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System Study: Technology Assessment and Prioritizing UpdateFor the Intelligent Engine System (Propulsion 21) study, each technology was evaluated to determine the impact to fuel burn, acoustics, and NOx emissions. The optimum combination of technologies and their overall benefits to the system were also evaluated, resulting in noise improvement potential of 1.89 EPNdB cumulative margin,-1.34 percent fuel burn, and 50 percent NOx reduction from the 2015 UEET-QAT baseline. All the technology evaluations, except T18-20D, were based on newengines, where the engine was resized to obtain the maximum system benefit while maintaining the same cycle parameters as the 2015 UEET-QAT baseline. The impact of turbine clearance control on deteriorated engines, T18-20D, was also evaluated. Recommendations for future system study work include, but were not limited to, validation of a university-developed engine deterioration model and customer value analysis as figures of merit beside fuel burn, emissions, and acoustics.
Document ID
20080023402
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Date Acquired
August 24, 2013
Publication Date
May 1, 2008
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-16492
NASA/CR-2008-215224
Report Number: E-16492
Report Number: NASA/CR-2008-215224
Funding Number(s)
WBS: WBS 984754.02.07.03.11.03
CONTRACT_GRANT: NAS3--01135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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