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Fracture control of H-O engine componentsAn investigation was made to obtain the material characterization and fatigue crack propagation data necessary to establish the salient characteristics of a Ti-6Al-2.5Sn(ELI) alloy fuel pump impeller to be used in a cryogenic service environment. Testing variables considered were: coupon orientation, frequency, load range ratio, and temperature. Data analysis correlated crack propagation data from conventional laboratory coupons with data from a parallel sided rotating disk used to model rotor stresses. Four major design recommendations when bore regions of fuel pump impellers to be operated in cryogenic environments are to be relatively highly stressed are discussed.
Document ID
19770013263
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ryder, J. T.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1977
Subject Category
Metallic Materials
Report/Patent Number
LR-27810
NASA-CR-135137
Report Number: LR-27810
Report Number: NASA-CR-135137
Accession Number
77N20207
Funding Number(s)
CONTRACT_GRANT: NAS3-18896
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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