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Pressure-Gain Combustion for Gas TurbinesPressure Gain Combustion (PGC) is under investigation as a means to improve the thermal efficiency of gas turbines. PGC is a fundamentally unsteady combustion process which, through some means of confinement, raises the total pressure of the working fluid relative to the initial process state. When implemented in a combustor it yields a total pressure gain across the device instead of the typical loss seen in a conventional combustor. This pressure gain can significantly improve gas turbine performance. The tutorial will provide an introduction to the concept of PGC. It will begin with a process description in fundamental thermodynamic terms, and will quantify potential benefits. The majority of the presentation will describe the various approaches to implementation that are under investigation by the PGC.
Document ID
20180003957
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Paxson, Dan
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
July 13, 2018
Publication Date
June 11, 2018
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN55268
Meeting Information
Meeting: ASME 2018 Turbo Expo
Location: Lillestrom
Country: Norway
Start Date: June 11, 2018
End Date: June 15, 2018
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 109492.02.03.02.30
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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