Spiral grooved thrust generator on turbine wheel back plate
Turbochargers for use in an engine having an internal combustion engine. The design includes, in examples, a shaft having a rotation axis, a turbine housing, a compressor housing, a center housing extending from the turbine housing to the compressor housing with the shaft therethrough, a turbine wheel disposed in the turbine housing and operatively connected to the shaft, and a compressor wheel disposed in the compressor housing and operatively connected to the shaft. A turbine backplate structure is provided having one or more grooves adjacent a back side of the turbine wheel. The turbine backplate structure may be formed on the central housing, or may be a separate backplate installed in the central housing.
1. A turbocharger comprising:
a shaft having a rotational axis;
a turbine housing;
a compressor housing;
a center housing connecting the turbine housing and compressor housing, with the shaft extending within the center housing;
a turbine wheel disposed in the turbine housing and operatively connected to the shaft; and
a compressor wheel disposed in the compressor housing and operatively connected to the shaft;
further comprising a turbine backplate structure having one or more grooves adapted to generate an axial force along the rotational axis of the shaft.
2. The turbocharger of claim 1 , wherein the turbine backplate structure is formed on the center housing and facing the turbine wheel.
3. The turbocharger of claim 1 , wherein the turbine backplate structure is a separate piece positioned between the turbine wheel and the center housing, with the shaft passing through the separate piece.
4. The turbocharger of claim 1 , wherein the one or more grooves extend inward from a first circumference to a second circumference on the turbine backplate structure.
5. The turbocharger of claim 4 , wherein the one or more grooves have a depth which varies from a first end to a second end thereof.
6. The turbocharger of claim 4 , wherein the one or more grooves have a depth which does not vary from a first end to a second end thereof.
7. The turbocharger of claim 4 , wherein:
the turbine housing has an inlet and an outlet,
the inlet adapted to receive exhaust gasses from a combustion chamber,
air passing from the inlet to the outlet creates a force against the turbine wheel in a first direction, and
the grooves extend from a first end at the first circumference to a second end at the second circumference in the first direction.
8. The turbocharger of claim 4 , wherein:
the turbine housing has an inlet and an outlet,
the inlet adapted to receive exhaust gasses from a combustion chamber,
air passing from the inlet to the outlet creates a force against the turbine wheel in a first direction, and
the grooves extend from a first end at the first circumference to a second end at the second circumference in a direction opposite the first direction.
9. The turbocharger of claim 4 , wherein the one or more grooves each have an open end at the first circumference, and a closed end at the second circumference.
10. The turbocharger of claim 4 , wherein the one or more grooves each have a closed end at the first circumference, and a closed end at the second circumference.
11. The turbocharger of claim 4 , wherein the one or more grooves each have an open end at the first circumference, and an open end at the second circumference.
12. The turbocharger of claim 4 , wherein the one or more grooves each have a closed end at the first circumference, and an open end at the second circumference.
13. The turbocharger of claim 1 , wherein the turbine housing has an inlet and an outlet, and air passing from the inlet to the outlet creates a force against the turbine wheel in a first direction, and the one or more grooves include:
an inner set of grooves with a first orientation; and
an outer set of grooves with a second orientation.
14. The turbocharger of claim 13 , wherein the first orientation is in the first direction, and the second orientation is in the first direction.
15. The turbocharger of claim 13 , wherein the first orientation is in the first direction, and the second orientation is opposite of the first direction.
16. The turbocharger of claim 13 , wherein the first orientation is opposite of the first direction, and the second orientation is in the first direction.
17. The turbocharger of claim 13 , wherein the first orientation is opposite of the first direction, and the second orientation is opposite of the first direction.
18. The turbocharger of claim 1 , further comprising an electric motor coupled to the shaft, the electric motor configured to provide torque to the shaft in response to a control signal from a controller, wherein the controller is configured to generate the control signal to maintain a minimum speed on the shaft to thereby provide thrust bearing force using the grooves.
19. An engine system comprising an engine having one or more combustion chambers, an intake manifold, an exhaust manifold, and a turbocharger as in claim 1 , wherein the intake manifold is coupled to an airflow system which provides charged air from the compressor housing to the intake manifold, and the exhaust manifold is coupled by an exhaust system to the turbine housing.
20. A method of controlling a turbocharger comprising:
monitoring a speed of the turbocharger relative to a lower boundary; and
controlling the speed of the turbocharger to stay above the lower boundary;
wherein the turbocharger includes:
a shaft having a rotational axis;
a turbine housing;
a compressor housing;
a center housing connecting the turbine housing and compressor housing, with the shaft extending within the center housing;
a turbine wheel disposed in the turbine housing and operatively connected to the shaft;
a compressor wheel disposed in the compressor housing and operatively connected to the shaft; and
a turbine backplate structure having one or more grooves adapted to generate an axial force along the rotational axis of the shaft when the turbocharger is operated at or above the lower boundary.