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本文(EN 4265-2013 en Aerospace series - Bearing spherical plain metal to metal in corrosion resisting steel - Wide series - Dimensions and loads - Inch series《航空航天系列 轴承球平原 金属对金属的耐腐蚀钢-宽系.pdf)为本站会员(arrownail386)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

EN 4265-2013 en Aerospace series - Bearing spherical plain metal to metal in corrosion resisting steel - Wide series - Dimensions and loads - Inch series《航空航天系列 轴承球平原 金属对金属的耐腐蚀钢-宽系.pdf

1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS EN 4265:2013Aerospace series Bearing spherical plain, metal to metal in corrosion resisting steel Wide series Dimensions and loads Inch seriesBS EN 4265:2013 BRITISH STANDARDN

2、ational forewordThis British Standard is the UK implementation of EN 4265:2013. The UK participation in its preparation was entrusted to TechnicalCommittee ACE/12, Aerospace fasteners and fastening systems. A list of organizations represented on this committee can be obtained on request to its secre

3、tary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. The British Standards Institution 2013. Published by BSI Standards Limited 2013.ISBN 978 0 580 73964 4 ICS 49.035 Compliance with a British Standard cannot

4、 confer immunity from legal obligations.This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 January 2013.Amendments issued since publicationDate T e x t a f f e c t e dBS EN 4265:2013EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4265 Ja

5、nuary 2013 ICS 49.035 English Version Aerospace series - Bearing spherical plain, metal to metal in corrosion resisting steel - Wide series - Dimensions and loads - Inch series Srie arospatiale - Rotules lisses, mtal mtal en acier rsistant la corrosion - Srie large - Dimensions et charges - Sries en

6、 inches Luft- und Raumfahrt - Gelenklager, Metall auf Metall aus korrosionsbestndigem Stahl - Breite Reihe - Mae und Belastungen - Inch-Reihe This European Standard was approved by CEN on 10 March 2011. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the con

7、ditions 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 CEN-CENELEC Management Centre or to any CEN member. This European Standard exis

8、ts 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 CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national sta

9、ndards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, S

10、lovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2013 CEN All rights of exploitation in any form and by any means reserved worldwid

11、e for CEN national Members. Ref. No. EN 4265:2013: EBS EN 4265:2013EN 4265:2013 (E) 2 Contents Page Foreword 31 Scope 42 Normative references 43 Terms and definitions .54 Symbols and abbreviations 55 Requirements .55.1 Configuration, dimensions, tolerances and mass .55.2 Surface roughness 55.3 Mater

12、ial .55.4 Surface treatment 55.5 Loads and clearances .56 Designation . 147 Marking 148 Technical specification 14BS EN 4265:2013EN 4265:2013 (E) 3 Foreword This document (EN 4265:2013) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). Afte

13、r 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 ASD, prior to its presentation to CEN. This European Standard shall be given the status of a n

14、ational standard, either by publication of an identical text or by endorsement, at the latest by July 2013, and conflicting national standards shall be withdrawn at the latest by July 2013. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent

15、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 national standards organisations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croati

16、a, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the

17、 United Kingdom. BS EN 4265:2013EN 4265:2013 (E) 4 1 Scope This European Standard specifies the characteristics of spherical plain bearings, metal to metal, in corrosion resisting steel, passivated, wide series, inch series for aerospace applications. They are intended for use in fixed or moving par

18、ts of the aircraft structure and their control mechanisms. They shall be used in the temperature range 54 C to 150 C. As they are lubricated by means of the following greases: Code A: Grease as per MIL-PRF-23827C, operating temperature range 73 C to 121 C. Code B: Grease as per MIL-PRF-81322G, opera

19、ting temperature range 54 C to 177 C. The range of application for bearings lubricated with grease per code A is limited to 121 C. In both cases the spherical surface of the outer or inner ring have to be provided with a dry-film lubricant as per MIL-PRF-46010G or equivalent (anti-seizing protection

