BS ISO 9749-2001 Stud-ends in corrosion-resistant steel swaged on aircraft control wire rope - Dimensions and loads《航空器操纵钢丝绳上的锻制耐腐蚀钢螺柱端 尺寸规格及载荷》.pdf
《BS ISO 9749-2001 Stud-ends in corrosion-resistant steel swaged on aircraft control wire rope - Dimensions and loads《航空器操纵钢丝绳上的锻制耐腐蚀钢螺柱端 尺寸规格及载荷》.pdf》由会员分享,可在线阅读,更多相关《BS ISO 9749-2001 Stud-ends in corrosion-resistant steel swaged on aircraft control wire rope - Dimensions and loads《航空器操纵钢丝绳上的锻制耐腐蚀钢螺柱端 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 9
2、749:2000 ICS 49.035 NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAW Stud-ends, in corrosion-resistant steel, swaged on aircraft control wire rope Dimensions and loadsThis British Standard, having been prepared under the direction of the Engineering Sector Committee, was publis
3、hed under the authority of the Standards Committee and comes into effect on 15 March 2001 BSI 03-2001 ISBN 0 580 35044 4 BS ISO 9749:2000 Amendments issued since publication Amd. No. Date Comments National foreword This British Standard reproduces verbatim ISO 9749:2000 and implements it as the UK n
4、ational standard. The UK participation in its preparation was entrusted to Technical Committee ACE/14, Aerospace details and parts, which has the responsibility to: aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation,
5、or proposals for change, and keep the UK interests informed; monitor related international and European developments and promulgate them in the UK. A list of organizations represented on this committee can be obtained on request to its secretary. Cross-references The British Standards which implemen
6、t 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 include a
7、ll 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. Summary of pages This document comprises a front cover, an inside front cover, the ISO ti
8、tle page, pages ii and iii, a blank page, pages 1 to 5 and a back cover. The BSI copyright notice displayed in this document indicates when the document was last issued.A Referencenumbe r ISO9748:2000 (E) INTERNATIONAL STANDARD ISO 9749 Firstedition 20001215 AerospaceStudends,incorrosion resistantst
9、eel,swagedonaircraftcontrol wireropeDimensionsandloads AronautiqueetespaceEmboutstendeurs,enacierrsistantla corrosion,sertirsurcblesdecommandedaronefsDimensionset chargesISO9749:2000(E) iiISO9749:2000(E) iii Foreword ISO(theInternationalOrganizationforStandardization)isaworldwidefederationofnational
10、standardsbodies(ISO memberbodies).TheworkofpreparingInternationalStandardsisnormallycarriedoutthroughISOtechnical committees.Eachmemberbodyinterestedinasubjectforwhichatechnicalcommitteehasbeenestablishedhas therighttoberepresentedonthatcommittee.Internationalorganizations,governmentalandnongovernme
11、ntal,in liaisonwithISO,alsotakepartinthework.ISOcollaboratescloselywiththeInternationalElectrotechnical Commission(IEC)onallmattersofelectrotechnicalstandardization. InternationalStandardsaredraftedinaccordancewiththerulesgivenintheISO/IECDirectives,Part3. DraftInternationalStandardsadoptedbythetech
12、nicalcommitteesarecirculatedtothememberbodiesforvoting. PublicationasanInternationalStandardrequiresapprovalbyatleast75%ofthememberbodiescastingavote. InternationalStandardISO9749waspreparedbyTechnicalCommitteeISO/TC20, Aircraftandspacevehicles, SubcommitteeSC12, Mechanicalsystemparts . AnnexAformsa
13、normativepartofthisInternationalStandard.INTERNATIONALSTANDARD OISO9749:2000(E) 1 AerospaceStudends,incorrosionresistantsteel,swagedon aircraftcontrolwireropeDimensionsandloads 1Scope ThisInternationalStandardspecifiesthecharacteristicsofstudendsincorrosionresistantsteelswagedonaircraft controlwirer
14、ope. 2Normative references Thefollowingnormativedocumentscontainprovisionswhich,throughreferenceinthistext,constituteprovisionsofthis InternationalStandard.Fordatedreferences,subsequentamendmentsto,orrevisionsof,anyofthesepublicationsdo notapply.However,partiestoagreementsbasedonthisInternationalSta
15、ndardareencouragedtoinvestigatethe possibilityofapplyingthemostrecenteditionsofthenormativedocumentsindicatedbelow.Forundatedreferences, thelatesteditionofthenormativedocumentreferredtoapplies.MembersofISOandIECmaintainregistersof currentlyvalidInternationalStandards. ISO20201:1997, Aerospace Prefor
16、medflexiblesteelwireropeforaircraftcontrols Part 1:Dimensionsand loads. ISO8074:1985, AerospaceSurfacetreatmentofausteniticstainlesssteelparts. ISO9761:1999, Aerospace Loc kingc lips,inc orrosion resistants teel,for air craftc ontrolwir er opetur nbuckles Dimensions. ISO10955:1999, AerospaceEndfitti
17、ngsandturnbarrelsforaircraftcontrolwireropeTechnicalspecification . ISO13715:2000, TechnicaldrawingsEdgesofundefinedshapeVocabularyandindicationondrawings . EN2465 1) , AerospaceseriesSteelFEPA11SoftenedBars D e 100mm . 2) SAEAMS2431/6A, PeeningMedia,GlassShot. SAEAMS5639G, Steel,CorrosionResistant,
18、Bars,Wire,Forgings,Tubing,andRings,19Cr10Ni,SolutionHeat Treated. SAEAMS5641F, Steel,CorrosionResistant,Bars,Wire,andForgings,18.5Cr10Ni0.22SeFreeMachining; SwagingorUpsetting,SolutionHeatTreated. 3 Configuration,dimensions,loadsandmasses Configuration,dimensions,loadsandmassesshallbeinaccordancewit
19、hFigure1andTable1. Studendsshouldbemanufacturedfromahexagonalbar(type1);however,wherebarsofhexagonalcrosssectionare difficulttoobtain,theymaybeproducedfrommilledflats(type2). 1) Tobepublished. 2) AECMA.ISO9749:2000(E) 2 Dimensionsinmillimetres/Surfaceroughnessinmicrometres a Thread d Slotforlockingc
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