US Patent 11230931 Inserts for airfoils of gas turbine engines
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Edits on 13 Dec, 2023
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Patent abstract
Baffle inserts for airfoils of gas turbine engines are described. The baffle inserts include a baffle insert body having a first side portion and a second side portion, wherein each side portion has a respective end, a first set of vortex generation elements is arranged at the end of the first side portion, and a second set of vortex generation elements is arranged at the end of the second side portion. The first set of vortex generation elements and the second set of vortex generation elements are arranged at an aft end of the baffle insert body.
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Patent Inventor Names
Dominic J. Mongillo, Jr.0
Lucas Dvorozniak0
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Official Website
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Patent Jurisdiction
Patent Number
112309310
Date of Patent
January 25, 2022
0Patent Application Number
169204960
Date Filed
July 3, 2020
0Official Website
Patent Citations
Patent Primary Examiner
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Edits on 27 Jan, 2022
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US Patent 11230931 Inserts for airfoils of gas turbine engines
Infobox
Is a
Patent jurisdiction
Patent number
11230931
Date of patent
January 25, 2022
Patent application number
16920496
Date Filed
July 3, 2020
Patent primary examiner
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