20、). The slide hole treatment either at the outer ring or inner ring. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references

21、, the latest edition of the referenced document (including any amendments) applies. EN 2030, Aerospace series - Steel FE-PM3501 (X105CrMo17) - Hardened and tempered - Bars D 150 mm1)EN 2337, Aerospace series Spherical plain bearings Technical specification EN 2424, Aerospace series Marking of aerosp

22、ace products 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 ISO 1132-1, Rolling bearings Tolerances Part 1: Terms and definitions ISO 8075, Aerospace Surface treatment of hardenable stainless steel parts TR

23、4475, Aerospace series Bearings and mechanical transmissions for airframe applications Vocabulary 1)MIL-PRF-23827C, Grease Aircraft and instrument Gear and actuator screw NATO code number G-354 2)MIL-PRF-46010G, Lubricant Solid film Heat cured Corrosion inhibiting 2)MIL-PRF-81322G, Grease Aircraft G

24、eneral purpose Wide temperature range NATO code number G-395 2)1) Published as ASD-STAN Technical Report at the date of publication of this standard, (www.asd-stan.org). 2) Published by: Department of Defense (DoD), http:/www.defenselink.mil/ BS EN 4265:2013EN 4265:2013 (E) 5 3 Terms and definitions

25、 For the purposes of this document, the terms and definitions given in TR 4475 apply. 4 Symbols and abbreviations Symbols of limit deviations are in accordance with definitions of ISO 1132-1. is the maximum angle of tilt of the outer ring with respect to the inner ring, with the spherical surface of

26、 the outer ring being completely in contact with the inner ring; Ca is the permissible static axial load; Cs is the permissible static radial load; dmp is the single plane mean bore diameter deviation; Dmp is the single plane mean outside diameter deviation; ds is the deviation of a single bore diam

27、eter; Ds is the deviation of a single outside diameter. Definitions and vocabulary according to TR 4475. 5 Requirements 5.1 Configuration, dimensions, tolerances and mass According to Figures 1 and 2 and Table 1. Dimensions and tolerances are expressed in millimetres (inches). Values apply after to

28、surface treatment. 5.2 Surface roughness In accordance with Figures 1 and 2. Values in micrometres (micro inches), apply prior to surface treatment. 5.3 Material Inner ring: According to EN 2030, hardness 55 HRC 62. Outer ring: According to EN 3161, hardness 28 HRC 38 before swaging. 5.4 Surface tre

29、atment Surface treatment according to ISO 8075 for inner ring before swaging. 5.5 Loads and clearances According to Tables 2 and 3. BS EN 4265:2013EN 4265:2013 (E) 6 aSet back bFor the inner ring cFor the outer ring Figure 1 Code S Without swaging grooves BS EN 4265:2013EN 4265:2013 (E) 7 aSet back

30、bFor the inner ring cFor the outer ring Figure 2 Code R With swaging grooves BS EN 4265:2013EN 4265:2013 (E) 8 Figure 3 Grease hole code “E” Without grease hole and lubricating groove aThree holes e distributed over the circumference at distance of 120 Figure 4 Grease hole code “F” With grease hole

31、on inner ring and lubricating groove on: Bore of inner ring Spherical surface of the outer ring The hole should allow the passage of the grease BS EN 4265:2013EN 4265:2013 (E) 9 aThree holes e distributed over the circumference at distance of 120 Figure 5 Grease hole code “G” With grease hole on out

32、er ring and lubricating groove on: Outer surface of outer ring Spherical surface of the outer ring The hole should allow the passage of the grease BS EN 4265:2013EN 4265:2013 (E) 10 Table 1 Dimensions, tolerances and mass (1 of 2) Dimensions in millimetres (in inches) Diameter code aDiameter B C d1d

