Thrust reverser system actuator having an integral torque limiter

• US 6,974,107 B2
• Filed: 06/18/2003
• Issued: 12/13/2005
• Est. Priority Date: 06/18/2003
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Hanlon, Casey, Christensen, Donald J., Johnson, Andrew, Hopper, Douglas T., Kortum, Robert D.
• Primary Examiner(s): Luu, Teri P.
• Assistant Examiner(s): HOLZEN, STEPHEN A
• Application Number:
  US10/465,413
• Publication Number:
  US 20050040284A1
• Time in Patent Office: 909 Days
• Field of Search: 244/101, 244/102.R, 244/102.A, 244/102.SS, 244/53.R, 244/54, 244/56, 244/57, 244/58, 244/53.B, 746/50, 173/178
• US Class Current: 244/101
• CPC Class Codes: F02K 1/763 with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
• CPC Class Codes: F05D 2270/114 by limiting mechanical stresses
• CPC Class Codes: F16H 2025/2075 Coaxial drive motors
• CPC Class Codes: F16H 25/2021 with means for avoiding overloading
• CPC Class Codes: F16H 48/12 without gears having orbital motion
• CPC Class Codes: Y10T 74/19005 Nonplanetary gearing differential type [e.g., gearless differentials]

Abstract

A thrust reverser system actuator assembly is provided that includes a torque limiter to limit the number of torque that may be applied to the actuator assembly. The actuator assembly includes an actuator and a torque limiter assembly. The actuator is adapted to receive a drive force and is configured, in response to receipt of the drive force, to move between a stowed position and a deployed position. The torque limiter assembly is coupled to an end of the actuator and is configured to limit torque applied to the actuator assembly upon a torque magnitude being reached in at least the actuator.

Claims

1. A thrust reverser control system, comprising:

a power drive unit operable to supply a drive force;

at least two drive mechanisms each coupled to receive the drive force from the power drive unit; and

at least two actuator assemblies, each actuator assembly coupled to at least one of the drive mechanisms and including;

an actuator coupled to receive the drive force from one of the drive mechanisms, the actuator having at least one end that rotates in response to the drive force and configured to move, upon receipt of the drive force, between a stowed position and a deployed position,

a torque limiter assembly mounted to the end of the actuator and configured to limit torque in the actuator assembly upon a torque magnitude being reached in at least the actuator while allowing continued rotation of the at least one end of the actuator,

at least two roller pins, each roller pin having an outer surface and moveably mounted in one of the rod end assembly grooves, and

at least two substantially resilient cantilever arms each having a fixed end and a free end, each cantilever arm fixed end fixedly coupled to the extension tube and each cantilever arm free end in contact with the outer surface of one of the roller pins, to thereby apply a radial load thereon.

2. The system of claim 1, wherein the actuator comprises:

a rotationally mounted actuator shaft configured to rotate, upon receipt of the drive force, in a stow direction and a deploy direction; and

an extension tube mounted on the actuator shaft and coupled to the torque limiter assembly, the extension tube configured to translate between the stowed position and the deployed position in response to actuator shaft rotation in the stow direction and the deploy direction, respectively.

3. The system of claim 2, further comprising:

a rod end assembly selectively moveably coupled to the torque limiter assembly, the rod assembly configured to selectively rotate relative to the extension tube, and adapted to couple to a thrust reverser moveable component.

4. The system of claim 3, wherein the torque limiter assembly at least partially decouples the extension tube from the rod end assembly upon the torque magnitude being reached in the extension tube, to thereby limit torque applied to the actuator assembly.

5. The system of claim 2, wherein the extension tube is further configured to rotate in substantial synchronism with the actuator shaft when the torque limiter assembly limits the applied torque.

6. The system of claim 2, wherein:

the actuator shaft comprises a ball screw; and

the extension tube comprises a ball nut mounted on the ball screw, the ball nut configured to translate between the stowed position and the deployed position in response to ball screw rotation in the stow direction and the deploy direction, respectively.

7. The system of claim 3, wherein the torque limiter assembly comprises:

at least two roller pins, each roller pin having an outer surface and moveably mounted in a groove formed in the rod end assembly; and

at least two substantially resilient cantilever arms each having a fixed end and a free end, each cantilever arm fixed end fixedly coupled to the actuator and each cantilever arm free end in contact with the outer surface of one of the roller pins, to thereby apply a radial load thereon.

8. The system of claim 7, wherein:

the grooves formed in the rod assembly each have a substantially equivalent groove depth; and

the torque magnitude at which the torque limiter assembly limits torque applied to the actuator assembly is based, at least in part, on groove depth.

9. The system of claim 7, wherein the torque magnitude at which the torque limiter assembly limits torque applied to the actuator assembly is based, at least in part, on the radial load applied by each cantilever arm on each roller pin.

