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Wave-Rotor-Enhanced Gas Turbine Engine DemonstratorThe U.S. Army Research Laboratory, NASA Glenn Research Center, and Rolls-Royce Allison are working collaboratively to demonstrate the benefits and viability of a wave-rotor-topped gas turbine engine. The self-cooled wave rotor is predicted to increase the engine overall pressure ratio and peak temperature by 300% and 25 to 30%. respectively, providing substantial improvements in engine efficiency and specific power. Such performance improvements would significantly reduce engine emissions and the fuel logistics trails of armed forces. Progress towards a planned demonstration of a wave-rotor-topped Rolls-Royce Allison model 250 engine has included completion of the preliminary design and layout of the engine, the aerodynamic design of the wave rotor component and prediction of its aerodynamic performance characteristics in on- and off-design operation and during transients, and the aerodynamic design of transition ducts between the wave rotor and the high pressure turbine. The topping cycle increases the burner entry temperature and poses a design challenge to be met in the development of the demonstrator engine.
Document ID
20000018016
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Welch, Gerard E.
(Army Research Lab. Cleveland, OH United States)
Paxson, Daniel E.
(NASA Glenn Research Center Cleveland, OH United States)
Wilson, Jack
(DYNACS Engineering Co., Inc. Brook Park, OH United States)
Synder, Philip H.
(Rolls-Royce Allison Indianapolis, IN United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 1999
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ARL-TR-2113
E-11958
NAS 1.15:209459
NASA/TM-1999-209459
Report Number: ARL-TR-2113
Report Number: E-11958
Report Number: NAS 1.15:209459
Report Number: NASA/TM-1999-209459
Meeting Information
Meeting: Gas Turbine Operation and Technology for Land, Sea and Air Propulsion and Power Systems
Location: Ottawa
Country: Canada
Start Date: October 18, 1999
End Date: October 21, 1999
Sponsors: Research and Technology Organization
Funding Number(s)
PROJECT: DA Proj. 1L1-62211-A4-7A
PROJECT: RTOP 523-26-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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