Turbine wheel with reduced inertia
A turbine wheel for a turbocharger is provided. The turbine wheel includes a plurality of blades and a mid-plane is defined between a pressure side and a suction side of adjacent blades. Each of the blades has a leading edge, and is coupled to the wheel hub along a respective blade hub camber line. The wall has a first radii at the leading edge that extends for a first circumferential distance adjacent to the suction side. The first circumferential distance is at least 12% of a circumferential distance that extends between adjacent blades. The wheel hub includes a plurality of scallops defined through the wall. Each of the scallops is asymmetrical about the mid-plane. For each of the scallops, the wall has a second minimum radii defined offset from the mid-plane toward the suction side and a third minimum radii defined offset from the mid-plane toward the pressure side.
1. A turbine wheel for a turbocharger, comprising:
a plurality of blades each having a pressure side and a suction side, each of the plurality of blades coupled to a wheel hub along a root of the blade such that the pressure side of each one of the plurality of blades faces the suction side of another one of the plurality of blades about the wheel hub, with a mid-plane defined between the pressure side and the suction side of adjacent ones of the plurality of blades, each of the plurality of blades has a leading edge that terminates at a wall of the wheel hub, each of the plurality of blades coupled to the wheel hub along a respective blade hub camber line, the wall having a first radius at the leading edge of each of the plurality of blades that extends for a first circumferential distance adjacent to the suction side of each of the plurality of blades, the first circumferential distance is at least 12% of a circumferential distance that extends between the adjacent ones of the plurality of blades; and
the wheel hub includes a plurality of scallops defined through the wall of the wheel hub between the adjacent ones of the plurality of blades, with each of the plurality of scallops asymmetrical about the mid-plane, and for each of the plurality of scallops, the wall of the wheel hub has a second minimum radius defined offset from the mid-plane toward the suction side of a respective one of the plurality of blades and a third minimum radius defined offset from the mid-plane toward the pressure side of another one of the plurality of blades, with the second minimum radius less than the third minimum radius and the first radius.
2. The turbine wheel of claim 1 , wherein the wall has a fourth radius defined between the second minimum radius and the third minimum radius, the fourth radius greater than the second minimum radius and the third minimum radius, and less than the first radius.
3. The turbine wheel of claim 2 , wherein each of the plurality of scallops is defined by a plurality of segments, which cooperate to transition from the first radius to the second minimum radius, from the second minimum radius to the fourth radius, from the fourth radius to the third minimum radius and the third minimum radius to the first radius along the wall of the wheel hub.
4. The turbine wheel of claim 3 , wherein the plurality of segments includes a first segment that transitions from the first radius to the second minimum radius and the first segment is offset from the mid-plane toward the suction side.
5. The turbine wheel of claim 4 , wherein the first segment is arcuate.
6. The turbine wheel of claim 3 , wherein the plurality of segments includes a second segment that transitions from the second minimum radius to the fourth radius and the second segment is offset from the mid-plane toward the suction side.
7. The turbine wheel of claim 6 , wherein the second segment has an inclined surface.
8. The turbine wheel of claim 3 , wherein the plurality of segments includes a third segment that transitions from the fourth radius to the third minimum radius, the third segment crosses the mid-plane and the third segment has a sloped surface.
9. The turbine wheel of claim 3 , wherein the plurality of segments includes a fourth segment that transitions from the fourth radius to the first radius, the fourth segment is offset from the mid-plane toward the pressure side and the fourth segment is substantially planar.
10. The turbine wheel of claim 1 , wherein the plurality of scallops are defined through the wall of the wheel hub along an axis substantially parallel to a center line of the wheel hub.
11. The turbine wheel of claim 1 , wherein the plurality of scallops are defined through the wall of the wheel hub along an axis that is substantially oblique to a center line of the wheel hub.
12. The turbine wheel of claim 1 , wherein the wall extends from the leading edge of the plurality of blades adjacent to the suction side toward the mid-plane at the first radius for the first circumferential distance, which is less than 50% of a second circumferential distance defined between the blade hub camber line of each of the plurality of blades along the suction side and the mid-plane of the each of the plurality of blades.
13. The turbine wheel of claim 1 , wherein the wall extends from the leading edge of the plurality of blades adjacent to the suction side toward the mid-plane at the first radius for the first circumferential distance, which is less than 120% of a second circumferential distance defined between the blade hub camber line of each of the plurality of blades along the suction side and the mid-plane of each of the plurality of blades.
14. A turbine wheel for a turbocharger, comprising:
a plurality of blades each having a pressure side and a suction side, each of the plurality of blades coupled to a wheel hub along a root of the blade such that the pressure side of each one of the plurality of blades faces the suction side of another one of the plurality of blades about the wheel hub, with a mid-plane defined between the pressure side and the suction side of adjacent ones of the plurality of blades, each of the plurality of blades has a leading edge that terminates at a wall of the wheel hub, each of the plurality of blades coupled to the wheel hub along a respective blade hub camber line, the wall having a first radius at the leading edge of each of the plurality of blades, the wall extends from the leading edge of each of the plurality of blades adjacent to the suction side toward the mid-plane at the first radius for a first circumferential distance, which is less than 120% of a second circumferential distance defined between the blade hub camber line of each of the plurality of blades along the suction side and the mid-plane of each of the plurality of blades and the first circumferential distance is at least 12% of a circumferential distance that extends between the adjacent ones of the plurality of blades; and
the wheel hub includes a plurality of scallops defined through the wall of the wheel hub between the adjacent ones of the plurality of blades, with each of the plurality of scallops asymmetrical about the mid-plane, and for each of the plurality of scallops, the wall of the wheel hub has a second minimum radius defined offset from the mid-plane toward the suction side of a respective one of the plurality of blades and a third minimum radius defined offset from the mid-plane toward the pressure side of another one of the plurality of blades, with the second minimum radius less than the third minimum radius and the first radius,
wherein the wall has a fourth radius defined between the second minimum radius and the third minimum radius, the fourth radius greater than the second minimum radius and the third minimum radius, and less than the first radius.
15. The turbine wheel of claim 14 , wherein each of the plurality of scallops is defined by a plurality of segments, which cooperate to transition from the first radius to the second minimum radius, from the second minimum radius to the fourth radius, from the fourth radius to the third minimum radius and the third minimum radius to the first radius along the wall of the wheel hub.
16. The turbine wheel of claim 15 , wherein the plurality of segments includes a first segment that transitions from the first radius to the second minimum radius and the first segment is offset from the mid-plane toward the suction side.
17. The turbine wheel of claim 15 , wherein the plurality of segments includes a second segment that transitions from the second minimum radius to the fourth radius and the second segment is offset from the mid-plane toward the suction side.
18. The turbine wheel of claim 15 , wherein the plurality of segments includes a third segment that transitions from the fourth radius to the third minimum radius and the third segment crosses the mid-plane.
19. The turbine wheel of claim 15 , wherein the plurality of segments includes a fourth segment that transitions from the fourth radius to the first radius and the fourth segment is offset from the mid-plane toward the pressure side.