NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Prop-fan propulsion - Its status and potentialStudies have established that advanced turboprop (prop-fan) equipped aircraft will reduce fuel consumption by 15 to 30 percent compared to aircraft equipped with high-bypass turbofan engines of equivalent technology. A reduction in direct operating costs of approximately 10 percent has been identified for commercial aircraft as well as approximately 20 percent lower gross weight airplane for long endurance military missions. The prop-fan propulsion system is being investigated as part of the NASA Aircraft Energy Efficiency program which includes both analytical studies and experimental tests. The experimental work encompasses performance and acoustic wind tunnel tests on several prop-fan models. The prop-fan technology status is reviewed in the major areas of performance, installed effects, cabin noise, blade structure and maintenance cost. Also, further activities required to complete the technical validation of prop-fans are described.
Document ID
19790041867
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dugan, J. F., Jr.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Gatzen, B. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Adamson, W. M.
(United Technologies Corp. Hartford, Conn., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
SAE PAPER 780995
Report Number: SAE PAPER 780995
Meeting Information
Meeting: Society of Automotive Engineers, Aerospace Meeting
Location: San Diego, CA
Start Date: November 27, 1978
End Date: November 30, 1978
Sponsors: Society of Automotive Engineers
Accession Number
79A25880
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available