Invention Grant
- Patent Title: Cooling structure for gas turbine combustor
- Patent Title (中): 燃气轮机燃烧器的冷却结构
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Application No.: US12895248Application Date: 2010-09-30
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Publication No.: US08220273B2Publication Date: 2012-07-17
- Inventor: Hidekazu Iwasaki
- Applicant: Hidekazu Iwasaki
- Applicant Address: JP Hyogo
- Assignee: Kawasaki Jukogyo Kabushiki Kaisha
- Current Assignee: Kawasaki Jukogyo Kabushiki Kaisha
- Current Assignee Address: JP Hyogo
- Agency: Sughrue Mion, PLLC
- Priority: JP2008-092813 20080331
- Main IPC: F02C1/00
- IPC: F02C1/00

Abstract:
A gas turbine combustor having an improved cooling structure effective to efficiently suppress a possible occurrence of buckling in the combustion liner while exhibiting a convection cooling effect to the combustion liner, the gas turbine combustor includes a combustion liner having a combustion chamber defined therein and an outer peripheral surface forming a path of a compressed air, and a heat transfer enhancement structure provided on the outer peripheral surface of the combustion liner. The heat transfer enhancement structure referred to above is of a honeycomb construction defined by ribs protruding outwardly from the outer surface of the combustion liner. The honeycomb construction may be of a geometry in which hexagonal shapes, rhombic shapes, parallelogrammic shapes, bent rectangular shapes or triangular shapes are deployed next to each other.
Public/Granted literature
- US20110016869A1 COOLING STRUCTURE FOR GAS TURBINE COMBUSTOR Public/Granted day:2011-01-27
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