33、2d3d D Limit deviation 0 0,05 + 0,13 0 0 0,20 dmp ds Dmp Ds 0.0020+00.005min. 0.008003 c 4,826 (0.190 0) 15,875 (0.625 0) 0,0130 50.00000,0130 50.00000.0080 30.00000,0130 50.000011,10 (0.437) 8,31 (0.327) 7,62 (0.300) 13,5 (0.53) 14,30 (0.563) 04 c 6,350 (0.250 0) 05c 7,938 (0.312 5) 19,5 (0.687 5)

34、8,05 (0.317) 9,14 (0.360) 14,4 (0.57) 15,88 (0.625) 06c 9,525 (0.375 0) 20,638 (0.812 5) 0,0090 40.000012,70 (0.500) 10,31 (0.405) 11,84 (0.466) 17,4 (0.69) 18,08 (0.712) 07 11,113 (0.437 5) 23,813 (0.937 5) 14,27 (0.562) 11,23 (0.442) 13,64 (0.537) 19,7 (0.78) 21,26 (0.837) 07A 23,017 (0.906 2) 20,

35、52 (0.808) 08 12,700 (0.500 0) 25,400 (1.000 0) 15,88 (0.625) 12,83 (0.505) 15,42 (0.607) 22,1 (0.87) 22,86 (0.900) 09 14,288 (0.562 5) 28,575 (1.125 0) 17,45 (0.687) 13,61 (0.536) 18,31 (0.721) 25,4 (1.00) 26,04 (1.025) 10 15,875 (0.625 0) 30,163 (1.187 5) 19,05 (0.750) 14,40 (0.567) 18,97 (0.747)

36、26,9 (1.06) 27,61 (1.087) 12 19,050 (0.750 0) 34,925 (1.375 0) 0,0110 40.000022,23 (0.875) 16,00 (0.630) 21,46 (0.845) 31,0 (1.22) 31,78 (1.251) 14 22,225 (0.875 0) 41,275 (1.625 0) 19,18 (0.755) 25,27 (0.995) 33,7 (1.33) 38,13 (1.501) 16 25,400 (1.000 0) 53,975 (2.125 0) 0,0150,003+60.00010.0000,01

37、30 50.00000,0150,003+60.00010.00034,93 (1.375) 25,53 (1.005) 32,23 (1.269) 47,5 (1.87) 50,83 (2.001) 20 31,750 (1.250 0) 60,325 (2.375 0) 38,10 (1.500) 28,70 (1.130) 37,13 (1.462) 53,2 (2.09) 57,18 (2.251) 24 38,100 (1.500 0) 68,263 (2.687 5) 42,85 (1.687) 31,06 (1.223) 43,10 (1.697) 60,8 (2.39) 65,

38、10 (2.563) 28 44,450 (1.750 0) 76,200 (3.00) 46,02 (1.812) 33,45 (1.317) 49,91 (1.965) 67,9 (2.67) 73,05 (2.876) 32 50,800 (2.000 0) 82,550 (3.250 0) 49,20 (1.937) 35,05 (1.380) 56,10 (2.209) 74,6 (2.94) 79,35 (3.124) BS EN 4265:2013EN 4265:2013 (E) 11 Table 1 (2 of 2) Dimensions in millimetres (in

39、inches) Diameter code a P efr1r2 r3 b U t Mass 0 0,25 0,20 0,20 0 0,25 degree degree g/piece 0.0100( 0.008) ( 0.008) 0.0100min. 0,5 max. 03c 0,64 (0.025) 0,64 (0.025) 0,13 to 0,38 00.015to00.0050,127 to 0,254 00.010to00.00516,0 20 0,08 (0.003) 0,5 (0.02) 13 04c12 05c15,5 30 13 06c0,89 (0.035) 0,254

