发明授权
- 专利标题: Combustor of gas turbine with concentric swirler vanes
- 专利标题(中): 燃气轮机与同心旋流叶片的燃烧器
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申请号: US11334744申请日: 2006-01-19
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公开(公告)号: US07669421B2公开(公告)日: 2010-03-02
- 发明人: Keijiro Saitoh , Masataka Ohta , Satoshi Tanimura , Shigemi Mandai
- 申请人: Keijiro Saitoh , Masataka Ohta , Satoshi Tanimura , Shigemi Mandai
- 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: JP2005-124690 20050422
- 主分类号: F02C3/00
- IPC分类号: F02C3/00
摘要:
A gas turbine combustor having an inner tube and a transition pipe connected together is provided. The combustor includes an internal swirler and an external swirler. The internal swirler is composed of a cylindrical inward swirler ring disposed concentrically with respect to a central axis of the inner tube, and a plurality of inward swirler vanes provided on an outer peripheral surface of the inward swirler ring. The external swirler is composed of a cylindrical outward swirler ring disposed on an outer peripheral side of the inward swirler vanes and concentrically with respect to the inward swirler ring, and a plurality of outward swirler vanes provided on an outer peripheral surface of the outward swirler ring. The internal swirler and the external swirler are disposed within the inner tube.
公开/授权文献
- US20060236700A1 Combustor of gas turbine 公开/授权日:2006-10-26
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