Invention Grant
- Patent Title: Gas turbine engine component with a cooling circuit having a flared base
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Application No.: US16239949Application Date: 2019-01-04
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Publication No.: US10815792B2Publication Date: 2020-10-27
- Inventor: James Tilsley Auxier , Jeffrey T. Morton , Matthew S. Gleiner , Parth Jariwala , Charles Thistle , Megan J. Kwolek
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D25/12
Abstract:
A component for a gas turbine engine includes a body portion that extends between a leading edge and a trailing edge of the component. The trailing edge includes a flared region and a non-flared region. At least one discharge slot is disposed at least partially within the flared region of the component.
Public/Granted literature
- US20200217208A1 GAS TURBINE ENGINE COMPONENT WITH DISCHARGE SLOT HAVING A FLARED BASE Public/Granted day:2020-07-09
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