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Home › Method for producing a gas turbine component which is to be coated, with exposed holes, device for carrying out the method, and coatable turbine blade with film cooling holes

Method for producing a gas turbine component which is to be coated, with exposed holes, device for carrying out the method, and coatable turbine blade with film cooling holes

US Patent 8414264 · Granted Apr 9, 2013

Estimated economic value: $699,000 ⓘ

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