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US Patent 9587645 Airfoil blade

Patent 9587645 was granted and assigned to Pratt & Whitney Canada on March, 2017 by the United States Patent and Trademark Office.

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Patent abstract

A fan blade of a gas turbine engine, and a method of producing same, is disclosed which is composed of a core substrate and a nanocrystalline metal coating provided on at least a portion of the airfoil of the fan blade. The method includes the steps of providing a fan blade core having an airfoil and then applying a nanocrystalline metal coating over at least a portion of the fan blade core.

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