CPC F01D 5/288 (2013.01) [C09D 5/103 (2013.01); C09D 5/106 (2013.01); C09D 7/61 (2018.01); C09D 7/69 (2018.01); F01D 5/005 (2013.01); C08K 3/14 (2013.01); C08K 3/40 (2013.01); C08K 2201/009 (2013.01); C09D 5/04 (2013.01); C09D 5/08 (2013.01); C09D 5/082 (2013.01); F05D 2230/90 (2013.01); F05D 2260/95 (2013.01); F05D 2300/611 (2013.01)] | 12 Claims |
1. A coating composition for coating of a compressor blade or vane of a gas turbine, which the compressor blade or vane is exposed to a fluid stream of the gas turbine, the coating composition comprising:
anticorrosion pigments,
a thixotropic agent,
and
hard material particles,
wherein the coating composition comprises a 2k (two-component) room temperature curing coating composition comprising a paint base and a curing agent; and the coating composition is exposed to the fluid stream on the outermost layer of the compressor blade or vane.
|