A compressor for an internal combustion engine is provided. The compressor includes a compressor shaft having compressor blades attached thereto, positioned in an intake air duct, and rotating about an axis during compressor operation and a magnetic bearing positioned upstream of the compressor blad
A compressor for an internal combustion engine is provided. The compressor includes a compressor shaft having compressor blades attached thereto, positioned in an intake air duct, and rotating about an axis during compressor operation and a magnetic bearing positioned upstream of the compressor blades in the intake air duct, including a ring positioned around the compressor shaft, stator electrics arranged in the ring, and at least two magnets arranged on the compressor shaft configured to exert a magnetic force on the stator electrics to form an air gap between the ring and the compressor shaft.
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1. A compressor for an internal combustion engine comprising: a compressor shaft which is provided with compressor blades positioned in an intake air duct, the compressor shaft and compressor blades configured to rotate about an axis of rotation; anda magnetic bearing positioned upstream of the comp
1. A compressor for an internal combustion engine comprising: a compressor shaft which is provided with compressor blades positioned in an intake air duct, the compressor shaft and compressor blades configured to rotate about an axis of rotation; anda magnetic bearing positioned upstream of the compressor blades in the intake air duct, the magnetic bearing including a ring positioned around the compressor shaft with an air gap between the ring and the compressor shaft, stator electrics arranged in the ring, and at least two magnets mounted within respective magnetic recesses on the compressor shaft, the at least two magnets configured to exert a magnetic force on the stator electrics. 2. The compressor of claim 1, wherein the ring is retained by at least one strut in the intake air duct. 3. The compressor of claim 2, wherein a supply line for the stator electrics is arranged within the at least one strut. 4. The compressor of claim 2, wherein the at least one strut has a drop-shaped cross-section. 5. The compressor of claim 1, wherein the compressor shaft is connected to a turbine shaft of an exhaust gas turbine such that torque is transmitted from the turbine shaft to the compressor shaft. 6. The compressor of claim 1, wherein the at least two magnets and the stator electrics are configured to repel one another via magnetic forces. 7. The compressor of claim 1, wherein the magnetic bearing is formed as an electric motor. 8. A compressor comprising: a compressor shaft having compressor blades and positioned in an intake air duct;a magnetic bearing positioned upstream of the compressor blades in the duct, including a ring positioned around the compressor shaft, stator electrics arranged in the ring, and at least two magnets arranged on the compressor shaft configured to exert a magnetic force on the stator electrics to form an air gap between the ring and the compressor shaft; anda strut coupled to the ring and a housing of the intake air duct;wherein the strut includes a curved surface on an upstream side of the strut and a second curved surface on a downstream side of the strut, and the strut tapers in the downstream direction, the upstream side and the downstream side in a direction of air flow; andwherein the strut includes one or more electrical conduits for coupling the stator electrics with a controller. 9. The compressor of claim 8, where the stator electrics include wires extending around the ring. 10. The compressor of claim 9, where the wires are enclosed by the ring. 11. The compressor of claim 8, where the one or more electric conduits extend through the strut. 12. The compressor of claim 8, where the strut extends through a section of the intake air duct. 13. The compressor of claim 8, where the controller is configured to electrically drive the stator electrics to form the air gap. 14. The compressor of claim 8, where the stator electrics are configured to be electrically driven by the controller to apply torque to the compressor shaft. 15. The compress of claim 14, where the controller is configured to drive the stator electrics while the compressor shaft is receiving rotational input from a turbine shaft rotationally coupled to the compressor shaft. 16. The compressor of claim 14, where the controller is configured to drive the stator electrics when the compressor shaft is rotating below a threshold speed. 17. The compressor of claim 8, where the at least two magnets are permanent magnets. 18. A motor vehicle comprising: an internal combustion engine;a supply air branch providing intake air to the internal combustion engine; anda compressor arranged in the supply air branch, the compressor including: a compressor shaft which is provided with compressor blades positioned in an intake air duct, the compressor shaft and compressor blades configured to rotate about an axis of rotation;a magnetic bearing positioned upstream of the compressor blades in the intake air duct, the magnetic bearing including a ring positioned around the compressor shaft with an air gap between the ring and the compressor shaft, stator electrics arranged in the ring, and at least two magnets mounted within respective magnetic recesses on the compressor shaft, the at least two magnets configured to exert a magnetic force on the stator electrics; anda strut coupled to the ring and a housing of the intake air duct, the strut including a curved surface on an upstream side and a second curved surface on a downstream side, the upstream side and the downstream side in a direction of air flow in the intake air duct.
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