Granted Patent B2

US 10,233,827 · App. 15/218,045 · Granted Mar 19, 2019

Abstract

Claims (23)

1. A turbine housing assembly comprising:

a turbine housing that comprises an exterior surface, an interior surface that comprises a wastegate seat, and a bore that extends between the interior surface and the exterior surface;

a bushing disposed at least partially in the bore wherein the bushing comprises a bushing bore and a ring portion of the bushing;

a wastegate that comprises a shaft that extends through the bushing bore to a shaft end, a shaft shoulder disposed in the bushing bore, a plug, and an arm disposed between the shaft and the plug;

a resilient mesh ring encased in the bushing bore between the shaft shoulder and the ring portion of the bushing that absorbs axial thrust energy associated with axial movement of the shaft; and

a control arm connected to the shaft proximate to the shaft end to define an axial distance between a surface of the control arm and the shaft shoulder wherein the resilient mesh ring comprises an axial length that is less than the axial distance.

2. The turbine housing assembly of claim 1 comprising a ring weld that fixes the resilient mesh ring to the bushing.

3. The turbine housing assembly of claim 1 wherein the shaft comprises a journal and wherein the shaft shoulder comprises a shaft journal shoulder.

4. The turbine housing assembly of claim 3 wherein the shaft comprises two journals.

5. The turbine housing assembly of claim 1 wherein the wastegate seat comprises a conical surface.

6. The turbine housing assembly of claim 1 wherein the plug comprises a convex toroidal surface.

7. The turbine housing assembly of claim 1 wherein the control arm is welded to the shaft.

8. The turbine housing assembly of claim 1 wherein a difference between the axial distance and the axial length defines an axial clearance.

9. The turbine housing assembly of claim 8 wherein the axial clearance corresponds to a shim dimension.

10. The turbine housing assembly of claim 1 comprising a shim disposed in a clearance defined by a difference between the axial distance and the axial length.

11. The turbine housing assembly of claim 1 wherein the bushing comprises a shoulder, wherein the exterior surface of the turbine housing comprises a seat surface disposed about the bore and wherein the shoulder of the bushing is seated against the seat surface of the turbine housing.

12. The turbine housing assembly of claim 1 wherein the resilient mesh ring comprises a pre-determined uncompressed operational axial length and a predetermined compressed operational axial length.

13. The turbine housing assembly of claim 1 wherein the bushing bore comprises a plurality of inner diameter.

14. The turbine housing assembly of claim 1 wherein the resilient mesh ring comprises a metal wire mesh ring.

15. The turbine housing assembly of claim 1 wherein the ring portion of the bushing is formed by joining a ring to the bushing.

16. The turbine housing assembly of claim 1 wherein the ring portion of the bushing comprises a welded ring portion.

17. The turbine housing assembly of claim 1 wherein the arm of the wastegate comprises a shoulder that, responsive to axial thrust energy, abuts an end of the bushing to limit outward axial movement of the wastegate.

18. The turbine housing assembly of claim 17 wherein, where the shoulder of the arm abuts the end of the bushing due to axial thrust energy, the resilient mesh ring is compressed with paths therethrough altered that hinder outward flow of gas through the bore of the bushing.

Assignments (8)