Electric direct drive for aircraft propulsion and lift
The present disclosure provides an apparatus with a prime mover coupled to a generator that is directly electrically coupled to an electric motor. A propeller or fan may be coupled to and driven by the electric motor. A bi-directional power converter may be coupled to the generator and further coupled to an energy storage device. The energy storage device may be selectively coupled to the electric motor. Methods of using the apparatus are also provided.
1. An apparatus of an aircraft propulsion system, comprising:
a prime mover of an aircraft coupled to a generator;
an electric motor electrically coupled to the generator; and
a bi-directional power converter coupled to the generator and an energy storage device,
wherein the energy storage device is selectively coupled to the electric motor such that when emergency power is demanded the bi-directional power converter inverts DC power from the energy storage device to AC power for the electric motor.
2. The apparatus of claim 1 , wherein the energy storage device only carries sufficient energy to deliver the aircraft from an operating altitude to ground.
3. The apparatus of claim 1 , wherein the bi-directional power converter includes a DC/AC converter to convert AC power from the generator to DC power to charge the energy storage device.
4. The apparatus of claim 1 , wherein the electric motor is at least one of a polyphase synchronous motor and a wound field synchronous motor.
5. The apparatus of claim 1 , wherein the generator is at least one of a wound field synchronous polyphase electric generator and a permanent magnet polyphase electric generator.
6. The apparatus of claim 1 , wherein the energy storage device comprises a battery.
7. The apparatus of claim 1 , wherein the energy storage device comprises an engine generator.
8. An aircraft propulsion system comprising:
a prime mover coupled to an electric generator;
first and second electric motors electrically coupled to the electric generator; and
a bi-directional power converter coupled to the electric generator and an energy storage device,
wherein the energy storage device is selectively coupled to the first and second electric motors such that when emergency power is demanded the bi-directional power converter inverts DC power from the energy storage device to AC power for the first and second electric motors.
9. The system of claim 8 , wherein the energy storage device only carries sufficient energy to deliver the aircraft from an operating altitude to ground.
10. The system of claim 8 , wherein the bi-directional power converter includes a DC/AC converter to convert AC power from the generator to DC power to charge the energy storage device.
11. The system of claim 8 , wherein at least one of the first and second electric motors is at least one of a polyphase synchronous motor and a wound field synchronous motor.
12. The system of claim 8 , wherein the generator is at least one of a wound field synchronous polyphase electric generator and a permanent magnet polyphase electric generator.
13. The system of claim 8 , wherein the energy storage device comprises a battery.
14. The system of claim 8 , wherein the energy storage device comprises an engine generator.
15. A method of an aircraft propulsion system, comprising:
coupling a prime mover of an aircraft to an electric generator that is electrically coupled to an electric motor;
varying the speed of the electric motor via variations in at least one of a speed of the prime mover and a field excitation; and
delivering only sufficient energy from the energy storage device to deliver the aircraft from an operating altitude to ground.
16. The method of claim 15 , wherein the bi-directional power converter includes a DC/AC converter, and further comprising:
converting AC power from the generator to DC power to charge the energy storage device.
17. The method of claim 15 , wherein the electric motor is at least one of a polyphase synchronous motor and a wound field synchronous motor.
18. The method of claim 15 , wherein the generator is at least one of a wound field synchronous polyphase electric generator and a permanent magnet polyphase electric generator.
19. The method of claim 15 , wherein the energy storage device comprises a battery.
20. The method of claim 15 , wherein the energy storage device comprises an engine generator.