Turbocharger turbine wastegate assembly
A turbocharger turbine wastegate assembly includes a turbine housing that includes a wastegate seat and a bore; a bushing with a stepped bore that includes an axial face; a wastegate that includes a shaft, a plug and an arm, where the shaft includes an end portion, a first axial face, a journal portion, a second axial face and a shoulder portion, where the first axial face is defined at least in part by an end portion diameter and a journal portion diameter, and where the second axial face is defined at least in part by the journal portion diameter and a shoulder portion diameter; a mesh spacer disposed radially about an axial length of the end portion of the shaft between the axial face of the stepped bore of the bushing and the first axial face of the shaft; and a control arm connected to the end portion of the shaft where an axial length of the bushing is disposed between the mesh spacer and the control arm.
1. A turbocharger turbine wastegate 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 exterior surface and the interior surface;
a bushing disposed at least partially in the bore of the turbine housing wherein the bushing comprises a stepped bore that comprises a first bore portion, a second bore portion and an axial face;
a wastegate that comprises a shaft, a plug and an arm, wherein the arm extends from the shaft and the plug extends from the arm, wherein the shaft comprises an end portion, a first axial face, a journal portion, a second axial face and a shoulder portion, wherein the first axial face is defined at least in part by an end portion diameter and a journal portion diameter, and wherein the second axial face is defined at least in part by the journal portion diameter and a shoulder portion diameter;
a mesh spacer disposed radially about an axial length of the end portion of the shaft between the axial face of the stepped bore of the bushing and the first axial face of the shaft; and
a control arm connected to the end portion of the shaft wherein an axial length of the bushing is disposed between the mesh spacer and the control arm.
2. The turbocharger turbine wastegate assembly of claim 1 comprising a weld that connects the control arm to the end portion of the shaft.
3. The turbocharger turbine wastegate assembly of claim 1 wherein the mesh spacer imparts a load between the axial face of the stepped bore of the bushing and the first axial face of the shaft.
4. The turbocharger turbine wastegate assembly of claim 1 wherein an axial gap exists between an end of the bushing and the second axial face of the shaft.
5. The turbocharger turbine wastegate assembly of claim 1 wherein an axial length of the bushing exceeds an axial length of the bore of the turbine housing.
6. The turbocharger turbine wastegate assembly of claim 1 wherein the bushing is axially located with respect to the turbine housing.
7. The turbocharger turbine wastegate assembly of claim 1 wherein a diameter of the second bore portion exceeds a diameter of the first bore portion.
8. The turbocharger turbine wastegate assembly of claim 7 wherein an axial length of the second bore portion exceeds an axial length of the first bore portion.
9. The turbocharger turbine wastegate assembly of claim 1 wherein the mesh spacer is disposed in the second bore portion.
10. The turbocharger turbine wastegate assembly of claim 1 wherein a transverse dimension of the mesh spacer exceeds a diameter of the first bore portion.
11. The turbocharger turbine wastegate assembly of claim 1 wherein the mesh spacer contacts the end portion of the shaft.
12. The turbocharger turbine wastegate assembly of claim 1 wherein the mesh spacer is a floating mesh spacer.
13. The turbocharger turbine wastegate assembly of claim 1 wherein the mesh spacer comprises an uncompressed, free-standing state and a compressed, installed state.
14. The turbocharger turbine wastegate assembly of claim 1 wherein the wastegate comprises a unitary component.
15. A method comprising:
positioning a mesh spacer on an end portion of a shaft of a wastegate to form a first subassembly wherein the wastegate comprises a plug and an arm, wherein the arm extends from the shaft and the plug extends from the arm, wherein the shaft comprises an end portion, a first axial face, a journal portion, a second axial face and a shoulder portion, wherein the first axial face is defined at least in part by an end portion diameter and a journal portion diameter, and wherein the second axial face is defined at least in part by the journal portion diameter and a shoulder portion diameter;
providing a second subassembly that comprises a bushing in a bore of a turbine housing wherein the turbine housing comprises an exterior surface, an interior surface that comprises a wastegate seat, wherein the bore extends between the exterior surface and the interior surface, and wherein the bushing comprises a stepped bore that comprises a first bore portion, a second bore portion and an axial face;
inserting at least a portion of the first subassembly into the stepped bore to contact the mesh spacer and the axial face of the stepped bore of the bushing wherein the mesh spacer is disposed radially about an axial length of the end portion of the shaft between the axial face of the stepped bore of the bushing and the first axial face of the shaft; and
fixing a control arm to the end portion of the shaft wherein an axial length of the bushing is disposed between the mesh spacer and the control arm and wherein the mesh spacer imparts a load to the bushing and the wastegate.