航空动力装置12发动机特性.ppt
GasTurbine
Aero-engineByZhaoTingyuThermalenergyandpowerengineeringstaffsection
CompanyLogoEngineperformanceEnginePerformanceEngineCharacteristicsEngineThrust-settingParameterEfficienciesEngineOperationandMonitoringTakeoffThrustSetting
CompanyLogoEngineThrust-settingParameterEnginePressureRatio(EPR)
CompanyLogoEngineThrust-settingParameterEngineRPM
CompanyLogoEngineCharacteristicsEffectofEngineRPMChanges(SpeedCharacteristic)
CompanyLogoEngineCharacteristicsEffectsofAltitudeChanges(AltitudeCharacteristic)
CompanyLogoEngineCharacteristics
CompanyLogoEngineCharacteristicsEffectsofAircraftForwardSpeedChanges(VelocityCharacteristic)
CompanyLogoEngineCharacteristics
CompanyLogoEngineCharacteristicsEffectsofTemperatureChanges
CompanyLogoEngineCharacteristicsEffectsofbleedair
CompanyLogoEngineCharacteristicsEffectsofbleedairThebleedingofairfromthecompressor★reducestheamountofmassairflow★decreasingthrust/rpm,increasing★exhaustgastemperatureandspecificfuelconsumption★improveitsworkingstability
CompanyLogoEfficienciesInternalefficiencyThethermalefficiencyspecifiestheenergylossestotheatmosphereduetoexhaustgasheat:
EfficienciesThequalitycoefficienttheworkinglossesoftherealgasturbine:Theinternalefficiencyexpressesthequalityofajetengineasaheatengine.Itspecifiesthepercentageoffuelenergyinputwhichisconvertedintokineticenergyofthegasstream.
EfficienciesPropulsionefficiencyTheefficiencyofconversionofkineticenergytopropulsiveworkistermedthepropulsiveorexternalefficiencyandisaffectedbytheamountofkineticenergywastedbythepropellingmechanism.
EfficienciesEnginepropulsionefficiencies
CompanyLogoEngineOperationandMonitoringEngineRegimesMaximumtake-offthrustMaximumgo-aroundthrustMaximumcontinuousthrustMaximumclimbthrustMaximumcruisethrustIdle
CompanyLogoEngineOperation