Variable turbine and/or compressor geometry for an exhaust-gas turbocharger
A variable geometry may include a blade bearing ring, guide blades mounted therein or thereon in a rotatable manner, and an adjustment ring for simultaneously adjusting the guide blades. The adjustment ring may be in operative connection with adjusting levers of the guide blades, and may be mounted on the blade bearing ring via rollers. A roll engagement may be provided for each roller, which may be guided into and may roll onto the respective roll engagement. Each roller may have two guide collars between which a groove runs and on which the roller may roll onto the blade bearing ring. A rail may be arranged on the blade bearing ring, and may engage in the groove between the two guide collars for each roller. Each roller may be retained on the blade bearing ring and on the adjustment ring exclusively via the guide collars of the respective roller.
1. A variable geometry for an exhaust-gas turbocharger, comprising:
a blade bearing ring,
guide blades mounted one of in or on the blade bearing ring in a rotatable manner, and
an adjustment ring for simultaneously adjusting the guide blades, the adjustment ring being in operative connection with adjusting levers of the guide blades,
the adjustment ring being mounted on the blade bearing ring via rollers,
wherein a roll engagement is provided for each roller on the adjustment ring, each roller being guided into and rolling onto the respective roll engagement,
wherein each roller has two guide collars between which a groove runs and on which the roller rolls onto the blade bearing ring,
wherein a rail is arranged on the blade bearing ring, the rail engaging in the groove between the two guide collars, and
wherein each roller is retained on the blade bearing ring and on the adjustment ring exclusively via the guide collars of the respective roller.
2. A variable geometry according to claim 1 , further comprising an axial extension arranged on at least one roller as an axial stop on the blade bearing ring.
3. A variable geometry according to claim 2 , wherein the rail includes at least one recess on the blade bearing ring through which the roller is able to be introduced.
4. A variable geometry according to claim 2 , wherein the two guide collars include conical inner flanks.
5. A variable geometry according to claim 4 , wherein the rail includes conical outer flanks on the blade bearing ring.
6. A variable geometry according to claim 5 , wherein the conical inner flanks on the guide collars are steeper than the conical outer flanks on the rail.
7. A variable geometry according to claim 1 , wherein the rail includes at least one recess on the blade bearing ring through which the roller is able to be introduced.
8. A variable geometry according to claim 1 , wherein the two guide collars include conical inner flanks.
9. A variable geometry according to claim 8 , wherein the rail includes conical outer flanks on the blade bearing ring.
10. A variable geometry according to claim 9 , wherein the conical inner flanks on the guide collars are steeper than the conical outer flanks on the rail.
11. An exhaust-gas turbocharger comprising a variable geometry having:
a blade bearing ring,
guide blades mounted one of in or on the blade bearing ring in a rotatable manner, and
an adjustment ring for simultaneously adjusting the guide blades, the adjustment ring being in operative connection with adjusting levers of the guide blades, the adjustment ring being mounted on the blade bearing ring via rollers,
wherein a roll engagement is provided for each roller on the adjustment ring, each roller being guided into and rolling onto the respective roll engagement,
wherein each roller has two guide collars between which a groove runs and on which the roller rolls onto the blade bearing ring,
wherein a rail is arranged on the blade bearing ring, the rail engaging in the groove between the two guide collars for each roller, and
wherein each roller is retained on the blade bearing ring and on the adjustment ring exclusively via the guide collars of the respective roller.
12. An exhaust-gas turbocharger according to claim 11 , further comprising an axial extension arranged on at least one roller as an axial stop on the blade bearing ring.
13. An exhaust-gas turbocharger according to claim 12 , wherein the rail includes at least one recess on the blade bearing ring through which the roller is able to be introduced.
14. An exhaust-gas turbocharger according to claim 11 , wherein the rail includes at least one recess on the blade bearing ring through which the roller is able to be introduced.
15. An exhaust-gas turbocharger according to claim 11 , wherein the two guide collars include conical inner flanks.
16. An exhaust-gas turbocharger according to claim 15 , wherein the rail includes conical outer flanks on the blade bearing ring.
17. An exhaust-gas turbocharger according to claim 16 , wherein the conical inner flanks on the guide collars are steeper than the conical outer flanks on the rail.
18. An exhaust-gas turbocharger according to claim 11 , wherein the rail includes conical outer flanks on the blade bearing ring.
19. A variable geometry according to claim 1 , wherein the rail includes conical outer flanks on the blade bearing ring.
20. A method for assembling a variable geometry, comprising:
inserting rollers in associated roller engagements of an adjustment ring of the variable geometry,
positioning the adjustment ring in relation to a blade bearing ring of the variable geometry such that the roller engagements and recesses on the blade bearing ring allow the rollers to be introduced into a rail of the blade bearing ring,
rotating the adjustment ring,
inserting guide blades, including blade bearing trunnions, in the blade bearing ring, and
attaching an adjusting lever to the blade bearing trunnions in such a way that it is in operative contact with the adjustment ring.