BS EN 3288-1994 Bearings airframe rolling - Double row self-aligning ball bearings in steel cadmium plated - Diameter series 2 Dimensions and loads《机体轴承 钢制的镀镉双列自调心球轴承 2号直径系列 尺寸和负荷》.pdf

1、BRITISH STANDARD AEROSPACE SERIES BS EN 3288:1994 Bearings, airframe rolling Doublerow self-aligning ball bearings in steel, cadmium plated Diameterseries2 Dimensions and loads The European Standard EN3288:1994 has the status of a BritishStandard UDC 629.7.02:681.822.7.004.1:681.828:669.14:669.738BS

2、EN3288:1994 This BritishStandard, having been prepared under the directionof the Aerospace Standards Policy Committee, waspublished under the authorityof the Standards Boardand comes into effect on 15August1994 BSI01-2000 The following BSI references relate to the work on this standard: Committee re

3、ference MCE/7 Draft for comment88/72196 DC ISBN 0 580 21890 2 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

4、Normungsinstitut Belgium Institut belge de normalisation Denmark Dansk Standardiseringsraad Finland Suomen Standardisoimisliito, r.y. France Association franaise de normalisation Germany Deutsches Institut fr Normung e.V. Greece Hellenic Organization for Standardization Iceland Technological Institu

5、te of Iceland Ireland National Standards Authority of 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 Espao

6、la de Normalizacin y Certificacin Sweden Standardiseringskommissionen i Sverige Switzerland Association suisse de normalisation United Kingdom BritishStandards Institution Amendments issued since publication Amd. No. Date CommentsBSEN3288:1994 BSI 01-2000 i Contents Page Cooperating organizations In

7、side front cover National foreword ii Foreword 2 1 Scope 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)

8、 Cross-references Inside back cover Figure 1 5 Table 1 5BSEN3288:1994 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 EN3288:1994 Aerospace series Bearings, airframe rolling

9、 Double row self-aligning ball bearings in steel, cadmium plated Diameter series2 Dimensions and loads, published by the European Committee for Standardization (CEN). EN3288 was produced as a result of international discussions in which the United Kingdom took an active part. A British Standard does

10、 not purport to include all the necessary provisions of a contract. Users 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 insid

11、e front cover, pagesi andii, theEN title page, pages2 to6, an inside back 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 EU

12、ROPISCHE NORM EN3288 May1994 UDC 629.7.02:681.822.7.004.1:681.828.669.14:669.738 Descriptors: Aircraft industry, airframe bearings, self-aligning bearings, ball bearings, steel, cadmium, dimensions, static loads English version Aerospace series Bearings, airframe rolling Doublerow self-aligning ball

13、 bearings in steel, cadmiumplated Diameter series2 Dimensionsandloads Srie arospatiale Roulements pour structures daronefs Roulements en acier, cadmis, rotule, sur deux ranges de billes Srie de diamtres2 Dimensions et charges Luft- und Raumfahrt Flugwerklager Zweireihige Pendelkugellager aus Stahl,

14、verkadmet Durchmesserreihe2 Mae und Belastungen This European Standard was approved by CEN on1994-05-19. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration

15、. 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 Standard exists in three official versions (English, French, German). A version in any other language made by translation

16、 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 standards bodies of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Net

17、herlands, Norway, Portugal, Spain, Sweden, Switzerland andUnited Kingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels 1994 Copyright reserved to CEN members Ref. No. EN3288:1994 EEN3

18、288:1994 2 BSI 01-2000 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries and votes carried out in accordance with the rules of this Association, this standard has successively received the approval of the National Associ

19、ations and the Official Services of the member countries of AECMA, prior to its presentation to CEN. This standard was submitted for formal vote, and the result was positive. This European Standard shall be given the status of a national standard, either by publication of an identical text or by end

20、orsement, at the latest by November1994, and conflicting national standards shall be withdrawn at the latest by November1994. According to the Internal Regulations of CEN/CENELEC, the following countries are bound to implement this European Standard: CEN members are the national standards bodies of

21、Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland, United Kingdom.EN3288:1994 BSI 01-2000 3 1 Scope This standard specifies the characteristics of double row self-aligning ball bearings in steel

22、 1) , cadmium plated, of diameter series 2)designed to withstand only slow rotations, oscillations and/or swivelling under load. They are intended for use between fixed and moving parts of the aircraft structure and their control mechanisms. The airframe rolling bearings defined in this standard are

23、 used from54 C to+150 C. However, being lubricated with the following greases: very high pressure grease, ester type (code A), operational range73 C to+121 C or very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range54 C to+177 C (see EN3280), their field of ap

24、plication 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 at the appropriate places in the text and the publications are listed he

25、reafter. 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 the publication referred to applies. ISO15, Rolling bearings Radial be

26、arings Boundary dimensions General plan. ISO1132, Rolling bearings Tolerances Definitions. EN2031, Steel FE-PL31 Hardened and tempered Bars Aerospace series 3) . EN2133, Cadmium plating of steels with maximum specified tensile strength equal to or less than1450MPa and copper and copper alloys Aerosp

