BS EN 4034-2007 Aerospace series - Bearings airframe rolling - Double row self-aligning ball bearings with flanged outer ring in corrosion resisting steel reduced internal radial c.pdf

1、 g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58self-aligning ball bearings with flanged outer ring in corrosion resisting steel, reduced internal

2、radial clearance Dimensions and loadsThe European Standard EN 4034:2007 has the status of a British StandardICS 49.035Aerospace series Bearings, airframe rolling Double row BRITISH STANDARDBS EN 4034:2007BS EN 4034:2007This British Standard was published under the authority of the Standards Policy a

3、nd Strategy Committee on 31 July 2007 BSI 2007ISBN 978 0 580 56303 4Amendments issued since publicationAmd. No. Date CommentsCompliance with a British Standard cannot confer immunity from legal obligations.National forewordThis British Standard is the UK implementation of EN 4034:2007.The UK partici

4、pation in its preparation was entrusted to Technical Committee MCE/7, Rolling bearings.A list of organizations represented on this committee 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

5、its correct application.EUROPEAN STANDARDNORME EUROPENNEEUROPISCHE NORMEN 4034June 2007ICS 49.035English VersionAerospace series - Bearings, airframe rolling - Double row self-aligning ball bearings with flanged outer ring in corrosionresisting steel, reduced internal radial clearance - Dimensionsan

6、d loadsSrie arospatiale - Roulements pour structures daronefs- Roulements en acier rsistant la corrosion, sur deuxranges de billes, avec bague extrieure collerette, jeuradial rduit - Dimensions et chargesLuft- und Raumfahrt - Flugwerklager - Kugellager auskorrosionsbestndigem Stahl Zweireihige Pende

7、lkugellagermit Flanschauenring, reduzierte radiale Lagerluft - Maeund BelastungenThis European Standard was approved by CEN on 16 March 2006.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a natio

8、nal standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the CEN Management Centre or to any CEN member.This European Standard exists in three official versions (English, French, German). A version in any

9、 other language made by translationunder the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as theofficial versions.CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estoni

10、a, Finland,France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMIT EUROPEN DE NORMALISATIONEUROPISCHES

11、 KOMITEE FR NORMUNGManagement Centre: rue de Stassart, 36 B-1050 Brussels 2007 CEN All rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4034:2007: E2 Contents Page Foreword3 1 Scope 4 2 Normative references 4 3 Terms and definitions .4 4 Symb

12、ols and abbreviations 5 5 Required characteristics.5 6 Designation 7 7 Marking .7 8 Technical specification .8 EN 4034:20073 Foreword This document (EN 4034:2007) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes c

13、arried 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 national standard, eithe

14、r by publication of an identical text or by endorsement, at the latest by December 2007, and conflicting national standards shall be withdrawn at the latest by December 2007. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and

15、/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 organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republi

16、c, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 4034:20074 1 Scope This standard specifies the char

17、acteristics of self-aligning double row ball bearings with flanged outer ring in corrosion resisting steel, reduced internal clearance, designed to withstand only slow rotations and oscillations under load. They are intended for use between fixed and moving parts of the aircraft structure and their

18、control mechanisms. They are intended to be used in the temperature range: 54 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 (code

19、B), operational range 54 C to 177 C (see EN 3280), their field of application when lubricated with code A grease is limited to 121 C. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies

20、. 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 hardenable stainless steel parts. EN 2030, Steel FE-PM43 Hardened and tempered B

21、ars D 150 mm Aerospace series. 1)EN 2226, Steel FE-PM43 Hardened and tempered Hand and die forgings De 150 mm Aerospace series. 1)EN 2424, Aerospace series Marking of aerospace products. EN 3280, Aerospace series Bearings, airframe rolling, rigid or self-aligning Technical specification. 3 Terms and

22、 definitions For the purposes of this standard, the terms and definitions given in ISO 1132-1 apply. 1) Published as ASD Standard at the date of publication of this standard. EN 4034:20075 4 Symbols and abbreviations dmp= single plane mean bore diameter deviation Dmp= single plane mean outside diame

23、ter deviation Cs= permissible static radial load Famax.= permissible static axial load Kea= radial runout of assembled bearing outer ring Kia= radial runout of assembled bearing inner ring 5 Required characteristics 5.1 Dimensions Tolerances Masses Configuration : see Figure 1; the bearings are fitt

24、ed with either seals or shields. Values : see Figure 1 and Table 1: values after surface treatment. 5.2 Surface roughness Rolling elements and raceways: Ra= 0,2 m Bore, side faces and cylindrical outer surface: Ra= 0,8 m For code T, values prior to the surface treatment 5.3 Materials Inner ring : St

25、eel EN 2030 or EN 2226, 58 HRC Outer ring : Steel EN 2030 or EN 2226, 58 HRC Balls : Steel EN 2030, 58 HRC Shields : Corrosion resisting material Seals : Polytetrafluoroethylene (PTFE) or glass fabric reinforced polytetrafluoroethylene (PTFE) 5.4 Surface treatment Passivated ISO 8075: code T With no

26、 surface treatment: no code EN 4034:20076 Dimensions in millimetres Type with shields Code P Type with seals Code E Key 1 230 min. The acceptance value is the maximum value for the user. NOTE 1 The installation of seals and shields is at manufacturers option. NOTE 2 The seals shall not extend beyond

27、 “B“. Figure 1 Table 1 Dimensions in millimetres Diameter d B D d1d2d3E F Mass Code Nominal Tolerance m g/pieces dmpDmp0 0,12 min. 15 15 58 16 16 0 8 0 11 33 19,6 41 34 61 20 20 0 9 13 38 24,7 46 39 74 25 25 43 28,6 51 44 1 1,5 90 32 32 0 10 0 13 14 52 38 60 55 2 2 132 EN 4034:20077 5.5 Loads, start

28、ing torques and clearances See Table 2. Table 2 Permissible static loads kN Radial clearance m Radial runout tolerances max. m Starting torque a max. mN.m Swivelling torqueamax. N.m Axial load Radial load With shields With seals Diameter code Famax. CsKiaKea15 16 15,7 3 to 9 12 18 20 19 23 35 25 21,

29、6 5 to 10 30 42 32 5,3 27,5 10 to 18 26 43 40 55 0,1 aDefinition: see EN 3280. EN 3280 incorporates no test of swivelling torque. 6 Designation EXAMPLE EXAMPLE Description block BEARING Identity block EN4034A15PT Number of this standard Code letter for grease type (see Clause 1) Diameter code (see T

30、able 1) Code for shields or seals (see Figure 1) Surface treatment (see 5.4) NOTE If necessary, the code I9005 shall be placed between the description block and the identity block. 7 Marking EN 2424, style A Marking position and method are at manufacturers option. EN 4034:20078 8 Technical specifica

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