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US Patent 11608748 Preform crossovers for composite airfoils
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Patent
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Date Filed
June 4, 2021
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Date of Patent
March 21, 2023
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Patent Application Number
17339198
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Patent Citations
US Patent 10408084 Vane assembly for a gas turbine engine
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US Patent 10458251 Airfoil cooling using non-line of sight holes
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US Patent 10465533 Ceramic matrix composite component and process of producing a ceramic matrix composite component
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US Patent 10724387 Continuation of a shear tube through a vane platform for structural support
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US Patent 10774005 Needled ceramic matrix composite cooling passages
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US Patent 10934854 CMC component cooling cavities
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US Patent 11286792 Ceramic matrix composite vane with cooling holes and methods of making the same
US Patent 11180999 Ceramic matrix composite component and method of producing a ceramic matrix composite component
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US Patent 11352887 Airfoil cooling using non-line of sight holes
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US Patent 10207471 Perforated ceramic matrix composite ply, ceramic matrix composite article, and method for forming ceramic matrix composite article
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•••
Patent Inventor Names
Tyler G. Vincent
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Howard J. Liles
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11608748
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Patent Primary Examiner
Topaz L. Elliott
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CPC Code
F01D 5/282
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F01D 5/187
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F01D 5/18
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F01D 5/186
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