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US Patent 10024172 Gas turbine engine airfoil

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Patent abstract

An airfoil includes an airfoil wall including an exterior airfoil surface and at least partially defines an airfoil cavity. A fillet is on the exterior airfoil surface. A recess is in an interior surface of the airfoil wall adjacent the fillet. A baffle tube is located in the airfoil cavity spaced from the recess.

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Patent citations received
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US Patent 11396819 Components for gas turbine engines
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US Patent 11248470 Airfoil with core cavity that extends into platform shelf
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US Patent 11021966 Vane core assemblies and methods
Edits on 31 Jan, 2022
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US Patent 10526894 Short inlet with low solidity fan exit guide vane arrangements
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 US Patent 10024172 Gas turbine engine airfoil

Infobox
Is a
Patent
Patent
Patent applicant
United Technologies
United Technologies
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
10024172
Date of patent
July 17, 2018
Patent application number
14634006
Date Filed
February 27, 2015
Patent primary examiner
‌
Jason Shanske

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