- 专利标题: Gas turbine and gas turbine cooling method
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申请号: US11174555申请日: 2005-07-06
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公开(公告)号: US20060034685A1公开(公告)日: 2006-02-16
- 发明人: Nobuaki Kizuka , Shinya Marushima , Masami Noda , Shinichi Higuchi , Yasuhiro Horiuchi
- 申请人: Nobuaki Kizuka , Shinya Marushima , Masami Noda , Shinichi Higuchi , Yasuhiro Horiuchi
- 优先权: JP2004-200005 20040707
- 主分类号: F01D9/00
- IPC分类号: F01D9/00
摘要:
A gas turbine includes a nozzle vane and a sealing unit engaged with the nozzle vane inside a turbine supplied with combustion gases produced by mixing and burning air for combustion and fuel. The nozzle vane and the sealing unit are disposed in a channel of the downward flowing combustion gases on the outlet side of a gas path. A plurality of engagement portions between the sealing unit and the nozzle vane are provided successively from the upstream side toward the downstream side in a direction of flow of the combustion gases, and a downstream one of the plurality of engagement portions has a contact interface formed in a direction across a turbine rotary shaft. A reduction in the thermal efficiency of the gas turbine can be suppressed.
公开/授权文献
- US07507069B2 Gas turbine and gas turbine cooling method 公开/授权日:2009-03-24
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