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NASA CF6 jet engine diagnostics program: Long-term CF6-6D low-pressure turbine deteriorationBack-to-back performance tests were run on seven airline low pressure turbine (LPT) modules and four new CF6-6D modules. Back-to-back test cell runs, in which an airline LPT module was directly compared to a new production module, were included. The resulting change, measured in fuel burn, equaled the level of LPT module deterioration. Three of the LPT modules were analytically inspected followed by a back-to-back test cell run to evaluate current refurbishment techniques.
Document ID
19790021020
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smith, J. J.
(General Electric Co. Evendale, OH, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1979
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-159618
R79AEG356
Report Number: NASA-CR-159618
Report Number: R79AEG356
Accession Number
79N29191
Funding Number(s)
CONTRACT_GRANT: NAS3-20631
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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