Invention Grant
- Patent Title: Internally cooled turbine blade
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Application No.: US17651179Application Date: 2022-02-15
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Publication No.: US11885235B2Publication Date: 2024-01-30
- Inventor: Carlos Calixtro , Alex D. Wong , Yanhu Guo
- Applicant: Raytheon Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RTX CORPORATION
- Current Assignee: RTX CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Kinney & Lange, P. A.
- Main IPC: F01D5/18
- IPC: F01D5/18

Abstract:
An internally cooled turbine blade for use in a gas turbine engine includes a serpentine channel extending within the turbine blade for flowing cooling air through the interior of the blade. The turbine blade includes turbulators positioned within the serpentine channel to cause or increase turbulence of the cooling air flowing through the serpentine channel, increasing the heat transfer between the turbine blade and the cooling air before exiting a plurality of air outlets within the turbine blade.
Public/Granted literature
- US20230258090A1 INTERNALLY COOLED TURBINE BLADE Public/Granted day:2023-08-17
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