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

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 operably coupled to a housing, the drive assembly comprising:

a carrier operably coupled to the actuation assembly such that actuation of the actuation assembly to provide the first output causes the carrier to translate a first distance towards the mechanical joint; and

a ring gear operably coupled to the carrier such that rotational movement of the carrier causes rotational movement of the ring gear, the ring gear being operably coupled to the housing such that rotation of the ring gear causes translation of the drive assembly relative to the housing; and

an expanding pin assembly operably coupled to the drive assembly such that the expanding pin assembly translates the first distance with the carrier thereby advancing an expandable part of the expanding pin assembly across at least a part of the mechanical joint for locking the mechanical joint as a result of the expandable part being expanded.

2. The expanding pin system of claim 1 , further comprising 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, the expandable part being caused to expand when the sun gear rotates in the first direction.

3. The expanding pin system of claim 2 , 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.

4. The expanding pin system of claim 2 , 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, the expandable part being positioned along a distal end of the shear pin.

5. The expanding pin system of claim 4 , wherein translation of the shear pin in a proximal direction relative to the sun gear causes the expandable part to expand, and wherein translation of the shear pin in a distal direction relative to the sun gear causes the expandable part to contract.

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

7. 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.

8. 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.

9. The expanding pin system of claim 8 , 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.

10. The expanding pin system of claim 9 , 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.

11. The expanding pin system of claim 10 , 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.

12. 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 comprising a carrier operably coupled to the actuation assembly such that the carrier translates a first distance towards the mechanical joint when the actuation assembly is actuated to provide the first output; and

an expanding pin assembly operably coupled to the drive assembly such that the expanding pin assembly translates the first distance with the carrier thereby advancing an expandable part of the expanding pin assembly across at least a part of the mechanical joint for locking the mechanical joint upon expansion of the expandable part, the expanding pin assembly comprising:

a plunger biased in a first position within the pin driving assembly thereby causing a detent feature to restrict translation of the expanding pin assembly relative to the drive assembly, and wherein the plunger, when forced into a second position, causes the detent feature to allow translation of the expanding pin assembly relative to the drive assembly.

13. The expanding pin system of claim 12 , further comprising 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, the expandable part being caused to expand when the sun gear rotates in the first direction.

14. The expanding pin system of claim 13 , 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, and

wherein the carrier is configured to translate along the housing and retract the expandable part from the mechanical joint when the actuation assembly is actuated to provide the second output.

15. The expanding pin system of claim 13 , 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, the expandable part being positioned along a distal end of the shear pin.

16. The expanding pin system of claim 15 , wherein translation of the shear pin in a proximal direction relative to the sun gear causes the expandable part to expand, and wherein translation of the shear pin in a distal direction relative to the sun gear causes the expandable part to contract.

17. The expanding pin system of claim 12 , wherein the carrier is configured to translate away from the mechanical joint and retract the expandable part from the mechanical joint when the actuation assembly is actuated to provide the second output.

18. The expanding pin system of claim 12 , 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.

19. The expanding pin system of claim 12 , further comprising a pin aligned with a distal end of the plunger, the pin configured to force the plunger from the first position to the second position when the pin driving assembly engages the pin during distal translation of the pin driving assembly.