Invention Grant
- Patent Title: Splayed tip features for gas turbine engine airfoil
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Application No.: US16239689Application Date: 2019-01-04
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Publication No.: US11268387B2Publication Date: 2022-03-08
- Inventor: San Quach , Tracy A. Propheter-Hinckley , Dominic J. Mongillo, Jr. , Steven Bruce Gautschi
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Bachman & LaPointe, P.C.
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D5/14 ; B22C9/10 ; F01D5/28
Abstract:
A component for a gas turbine engine includes a trailing edge tip corner that at least partially defines a trailing edge cavity and a multiple of corner features within the trailing edge cavity, the multiple of corner features splayed along the trailing edge tip corner.
Public/Granted literature
- US20200024957A1 SPLAYED TIP FEATURES FOR GAS TURBINE ENGINE AIRFOIL Public/Granted day:2020-01-23
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