发明授权
- 专利标题: Cooling structure of gas turbine combustor
- 专利标题(中): 燃气轮机燃烧器的冷却结构
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申请号: US12598100申请日: 2008-09-24
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公开(公告)号: US08813502B2公开(公告)日: 2014-08-26
- 发明人: Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
- 申请人: Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
- 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
- 优先权: JP2007-247224 20070925
- 国际申请: PCT/JP2008/067188 WO 20080924
- 国际公布: WO2009/041435 WO 20090402
- 主分类号: F02C1/08
- IPC分类号: F02C1/08 ; F02G1/055 ; F02C7/12 ; F23R3/28 ; F23R3/00 ; F23R3/06
摘要:
It is required for a gas turbine combustor to exhaust low NOx. The gas turbine combustor is provided with a combustion tube which has a cooling passage through which cooling air flows in a double wall structure. The cooling passage has a main cooling air supply opening opened to a side of a combustion zone. The cooling air supplied from the main cooling air supply opening is guided to a direction along an inner wall surface of the combustion tube by a guide. The cooling air flows through the cooling passage inside the combustion tube, and then is reused for film cooling along the inner wall surface. Thus, it is possible to save cooling air. Therefore, a more part of the air supplied from a compressor can be used as air for combustion and it becomes possible to exhaust low NOx.
公开/授权文献
- US20100180601A1 COOLING STRUCTURE OF GAS TURBINE COMBUSTOR 公开/授权日:2010-07-22