Invention Grant
- Patent Title: Gas turbine combustor with a premixing burner having a reduced metal temperature by injecting air along a burner end face
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Application No.: US14018469Application Date: 2013-09-05
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Publication No.: US10041678B2Publication Date: 2018-08-07
- Inventor: Keisuke Miura , Satoshi Dodo , Tomomi Koganezawa , Yoshitaka Hirata , Kazuki Abe
- 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: JP2012-209073 20120924
- Main IPC: F23R3/28
- IPC: F23R3/28 ; F23R3/34 ; F23D14/82 ; F23R3/10

Abstract:
A combustor has at least one premixing burner for premixing fuel with air and jetting the mixed gas into a chamber for combustion. A cylinder attached to an outer circumferential portion of an end face of the burner is provided with air supply holes. An interval D1 defined between the adjacent air supply holes and an interval D2 defined between each air supply hole and the end face of the burner are each made narrower than the quenching distance in the premixed gas jetted from the premixing burner.
Public/Granted literature
- US20140083102A1 GAS TURBINE COMBUSTOR Public/Granted day:2014-03-27
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