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Burner Rig Evaluation of Thermal Barrier Coating Systems for Nickel-Base AlloysEight plasma sprayed bond coatings were evaluated for their potential use with ZrO2-Y2O3 thermal barrier coatings (TECs) which are being developed for coal derived fuel fired gas turbines. Longer TBC lives in cyclic burner rig oxidation to 1050 C were achieved with the more oxidation resistant bond coatings. These were Ni-14.1Cr-13.4A1-0.10Ar, Ni-14.1C4-14.4Al-0.16Y, and Ni-15.8Cr-12.8Al-0.36Y on Rene 41. The TBC systems performed best when 0.015-cm thick bond coatings were employed that were sprayed at 20 kW using argon 3.5v/o hydrogen. Cycling had a more life limiting influence on the TBC than accumulated time at 1050 C.
Document ID
19810019693
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Authors
Gedwill, M. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1981
Subject Category
Metallic Materials
Report/Patent Number
E-712
NASA-TM-81684
DOE/NASA/2593-26
Report Number: E-712
Report Number: NASA-TM-81684
Report Number: DOE/NASA/2593-26
Accession Number
81N28231
Funding Number(s)
PROJECT: RTOP 778-11-08
CONTRACT_GRANT: EF-77-A-01-2593
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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