BS ISO 9736-2001 Eye-ends in corrosion-resistant steel threaded for aircraft control wire rope - Dimensions and loads《航空器操纵钢丝绳用耐腐蚀钢制螺纹式有眼端 尺寸规格及载荷》.pdf

1、BRITISH STANDARD AEROSPACE SERIES BS ISO 9736:2000 Eye-ends, in corrosion-resistant steel, threaded, for aircraft control wire rope Dimensions and loads ICS 49.035 NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBS ISO 9736:2000 This British Standard, having been prepared under

2、 the direction of the Engineering Sector Committee, was published under the authority of the Standards Committee and comes into effect on 15 March 2001 BSI 01-2001 ISBN 0 580 54046 0 National foreword This British Standard reproduces verbatim ISO 9736:2000 and implements it as the UK national standa

3、rd. The UK participation in its preparation was entrusted to Technical Committee ACE/14, Aerospace details and parts, which has the responsibility to: A list of organizations represented on this committee can be obtained on request to its secretary. Cross-references The British Standards which imple

4、ment international publications referred to in this document may be found in the BSI Standards Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Find” facility of the BSI Standards Electronic Catalogue. A British Standard does not purport to includ

5、e 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. aid enquirers to understand the text; present to the responsible international/Europea

6、n committee any enquiries on the interpretation, or proposals for change, and keep the UK interests informed; monitor related international and European developments and promulgate them in the UK. Summary of pages This document comprises a front cover, an inside front cover, the ISO title page, page

7、s ii and iii, a blank page, pages 1 to 5, and a back cover. The BSI copyright date displayed in this document indicates when the document was last issued. Amendments issued since publication Amd. No. Date CommentsA Referencenumbe r ISO9736:2000 (E) INTERNATIONAL STANDARD ISO 9736 Firstedition 200012

8、15 AerospaceEyeends,insteel,threaded, foraircraftcontrolwireropeDimensions andloads AronautiqueetespaceEmboutsil,enacier,filets,pourcblesde commandedaronefsDimensionsetchargesISO9736:2000(E) iiISO9736:2000(E) iii Foreword ISO(theInternationalOrganizationforStandardization)isaworldwidefederationofnat

9、ionalstandardsbodies(ISO memberbodies).TheworkofpreparingInternationalStandardsisnormallycarriedoutthroughISOtechnical committees.Eachmemberbodyinterestedinasubjectforwhichatechnicalcommitteehasbeenestablishedhas therighttoberepresentedonthatcommittee.Internationalorganizations,governmentalandnongov

10、ernmental,in liaisonwithISO,alsotakepartinthework.ISOcollaboratescloselywiththeInternationalElectrotechnical Commission(IEC)onallmattersofelectrotechnicalstandardization. InternationalStandardsaredraftedinaccordancewiththerulesgivenintheISO/IECDirectives,Part3. DraftInternationalStandardsadoptedbyth

11、etechnicalcommitteesarecirculatedtothememberbodiesforvoting. PublicationasanInternationalStandardrequiresapprovalbyatleast75%ofthememberbodiescastingavote. InternationalStandardISO9736waspreparedbyTechnicalCommitteeISO/TC20, Aircraftandspacevehicles, SubcommitteeSC12, Mechanicalsystemparts . AnnexAf

12、ormsanormativepartofthisInternationalStandard.INTERNATIONALSTANDARD OISO9736:2000(E) 1 AerospaceEyeends,insteel,threaded,foraircraftcontrolwire ropeDimensionsandloads 1Scope ThisInternationalStandardspecifiesthecharacteristicsofeyeends,ineitherlowalloysteelorcorrosionresistant steel,intendedforthetu

13、rnbarrelsofaircraftcontrolwirerope. 2Normative references Thefollowingnormativedocumentscontainprovisionswhich,throughreferenceinthistext,constituteprovisionsofthis InternationalStandard.Fordatedreferences,subsequentamendmentsto,orrevisionsof,anyofthesepublicationsdo notapply.However,partiestoagreem

14、entsbasedonthisInternationalStandardareencouragedtoinvestigatethe possibilityofapplyingthemostrecenteditionsofthenormativedocumentsindicatedbelow.Forundatedreferences, thelatesteditionofthenormativedocumentreferredtoapplies.MembersofISOandIECmaintainregistersof currentlyvalidInternationalStandards.

15、ISO20201:1997, Aerospace Preformedflexiblesteelwireropeforaircraftcontrols Part 1:Dimensionsand loads. ISO58552:1999, AerospaceMJthreadsPart2:Limitdimensionsforboltsandnuts. ISO8074:1985, AerospaceSurfacetreatmentofausteniticstainlesssteelparts. ISO9761:1999, Aerospace Loc kingc lips,inc orrosion re

16、sistants teel,for air craftc ontrolwir er opetur nbuckles Dimensions. ISO10955:1999, AerospaceEndfittingsandturnbarrelsforaircraftcontrolwireropeTechnicalspecification . ISO13715:2000, TechnicaldrawingsEdgesofundefinedshapeVocabularyandindicationondrawings. EN2133:1997, Aerospaces eries Cadmiumplati

17、ngofs teelswiths pecifiedtens iles trength 1450MPa, copper, copperalloysandnickelalloys. EN2207: 1) ,AerospaceseriesSteelFEPL43S900MPa R m 1100MPa Handanddieforging D e 40mm . 2) EN3487: 1) ,AerospaceseriesSteelF EPA3601Softened500MPa R m 700MPa Barsfor machining D e 100mm . 2) SAEAMS2431/6A, Peenin

