Invention Grant
- Patent Title: Turbine blade with trailing edge impingement cooling
- Patent Title (中): 涡轮叶片具有后缘冲击冷却
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Application No.: US12365396Application Date: 2009-02-04
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Publication No.: US08096768B1Publication Date: 2012-01-17
- 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 blade for an industrial gas turbine engine, the blade includes a squealer pocket formed by a pressure side tip rail and a suction side tip rail with tip cooling holes opening onto the tip floor in the trailing edge region, a tip corner and two impingement cooling air exit slots formed between the pressure side and the suction side tip rails and the tip corner. The cooling air flowing along the tip pocket flows out the exit slots as impingement jets and provide cooling for the tip corner to prevent an over-temperature that results in erosion.
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