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ID:30276291
大小:1.31 MB
页数:42页
时间:2018-12-28
《1984 real-time hybrid computer simulation of a small turboshaft engine and control system》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、N84-21548---NASATechnicalMemorandum83579'Real-TimeHybridComputerSimulationofaSmallTurboshaftEngineandControlSystemClintE.HartandLeonM.WenzeI......LewisResearchCenterCleveland,Ohio...........x-.........,t•.-.........................February1984IXl/AItl
2、_I[REAL-TIMEHYBRIDCOMPUTERSI
3、MULATIONOFASMALLTURBOSHAFTENGINEANDCONTROLSYSTEMClintE.HartandLeonM.WenzelNationalAeronauticsandSpaceAdministrationLewisResearchCenterCleveland,Ohio44135SUMMARYThisreportdescribesthedevelopmentofananalyticalmodelofasmallturboshaftenginedesignedforhelicopterpropulsionsystems.Themo
4、delequa-tionswereimplementedonahybridcomputersystemtoprovideareal-timenon-linearsimulationoftheengineperformanceoverawideoperatingrange.Thereal-timehybridsimulationoftheenginewasusedasatestbedforevaluat-ingamicroprocessor-baseddigitalcontrolmodule.Thisdigitalcontrolmodulewasdevel
5、opedaspartofanadvancedrotorcraftcontrolprogramthathasthelong-termgoalofrotorcraftflightandpropulsioncontrolintegration.Aftertestswiththehybridenginesimulationthedigitalcontrolmodulewasusedtocontrolarealengineinanexperimentalprogram.Ahybridsimulationoftheengine'selectrical-hydrome
6、chanicalcontrolsystemwasalsodeveloped.Thisprovidedaconvenientwayofvaryingthefuelflowandtorqueloadinputstothehybridenginesimulationforsimulatingtransientoperation.Acomparisonofsteady-statedataobtainedfromthesimulationandtheexperimentaltestsispresentedthatvalidatesthesimula-tionres
7、ults.Analyticalmodelequations,analogcomputerdiagrams,andadigitalcomputerflowchartaregivenintheappendixes.INTRODUCTIONNewmissionrequirementsforhelicoptersareleadingtodemandsforfasterresponsefromthehelicopterpropulsionsystemanditsassociatedcontrol.Themostcommonhelicopterpropulsions
8、ystememploysoneortwosmallturboshaftengines.Currentturboshaftenginecontrolsusepneumatic,hydraulic,andmechanicalcomponentstoperformthecontrolsensing,computation,andactua-tion.Therearelimitationsonthedynamicresponseofthesetypesofcom-ponentandthecomplexityofthecontrolfunctionsthatthe
9、ycanhandle.Onemeansofovercomingtheselimi
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