Disabling circuit in steam turbines for shutting off saturated steam

Abstract

A cooling option for a steam turbine is provided, wherein the steam turbine includes a high-pressure zone and a medium-pressure zone, wherein the saturated steam streaming out of the high-pressure zone is discharged via a saturated steam conduit to a first pressure chamber in a second flow channel of the medium-pressure zone and thus the possibility of the saturated steam causing damage by corrosion and erosion in the high-pressure zone is prevented.

Claims

1. A steam turbine, comprising: a rotatably mounted rotor on which there is a first blading region and a second blading region, each blading region comprising a plurality of rotor blades, wherein the first blading region is arranged in a high pressure flow duct and the second blading region is arranged in a second flow duct; an inner casing arranged around the rotor; wherein the high-pressure flow duct is arranged between the rotor and the inner casing; wherein the rotor comprises a dummy piston prechamber and a dummy piston, wherein the steam turbine has a dummy piston line directly connected to a source of superheated steam, wherein the dummy piston line opens into the dummy piston prechamber such that superheated steam flows into the dummy piston prechamber and substantially fills the dummy piston prechamber with superheated steam, wherein the steam turbine has a wet steam line, which establishes a direct fluidic connection between a gap space arranged between the rotor and inner casing and a first pressure space disposed in the second blading region, wherein a pressure in the gap space is higher than in the first pressure space such that wet steam flows from the gap space to the first pressure space, thereby substantially preventing flow of wet steam into the dummy piston prechamber, and wherein the gap space is further arranged between the dummy piston prechamber and a high-pressure outflow zone of the high-pressure flow duct; and wherein the first pressure space is disposed between adjacent rotor blades in the second blading region.

2. The steam turbine as claimed in claim 1, wherein the dummy piston is designed to compensate for rotor thrust which occurs during operation.

3. The steam turbine as claimed in claim 1 wherein the dummy piston extends in a radial direction.

4. The steam turbine as claimed in claim 3, wherein the dummy piston prechamber is formed between the dummy piston and the inner casing.

5. The steam turbine as claimed in claim 1, wherein the steam source is arranged outside the steam turbine.

6. The steam turbine as claimed in claim 1, wherein the second flow duct has the first pressure space and a feed opening for feeding steam into the first pressure space.

7. The steam turbine as claimed in claim 6, wherein the second flow duct has a plurality of blade stages arranged in series in a direction of flow and comprises guide and rotor blades, and wherein the first pressure space is arranged downstream of one blade stage of the plurality of blade stages.

8. The steam turbine as claimed in claim 1, wherein the inner casing has a cavity which opens toward the gap space.

9. The steam turbine as claimed in claim 1, wherein the high-pressure flow duct and the second flow duct are arranged in the common inner casing.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The invention is now described in greater detail with reference to an illustrative embodiment. The components with the same reference signs operate in essentially the same way.

(2) In the drawing:

(3) FIG. 1 shows a cross section through a steam turbine according to the invention;

(4) FIG. 2 shows an enlarged detail in the region of the dummy piston of the steam turbine in FIG. 1.

DETAILED DESCRIPTION OF INVENTION

(5) FIG. 1 shows a cross section through a steam turbine 1. The steam turbine 1 comprises a combined high-pressure and medium-pressure turbine section 2. The significant feature of the steam turbine 1 is that a common outer casing 3 is arranged around the high-pressure and medium-pressure turbine section 2. The steam turbine 1 comprises a rotor 4, on which there is a first blading region 5, which is arranged in a high-pressure flow duct 6. The rotor 5 furthermore comprises a second blading region 7, which is arranged in a medium-pressure flow duct 8. Both the high-pressure flow duct 6 and the medium-pressure flow duct 8 comprise a plurality of rotor blades (not provided with a reference sign), which are arranged on the rotor 4, and a plurality of guide blades (not provided with a reference sign), which are arranged in an inner casing 9. The terms “high-pressure turbine section” and “medium-pressure turbine section” refer to the steam parameters of the inflowing steam. Thus, the pressure of the steam flowing into the high-pressure turbine section is higher than the pressure of the steam flowing into the medium-pressure turbine section. The terms “high-pressure turbine section” and “medium-pressure turbine section” also differ in the feature that the steam flowing out of the high-pressure turbine section is reheated in an intermediate superheater and then flows into the medium-pressure turbine section.

(6) There is no standard definition of high-pressure and medium-pressure turbine sections which is used by those skilled in the art.

