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Low speed propellers: Impact of advanced technologiesSensitivity studies performed to evaluate the potential of several advanced technological elements on propeller performance, noise, weight, and cost for general aviation aircraft are discussed. Studies indicate that the application of advanced technologies to general aviation propellers can reduce fuel consumption in future aircraft an average of ten percent, meeting current regulatory noise limits. Through the use of composite blade construction, up to 25 percent propeller weight reduction can be achieved. This weight reduction in addition to seven percent propeller efficiency improvements through application of advanced technologies result in four percent reduction in direct operating costs, ten percent reduction in aircraft acquisition cost, and seven percent lower gross weight for general aviation aircraft.
Document ID
19800013855
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Keiter, I. D.
(Cessna Aircraft Co. Wichita, KS, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1980
Publication Information
Publication: NASA. Lewis Res. Center Gen. Aviation Propulsion
Subject Category
Aircraft Propulsion And Power
Accession Number
80N22342
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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