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Highly loaded multi-stage fan drive turbine: Leaned stator configuration designThe results of the high lift blade configuration design study are reported. The three-stage constant-inside-diameter turbine utilizes a ten degree tangentially leaned stator in stage three. All other bladerows use plain blades. Analysis of the leaned stator is discussed, and detailed design data are summarized. Steady-state stresses are discussed, and the results of the mechanical design analysis are presented.
Document ID
19720021143
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Evans, D. C. (General Electric Co. Cincinnati, OH, United States)
Wolfmeyer, G. W. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1972
Publication Information
Publisher: NASA
Subject Category
Propulsion Systems
Report/Patent Number
R71AEG309
NASA-CR-2096
Report Number: R71AEG309
Report Number: NASA-CR-2096
Accession Number
72N28793
Funding Number(s)
CONTRACT_GRANT: NAS3-14304
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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