ANTI-ICE COATING FOR COMPRESSOR BLADES

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United States of America Patent

SERIAL NO

14636435

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Abstract

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The present invention relates to a composition for producing a coating for components of a turbomachine having anti-ice properties, wherein the composition comprises a binder which comprises at least one silicon-organic constituent, ceramic particles, boron nitride particles and a solvent and also polytetrafluoroethylene and/or graphite. The ceramic particles can have an average or maximum grain size of less than 4 μm and the boron nitride particles can have an average or maximum grain size of less than 12 μm. In addition, the present invention relates to a process for producing a coating by means of such a composition and also a coating produced in this way and a component provided therewith.

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Patent Owner(s)

Patent OwnerAddress
MTU AERO ENGINES AGDACHAUER STRASSE 665 MUNICH 80995

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
HEUSING, Melanie Rinteln, DE 2 0
LOPEZ, LAVERNIA Natividad Munich, DE 5 6
NIEGL, Max Munich, DE 11 22

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