Turbocharger turbine wastegate mechanism

Patent metadata

Field	Value
Publication number	US-9638099-B2
Application number	US-201414194913-A
Country	US
Kind code	B2
Filing date	Mar 3, 2014
Priority date	Mar 3, 2014
Publication date	May 2, 2017
Grant date	May 2, 2017

Abstract

An assembly can include a turbine housing that includes a bore, a wastegate seat and a wastegate passage that extends to the wastegate seat; a bushing configured for receipt by the bore; a rotatable wastegate shaft configured for receipt by the bushing; a wastegate plug extending from the wastegate shaft; a control arm operatively coupled to the wastegate shaft; and a biasing cam operatively coupled to the control arm wherein the biasing cam comprises a disengaged orientation associated with a closed position of the wastegate plug with respect to the wastegate seat and an engaged orientation associated with an open position of the wastegate plug with respect to the wastegate seat. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.

First claim

What is claimed is:

1. An assembly comprising:
a turbine housing that comprises a bore, a wastegate seat and a wastegate passage that extends to the wastegate seat;
a bushing received by the bore wherein an axial end of the bushing comprises a sloping surface that spans an angle about an axis of the bushing between a recessed axial end surface and an upper axial end surface;
a rotatable wastegate shaft received by the bushing;
a wastegate plug that extends from the rotatable wastegate shaft;
a control arm operatively coupled to the rotatable wastegate shaft; and
a cam operatively coupled to the control arm wherein the cam comprises a member that, responsive to rotation of the control arm that transitions the wastegate plug to an open orientation, with respect to the wastegate seat rides the sloping surface of the bushing to an engaged orientation with a zero axial clearance for axial movement of the rotatable wastegate shaft with respect to the bushing and that, responsive to rotation of the control arm that transitions the wastegate plug to a closed orientation with respect to the wastegate seat, rides the sloping surface to a disengaged orientation with a nonzero axial clearance for axial movement of the rotatable wastegate shaft with respect to the bushing.

2. The assembly of claim 1 wherein the nonzero axial clearance of the disengaged orientation provides for self-centering of the wastegate plug with respect to the wastegate seat.

3. The assembly of claim 1 wherein the zero axial clearance prevents rattling between the rotatable wastegate shaft and the bushing.

4. The assembly of claim 1 wherein the cam comprises a base and wherein the member extends from the base.

5. The assembly of claim 1 wherein the rotatable wastegate shaft and the wastegate plug comprise a unitary component.

6. The assembly of claim 1 wherein the wastegate seat comprises a profile defined in part by a cone, wherein the wastegate plug comprises a profile defined at least in part by a portion of a torus for contacting the profile of the wastegate seat defined in part by the cone and wherein, in the disengaged orientation, an axial clearance exists for axial movement of the rotatable wastegate shaft with respect to the bushing that centers the wastegate plug with respect to the wastegate seat.

7. The turbine assembly of claim 1 wherein the axial end of the bushing comprises a plurality of sloping surfaces.

8. The turbine assembly of claim 7 wherein the cam comprises a plurality of members.

9. The turbine assembly of claim 8 wherein each of the plurality of members rides a corresponding one of the plurality of sloping surfaces.

10. The turbine assembly of claim 1 wherein the cam comprises a biasing cam.

11. The turbine assembly of claim 10 wherein the member comprises a biasing member for applying a biasing force to the sloping surface of the bushing.

12. A method comprising:
providing an assembly that comprises
a turbine housing that comprises a bore, a wastegate seat and a wastegate passage that extends to the wastegate seat,
a bushing received by the bore wherein an axial end of the bushing comprises a sloping surface that spans an angle about an axis of the bushing between a recessed axial end surface and an upper axial end surface,
a rotatable wastegate shaft received by the bushing,
a wastegate plug that extends from the rotatable wastegate shaft,
a control arm operatively coupled to the rotatable wastegate shaft, and
a cam operatively coupled to the control arm wherein the cam comprises a member;

rotating the control arm;
responsive to rotating the control arm, causing the member to ride along the sloping surface for reducing an axial clearance between the bushing and the rotatable wastegate shaft;
rotating the control arm in an opposite rotational direction; and
responsive to the rotating in the opposite rotational direction, riding the member along the sloping surface for increasing the axial clearance between the bushing and the rotatable wastegate shaft.

13. The method of claim 12 comprising providing the nonzero axial clearance between at least a portion of the member and the recessed axial end surface.

14. A turbocharger comprising:
a compressor assembly;
a center housing assembly; and
a turbine assembly that comprises
a turbine housing that comprises a bore, a wastegate seat and a wastegate passage that extends to the wastegate seat;
a bushing received by the bore wherein an axial end of the bushing comprises a sloping surface that spans an angle about an axis of the bushing between a recessed axial end surface and an upper axial end surface;
a rotatable wastegate shaft received by the bushing;
a wastegate plug that extends from the rotatable wastegate shaft;
a control arm operatively coupled to the rotatable wastegate shaft; and
a cam operatively coupled to the control arm wherein the cam comprises a member that, responsive to rotation of the control arm that transitions the wastegate plug to an open orientation with respect to the wastegate seat, rides the sloping surface of the bushing to an engaged orientation with a zero axial clearance for axial movement of the rotatable wastegate shaft with respect to the bushing and that, responsive to rotation of the control arm that transitions the wastegate plug to a closed orientation with respect to the wastegate seat, rides the sloping surface of the bushing to a disengaged orientation with a nonzero axial clearance for axial movement of the rotatable wastegate shaft with respect to the bushing.

15. The turbocharger of claim 14 comprising an actuator that comprises a linkage operatively coupled to the control arm and a biasing mechanism that is operatively coupled to the linkage and that is operatively coupled to one or more of the compressor assembly, the center housing assembly and the turbine assembly.

Assignees

• Honeywell Int Inc

Inventors

• Micanek Vit
• Cizek Petr
• Hahn Stanislav

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F01D17/105

  by passing part of the fluid · CPC title

• F02B37/186 Primary

  Arrangements of actuators or linkage for bypass valves · CPC title

• F04B49/22

  by means of valves (F04B49/03 takes precedence) · CPC title

• Y02T10/144

  Cross-Sectional Technologies · mapped topic