Sheet metal turbine housing with biaxial volute configuration
View Patent ↗Turbine housing assemblies and related turbocharger systems are provided. One exemplary turbine housing assembly includes and inner shell and an outer shell. The inner shell includes an inner base portion defining an inlet and a volute portion defining an outer contour of a volute in fluid communication with the inlet. The outer shell circumscribing the volute portion in a radial plane and includes an outer base portion circumscribing the inner base portion. The inner shell includes a first plurality of sheet metal structures joined to one another in the radial plane, the outer shell includes a second plurality of sheet metal structures, and first portions of the second plurality of sheet metal structures surrounding the volute portion are joined to one another in an axial plane transverse to the radial plane.
1. A turbine housing assembly comprising:
an inner shell comprising:
an inner base portion defining an inlet; and
a volute portion defining an outer contour of a volute in fluid communication with the inlet;
an outer shell circumscribing the volute portion in a radial plane and including an outer base portion circumscribing the inner base portion, wherein:
the inner shell comprises a first plurality of sheet metal structures joined to one another in the radial plane;
the outer shell comprises a second plurality of sheet metal structures;
first portions of the second plurality of sheet metal structures surrounding the volute portion are joined to one another in an axial plane transverse to the radial plane;
a first extension of the inner base portion relative to a turbine wheel rotational axis is greater than a second extension of the outer base portion relative to the turbine wheel rotational axis; and
a third extension of the outer shell along the turbine wheel rotational axis distal to a turbine wheel is greater than a fourth extension of the inner shell along the turbine wheel rotational axis distal to the turbine wheel.
2. The turbine housing assembly of claim 1 , wherein:
the first plurality of sheet metal structures are coupled about the volute portion; and
second portions of the second plurality of sheet metal structures enclosing the volute portion in an axial direction are coupled diametrically.
3. The turbine housing assembly of claim 1 , wherein the outer shell defines a bearing opening having a radial dimension greater than a radial dimension of the volute portion and an outlet opening in an axial direction opposite the bearing opening.
4. The turbine housing assembly of claim 3 , wherein the outer shell encloses the inner shell in the axial direction opposite the bearing opening.
5. The turbine housing assembly of claim 1 , wherein:
each of the first plurality of sheet metal structures includes a flange extending radially outward from the volute portion; and
the flanges of the first plurality of sheet metal structures are welded together.
6. The turbine housing assembly of claim 1 , wherein each of the second plurality of sheet metal structures comprises an arcuate portion extending from a respective portion of the outer base portion.
7. The turbine housing assembly of claim 6 , wherein an interface between the arcuate portions is welded in an axial direction substantially parallel to the turbine wheel rotational axis.
8. The turbine housing assembly of claim 1 , wherein a thickness of the outer shell is greater than a thickness of the inner shell.
9. The turbine housing assembly of claim 1 , wherein the inner shell and the outer shell are freestanding with respect to one another.
10. The turbine housing assembly of claim 1 , wherein the first portions of the second plurality of sheet metal structures overlap in an axial direction aligned with the turbine wheel rotational axis.
11. A turbine housing assembly comprising:
an inner shell comprising a first plurality of sheet metal structures joined to one another at a first seam in a radial plane; and
an outer shell comprising a second plurality of sheet metal structures joined to one another at a second seam in an axial plane transverse to the radial plane, wherein:
the inner shell includes a volute portion defining an outer contour of a volute in the radial plane;
the outer shell substantially surrounds the volute portion and encloses the volute portion in an axial direction; and
an outer base portion of the outer shell circumscribes an inner base portion of the inner shell that defines an inlet in fluid communication with the volute;
a first extension of the inner base portion relative to a turbine wheel rotational axis is greater than a second extension of the outer base portion relative to the turbine wheel rotational axis; and
a third extension of the outer shell along the turbine wheel rotational axis distal to a turbine wheel is greater than a fourth extension of the inner shell along the turbine wheel rotational axis distal to the turbine wheel.
12. The turbine housing assembly of claim 11 , wherein a thickness of the outer shell is greater than a thickness of the inner shell.
13. The turbine housing assembly of claim 11 , wherein the volute portion of the first plurality of sheet metal structures is welded about at least a portion of a perimeter to provide the first seam.
14. The turbine housing assembly of claim 13 , wherein portions of the second plurality of sheet metal structures are welded along at least a portion of a radius to provide the second seam.
15. The turbine housing assembly of claim 14 , wherein the portions of the second plurality of sheet metal structures enclose the volute portion in the axial direction.
16. The turbine housing assembly of claim 11 , wherein:
each of the first plurality of sheet metal structures includes a flange extending radially outward; and
the flanges of the first plurality of sheet metal structures are welded together about the volute portion.
17. The turbine housing assembly of claim 11 , wherein the inner shell and the outer shell are freestanding with respect to one another.
18. A turbine housing assembly comprising:
an inner sheet metal shell comprising a first pair of sheet metal structures coupled together along a radial plane orthogonal to a turbine wheel rotational axis; and
an outer sheet metal shell comprising a second pair of sheet metal structures coupled together along a first plane transverse to the radial plane, wherein:
each of the first pair of sheet metal structures includes a volute portion defining an outer contour of a volute in the radial plane and a base portion defining an inlet in fluid communication with the volute;
each of the second pair of sheet metal structures includes an arcuate portion radially overlapping at least a portion of the volute portions in the radial plane and an outer base portion radially overlapping at least a portion of the base portions in a second plane transverse to the radial plane;
a first extension of the base portion of the first pair of sheet metal structures relative to a turbine wheel rotational axis is greater than a second extension of the outer base portion of the second pair of sheet metal structures relative to the turbine wheel rotational axis; and
a third extension of the outer sheet metal shell along the turbine wheel rotational axis distal to a turbine wheel is greater than a fourth extension of the inner sheet metal shell along the turbine wheel rotational axis distal to the turbine wheel.
19. The turbine housing assembly of claim 18 , wherein:
each of the first pair of sheet metal structures includes a flange extending radially outward about the volute portion;
the flanges of the first pair of sheet metal structures are coupled together circumferentially about the volute portion;
overlapping portions of the arcuate portions are coupled together in an axial direction aligned with the turbine wheel rotational axis to surround the volute portions; and
each of the second pair of sheet metal structures includes a tapered outlet portion coupled to the other to enclose the volute portion in the axial direction.