Invention Grant
US09395085B2 Communicating structure between adjacent combustors and turbine portion and gas turbine
有权
相邻燃烧器与涡轮机部分和燃气轮机之间的通信结构
- Patent Title: Communicating structure between adjacent combustors and turbine portion and gas turbine
- Patent Title (中): 相邻燃烧器与涡轮机部分和燃气轮机之间的通信结构
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Application No.: US13500009Application Date: 2010-05-14
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Publication No.: US09395085B2Publication Date: 2016-07-19
- Inventor: Rosic Budmir , Yasuro Sakamoto , Sumiu Uchida , Eisaku Ito , Tsuyoshi Kitamura , Satoshi Hada , Sosuke Nakamura
- Applicant: Rosic Budmir , Yasuro Sakamoto , Sumiu Uchida , Eisaku Ito , Tsuyoshi Kitamura , Satoshi Hada , Sosuke Nakamura
- Applicant Address: JP Yokohama-shi
- Assignee: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- Current Assignee: MITSUBISHI HITACHI POWER SYSTEMS, LTD.
- Current Assignee Address: JP Yokohama-shi
- Agency: Westerman, Hattori, Daniels & Adrian, LLP
- Priority: JP2009-277746 20091207
- International Application: PCT/JP2010/058171 WO 20100514
- International Announcement: WO2011/070806 WO 20110616
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F23R3/60 ; F01D9/06 ; F23R3/34

Abstract:
In a communicating structure between combustors that generates combustion gas inside pipe pieces and a turbine portion that generates a rotational driving force by making the combustion gas sequentially pass through a turbine stage formed of turbine stator vanes and turbine rotor blades, at least some of the first-stage turbine stator vanes closest to the combustor among the turbine stator vanes are disposed downstream of sidewalls of one pipe piece and another pipe piece that are adjacent to each other, and the distance from leading edges of the first-stage turbine stator vanes disposed downstream of the sidewalls of the pipe pieces to end portions of the sidewalls closer to the turbine portion is equal to or less than a spacing between an internal surface of the sidewall of the one pipe piece and an internal surface of the sidewall of the other pipe piece.
Public/Granted literature
- US20120247125A1 COMMUNICATING STRUCTURE BETWEEN COMBUSTOR AND TURBINE PORTION AND GAS TURBINE Public/Granted day:2012-10-04
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