Invention Grant
- Patent Title: Cooling path structure for concentrated cooling of seal area and gas turbine combustor having the same
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Application No.: US16026065Application Date: 2018-07-03
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Publication No.: US10830143B2Publication Date: 2020-11-10
- Inventor: In Chan Choi
- Applicant: DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO., LTD.
- Applicant Address: KR Gyeongsangnam-do
- Assignee: Doosan Heavy Industries Construction Co., Ltd
- Current Assignee: Doosan Heavy Industries Construction Co., Ltd
- Current Assignee Address: KR Gyeongsangnam-do
- Agency: Invenstone Patent, LLC
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@72bc1eb1
- Main IPC: F02C7/12
- IPC: F02C7/12 ; F01D9/02 ; F23R3/00 ; F01D25/12 ; F23R3/04 ; F02C7/28 ; F16J15/02

Abstract:
A cooling path structure for concentrated cooling of a seal area in a duct assembly and a gas turbine combustor having the same are provided. The cooling path structure includes a concentrated cooling guide plate facing the seal area to introduce compressed cooling air into the seal area through a plurality of first cooling holes and a plurality of second cooling holes respectively formed in the guide plate. The first cooling holes are formed along a first inlet axis such that the introduced cooling air approaches a central axis of the seal area in a forward direction, and the second cooling holes are formed along a second inlet axis such that the introduced cooling air approaches the central axis of the seal area in a backward direction. The first and second inlet axes each are inclined at an acute angle relative to the central axis of the seal area.
Public/Granted literature
- US20190063320A1 COOLING PATH STRUCTURE FOR CONCENTRATED COOLING OF SEAL AREA AND GAS TURBINE COMBUSTOR HAVING THE SAME Public/Granted day:2019-02-28
Information query
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