18、gMedia,GlassShot . SAEAMS5643P, Steel,CorrosionResistant,Bars,Wire,Forgings,TubingsandRings ,16Cr4.0Ni0.30(Cb+Ta) 4.0CuSolutionHeatTreated,PrecipitationHardenable . SAEAMS6370K, SteelBars,Forgings,andRings0.95Cr0.20Mo(0.280.33C) . QQP416F, Plating,Cadmium(Electrodeposited) . 3) 1) Tobepublished. 2)

19、AECMA 3) MaybeobtainedfromDODSSPCustomerService,DefensePrintingServiceDetachmentOffice,Building4D,700Robbions Ave.,Philadelphia,PA191115094,USA.ISO9736:2000(E) 2 3 Configuration,dimensions,loadsandmasses Configuration,dimensions,loadsandmassesshallbeinaccordancewithFigure1andTable1. Dimensionsinmill

20、imetres Surfaceroughnessinmicrometres a Pitchdiameter b Thread c Slotforlockingclip d Marking e Notchforthreadonleftonly Figure1ISO9736:2000(E) 3 Table1 Dimensionsinmillimetres Thread a Mass Minimum Nominal D 1 b D 2 D 3 EH L 1 L 2 L 3 L 4 L 5 PRT breaking diameterof Code Designation Code load c wir

21、erope c - + 025 06 , , H8 nom. lim. dev. h11 0 025 + , 0,5 0,5 0,5 0,5 0,5 min. max. 0 1 + g/piece kN 04 MJ4 0,74h6h 10 2,9 -01 0 , 2,5 S 37 11 15 8 24,5 3,26 3,36 0,04 3,9 2,15 1,6 05 MJ5 0,84h6h 12 3,8 3 S 50 10 30,5 4,18 4,33 3 0,05 8,1 4,45 2,4 5 L 63 15,5 23 43,5 9,3 06 MJ6 14h6h 14 4,6 5 1 S 5

22、5 12 35 5,1 5,27 0,08 15,4 8,9 3,2 L 71 51 5 17,5 07 MJ7 14h6h 17 6 5,6 -015 0 , 6 S 62 17,5 25 14 39,5 6,09 6,27 25,4 12,45 4 L 80 57,5 28,9 08 MJ8 14h6h 20 8 6,6 6,5 S 70 18,5 28 16 44,5 7,1 7,27 6 0,1 36,6 18,6 4,8 10 MJ10 1,254h6h 23 7,8 7,5 1,5 S 84 20 31 20 56,5 8,93 9,11 8 59,4 24,9 5,6 12 MJ

23、12 1,254h6h 25 10 9,8 8 S 88 23,5 35 24 57 10,91 11,11 85,7 31,2 6,4 a InaccordancewithISO58552. b Afaultintheshapeofthesphericalsurfaceofradius D 1 /2ispermittedwithinthelimitsofthelimitdeviationvaluefor D 1 . c InaccordancewithISO20201. 4Material CodeA:corrosionresistantsteel(inaccordancewithannex

24、A). CodeB:lowalloysteel(inaccordancewithannexA). 5Surface treatment Corrosionresistantsteel:passivation(codeP)inaccordancewithISO8074orpeening(codeG)(inaccordance withannexA). Lowalloy:cadmiumplatinginaccordancewithannexA. 6Designation EacheyeendinaccordancewiththisInternationalStandardshallbedesign

25、atedasshowninthefollowingexample. EXAMPLEISO9736:2000(E) 4 Wherethefollowingcodesareappliedforthethreaddirection: codeR:righthandthread; codeL:lefthandthread. 7Marking ThemarkingpositionshallbeinaccordancewithFigure1. Inadditiontothemanufacturersownmarking,eacheyeendinaccordancewiththisInternational

26、Standardshallbe markedusingtheidentityblockspecifiedinclause6. Themarkingmethodisatthemanufacturersoption. 8Technical specification InaccordancewithISO10955.ISO9736:2000(E) 5 AnnexA (normative) Correspondencebetweennationalstandards Thisannexestablishesacorrespondencebetweendifferentmaterialsandsurf

27、acetreatmentstandardsfromcertain usercountries.Othermemberbodiesareinvitedtodeclaretheirmaterialsandsurfacetreatmentstandardsinthis annex. ThematerialsandprocessescitedinTables A.1andA.2areconsideredtobeequivalent,assumingthatthe requirementsforeyeendsspecifiedinthisInternationalStandardarerespected

28、. TableA.1Europeanstandards Code Material Surfacetreatment Family Standard Nature Standard A Corrosionresistantsteel EN3487 Passivation ISO8074 Peening SAEAMS2431/6A B Lowalloysteel EN2207 Cadmiumplating EN2133 TableA.2U.S.standards Code Material Surfacetreatment Family Standard Nature Standard A Co

29、rrosionresistantsteel SAEAMS5643 Passivation ISO8074 Peening SAEAMS 2431/6A B Lowalloysteel SAEAMS6370 Cadmiumplating QQP416 TypeII,Class2BS ISO 9736:2000 BSI 389 Chiswick High Road London W4 4AL BSI British Standards Institution BSI is the independent national body responsible for preparing British

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