欢迎来到麦多课文档分享! | 帮助中心 海量文档,免费浏览,给你所需,享你所想!
麦多课文档分享
全部分类
  • 标准规范>
  • 教学课件>
  • 考试资料>
  • 办公文档>
  • 学术论文>
  • 行业资料>
  • 易语言源码>
  • ImageVerifierCode 换一换
    首页 麦多课文档分享 > 资源分类 > PDF文档下载
    分享到微信 分享到微博 分享到QQ空间

    ISO 13415-1997 Aerospace - Airframe needle track roller stud type single-row sealed - Inch series《航空航天 飞机结构用柱型单列密封的滚针滚道式滚子 英制系列》.pdf

    • 资源ID:1250732       资源大小:511KB        全文页数:18页
    • 资源格式: PDF        下载积分:10000积分
    快捷下载 游客一键下载
    账号登录下载
    微信登录下载
    二维码
    微信扫一扫登录
    下载资源需要10000积分(如需开发票,请勿充值!)
    邮箱/手机:
    温馨提示:
    如需开发票,请勿充值!快捷下载时,用户名和密码都是您填写的邮箱或者手机号,方便查询和重复下载(系统自动生成)。
    如需开发票,请勿充值!如填写123,账号就是123,密码也是123。
    支付方式: 支付宝扫码支付    微信扫码支付   
    验证码:   换一换

    加入VIP,交流精品资源
     
    账号:
    密码:
    验证码:   换一换
      忘记密码?
        
    友情提示
    2、PDF文件下载后,可能会被浏览器默认打开,此种情况可以点击浏览器菜单,保存网页到桌面,就可以正常下载了。
    3、本站不支持迅雷下载,请使用电脑自带的IE浏览器,或者360浏览器、谷歌浏览器下载即可。
    4、本站资源下载后的文档和图纸-无水印,预览文档经过压缩,下载后原文更清晰。
    5、试题试卷类文档,如果标题没有明确说明有答案则都视为没有答案,请知晓。

    ISO 13415-1997 Aerospace - Airframe needle track roller stud type single-row sealed - Inch series《航空航天 飞机结构用柱型单列密封的滚针滚道式滚子 英制系列》.pdf

    1、A Referencenumbe r ISO13415:1997 (E) INTERNATIONAL STANDARD ISO 13415 Firstedition 19971215 AerospaceAirframeneedletrackroller, studtype,singlerow,sealedInchseries AronautiqueetespaceGaletsdecameaiguilles,suraxe,une range,avecjoints,pourcelluledaronefSrieinchISO13415:1997(E) ISO1997 Allrightsreserve

    2、d.Unlessotherwisespecified,nopartofthispublicationmaybereproducedorutilizedinanyformorbyan ymeans,electronic ormechanical,includingphotocopyingandmicrofilm,withoutpermissioninwritingfromthepublisher. InternationalOrganizationforStandardization Casepostale56 CH1211Genve20 Switzerland Internet central

    3、iso.ch X.400 c=ch;a=400net;p=iso;o=isocs;s=central PrintedinSwitzerland ii Foreword ISO(theInternationalOrganizationforStandardization)isaworldwidefederationofnationalstandardsbodies (ISOmemberbodies).TheworkofpreparingInternationalStandardsisnormallycarriedoutthroughISOtechnical committees.Eachmemb

    4、erbodyinterestedinasubjectforwhichatechnicalcommitteehasbeenestablishedhas therighttoberepresentedonthatcommittee.Internationalorganizations,governmentalandnongovernmental,in liaisonwithISO,alsotakepartinthework.ISOcollaboratescloselywiththeInternationalElectrotechnical Commission(IEC)onallmattersof

    5、electrotechnicalstandardization. DraftInternationalStandardsadoptedbythetechnicalcommitteesarecirculatedtothememberbodiesforvoting. PublicationasanInternationalStandardrequiresapprovalbyatleast75%ofthememberbodiescastingavote. InternationalStandardISO13415waspreparedbyTechnicalCommitteeISO/TC20, Air

    6、craftandspacevehicles , SubcommitteeSC15, Airframebearings . AnnexesAandBofthisInternationalStandardareforinformationonly. ISO ISO13415:1997(E) iii Introduction AtthetimethisInternationalStandardwasdeveloped,theImperialunitssizesofairframeneedlerollerbearingswere dominantinworldapplication.Thebasisf

