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TurboGen TM Gas Turbine Power System Lab Experiment Manual Lab Session #4: Engine Performance Analysis Purpose: To perform system performance calculations of the engine at the compressor inlet and nozzle exit. The data for these calculations comes from the information recorded and plotted in a previous lab session Procedure: Perform requested analysis and calculations at this location and operational point. COMPRESSOR INLET Temperature Probe Pitot-Static Tube What is the Pitot-Static Recorded Pressure (Compressor Inlet Pressure) and Air Density at this location and operating condition? Copyright April, 2010 18 Turbine Technologies, Ltd.
Calculate the gas (air) Velocity into compressor at this operating condition. Calculate the Volumetric Flow Rate of air into compressor at this operating condition. Calculate Mass Flow Rate of air into compressor at this operating condition. Copyright April, 2010 19 Turbine Technologies, Ltd.
Page 1 and 2: TurboGen TM Gas Turbine Electrical
Page 3 and 4: How it works! Engine Air Intake Com
Page 5 and 6: SR-30 Gas Turbine Engine / TG-2000
Page 7 and 8: In preparation for system operation
Page 9 and 10: Copyright April, 2010 9 Turbine Tec
Page 11 and 12: TurboGen TM Gas Turbine Electrical
Page 13 and 14: Graphing Data using MS-Excel Spread
Page 15 and 16: Name Graph, Click as New Sheet, Fin
Page 17: For the analysis point chosen in La
Page 21 and 22: the winding, where maximum coupling
Page 23 and 24: Power Output = IV: To hold at this
Page 25 and 26: Copyright April, 2010 25 Turbine Te
Page 27: Copyright April, 2010 27 Turbine Te

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