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Turboprop Cargo Aircraft Systems study, phase 1The effects of advanced propellers (propfan) on aircraft direct operating costs, fuel consumption, and noiseprints were determined. A comparison of three aircraft selected from the results with competitive turbofan aircraft shows that advanced turboprop aircraft offer these potential benefits, relative to advanced turbofan aircraft: 21 percent fuel saving, 26 percent higher fuel efficiency, 15 percent lower DOCs, and 25 percent shorter field lengths. Fuel consumption for the turboprop is nearly 40 percent less than for current commercial turbofan aircraft. Aircraft with both types of propulsion satisfy current federal noise regulations. Advanced turboprop aircraft have smaller noiseprints at 90 EPNdB than advanced turbofan aircraft, but large noiseprints at 70 and 80 EPNdB levels, which are usually suggested as quietness goals. Accelerated development of advanced turboprops is strongly recommended to permit early attainment of the potential fuel saving. Several areas of work are identified which may produce quieter turboprop aircraft.
Document ID
19810007526
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Muehlbauer, J. C.
(Lockheed-Georgia Co. Marietta, GA, United States)
Hewell, J. G., Jr.
(Lockheed-Georgia Co. Marietta, GA, United States)
Lindenbaum, S. P.
(Lockheed-Georgia Co. Marietta, GA, United States)
Randall, C. C.
(Lockheed-Georgia Co. Marietta, GA, United States)
Searle, N.
(Lockheed-Georgia Co. Marietta, GA, United States)
Stone, F. R., Jr.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-159355
LG80ER0112
Report Number: NASA-CR-159355
Report Number: LG80ER0112
Accession Number
81N16041
Funding Number(s)
CONTRACT_GRANT: NAS1-15708
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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