Invention Grant
- Patent Title: Gas turbine engine article with cooling holes for mitigating recession
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Application No.: US17970662Application Date: 2022-10-21
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Publication No.: US11959396B2Publication Date: 2024-04-16
- Inventor: Thomas J. Martin , Gajawalli V. Srinivasan , Paul F. Croteau , Matthew B. Kennedy
- Applicant: RAYTHEON TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: RTX CORPORATION
- Current Assignee: RTX CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F23R3/00

Abstract:
A gas turbine engine article includes a silicon-containing ceramic wall that has an external combustion gaspath side and an internal side that borders a cooling air cavity. The external combustion gaspath side has an associated combustion gas flow direction there along. An array of cooling holes extends through the silicon-containing ceramic wall and connects the internal side with the external combustion gaspath side. The cooling holes are oriented to discharge cooling air to the external gaspath side in a direction counter to the combustion gas flow direction.
Public/Granted literature
- US20230212949A1 GAS TURBINE ENGINE ARTICLE WITH COOLING HOLES FOR MITIGATING RECESSION Public/Granted day:2023-07-06
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