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ID:30276963
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页数:7页
时间:2018-12-28
《2003 a new scaling method for component maps of gas turbine using system identification》由会员上传分享,免费在线阅读,更多相关内容在学术论文-天天文库。
1、ANewScalingMethodforComponentMapsofGasTurbineC.KongUsingSystemIdentificatione-mail:cdgong@mail.chosun.ac.krJ.KiAscalingmethodforcharacteristicsofgasturbinecomponentsusingexperimentaldatae-mail:kijayoung@hanmir.comorpartiallygivendatafromenginemanufactu
2、rerswasnewlyproposed.Incaseofcur-rentlyusedtraditionalscalingmethods,thepredictedperformancearoundtheon-designM.Kangpointmaybewellagreedwiththerealengineperformance,butthesimulatedperfor-e-mail:k0914@stmail.chosun.ac.krmanceatoff-designpointsfarawayfro
3、mtheon-designpointmaynotbewellagreedwiththerealengineperformancegenerally.Itwouldbecausedthatcomponentscalingfactors,DepartmentofAerospaceEngineering,whichwereobtainedaton-designpoint,isalsousedatallotheroperatingpointsandChosunUniversity,components'ma
4、psarederivedfromdifferentknownenginecomponents.Thereforeto#375Seosuk-dong,minimizetheanalyzedperformanceerrorinthethisstudy,®rstcomponents'mapsareDong-gu,constructedbyidentifyingperformancesgivenbyenginemanufacturersatsomeoperatingKwangju501-759,Koreac
5、onditions,thenthesimulatedperformanceusingtheidenti®edmapsiscomparedwithperformancesusingcurrentlyusedscalingmethods.Incomparison,theanalyzedperfor-mancebythecurrentlyusedtraditionalscalingmethodwaswellagreedwiththerealengineperformanceaton-designpoint
6、buthadmaximum22%erroratoffdesignpointswithinthe¯ightenvelopeofastudyturbopropengine.However,theperformanceresultbythenewlyproposedscalingmethodinthisstudyhadmaximum6%reasonableerrorevenatall¯ightenvelope.@DOI:10.1115/1.1610014#Introductionusingexperime
7、ntaldataorpartiallygivendatafromenginemanu-facturerswasproposed.ThismethodcanberealizedusingthePerformancesimulationisoneofthemostimportantactivitiesfollowingprocedure:itisthat®rstafterobtainingthescalingnotonlytominimizeriskandcostindevelopmentphasebu
8、talsomapswiththescalingfactorsofcomponentsfromtheknowntomonitorenginehealthinoperationphase.performancedataortheknownexperimentaldatabyengineInordertosimulategasturbineperformanceitisabsolutelymanufacturersatsomeoperationpoints,andthenc
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