Self-centering landing platform

Patent metadata

Field	Value
Publication number	US-11655048-B2
Application number	US-201816966225-A
Country	US
Kind code	B2
Filing date	Feb 14, 2018
Priority date	Feb 14, 2018
Publication date	May 23, 2023
Grant date	May 23, 2023

Abstract

Example landing platform systems and methods are described. In one implementation, a landing platform includes a top plate configured to support an unmanned aerial vehicle (UAV), where the top plate has a plurality of slots therethrough. A rotating plate is located adjacent the top plate and includes multiple centering pins extending therefrom and extending through the plurality of slots in the top plate. A motor is capable of rotating the rotating plate, which causes the multiple centering pins to center the UAV on the top plate.

First claim

The invention claimed is:

1. A landing platform comprising:
a top plate configured to support an unmanned aerial vehicle (UAV), wherein the top plate has a plurality of slots therethrough;
a rotating plate adjacent the top plate and including a plurality of centering pins extending therefrom and extending through the plurality of slots; and
a motor configured to rotate the rotating plate to cause the plurality of centering pins to center the UAV on the top plate.

2. The landing platform of claim 1 , wherein at least one of the plurality of centering pins engage a landing structure of the UAV.

3. The landing platform of claim 1 , wherein the rotating plate is attached to the motor such that activation of the motor rotates the rotating plate.

4. The landing platform of claim 3 , wherein activation of the motor causes at least one of the plurality of centering pins to engage a landing structure of the UAV.

5. The landing platform of claim 3 , wherein activation of the rotating plate causes the plurality of centering pins to move in a spiral motion toward the center of the top plate, thereby moving the UAV toward the center of the top plate.

6. The landing platform of claim 1 , wherein the plurality of centering pins are slidably attached to the rotating plate.

7. The landing platform of claim 1 , further comprising:
an internal gear attached to the rotating plate; and
a pinion gear attached to the motor, wherein the pinion gear engages the internal gear to rotate the rotating plate when the motor is activated.

8. The landing platform of claim 1 , wherein each of the plurality of slots are curved, and wherein each of the plurality of centering pins follow the curvature of a corresponding slot as the rotating plate is activated.

9. The landing platform of claim 1 , further comprising an aperture in the center of the top plate, wherein activation of the motor causes the centering pins to engage a landing structure of the UAV and center the UAV over the aperture.

10. The landing platform of claim 9 , wherein centering the UAV over the aperture provides access to the bottom of the UAV for at least one of loading payload, unloading payload, and recharging the UAV.

11. The landing platform of claim 1 , further comprising an aperture in the center of the top plate, wherein the motor is offset from the aperture such that the motor does not obstruct access to the UAV through the aperture.

12. The landing platform of claim 1 , wherein the landing platform is mounted to the top of a vehicle.

13. A landing platform comprising:
a top plate configured to support an unmanned aerial vehicle (UAV), wherein the top plate has a plurality of slots therethrough;
a rotating plate adjacent the top plate and including a plurality of centering pins slidably attached to the rotating plate, wherein the plurality of centering pins extend from the rotating plate and through the plurality of slots in the top plate; and
a motor configured to rotate the rotating plate to cause the plurality of centering pins to engage a landing structure of the UAV and center the UAV on the top plate.

14. The landing platform of claim 13 , wherein the rotating plate is attached to the motor such that activation of the motor rotates the rotating plate.

15. The landing platform of claim 14 , wherein the activation of the motor causes the plurality of centering pins to move in a spiral motion toward the center of the top plate, thereby moving the UAV toward the center of the top plate.

16. The landing platform of claim 13 , further comprising:
an internal gear attached to the rotating plate; and
a pinion gear attached to the motor, wherein the pinion gear engages the internal gear to rotate the rotating plate when the motor is activated.

17. The landing platform of claim 13 , further comprising an aperture in the center of the top plate, wherein activation of the motor causes the centering pins to engage a landing structure of the UAV and center the UAV over the aperture.

18. A method comprising:
responsive to an unmanned aerial vehicle (UAV) landing on a top plate of a landing platform, activating a motor associated with the landing platform to move a rotating plate having a plurality of centering pins extending from the rotating plate, wherein activating the motor moves the plurality of centering pins along a plurality of slots in the top plate of the landing platform;
maintaining activation of the motor to continue moving the plurality of centering pins along the plurality of slots to move the UAV toward the center of the landing platform; and
deactivating the motor when the UAV reaches the center of the landing platform.

19. The method of claim 18 , wherein maintaining activation of the motor causes the plurality of centering pins to move in a spiral motion toward the center of the landing platform.

20. The method of claim 18 , wherein activating the motor includes rotating a pinion gear attached to the motor, wherein the pinion gear engages an internal gear attached to the rotating plate.

Assignees

• Ford Global Tech Llc

Inventors

• Sugimoto Yuji
• Carthew James
• Singh Aditya

Classifications

• B64F1/22 Primary

  for handling aircraft · CPC title

• B64U2101/30

  for imaging, photography or videography · CPC title

• B64U70/97

  Means for guiding the UAV to a specific location on the platform, e.g. platform structures preventing landing off-centre · CPC title

• B64U70/93

  for use on a land or nautical vehicle · CPC title

• F16H25/16

  for interconverting rotary motion and oscillating motion · CPC title