Expanding pin assembly controlled by actuator for locking and unlocking mechanical joint

Patent metadata

Field	Value
Publication number	US-10808808-B2
Application number	US-201715587945-A
Country	US
Kind code	B2
Filing date	May 5, 2017
Priority date	May 5, 2017
Publication date	Oct 20, 2020
Grant date	Oct 20, 2020

Abstract

An expanding pin system is described that can provide automated and/or power controlled locking and unlocking of an expanding pin assembly in a mechanical joint. For example, the expanding pin system can include an actuation assembly that includes a single actuator (e.g., motor) to control an expanding pin assembly for locking and unlocking a mechanical joint.

First claim

What is claimed is:

1. An expanding pin system for releasably locking a mechanical joint associated with a deployable wing of an aircraft for releasably securing the deployable wing in a deployed position, the expanding pin system, comprising:
an actuation assembly configured to provide a first output for locking the mechanical joint and a second output for unlocking the mechanical joint; and
a pin driving assembly operably coupled to the actuation assembly, the pin driving assembly comprising:
a drive assembly including a carrier operably coupled to the actuation assembly and an outer housing such that the carrier translates a first distance along the housing when the actuation assembly is actuated to provide the first output, the drive assembly further including a sun gear operably coupled to the carrier such that the sun gear is caused to rotate in a first direction after the carrier translates the first distance; and
an expanding pin assembly operably coupled to the drive assembly such that the expanding pin assembly translates the first distance with the drive assembly thereby advancing an expandable part of the expanding pin assembly across at least a part of the mechanical joint, the expandable part being caused to expand when the sun gear rotates in the first direction,
wherein the outer housing includes an inner chamber with an inner wall that is threadably engaged with a ring gear positioned around a distal end of the carrier such that rotation of the carrier causes rotation of the ring gear, and wherein rotation of the ring gear causes translation of the drive assembly and the expanding pin assembly relative to the outer housing.

2. The expanding pin system of claim 1 , wherein the sun gear is configured to rotate in a second direction when the actuation assembly is actuated to provide the second output to thereby cause the expandable part to contract.

3. The expanding pin system of claim 1 , wherein the carrier is configured to translate along the housing thereby causing the expandable part to retract from the mechanical joint when the actuation assembly is actuated to provide the second output.

4. The expanding pin system of claim 1 , wherein the actuation assembly includes one or more of a DC brush motor, a DC brushless motor, a stepper motor, an AC motor, and a rotary hydraulic actuator.

5. The expanding pin system of claim 1 , wherein the pin driving assembly further includes a detent feature that, when in an engaged position, is operatively coupled to both the drive assembly and the expanding pin assembly to thereby restrict translation of the expanding pin assembly relative to the drive assembly.

6. The expanding pin system of claim 5 , wherein the detent feature, when in a disengaged position, is uncoupled from the drive assembly to thereby allow translation of the expanding pin assembly relative to the drive assembly.

7. The expanding pin system of claim 6 , wherein the pin driving assembly further includes a plunger that is biased in a distal position within the pin driving assembly thereby causing the detent feature to be in the engaged position, and wherein the plunger causes the detent feature to be in the disengaged position when forced in a proximal position.

8. The expanding pin system of claim 7 , wherein the housing further includes a pin aligned with a distal end of the plunger, and wherein the pin is configured to force the plunger from the distal position to the proximal position when the pin driving assembly engages the pin during distal translation of the pin driving assembly.

9. The expanding pin system of claim 1 , wherein the expanding pin assembly further includes a shear pin that is rotationally restricted and threadably engaged with the sun gear such that rotation of the sun gear causes translation of the shear pin.

10. The expanding pin system of claim 9 , wherein the expandable part is positioned along a distal end of the shear pin.

11. The expanding pin system of claim 10 , wherein translation of the shear pin in a proximal direction relative to the sun gear causes the expandable part to expand.

12. The expanding pin system of claim 10 , wherein translation of the shear pin in a distal direction relative to the sun gear causes the expandable part to contract.

13. The expanding pin system of claim 10 , wherein the expandable part includes one or more bushings.

14. An expanding pin system for releasably locking a mechanical joint associated with a deployable wing of an aircraft for releasably securing the deployable wing in a deployed position, the expanding pin system, comprising:
an actuation assembly configured to provide a first output for locking the mechanical joint and a second output for unlocking the mechanical joint; and
a pin driving assembly operably coupled to the actuation assembly, the pin driving assembly comprising:
a drive assembly including a carrier operably coupled to the actuation assembly and an outer housing such that the carrier translates a first distance along the housing when the actuation assembly is actuated to provide the first output, the drive assembly further including a sun gear operably coupled to the carrier such that the sun gear is caused to rotate in a first direction after the carrier translates the first distance;
an expanding pin assembly operably coupled to the drive assembly such that the expanding pin assembly translates the first distance with the drive assembly thereby advancing an expandable part of the expanding pin assembly across at least a part of the mechanical joint, the expandable part being caused to expand when the sun gear rotates in the first direction;
a detent feature that, when in an engaged position, is operatively coupled to both the drive assembly and the expanding pin assembly to thereby restrict translation of the expanding pin assembly relative to the drive assembly, the detent feature, when in a disengaged position, being uncoupled from the drive assembly to thereby allow translation of the expanding pin assembly relative to the drive assembly; and
a plunger that is biased in a distal position within the pin driving assembly thereby causing the detent feature to be in the engaged position, and wherein the plunger causes the detent feature to be in the disengaged position when forced in a proximal position.

15. The expanding pin system of claim 14 , wherein the sun gear is configured to rotate in a second direction when the actuation assembly is actuated to provide the second output to thereby cause the expandable part to contract.

16. The expanding pin system of claim 14 , wherein the carrier is configured to translate along the housing thereby causing the expandable part to retract from the mechanical joint when the actuation assembly is actuated to provide the second output.

17. The expanding pin system of claim 14 , wherein the actuation assembly includes one or more of a DC brush motor, a DC brushless motor, a stepper motor, an AC motor, and a rotary hydraulic actuator.

18. The expanding pin system of claim 14 , wherein the outer housing includes an inner chamber with an inner wall that is threadably engaged with a ring gear positioned around a distal end of the carrier such that rotation of the carrier causes rotation of the ring gear, and wherein rotation of the ring gear causes translation of the drive assembly and the expanding pin assembly relative to the outer housing.

19. The expanding pin system of claim 14 , wherein the housing further includes a pin aligned with a distal end of the plunger, and wherein the pin is con

Assignees

• Sierra Nevada Corp

Inventors

• Crine Jake
• Cunningham Benjamin Paul
• Devereaux Alec B
• Lewis Sonny J
• Peritt Jonathan

Classifications

• F16B13/068 Primary

  expanded in two or more places · CPC title

• B64C3/56 Primary

  Folding or collapsing to reduce overall dimensions of aircraft · CPC title

• F16H19/02 Primary

  for interconverting rotary {or oscillating} motion and reciprocating motion · CPC title

• F16H57/082

  Planet carriers · CPC title

• Y02T50/10

  Drag reduction · CPC title