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publicationDate 2011-01-06-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CA-2766493-A1
titleOfInvention Heat-protective coating for a turbine engine part, and method for producing same
abstract Thermal protection coating, in particular of a turbomachine part (12), deposited by thermal spraying on the surface of the part (12) and comprising at least 80% by volume of hollow micro-ceramic balls distributed in a metal alloy to nickel-cobalt base, which coating may be deposited on a metal alloy layer (22) and coated with a layer (26) for protection against erosion or against frictional wear or layer reflecting thermal radiation.
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