ROMAC齿轮与齿轮传动系统分析.pptx
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ROMAC齿轮与齿轮传动系统分析.pptx
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,Talk25AnalysisofGearsandGearedSystems,JasonKaplanPaulAllaireTimDimondBradNicholsAmirYounan,TableofContents,IntroductionObjectivesMotivationModelingofgearmeshstiffnessExternalParallelShaft-StagesSpurgearsHelicalgearsPlanetaryStagesApplicationsSteam-Turbine/GeneratorGearboxNRELWindTurbineGearboxConclusions/Futurework,07/26/2011,2,ROMACObjectives,GearedsystemsarequiteimportanttomanyrotatingmachinesNomajorROMACgearedsystemscodecurrentlyNewmajoradvanceinROMACcodesBlakeStringerdeveloped12x12generalizedgearstiffnessmatrixin2006NeedstobemergedwithMatlabRotorcodecombinedlateral,torsional,axialmotionsNowexpandedintoplanetarygearsandothernewmodelingofgearedsystemcomponentsManynewapplications,07/26/2011,3,FromthegearboxesinthecarstotheJetengines.Alsointhehelicopterspeciallyintherotorshatanditstransmissionsystem.ThefocusofourtalktodayintheModelsofthesegearsstiffness,PW-1000GGearedTurbofan,JetEngineinAircraft,Introduction(GearApplication),4,AH-64DApacheLon0g7b/2o6w/2011,Automotivegearbox,OH-58DKiowaWarrior,Motivation,GearingexistsinalargevarietyofdifferentrotatingmachineswherespeedandtorqueconversionisnecessaryGearmeshstiffnesshassignificanteffectsonthemodeshapesandcriticalspeedsforthecoupledlowandhighspeedshaftsStatictransmissionerrorandothergeometricimperfectionsmayproducesignificantexcitationforcesFailuretoproperlymodelgearmeshstiffnessandexcitationsourceswouldhindertheabilitytopredictmachinevibrationlevels,07/26/2011,5,Thefirstistherotordynamicwherethegearislookatasaconnectionbetweentwopoint.Inthesemodels,theforcesofthegearismodeledinastiffnessmatrixtoconnectbetweentwonodes.Onasmallerlevel,thecontactbetweenthesurfaceofthegearinmeshareaffectedwiththeEHLwhichtakesplace.EHLcontributetothestiffnessbetweentheteethduetotheelasticdeformationoftheteethaswellasthecompressibilityoftheoil.Thethirdpartisthetoothcomplianceasseenasacontiliver.Thosethreestiffnessarethethreemajorcontributortobuildafullgearstiffness.WewillbefocusingontheRotordynamicandEHLstiffness,Introduction(MainIdea),EHLStiffnessModels,ToothComplianceModels,RotorDynamicsModels,FullGearStiffnessmodel,07/26/2011,6,Thestiffnessmatrixisfunctionofthedimensionofthegearaswellastheorientationanglesoftheforce.Alsothismatrixisfunctionofthestiffnesscoefficientwhichismultipliedbythematrix.Inthesametime,theEHLanalysisfocusonthepressuredistributionofthelubricantandtheelasticdeformationwhichtakesplacebetweentheteeth.Asseenintherightdiagram.Theelasticityofthesurfaceaswellasthecompressibilityofthelubricantaffectsthestiffnessofgear.Here,itcametheideaofmergingtheworkdoneonthegeardynamicwiththeEHLlubricationtocomeupwithageneralmodelforthestiffness,Introduction(OurFocus),07/26/2011,7,x,y,K,r2,r1,2,O2,O1,1,1RotordynamicAnalysis,(Stringer,2008),SpurGearsvs.HelicalGears,Forcesandmomentsactinxy-planeonly(2-Dspace)Functionofpressureangle(an)only3-DOFmodel(x,y,qz),Forcesandmomentsin3-DspaceFunctionofpressureangle(an)andhelicalangle(b)6-DOFmodel(x,y,z,qx,qyqz),07/26/2011,8,General12-DOFMeshStiffnessMatrix,Constructedbyusingdirectmethodalongline-of-action.,Matrixisafunctionofaxisorientation(j),pressureangle(an),helicalangle(b),gearandpinionpitchradii(riandrj),andaveragegearmeshstiffness(Kg).,x,y,K,rj,ri,j,Oj,Oi,i,i,07/26/2011,9,j,Why12Degrees-of-Freedom?
12-DOFmodelssparseinliteratureApplicabletospurgears(3DOFs)andhelicalgears(6DOFs)Ifmodelingaspurgearmesh,helicalanglewillbesettozero,andtheextraDOFsreducetozeroNumberofDOFsaregenerallyreducedbyconvenientchoiceofaxes.Convenientchoicesarenotalwaysavailable(i.e.,rotorcrafttransmission),12DOFmodelnecessary,x,y,K,rj,ri,j,Oj,Oi,i,07/26/2011,10,Averagegearmeshstiffness,(Spotts,1985)Formulaappliesforsingle-tooth-to-toothcontactwhere,b=facewidthE1=ElasticmodulusofpinionE2=Elasticmodulusofgear,ImageFromWikipedia,07/26/2011,11,Averagegearmeshstiffness,Factorof1.3addedtoaccountfortheaveragenumberofteethincontact(Stringer,2008)NowautomaticallyincludedincodeActualstiffnessistime-varyingasnumberofcontactpairschanges,TradeI,07/26/2011,12,Force/MomentDisplacementRelationship,x,NodesiandjcontaintheDOFsolutionsforthecoupledshaftsatthelocationsofthegearandpinion.AllelementsofKmesharethenaddedintotheglobalstiffnessmatrixsuchthattheDOFsatnodesiandjmatchtheDOFsatthenodallocationsofthegearsontheshaft.y,K,rj,ri,j,Oj,Oi,i,i,07/26/2011,13,j,General12-DOFMeshStiffnessMatrix,07/26/2011,14,PlanetaryStageModeling,SunnPlanetsCarrierAnnulus,Kahraman,1994,rji
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- ROMAC 齿轮 传动系统 分析