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Materials for Advanced Turbine Engines: Power Metallurgy Rene 95 Rotating Turbine Engine Parts - Volume 1An attempt was made to improve methods for producing powder metallurgy aircraft gas turbine engine parts from the nickel base superalloy known as Rene 95. The parts produced were the high pressure turbine aft shaft for the CF6-50 engine and the stages 5 through 9 compressor disk forgings for the CFM56/F101 engines. A 50% cost reduction was achieved as compared to conventional cast and wrought processing practices. An integrated effort involving several powder producers and a major forging source were included.
Document ID
19800019998
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Pfouts, W. R.
(General Electric Co. Cincinnati, OH, United States)
Shamblen, C. E.
(General Electric Co. Cincinnati, OH, United States)
Mosier, J. S.
(General Electric Co. Cincinnati, OH, United States)
Peebles, R. E.
(General Electric Co. Cincinnati, OH, United States)
Gorsler, R. W.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1979
Subject Category
Metallic Materials
Report/Patent Number
NASA-CR-159802
R79AEG416-VOL-1
Report Number: NASA-CR-159802
Report Number: R79AEG416-VOL-1
Accession Number
80N28499
Funding Number(s)
CONTRACT_GRANT: NAS3-20074
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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