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T. Cosack
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Proceedings Papers
ITSC1999, Thermal Spray 1999: Proceedings from the United Thermal Spray Conference, 542-545, March 17–19, 1999,
Abstract
View Papertitled, Weiterentwickelte Gebrauchseigenschaften an Wärmedämmschichten (Enhanced Properties of Thermal Barrier Coatings)
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for content titled, Weiterentwickelte Gebrauchseigenschaften an Wärmedämmschichten (Enhanced Properties of Thermal Barrier Coatings)
The application of thermal barrier coatings is increasing in aeroengines. The service life of turbine components could be improved by optimized structures of the zirconia top coating. The thermal barrier coatings on turbine blades were tested in a hot gas thermal shock test. Up to 6500 thermal cycles until first spallation a plasma sprayed ceramic thermal barrier coatings can be very well compared with the service life of EB-PVD thermal barrier coatings with 8000 - 9000 thermal cycles until first spallation. Paper text in German.