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Notched fatigue of single crystal PWA 1480 at turbine attachment temperaturesThe focus is on the lower temperature, uncoated and notched features of gas turbine blades. Constitutive and fatigue life prediction models applicable to these regions are being developed. Fatigue results are presented which were obtained thus far. Fatigue tests are being conducted on PWA 1480 single crystal material using smooth strain controlled specimens and three different notched specimens. Isothermal fatigue tests were conducted at 1200, 1400, and 1600 F. The bulk of the tests were conducted at 1200 F. The strain controlled tests were conducted at 0.4 percent per second strain rate and the notched tests were cycled at 1.0 cycle per second. A clear orientation dependence is observed in the smooth strain controlled fatigue results. The fatigue lifes of the thin, mild notched specimens agree fairly well with this smooth data when elastic stress range is used as a correlating parameter. Finite element analyses were used to calculate notch stresses. Fatigue testing will continue to further explore the trends observed thus far. Constitutive and life prediction models are being developed.
Document ID
19910014997
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Meyer, T. G.
(United Technologies Research Center East Hartford, CT., United States)
Nissley, D. M.
(Pratt and Whitney Aircraft East Hartford, CT., United States)
Swanson, G. A.
(Pratt and Whitney Aircraft East Hartford, CT., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1989
Publication Information
Publication: NASA. Lewis Research Center, Structural Integrity and Durability of Reusable Space Propulsion Systems
Subject Category
Structural Mechanics
Accession Number
91N24310
Funding Number(s)
CONTRACT_GRANT: NAS3-23939
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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