Steam turbine and method for operating a steam turbine
View Patent ↗A steam turbine having a cooling option, in which steam is taken from the flow channel, the steam cooling the thrust-compensating intermediate floor, being mixed with a small amount of live steam and being returned to the flow channel. A method cools the steam turbine, wherein steam is extracted from the high-pressure region and is fed to a space between the thrust-compensating partition wall and inner casing, wherein steam from the space between the thrust-compensating partition wall and the inner casing is fed via a first cross feedback passage to the high-pressure region.
1. A steam turbine comprising:
an inner casing and an outer casing and also a rotor which is arranged in a rotatably supported manner inside the inner casing,
wherein the outer casing is arranged around the inner casing,
wherein the rotor has a high-pressure region which is arranged along a first flow direction and an intermediate-pressure region which is arranged along a second flow direction,
wherein the inner casing has a plurality of high-pressure stator blades in the high-pressure region, which are arranged in such a way that a high-pressure flow passage, having a plurality of high-pressure blading stages which in each case have a row of high-pressure rotor blades and a row of high-pressure stator blades, is formed along the first flow direction,
wherein the inner casing has a plurality of intermediate-pressure stator blades in the intermediate-pressure region, which are arranged in such a way that an intermediate-pressure flow passage, having a plurality of intermediate-pressure blading stages which in each case have a row of intermediate-pressure rotor blades and a row of intermediate-pressure stator blades, is formed along the second flow direction,
wherein the rotor has a thrust-compensating partition wall between the high-pressure region and the intermediate-pressure region,
wherein the inner casing has a connection which, as a communicating pipe, is formed between the high-pressure flow passage, downstream of a first high-pressure blading stage, and a first thrust-compensating partition wall space,
wherein the inner casing has a first cross feedback passage which, as a communicating pipe, is formed between a second thrust-compensating partition wall space, which is arranged between the thrust-compensating partition wall and the inner casing, and
a high-pressure inflow space, in the high-pressure flow passage, which is arranged downstream of a second high-pressure blading stage,
wherein between the inner casing and the thrust-compensating partition wall a first brush seal is arranged upstream of the second thrust-compensating partition wall space along the second flow direction and a second brush seal is arranged downstream of the first thrust-compensating partition wall space along the second flow direction.
2. The steam turbine as claimed in claim 1 ,
wherein the first high-pressure blading stage is arranged upstream of the second high-pressure blading stage as seen along the first flow direction.
3. The steam turbine as claimed in claim 1 ,
wherein the first thrust-compensating partition wall space is arranged upstream of the second thrust-compensating partition wall space as seen along the first flow direction.
4. The steam turbine as claimed in claim 1 ,
wherein the first cross feedback passage is formed by pipes.
5. The steam turbine as claimed in claim 1 ,
wherein the connection is formed by connecting pipes.
6. A steam turbine comprising:
an inner casing and an outer casing and also a rotor which is arranged in a rotatably supported manner inside the inner casing,
wherein the outer casing is arranged around the inner casing,
wherein the rotor has a high-pressure region which is arranged along a first flow direction and an intermediate-pressure region which is arranged along a second flow direction,
wherein the inner casing has a plurality of high-pressure stator blades in the high-pressure region, which are arranged in such a way that a high-pressure flow passage, having a plurality of high-pressure blading stages which in each case have a row of high-pressure rotor blades and a row of high-pressure stator blades, is formed along the first flow direction,
wherein the inner casing has a plurality of intermediate-pressure stator blades in the intermediate-pressure region, which are arranged in such a way that an intermediate-pressure flow passage, having a plurality of intermediate-pressure blading stages which in each case have a row of intermediate-pressure rotor blades and a row of intermediate-pressure stator blades, is formed along the second flow direction,
wherein the rotor has a thrust-compensating partition wall between the high-pressure region and the intermediate-pressure region,
wherein the inner casing has a connection which, as a communicating pipe, is formed between the high-pressure flow passage, downstream of a first high-pressure blading stage, and a first thrust-compensating partition wall space,
wherein the inner casing has a first cross feedback passage which, as a communicating pipe, is formed between a second thrust-compensating partition wall space, which is arranged between the thrust-compensating partition wall and the inner casing, and
a high-pressure inflow space, in the high-pressure flow passage, which is arranged downstream of a second high-pressure blading stage, further comprising:
a second cross feedback passage which, as communicating pipe, is formed between a third thrust-compensating partition wall space, which is arranged between the thrust-compensating partition wall and the inner casing, and
a high-pressure inflow space, in the high-pressure flow passage, which is arranged downstream of a third high-pressure blading stage.
7. The steam turbine as claimed in claim 6 ,
wherein the third high-pressure blading stage is arranged downstream of the second high-pressure blading stage as seen in the first flow direction.
8. The steam turbine as claimed in claim 6 ,
wherein the first high-pressure blading stage is arranged upstream of the second high-pressure blading stage as seen along the first flow direction.
9. The steam turbine as claimed in claim 6 ,
wherein the first thrust-compensating partition wall space is arranged upstream of the second thrust-compensating partition wall space as seen along the first flow direction.
10. The steam turbine as claimed in claim 6 ,
wherein between the inner casing and the thrust-compensating partition wall a first brush seal is arranged upstream of the second thrust-compensating partition wall space along the second flow direction and a second brush seal is arranged downstream of the first thrust-compensating partition wall space along the second flow direction.
11. The steam turbine as claimed in claim 6 ,
wherein the first cross feedback passage is formed by pipes.
12. The steam turbine as claimed in claim 6 ,
wherein the connection is formed by connecting pipes.
13. The steam turbine as claimed in claim 6 ,
wherein the third high-pressure blading stage is arranged downstream of the second high-pressure blading stage as seen in the first flow direction.
14. A method for cooling a steam turbine, wherein the steam turbine has a high-pressure region and an intermediate-pressure region, wherein a rotor has a thrust-compensating partition wall between the high-pressure region and the intermediate-pressure region, the method comprising:
extracting steam from the high-pressure region and feeding to a space between the thrust-compensating partition wall and inner casing,
feeding steam from the space between the thrust-compensating partition wall and the inner casing via a first cross feedback passage to the high-pressure region, further comprising:
between thrust-compensating partition wall and inner casing, feeding additional steam via a second cross feedback passage into the high-pressure region.