Invention Grant
- Patent Title: Internally cooled airfoil
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Application No.: US16675879Application Date: 2019-11-06
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Publication No.: US10830054B2Publication Date: 2020-11-10
- Inventor: James T. Auxier , Parth Jariwala , Bret M. Teller
- 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: Snell & Wilmer L.L.P.
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D9/02 ; F01D11/08 ; F01D25/12 ; F23R3/00

Abstract:
A casting core may comprise a tip flag material having a forward cavity and a first spear cavity disposed aft of the forward cavity. A trailing edge discharge material may be separated from the tip flag material and include a first row of cavities. The first row of cavities may comprise a first racetrack cavity. A second row of cavities may be disposed aft of the first row of cavities and include a second racetrack cavity. A third row of cavities may be disposed aft of the second row of cavities and include a circular cavity. A fourth row of cavities may be disposed aft of the third row of cavities and include a second spear cavity.
Public/Granted literature
- US20200088042A1 INTERNALLY COOLED AIRFOIL Public/Granted day:2020-03-19
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