Device and method for cooling a housing of a gas turbine or a combustion chamber
View Patent ↗The invention relates to a device for cooling a housing of a gas turbine and/or of a combustion chamber, in particular of a gas turbine, comprising: a cooling gas supply device with a cooling gas outlet, out of which a cooling gas stream flows when the cooling gas supply device is in operation, and with a cooling gas inlet, via which the cooling gas stream flows back to the cooling gas supply device when the cooling gas supply device is in operation; and a cooling gas path which is led through the housing in the circumferential direction of the latter and which connects a first housing connection to a second housing connection. So that a circumferential temperature difference of the housing can be set independently of an average temperature of the housing, the cooling device is equipped with a switching device for reversing the flow direction.
1. A device for cooling a housing of a gas turbine or a combustion chamber thereof, comprising:
a cooling gas supply device with a cooling gas outlet out of which a cooling gas stream flows during operation of the cooling gas supply device, and a cooling gas inlet via which the cooling gas stream flows back to the cooling gas supply device during operation of the cooling gas supply device;
a cooling gas path which is led through the housing in a circumferential direction thereof and which connects a first housing connection to a second housing connection;
a switching device for reversing a direction of flow of the cooling gas stream, the switching device being operable between a first switching position in which the switching device connects the cooling gas outlet to the first housing connection and the cooling gas inlet to the second housing connection, and a second switching position in which the switching device connects the cooling gas outlet to the second housing connection and the cooling gas inlet to the first housing connection.
2. The device of claim 1 , wherein the switching device comprises:
a first connection connected to the cooling gas outlet;
a second connection connected to the cooling gas inlet;
a third connection connected to the first housing connection; and
a fourth connection connected to the second housing connection;
a flap arrangement which in the first switching position defines a first path leading from the first connection to the third connection and a second path leading from the fourth connection to the second connection, and which in the second switching position defines a third path leading from the first connection to the fourth connection and a fourth path leading from the third connection to the second connection.
3. The device of claim 2 , wherein the switching device comprises:
a first line leading from the first connection to the third connection;
a second line leading from the second connection to the fourth connection;
a first port controllable with a first flap and connecting the first line to the second line;
a second port controllable with a second flap and located in the first line;
a third port controllable with a third flap and located in the second line; and
a third line connecting the second port to the third port;
wherein the first flap, in the first switching position, closes the first port and, in the second switching position, opens the first port and shuts off the first line between the first port and the second port;
wherein the second flap, in the first switching position, closes the second port and, in the second switching position, opens the second port; and
wherein the third flap, in the first switching position, closes the third port and, in the second switching position, opens the third port and shuts off the second line between the first port and the third port.
4. The device of claim 3 , wherein a common actuator is provided for the simultaneous adjustment of the three flaps.
5. A method for cooling a housing of a gas turbine or a combustion chamber thereof, the method comprising:
acting upon a cooling gas path with a cooling gas flow, the path being led through the housing in a circumferential direction thereof and connecting a first housing connection to a second housing connection; and
varying a circumferential temperature difference of the housing between an outlet temperature measured at one of the housing connections and an inlet temperature measured at the other of the housing connections by changing a flow direction of the cooling gas in the cooling gas path.
6. The method of claim 5 , wherein the circumferential temperature difference is reduced by raising a changeover frequency and is increased by lowering the changeover frequency.
7. The method of claim 5 , wherein the flow direction of the cooling gas is changed whenever the circumferential temperature difference overshoots a predetermined limit value.
8. The method of claim 5 , wherein the flow direction of the cooling gas is changed whenever the circumferential temperature difference overshoots a predeterminable limit value.
9. The method of claim 5 , wherein an average temperature of the housing is varied by varying an inlet temperature of the cooling gas upon entry into the cooling gas path and by varying a mass flow of the cooling gas supplied to the cooling gas path.
10. The method of claim 9 , wherein the average temperature of the housing is defined by a mean value of the inlet temperature and the outlet temperature.
11. The method of claim 5 , wherein an average temperature of the housing is varied by varying an inlet temperature of the cooling gas upon entry into the cooling gas path.
12. The method of claim 11 , wherein the average temperature of the housing is defined by a mean value of the inlet temperature and the outlet temperature.
13. The method of claim 5 , wherein an average temperature of the housing is varied by varying a mass flow of the cooling gas supplied to the cooling gas path.
14. The method of claim 13 , wherein the average temperature of the housing is defined by a mean value of the inlet temperature and the outlet temperature.