Turbine comprising a sealing device between the stator blade carrier and the housing
View Patent ↗The invention relates to a turbine of a power plant, having a stator, which has a housing and in the housing at least one stator blade carrier comprising stator blades. A rotor is provided which has a rotor shaft having rotor blades. At least one sealing device is provided which axially seals the respective stator blade carrier with respect to the housing and separates two regions having different pressures from one another. Improved sealing action is achieved in that the sealing device includes an axially acting primary sealing ring extending in the circumferential direction, and an axially acting additional sealing ring extending in the circumferential direction. The primary sealing ring facing the region has the lower pressure. The additional sealing ring facing the region has the higher pressure. The primary sealing ring is attached axially rigidly on the stator blade carrier. The additional sealing ring is attached axially movably, wherein the additional sealing ring is tensioned axially in the direction of the region having the higher pressure by means of at least one spring element.
1. A turbine of a power plant, preferably a steam turbine, the turbine comprising:
a stator which has a housing and in the housing at least one stator blade carrier with stator blades,
a rotor which has a rotor shaft with moving blades,
at least one sealing device which seals the respective stator blade carrier axially with respect to the housing and separates two regions of different pressure from one another, the sealing device having a main sealing ring, which extends in the circumferential direction and acts axially and which confronts the region having the lower pressure, and an additional sealing ring, which extends in the circumferential direction and acts axially and which confronts the region having the higher pressure,
wherein the main sealing ring is fixingly attached axially to the stator blade carrier and the additional sealing ring is attached axially movably to the stator blade carrier, the additional sealing ring being tensioned axially in the direction of the region having the higher pressure by at least one spring element wherein
the main sealing ring is arranged on an annular shoulder projecting radially from the respective stator blade carrier and extending in the circumferential direction and has an axial sealing contour which cooperates with an axial countersealing contour formed on the housing wherein, the countersealing contour is formed in a reception groove which extends in the circumferential direction and into which the annular shoulder penetrates radially.
2. The turbine as claimed in claim 1 , wherein
for the main sealing ring, the stator blade carrier has provided on it fastening screws which run axially and which engage into the main sealing ring on an axial side confronting the additional sealing ring.
3. The turbine as claimed in claim 1 wherein
the main sealing ring is inserted into a main annular groove which is open axially toward the region having the lower pressure and which extends in the circumferential direction, wherein, the main annular groove has a cross-sectional profile which is undercut-free in the axial direction.
4. A turbine of a power plant, preferably a steam turbine, the turbine comprising:
a stator which has a housing and in the housing at least one stator blade carrier with stator blades,
a rotor which has a rotor shaft with moving blades,
at least one sealing device which seals the respective stator blade carrier axially with respect to the housing and separates two regions of different pressure from one another, the sealing device having a main sealing ring, which extends in the circumferential direction and acts axially and which confronts the region having the lower pressure, and an additional sealing ring, which extends in the circumferential direction and acts axially and which confronts the region having the higher pressure,
wherein the main sealing ring is fixingly attached axially to the stator blade carrier and the additional sealing ring is attached axially movably to the stator blade carrier, the additional sealing ring being tensioned axially in the direction of the region having the higher pressure by at least one spring element, and
the additional sealing ring is arranged on an annular shoulder projecting radially from the respective stator blade carrier and extending in the circumferential direction and has an axial sealing contour which cooperates with an axial countersealing contour formed on the housing, wherein, the countersealing contour is formed in a reception groove which extends in the circumferential direction and into which the annular shoulder penetrates radially.
5. The turbine as claimed in claim 1 wherein
the additional sealing ring is inserted into an additional annular groove which is open axially toward the region having the higher pressure and which extends in the circumferential direction, wherein, the additional annular groove has a cross-sectional profile with an undercut in the axial direction.
6. The turbine as claimed in claim 5 , wherein
the respective spring element is arranged in the additional annular groove axially between the additional sealing ring and the stator blade carrier.
7. The turbine at least as claimed in claim 2 , wherein
the additional sealing ring overlaps the fastening screws axially, wherein, the fastening screws are arranged so as to be countersunk axially in the additional annular groove.