27、ace series 3) . EN2221, Steel FE-PL31 Hardened and tempered Hollow bars3,5mmk ak 55mm Aerospaceseries 3) . EN2222, Steel FE-PL31 Hardened and tempered Hand and die forgings Aerospace series 3) . EN3280, Aerospace series Bearings, airframe rolling, rigid or self-aligning Technical specification. EN32

28、89, Aerospace series Bearings, airframe rolling Double row self-aligning ball bearings in corrosion resisting steel Diameter series2 Dimensions and loads. 3 Definition For the purposes of this standard, the following definition applies: bearing full complement of balls (without cage) 4 Symbols The d

29、efinitions of tolerances and clearances are given in ISO1132. 1) For new design, use preferably bearings in corrosion resisting steel, see EN3289 2) See ISO15 3) Published as AECMA Standard at the date of publication of this standard % dmp = single plane mean bore diameter deviation % Dmp = single p

30、lane 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 = radial internal clearance K ia = radial runout of assembled bearing inner ringEN3288:1994 4 BSI 01-2000 5 Required characteristics 5.1 Di

31、mensions Tolerances Clearances Loads Mass Configuration: see Figure 1; the bearings are fitted with either seals or shields. Values: see Table 1; the dimensions and tolerances apply after protection. 5.2 Surface roughness Raceways and rolling elements: R a =0,24m Bore, side faces and cylindrical out

32、er surface: R a =0,84m The values apply prior to cadmium plating. 5.3 Materials 5.4 Surface treatment EN2133 thickness,54m to124m, on the inner and outer rings, the bore and raceways are not cadmium plated. As soon as possible after plating, and within16h de-embrittlement heat treatment shall be car

33、ried out at a temperature and for a time (compatible with the performance requirements of the bearing) which shall be subject to written approval of the qualifying authorities. K ea = radial runout of assembled bearing outer ring F amax. = permissible static axial load C s = permissible static radia

34、l load P or = static equivalent radial load F a = bearing axial load, axial component of actual bearing load F r = bearing radial load, radial component of actual bearing load. Inner ring : EN2031 or EN2221 or EN2222,59 HRC to64 HRC Outer ring : EN2031 or EN2221 or EN2222,59 HRC to64 HRC Balls : EN2

35、031,59 HRC to64 HRC Shields : Corrosion resisting material Seals : Polytetrafluoroethylene (PTFE) or polytetrafluoroethylene (PTFE) reinforced with fibreglass.EN3288:1994 BSI 01-2000 5 Table 1 NOTEThe installation of seals and shields is at the manufacturers option. Figure 1 Dimensions in millimetre

36、s d B C D d1 min. F max. G max. Tolerances 4m r Mass kg/1000 parts Code Nominal a a % % dmp % % Dmp % % ds % % Ds 05 5 12 8 16 7,6 10 12 0,3 to 0,8 9 06 6 14 10 19 8,6 12 14,4 14 08 8 15 24 11,1 13 19,8 30 10 10 20 14 30 13,6 17 24 57 12 12 32 15,4 26,5 62 15 15 35 18,5 30 75 17 17 22 16 40 21,2 19

37、34 110 20 20 24 18 47 23,6 20 39,7 170 0 0,12 0 0,12 0 8 0 8 + 2 10 +2 10 0 9 +2 11 0 11 +3 11 +3 14 0 10 +3 13EN3288:1994 6 BSI 01-2000Table 1 6 Designation EXAMPLE: NOTEIf necessary, the codeI9005 shall be placed between the description block and the identity block. 7 Marking In addition to the ma

38、nufacturers 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 See EN3280. d Internal clearances 4m Runout tolerances radial max. 4m Starting torque binmN.m Permissib

39、le static loads c kN Axial max. G a Radial G r Code Special group Code R Normal group Code N Group 3 CodeL Special group Code R Normal group Code N Group3 Code L K ia K ea Code P Code E Axial F amax. Radial C s 05 70 100 2 to6 2 to13 10 to20 25 40 4 8 1,2 3,7 06 4,5 9 1,8 5,7 08 80 2 to7 5,5 10 2,8

40、9,1 10 120 7,5 12 4,4 14,1 12 3 to9 3 to18 13 to23 9 14 5 16,1 15 12 18 5,9 18,8 17 160 18 25 7,6 24,3 20 180 5 to 10 5 to20 15 to25 23 35 10,2 32,6 a Dimensions of the shields are at the manufacturers option within the limits of F and G. b Definition, see EN3280. c F r +3,2 F a = P or ; P orshall b

41、ek C s . For ultimate static loads, see EN3280.BSEN3288:1994 BSI 01-2000 National 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

42、 upon which the following bodies were represented: Ball and Roller Bearing Manufacturers 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 t

43、ext are as follows. International Standard Corresponding BritishStandard ISO15:1981 BS6267:1982 Specification for rolling bearings: boundary dimensions for radial bearings ISO76:1987 BS5645:1987 Specification for static load ratings for rolling bearings ISO1132:1980 BS6107 Rolling bearings: toleranc

44、es Part1:1981 Glossary of termsBS EN 3288:1994 BSI 389 Chiswick High Road London W4 4AL BSIBritishStandardsInstitution BSI is the independent national body responsible for preparing BritishStandards. It presents the UK view on standards in Europe and at the international level. It is incorporated by

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