Invention Grant
- Patent Title: Slinger combustor having main combustion chamber and sub-combustion chamber, and gas turbine engine system having the same
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Application No.: US15609354Application Date: 2017-05-31
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Publication No.: US10907834B2Publication Date: 2021-02-02
- Inventor: Soo Youl Park
- Applicant: HANWHA AEROSPACE CO., LTD.
- Applicant Address: KR Changwon-si
- Assignee: HANWHA AEROSPACE CO., LTD.
- Current Assignee: HANWHA AEROSPACE CO., LTD.
- Current Assignee Address: KR Changwon-si
- Agency: Sughrue Mion, PLLC
- Priority: KR10-2016-0083535 20160701
- Main IPC: F23R3/38
- IPC: F23R3/38 ; F23R3/26 ; F02C7/228 ; F23R3/34 ; F02C7/262 ; F23D14/72 ; F02C7/264

Abstract:
A slinger combustor includes; a first compressed air line connected to a compressor and configured to supply compressed air; a first fuel line connected to a fuel storage and configured to supply fuel; a rotation shaft configured to rotate and inject the fuel supplied from the first fuel line; a main combustion chamber configured to receive the fuel injected from the rotation shaft and receive the compressed air from the first compressed air line; and a sub-combustion chamber configured to selectively discharge a flame generated in an inner space of the sub-combustion chamber to the main combustion chamber.
Public/Granted literature
- US20180003388A1 SLINGER COMBUSTOR AND GAS TURBINE ENGINE SYSTEM HAVING THE SAME Public/Granted day:2018-01-04
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