EN 2335-2005 en Aerospace series - Bearings spherical plain in corrosion resisting steel without assembly slot - Dimensions and loads《航空航天系列 无装配槽的耐腐蚀钢制普通球面轴承 尺寸和载荷》.pdf

1、BRITISH STANDARDBS EN 2335:2005Aerospace series Bearings, spherical plain in corrosion resisting steel without assembly slot Dimensions and loadsThe European Standard EN 2335:2005 has the status of a British StandardICS 49.035g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53

2、g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 2335:2005This British Standard was published under the authority of the Standards Policy and Strategy Committee on 29 December 2006 BSI 2006ISBN 0 580 49854 9National f

3、orewordThis British Standard was published by BSI. It is the UK implementation of EN 2335:2005. It supersedes BS EN 2335:1990 which is withdrawn.The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems.A list of organizations repr

4、esented on ACE/12 can be obtained on request to its 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

5、since publicationAmd. No. Date CommentsEUROPEAN STANDARDNORME EUROPENNEEUROPISCHE NORMEN 2335December 2005ICS 49.035 Supersedes EN 2335:1988 English VersionAerospace series - Bearings, spherical plain in corrosionresisting steel without assembly slot - Dimensions and loadsSrie arospatiale - Rotules

6、lisses en acier rsistant lacorrosion sans encoche dassemblage - Dimensions etchargesLuft- und Raumfahrt - Gelenklager auskorrosionsbestndigem Stahl ohne Einfhrnut - Mae undBelastungenThis European Standard was approved by CEN on 26 October 2005.CEN members are bound to comply with the CEN/CENELEC In

7、ternal 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 application to the Central Secretariat or to any CEN membe

8、r.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 Central Secretariat has the same status as the officialversions.CEN members are

9、the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia,Slovenia, Spain, Sweden, Switzerland and United Kingdo

10、m.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMIT EUROPEN DE NORMALISATIONEUROPISCHES KOMITEE FR NORMUNGManagement Centre: rue de Stassart, 36 B-1050 Brussels 2005 CEN All rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 2335:2005: E2 Contents Pa

11、ge Foreword 3 1 Scope .4 2 Normative references .4 3 Terms and definitions.4 4 Symbols and abbreviations5 5 Required characteristics 5 6 Designation .9 7 Marking 9 8 Technical specification.9 EN 2335:20053 Foreword This European Standard (EN 2335:2005) has been prepared by the European Association o

12、f Aerospace Manufacturers - Standardization (AECMA-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 Official Services of the member countries of AECMA, prior to its presentation

13、 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 June 2006, and conflicting national standards shall be withdrawn at the latest by June 2006. Attention is drawn to the possibility that som

14、e 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. This European Standard supersedes EN 2335:1988. According to the CEN/CENELEC Internal Regulations, the national standards organizati

15、ons of the following countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Sloveni

16、a, Spain, Sweden, Switzerland and the United Kingdom. EN 2335:20054 1 Scope This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, without assembly slot, with or without swaging groove, with or without lubrication holes and grooves, intended for use in

17、fixed or moving parts of aircraft structure and control mechanisms. They may be used in the temperature range from 54 C to 150 C. However, as they are lubricated with the following greases (see EN 2337): ester type very high pressure grease (code letter A), operating range from 73 C to 121 C or, syn

18、thetic hydrocarbon 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 grease code letter A is limited to 121 C. 2 Normative references The following referenced documents are indispensable for the applica

19、tion of this document. For dated references, only the edition cited applies. For undated references, the latest 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 harde

20、nable stainless steel parts. EN 2030, Steel FE-PM43 Hardened and tempered Bars D 150 mm Aerospace series. 1)EN 2337, Aerospace series Spherical plain bearings Technical specification. EN 2424, Aerospace series Marking of aerospace products. EN 2491, Aerospace series Molybdenum disulphide dry lubrica

21、nts Coating methods. 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.2)EN 3490, Aerospace series Steel FE-PM3901 (X15CrNi17-3) Air melted Hardened and tempered Bar for machining De 200 mm 900 MPa Rm 1 100 MPa

22、. 2)3 Terms and definitions For the purposes of this standard, the terms and definitions given in ISO 1132-1 apply. 1) Published as AECMA Standard at the date of publication of this standard 2) Published as AECMA Prestandard at the date of publication of this standard EN 2335:20055 4 Symbols and abb

23、reviations The following symbols for tolerances are used: dmp: single plane mean bore diameter deviation ds: deviation of a single bore diameter Dmp: single plane mean outside diameter deviation Ds: deviation of a single outside diameter : angle of tilt of the outer ring with respect to the inner ri

24、ng, the spherical surface of the outer ring being completely in contact with the inner ring 5 Required characteristics 5.1 Configuration, dimensions and masses According to Figures 1, 2 and 3 and Table 1. The dimensions are expressed in millimetres and apply after surface treatment. 5.2 Surface roug

