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Stress relaxation of low pressure plasma-sprayed NiCrAlY alloysThe stress relaxation behavior of three NiCrAlY alloys that are commonly used as bond coats for thermal barrier coatings (TBCs) has been directly measured. The relaxation study was conducted at temperatures of 800-1000 C and over a wide range of stresses. It was established that all three bond coat alloys relaxed quite rapidly at temperatures of 900 C and above. Since the upper use temperatures for bond coats in gas turbine engines are between 900 and 1000 C, bond coat relaxation is expected to occur in service. Therefore, relaxation of the bond coat has the potential to affect TBC life. Furthermore, the relaxation differences observed between the three alloys offers a possible explanation for the differences in TBC life observed for these bond coats. While bond coat relaxation is expected to occur for a TBC in service, the mechanism for a relaxation effect on TBC life, if it exists, is yet to be determined.
Document ID
19930068873
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Brindley, W. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Whittenberger, J. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: Materials Science and Engineering, Part A - Structural Materials: Properties, Microstructures and Processing
ISSN: 0921-5093
Subject Category
Metallic Materials
Accession Number
93A52870
Distribution Limits
Public
Copyright
Other

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