1、BRITISH STANDARD AEROSPACE SERIES BS EN 3283:1994 Bearings, airframe rolling Rigid single row ball bearings in corrosion resisting steel Diameter series8 and9 Dimensions and loads The European Standard EN3283:1994 has the status of a BritishStandard UDC 629.7.02:621.822.74.004.1:669.14.018.89BSEN328
2、3:1994 This BritishStandard, having been prepared under the directionof the Aerospace Standards Policy Committee, waspublished under the authorityof the Standards Boardand comes into effect on 15September1994 BSI01-2000 The following BSI references relate to the work on this standard: Committee refe
3、renceMCE/7 Draft for comment88/72196DC ISBN 0 580 21883 X 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 Norm
4、ungsinstitut Belgium Institut belge 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 Ir
5、eland 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 Espaola de Normalizac
6、in y Certificacin Sweden Standardiseringskommissionen i Sverige Switzerland Association suisse de normalisation UnitedKingdom BritishStandards Institution Amendments issued since publication Amd. No. Date CommentsBSEN3283:1994 BSI 01-2000 i Contents Page Cooperating organizations Inside front cover
7、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) Cross-references
8、 Inside back cover Figure 1 4 Table 1 5BSEN3283:1994 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 EN3283:1994 Aerospace series Bearings, airframe rolling Rigid single row
9、 ball bearings in corrosion resisting steel Diameter series8 and9 Dimensions and loads, published by the European Committee for Standardization (CEN). EN3283 was produced as a result of international discussions in which the United Kingdom took an active part. A British Standard does not purport to
10、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 inside front cover, p
11、agesi 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 EUROPISCHE NORM EN
12、 3283 June1994 UDC 629.7.02:621.822.74.004.1:669.14.018.89 Descriptors: Aircraft industry, airframe bearings, ball bearings, corrosion resisting steel, dimensions, static loads English version Aerospace series Bearings, airframe rolling Rigid single row ball bearings in corrosion resisting steel Dia
13、meter series8 and9 Dimensions and loads Srie arospatiale Roulements pour structures daronefs Roulements en acier rsistant la corrosion rigides, une range de billes Srie de diamtres8 et9 Dimensions et charges Luft- und Raumfahrt Flugwerklager Einreihige Rillenkugellager aus korrosionsbestndigem Stahl
14、 Durchmesserreihen8 und9 Mae und Belastungen This European Standard was approved by CEN on1994-06-07. 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. U
15、p-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 un
16、der 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, Nether
17、lands, Norway, Portugal, Spain, Sweden, Switzerland and UnitedKingdom. 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. EN 3283:1994EEN3283
18、: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 accordance with the rules of this Association, this standard has successively received the approval of the National Associati
19、ons 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 endors
20、ement, at the latest by December1994, and conflicting national standards shall be withdrawn at the latest by December1994. According to the CEN/CENELEC Internal Regulations, the following countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Gr
21、eece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland, UnitedKingdom.EN3283:1994 BSI 01-2000 3 1 Scope This standard specifies the characteristics of rigid single row ball bearings in corrosion resisting steel of diameter series8 and9 1)designed to with
22、stand only slow rotations and oscillations 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 used from54Cto+150 C. However, being lubricated with the following grease
23、s: 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 (seeEN3280), their field of application when lubricated with code A grease is limited to+121 C. 2 Normative
24、 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 hereafter. For dated references, subsequent amendments to or revisions of any o