25、hness According to Figures 1 and 2. The values are expressed in micrometres and apply before surface treatment. aFor the inner ring bFor the outer ring Figure 1 Bearing without swaging grooves, code letter S EN 2335:20056 aFor the inner ring bFor the outer ring Figure 2 Bearing with swaging grooves,

26、 code letter R Code letter E: Bearing without lubrication holesand groove Code letter F: Bearing with lubrication holes oninner ring and: a lubrication groove on the boreof the inner ring a distribution groove on sphericalsurface of the inner or outer ringCode letter G: Bearing with lubrication hole

27、s on the outer ring and: a lubrication groove on the outer surface of outer ring a distribution groove on spherical surface of the inner or outer ringKey 1 Three holes d3at 120 NOTE The configuration with or without lubrication hole and lubrication groove applies to bearings either code letter R or

28、code letter S. Figure 3 1EN 2335:20057 Table 1 d B C D Tolerances m d1d2d3d4k l1l2r1r2r3 Massg Code Nom. 0 0,06 0,1 dmpdsDmpDsmin.+ 0,10 0,2 0,2 0 0,2max. + 0,10 min.d 04 4 5 3 12 6 8 16 3 05 5 06 6 6 4 14 8 10 0,4 to 0,7 13 5 08 8 8 5 16 80 135+10 130,3 to 0,6 15 8 10 10 9 6 19 102+13 c 16 c 0,5 to

29、 0,8 c 12 12 12 12 10 7 22 15 20,2b 18 0,5 11 17 15 24,20,715 a15 12 9 26 90 156+18 24 1,5 22 0,90,6 to 1 8 32 17 28,2 0,717 a17 14 10 30 80113+20 28 2,825 0,910 49 20 33,2 0,720 a20 16 12 35 24 33 2 2,9 29 0,29 65 25 39,40,925 a25 20 16 42 29 38,836 1,47 115 30 44,4 0,930 a30 22 18 47 100133+110 19

30、8+34 43,841 0,8 0,5 to 0,8 160 35 35 25 20 55 39 51,8 47 0,9 to 1,3 6 230 40 40 28 22 62 45 58,8 53 315 45 45 32 25 68 50 64,8 60 0,6 to 1 7 460 50 50 35 28 75 120153+130 2310+55 71,82,5 4 66 560 60 60 44 36 90 150194+150 2813+66 86,8 3 4,5 80 1,41 1,2 to 1,7 1,4 to 1,8 0,36 1 100aCode number 1 to b

31、e added to the end of identity block. bWithout lubrication holes and groove. cWithout swaging groove. dMaximum values for the user. 5.3 Clearances and loads See Table 2. EN 2335:20058 Table 2 Internal clearances m Permissible static loads kN axial radial max. d Code number normal code letter N reduc

32、ed code letter P normal code letter N normal code letter P radial Csaxial aCa04 7,2 0,45 05 12,6 0,8 06 16 1 08 21 1,8 10 31 2,512 40,5 3,5 15 35 to 75 5 to 35 20 10 70 5,317 91,4 6,7 20 40 to 80 5 to 40 25 12 130 9,8 25 216,7 18 30 277,5 25 35 359,9 31 40 50 to 100 5 to 50 30 15 428,8 38 45 558,4 5

33、0 50 760,1 64 60 60 to 120 5 to 60 35 20 1056 104,00 aThese values apply to bearings without swaging groove. For bearings with swaging grooves, the push-out loads may be smaller than these values. 5.4 Materials Inner ring: according to EN 2030, 55 HRC to 62 HRC Outer ring: according to EN 3490 or EN

34、 3161, 28 HRC to 37 HRC before swaging 5.5 Surface treatment 5.5.1 Outer ring Dry-film lubricant on the spherical surface (antiscoring treatment) applied according to EN 2491. 5.5.2 Inner ring Passivation according to ISO 8075: code letter T Without surface treatment (passivation): without code lett

35、er EN 2335:20059 6 Designation EXAMPLE Description block PLAIN BEARING Identity block EN2335AP15ERT1 Number of this standard Grease code letter (see Clause 1) Internal clearances (see Table 2) Diameter code number d (see Table 1) Lubrication holes and grooves code letter (see Figure 3) Swaging groov

36、es code letter (see Figures 1 and 2) Surface treatment code letter (see 5.5) Dimensional varieties code number for swaging grooves (see Table 1) NOTE If necessary, the code 9005 shall be placed between the description block and the identity block. 7 Marking EN 2424, style A The marking position is a

37、t the manufacturers option. 8 Technical specification See EN 2337 EN 2335:2005BS EN 2335:2005BSI389 Chiswick High RoadLondonW4 4ALBSI British Standards InstitutionBSI is the independent national body responsible for preparing British Standards. It presents the UK view on standards in Europe and at t

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