(7) The steam turbine 1 illustrated in FIG. 1 is distinguished by a common inner casing 9 for the first blading region 5 and the second blading region 7. During operation, a steam flows into a high-pressure inflow zone 10. From there, the steam flows through the first blading region 5 in a first direction of flow 11. After flowing through the first blading region 5, the steam flows into a high-pressure outflow region 12 and out of the steam turbine. The steam in the high-pressure outflow zone 12 has temperature and pressure values which differ from the temperature and pressure values of the steam in the high-pressure inflow zone 10. In particular, the temperature and pressure values have fallen due to expansion of the steam. The steam in the high-pressure outflow zone 12 has temperature and pressure values such that this steam can be referred to as wet steam. This means that said steam contains extremely small condensed water particles. These extremely small water particles in the wet steam lead to erosion and corrosion damage in the case of impact on a component of the steam turbine 1 at high velocities. The majority of the wet steam flows out of the steam turbine 1 via the high-pressure outflow zone 12. However, a residual leakage flow remains in a gap space 13 between the rotor 4 and the inner casing 9. This wet steam in the gap space 13 flows in the first direction of flow 11 and impinges upon a dummy piston 14. The dummy piston 14 has a dummy piston prechamber 15, in which a superheated steam flows in. This superheated steam is in the dummy piston prechamber 15 arranged between the dummy piston 14 and a rear wall 16 of the inner casing 9. The superheated steam in the dummy piston prechamber 15 leads to an axial force acting on the dummy piston 14 and hence on the rotor 4.

(8) There is a gap 17 between the inner casing 9 and the rotor 4 in the region of the dummy piston 14. A steam can flow through this gap, entering an intermediate space 18 situated between the outer casing 3 and the inner casing 9. A wet steam in the gap 17 could lead to an increased risk of corrosion and erosion of the outer casing 3.

(9) According to the invention, a wet steam line 19 is now arranged in the steam turbine 1, establishing a fluidic connection between the gap space 13 and a first pressure space 20, wherein the gap space 13 is arranged between the rotor 4 and the inner casing 9. The first pressure space 20 is situated in the second blading region 7, in particular in a second flow duct 21. The illustrative embodiment shown in FIG. 1 shows that the first pressure space 20 is arranged in the region of the second flow duct 21. The pressure in this first pressure space 20 should likewise be such that the pressure for the wet steam in the gap space 13 is higher than in the first pressure space 20, with the result that a pressure gradient prevails in the wet steam line 19, leading to the wet steam passing from the gap space 13 to the first pressure space 20.

(10) The dummy piston 14 extends in a radial direction 22 which is substantially perpendicular to the axis of rotation 23.

(11) The dummy piston steam line 24 is connected fluidically to a steam source 25. As illustrated in FIG. 1, the inflow zone 26 forms the steam source 25. This steam, which flows in the inflow zone 26 into the medium-pressure turbine section, is a superheated steam, which enters the dummy piston prechamber 15. In an alternative embodiment, the steam source 25 can also be arranged outside the steam turbine 1.

(12) The inner casing 9 has a feed opening 27, to which the wet steam line 19 can be connected.

(13) FIG. 2 shows an enlarged detail of the high-pressure outflow zone 12 of the high-pressure turbine section. The inner casing 9 is designed in such a way that a high-pressure outflow zone 12 is surrounded and lies opposite the rotor 4 in the region of the gap space 13. The gap space 13 should be as small as possible to ensure that the wet steam in the high-pressure outflow zone 12 does not flow out via the gap space 13. The majority of the wet steam will pass via the high-pressure outflow zone 12 to an intermediate superheater. A smaller part passes as a leakage flow between the rotor 4 and the inner casing 9 and into the gap space 13. A cavity (not shown specifically), which is connected to the gap space 13, is therefore arranged in the inner casing 9. Via this cavity and via the wet steam line 19, the leakage flow is as it were extracted. The first pressure space 20 is used to drive this extraction, having a lower pressure than the pressure in the gap space 13. Further flow of the leakage flow formed by wet steam in the gap space 13 in the direction of the dummy piston prechamber 15 is prevented by the fact that the majority of the wet steam is extracted in the wet steam line 19. The superheated steam which enters the dummy piston prechamber 15 via a dummy piston line 24 will likewise propagate in two directions. First of all, the superheated steam will propagate in the direction of the gap 17 and finally impinge upon the outer casing 3. Another part of the superheated steam flows in the direction of the gap space 13 and, like the wet steam, is extracted via the wet steam line 19 toward the first pressure space 20.