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US Patent 10975710 Cooling circuit for gas turbine engine component
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Patent
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Date Filed
December 5, 2018
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Date of Patent
April 13, 2021
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Patent Application Number
16210393
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Patent Citations
US Patent 10208603 Staggered crossovers for airfoils
US Patent 10196901 Cooling of engine components
US Patent 10641103 Trailing edge configuration with cast slots and drilled filmholes
US Patent 10145246 Staggered crossovers for airfoils
US Patent 10190420 Flared crossovers for airfoils
Patent Inventor Names
Dominic Mongillo
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Allan N. Arisi
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Brandon W. Spangler
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
10975710
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Patent Primary Examiner
Eldon T Brockman
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