Invention Grant
- Patent Title: Gas turbine combustor
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Application No.: US14818006Application Date: 2015-08-04
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Publication No.: US10041680B2Publication Date: 2018-08-07
- Inventor: Tomohiro Asai , Akinori Hayashi , Yasuhiro Akiyama
- Applicant: Mitsubishi Hitachi Power Systems, Ltd.
- Applicant Address: JP Yokohama
- Assignee: Mitsubishi Hitachi Power Systems, Ltd.
- Current Assignee: Mitsubishi Hitachi Power Systems, Ltd.
- Current Assignee Address: JP Yokohama
- Agency: Crowell & Moring LLP
- Priority: JP2014-159330 20140805
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23R3/00 ; F23R3/10 ; F23R3/34 ; F23R3/60

Abstract:
A gas turbine combustor of the present invention includes a cylindrical combustor liner, a cylindrical combustion chamber inside the combustor liner, and a burner that includes a plurality of fuel nozzles for injecting the gas fuel into the combustion chamber and an air hole plate with a plurality of air holes for guiding the compressed air into the combustion chamber. The air hole plate joins the combustor liner and is disposed between the fuel nozzles and the combustion chamber. The junction between the air hole plate and the combustor liner is provided with an inclined component which covers the junction and has a connecting surface connecting the air hole plate and the combustor liner.
Public/Granted literature
- US20160040883A1 Gas Turbine Combustor Public/Granted day:2016-02-11
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