ISO 13416-1997 Aerospace - Airframe needle track roller yoke type single-row sealed - Metric series《航空航天 飞机结构用轭型单列密封的滚针滚道式滚子 米制系列》.pdf
《ISO 13416-1997 Aerospace - Airframe needle track roller yoke type single-row sealed - Metric series《航空航天 飞机结构用轭型单列密封的滚针滚道式滚子 米制系列》.pdf》由会员分享,可在线阅读,更多相关《ISO 13416-1997 Aerospace - Airframe needle track roller yoke type single-row sealed - Metric series《航空航天 飞机结构用轭型单列密封的滚针滚道式滚子 米制系列》.pdf(12页珍藏版)》请在麦多课文档分享上搜索。
1、A Referencenumbe r ISO13416:1997 (E) INTERNATIONAL STANDARD ISO 13416 Firstedition 19971215 AerospaceAirframeneedletrackroller, yoketype,singlerow,sealedMetric series AronautiqueetespaceGaletsdecameaiguillespourtrier, unerange,avecjoints,pourcelluledaronefSriemtriqueISO13416:1997(E) ISO1997 Allright
2、sreserved.Unlessotherwisespecified,nopartofthispublicationmaybereproducedorutilizedinanyformorbyan ymeans,electronic ormechanical,includingphotocopyingandmicrofilm,withoutpermissioninwritingfromthepublisher. InternationalOrganizationforStandardization Casepostale56 CH1211Genve20 Switzerland Internet
3、 centraliso.ch X.400 c=ch;a=400net;p=iso;o=isocs;s=central PrintedinSwitzerland ii Foreword ISO(theInternationalOrganizationforStandardization)isaworldwidefederationofnationalstandardsbodies (ISOmemberbodies).TheworkofpreparingInternationalStandardsisnormallycarriedoutthroughISOtechnical committees.
4、Eachmemberbodyinterestedinasubjectforwhichatechnicalcommitteehasbeenestablishedhas therighttoberepresentedonthatcommittee.Internationalorganizations,governmentalandnongovernmental,in liaisonwithISO,alsotakepartinthework.ISOcollaboratescloselywiththeInternationalElectrotechnical Commission(IEC)onallm
5、attersofelectrotechnicalstandardization. DraftInternationalStandardsadoptedbythetechnicalcommitteesarecirculatedtothememberbodiesforvoting. PublicationasanInternationalStandardrequiresapprovalbyatleast75%ofthememberbodiescastingavote. InternationalStandardISO13416waspreparedbyTechnicalCommitteeISO/T
6、C20, Aircraftandspacevehicles , SubcommitteeSC15, Airframebearings . AnnexAformsanintegralpartofthisInternationalStandard.INTERNATIONALSTANDARD ISO ISO13416:1997(E) 1 AerospaceAirframeneedletrackroller,yoketype,singlerow, sealedMetricseries 1Scope ThisInternationalStandardspecifiesthecharacteristics
7、,boundarydimensions,tolerances,internalclearancesand permissibleradialstaticloadsofmetricseries,singlerow,yoketypeneedletrackrollersusedinairframeapplications. TheairframeneedletrackrollerscoveredbythisInternationalStandardaredesignedtooperateinthetemperature range54Cto+121C. 2Normativereferences Th
8、efollowingstandardscontainprovisionswhich,throughreferenceinthistext,constituteprovisionsofthis InternationalStandard.Atthetimeofpublication,theeditionsindicatedwerevalid.Allstandardsaresubjecttorevision, andpartiestoagreementsbasedonthisInternationalStandardareencouragedtoinvestigatethepossibilityo
9、f applyingthemostrecenteditionsofthestandardsindicatedbelow.MembersofIECandISOmaintainregistersof currentlyvalidInternationalStandards. ISO68317: 1) , Heattreatedsteels,alloysteelsandfreecuttingsteelsPart17:Ballandrollerbearingsteels. ISO1132:1980, RollingbearingsTolerancesDefinitions. ISO2082:1986,
10、 MetalliccoatingsElectroplatedcoatingsofcadmiumonironorsteel. ISO28591: 2) , SamplingproceduresforinspectionbyattributesPart1:Samplingplansindexedbyacceptable qualitylevel(AQL)forlotbylotinspection. ISO4520:1981, Chromateconversioncoatingsonelectroplatedzincandcadmiumcoatings. ISO5593:1997, Rollingb
