1、BRITISH STANDARD AEROSPACE SERIESBS EN 4036:2006Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance Dimensions and loadsThe European Standard EN 4036:2006 has the status of a British StandardICS 49.035g49g
2、50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 4036:2006This British Standard was published under the authority of the Standards Policy and Strat
3、egy Committee on 30 June 2006 BSI 2006ISBN 0 580 48555 2National forewordThis British Standard is the official English language version of EN 4036:2006. The UK participation in its preparation was entrusted to Technical Committee ACE/12, Aerospace fasteners and fastening systems, which has the respo
4、nsibility to:A list of organizations represented on this committee can be obtained on request to its secretary.Cross-referencesThe British Standards which implement international or European publications referred to in this document may be found in the BSI Catalogue under the section entitled “Inter
5、national Standards Correspondence Index”, or by using the “Search” facility of the BSI Electronic Catalogue or of British Standards Online.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with a Brit
6、ish Standard does not of itself confer immunity from legal obligations. aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep UK interests informed; monitor related international and Eu
7、ropean developments and promulgate them in the UK.Summary of pagesThis document comprises a front cover, an inside front cover, the EN title page, pages 2 to 9 and a back cover.The BSI copyright notice displayed in this document indicates when the document was last issued.Amendments issued since pub
8、licationAmd. No. Date CommentsEUROPEAN STANDARDNORME EUROPENNEEUROPISCHE NORMEN 4036May 2006ICS 49.035English VersionAerospace series Rod ends, adjustable with self-aligningdouble row ball bearing and threaded shank in corrosionresisting steel, reduced internal radial clearance Dimensionsand loadsSr
9、ie arospatiale Embouts rglables rotule sur deuxranges de billes et tige filete en acier rsistant lacorrosion, jeu radial rduit Dimensions et chargesLuft- und Raumfahrt Einstellbare senkpfe mitzweireihigem Pendelkugellager und Gewindeschaft auskorrosionsbestndigem Stahl, reduzierte radiale Lagerluft
10、Mae und 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 national standard without any alteration. Up-to-date lists and bibl
11、iographical references concerning such nationalstandards 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 translationunder the responsibility of a
12、 CEN member into its own language and notified to the Central Secretariat has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia
13、, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania,Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMIT EUROPEN DE NORMALISATIONEUROPISCHES KOMITEE FR NORMUNGManagement Centre: rue de Stassart, 36 B-1050 Brussels 20
14、06 CEN All rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4036:2006: E2 Contents Page Foreword 3 1 Scope .4 2 Normative references .4 3 Terms and definitions.5 4 Symbols and abbreviations5 5 Required characteristics 5 6 Designation .9 7 Mar
15、king 9 8 Technical specification.9 EN 4036:20063 Foreword This European Standard (EN 4036:2006) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standa
16、rd has received the approval of the National Associations and the Official Services of the member countries of AECMA, prior to its presentation 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
17、 by November 2006, and conflicting national standards shall be withdrawn at the latest by November 2006. Attention is drawn to the possibility that some 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 s
18、uch 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, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland
19、, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 4036:20064 1 Scope This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing wi
20、th reduced internal radial clearance and threaded shank in corrosion resisting steel, designed to withstand only slow rotations and oscillations under load. They consist of: a rod end comprising: circumferential groove to identify location; either seals or shields; an optional longitudinal groove fo
21、r locking purpose; an inner ring with balls. These rod ends are intended for use with flight control rods or rods for aerospace structures. 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 typ
22、e (code A), operational range 73 C to 121 C or very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range 54 C to 177 C (see EN 2067), their field of application when lubricated with code A grease is limited to 121 C. 2 Normative references The following reference
23、d documents are indispensable for the application 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. I
24、SO 3353-1, Aerospace Lead and runout threads Part 1: Rolled external threads. ISO 5855-2, Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts. ISO 8074, Aerospace Surface treatment of austenitic stainless steel parts. ISO 8075, Aerospace Surface treatment of hardenable stainless steel p
25、arts. EN 2030, Steel FE-PM43 Hardened and tempered Bars D 150 mm Aerospace series. 1) EN 2067, Aerospace series Rod ends with self-aligning ball bearings Technical specification.1) Published as AECMA Standard at the date of publication of this standard. EN 4036:20065 EN 2136 2), Steel FE-PM42 900 MP
26、a Rm 1100 MPa Bars De 100 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 3490, Aerospace series Steel FE-PM3901 (X15CrNi17-3) Air melted Hardened and tempered Bar for
27、machining De 200 mm 900 MPa Rm 1 100 MPa. 3) TR 3775, Aerospace series Bolts and pins Materials. 4) 3 Terms and definitions For the purposes of this standard, the terms and definitions given in ISO 1132-1 apply. 4 Symbols and abbreviations ds= deviation of a single bore diameter dmp= single plane me
28、an bore diameter deviation Cs= permissible static radial load Famax.= permissible static axial load 5 Required characteristics 5.1 Dimensions Tolerances Masses Configuration : see Figure 1; the bearings are fitted with either seals or shields. Values : see Figure 1 and Table 1: values after surface
29、treatment. 5.2 Surfaces roughness Rolling elements and raceway: Ra= 0,2 m Bore, side faces and cylindrical outer surface: Ra= 0,8 m For code T values prior to the surface treatment 2) Inactive for new design, see EN 3490. 3) Published as AECMA Prestandard at the date of publication of this standard.
