US Patent 11319822 Hybrid vane segment with ceramic matrix composite airfoils
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Patent Number
113198220
Date of Patent
May 3, 2022
0Patent Application Number
168681100
Date Filed
May 6, 2020
0Patent Primary Examiner
Edits on 26 Sep, 2022
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Patent Number
113198220
Date of Patent
May 3, 2022
0Patent Application Number
168681100
Date Filed
May 6, 2020
0Patent Primary Examiner
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US Patent 11319822 Hybrid vane segment with ceramic matrix composite airfoils
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A vane assembly for use with a gas turbine engine includes an outer wall, an inner wall, and a plurality of airfoils. The outer wall and the inner wall extend at least partway about an axis. At least one of the airfoils is coupled with the outer end wall and the inner end wall to transmit force loads through the vane assembly.
Infobox
Is a
Patent jurisdiction
Patent number
11319822
Date of patent
May 3, 2022
Patent application number
16868110
Date Filed
May 6, 2020
Patent primary examiner
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