Electric compressor
US-2024295220-A1 · Sep 5, 2024 · US
US10273960B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10273960-B2 |
| Application number | US-201415029205-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 13, 2014 |
| Priority date | Oct 14, 2013 |
| Publication date | Apr 30, 2019 |
| Grant date | Apr 30, 2019 |
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An impeller for a side channel flow machine has impeller blades. An inlet region of the impeller blade is off-set from the outlet region. The inlet region is connected to the outlet region via a sloped transition region. The impeller allows a high degree of efficiency of the side channel flow machine and can be produced at particularly low cost.
Opening claim text (preview).
The invention claimed is: 1. An impeller for a side channel continuous flow machine comprising: a ring of impeller blades that delimit blade chambers, in at least one of the impeller's end sides, the impeller blades each having a radially inner inlet region and a radially outer outlet region in a plan view of an end side of the impeller, the impeller blades being inclined differently in the radially inner inlet region and in the radially outer outlet region, wherein respective edges of the impeller blades that adjoin the end side of the impeller have sections that are offset with respect to one another in the radially inner inlet region and in the radially outer outlet region, and in that the radially inner inlet region and the radially outer outlet region are connected to one another via an inclined transition region, wherein an end of each of the impeller blades that faces away from the impeller's end side has a continuous circular arc that extends entirely from the radially outer outlet region to the radially inner inlet region. 2. The impeller as claimed in claim 1 , wherein the radially inner inlet region is inclined more in a rotational direction of the impeller than the radially outer outlet region. 3. The impeller as claimed in claim 2 , wherein the impeller blades are substantially planar in the radially inner inlet region and in the radially outer outlet region. 4. The impeller as claimed in claim 3 , wherein the respective edges of the impeller blades that adjoin the end side of the impeller resembles a shape of a hyperbolic tangent function. 5. The impeller as claimed in claim 4 , wherein the respective edges of the impeller blades that adjoin the end side has a same wall thickness over an entire length of the respective edge. 6. The impeller as claimed in claim 5 , wherein at least a portion of the respective edges of the impeller blades that adjoins the end side point toward a center of the impeller. 7. The impeller as claimed in claim 1 , wherein the impeller blades are substantially planar in the radially inner inlet region and in the radially outer outlet region. 8. The impeller as claimed in claim 1 , wherein each respective edge of the impeller blades that adjoins the end side of the impeller resembles a shape of a hyperbolic tangent function. 9. The impeller as claimed in claim 1 , wherein the respective edge of the impeller blades that adjoins the end side has a same wall thickness over an entire length of the respective edge. 10. The impeller as claimed in claim 1 , wherein at least a portion of the respective edges of the impeller blades that adjoins the end side point toward a center of the impeller. 11. The impeller as claimed in claim 1 , wherein the side channel continuous flow machine is a side channel blower.
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