Electric drive system line replaceable unit with integrated cyclic actuation

Patent metadata

Field	Value
Publication number	US-11565803-B2
Application number	US-202016808851-A
Country	US
Kind code	B2
Filing date	Mar 4, 2020
Priority date	Mar 4, 2020
Publication date	Jan 31, 2023
Grant date	Jan 31, 2023

Abstract

One embodiment is an electric drive system including 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 via a swashplate; a gear box associated with the plurality of redundant motors; a cyclic actuation system for controlling an individual pitch of the rotor blades connected to the swashplate; and at least one structural element for retaining the redundant motors, the gear box, and the cyclic actuation system together as a single integrated unit.

First claim

What is claimed is:

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 via a swashplate;
a cyclic actuation system for controlling an individual pitch of the rotor blades connected to the swashplate;

at least one structural element for retaining the stack of redundant motors and the cyclic actuation system together as a single integrated unit; and
a cooling fan for drawing air into the single integrated unit across an electronic component of the electric drive system to cool the electronic component and for expelling air into an oil cooler for cooling oil contained therein, wherein the cooling fan is mechanically powered by the rotor shaft.

2. The electric drive system of claim 1 , wherein the cooling fan is electrically powered.

3. The electric drive system of claim 1 further comprising an oil distribution system for distributing oil cooled by an 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.

4. The electric drive system of claim 3 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.

5. The electric drive system of claim 4 further comprising a pump associated with the reservoir for returning the oil collected in the reservoir to the oil cooler.

6. The electric drive system unit of claim 1 wherein the least one structural element comprises a housing having electrical connectors therethrough.

7. The electric drive system of claim 1 , wherein the at least one structural element comprises first and second rails disposed on opposite sides of the unit.

8. The electric drive system of claim 1 , wherein each of the motors comprises an electric motor.

9. The electric drive system of claim 1 , wherein the rotor shaft is disposed through a center of the integrated unit.

10. The electric drive system of claim 1 , wherein each of the motors has associated therewith a one-way clutch.

11. A rotor system comprising:
an unducted rotor comprising a plurality of rotor blades connected to a rotor shaft via a swashplate;
a nacelle for supporting the unducted rotor; and
an electric drive system comprising:
a plurality of redundant motors arranged in a stack;
a gearbox associated with the plurality of redundant motors;
a cyclic actuation system for controlling an individual pitch of the rotor blades connected to the rotor shaft via the swashplate; and
at least one structural element for retaining the stack of motors, the gearbox, and the cyclic actuation system together as a single integrated unit; and

a cooling fan for drawing air into the single integrated unit across an electronic component of the electric drive system to cool the electronic component and for expelling air into an oil cooler for cooling oil contained therein, wherein the cooling fan is mechanically powered by the rotor shaft;
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 nacelle.

12. The rotor system of claim 11 , wherein the at least one structural element comprises a housing.

13. The rotor system of claim 11 , wherein each of the motors comprises an electric motor having associated therewith a one-way clutch.

14. The rotor system of claim 11 , wherein the rotor shaft is disposed through a center of the line replaceable unit.

15. A rotorcraft comprising:
a rotor system comprising an unducted rotor comprising a plurality of rotor blades connected to a rotor shaft via a swashplate;
a nacelle for supporting the unducted rotor; and
an electric drive system comprising:
a plurality of redundant motors arranged in a stack;
a gearbox associated with the plurality of redundant motors;
a cyclic actuation system for controlling an individual pitch of the rotor blades connected to the rotor shaft via the swashplate; and
at least one structural element for retaining the stack of motors, the gearbox, and the cyclic actuation system together as a single integrated unit; and

a cooling fan for drawing air into the single integrated unit across an electronic component of the electric drive system to cool the electronic component and for expelling air into an oil cooler for cooling oil contained therein, wherein the cooling fan is mechanically powered by the rotor shaft;
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 nacelle.

16. The rotorcraft of claim 15 , wherein the at least one structural element comprises a housing.

17. The rotorcraft of claim 15 , wherein each of the motors comprises an electric motor having associated therewith a one-way clutch.

18. The rotor system of claim 15 , wherein the rotor shaft is disposed through a center of the line replaceable unit.

19. The rotor system of claim 11 , wherein the at least one structural element comprises first and second rails disposed on opposite sides of the unit.

20. The rotorcraft of claim 15 , wherein the at least one structural element comprises first and second rails disposed on opposite sides of the unit.

Assignees

• Bell Textron Inc
• Textron Innovations Inc

Inventors

• Heironimus William Kyle
• Chung Stephen Yibum

Classifications

• B64D35/02

  specially adapted for specific power plants · CPC title

• B64D33/08

  of power plant cooling systems · CPC title

• H02K9/193

  with provision for replenishing the cooling medium; with means for preventing leakage of the cooling medium · CPC title

• B64D27/24

  using steam or spring force (jet aircraft B64D27/16) · CPC title

• H02K7/116

  with gears · CPC title