Invention Grant
- Patent Title: Cooling structure with ribs for gas turbine engine
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Application No.: US16206154Application Date: 2018-11-30
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Publication No.: US11215361B2Publication Date: 2022-01-04
- Inventor: Tomoko Tsuru , Katsuhiko Ishida , Yuwa Kawahara
- Applicant: KAWASAKI JUKOGYO KABUSHIKI KAISHA
- Applicant Address: JP Kobe
- Assignee: KAWASAKI JUKOGYO KABUSHIKI KAISHA
- Current Assignee: KAWASAKI JUKOGYO KABUSHIKI KAISHA
- Current Assignee Address: JP Kobe
- Agency: Sughrue Mion, PLLC
- Priority: JPJP2016-109874 20160601
- Main IPC: F23M5/08
- IPC: F23M5/08 ; F02C7/18 ; F23R3/00 ; B23C3/34

Abstract:
In a structure for cooling a component member of a gas turbine using a working gas, a plurality of heat transfer enhancement ribs having W shapes are provided so as to project from the wall surface of a passage wall facing a cooling medium passage through which a cooling medium flows. In each heat transfer enhancement rib, outside corner portions facing toward the upstream side are formed in an angled shape, and at least any one of inside corner portions and outside corner portions other than the outside corner portion facing toward the upstream side are formed in a curved shape.
Public/Granted literature
- US11168884B2 Cooling structure with ribs for gas turbine engine Public/Granted day:2021-11-09
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