MCE/7 upon which the following bodies were represented: Ball and Roller Bearing Manufa

38、cturers Association Ministry of Defence Society of British Aerospace Companies Ltd. National annex NB (informative) Cross-references The BritishStandards corresponding to the International Standards referred to in the text are as follows. International Standard Corresponding BritishStandard ISO76:19

39、87 BS5645:1987 Specification for static load ratings for rolling bearings ISO1132:1980 BS6107 Rolling bearings: tolerances Part1:1981 Glossary of termsBS EN 3053:1994 BSI 389 Chiswick High Road London W4 4AL BSIBritishStandardsInstitution BSI is the independent national body responsible for preparin

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