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Creep fatigue life prediction for engine hot section materials (isotropic)A series of high temperature strain controlled fatigue tests have been completed to study the effects of thermomechanical fatigue, multiaxial loading, reactive environments, and imposed mean stresses. The baseline alloy used in these tests was cast B1900+Hf (with and without coatings); a small number of tests of wrought INCO 718 are also included. A strong path dependence was demonstrated during the thermomechanical fatigue testing, using in-phase, out-phase, and non-proportional (elliptical and 'dogleg') strain-temperature cycles. The multiaxial tests also demonstrated cycle path to be a significant variable, using both proportional and non-proportional tension-torsion loading. Environmental screening tests were conducted in moderate pressure oxygen and purified argon; the oxygen reduced the specimen lives by two, while the argon testing produced ambiguous data. Both NiCoCrAlY overlay and diffusion aluminide coatings were evaluated under isothermal and TMF conditions; in general, the lives of the coated specimens were higher that those of uncoated specimens. Controlled mean stress TMF tests showed that small mean stress changes could change initiation lives by orders of magnitude; these results are not conservatively predicted using traditional linear damage summation rules. Microstructures were evaluated using optical, SEM and TEM methods.
Document ID
19930011063
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nelson, R. S.
(United Technologies Corp. East Hartford, CT, United States)
Levan, G. W.
(United Technologies Corp. East Hartford, CT, United States)
Schoendorf, J. F.
(United Technologies Corp. East Hartford, CT, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PWA-5894
NASA-CR-189220
NAS 1.26:189220
Report Number: PWA-5894
Report Number: NASA-CR-189220
Report Number: NAS 1.26:189220
Accession Number
93N20252
Funding Number(s)
CONTRACT_GRANT: NAS3-23288
PROJECT: RTOP 590-21-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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