Structure of exhaust section of gas turbine and gas turbine
View Patent ↗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.
1. A structure of an exhaust section of a gas turbine, comprising:
a casing defining a gas path part and an opening therein;
a bearing part for rotatably supporting a rotor having moving blades of a turbine section;
a strut extending inwardly from the casing and supporting the bearing part;
a strut cover extending along the strut to define a space between the strut and the strut cover; and
an internal diffuser extending along a rotational axis of the turbine section to form an air space surrounding the bearing part;
wherein the space defined between the strut and the strut cover extends from the opening toward the bearing part along the strut, and
wherein the air space surrounding the bearing part is in communication with the space defined between the strut and the strut cover to form a cooling flow channel together with the space defined between the strut and the strut cover, the cooling flow channel guiding air from the opening to the air space surrounding the bearing part via the space defined between the strut and the strut cover, and
wherein the cooling flow channel has an another opening for guiding air from the opening to the gas path part and introducing the air into the gas path part at a position downstream of a last-stage moving blade of the turbine section.
2. The structure of an exhaust section of a gas turbine according to claim 1 , further comprising:
a hollow strut extending from the casing, supporting the internal diffuser and connecting the outside of the casing and the inside of the internal diffuser to each other; and
a lid part for adjusting an opening area of the hollow strut on the casing.
3. A gas turbine, comprising:
a compressor section for compressing air;
a combustor for mixing the air compressed by the compressor section and fuel to cause combustion to generate combustion gas;
a turbine section for deriving rotational driving force from the combustion gas; and
the exhaust section according to claim 1 for receiving exhaust gas discharged from the turbine section flows.