Compressor-side shaft seal of an exhaust-gas turbocharger
The piston ring sealing points of a sealing apparatus between the rotor and the housing of a continuous-flow machine each have a piston ring, a cylindrical contact surface, which is directed radially inward, on the housing, as well as an axial stop on the rotor. In this case, the piston ring of the outer piston ring sealing point has a larger external radius and a smaller internal radius than the piston ring of the inner piston ring sealing point. At the same time, the outer piston ring sealing point has a smaller internal radius than the inner piston ring sealing point. Because of the V-shaped arrangement concept, there is no need for a steel ring, shrunk onto the rotor, between the piston ring sealing points.
1. A sealing apparatus between a rotor and a housing of a continuous flow machine, wherein the rotor comprises a shaft and at least one bladed wheel, and the shaft is arranged in a shaft bushing hole in the housing,
wherein the sealing apparatus comprises two piston ring sealing points, which are arranged at an axial distance from one another, the two piston ring sealing points comprising an outer piston ring sealing point which is located closest to the bladed wheel, and an inner piston ring sealing point,
wherein the piston ring sealing points each comprise a piston ring, a cylindrical contact surface on the housing, and a projection with an axial stop surface on the rotor,
wherein the piston ring of the outer piston ring sealing point has an external radius which is greater than an external radius of the piston ring of the inner piston ring sealing point,
wherein the piston ring of the outer piston ring sealing point has an internal radius which is less than an internal radius of the piston ring of the inner piston ring sealing point,
wherein an internal radius of the cylindrical contact surface of the outer piston ring sealing point is greater than an internal radius of the cylindrical contact surface of the inner piston ring sealing point, and
wherein a maximum radial extent of the axial stop surface on the projection on the rotor of the outer piston ring sealing point is less than a maximum radial extent of the axial stop surface on the projection on the rotor of the inner piston ring sealing point, such that the axial stop surfaces on the projections on the rotor are radially stepped with respect to one another.
2. The sealing apparatus as claimed in claim 1 , wherein a radial recess edge is arranged between the cylindrical contact surface of the outer piston ring sealing point and the cylindrical contact surface of the inner piston ring sealing point on the housing, the radial recess edge having a very small radial extent which is less than the internal radius of the cylindrical contact surface of the inner piston ring sealing point.
3. The sealing apparatus as claimed in claim 1 , wherein on the side of the cylindrical contact surfaces facing away from the bladed wheel, the housing in each case has a radial step with a smaller diameter, which radial steps each form an axial stop for the piston rings.
4. The sealing apparatus as claimed in claim 1 , comprising a plurality of the piston ring sealing points,
wherein, in the direction facing away from the bladed wheel from one piston ring sealing point to the next piston ring sealing point,
the piston rings are each stepped with a decreasing external radius and an increasing internal radius,
the cylindrical contact surfaces are each stepped with a decreasing internal radius, and
the axial stops are each stepped with an increasing maximum radial extent.
5. The sealing apparatus as claimed in claim 4 , wherein on the side of the cylindrical contact surfaces facing away from the bladed wheel, the housing in each case has a radial step with a smaller diameter, the radial steps each forming an axial stop for the respective piston rings.
6. The sealing apparatus as claimed in claim 4 , wherein a radial recess edge is arranged between the cylindrical contact surfaces of two adjacent piston ring sealing points on the housing and has a very small radial extent, which is less than the internal radii of the cylindrical contact surface of the two adjacent piston ring sealing points arranged on the side facing away from the bladed wheel.
7. The sealing apparatus as claimed in claim 6 , wherein on the side of the cylindrical contact surfaces facing away from the bladed wheel, the housing in each case has a radial step with a smaller diameter, the radial steps each forming an axial stop for the respective piston rings.
8. A continuous-flow machine, comprising a sealing apparatus between a rotor, which has a shaft and a bladed wheel, and a housing of the continuous flow machine, wherein the sealing apparatus is the sealing apparatus as claimed in claim 1 .
9. An exhaust gas turbocharger, comprising a sealing apparatus between a rotor, which has a shaft and a compressor wheel, and a housing of the exhaust gas turbocharger, wherein the sealing apparatus is the sealing apparatus as claimed in claim 1 .
10. The sealing apparatus as claimed in claim 1 , wherein
a radial recess edge is arranged between the cylindrical contact surface of the outer piston ring sealing point and the cylindrical contact surface of the inner piston ring sealing point on the housing, the radial recess edge having a very small radial extent which is less than the internal radius of the cylindrical contact surface of the inner piston ring sealing point.
11. The sealing apparatus as claimed in claim 1 , wherein on the side of the cylindrical contact surfaces facing away from the bladed wheel, the housing in each case has a radial step with a smaller diameter, which radial steps each form an axial stop for the piston rings.
12. The sealing apparatus as claimed in claim 1 , comprising a plurality of the piston ring sealing points,
wherein, in the direction facing away from the bladed wheel from one piston ring sealing point to the next piston ring sealing point,
the piston rings are each stepped with a decreasing external radius and an increasing internal radius,
the cylindrical contact surfaces are each stepped with a decreasing internal radius, and
the axial stops are each stepped with an increasing maximum radial extent.
13. The sealing apparatus as claimed in claim 12 , wherein on the side of the cylindrical contact surfaces facing away from the bladed wheel, the housing in each case has a radial step with a smaller diameter, the radial steps each forming an axial stop for the respective piston rings.
14. The sealing apparatus as claimed in claim 12 , wherein a radial recess edge is arranged between the cylindrical contact surfaces of two adjacent piston ring sealing points on the housing and has a very small radial extent, which is less than the internal radii of the cylindrical contact surface of the two adjacent piston ring sealing points arranged on the side facing away from the bladed wheel.
15. The sealing apparatus as claimed in claim 14 , wherein on the side of the cylindrical contact surfaces facing away from the bladed wheel, the housing in each case has a radial step with a smaller diameter, the radial steps each forming an axial stop for the respective piston rings.
16. A continuous-flow machine, comprising a sealing apparatus between the rotor, which has a shaft and a bladed wheel, and the housing of the continuous flow machine, wherein the sealing apparatus is the sealing apparatus as claimed in claim 1 .
17. An exhaust gas turbocharger, comprising a sealing apparatus between a rotor, which has a shaft and a compressor wheel, and a housing of the exhaust gas turbocharger, wherein the sealing apparatus is the sealing apparatus as claimed in claim 1 .