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Plasma sprayed ceramic thermal barrier coatings for turbine vane platformsThe paper describes the results to date of an investigation of advanced plasma sprayed ceramic coatings to demonstrate cooling concepts applicable for turbine vane platforms. It is noted that the increased resistance of plasma sprayed ceramic coatings to cyclic thermal exposure can be achieved by increasing the strain tolerance of the ceramic and by controlling harmful residual stresses. Strain tolerance can be increased by controlling internal structure to minimize harmful flaws and to add favorable discontinuities.
Document ID
19800055466
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ruckle, D. L.
(United Technologies Corp. Pratt and Whitney Aircraft Group, East Hartford, Conn., United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1980
Subject Category
Nonmetallic Materials
Meeting Information
Meeting: International Conference on Metallurgical Coatings
Location: San Diego, CA
Start Date: April 21, 1980
End Date: April 25, 1980
Sponsors: American Vacuum Society
Accession Number
80A39636
Funding Number(s)
CONTRACT_GRANT: NAS-20630
Distribution Limits
Public
Copyright
Other

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