    7、orthisInternationalStandardistheimperialunitsprovidedinannexA.INTERNATIONALSTANDARD ISO ISO13415:1997(E) 1 AerospaceAirframeneedletrackroller,studtype,singlerow, sealedInchseries 1Scope ThisInternationalStandardspecifiesthecharacteristics,boundarydimensions,tolerances,internalclearancesand permissib

    8、lestaticradialloadsofinchseries,singlerow,studtypeneedletrackrollersusedinairframeapplications. TheairframeneedletrackrollerscoveredbythisInternationalStandardaredesignedtooperateinthetemperature range54Cto+121C. 2Normativereferences Thefollowingstandardscontainprovisionswhich,throughreferenceinthis

    9、text,constituteprovisionsofthis InternationalStandard.Atthetimeofpublication,theeditionsindicatedwerevalid.Allstandardsaresubjectto revision,andpartiestoagreementsbasedonthisInternationalStandardareencouragedtoinvestigatethepossibility ofapplyingthemostrecenteditionsofthestandardsindicatedbelow.Memb

    10、ersofIECandISOmaintainregistersof currentlyvalidInternationalStandards. ISO68317: 1) , Heattreatedsteels,alloysteelsandfreecuttingsteelsPart17:Ballandrollerbearingsteels. ISO1132:1980, RollingbearingsTolerancesDefinitions. ISO2082:1986, MetalliccoatingsElectroplatedcoatingsofcadmiumonironorsteel. IS

    11、O3161:1996, AerospaceUNJthreads,withcontrolledrootradius,foraerospaceInchseries . ISO3353:1976, AerospaceRolledthreadsforboltsLeadandrunoutrequirements . ISO4520:1981, Chromateconversioncoatingsonelectroplatedzincandcadmiumcoatings. ISO5593:1997, RollingbearingsVocabulary. ISO6158:1984, Metalliccoat

    12、ingsElectroplatedcoatingsofchromiumforengineeringpurposes. ISO13411:1997,Aerospace Airframeneedleroller,cylindricalrollerandtrackrollerbearings Technical specification. AMS2417E:1993, Plating,zincnickelalloy. 2) 1) Tobepublished.(RevisionofISO68317:1976) 2) Availablefrom: SAEInternational 400Commonw

    13、ealthDrive Warrendale,PA150960001 USAISO13415:1997(E) ISO 2 3Definitions ForthepurposesofthisInternationalStandard,thedefinitionsgiveninISO5593apply. 4Symbols 4.1ForthepurposesofthisInternationalStandard,thesymbolsgiveninISO1132apply.Thesymbols(exceptthose fortolerances)showninthefiguresandthevalues

    14、giveninthetablesdenotenominaldimensionsunlessspecified otherwise. 4.2ThefollowingadditionalsymbolsforbearingscoveredbythisInternationalStandardalsoapply. C 1 trackcontactwidth C s permissiblestaticradialload d 1 studdiameter d 2 cotterpinholediameter d a clampingfacediameter R crownradiusofouterring

    15、 L 1 lengthofthreadonstud L 2 distancefromcentrelineofcotterpinholetoendofthread L 3 distancefrombottomofslottooppositesideofstud L 4 slotlength(bottomofslot) H bottomofslottooppositesideofstudgrip b slotwidth 5Requiredcharacteristics 5.1DimensionsTolerancesInternalclearancesLoads Forvalues,seetable

    16、1.Forconfiguration,seefigure1. ISO ISO13415:1997(E) 3 Table1ISO13415:1997(E) ISO 4 Dimensionsinmillimetres 1) SeeISO3353forthreadrunoutrequirements. 2) SeeannexB. Figure1 5.2Surfaceroughness Rollers: R a =0,2 mmmax. Innerringraceway: R a =0,4 mmmax. Outerringraceway: R a =1,0 mmmax. Endwashers: R a

    17、=1,6 mmmax.atrollercontactarea. 6Materials Ring/stud: bearingsteelISO68317,type1,racewaysandstudflangehardness58HRCto66HRC(670HVto 860HV),studcorehardness36HRCto44HRC(354HVto434HV). Rollers: bearingsteelISO68317,type1,heattreatedto58HRCto66HRC(670HVto860HV). Endwashers: steelheattreatedto51HRCto60HR

    18、C(528HVto697HV)atrollercontactarea. Seals: acetalresin,nylonorequivalent. ISO ISO13415:1997(E) 5 7Surfacetreatment 7.1Bearingsmadeofconventionalrollingbearingsteelshallhavetheexternalsurfacesoftheouterringchromium plated,andallotherexternalsurfacescadmiumorzincnickelplated. 7.2Wherecadmiumplatingiss

