Turbocharger turbine assembly
A turbine housing of a turbocharge can include a surface that defines a portion of a volute, an annular surface that extends radially inwardly to define a portion of a pressure chamber that is in fluid communication with the volute, a substantially annular plate that defines a portion of the pressure chamber, an annular component, at least one spacer that defines a minimum axial distance between the substantially annular plate and the annular component to define a nozzle that is in fluid communication with the volute and in fluid communication with a turbine wheel space where, responsive to fluid flow in the volute and through the nozzle to the turbine wheel space, the pressure chamber has a fluid pressure that exceeds a fluid pressure of the nozzle to apply a biasing force to the substantially annular plate in an axial direction toward a center housing.
1. A turbocharger comprising:
a center housing;
a bearing disposed in a through bore of the center housing wherein the through bore of the center housing defines a longitudinal axis;
a shaft rotatably supported by the bearing;
a compressor wheel operatively coupled to the shaft;
a turbine wheel operatively coupled to the shaft; and
a turbine housing assembly operatively coupled to the center housing wherein the turbine housing assembly comprises:
a turbine housing that comprises a concave surface that defines a portion of a volute wherein the concave surface extends to a substantially annular surface of the turbine housing that extends radially inwardly in a direction toward the longitudinal axis to an annular surface of the turbine housing to define a portion of a pressure chamber that is in fluid communication with the volute,
a substantially annular plate that defines a portion of the pressure chamber wherein the substantially annular plate is a floating plate,
at least one seal ring disposed radially between the annular surface of the turbine housing and the substantially annular plate that permits axial movement of the substantially annular plate and radial expansion and contraction of the substantially annular plate without binding to the annular surface of the turbine housing,
an annular component,
a resilient heat shield disposed between the annular component and the center housing that forcibly biases the annular component in an axial direction away from the center housing,
a locating feature that axially locates the annular component as forcibly biased in the axial direction, and
at least one spacer wherein the at least one spacer defines a minimum axial distance between the substantially annular plate and the annular component to define a nozzle that is in fluid communication with the volute and in fluid communication with a turbine wheel space defined at least in part by the turbine housing,
wherein the at least one spacer is not physically attached or connected to the substantially annular plate such that the substantially annular plate is in its entirety floatable in an axial direction away from the annular component independent of axial movement of the annular component,
wherein the substantially annular plate expands and contracts responsive to changes in temperature without being constrained by the at least one spacer,
wherein at the minimum axial distance between the substantially annular plate and the annular component, the least one seal ring hinders fluid flow from the pressure chamber to the nozzle,
wherein, responsive to fluid flow in the volute and through the nozzle to the turbine wheel space, the pressure chamber comprises a fluid pressure that exceeds a fluid pressure of the nozzle to apply a biasing force to the substantially annular plate in an axial direction toward the center housing to maintain the minimum axial distance between the substantially annular plate and the annular component as defined by the at least one spacer.
2. The turbocharger of claim 1 wherein the turbine housing comprises a shroud surface.
3. The turbocharger of claim 1 comprising a spring disposed between the substantially annular plate and the turbine housing.
4. The turbocharger of claim 1 comprising at least one bolt that connects the annular component to the center housing.
5. The turbocharger of claim 1 wherein the substantially annular plate comprises opposing surfaces that extend between an inner perimeter and an outer perimeter.
6. The turbocharger of claim 5 wherein the opposing surfaces are substantially parallel.
7. The turbocharger of claim 1 wherein the substantially annular plate comprises a substantially rectangular cross-sectional profile.
8. The turbocharger of claim 1 wherein the substantially annular plate comprises an annular groove that seats at least one of the at least one seal ring.
9. The turbocharger of claim 1 wherein the turbine housing comprises an annular groove that seats at least one of the at least one seal ring.
10. The turbocharger of claim 1 wherein a portion of the turbine housing defines the nozzle with respect to the annular component.
11. The turbocharger of claim 1 wherein the nozzle comprises a fixed portion and a floating portion, wherein the annular component defines in part the fixed portion and wherein the substantially annular plate defines in part the floating portion.
12. The turbocharger of claim 1 wherein the locating feature is a component that is clamped between the center housing and the turbine housing to axially locate the annular component.
13. The turbocharger of claim 1 comprising vanes disposed in the nozzle.
14. The turbocharger of claim 13 wherein the minimum axial distance between the substantially annular plate and the annular component as defined by the at least one spacer is greater than a maximum vane height of the vanes.