Wave Rotor Enhanced Gas Turbine Engine Demonstrator
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Wave Rotor Enhanced Gas Turbine Engine Demonstrator
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Author :
language : en
Publisher:
Release Date : 1999
Wave Rotor Enhanced Gas Turbine Engine Demonstrator written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with categories.
The 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.
Wave Rotor Enhanced Gas Turbine Engine Demonstrator
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-06-15
Wave Rotor Enhanced Gas Turbine Engine Demonstrator written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-06-15 with categories.
The 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. Welch, Gerard E. and Paxson, Daniel E. and Wilson, Jack and Synder, Philip H. Glenn Research Center NASA/TM-1999-209459, NAS 1.15:209459, ARL-TR-2113, E-11958
Wave Rotor Enhanced Gas Turbine Engine Demonstrator
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Author : Gerard E. Welch
language : en
Publisher:
Release Date : 1999
Wave Rotor Enhanced Gas Turbine Engine Demonstrator written by Gerard E. Welch and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with categories.
The 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.
Performance Prediction And Preliminary Design Of Wave Rotors Enhancing Gas Turbine Cycles
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Author : Pezhman Akbari
language : en
Publisher:
Release Date : 2004
Performance Prediction And Preliminary Design Of Wave Rotors Enhancing Gas Turbine Cycles written by Pezhman Akbari and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2004 with Gas-turbines categories.
Integration Of A Wave Rotor To An Ultra Micro Gas Turbine U Mu Gt
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Author : Florin Iancu
language : en
Publisher:
Release Date : 2005
Integration Of A Wave Rotor To An Ultra Micro Gas Turbine U Mu Gt written by Florin Iancu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with Gas-turbines categories.
Research Technology 1997
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Author :
language : en
Publisher: DIANE Publishing
Release Date : 1998
Research Technology 1997 written by and has been published by DIANE Publishing this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.
Dynamic Simulation Of A Wave Rotor Topped Turboshaft Engine
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Author : R. B. Greendyke
language : en
Publisher:
Release Date : 1997
Dynamic Simulation Of A Wave Rotor Topped Turboshaft Engine written by R. B. Greendyke and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with categories.
38th Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit 02 4050 02 4099
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Author :
language : en
Publisher:
Release Date : 2002
38th Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit 02 4050 02 4099 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with Airplanes categories.
Design Considerations For Micro Wave Disc Engines
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Author : Marco Vagani
language : en
Publisher:
Release Date : 2008
Design Considerations For Micro Wave Disc Engines written by Marco Vagani and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2008 with Internal combustion engines categories.
Wave Engine Topping Cycle Assessment
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Author :
language : en
Publisher:
Release Date : 1996
Wave Engine Topping Cycle Assessment written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with categories.