US Patent 11261747 Ceramic matrix composite vane with added platform
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Patent abstract
A turbine vane assembly adapted for use in a gas turbine engine includes an aerofoil configured to interact with gases flowing through the gas turbine engine along a gas path, an outer platform that defines an outer boundary of a gas path, and an inner platform that defines an inner boundary of the gas path.
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Edward M. Jones0
Emma C. Steedman0
James C. Smith0
Michael J. Whittle0
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Patent Number
112617470
Date of Patent
March 1, 2022
0Patent Application Number
164151720
Date Filed
May 17, 2019
0Official Website
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US Patent 11261747 Ceramic matrix composite vane with added platform
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
11261747
Date of patent
March 1, 2022
Patent application number
16415172
Date Filed
May 17, 2019
Patent citations
Patent primary examiner
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