10. The system of claim 7, wherein each of the roller pins rolls out of one groove and into an adjacent groove when the torque magnitude is reached, to thereby at least partially decouple the actuator from the rod end assembly.

11. The actuator assembly of claim 3, further comprising:

a thrust bearing assembly coupled between the actuator and the torque limiter assembly.

12. The actuator of claim 11, wherein the thrust bearing assembly comprises:

a bearing groove formed in at least one of the actuator and the rod end assembly; and

a plurality of ball bearings disposed within the bearing groove and in moveable contact with the actuator and the rod end assembly,

wherein the bearing groove and ball bearings are configured to transmit an axial force between the actuator and the rod end assembly and, when the torque magnitude is reached, whereby relative rotation between the actuator and the rod end assembly is allowed.

13. A thrust reverser actuator assembly, comprising:

an actuator adapted to receive a drive force, the actuator having at least one end that rotates in response to the drive force and configured, in response to receipt of the drive force, to move between a stowed position and a deployed position, the actuator including

a rotationally mounted actuator shaft configured to rotate, upon receipt of the drive force, in a stow direction and a deploy direction,

an extension tube mounted on the actuator shaft and configured to translate between the stowed postion and the deployed position in response to actuator shaft rotation in the stow direction and the deploy direction, respectively, and

a rod end assembly having at least two grooves formed in an outer surface thereof; and

a torque limiter assembly mounted to the end of the actuator and configured to limit torque applied to the actuator assembly upon a torque magnitude being reached in at least the actuator while allowing continued rotation of the at least one end of the actuator, the torque limiter assembly including;

at least two roller pins, each roller pin having an outer surface and moveably mounted in one of the rod end assembly grooves, and

at least two substantially resilient cantilever arms each having a fixed end and a free end, each cantilever arm fixed end fixedly coupled to the extension tube and each cantilever arm free end in contact with the outer surface of one of the roller pins, to thereby apply a radial load thereon.

14. The actuator assembly of claim 13, wherein the actuator comprises:

a rotationally mounted actuator shaft configured to rotate, upon receipt of the drive force, in a stow direction and a deploy direction; and

an extension tube mounted on the actuator shaft and coupled to the torque limiter assembly, the extension tube configured to translate between the stowed position and the deployed position in response to actuator shaft rotation in the stow direction and the deploy direction, respectively.

15. The actuator assembly of claim 14, further comprising:

a rod end assembly coupled to the torque limiter assembly, the rod end assembly configured to selectively rotate relative to the extension tube and the torque limiter assembly, and adapted to couple to a thrust reverser moveable component.

16. The actuator assembly of claim 15, wherein the torque limiter assembly at least partially decouples the extension tube from the rod end assembly upon the torque magnitude being reached in the extension tube, to thereby limit torque applied to the actuator assembly.

17. The actuator assembly of claim 14, wherein the extension tube is further configured to rotate in substantial synchronism with the actuator shaft when the torque limiter assembly limits the applied torque.

18. The actuator assembly of claim 14, wherein:

the actuator shaft comprises a ball screw; and

the extension tube comprises a ball nut mounted on the ball screw, the ball nut configured to translate between the stowed position and the deployed position in response to ball screw rotation in the stow direction and the deploy direction, respectively.

19. The actuator assembly of claim 15, wherein the torque limiter assembly comprises:

at least two roller pins, each roller pin having an outer surface and moveably mounted in a groove formed in the rod end assembly; and

at least two substantially resilient cantilever arms each having a fixed end and a free end, each cantilever arm fixed end fixedly coupled to the actuator and each cantilever arm free end in contact with the outer surface of one of the roller pins, to thereby apply a radial load thereon.

20. The actuator assembly of claim 19, wherein:

the grooves formed in the rod end assembly each have a substantially equivalent groove depth; and

the torque magnitude at which the torque limiter assembly limits torque applied to the actuator assembly is based, at least in part, on groove depth.

21. The actuator assembly of claim 19, wherein the torque magnitude at which the torque limiter assembly limits torque applied to the actuator assembly is based, at least in part, on the radial load applied by each cantilever arm on each roller pin.

22. The actuator assembly of claim 19, wherein each of the roller pins rolls out of one groove and into an adjacent groove when the torque magnitude is reached, to thereby at least partially decouple the actuator from the rod end assembly.

23. The actuator assembly of claim 15, further comprising:

a thrust bearing assembly coupled between the actuator and the torque limiter assembly.

24. The actuator assembly of claim 14, wherein the thrust bearing assembly comprises:

a bearing groove formed in at least one of the actuator and the rod end assembly; and

a plurality of ball bearings disposed within the bearing groove and in moveable contact with the actuator and the rod end assembly,

wherein the bearing groove and ball bearings are configured to transmit an axial force between the actuator and the rod end assembly and, when the torque magnitude is reached, whereby relative rotation between the actuator and the rod end assembly is allowed.