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Keywords: Gas Turbine PerformanceClose
Proc. ASME. GT2020, Volume 8: Industrial and Cogeneration; Manufacturing Materials and Metallurgy; Marine; Microturbines, Turbochargers, and Small Turbomachines, V008T17A003, September 21–25, 2020
Paper No: GT2020-14500
... efficiencies and the variation of these component efficiencies within the operating range. This paper describes how each one of these factors, individually, influences the outcome. gas turbine performance single-shaft two-shaft thermal efficiency specific work OFF-DESIGN PERFORMANCE COMPARISON...
Jesuíno Takachi Tomita, Cleverson Bringhenti, João Roberto Barbosa, Vitor Alexandre Carlesse Martins
Proc. ASME. GT2012, Volume 3: Cycle Innovations; Education; Electric Power; Fans and Blowers; Industrial and Cogeneration, 449-456, June 11–15, 2012
Paper No: GT2012-70020
... with the design methodology of a 5:1 pressure ratio, 5-stage axial flow compressor with VIGV and a single stage axial flow turbine. These components were designed and their maps synthesized and fed to the gas turbine performance simulation program. The engine performance results were analyzed and verified...
Joa˜o Roberto Barbosa, Franco Jefferds dos Santos Silva, Jesuino Takachi Tomita, Cleverson Bringhenti
Proc. ASME. GT2011, Volume 4: Cycle Innovations; Fans and Blowers; Industrial and Cogeneration; Manufacturing Materials and Metallurgy; Marine; Oil and Gas Applications, 273-281, June 6–10, 2011
Paper No: GT2011-46565
..., the compressor map was generated and fed to the gas turbine performance simulation program. The transient study was carried out for a number of blade settings, using different VIGV geometry scheduling, giving indication that simulations needed to study the control strategy can be easily achieved. The results...
Proc. ASME. GT2010, Volume 3: Controls, Diagnostics and Instrumentation; Cycle Innovations; Marine, 703-710, June 14–18, 2010
Paper No: GT2010-22867
... are discussed. Gas Turbine Performance Axial Flow Compressor Turbine Cooling Compressible Flows Copyright © 2010 by ASME 1 PERFORMANCE STUDY OF A 1 MW GAS TURBINE USING VARIABLE GEOMETRY COMPRESSOR AND TURBINE BLADE COOLING Cleverson Bringhenti Instituto Tecnológico de Aeronáutica - ITA Gas Turbine...