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The CF6 jet engine performance improvement: New front mountThe New Front Mount was evaluated in component tests including stress, deflection/distortion and fatigue tests. The test results demonstrated a performance improvement of 0.1% in cruise sfc, 16% in compressor stall margin and 10% in compressor stator angle margin. The New Front Mount hardware successfully completed 35,000 simulated flight cycles endurance testing.
Document ID
19800005870
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fasching, W. A.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-159639
R79AEG366
Accession Number
80N14127
Funding Number(s)
CONTRACT_GRANT: NAS3-20629
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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