Invention Grant
- Patent Title: Combustor
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Application No.: US15742332Application Date: 2015-10-13
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Publication No.: US10648673B2Publication Date: 2020-05-12
- Inventor: Ik Soo Kim
- 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: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@1a50f607
- International Application: PCT/KR2015/010778 WO 20151013
- International Announcement: WO2017/007068 WO 20170112
- Main IPC: F23R3/34
- IPC: F23R3/34 ; F23R3/42 ; F02C7/22 ; F23C6/04 ; F23R3/16 ; F23C9/00 ; F23R3/44 ; F23R3/28 ; F02C3/34 ; F23C5/08 ; F23C9/06 ; F23C9/08 ; F23R3/06 ; F23R3/14

Abstract:
A combustor includes a combustion tube having a cylindrical shape with a combustion space where fuel is combusted and including an inlet through which the fuel is introduced, an outlet through which a gas generated when the fuel is combusted is discharged, and a protrusion protruding inward from a wall surface between the inlet and the outlet; an injection unit configured to inject fuel into the combustion tube through the inlet of the combustion tube; and an additional injection unit located on the protrusion of the combustion tube and configured to inject fuel into the combustion tube.
Public/Granted literature
- US20180202662A1 COMBUSTOR Public/Granted day:2018-07-19
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