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CF6-6D engine performance deteriorationCruise cockpit recordings and test cell performance data in conjunction with hardware inspection data from airline overhaul shops were analyzed to define the extent and magnitude of performance deterioration of the General Electric CF6-6D model engine. These studies successfully isolated short-term deterioration from the longer term, and defined areas where a significant reduction in aircraft energy requirements for the 1980's can be realized. Unrestored losses which remain after engine refurbishment represent over 70% of the loss at engine shop visit. Sixty-three percent of the unrestored losses are cost-effective to restore which could reduce fuel consumed by CF6-6D engines in 1980 by 10.9 million gallons.
Document ID
19800018863
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wulf, R. H.
(General Electric Co. Cincinnati, OH, United States)
Kramer, W. H.
(General Electric Co. Cincinnati, OH, United States)
Pass, J. E.
(General Electric Co. Cincinnati, OH, United States)
Smith, J. J.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
R80AEG218
NASA-CR-159786
Report Number: R80AEG218
Report Number: NASA-CR-159786
Accession Number
80N27364
Funding Number(s)
CONTRACT_GRANT: NAS3-20631
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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