Invention Grant
- Patent Title: Turbine airfoil with minicore passage having sloped diffuser orifice
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Application No.: US16373008Application Date: 2019-04-02
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Publication No.: US10968752B2Publication Date: 2021-04-06
- Inventor: James Tilsley Auxier , Tracy A. Propheter-Hinckley , Allan N. Arisi
- Applicant: RAYTHEON 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

Abstract:
A turbine airfoil includes an airfoil outer wall that defines leading and trailing ends and first and second sides that join the leading and trailing ends. At least one cooling passage is embedded in the airfoil outer wall and has a radially-elongated entrance manifold, a radially-elongated diffuser orifice that opens to an exterior surface of the airfoil outer wall, and a bank of sub-passages fluidly connecting the radially-elongated entrance manifold with the radially-elongated diffuser orifice. The radially-elongated diffuser orifice is sloped relative to the radially-elongated entrance manifold.
Public/Granted literature
- US20190383147A1 TURBINE AIRFOIL WITH MINICORE PASSAGE HAVING SLOPED DIFFUSER ORIFICE Public/Granted day:2019-12-19
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