Invention Grant
- Patent Title: Turbine vane with impingement cooling insert
- Patent Title (中): 带有冲击冷却插件的涡轮叶片
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Application No.: US13049371Application Date: 2011-03-16
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Publication No.: US08777569B1Publication Date: 2014-07-15
- Inventor: George Liang
- Applicant: George Liang
- Applicant Address: US FL Jupiter
- Assignee: Florida Turbine Technologies, Inc.
- Current Assignee: Florida Turbine Technologies, Inc.
- Current Assignee Address: US FL Jupiter
- Agent John Ryznic
- Main IPC: F01D5/08
- IPC: F01D5/08 ; F01D5/18

Abstract:
A turbine stator vane with cooling air cavities each having an impingement cooling insert secured therein, and an impingement cooling insert secured within each cavity. A leading edge impingement insert and a mid-chord impingement insert have a section on the pressure side wall with impingement holes forming a parallel flow of impingement cooling air and a section on the suction side wall with a sinusoidal shaped piece that forms a series of impingement cooling holes that produces impingement cooling on cooler surfaces of the airfoil but with less cooling air flow.
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