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Fuel and Combustor Concerns for Future Commercial CombustorsCivil aircraft combustor designs will move from rich-burn to lean-burn due to the latter's advantage in low NOx and nvPM emissions. However, the operating range of lean-burn is narrower, requiring premium mixing performance from the fuel injectors. As the OPR increases, the corresponding combustor inlet temperature increase can benefit greatly with fuel composition improvements. Hydro-treatment can improve coking resistance, allowing finer fuel injection orifices to speed up mixing. Selective cetane number control across the fuel carbon-number distribution may allow delayed ignition at high power while maintaining low-power ignition characteristics.
Document ID
20170008119
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Chang, Clarence T.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
August 31, 2017
Publication Date
June 27, 2017
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN43989
Report Number: GRC-E-DAA-TN43989
Meeting Information
Meeting: ASME Turbo Expo 2017
Location: Charlotte, NC
Country: United States
Start Date: June 26, 2017
End Date: June 30, 2017
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 081876.02.03.04.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Combustor
Fuels
Cetane
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