Star worm gear

Patent metadata

Field	Value
Publication number	US-11674563-B2
Application number	US-202217811466-A
Country	US
Kind code	B2
Filing date	Jul 8, 2022
Priority date	Oct 28, 2019
Publication date	Jun 13, 2023
Grant date	Jun 13, 2023

Abstract

The subject matter of this specification can be embodied in, among other things, an actuator that includes a worm drive assembly having a worm shaft, and a worm wheel configured as a ring having a radially outer perimeter comprising a first collection of gear teeth extending radially outward from the radially outer perimeter and at least partly engaged with the worm shaft, and a coaxial radially inner perimeter comprising a second collection of gear teeth extending radially inward from the inner perimeter, and an epicyclic gear assembly having a sun gear and a planet gear engaged with the sun gear and the second collection of gear teeth.

First claim

What is claimed is:

1. An actuator comprising:
a housing;
a back-drivable worm drive assembly comprising:
a multiple start worm shaft configured to rotate about a first axis; and
a worm wheel configured as a ring configured to rotate about a second axis that is substantially perpendicular to the first axis and having a radially outer perimeter comprising a first collection of gear teeth extending radially outward from the radially outer perimeter and at least partly engaged with the worm shaft, and a coaxial radially inner perimeter comprising a second collection of gear teeth extending radially inward from the coaxial radially inner perimeter; and

an epicyclic gear assembly comprising:
a grounded sun gear groundedly affixed to the housing;
a planet gear carrier; and
a planet gear carried by the planet gear carrier and engaged with the grounded sun gear and the second collection of gear teeth;

a rotary-to-linear motion conversion assembly comprising a rotary assembly and a linear assembly;
a rotary shaft engaged to the rotary assembly and the planet gear carrier; and
a linear member engaged to the linear assembly and configured to move linearly.

2. The actuator of claim 1 , further comprising a first rotary shaft engaged with the worm shaft.

3. The actuator of claim 1 , wherein the worm shaft is rotatably coupled to a second worm shaft of a second actuator comprising a second worm drive assembly.

4. The actuator of claim 3 , wherein the worm shaft is rotatably coupled to the second worm shaft by a synchronization shaft configured to substantially synchronize actuation of two or more aircraft engine thrust reverser actuation systems.

5. The actuator of claim 1 , wherein:
the rotary shaft is engaged to the planet gear carrier and is responsive to revolution of the planet gear carrier; and
the linear member comprises a nut engaged with the rotary shaft and axially movable along the rotary shaft in response to rotation of the rotary shaft.

6. The actuator of claim 5 , wherein the nut comprises a ball nut, and the rotary shaft comprises a ball screw.

7. The actuator of claim 6 , further comprising a linear actuator engaged with the nut and axially moveable between a retracted position and an extended position in response to axial movement of the ball nut.

8. The actuator of claim 7 , wherein the linear actuator is configured as an actuator of an aircraft engine thrust reverser actuation system.

9. The actuator of claim 5 , further comprising a linear actuator engaged with the nut and axially moveable between a retracted position and an extended position in response to axial movement of the nut.

10. The actuator of claim 9 , wherein the nut comprises a ball nut, and the rotary shaft comprises a ball screw.

11. The actuator of claim 1 , wherein the worm shaft is configured to be driven by an external force at a rotational input, and one of the planet gear carrier or the worm wheel are configured to drive the worm shaft.

12. The actuator of claim 1 , further comprising a nut affixed to the linear member and engaged with the rotary shaft, and axially movable along the rotary shaft in response to rotation of the rotary shaft.

13. The actuator of claim 12 , wherein the nut comprises a captured nut, and the rotary shaft comprises a threaded rotary shaft.

14. The actuator of claim 13 , wherein the linear member is axially moveable between a retracted position and an extended position in response to axial movement of the nut.

15. The actuator of claim 14 , wherein the linear member is configured as an actuator of an aircraft engine thrust reverser actuation system.

16. A method of rotary-to-linear actuation comprising:
rotating a multiple start worm shaft of a back-drivable worm drive assembly about a first axis;
urging, by the multiple start worm shaft, rotation of a worm wheel of the back-drivable worm drive assembly about a second axis that is substantially perpendicular to the first axis, wherein the worm wheel is configured as a ring having a radially outer perimeter comprising a first collection of gear teeth extending radially outward from the radially outer perimeter and at least partly engaged with the worm shaft, and a radially inner perimeter comprising a second collection of gear teeth extending radially inward from the radially inner perimeter;
urging, by the worm wheel, rotation of a planet gear, carried by a planet gear carrier, and engaged with the second collection of gear teeth about a grounded sun gear engaged with the planet gear, wherein the worm wheel, the planet gear, and the grounded sun gear are configured as an epicyclic gear assembly;
urging, by the planet gear carrier, rotation of a rotary output member;
urging, by the rotary output member, rotation of a rotary assembly of a rotary-to-linear motion conversion assembly; and
urging, by the rotary-to-linear motion conversion assembly, linear movement of a linear assembly of the rotary-to-linear motion conversion assembly.

17. The method of claim 16 , further comprising:
urging, by the planet gear, rotation of the planet gear carrier; and
urging, by the planet gear carrier, rotation of the rotary output member.

18. The method of claim 16 , further comprising urging rotation of a second worm shaft by the multiple start worm shaft, wherein the multiple start worm shaft is configured to urge rotation of the second worm shaft.

19. The method of claim 18 , further comprising urging substantially synchronous deployment or stowage of two or more aircraft engine thrust reverser actuation systems, wherein the multiple start worm shaft is a first worm shaft of a first aircraft engine thrust reverser actuation system and a second aircraft thrust reverser actuation system comprises the second worm shaft, and the first worm shaft is rotatably coupled to the second worm shaft by a synchronization shaft configured to substantially synchronize actuation of the two or more aircraft engine thrust reverser actuation systems.

20. The method of claim 16 , further comprising:
urging, by the rotary output member, rotation of a leadscrew;
urging, by the leadscrew, axial movement of a nut engaged with the leadscrew; and
urging, by the nut, axial motion of a linear output member between a retracted position and an extended position.

21. The method of claim 16 , further comprising:
urging, by the rotary output member, rotation of a nut;
urging, by the nut, axial movement of a leadscrew engaged with the nut; and
urging, by the leadscrew, axial motion of a linear output member between a retracted position and an extended position.

22. The method of claim 21 , further comprising:
urging, by axial movement of the linear output member, movement of an aircraft engine thrust reverser system between a stowed configuration and a deployed configuration.

23. The method of claim 16 , further comprising:
urging, by the planet gear carrier, opposite rotation of the epicyclic gear assembly;
urging, by the epicyclic gear assembly, opposite rotation of the worm wheel; and
urging, by the worm wheel, opposite rotation of the multiple start worm shaft.

Assignees

• Woodward Inc

Inventors

• Kopecek Joseph Thomas

Classifications

• F16H2025/209

  using worm gears · CPC title

• F05D2260/53

  using gears · CPC title

• F16H2025/2087

  using planetary gears · CPC title

• F16H1/30 Primary

  in which an orbital gear has an axis crossing the main axis of the gearing and has helical teeth or is a worm · CPC title

• F02K1/763

  with actuating systems or actuating devices; Arrangement of actuators for thrust reversers · CPC title