多级涡轮密封泄漏的数值模拟PPT推荐.pptx
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多级涡轮密封泄漏的数值模拟PPT推荐.pptx
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,InletValve,ExhaustHood,OriginalModel,RedesignedModel,straight,twisted,Blade3DSTM,3DVTM,Potentialimprovements?
LeakageLoss,BladeShapeLoss,SecondaryFlowLoss,Rotor/StatorInteractionLossCavityFlowLoss,BladeTipSealsLossRatio:
40%PowerLoss:
3149KWHeatConsumption:
71.7KJ/KWh,ShaftSealsLossRatio:
16%PowerLoss:
1618KWHeatConsumption:
28.5KJ/KWh,DiaphragmSealsLossRatio:
11%PowerLoss:
898KWHeatConsumption:
18.9KJ/KWh,BladeShapeLossRatio:
2%PowerLoss:
179KWHeatConsumption:
3.2KJ/KWh,SurfaceRoughnessLossRatio:
31%PowerLoss:
2765KWHeatConsumption:
54.9KJ/KWh,PowerandHeatLossFactorofHP/IPCylinder,Howtoreduceleakageloss?
ReasonsofEfficiencyLossCausedbySealsLeakageFlow:
DirectLoss:
massflowreductionofmainsteampartakingexpansioninbladepathandthusreductionofworkLossofbladeliftintheendsectionsandthusreductionofwork,IndirectLoss:
IncreasedincidenceondownstreamstagewithconsecutiveincreaseinsecondaryflowMixinglossoftipvortexandtipjetrespectively,Unshrouded,Shrouded,SealsUsedinSteam/GasTurbine:
LabyrinthSeal,HoneycombSeal,BrushSeal,LabyrinthSealsCharacters:
simplicityreliabilityeasyreplacementlowcost,Disadvantage:
limitedbymaterial,labyrinthsealsshouldkeeparelevantclearanceduringoperationsolargeleakageinfluencestheefficiencyofturbine,especiallyduringenginetransients,Toreduceleakagerate,honeycomb&
brushsealusedmoreandmoreintheturbinemachinery.,Advantagescomparetolabyrinthseal:
Honeycombseals,rotoroutletbeforedrainoff,nextstageafterdrainoff,EFFICIENCY,0.08%,Unsaturated(wet)steamdomain,EXPERIMENT,TESTBENCH,TESTPIECE,NUMERICALSIMULATIONToInsureResultMoreAccuracyandOperateMoreConvenientWechoose:
LabyrinthSeaL,LeakageFlowSimulation:
1.09%,shroud43%diaphragmleakageinshroudis43%largerthanIndiaphragmallleakageflow(2.1kg/s)accountsfor0.83%ofmainstreamflow(254.4kg/s),efficiencylosscausedbyleakageflowis1.09%inthisturbinestage,Flowlinesinlabyrinthseals:
pressuredropinaxialdirectionthrottlingeffectoftooth,NumericalSimulationStrategy:
Calculationdomain,HoneycombSeal,BladeStage,DiaphragmSeal,HoneycombSeal,NumericalSimulationStrategy:
MeshGeneration,AutoGrid5,iGG,iGG,SomeResultsofSimulation,SomeResultsofSimulation:
Velocityvectorsinaxialcuttingplane:
Vortexinhoneycomb:
Velocityvectorsatdifferentradialheight:
FlowdirectioninZ(axialdirection),Withtheradialheightincreasing:
FlowdirectioninreverseaxialdirectionMagnitudeofvelocityDecreasedVortexesshaped,LeakageinDifferentSeals,Clearance:
0.75mm,Clearance:
0.2mm,OtherExample,HeadingPlateBackingPlate,BristlePack,BrushsealNumericalSimulationStrategy:
Geometry,MeshGeneration,2D,3D,ConnecttoblademeshinIGG,PorousMediaModel,DarcyLaw:
Themodelcanbeusedbyspecifyingthefollowingparameters:
TheporositywhichdependsonthestructureofthebristlepackThemeandiameteroftheinclusiondThenthepremeabilitykisgivenbytheCarman-Kozenyrelation:
Pressuredropsinbristlepack:
Flowlinesinbrushseal:
a,b,c,d,e,f,Conclusion:
Inturbinestage,leakageratesinfluenceflowefficiencydramatically.Analyzingtheleakageofdifferentsealsisveryusefultoenhancetheflowefficiency.NUMECAispowerfultosimulateleakageofsealsinturbineandtheflowdetailsarealsocapturedthroughCFD.Allofthesecanaidindesigninglowleakagesealstoenhancetheflowefficiency,Suggestions:
Forporousmediummodel:
Inthiscase,thepremeabilitykinaxialandradialdirectionisnotthesame.however,theporousmediumprovidedbyNUMECA,onlyonepremeabilitykcouldbesetted.sothepremeabilityisthesameinalldirection.Thisisnotverysimilarwiththephysicalphenomenon.,thisproblemcouldbesolvedbysettingpremeabilitykindifferentdirections,Suchasinthiscase:
inaxialdirection-KZinradialdirection-Kr,Forconvergenceofefficiency:
Forsteamturbine,condensable_water_steamischosedasfluidmodel.Andallth
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- 关 键 词:
- 多级 涡轮 密封 泄漏 数值 模拟