Invention Grant
- Patent Title: Gas turbine combustor and fuel supply method for same
- Patent Title (中): 燃气轮机燃烧器和燃油供应方法相同
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Application No.: US12498882Application Date: 2009-07-07
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Publication No.: US08393159B2Publication Date: 2013-03-12
- Inventor: Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
- Applicant: Shouhei Yoshida , Yoshitaka Hirata , Kazuyuki Itou , Tomoya Murota , Hiroshi Inoue , Tomohiro Asai
- Applicant Address: JP Tokyo
- Assignee: Hitachi, Ltd.
- Current Assignee: Hitachi, Ltd.
- Current Assignee Address: JP Tokyo
- Agency: Mattingly & Malur, PC
- Priority: JP2003-175030 20030619
- Main IPC: F23R3/12
- IPC: F23R3/12 ; F23R3/28

Abstract:
A gas turbine combustor for mixing fuel into combustion air introduced from a compressor, burning an air-fuel mixture, and supplying produced combustion gas to a gas turbine. The combustor has a liquid fuel nozzle for jetting out liquid fuel and a pre-mixture chamber wall having a hollow conical shape gradually spreading in the direction in which the fuel is jetted out from the liquid fuel nozzle, and defining a pre-mixture chamber therein. A plurality of gaseous fuel nozzles are disposed around the pre-mixture chamber wall in an opposing relation respectively to a plurality of air inlet holes bored through the pre-mixture chamber wall and jet out gaseous fuel substantially coaxially with the axes of the air inlet holes.
Public/Granted literature
- US20100000218A1 GAS TURBINE COMBUSTOR AND FUEL SUPPLY METHOD FOR SAME Public/Granted day:2010-01-07
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