Invention Grant
US07766616B2 Turbine blade for a gas turbine, use of a turbine blade and method for cooling a turbine blade
有权
用于燃气轮机的涡轮叶片,涡轮叶片的使用和用于冷却涡轮叶片的方法
- Patent Title: Turbine blade for a gas turbine, use of a turbine blade and method for cooling a turbine blade
- Patent Title (中): 用于燃气轮机的涡轮叶片,涡轮叶片的使用和用于冷却涡轮叶片的方法
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Application No.: US11791095Application Date: 2005-11-07
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Publication No.: US07766616B2Publication Date: 2010-08-03
- Inventor: Stefan Baldauf , Michael Händler , Christian Lerner
- Applicant: Stefan Baldauf , Michael Händler , Christian Lerner
- Applicant Address: DE Munich
- Assignee: Siemens Aktiengesellschaft
- Current Assignee: Siemens Aktiengesellschaft
- Current Assignee Address: DE Munich
- Priority: EP04027789 20041123
- International Application: PCT/EP2005/055779 WO 20051107
- International Announcement: WO2006/056525 WO 20060601
- Main IPC: F01D5/08
- IPC: F01D5/08

Abstract:
There is described a turbine blade of a gas turbine comprising a suction-side blade wall and a pressure-side blade wall that, in the trailing edge area, runs toward the suction-side blade wall. This suction-side blade wall has a trailing edge projection projecting over the end edge of the pressure-side blade wall at least in a partial section of the trailing edge area. A turbine blade of the aforementioned type is designed for a particularly long serviceable life while requiring little cooling air. To this end, the pressure-side surface of the trailing edge projection has a number of trough-shaped recesses that increase the transfer of heat from the trailing edge projection by a local swirling of the cooling air.
Public/Granted literature
- US20080124225A1 Turbine Blade for a Gas Turbine, Use of a Turbine Blade and Method for Cooling a Turbine Blade Public/Granted day:2008-05-29
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