    19、pecified(codelettersDandM),itshallbeinaccordancewithISO2082.Thethickness oftheplatingshallnotbelessthan7mandnotmorethan15m.Thebearingshallbeembrittlementrelievedwithin 4hofplatingbyheattreatmentat140C10Cforaminimumof8hfollowedbychromatetreatmentinaccordance withISO4520(codeletterDonly). 7.3Wherechro

    20、miumplatingisspecified(codelettersD,MandZ),itshallbeinaccordancewithISO6158.Thethick nessoftheplatingshallbenotlessthan10m,8monfacesandringchamfers,andnotmorethan25m. 7.4Wherezincnickelplatingisspecified(codeletterZ),itshallbeinaccordancewithAMS2417E,type2.The thicknessoftheplatingshallnotbelessthan

    21、7mandnotmorethan15m. 8Optionalfeatures 8.1Lubricationfitting/cotterpinholeandslotinthreadedendofstud Bearingsmaybesuppliedwithasuitablelubricationfitting(seeannexB)intheflangedorthethreadedendofthestud. Theymayalsobesuppliedwithacotterpinhole.Bearingsmaybesuppliedwithaslotinthethreadedendofthestud t

    22、oreceiveatangintheboreofamountingwasher.Thesefeaturesarespecifiedthroughadesignationcodeinthepart numberasnotedbelow. Code Feature S lubricationfittinginflangedendofstud,nocotterpinhole,noslotinthreadedendofstud R lubricationfittinginflangedendofstud,nocotterpinhole,slotinthreadedendofstud P lubrica

    23、tionfittinginflangedendofstud,withcotterpinhole,noslotinthreadedendofstud J lubricationfittinginflangedendofstud,withcotterpinhole,slotinthreadedendofstud T lubricationfittinginthreadedendofstud,nocotterpinhole,noslotinthreadedendofstud U lubricationfittinginthreadedendofstud,nocotterpinhole,slotint

    24、hreadedendofstud L lubricationfittinginboththreadedandflangedendsofstud,nocotterpinhole,noslotinthreadedend ofstud W lubricationfittinginboththreadedandflangedendsofstud,nocotterpinhole,slotinthreadedendof stud 8.2Outerringprofile Bearingsmaybesuppliedwiththeoutsidesurfaceoftheouterringcrowned.Thisf

    25、eatureisspecifiedthrougha designationcodeinthepartnumberasnotedbelow. Code Feature N nocrown(cylindrical) C crownontheouterring 8.3Griplength Bearingsshallbesuppliedwithgriplengthsdesignatedbyatwodigitcodeasspecifiedintable2.ISO13415:1997(E) ISO 6 Table2 Griplength code Nominalgrip length mm Griplen

    26、gth code Nominalgrip length mm 01 1,588 41 65,088 02 3,175 42 66,675 03 4,762 43 68,262 04 6,35 44 69,85 05 7,938 45 71,438 06 9,525 46 73,025 07 11,112 47 74,612 08 12,7 48 76,2 09 14,288 49 77,788 10 15,875 50 79,375 11 17,462 51 80,962 12 19,05 52 82,55 13 20,638 53 84,138 14 22,225 54 85,725 15

    27、23,812 55 87,312 16 25,4 56 88,9 17 26,988 57 90,488 18 28,575 58 92,075 19 30,162 59 93,662 20 31,75 60 95,25 21 33,338 61 96,838 22 34,925 62 98,425 23 36,512 63 100,012 24 38,1 64 101,6 25 39,688 65 103,188 26 41,275 66 104,775 27 42,862 67 106,362 28 44,45 68 107,95 29 46,038 69 109,538 30 47,62

    28、5 70 111,125 31 49,212 71 112,712 32 50,8 72 114,3 33 52,388 73 115,888 34 53,975 74 117,475 35 55,562 75 119,062 36 57,15 76 120,65 37 58,738 77 122,238 38 60,325 78 123,825 39 61,912 79 125,412 40 63,5 80 127 ISO ISO13415:1997(E) 7 9Lubrication ThebearingshallbeprelubricatedwitheithergreaseAorB,as

    29、specifiedbythecustomer. NOTEDescriptionsofgreaseAandgreaseBaregiveninISO13411:1997,annexI. 10Designation BearingscoveredbythisInternationalStandardshallbedesignatedonlyinthemannershowninthefollowing example: wherethefollowingcodesareapplied: greases: A=estertypegrease; B=synthetichydrocarbontypegrea

