US Patent 10954802 Turbine section assembly with ceramic matrix composite vane
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A turbine assembly adapted for use in a gas turbine engine with a turbine vane comprising ceramic matrix composite materials. The turbine vane is configured to redirect air moving through a primary gas path of the gas turbine engine. The turbine assembly includes a vane-stage support for holding the turbine vane in place relative to a turbine case.
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Patent Number
109548020
Date of Patent
March 23, 2021
0Patent Application Number
163918110
Date Filed
April 23, 2019
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Patent Number
109548020
Date of Patent
March 23, 2021
0Patent Application Number
163918110
Date Filed
April 23, 2019
0Official Website
Patent Citations
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US Patent 10954802 Turbine section assembly with ceramic matrix composite vane
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
10954802
Date of patent
March 23, 2021
Patent application number
16391811
Date Filed
April 23, 2019
Patent citations
Patent primary examiner
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