Combined sealing and balancing arrangement for a turbine disc
View Patent ↗A turbine disc for a turbine is provided with a first protrusion and a second protrusion. The first protrusion and the second protrusion are formed in such a way that a balancing weight is coupleable between the first protrusion and the second protrusion. The first protrusion has a sealing section that is capable of sealing a fluid passage between the turbine disc and a further turbine part of the turbine.
1. A turbine disc for a turbine, comprising
a first protrusion and a second protrusion extending in radially spaced apart positions that form a recess positioned in a radial direction between the first and second protrusions with respect to a shaft of the turbine, when the turbine disc is coupled to the shaft of the turbine,
wherein the first protrusion and the second protrusion are formed in such a way that a balancing weight is coupleable in the recess between and directly to the first protrusion and the second protrusion, and
wherein the first protrusion comprises a sealing section that is capable of sealing a fluid passage between the turbine disc and a further turbine part of the turbine,
wherein the sealing section comprises at least one sealing lip.
2. The turbine disc of claim 1 , further comprising
a first surface and a second surface,
wherein the first protrusion and the second protrusion are formed on at least one of the first surface or second surface.
3. The turbine disc of claim 2 , wherein the turbine disc is coupleable to the turbine in such a way that the first surface and the second surface are opposed surfaces in an axial direction of a shaft of the turbine.
4. The turbine disc of claim 3 , wherein the turbine disc is coupleable to the turbine in such a way that the first surface is orientated upstream with respect to a fluid flow of the turbine and the second surface is orientated downstream with respect to the fluid flow.
5. The turbine disc of claim 1 , wherein the sealing section comprises a labyrinth seal.
6. The turbine disc of claim 1 , wherein the recess is formed in such a way that the recess proceeds in a circumferential direction with respect to the shaft of the turbine, when the turbine disc is coupled to the turbine.
7. The turbine disc of claim 6 ,
wherein the recess is formed in such a way that the recess and the balancing weight are coupleable by a dovetail connection.
8. The turbine disc of claim 1 ,
wherein the first protrusion is located at a first position and the second protrusion is located at a second position,
wherein a first distance between the first position and a centre of the turbine disc is larger than a second distance between the second position and the centre of the turbine disc.
9. The turbine disc of claim 1 ,
wherein the first protrusion and the second protrusion are detachably mounted on the turbine disc.
10. The turbine disc of claim 1 , wherein the first protrusion and the second protrusion are integrally formed with the turbine disc.
11. The turbine disc of claim 2 , wherein the second surface is free of a balancing weight arrangement and a further sealing section.
12. A turbine, comprising:
the shaft, the further turbine part, and the turbine disc according to claim 1 ,
the balancing weight mounted inside the recess,
wherein the turbine disc is mounted to the shaft and is rotatable with the shaft such that the first protrusion and the second protrusion extend in the radially spaced apart positions with respect to the shaft,
wherein the turbine disc is coupleable to the further turbine part in such a way that the sealing section of the first protrusion of the turbine disc seals the fluid passage between the turbine disc and the further turbine part.
13. The turbine of claim 12 , wherein the turbine is a gas turbine.
14. A method of producing a turbine disc for a turbine, the method comprising:
forming a first protrusion and a second protrusion onto the turbine disc, which extend in radially spaced apart positions that form a recess positioned in a radial direction between the first and second protrusions with respect to a shaft of the turbine, when the turbine disc is coupled to the shaft of the turbine,
wherein the first protrusion and the second protrusion are formed in such a way that a balancing weight is coupleable in the recess between and directly to the first protrusion and the second protrusion, and
wherein the first protrusion comprises a sealing section that is capable of sealing a fluid passage between the turbine disc and a further turbine part of the turbine,
wherein the sealing section comprises at least one sealing lip.
15. The method of claim 14 , further comprising, peening the balancing weight into place inside the recess.
16. The turbine of claim 12 , wherein the balancing weight is peened into place inside the recess.
17. The turbine of claim 1 , wherein the sealing section is located radially inwards of a cooling air duct.
18. The turbine of claim 1 , wherein the at least one sealing lip is pressed against the further part of the turbine.
19. The turbine of claim 18 , wherein the sealing section comprises a labyrinth seal.
20. The method of claim 14 , wherein the sealing section is located radially inwards of a cooling air duct.
21. The method of claim 14 , wherein the at least one sealing lip is pressed against the further part of the turbine.
22. The method of claim 21 , wherein the sealing section comprises a labyrinth seal.