Exhaust bypass valve of multi-stage turbocharger
View Patent ↗An assembly for a two-stage turbocharger can include a first turbocharger stage and a second turbocharger stage where one of the stages includes a boss that includes a bore; an exhaust bypass valve that includes an arm pivotable to orient the exhaust bypass valve in an open state and a closed state; a valve shaft disposed at least in part in the bore and operatively coupled to the exhaust bypass valve where the valve shaft includes an inner end, an outer end and an axial stop disposed between the inner end and the outer end; an outer bushing disposed at least in part in the bore and located axially along the valve shaft; and an inner bushing disposed at least in part in the bore and located axially along the valve shaft between the axial stop and a portion of the arm of the exhaust bypass valve.
1. An assembly for an exhaust bypass valve of a two-stage turbocharger, the assembly comprising:
a first turbocharger stage and a second turbocharger stage wherein one of the stages comprises a boss that comprises a bore wherein the bore comprises an outer bore, an opening to the outer bore, an inner bore, a transition region between the outer bore and the inner bore, an inner opening to the inner bore wherein the transition region transitions from a smaller diameter of the inner bore to a larger diameter of the outer bore;
an exhaust bypass valve that comprises an arm pivotable to orient the exhaust bypass valve in an open state and a closed state;
a valve shaft disposed at least in part in the bore and operatively coupled to the exhaust bypass valve wherein the valve shaft comprises an inner end, an outer end and an axial stop disposed between the inner end and the outer end wherein the axial stop is disposed in the inner bore;
an outer bushing disposed at least in part in the bore and located axially along the valve shaft; and
an inner bushing axially fixed at least in part in the inner bore, partially within a chamber that is an exhaust chamber where the exhaust bypass valve operates and located axially along the valve shaft between a portion of the arm of the exhaust bypass valve and the axial stop of the valve shaft wherein one end of the inner bushing and the axial stop and an opposing end of the inner bushing and a portion of the arm of the exhaust bypass valve define an overall axial clearance that limits axial movement of the valve shaft in the bore of the boss.
2. The assembly of claim 1 wherein the arm of the exhaust bypass valve is fixed to the valve shaft to define an axial span between a portion of the arm and the axial stop.
3. The assembly of claim 2 wherein the inner bushing comprises an axial length that is less than the axial span.
4. The assembly of claim 3 wherein a difference between the axial length of the inner bushing and the axial span defines the overall axial clearance.
5. The assembly of claim 4 wherein the overall axial clearance is defined at least in part via a thermal expansion coefficient of the valve shaft and a thermal expansion coefficient of the inner bushing.
6. The assembly of claim 1 wherein the inner bushing and the valve shaft are made of different materials.
7. The assembly of claim 1 wherein the valve shaft comprises a unitary shaft.
8. The assembly of claim 1 wherein the valve shaft comprises a length that is greater than approximately six times an average diameter of the shaft.
9. The assembly of claim 1 wherein the valve shaft comprises at least one annular groove and comprising at least one seal ring disposed at least in part in the annular groove.
10. The assembly of claim 9 wherein the at least one seal ring contacts a surface of one of the bushings.
11. The assembly of claim 1 comprising a crank arm that is bolted to the outer end of the valve shaft.
12. The assembly of claim 1 wherein the boss comprises a boss of a turbine housing.
13. The assembly of claim 1 wherein the boss comprises a boss of an exhaust manifold.
14. The assembly of claim 1 wherein the exhaust bypass valve, in the open state, allows at least a portion of exhaust gas of an internal combustion engine to bypass one of the turbocharger stages.