Electric drive system line replaceable unit with integrated collective actuation
One embodiment is an electric drive system for an aircraft comprising a plurality of redundant motors, wherein power generated by the plurality of motors is used to drive a rotor system comprising a rotor shaft having a plurality of rotor blades connected thereto; a gear box associated with the plurality of redundant motors; a collective actuator for controlling a collective pitch of the rotor blades connected to the rotor shaft; and at least one structural element for retaining the redundant motors, the gear box, and the collective actuator together as a single integrated unit.
1. An electric drive system comprising:
a plurality of redundant motors arranged in a stack relative to one another, wherein power generated by the plurality of motors is used to drive a rotor system comprising a rotor shaft having a plurality of rotor blades connected thereto;
a gear box associated with the plurality of redundant motors;
a collective actuator for controlling a collective pitch of the rotor blades connected to the rotor shaft; and
at least one structural element for retaining the stack of redundant motors, the gear box, and the collective actuator together as a single integrated unit.
2. The electric drive system of claim 1 further comprising a cooling fan for drawing air across an electronic component to cool the electronic component and for expelling air into an oil cooler for cooling oil contained therein.
3. The electric drive system of claim 2 , wherein the cooling fan is mechanically powered by the rotor shaft.
4. The electric drive system of claim 2 , wherein the cooling fan is electrically powered.
5. The electric drive system of claim 1 further comprising an oil distribution system for distributing oil cooled by the oil cooler to at least one motor and at least one gearbox, wherein the distributed oil is used to cool the at least one motor and the at least one gearbox.
6. The electric drive system of claim 5 further comprising a reservoir for collecting the distributed oil after it has been used to cool the at least one motor and the at least one gearbox.
7. The electric drive system of claim 6 further comprising a pump associated with the reservoir for returning the oil collected in the reservoir to the oil cooler.
8. The electric drive system unit of claim 1 wherein the least one structural element comprises a housing having electrical connectors therethrough.
9. The electric drive system of claim 1 , wherein the at least one structural element comprises a first rail on a first side of the unit and a second on a second side of the unit opposite the first side of the unit.
10. The electric drive system of claim 1 , wherein each of the motors comprises an electric motor.
11. The electric drive system of claim 1 , wherein the rotor shaft is disposed through a center of the integrated unit.
12. The electric drive system of claim 1 , wherein each of the motors has associated therewith a one-way clutch.
13. A rotor system comprising:
a ducted rotor comprising a plurality of rotor blades connected to a rotor shaft;
a hub for supporting the ducted rotor; and
an electric drive system comprising:
a plurality of redundant motors configured in a stacked arrangement;
a gear box associated with the plurality of redundant motors;
a collective actuator for controlling a collective pitch of the rotor blades connected to the rotor shaft; and
at least one structural element for retaining the stacked arrangement of the redundant motors, the gear box, and the collective actuator together as a single integrated unit;
wherein power generated by the plurality of motors is used to drive the rotor shaft; and
wherein the electric drive system is implemented as a line replaceable unit disposed in the hub.
14. The rotor system of claim 13 , wherein the at least one structural element comprises at least one of a housing and first and second rails disposed on opposite sides of the unit.
15. The rotor system of claim 13 , wherein each of the motors comprises an electric motor having associated therewith a one-way clutch.
16. The rotor system of claim 13 , wherein the rotor shaft is disposed through a center of the line replaceable unit.
17. A rotorcraft comprising:
a rotor system comprising a ducted rotor comprising a plurality of rotor blades connected to a rotor shaft;
a hub for supporting the ducted rotor; and
an electric drive system comprising:
a motor stack comprising a plurality of redundant motors;
a gear box associated with the motor stack;
a collective actuator for controlling a collective pitch of the rotor blades connected to the rotor shaft; and
at least one structural element for retaining the motor stack, the gear box, and the collective actuator together as a single integrated unit;
wherein power generated by the motor stack is used to drive the rotor shaft; and
wherein the electric drive system is implemented as a line replaceable unit disposed in the hub.
18. The rotorcraft of claim 17 , wherein the at least one structural element comprises at least one of a housing and first and second rails disposed on opposite sides of the unit.
19. The rotorcraft of claim 17 , wherein each of the motors comprises an electric motor having associated therewith a one-way clutch.
20. The rotor system of claim 17 , wherein the rotor shaft is disposed through a center of the motor stack.