Invention Grant
- Patent Title: Gas turbine and turbine blade for such a gas turbine
- Patent Title (中): 用于这种燃气轮机的燃气轮机和涡轮叶片
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Application No.: US14061018Application Date: 2013-10-23
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Publication No.: US09482094B2Publication Date: 2016-11-01
- Inventor: Sascha Justl , Carlos Simon-Delgado , Thomas Zierer , Sven Olmes
- Applicant: ALSTOM Technology Ltd
- Applicant Address: CH Baden
- Assignee: GENERAL ELECTRIC TECHNOLOGY GMBH
- Current Assignee: GENERAL ELECTRIC TECHNOLOGY GMBH
- Current Assignee Address: CH Baden
- Agency: Buchanan Ingersoll & Rooney PC
- Priority: EP12189577 20121023
- Main IPC: F01D5/08
- IPC: F01D5/08 ; F01D5/18

Abstract:
A gas turbine includes a rotor concentrically surrounded by a casing, with an annular hot gas channel axially extending between the rotor and the casing. The rotor includes a plurality of blades arranged annularly on the rotor. Each of the blades is mounted with a root in a respective axial slot on a rim of the rotor radially extending with an airfoil into the hot gas channel and adjoining with an axially oriented root surface to an annular rim cavity. A cooling device is provided at the root of each blade to receive cooling air injected into the rim cavity through stationary injectors. An optimized cooling is achieved by providing an essentially plane root surface and the cooling device includes a scoop for capturing and redirecting at least part of the injected cooling air, which scoop is a recess with respect to the root surface.
Public/Granted literature
- US20140112798A1 GAS TURBINE AND TURBINE BLADE FOR SUCH A GAS TURBINE Public/Granted day:2014-04-24
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