30、 4) Published as AECMA Technical Report at the date of publication of this standard. EN 4036:20066 5.3 Materials Rod ends : steel EN 2136 or TR 3775; heat treated to obtain: by case hardening, hardening and tempering a surface hardness of 58 HRC on the raceway; by hardening and tempering to a streng
31、th of Rm 830 MPa on the whole rod end. Bearing : Inner ring : Steel EN 2030 or EN 2226, 58 HRC Balls : Steel EN 2030 or EN 2226, 58 HRC Seals : Polytetrafluoroethylene (PTFE) or glass fabric reinforced polytetrafluoroethylene (PTFE) Shields : Corrosion resisting material 5.4 Surface treatment Rod en
32、d : passivation ISO 8074 Bearing : passivation ISO 8075: code T with no surface treatment: no code 5.5 Thread MJ thread to ISO 5855-2, rolled Right hand thread, code R Left hand thread, code L EN 4036:20067 3,2 0,8 0,8 Break sharp edges and corners and remove all burrs and slivers A-A Longitudinal g
33、roove Type 1 Code K Type 2 Code M Type with shields Code P Type with seals Code E X (3:1) Break sharp corner Type 3 without groove Code N Key 1 6 min. The acceptance value is the maximum value for the user. 2 Conform to ISO 3353-1. 3 Thread Figure 1 EN 4036:20068 NOTE 1 The circumferential groove an
34、d the longitudinal groove over the distance F shall be painted red. NOTE 2 The installation of seals and shields is at the manufacturers option. Table 1 Dimensions in millimetres Diameter d B C D d1F bCode Nominal Tolerance m dmpds0 0,12 + 0,10 + 0,20 min. Thread amin. 05 5 12 8,5 20,5 7,6 MJ 8 1,00
35、-4h6h 18 06 6 14 22,5 8,6 MJ 10 1,25-4h6h 23 08 8 15 10 28,5 11,1 MJ 12 1,25-4h6h 27 10 10 0 8 0 10 20 14 32,0 13,6 MJ 14 1,50-4h6h 31 (continued)(concluded) Code G c H L M N r1r2r3S W Mass g/piece min. + 0,5 0 0,5 + 0,10 0 0,1 0,5 0,2 REF 05 33 33 48 1,6 6,6 6 35 06 37 37 54 8,0 1,4 60 08 42 42 62
36、2,4 10,2 7 85 10 48 48 73 3,2 12,2 0,3 to0,86,50,1 to0,52,0 10 130 aSee ISO 5855-2. bF = minimum length of engaged thread: included thickness of lock washer and height of nut. cG = minimum length of useful thread. 5.6 Loads, starting torques and clearances See Table 2. EN 4036:20069 Table 2 Permissi
37、ble static loads kN Starting torque b max. mN.m Swivelling torque bmax. N.m Clearance b m Diameter code Radial load Cs a Axial load Famax.aWith seals With shieldsRadial Axial max. 05 4,70 1,47 6,5 4,3 06 6,75 2,11 7 4,6 0,15 08 8,90 2,78 16 10,6 10 14,00 4,38 19 12,5 0,2 1 to 5 80 aDefinition and te
38、sting for ultimate static loads as per EN 2067, Annex E. bDefinition and testing as per EN 2067. 6 Designation EXAMPLE Description block ROD END Identity block EN4036L05PKAT Number of this standard Code letter for thread (see 5.5) Diameter code (see Table 1) Code letter for shields or seals (see Fig
39、ure 1) Code for longitudinal groove type (see Figure 1) Code letter for grease type (see 1) Surface treatment (see 5.4) NOTE If necessary, the originator 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 man
40、ufacturers option. 8 Technical specification See EN 2067. EN 4036:2006BS EN 4036:2006BSI389 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 the inter
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