    30、se; lubricationfitting/cotterpinholeandslotinthreadedendofstud(see8.1): S=lubricationfittinginflangedendofstud,nocotterpinhole,noslotinthreadedendofstud; R=lubricationfittinginflangedendofstud,nocotterpinhole,slotinthreadedendofstud; P=lubricationfittinginflangedendofstud,withcotterpinhole,noslotint

    31、hreadedendofstud; J=lubricationfittinginflangedendofstud,withcotterpinhole,slotinthreadedendofstud; T=lubricationfittinginthreadedendofstud,nocotterpinhole,noslotinthreadedendofstud; U=lubricationfittinginthreadedendofstud,nocotterpinhole,slotinthreadedendofstud; L=lubricationfittinginboththreadedan

    32、dflangedendsofstud,nocotterpinhole,noslotinthreadedendof stud; W=lubricationfittinginboththreadedandflangedendsofstud,nocotterpinhole,slotinthreadedendofstud; outerringprofiles: N=nocrown(cylindrical); C=crownonouterring; materials/surfacetreatments: D=material:lowalloybearingsteel; surfacetreatment

    33、:outerringchromiumplated;ISO13415:1997(E) ISO 8 washercadmiumplatedwithchromateconversioncoating; stud/innerringcadmiumplatedwithchromateconversioncoating,orblackoxidecoated; M=material:lowalloybearingsteel; surfacetreatment:outerringchromiumplated; washercadmiumplatewithoutchromateconversioncoating

    34、; stud/innerringcadmiumplatedwithoutchromateconversioncoating; Z=material:lowalloybearingsteel; surfacetreatment:outerringchromiumplated; washerzincnickelplated; stud/innerringzincnickelplated. 11Identificationmarking Inadditiontothemanufacturersnameortrademark,eachbearingshallbepermanentlyandlegibl

    35、ymarked,usingthe identityblockasdefinedinclause10.Markingpositionandmethodshallbeatthemanufacturersoption. 12Technicalspecification AirframeneedletrackrollerssuppliedtothisInternationalStandardshallconformtotherequirementsofISO13411. ISO ISO13415:1997(E) 9 AnnexA (informative) Imperial(nonSI)units T

    36、ablesA.1andA.2givetheimperial(nonSI)unitinformationthatisthebasisforthisInternationalStandard. TableA.1ISO13415:1997(E) ISO 10 TableA.2 Griplength code Griplength in Griplength code Griplength in 01 0,0625 41 2,5625 02 0,125 42 2,625 03 0,1875 43 2,6875 04 0,25 44 2,75 05 0,3125 45 2,8125 06 0,375 4

    37、6 2,875 07 0,4375 47 2,9375 08 0,5 48 3 09 0,5625 49 3,0625 10 0,625 50 3,125 11 0,6875 51 3,1875 12 0,75 52 3,25 13 0,8125 53 3,3125 14 0,875 54 3,375 15 0,9375 55 3,4375 16 1 56 3,5 17 1,0625 57 3,5625 18 1,125 58 3,625 19 1,1875 59 3,6875 20 1,25 60 3,75 21 1,3125 61 3,8125 22 1,375 62 3,875 23 1

    38、,4375 63 3,9375 24 1,5 64 4 25 1,5625 65 4,0625 26 1,625 66 4,125 27 1,6875 67 4,1875 28 1,75 68 4,25 29 1,8125 69 4,3125 30 1,875 70 4,375 31 1,9375 71 4,4375 32 2 72 4,5 33 2,0625 73 4,5625 34 2,125 74 4,625 35 2,1875 75 4,6875 36 2,25 76 4,75 37 2,3125 77 4,8125 38 2,375 78 4,875 39 2,4375 79 4,9375 40 2,5 80 5 ISO ISO13415:1997(E) 11 AnnexB (informative) Lubricationfitting B.1General Thisannexprovidesthedescriptionofthelubricationfittingusedwiththeinchseriessinglerow,studtypesealed needletr


    注意事项

    本文(ISO 13415-1997 Aerospace - Airframe needle track roller stud type single-row sealed - Inch series《航空航天 飞机结构用柱型单列密封的滚针滚道式滚子 英制系列》.pdf)为本站会员(terrorscript155)主动上传,麦多课文档分享仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文档分享(点击联系客服),我们立即给予删除!




    关于我们 - 网站声明 - 网站地图 - 资源地图 - 友情链接 - 网站客服 - 联系我们

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1 

    收起
    展开