40、to 0,432 00.017to00.0109,5 0,12 (0.005) 0,8 (0.03) 23 07 1,50 (0.059) 2,80 (0.110) 0,76 (0.030) 11,0 33 07A 30 08 0,76 (0.030) 9,5 40 09 10,5 56 10 2,00 (0.079) 12,0 63 12 1,40 (0.055) 1,02 (0.040) 14,0 1,2 (0.05) 92 14 2,50 (0.098) 4,00 (0.157) 6,0 146 16 14,5 392 20 12,5 499 24 14,0 668 28 13,0 85

41、9 32 1 005 aThe diameter code corresponds to bore diameter d in 1/16 inch. bThe acceptance value is the maximum value for the user. cNot available with lubrification code F or code G. BS EN 4265:2013EN 4265:2013 (E) 12 Table 2 Loads Diameter code a Permissible static load kN Ultimate static load kN

42、Radial b c CsAxial b d e CaRadial b Axial b d Code E Code F/G Code E Code F/G Code E Code F/G Code E Code F/G 03f10,7 g 19,3 16,1 g 29,0 04f24,5 g 36,7 g 05f47,8 g 18,0 71,6 g 26,9 06f72,1 g 27,4 108,2 g 41,1 07 100,8 71,5 33,5 30,7 151,1 107,2 50,3 46,0 07A08 131,7 99,0 45,6 42,7 197,6 148,3 68,3 6

43、4,1 09 161,0 123,5 52,1 49,3 241,5 185,2 78,2 73,9 10 182,4 142,5 59,2 56,4 273,6 213,7 88,8 84,5 12 222,7 176,8 66,8 64,0 334,1 265,3 100,2 96,0 14 299,3 228,0 101,7 96,0 449,0 342,0 152,6 143,9 16 497,4 g 481,9 193,3 187,5 746,1 g 722,8 289,9 281,3 20 741,6 628,8 249,9 244,1 1 112,3 943,2 374,8 36

44、6,2 24 923,2 794,3 296,8 291,0 1 384,8 1 191,5 445,1 436,5 28 1 117,2 973,3 348,3 342,5 1 675,8 1 460,0 522,5 513,8 32 1 291,2 1 133,0 385,1 379,4 1 936,8 1 699,6 577,7 569,0 aThe diameter code corresponds to bore diameter d in 1/16 inch. bDefinition and testing for permissible and ultimate static l

45、oads according to EN 2337 and TR 4475. cPermissible surface pressure 530 MPa, definition per TR 4475. dThese values apply to loose spherical bearings. For installed bearings, the push-out loads may be smaller than these values. ePermissible surface pressure 460 MPa, definition per TR 4475. fNot avai

46、lable with lubrification code F or code G. gLimit by bolt bending. Definition: solid shaft; rigid clamping on both sides; uniform load; permissible bending stress 1 350 MPa; permissible shear stress 1 200 MPa. BS EN 4265:2013EN 4265:2013 (E) 13 Table 3 Clearance Dimensions in millimetres (in inches)

47、 Diameter code aClearance bRadial AxialNormal Code N Reduced Code P Normal Code N max. Reduced Code P max. 03 0,010 to 0,030 (0.000 4 to 0.001 2) 0,002 to 0,010 (0.0001 to 0.0004) 0,12 (0.005) 0,035 (0.001 4) 04 05 06 07 07A 08 0,010 to 0,050 (0.000 4 to 0.002 0) 0,229 (0.009 0) 09 0,003 to 0,012 (0

48、.000 1 to 0.000 5) 0,040 (0.001 6) 10 12 0,004 to 0,015 (0.000 15 to 0.000 6)0,050 (0.002 0) 14 16 20 24 28 32 0,005 to 0,020 (0.000 2 to 0.000 8) 0,060 (0.002 4) aThe diameter code corresponds to nominal diameter d in 1/16 inch. bDefinition and testing for clearance according to EN 2337. BS EN 4265:2013EN 4265:2013 (E) 14 6 Designation EXAMPLE Description blockBEARING Identity blockEN4265BP16ER Number of this standard Grease code (see Clause 1) Clearance code (see Table 3) Diameter code (see Table 1) Grease hole code (see F

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