发明授权
- 专利标题： Gas turbine combustor
- 专利标题（中）： 燃气轮机燃烧器
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申请号： US10927529申请日： 2004-08-27
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公开(公告)号： US07089741B2公开(公告)日： 2006-08-15
- 发明人: Kazufumi Ikeda , Tatsuo Ishiguro , Katsunori Tanaka , Satoshi Tanimura
- 申请人： Kazufumi Ikeda , Tatsuo Ishiguro , Katsunori Tanaka , Satoshi Tanimura
- 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： Kanesaka Berner & Partners, LLP
- 优先权： JP2003-308062 20030829
- 主分类号： F02C7/24
- IPC分类号： F02C7/24
摘要：
A gas turbine combustor includes a combustion liner in which a combustion region is formed; and a housing provided for a wall of the combustion liner in a predetermined circumferential region of the combustion liner to form a resonance space between the combustion liner and the housing. The combustion region and the resonance space are connected by a plurality of combustion liner through-holes, and a circumferential length of the housing is longer than a diameter of the combustion liner.
公开/授权文献
- US20050097890A1 Gas turbine combustor 公开/授权日：2005-05-12
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