Motor with multi-phase windings and series-stacked inverter
View Patent ↗In one aspect, a system is described. The system may include a rotor, a plurality of magnets positioned adjacent to the rotor, and a stator defining a plurality of sections. Each of the plurality of sections of the stator may include a plurality of teeth. The system may also include a plurality of winding wires wound around the plurality of teeth of each of the plurality of sections of the stator. The plurality of winding wires wound around the plurality of teeth may define a plurality of single-phase sub-motors. The plurality of single-phase sub-motors have a magnetic design such that at least one of the plurality of single-phase sub-motors are rotationally offset from an adjacent single-phase sub-motor, which may improve motor performance and voltage isolation. The system may also include a plurality of inverters coupled to the plurality of winding wires.
1. A system comprising:
a rotor;
a plurality of magnets positioned adjacent to the rotor;
a stator defining a plurality of sections, wherein each of the plurality of sections of the stator include a plurality of teeth;
a plurality of winding wires wound around the plurality of teeth of each of the plurality of sections of the stator, wherein the plurality of winding wires wound around the plurality of teeth define a plurality of single-phase sub-motors, and wherein at least one of the plurality of single-phase sub-motors is rotationally offset from an adjacent single-phase sub-motor; and
a plurality of inverters coupled to the plurality of winding wires, wherein each of the plurality of inverters comprises four switches, wherein two of the switches are configured to switch at a pulse-width modulation (PWM) frequency, and wherein two of the switches are configured to switch at twice a motor electrical frequency.
2. The system of claim 1 , further comprising:
a rotor shaft disposed coaxial to the rotor and coaxial to each of the plurality of single-phase sub-motors; and
a propeller coupled to the rotor shaft.
3. The system of claim 1 , wherein the plurality of single-phase sub-motors comprises six single-phase sub-motors.
4. The system of claim 3 , wherein a given single-phase sub-motor of the six single-phase sub-motors is phase shifted by one sixth of an electrical cycle from an adjacent single-phase sub-motor.
5. The system of claim 3 , wherein each of the plurality of single-phase sub-motors are rotationally offset from an adjacent single-phase sub-motor.
6. The system of claim 1 , further comprising a control system including a plurality of controllers, wherein a given controller of the plurality of controllers is coupled to each of the plurality of single-phase sub-motors such that each of the plurality of controllers may be configured to individually control a given sub-motor of the plurality of sub-motors.
7. The system of claim 6 , wherein plurality of controllers are configured to cause the system to operate in at least two modes: (i) a flight mode, wherein the stator is configured to cause the rotor to rotate relative to the stator in response to an input of electrical energy to the stator, thereby causing a propeller to rotate, and (ii) a power generation mode, wherein the stator is configured to output electrical energy in response to rotation of the rotor relative to the stator via wind energy acting on the propeller.
8. The system of claim 7 , wherein the electrical energy generated in the power generation mode is transmitted to a ground station via a tether.
9. An aerial wind turbine comprising:
a ground station;
an aerial vehicle;
a rotor/stator assembly comprising:
a rotor,
a rotor shaft,
a plurality of magnets positioned adjacent to the rotor;
a stator defining a plurality of sections, wherein each of the plurality of sections of the stator include a plurality of teeth, wherein the stator is disposed coaxial to the rotor, and wherein the rotor is configured to rotate relative to the stator,
a plurality of winding wires wound around the plurality of teeth of each of the plurality of sections of the stator, wherein the plurality of winding wires wound around the plurality of teeth define a plurality of single-phase sub-motors, and wherein at least one of the plurality of single-phase sub-motors is rotationally offset from an adjacent single-phase sub-motor, and
a plurality of inverters coupled to the plurality of winding wires, wherein each of the plurality of inverters comprises four switches, wherein two of the switches are configured to switch at a pulse-width modulation (PWM) frequency, and wherein two of the switches are configured to switch at twice a motor electrical frequency;
a propeller coupled to the rotor shaft; and
an electrically conductive tether coupled to the stator and to the ground station.
10. The aerial wind turbine of claim 9 , wherein the rotor/stator assembly is configured for at least two modes of operation: (i) a flight mode, wherein the stator is configured to cause the rotor to rotate relative to the stator in response to an input of electrical energy to the stator from the tether, thereby causing the propeller to rotate, and (ii) a power generation mode, wherein the stator is configured to output electrical energy in response to rotation of the rotor relative to the stator via wind energy acting on the propeller, and wherein the generated electrical energy is transmitted to the ground station via the tether.
11. The aerial wind turbine of claim 9 , wherein the plurality of single-phase sub-motors comprises six single-phase sub-motors.
12. The aerial wind turbine of claim 11 , wherein a given single-phase sub-motor of the six single-phase sub-motors is phase shifted by one sixth of an electrical cycle from an adjacent single-phase sub-motor.
13. A system comprising:
a motor system comprising (i) a rotor, (ii) a plurality of magnets positioned adjacent to the rotor; (iii) a stator defining a plurality of sections, wherein each of the plurality of sections of the stator include a plurality of teeth, (iv) a plurality of winding wires wound around the plurality of teeth of each of the plurality of sections of the stator, wherein the plurality of winding wires wound around the plurality of teeth define a plurality of single-phase sub-motors, and wherein at least one of the plurality of single-phase sub-motors is rotationally offset from an adjacent single-phase sub-motor, and (v) a plurality of inverters coupled to the plurality of winding wires, wherein each of the plurality of inverters comprises four switches, wherein two of the switches are configured to switch at a pulse-width modulation (PWM) frequency, and wherein two of the switches are configured to switch at twice a motor electrical frequency; and
a control system comprising a plurality of controllers, wherein a given controller of the plurality of controllers is coupled to each of the plurality of single-phase sub-motors such that each of the plurality of controllers may be configured to individually control a given sub-motor of the plurality of sub-motors.
14. The system of claim 13 , wherein the plurality of single-phase sub-motors comprises six single-phase sub-motors.
15. The system of claim 13 , wherein the control system is configured to cause the system to operate in at least two modes: (i) a flight mode, wherein the stator is configured to cause the rotor to rotate relative to the stator in response to an input of electrical energy to the stator, thereby causing a propeller to rotate, and (ii) a power generation mode, wherein the stator is configured to output electrical energy in response to rotation of the rotor relative to the stator via wind energy acting on the propeller.