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
《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》由会员分享,可在线阅读,更多相关《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(12页珍藏版)》请在麦多课文档分享上搜索。
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
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