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The Rene 150 directionally solidified superalloy turbine blades, volume 1Turbine blade design and analysis, preliminary Rene 150 system refinement, coating adaptation and evaluation, final Rene 150 system refinement, component-test blade production and evaluation, engine-test blade production, and engine test are discussed.
Document ID
19830012675
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Deboer, G. J. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-167992
R82AEB540-VOL-1
NAS 1.26:167992
Report Number: NASA-CR-167992
Report Number: R82AEB540-VOL-1
Report Number: NAS 1.26:167992
Accession Number
83N20946
Funding Number(s)
CONTRACT_GRANT: NAS3-20074
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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