8. The turbine as claimed in claim 1 , wherein
the housing, the respective stator blade carrier, the respective main sealing ring and the respective additional sealing ring are divided in a parting plane, which contains an axis of rotation of the rotor, into two housing parts, two stator blade carrier parts, two main sealing ring parts and two additional sealing ring parts, wherein the additional sealing ring part inserted into the half additional annular groove is secured to the stator blade carrier in the circumferential direction in the region of the parting plane, at least one circumferential end, by a securing element, in particular a securing screw.
9. The turbine as claimed in claim 1 , wherein
for the main sealing ring, the stator blade carrier has provided on it fastening screws which run axially and which engage into the main sealing ring on an axial side confronting the additional sealing ring.
10. The turbine as claimed in claim 1 , wherein
the main sealing ring is inserted into a main annular groove which is open axially toward the region having the lower pressure and which extends in the circumferential direction, wherein the main annular groove has a cross-sectional profile which is undercut-free in the axial direction.
11. The turbine as claimed in claim 2 wherein
the main sealing ring is inserted into a main annular groove which is open axially toward the region having the lower pressure and which extends in the circumferential direction, wherein the main annular groove has a cross-sectional profile which is undercut-free in the axial direction.
12. The turbine as claimed in claim 1 , wherein
the additional sealing ring is arranged on an annular shoulder projecting radially from the respective stator blade carrier and extending in the circumferential direction and has an axial sealing contour which cooperates with an axial countersealing contour formed on the housing, wherein the countersealing contour is formed in a reception groove which extends in the circumferential direction and into which the annular shoulder penetrates radially.
13. The turbine as claimed in claim 2 wherein
the additional sealing ring is arranged on an annular shoulder projecting radially from the respective stator blade carrier and extending in the circumferential direction and has an axial sealing contour which cooperates with an axial countersealing contour formed on the housing, wherein the countersealing contour is formed in a reception groove which extends in the circumferential direction and into which the annular shoulder penetrates radially.
14. The turbine as claimed in claim 3 wherein
the additional sealing ring is arranged on an annular shoulder projecting radially from the respective stator blade carrier and extending in the circumferential direction and has an axial sealing contour which cooperates with an axial countersealing contour formed on the housing, wherein the countersealing contour is formed in a reception groove which extends in the circumferential direction and into which the annular shoulder penetrates radially.
15. The turbine as claimed in claim 1 wherein
the additional sealing ring is inserted into an additional annular groove which is open axially toward the region having the higher pressure and which extends in the circumferential direction, wherein the additional annular groove has a cross-sectional profile with an undercut in the axial direction.
16. The turbine as claimed in claim 2 wherein
the additional sealing ring is inserted into an additional annular groove which is open axially toward the region having the higher pressure and which extends in the circumferential direction, wherein the additional annular groove has a cross-sectional profile with an undercut in the axial direction.
17. The turbine as claimed in claim 1 , wherein
the housing, the respective stator blade carrier, the respective main sealing ring and the respective additional sealing ring are divided in a parting plane, which contains an axis of rotation of the rotor, into two housing parts, two stator blade carrier parts, two main sealing ring parts and two additional sealing ring parts, wherein the additional sealing ring part inserted into the half additional annular groove is secured to the stator blade carrier in the circumferential direction in the region of the parting plane, at least one circumferential end, by a securing element, in particular a securing screw.
18. The turbine as claimed in claim 2 , wherein
the housing, the respective stator blade carrier, the respective main sealing ring and the respective additional sealing ring are divided in a parting plane, which contains an axis of rotation of the rotor, into two housing parts, two stator blade carrier parts, two main sealing ring parts and two additional sealing ring parts, wherein the additional sealing ring part inserted into the half additional annular groove is secured to the stator blade carrier in the circumferential direction in the region of the parting plane, at least one circumferential end, by a securing element, in particular a securing screw.
19. The turbine as claimed in claim 3 , wherein
the housing, the respective stator blade carrier, the respective main sealing ring and the respective additional sealing ring are divided in a parting plane, which contains an axis of rotation of the rotor, into two housing parts, two stator blade carrier parts, two main sealing ring parts and two additional sealing ring parts, wherein the additional sealing ring part inserted into the half additional annular groove is secured to the stator blade carrier in the circumferential direction in the region of the parting plane, at least one circumferential end, by a securing element, in particular a securing screw.