Method for introducing a balancing mark into the compressor wheel of a turbocharger, and turbocharger comprising a compressor wheel which has a balancing mark
US-2018313366-A1 · Nov 1, 2018 · US
US10989224B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10989224-B2 |
| Application number | US-201816190864-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 14, 2018 |
| Priority date | Nov 14, 2018 |
| Publication date | Apr 27, 2021 |
| Grant date | Apr 27, 2021 |
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A rotor for a fluid machine includes a wheel that is supported for rotation about an axis of rotation. The wheel includes a back wall with an outer rim edge. The rotor also includes a plurality of blades that are attached to the back wall and that are spaced apart about the axis of rotation. Moreover, the rotor includes an inter-blade area on the back wall between neighboring ones of the plurality of blades. Furthermore, the rotor includes a balancing feature that is included in the inter-blade area on the back wall. The balancing feature intersects and defines part of the outer rim edge.
Opening claim text (preview).
What is claimed is: 1. A rotor for a fluid machine comprising: a wheel that is supported for rotation about an axis of rotation, the wheel including a back wall with a front face, a back face, and an outer rim edge; a plurality of blades that are attached to the back wall and that are spaced apart about the axis of rotation; an inter-blade area on the back wall between neighboring ones of the plurality of blades; and a balancing aperture that is included in the inter-blade area on the front face of the back wall at the outer rim edge, the aperture having a plurality of portions including, at least, a first portion and a second portion, the first portion having a first depth measured from the front face along the axis of rotation, the second portion having a second depth measured from the front face along the axis of rotation, and the second depth being different from the first depth; at least one of the first portion and the second portion of the balancing aperture intersecting and defining part of the outer rim edge. 2. The rotor of claim 1 , wherein at least one of the first portion and the second portion of the balancing aperture is elongate and has a major axis that is arcuate. 3. The rotor of claim 2 , wherein the major axis has a radius that is substantially centered on the axis of rotation. 4. The rotor of claim 1 , wherein the at least one of the first portion and the second portion of the balancing aperture has an area of maximum depth measured from the front face; and wherein the area of maximum depth is disposed inward radially from the outer rim edge. 5. The rotor of claim 1 , wherein the first portion and the second portion are arranged at different radial locations on the front face of the back wall. 6. The rotor of claim 1 , wherein the first portion and the second portion are spaced apart angularly with respect to the axis of rotation. 7. The rotor of claim 1 , wherein the plurality of portions includes a third portion that intersects and shares a common boundary with the second portion. 8. A rotor for a charger device of a fluid machine comprising: a wheel that is supported for rotation about an axis of rotation, the wheel including a back wall, the back wall including a front face, a back face, and an outer rim edge; a plurality of blades that are attached to the front face of the back wall and that are spaced apart about the axis of rotation; an inter-blade area on the front face of the back wall between neighboring ones of the plurality of blades; and a balancing aperture in the front face in the inter-blade area on the front face of the back wall at the outer rim edge, the aperture having a plurality of portions including, at least, a first portion and a second portion, the first portion having a first depth measured from the front face along the axis of rotation, the second portion having a second depth measured from the front face along the axis of rotation, and the second depth being different from the first depth; at least one of the first portion and the second portion of the balancing aperture feature intersecting and defining part of the outer rim edge; the balancing aperture being elongate and having a major axis that is arcuate, the major axis having a radius that is centered substantially on the axis of rotation. 9. The rotor of claim 8 , wherein at least one of the first portion and the second portion of the balancing aperture has a point of maximum depth measured from the front face; and wherein the point of maximum depth is disposed inward radially from the outer rim edge. 10. The rotor of claim 8 , wherein the wheel is a compressor wheel of the rotor. 11. The rotor of claim 10 , wherein the charger device is a turbocharger. 12. The rotor of claim 8 , wherein the first portion and the second portion are arranged at different radial locations on the front face of the back wall. 13. The rotor of claim 8 , wherein the first portion and the second portion are spaced apart angularly with respect to the axis of rotation. 14. The rotor of claim 8 , wherein the plurality of portions includes a third portion that intersects and shares a common boundary with the second portion.
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by removing material · CPC title
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