NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Small Engine Component Technology (SECT) study. Program reportThe study was conducted to identify high payoff technologies for year 2000 small gas turbine applications and to provide a technology plan for guiding future research and technology efforts. A regenerative cycle turboprop engine was selected 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. The study indicated a potential reduction in fuel burn of 38.3 percent. At $1.00 per gallon fuel price, a potential DOC benefit of 12.5 percent would be achieved. At $2.00 per gallon, the potential DOC benefit would increase to 17.0 percent. Four advanced technologies are recommended and appropriate research and technology programs were established to reach the year 2000 goals.
Document ID
19910014891
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Almodovar, E.
(Avco Lycoming Div. Stratford, CT, United States)
Exley, T.
(Avco Lycoming Div. Stratford, CT, United States)
Kaehler, H.
(Avco Lycoming Div. Stratford, CT, United States)
Schneider, W.
(Avco Lycoming Div. Stratford, CT, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:175077
AVSCOM-TR-86-C-12
LYC-86-11
NASA-CR-175077
Report Number: NAS 1.26:175077
Report Number: AVSCOM-TR-86-C-12
Report Number: LYC-86-11
Report Number: NASA-CR-175077
Accession Number
91N24204
Funding Number(s)
PROJECT: DA PROJ. 1L1-61101-AH-45
PROJECT: RTOP 535-05-01
CONTRACT_GRANT: NAS3-24545
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available