发明授权
- 专利标题: Gas turbine and cooling air supply structure thereof
- 专利标题(中): 燃气轮机及其冷却空气供应结构
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申请号: US12164793申请日: 2008-06-30
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公开(公告)号: US08079803B2公开(公告)日: 2011-12-20
- 发明人: Keita Takamura , Shinya Hashimoto , Masanori Yuri
- 申请人: Keita Takamura , Shinya Hashimoto , Masanori Yuri
- 申请人地址: JP Tokyo
- 专利权人: Mitsubishi Heavy Industries, Ltd.
- 当前专利权人: Mitsubishi Heavy Industries, Ltd.
- 当前专利权人地址: JP Tokyo
- 代理机构: Westerman, Hattori, Daniels & Adrian, LLP
- 主分类号: F01D5/14
- IPC分类号: F01D5/14 ; F03D11/00 ; F04D29/38
摘要:
The present invention includes an introducing passage that is provided within a turbine stationary blade fixed within a turbine casing and that communicates an interior of the turbine casing with an exterior thereof; a nozzle that is provided in an inner circumference of the turbine stationary blade in a manner that the nozzle communicates with the introducing passage and that includes an outlet facing the opening of the rotor cavity and a swirler at the outlet; and a pressurizing passage that communicates a cooling passage with a rotor cavity. In this arrangement, the outlet of the nozzle and the connecting opening of the pressurizing passage are arranged so that distances of the outlet and of the connecting opening from the central axis line in the radial direction of the rotor are the same distance r.
公开/授权文献
- US20090324388A1 GAS TURBINE AND COOLING AIR SUPPLY STRUCTURE THEREOF 公开/授权日:2009-12-31
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