External rotor aircraft motor having force isolated cantilevered rotor
US-12166399-B2 · Dec 10, 2024 · US
US10630133B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10630133-B2 |
| Application number | US-201515547890-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 13, 2015 |
| Priority date | Apr 13, 2015 |
| Publication date | Apr 21, 2020 |
| Grant date | Apr 21, 2020 |
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In an electric driving apparatus, a sensor magnet is fixed to a first end portion of a rotary shaft of a motor. A sensor device includes a rotation sensor that detects a magnetic field generated by the sensor magnet. The rotation sensor opposes the sensor magnet in an axial direction of the rotary shaft. A control unit mounted on the motor includes an inverter circuit that is connected to an armature winding of the motor via a plurality of feeder wires. The inverter circuit is disposed in a position further from the sensor magnet than the rotation sensor in the axial direction of the rotary shaft. A shield plate formed from a magnetic material is disposed between the rotation sensor and the inverter circuit.
Opening claim text (preview).
The invention claimed is: 1. An electric driving apparatus comprising: a motor that includes a rotary shaft having a first end portion and a second end portion, a stator that includes an armature winding and is disposed around an axis of the rotary shaft, and a rotor that is fixed to the rotary shaft so as to rotate integrally with the rotary shaft relative to the stator; a sensor magnet fixed to the first end portion; a sensor device that opposes the sensor magnet in an axial direction of the rotary shaft, and includes a rotation sensor for detecting a magnetic field generated by the sensor magnet; and a control unit that is mounted on the motor and includes an inverter circuit connected to the armature winding via a plurality of feeder wires, wherein the inverter circuit is disposed in a position further from the sensor magnet than the rotation sensor in the axial direction of the rotary shaft, a shield plate formed from a magnetic material is disposed between the rotation sensor and the inverter circuit, the axis of the rotary shaft passes through a center of the shield plate, a shield through hole is provided in the center of the shield plate, and the shield through hole is disposed at a position away from the rotary shaft in the axial direction of the rotary shaft. 2. The electric driving apparatus according to claim 1 , wherein, when seen along the axis of the rotary shaft, the sensor magnet is disposed within a region of the shield plate and the plurality of feeder wires are disposed outside the region of the shield plate. 3. The electric driving apparatus according to claim 1 , wherein a distance between the shield plate and the rotation sensor in the axial direction of the rotary shaft is at least 7 mm. 4. The electric driving apparatus according to claim 1 , wherein the armature winding includes first and second three-phase AC windings, feeder wires of a U1 phase, a V1 phase, and a W1 phase are connected to the first three-phase AC winding, feeder wires of a U2 phase, a V2 phase, and a W2 phase are connected to the second three-phase AC winding, respective current phase differences between the feeder wires are set at 0° between the U1 phase and the U2 phase, between the V1 phase and the V2 phase, and between the W1 phase and the W2 phase, and positions of the feeder wires of at least one group, among a group constituted by the U1 phase and the U2 phase, a group constituted by the V1 phase and the V2 phase, and a group constituted by the W1 phase and the W2 phase, are out of point symmetry with the axis of the rotary shaft when seen along the axis of the rotary shaft. 5. The electric driving apparatus according to claim 1 , wherein the armature winding includes first and second three-phase AC windings, feeder wires of a U1 phase, a V1 phase, and a W1 phase are connected to the first three-phase AC winding, feeder wires of a U2 phase, a V2 phase, and a W2 phase are connected to the second three-phase AC winding, and respective current phase differences between the feeder wires are set at 30° between the U1 phase and the U2 phase, between the V1 phase and the V2 phase, and between the W1 phase and the W2 phase. 6. The electric driving apparatus according to claim 1 , wherein the armature winding includes first and second three-phase AC windings, feeder wires of a U1 phase, a V1 phase, and a W1 phase are connected to the first three-phase AC winding, feeder wires of a U2 phase, a V2 phase, and a W2 phase are connected to the second three-phase AC winding, and some currents, among currents flowing through the feeder wires of the U1 phase, the V1 phase, the W1 phase, the U2 phase, the V2 phase, and the W2 phase, are permanently stopped. 7. The electric driving apparatus according to claim 1 , wherein the armature winding includes a three-phase AC winding, and the plurality of feeder wires connected to the three-phase AC winding are disposed apart from each other.
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Magnetic effect devices, e.g. Hall-effect or magneto-resistive elements · CPC title
Mounting arrangements for bearing-shields or end plates · CPC title
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including housing for electronic control unit · CPC title
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