Invention Grant
- Patent Title: Stator blade for a gas turbine and gas turbine having same
- Patent Title (中): 具有相同燃气轮机和燃气轮机的定子叶片
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Application No.: US12892423Application Date: 2010-09-28
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Publication No.: US08801366B2Publication Date: 2014-08-12
- Inventor: Roland Dueckershoff , Shailendra Naik , Martin Schnieder
- Applicant: Roland Dueckershoff , Shailendra Naik , Martin Schnieder
- Applicant Address: CH Baden
- Assignee: Alstom Technology Ltd.
- Current Assignee: Alstom Technology Ltd.
- Current Assignee Address: CH Baden
- Agency: Buchanan Ingersoll & Rooney PC
- Priority: CH469/08 20080328
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F01D9/04 ; F01D5/18

Abstract:
A stator blade for a gas turbine with sequential combustion, has a blade airfoil which extends in the radial direction between a blade tip and a shroud, with cooling passages extending inside the blade airfoil, through which a cooling medium can flow for cooling the blade and can then discharge from the stator blade into the hot gas flow flowing through the turbine. The blade airfoil has a sharply curved shape in space in the radial direction, and three cooling passages, which extend in the radial direction, arranged inside the blade airfoil in series in the hot gas flow direction and are interconnected by deflection regions, which are arranged at ends of the blade airfoil, so that the cooling medium flows through the cooling passages one after the other, with change of direction. The cooling passages follow the curvature of the blade airfoil in space in the radial direction.
Public/Granted literature
- US20110103932A1 STATOR BLADE FOR A GAS TURBINE AND GAS TURBINE HAVING SAME Public/Granted day:2011-05-05
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