Invention Grant
- Patent Title: Duct assembly including helicoidal structure and gas turbine combustor including the same
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Application No.: US16111245Application Date: 2018-08-24
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Publication No.: US10731856B2Publication Date: 2020-08-04
- Inventor: Geun Cheol Kim
- 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@7b2fd092
- Main IPC: F23R3/00
- IPC: F23R3/00 ; F23R3/04 ; F23R3/44 ; F23R3/12 ; F01D25/26 ; F28F1/10 ; F28F1/36 ; F28D7/10 ; F16L9/18 ; F01D9/02

Abstract:
A helicoidal structure promotes cooling of a liner applied in an annular space of a double-shell structure formed of the liner and a flow sleeve to cool a duct assembly, by increasing the residence time and cooling area of cooling compressed air on the surface of the liner. The helicoidal structure includes a helicoidal rib protruding from a surface of the liner to guide the cooling compressed air at a predetermined angle with respect to an axial direction of the liner, the helicoidal rib having cooling holes and forming a first cooling passage along which main-cooling compressed air flows and a second cooling passage along which auxiliary-cooling compressed air flows. The second cooling passage induces a flow of the auxiliary-cooling compressed air through the cooling holes, and the flow of the auxiliary-cooling compressed air is derived from a flow of the main-cooling compressed air in the first cooling passage.
Public/Granted literature
- US20190086083A1 DUCT ASSEMBLY INCLUDING HELICOIDAL STRUCTURE AND GAS TURBINE COMBUSTOR INCLUDING THE SAME Public/Granted day:2019-03-21
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