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Long-term CF6 engine performance deterioration: Evaluation of engine S/N 451-380The performance testing and analytical teardown of CF6-6D engine serial number 451-380 which was recently removed from a DC-10 aircraft is summarized. The investigative test program was conducted inbound prior to normal overhaul/refurbishment. The performance testing included an inbound test, a test following cleaning of the low pressure turbine airfoils, and a final test after leading edge rework and cleaning the stage one fan blades. The analytical teardown consisted of detailed disassembly inspection measurements and airfoil surface finish checks of the as-received deteriorated hardware. Aspects discussed include the analysis of the test cell performance data, a complete analytical teardown report with a detailed description of all observed hardware distress, and an analytical assessment of the performance loss (deterioration) relating measured hardware conditions to losses in both specific fuel comsumption and exhaust gas temperature.
Document ID
19780021160
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kramer, W. H.
(General Electric Co. Cincinnati, OH, United States)
Smith, J. J.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-159390
Accession Number
78N29103
Funding Number(s)
CONTRACT_GRANT: NAS3-20631
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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