Rotary-Wing Vehicle, and Rotary-Wing Turbine
US-2024328327-A1 · Oct 3, 2024 · US
US10174669B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10174669-B2 |
| Application number | US-201515315502-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 27, 2015 |
| Priority date | Jun 3, 2014 |
| Publication date | Jan 8, 2019 |
| Grant date | Jan 8, 2019 |
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A turbocharger for a motor vehicle, including a compressor, which has a compressor wheel situated on a rotatably supported shaft, an electric machine being situated in a pipe section of an axial compressor inlet, the electric machine including a rotor situated on the shaft and a stator situated on the pipe section. The stator has multiple webs projecting inward which are distributed over the circumference and extend at least essentially in an axial direction, the webs being used for forming flow channels which extend in an axial direction and are situated at a distance from one another.
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What is claimed is: 1. A turbocharger for a motor vehicle, comprising: a compressor which includes a compressor wheel situated on a rotatably supported shaft, an electric machine situated in a pipe section of an axial compressor inlet, the electric machine including a rotor situated on the shaft, and a stator situated on the pipe section; wherein the stator has multiple webs projecting inward which are distributed over a circumference of the stator and extend in an axial direction, the webs being used for forming flow channels which extend in an axial direction and are situated at a distance from one another; and wherein the webs are part of a stator core of the stator and are partially wound by windings, and wherein each of the webs has an aerodynamic, flow-optimized, drop-shaped profile formed in an axial extension. 2. The turbocharger as recited in claim 1 , wherein the webs are situated uniformly distributed over the circumference. 3. The turbocharger as recited in claim 1 , wherein at least the webs of the stator are made from a ferromagnetic material. 4. The turbocharger as recited in claim 1 , wherein the stator is provided with at least one winding in the area of the webs which only partially fills the flow channel. 5. The turbocharger as recited in claim 1 , wherein the turbocharger is an exhaust gas turbocharger and has a turbine including a rotatably supported turbine wheel, which is operatively connected to the compressor wheel by the shaft. 6. The turbocharger as recited in claim 5 , wherein the compressor wheel and the turbine wheel are connected to one another operatively by a freewheel clutch which allows the compressor wheel to overtake the turbine wheel.
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