- 专利标题: Gas turbine combustor
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申请号: US13539559申请日: 2012-07-02
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公开(公告)号: US08959919B2公开(公告)日: 2015-02-24
- 发明人: Shinji Akamatsu , Hiroaki Kishida , Kenji Sato , Kentaro Tokuyama , Keisuke Matsuyama , Takayoshi Takashima
- 申请人: Shinji Akamatsu , Hiroaki Kishida , Kenji Sato , Kentaro Tokuyama , Keisuke Matsuyama , Takayoshi Takashima
- 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: JP2011-151310 20110707
- 主分类号: F02C7/24
- IPC分类号: F02C7/24 ; F02C1/00 ; F02G3/00 ; F02C3/00 ; F23R3/00
摘要:
A gas turbine combustor is provided with a combustor basket where combustion gas flows, the combustion gas being produced by combustion of fuel injected from a nozzle, and a first resonance device and a second resonance device mounted on an outer surface of the combustor basket. The second resonance device is disposed on a downstream side from the first resonance device in a flow of the combustion gas and damps combustion oscillation of a frequency higher than the first resonance device. The first and second resonance devices are acoustic liners each having a housing mounted to the outer surface of the combustor basket. A resonance space surrounded by the housing and the outer surface of the combustor basket communicates with an interior space of the combustor basket via a plurality of acoustic holes formed in the combustor basket.
公开/授权文献
- US09003800B2 Gas turbine combustor 公开/授权日:2015-04-14
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