11、earingsVocabulary. ISO6158:1984, MetalliccoatingsElectroplatedcoatingsofchromiumforengineeringpurposes. ISO13411:1997,Aerospace Airframeneedleroller,cylindricalrollerandtrackrollerbearings Technical specification. AMS2417E:1993, Plating,zincnickelalloy. 3) 1) Tobepublished.(RevisionofISO68317:1976)
12、2) Tobepublished.(RevisionofISO28591:1989) 3) Availablefrom: SAEInternational 400CommonwealthDrive Warrendale,PA150960001 USAISO13416:1997(E) ISO 2 3Definitions ForthepurposesofthisInternationalStandard,thedefinitionsgiveninISO5593apply. 4Symbols 4.1ForthepurposesofthisInternationalStandard,thesymbo
13、lsgiveninISO1132apply.Thesymbols(exceptthose fortolerances)showninthefiguresandthevaluesgiveninthetablesdenotenominaldimensionsunlessspecified otherwise. 4.2 ThefollowingadditionalsymbolsforbearingscoveredbythisInternationalStandardalsoapply. B overallwidth(overfacesofendwashers) C s permissiblestat
14、icradialload d a clampingfacediameter R crownradiusofouterring 5Requiredcharacteristics 5.1DimensionsTolerancesInternalclearancesLoads Forvalues,seetable1.Forconfiguration,seefigure1. Table1 Dimensionsinmillimetres, toleranceandclearancevaluesinmicrometres Diameter dDBC Tolerancevalues r s r 1s Rd a
15、 Internal clearance C s Mass code +50 -96 D dmp D Bs D Dmp K ea max. min. min. min. min. Radial, G r max. Axial, G a max. kN kg 05 5 16 12 11 192 10 6,88 0,01 06 08 6 8 19 24 12 15 11 14 +24 -260 0,3 228 288 12 14 8,8 13,7 0,02 0,04 10 10 32 18 17 0,6 384 20 24,8 0,09 12 12 37 21 20 444 22 28,8 0,14
16、 15 15 42 24 22 0 -12 +24 -320 +50 -26 40 0,3 504 26 40 76 39,5 0,19 17 17 47 27 25 1 564 29 48,2 0,27 20 20 58 34 32 696 36 80,8 0,53 25 25 72 40 38 +24 -380 864 44 126 0,98 30 35 30 35 85 100 48 56 46 54 +24 -450 1,5 0,6 1020 1200 54 65 208 306 1,65 2,68 ISO ISO13416:1997(E) 3 Key 1 Lubricationgro
17、ove 2 Lubricationgrooveandholes Figure1 5.2Surfaceroughness Rollers: R a =0,2 mmmax. Innerringraceway: R a =0,4 mmmax. Outerringraceway: R a =1,0 mmmax. Endwashers: R a =1,6 mmmax.atrollercontactarea. 6Materials Rings: bearingsteelISO68317,type1,racewayhardness58HRCto66HRC(670HVto860HV). Rollers: be
18、aringsteelISO68317,type1,heattreatedto58HRCto66HRC(670HVto860HV). Endwashers: steelheattreatedto51HRCto60HRC(528HVto697HV)atrollercontactarea. Seals: acetalresin,nylonorequivalent. 7Surfacetreatment 7.1Bearingsmadeofconventionalrollingbearingsteel,shallhavetheexternalsurfacesoftheouterringchromium p
19、lated,andallotherexternalsurfaces,excepttheinnerringboresurface,shallbecadmiumorzincnickelplated.Black oxidecoatingisapermissiblealternateonallinnerringexternalsurfaces(seeannexA). 7.2Wherecadmiumplatingisspecified(codelettersDandM),itshallbeinaccordancewithISO2082.Thethickness oftheplatingshallnotb
20、elessthan7mandnotmorethan15m.ThebearingshallbeembrittlementrelievedwithinISO13416:1997(E) ISO 4 4hofplatingbyheattreatmentat140C10Cforaminimumof8hfollowedbychromatetreatmentinaccordance withISO4520(codeletterDonly). 7.3Wherechromiumplatingisspecified(codelettersD,MandZ),itshallbeinaccordancewithISO6
21、158.The thicknessoftheplatingshallbenotlessthan12m,8monfacesandringchamfers,andnotmorethan25m. 7.4Wherezincnickelplatingisspecified(codeletterZ)itshallbeinaccordancewithAMS2417E,type2.The thicknessoftheplatingshallnotbelessthan7mandnotmorethan15m. 8Lubrication Thebearingshallbeprelubricatedwitheithe
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- ISO134161997AEROSPACEAIRFRAMENEEDLETRACKROLLERYOKETYPESINGLEROWSEALEDMETRICSERIES 航空 航天飞机 结构 用轭型 单列 密封

链接地址:http://www.mydoc123.com/p-1250733.html