Two-sided turbocharger wheel with differing blade parameters
View Patent ↗A two-sided turbocharger compressor wheel and a housing forming a diffuser for the compressor. A first side and a second side of the compressor wheel are characterized by different values of a trim and of an annulus area. A first side of the diffuser surrounds the first side of the compressor wheel, and a second side of the diffuser surrounds the second side of the compressor wheel. The first and second sides of the diffuser are characterized by different annulus area ratios. The blades of the first and second sides of the compressor wheel are angularly offset from one another. The compressor wheel is configured for greater flow through the side of the compressor wheel that faces away from a related turbine wheel.
1. A two-sided turbocharger compressor wheel, comprising:
a hub defining an axial axis of rotation; and
a plurality of blades including a first set of compressor blades attached to a first axial side of the hub; and a second set of compressor blades attached to a second axial side of the hub, the first set of compressor blades being completely axially separate from the second set of compressor blades;
wherein the first set of compressor blades defines a first inducer;
wherein the second set of compressor blades defines a second inducer, wherein the first inducer opens in a direction away from the second inducer, and wherein the second inducer opens in a direction axially opposite from the direction that the first inducer opens;
wherein the first set of compressor blades are characterized by a first set of blade parameters consisting of a first wheel trim and a first annulus area;
wherein the second set of compressor blades are characterized by a second set of blade parameters consisting of a second wheel trim and a second annulus area; and
wherein the values of the first set of blade parameters are not all identical to the values of the second set of blade parameters.
2. The two-sided turbocharger compressor wheel of claim 1 , wherein at least some of the root trailing edges of the blades of the second axial side of the hub are at different circumferential locations than the root trailing edges of any of the blades of the first axial side of the hub.
3. The two-sided turbocharger compressor wheel of claim 2 , wherein all of the root trailing edges of the blades of the second axial side of the hub are at different circumferential locations than the root trailing edges of any of the blades of the first axial side of the hub.
4. The two-sided turbocharger compressor wheel of claim 3 , wherein the root trailing edge of each of the blades of the second axial side of the hub are at a location that is angularly offset around the axis of rotation from the location of a root trailing edge of a corresponding blade of the first axial side of the hub by a singular angle.
5. The two-sided turbocharger compressor wheel of claim 4 , wherein the root trailing edge of each of the blades of the second axial side of the hub are at a location that is angularly half way between two consecutive blades of the first axial side of the hub around the axis of rotation.
6. A turbocharger, comprising:
a turbocharger housing; and
a rotor being mounted for axial rotation within the turbocharger housing, the rotor including a shaft extending axially between a turbine wheel and the two-sided turbocharger compressor wheel of claim 1 .
7. The turbocharger of claim 6 , wherein:
the housing defines a diffuser for the two-sided turbocharger compressor wheel, the diffuser including a first portion surrounding the first set of compressor blades, and the diffuser including an axially separate second portion surrounding the second set of compressor blades;
the diffuser is characterized by a first annulus area ratio for the diffuser first portion and by a second annulus area ratio for the diffuser second portion; and
the first annulus area ratio is not identical to the second annulus area ratio.