Invention Grant
- Patent Title: Liner cooling structure with reduced pressure losses and gas turbine combustor having same
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Application No.: US16819015Application Date: 2020-03-13
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Publication No.: US11242990B2Publication Date: 2022-02-08
- Inventor: Alexander Myatlev , Borys Shershnyov
- Applicant: DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO., LTD.
- Applicant Address: KR Changwon-si
- Assignee: DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO., LTD.
- Current Assignee: DOOSAN HEAVY INDUSTRIES & CONSTRUCTION CO., LTD.
- Current Assignee Address: KR Changwon-si
- Agency: Harvest IP Law, LLP
- Priority: KR10-2019-0041966 20190410
- Main IPC: F23M5/08
- IPC: F23M5/08 ; F23R3/00 ; F01D9/02

Abstract:
A liner cooling structure of a duct assembly reduces pressure loss generated in the compressed air flow for cooling the liner. The duct assembly includes a liner, a transition piece, and a flow sleeve, and the transition piece and the flow sleeve form a transition piece channel through which a main stream of compressed air is introduced to the duct assembly. The liner cooling structure includes a first flow passage through which the main stream of compressed air passes in a first direction; and a second flow passage formed as a plurality of inlet holes in the flow sleeve to communicate with the first flow passage and configured to pass an auxiliary stream of compressed air in a second direction from outside the flow sleeve to inside the flow sleeve, the auxiliary stream joining the main stream such that the second direction forms an acute angle with the first direction.
Public/Granted literature
- US20200326069A1 LINER COOLING STRUCTURE WITH REDUCED PRESSURE LOSSES AND GAS TURBINE COMBUSTOR HAVING SAME Public/Granted day:2020-10-15
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