发明授权
- 专利标题： Gas flow path for a gas turbine engine
- 专利标题（中）： 燃气涡轮发动机的气体流路
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申请号： US14185352申请日： 2014-02-20
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公开(公告)号： US09593853B2公开(公告)日： 2017-03-14
- 发明人: Matthew D. Montgomery , Richard C. Charron , Gary D. Snyder , William W. Pankey , Clinton A. Mayer , Benjamin G. Hettinger
- 申请人： Siemens Energy, Inc.
- 申请人地址： US FL Orlando
- 专利权人： SIEMENS ENERGY, INC.
- 当前专利权人： SIEMENS ENERGY, INC.
- 当前专利权人地址： US FL Orlando
- 主分类号： F23R3/46
- IPC分类号： F23R3/46
摘要：
A duct arrangement in a can annular gas turbine engine. The gas turbine engine has a gas delivery structure for delivering gases from a plurality of combustors to an annular chamber that extends circumferentially and is oriented concentric to a gas turbine engine longitudinal axis for delivering the gas flow to a first row of blades A gas flow path is formed by the duct arrangement between a respective combustor and the annular chamber for conveying gases from each combustor to the first row of turbine blades The duct arrangement includes at least one straight section having a centerline that is misaligned with a centerline of the combustor.
公开/授权文献
- US20150233582A1 GAS FLOW PATH FOR A GAS TURBINE ENGINE 公开/授权日：2015-08-20
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