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Small Engine Technology InvestigationThe primary objective of the small engine technology study task is to identify key, enabling jet engine component technologies for improved performance, primarily for commercial, regional subsonic aircraft. The study involved two regional engine applications: the CF34 turbofan engine, which is installed on a regional jet application and the CT7-9 turboprop, which is installed on regional turboprop applications. Technologies to improve the performance of these applications were identified. Estimates of the benefits and development costs for each technology were made. Performance sensitivities were calculated for each of the technology items identified. The technology improvements were then translated into component improvements and their impact on the aircraft economics was evaluated. A factor of merit based on sfc was calculated as the percent improvement in sfc times the probability of improvement divided by the development evaluation costs associated with that technology item. The technologies were ranked for both the turbofan and turboprop applications.
Document ID
20040013222
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Gregory, Brent B.
(General Electric Aircraft Engines Lynn, MA, United States)
Eisenberg, Joseph D.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2003
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2003-212519
E-14081
Report Number: NASA/CR-2003-212519
Report Number: E-14081
Funding Number(s)
CONTRACT_GRANT: NAS3-CR-26617
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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