Invention Grant
US08740550B2 Structure of exhaust section of gas turbine and gas turbine 有权
燃气轮机和燃气轮机排气段结构

Structure of exhaust section of gas turbine and gas turbine
Abstract:
There is provided an exhaust section of a gas turbine and a gas turbine that can cool a strut and the periphery of a bearing without decreasing the efficiency of the gas turbine. A structure of an exhaust section of a gas turbine has: a casing in which a gas path part is formed; a bearing part that rotatably supports moving blades of a turbine section; a strut that extends inwardly from the casing and supports the bearing part; an opening formed in the casing; and a cooling flow channel that extends from the opening toward the bearing part along the strut to guide air at a lower temperature than an exhaust gas flowing in the gas path part to the gas path part and opens into the gas path part at a position downstream of a last-stage moving blade of the turbine section.
Public/Granted literature
Information query
Patent Agency Ranking
0/0