US Patent 10563522 Composite airfoil for a gas turbine engine
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Patent abstract
Stationary vanes and rotating blades of a gas turbine engine are disclosed that include airfoils formed from ceramic matrix composite materials. The airfoils include at least one layer of ceramic-containing matrix material and ceramic-containing reinforcing fibers suspended in the matrix material. A core of the airfoils is surrounded by the at least one layer of ceramic-containing fiber/matrix material.
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Patent Inventor Names
David J. Thomas0
Jeffrey A. Walston0
Ted J. Freeman0
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US Patent 10563522 Composite airfoil for a gas turbine engine
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Patent jurisdiction
Patent number
10563522
Date of patent
February 18, 2020
Patent application number
14797916
Date Filed
July 13, 2015
Patent primary examiner
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