Stackable unmanned aerial vehicle (UAV) system and portable hangar system therefor

Patent metadata

Field	Value
Publication number	US-10322820-B2
Application number	US-201715704908-A
Country	US
Kind code	B2
Filing date	Sep 14, 2017
Priority date	Sep 14, 2017
Publication date	Jun 18, 2019
Grant date	Jun 18, 2019

Abstract

An unmanned aerial vehicle (UAV) system comprises a hangar structure configurable to mount on a host platform. The hangar structure comprises electrical circuits comprising a charging circuit and a communications circuit. The UAV system further comprises a plurality of stackable UAVs. The plurality of stackable UAVs comprise respective batteries and control circuits. The plurality of stackable UAVs are configured to cooperate with the charging circuit to charge the batteries and to cooperate with the communications circuit to communicate with the control circuits while the plurality of stackable UAVs are in a stacked configuration within the hangar structure.

First claim

What is claimed is:

1. An unmanned aerial vehicle (UAV) system comprising:
a hangar structure comprising mounting hardware to mount on a host platform, the hangar structure further comprising a charging circuit and a communications circuit; and
a plurality of unmanned aerial vehicles (UAVs) arranged in a stack, a particular UAV of the plurality of UAVs comprising:
a battery;
first electrical contacts on a first surface, the first electrical contacts configured to receive power to charge the battery from electrical contacts of an additional UAV located below the particular UAV in the stack and in physical contact with the particular UAV; and
second electrical contacts on a second surface, the second electrical contacts configured to provide power to electrical contacts of another UAV that is located above the particular UAV in the stack and in physical contact with the particular UAV.

2. The UAV system of claim 1 , wherein the hangar structure comprises an electrical connector configured to connect a plurality of electrical circuits to the host platform.

3. The UAV system of claim 1 , wherein the hangar structure comprises a communicative element including an antenna, a beacon, or both, the communicative element configured to communicate with the plurality of UAVs.

4. The UAV system of claim 1 , wherein a first UAV of the plurality of UAVs is configured to communicate with a second UAV of the plurality of UAVs for coordinating operation of the first UAV and the second UAV.

5. The UAV system of claim 4 , wherein the first UAV comprises a first communications subsystem configured to communicate with a second communications subsystem of the second UAV, wherein the first UAV further comprises a first processing subsystem to communicate with a second processing subsystem of the second UAV to plan cooperative operation of the first UAV and the second UAV.

6. The UAV system of claim 1 , wherein the hangar structure further comprises a processing circuit configured to control a first UAV and a second UAV, based on comparison of respective flight paths, to avoid conflicts as the first UAV and the second UAV attempt to land in the hangar structure.

7. The UAV system of claim 1 , wherein the plurality of UAVs are configured to cooperate with each other in a daisy-chained manner to charge batteries and to communicate with control circuits while the plurality of UAVs are in the stack within the hangar structure.

8. The UAV system of claim 1 , wherein the second surface is on an opposite side of the particular UAV than the first surface.

9. A hangar structure comprising:
an enclosure having a door selectively defining an opening configured to enable a plurality of unmanned aerial vehicles (UAVs) to take flight;
mounting hardware, the mounting hardware configured to mount the hangar structure on a host platform;
a support surface configured to support the plurality of UAVs in a stack; and
a charging circuit, the charging circuit comprising a set of electrical contacts on the support surface, the set of electrical contacts configured to provide power to each UAV of the stack of the plurality of UAVs via first electrical contacts of a first UAV located on a bottom of the stack, wherein the first UAV comprises the first electrical contacts on a first surface of first UAV and second electrical contacts on a second surface of the first UAV, the first electrical contacts configured to receive power from the set of electrical contacts on the support surface, and the second electrical contacts configured to provide power to electrical contacts of a second UAV that is located above the first UAV in the stack and in physical contact with the first UAV.

10. The hangar structure of claim 9 , wherein a plurality of electrical circuits are configured to charge batteries of the plurality of UAVs and to communicate with control circuits of the plurality of UAVs.

11. The hangar structure of claim 9 , further comprising:
an electrical connector configured to connect the hangar structure to the host platform.

12. The hangar structure of claim 9 , further comprising:
a communicative element including an antenna, a beacon, or both, the communicative element configured to communicate with the plurality of UAVs.

13. The hangar structure of claim 9 , wherein a communications circuit is configured to communicate with the plurality of UAVs in a daisy-chained manner.

14. The hangar structure of claim 9 , further comprising:
a bus structure coupled to a plurality of electrical circuits, the bus structure configured to conduct electrical signals directly from the electrical circuits to each of the plurality of UAVs.

15. The hangar structure of claim 9 , further comprising:
a processing circuit configured to control a third UAV and a fourth UAV, based on comparison of respective flight paths, to avoid conflicts as the third UAV and the fourth UAV attempt to land in the hangar structure.

16. A method comprising:
charging a first unmanned aerial vehicle (UAV) of a plurality of UAVs stacked in a hangar structure by applying power to first electrical contacts of the first UAV, wherein the first UAV is configured to charge a second UAV of the plurality of UAVs via second electrical contacts of the first UAV that are in physical contact with electrical contacts of the second UAV;
commanding, via a communications circuit of the hangar structure, the first UAV to take flight;
recalling the first UAV to land in the hangar structure; and
receiving the first UAV in the hangar structure.

17. The method of claim 16 , further comprising:
establishing connection of a host platform interface circuit to electrical circuits of the hangar structure via an electrical connector of the hangar structure, wherein the electrical circuits comprise the communications circuit.

18. The method of claim 16 , further comprising:
integrating, at the first UAV, a first set of sensor information obtained from a first sensor subsystem located at a host platform and a second set of sensor information obtained from the second UAV of the plurality of UAVs, wherein the second UAV is distinct from the first UAV.

19. The method of claim 18 , further comprising:
maneuvering the first UAV based on an integrated set of sensor information obtained from the integrating.

20. The hangar structure of claim 9 , wherein the door is coupled to a top of the enclosure such that, when the door is open, the door is configured to enable a top UAV of the stack to take flight vertically through the opening.

Assignees

• Sparkcognition Inc

Inventors

• Husain Syed Mohammad Amir
• Allen John Rutherford

Classifications

• B64U80/86

  Land vehicles · CPC title

• B64U80/70 Primary

  in containers (B64U80/60 takes precedence) · CPC title

• B64U2201/102

  adapted for flying in formations · CPC title

• B64U2201/10

  autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] · CPC title

• B64F1/222 Primary

  for storing aircraft, e.g. in hangars · CPC title