NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Small engine technology payoffs for future commuter aircraftHigh payoff technologies for a year 2000 regenerative cycle turboprop engine were identified for a 19 passenger commuter aircraft application. A series of engines incorporating eight levels of advanced technologies were studied and their impact on aircraft performance was evaluated. Four advanced technologies are recommended to achieve a potential reduction in fuel burn of 38.3 percent. At $1.00 per gallon fuel price, a potential direct operating cost (DOC) benefit of 12.5 percent is obtained. At $2.00 per gallon, the potential DOC benefit increases to 17.0 percent.
Document ID
19860057965
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaehler, H.
(Avco Lycoming Div. Stratford, CT, United States)
Schneider, W.
(Avco Lycoming Textron Stratford, CT, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 86-1544
Accession Number
86A42703
Funding Number(s)
CONTRACT_GRANT: NAS3-24545
Distribution Limits
Public
Copyright
Other

Available Downloads

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