Gas turbine and gas turbine operating method
A gas turbine is provided with an exhaust diffuser in which an exhaust flow path for circulating exhaust gas from a turbine is formed, and a cooling device for cooling a structure facing the exhaust flow path in the exhaust diffuser. The cooling device has a guide part in which a guide flow path for circulating a cooling medium is formed and which is configured to guide the cooling medium to the structure, and a switching part able to switch between a first state where a flow rate of the cooling medium flowing through the guide flow path is a first flow rate corresponding to a flow rate during a rated operation and a second state where the flow rate of the cooling medium is a second flow rate higher than the first flow rate.
1. A gas turbine comprising:
an exhaust diffuser in which an exhaust flow path for circulating exhaust gas from a turbine is formed; and
a cooling device for cooling a structure facing the exhaust flow path in the exhaust diffuser,
wherein:
the cooling device has
a guide part in which a guide flow path for circulating a cooling medium is formed, the guide part being configured to guide the cooling medium to the structure,
a valve part having a valve body that is movable to block the guide flow path in a first state and to open the guide flow path so as to widen a flow path area of the guide flow path in a second state, and
a supply part configured to supply the cooling medium at a first flow rate corresponding to a flow rate of the cooling medium flowing through the guide flow path during a rated operation of the gas turbine to the structure in the first state;
the guide part has an opening configured to accept outside air from an outside of the exhaust diffuser as the cooling medium;
the supply part is a linking hole defined in the guide part between the valve part and the structure so as to link the outside of the exhaust diffuser and the guide flow path, and the opening is further away from the structure than the valve body; and
the linking hole is one of a plurality of linking holes defined in the guide part and disposed about a circumference of the guide part.
2. The gas turbine according to claim 1 , wherein the valve part has a drive part configured to move the valve body, and the cooling device has a failsafe part configured to make the flow rate of the cooling medium flowing through the guide flow path a second flow rate when the drive part cannot be controlled.
3. The gas turbine according to claim 1 , wherein the exhaust diffuser has:
a tubular outer diffuser forming a portion of the exhaust flow path;
an inner diffuser inside the outer diffuser and defining the exhaust flow path together with the outer diffuser; and
a strut cover for linking the outer diffuser and the inner diffuser, and wherein the guide part has:
a strut cover guide part configured to guide the cooling medium to the strut cover as the structure; and
an outer diffuser guide part configured to guide the cooling medium to the outer diffuser as the structure.
4. The gas turbine according to claim 3 , wherein the guide part has a flow rate adjusting part configured to adjust the flow rate of the cooling medium being guided to at least one of the strut cover guide part and the outer diffuser guide part.
5. The gas turbine according to claim 1 , wherein the valve part is configured to switch between the first state and the second state based on a gas turbine output or a correlation value that is a value correlating to the gas turbine output.
6. A gas turbine comprising:
an exhaust diffuser in which an exhaust flow path for circulating exhaust gas from a turbine is formed; and
a cooling device for cooling a structure facing the exhaust flow path in the exhaust diffuser,
wherein:
the cooling device has
a guide part in which a guide flow path for circulating a cooling medium is formed, the guide part being configured to guide the cooling medium to the structure,
a valve part having a valve body that is movable to block the guide flow path in a first state and to open the guide flow path so as to widen a flow path area of the guide flow path in a second state, and
a stopper part configured to form a gap between the guide part and the valve body in the first state such that the cooling medium is supplied through the gap at a first flow rate corresponding to a flow rate of the cooling medium flowing through the guide flow path during a rated operation of the gas turbine to the structure in the first state.