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US Patent 10718215 Airfoil with stepped spanwise thickness distribution
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Patent
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Current Assignee
Pratt & Whitney Canada
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Date Filed
November 9, 2017
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Date of Patent
July 21, 2020
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Patent Applicant
Pratt & Whitney Canada
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Patent Application Number
15808060
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Patent Citations
US Patent 10280756 Gas turbine engine airfoil
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US Patent 10233758 Detuning trailing edge compound lean contour
US Patent 10309236 Subsonic shock strut
Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
10718215
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Patent Primary Examiner
Woody A Lee, Jr.
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