Invention Grant
- Patent Title: Combustion burner, combustor, and gas turbine having a swirl vane with opposite directed surfaces
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Application No.: US14897814Application Date: 2015-01-23
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Publication No.: US10240791B2Publication Date: 2019-03-26
- Inventor: Naonori Nagai , Katsuyoshi Tada , Kei Inoue , Keijiro Saito
- Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Applicant Address: JP Tokyo
- Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Current Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.
- Current Assignee Address: JP Tokyo
- Agency: Wenderoth, Lind & Ponack, L.L.P.
- Priority: JP2014-192017 20140919
- International Application: PCT/JP2015/051797 WO 20150123
- International Announcement: WO2016/042787 WO 20160324
- Main IPC: F23R3/14
- IPC: F23R3/14 ; F23R3/28 ; F02C7/22 ; F23D11/10 ; F23R3/00

Abstract:
A combustion burner includes a nozzle and a swirl vane disposed in an axial flow path extending along an axial direction of the nozzle. The swirl vane includes a tip portion for swirling gas, the gas flowing through a radially-outer region of the axial flow path, and a root portion disposed on an inner side in a radial direction of the nozzle, the root portion having a cutout on a side of a trailing edge. The radially-outer region and a radially-inner region of the axial flow path communicate with each other, at least in a range in the axial direction in which the swirl vane is disposed. The swirl vane has a pressure surface, a downstream region of the pressure surface of the root portion being defined by the cutout as a curved surface which curves in a direction opposite to the swirl direction toward the trailing edge.
Public/Granted literature
- US20160298845A1 COMBUSTION BURNER, COMBUSTOR, AND GAS TURBINE Public/Granted day:2016-10-13
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