25、f 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 bearings Boundary dimensions General plan. ISO1132, Rolling bearings Tolerances
26、 Definitions. EN2030, Steel FE-PM43 Hardened and tempered Bars Dk 150mm Aerospace series 2) . EN2226, Steel FE-PM43 Hardened and tempered Hand and die forgings D e k 150mm Aerospace series 2) . EN3280, Aerospace series Bearings, airframe rolling, rigid or self-aligning Technical specification. 3 Def
27、inition For the purposes of this standard, the following definition applies: bearing full complement of balls (without cage), with filling slot 4 Symbols The definitions of tolerances and clearances are given in ISO1132. 1) SeeISO15 2) Published as AECMA Standard at the date of publication of this s
28、tandard % dmp = single plane mean bore diameter deviation % Dmp = single plane mean outside diameter deviation G a = axial internal clearance G r = radial internal clearance S ia = assembled bearing inner ring face runout with raceway S ea = assembled bearing outer ring face runout with raceway K ia
29、 = radial runout of assembled bearing inner ring K ea = radial runout of assembled bearing outer ring F a max. = permissible static axial load C s = permissible static radial load.EN3283:1994 4 BSI 01-2000 5 Required characteristics 5.1 Dimensions Tolerances Clearances Loads Mass Configuration: seeF
30、igure 1; the bearings are fitted with either seals or shields. Values: seeTable 1. 5.2 Surface roughness Raceways and rolling elements: R a =0,24m Bore, side faces and cylindrical outer surface: R a =0,84m. 5.3 Materials Inner ring : EN2030 or EN2226, U 58HRC Outer ring : EN2030 or EN2226, U 58HRC B
31、alls : EN2030, U 58HRC Shields : Corrosion resisting material Seals : Polytetrafluoroethylene (PTFE) or polytetrafluoroethylene (PTFE) reinforced with fibreglass. NOTE 1The installation of seals and shields is at the manufacturers option. NOTE 2The shields shall not extend beyond B . Figure 1 EN3283
32、:1994 BSI 01-2000 5 Table 1 Table 1 Dimensions in millimetres d B D d1 min. Tolerances 4m r Mass kg/1000 parts Code Nominal % dmp % Dmp 10 10 6 22 13 0,3 to 0,8 11 12 12 24 15 13 15 15 7 28 17,6 16 17 17 30 19,6 18 20 20 32 23 20 25 25 37 28,1 23 30 30 42 33,1 26 35 35 47 38,3 30 40 40 52 43,3 38 50
33、 50 65 53 55 60 60 10 78 63,5 100 d Code Internal clearances 4m Runout tolerances max.4m Starting torque a in mN.m Permissible static loads b kN Axial max. Radial Axial Radial Code Code Axial Radial G a G r S ia S ea K ia K ea P E F amax. C s 10 100 2 to13 40 40 25 40 4,5 12 4,8 10,6 12 3 to18 5 13
34、5,6 12,3 15 5,5 14 7,4 16,2 17 6 15 8 17,6 20 5 to20 6,5 16 7,9 17,3 25 8,5 18 9,8 21,5 30 14 20 11,1 24,5 35 6 to20 18 23 12,9 28,4 40 22 29 14,5 31,8 50 120 6 to23 32 47 19,6 43,1 60 150 8 to28 55 77 31,8 70 a Definition, see EN3280. b Axial and radial loads may be applied simultaneously. For ulti
35、mate static loads, seeEN3280. 0 0,12 0 8 0 9 0 10 0 11 0 12 0 13 0 15EN3283:1994 6 BSI 01-2000 6 Designation EXAMPLE: NOTEIf necessary, the codeI9005 shall be placed between the description block and the identity block. 7 Marking In addition to the manufacturers own marking, each bearing shall be ma
36、rked, on one side face only, using the identity block, see6. Marking position and method are at the manufacturers option. 8 Technical specification SeeEN3280.BSEN3283:1994 BSI 01-2000 National annex NA (informative) Committees responsible The United Kingdom participation in the preparation of this E
37、uropean Standard was entrusted by the Aerospace Standards Policy Committee (ACE/-) to Technical CommitteeMCE/7 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 (inform
38、ative) Cross-references The BritishStandards corresponding to the International Standards referred to in the text are as follows. International Standard Corresponding BritishStandard ISO15:1981 BS6267:1982 Specification for rolling bearings: boundary dimensions for radial bearings ISO1132:1980 BS610
39、7 Rolling bearings: tolerances Part1:1981 Glossary of termsBS EN 3283:1994 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
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