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Preliminary study of creep thresholds and thermomechanical response in Haynes 188 at temperatures in the range 649 to 871 CThe following conclusions were drawn from this study of creep thresholds and thermomechanical response: (1) creep threshold can be determined using the latest electrohydraulic test equipment, providing that test durations are short and relatively large accumulations of creep strain are used in defining the threshold; (2) significant creep strains were measured under monotonic loading as stress levels as low as 4 ksi at temperatures predicted for solar receiver service; and (3) the material exhibited creep ratchetting during simulated service cycles, a result not predicted by analysis using current constitutive models for Haynes 188.
Document ID
19890007956
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ellis, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Bartolotta, P. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Mladsi, S. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: Turbine Engine Hot Section Technology, 1987
Subject Category
Structural Mechanics
Accession Number
89N17327
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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