NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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 as a gas turbine 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. This presentation is a modified and updated version of a 2018 tutorial of the same name. It is tailored to a graduate student audience that is familiar with the PGC concept, but has focused entirely on a specific type of implementation. It will provide a brief review of the concept of PGC and why it's important. The majority of the presentation will describe the various approaches to implementation that are under investigation by the PGC community. Emphasis will be on strategies other than the one that the students are investigating.
Document ID
20240010842
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Dan Paxson
(Glenn Research Center Cleveland, United States)
Date Acquired
August 21, 2024
Subject Category
Aircraft Propulsion and Power
Meeting Information
Meeting: INSPIRE Capstone Symposium
Location: Florence
Country: IT
Start Date: September 26, 2024
End Date: September 27, 2024
Sponsors: Technische Universität Berlin
Funding Number(s)
WBS: 109492.02.03.05.04
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
Combustion
Detonation
Pressure Gain Combustion
No Preview Available