Author: Pezhman Akbari
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 522
Book Description
Performance Prediction and Preliminary Design of Wave Rotors Enhancing Gas Turbine Cycles
Author: Pezhman Akbari
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 522
Book Description
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 522
Book Description
Wave-Rotor-Enhanced Gas Turbine Engine Demonstrator
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
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.
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
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 Test Rig Design Procedure for Gas Turbine Enhancement
Author: Pranav Ajit Sané
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 268
Book Description
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 268
Book Description
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 10-13 July 2005, Tucson, Arizona: 05-3800 - 05-3849
Integration of a Wave Rotor to an Ultra-micro Gas Turbine (U[mu]GT)
Author: Florin Iancu
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 566
Book Description
Publisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 566
Book Description
Preliminary Design Approach to the First Generation Internal Combustion Wave Disc Engine
Author: Kanishka Sharma
Publisher:
ISBN:
Category : Internal combustion engines
Languages : en
Pages : 232
Book Description
Publisher:
ISBN:
Category : Internal combustion engines
Languages : en
Pages : 232
Book Description
Wave Rotor-enhanced Gas Turbine Engines
Performance Benefits for Wave Rotor-Topped Gas Turbine Engines
Author: Scott M. Jones
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
Presented at the International Gas Turbine and Aeroengine Congress & Exhibition Birmingham, UK - June 10-13, 1996.
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
Presented at the International Gas Turbine and Aeroengine Congress & Exhibition Birmingham, UK - June 10-13, 1996.