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Adaptive Engine Technologies for Aviation CO2 Emissions ReductionAdaptive turbine engine technologies are assessed for their potential to reduce carbon dioxide emissions from commercial air transports.Technologies including inlet, fan, and compressor flow control, compressor stall control, blade clearance control, combustion control, active bearings and enabling technologies such as active materials and wireless sensors are discussed. The method of systems assessment is described, including strengths and weaknesses of the approach. Performance benefit estimates are presented for each technology, with a summary of potential emissions reduction possible from the development of new, adaptively controlled engine components.
Document ID
20060046621
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Mercer, Carolyn R.
(NASA Glenn Research Center Cleveland, OH, United States)
Haller, William J.
(NASA Glenn Research Center Cleveland, OH, United States)
Tong, Michael T.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2006
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA Paper 2006-5105
E-15670
NASA/TM-2006-214392
Meeting Information
Meeting: 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Sacreamento, CA
Country: United States
Start Date: July 9, 2006
End Date: July 12, 2006
Sponsors: American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc., American Society for Electrical Engineers
Funding Number(s)
WBS: WBS 846-02-07-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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