Landing and payload loading structures

Patent metadata

Field	Value
Publication number	US-10604252-B2
Application number	US-201615358935-A
Country	US
Kind code	B2
Filing date	Nov 22, 2016
Priority date	Nov 22, 2016
Publication date	Mar 31, 2020
Grant date	Mar 31, 2020

Abstract

An example UAV landing structure includes a landing platform for a UAV, a cavity within the landing platform, and a track that runs along the landing platform and at least a part of the cavity. The UAV may include a winch system that includes a tether that may be coupled to a payload. Furthermore, the cavity may be aligned over a predetermined target location. The cavity may be sized to allow the winch system to pass a tethered payload through the cavity. The track may guide the UAV to a docked position over the cavity as the UAV moves along the landing platform. When the UAV is in the docked position, a payload may be loaded to or unloaded from the UAV through the cavity.

First claim

We claim:

1. A landing structure comprising:
a landing platform for an unmanned aerial vehicle (UAV), wherein the UAV comprises a boom with a first landing pad, a second landing pad, and a winch system comprising a tether coupleable to a payload;
a cavity within the landing platform, wherein the cavity is aligned over a predetermined target location and is sized to allow the winch system to pass a tethered payload through the cavity; and
a track that runs along the landing platform and along at least a portion of the cavity such that the track guides the UAV to a docked position while the UAV travels along the landing platform under power from the UAV, wherein when in the docked position the tether is positioned over the cavity, such that the tether can raise or lower a payload through the cavity;
wherein the track comprises a slot in the landing platform, wherein the first landing pad and the second landing pad of the UAV each have a pin that extends beyond the pad such that when the UAV moves along the landing platform the pin in the first landing pad will engage the slot, then the second pin will engage the slot so as the UAV continues to move along the landing platform the UAV will follow a path of the slot to the docked position over the cavity.

2. The landing structure of claim 1 , further comprising:
at least one stop block near the cavity, wherein the at least one stop block prevents the UAV from traveling beyond the cavity.

3. The landing structure of claim 1 , further comprising:
at least one stop block near the cavity, wherein the at least one stop block prevents the UAV from traveling vertically.

4. The landing structure of claim 1 , wherein the track comprises:
a straight portion of track along the landing platform;
a tapered portion of track, wherein the tapered portion of track begins at the straight portion of track and tapers out to edges of the cavity; and
a cavity portion of track, wherein the cavity portion of track runs alongside at least part of the cavity.

5. The landing structure of claim 1 , wherein the tether is coupled to a payload coupling apparatus at a first end and the winch system at a second end.

6. The landing structure of claim 1 , wherein the landing platform is attached to an exterior wall of a building.

7. The landing structure of claim 1 , wherein the landing platform is integrated into an awning attached to a building.

8. The landing structure of claim 1 , wherein the landing platform is attached to another vehicle.

9. The landing structure of claim 1 , wherein the cavity is large enough for at least two UAVs positioned over the cavity at a same time.

10. The landing structure of claim 1 , further comprising:
a plurality of mechanical restraints that maintain the UAV in the docked position over the cavity of the landing platform.

11. The landing structure of claim 1 , wherein the landing platform is at least nine feet above a ground surface.

12. The landing structure of claim 1 , wherein the UAV comprises a propulsion unit and the UAV travels along the landing platform using the propulsion unit.

13. The landing structure of claim 1 , further comprising:
a vertical support structure coupled to the bottom of the landing platform, wherein the vertical support structure comprises a payload platform located below the cavity.

14. The landing structure of claim 13 , wherein the payload platform comprises an elevator platform that travels between a ground level and a loading level, wherein the payload is secured to the UAV at the loading level and is loaded or unloaded by a user at the ground level.

15. A system comprising:
an unmanned aerial vehicle (UAV) comprising a winch system and a boom, wherein the winch system comprises a tether coupleable to a payload, and further wherein the boom comprises a first pin and a second pin, wherein the first pin and the second pin each extend outwards from the boom; and
a landing platform comprising:
a cavity that is aligned over a predetermined target location and is sized to allow the winch system to pass a tethered payload through the cavity; and
a slot that runs along the landing platform and along at least a portion of the cavity such that when the UAV moves along the landing platform the first pin will engage the slot and then the second pin will engage the slot, so as the UAV continues to move along the landing platform the UAV will follow a path of the slot to the docked position over the cavity, and wherein when in the docked position the tether is positioned over the cavity, such that the tether can raise or lower the payload through the cavity.

16. The system of claim 15 , wherein landing gear of the UAV comprises the first pin and the second pin of the boom of the UAV, the system further comprising:
a control system configured to:
instruct the UAV to apply a forward thrust such that at least a portion of the landing gear of the UAV contacts the slot; and
instruct the UAV to continue to apply the forward thrust until the UAV reaches the docked position.

17. The system of claim 15 , further comprising:
a control system configured to:
determine if the UAV has reached the docked position; and
based on the determination that the UAV has reached the docked position, activate the winch system to lower the tether through the cavity.

18. The system of claim 15 , further comprising:
a control system configured to:
determine that the tether has coupled to the payload or that the tether has decoupled from the payload; and
based on the determination that the tether has coupled to the payload or that the tether has decoupled from the payload, activate the winch system to raise the tether through the cavity.

19. The system of claim 15 , further comprising:
a vertical support structure coupled to the bottom of the landing platform; and
a payload platform movably coupled to the vertical support structure such that the payload platform travels vertically between a ground level and a loading level, wherein the payload platform is located below the cavity of the landing platform, and wherein the payload is secured to the UAV at the loading level and is loaded or unloaded by a user at the ground level.

20. The system of claim 15 , further comprising:
at least one stop block, wherein the at least one stop block prevents the UAV from traveling beyond the cavity.

21. The system of claim 15 , wherein the slot comprises:
a straight portion of the slot along the landing platform;
a tapered portion of the slot, wherein the tapered portion of the slot begins at the straight portion of the slot and tapers out to edges of the cavity; and
a cavity portion of the slot, wherein the cavity portion of the slot runs alongside at least part of the cavity.

22. The system of claim 15 , wherein the landing platform further comprises:
a navigational aid, wherein the navigational aid is configured to transmit a signal to the UAV.

23. The system of claim 15 , wherein the landing platform is coupled to an exterior wall of a building.

24. The system of claim 15 , wherein the landing platform is located at least nine feet about a ground surface.

25. A method comprising:
landing, by an unmanned aerial vehicle (UAV), on a landing platform, wherein the UAV comprises a winch system and a boom, wherein the winch system comprises a tether coupleable to a payload, and further wherein the boom comprises a first landing pad with a first

Assignees

• Wing Aviation Llc

Inventors

• Blake Jesse
• Schmalzried Jim
• Shannon Trevor
• Simonian Michael
• Klepp Sindre
• Benson Stephen
• Woodworth Adam

Classifications

• B64C39/024 Primary

  of the remote controlled vehicle type, i.e. RPV · CPC title

• B64C2201/128

  Operations & Transport · mapped topic

• B64C2201/18

  Operations & Transport · mapped topic

• B64U2101/21

  for providing Internet access · CPC title

• B64U2101/23

  for providing telephone services · CPC title