Unmanned aerial vehicle and cargo attachment system for the unmanned aerial vehicle

Patent metadata

Field	Value
Publication number	US-11858637-B2
Application number	US-202016784906-A
Country	US
Kind code	B2
Filing date	Feb 7, 2020
Priority date	Feb 7, 2020
Publication date	Jan 2, 2024
Grant date	Jan 2, 2024

Abstract

Example methods and systems for coupling and controlling transport of cargo using an unmanned aerial vehicle (UAV) are provided, comprising coupling at least one electronically-controllable attachment device positioned on an underside of the UAV to a sling cable, the sling cable being secured to the cargo. The UAV flies to a predetermined area above the cargo, and responsive to determining that the UAV is positioned within the predetermined area, the UAV elevates above the initial operating height to lift the cargo and navigates to a target location.

First claim

What is claimed is:

1. A cargo attachment system for an unmanned aerial vehicle (UAV) having at least four laterally-arranged rotors, the system comprising:
a support beam structure comprising a plurality of support beams, at least one of the plurality of support beams being affixed to an underside of the UAV, the support beam structure further comprising:
an alignment feature connected to a support beam of the plurality of support beams, the alignment feature defining a lumen; and
an electric wire having a first end and a second end and an intermediate portion between the first end and the second end, wherein the intermediate portion extends through the lumen of the alignment feature; and

an attachment device coupled to at least one of the plurality of support beams, the attachment device being electrically controllable, wherein the second end of the electric wire is connected to the attachment device and electrically couples the attachment device to a control unit on the UAV.

2. The cargo attachment system of claim 1 , further comprising:
a cable having a first portion and a second portion, the first portion being releasably coupled to the attachment device and the second portion being secured to a cargo.

3. The cargo attachment system of claim 2 , wherein the cable has a predetermined length of at least 25 feet.

4. The cargo attachment system of claim 2 , wherein the cable is a first cable and the attachment device is a first attachment device, and the system further comprises a second cable extending from a second attachment device, the second attachment device being coupled to at least one of the plurality of support beams and being electrically controllable.

5. The cargo attachment system of claim 4 , wherein the first cable and the second cable each comprise a sling cable.

6. The cargo attachment system of claim 1 , wherein the plurality of support beams comprises an upper support beam affixed to the underside of the UAV and extending away from the UAV.

7. A UAV comprising:
a rotorcraft having at least four laterally-arranged rotors;
a landing gear structure affixed to an underside of the UAV;
a support beam structure comprising a plurality of support beams affixed to an underside of the UAV, wherein at least one of the plurality of support beams projects away from the landing gear structure, the support beam structure further comprising:
an alignment feature connected to a support beam of the plurality of support beams, the alignment feature defining a lumen; and
an electric wire having a first end and a second end and an intermediate portion between the first end and the second end, wherein the intermediate portion extends through the lumen of the alignment feature; and

an attachment device coupled to at least one of the plurality of support beams, the attachment device being electrically controllable, wherein the second end of the electric wire is connected to the attachment device and electrically couples the attachment device to a control unit on the UAV.

8. The UAV of claim 7 , further comprising:
a cable having a first portion and a second portion, the first portion being releasably coupled to the attachment device and the second portion being secured to a cargo.

9. The UAV of claim 8 , wherein the attachment device is a first attachment device and the cable is a first cable, and the UAV further comprises a second cable extending from a second attachment device, the second attachment device being coupled to at least one of the plurality of support beams and being electrically controllable.

10. The UAV of claim 9 , further comprising a plurality of lateral arresting cable portions extending between the first cable and the second cable to prevent interference of the first cable or the second cable with the landing gear structure.

11. The UAV of claim 10 , wherein the plurality of support beams comprises a first support beam affixed to the underside of the UAV and extending away from the UAV, a second support beam attached to the first support beam at a first end and to the landing gear structure at a second end.

12. The UAV of claim 11 , wherein the plurality of support beams further comprises a third support beam affixed to the first support beam at a first end and to the landing gear structure at a second end, and a fourth support beam extending between the second support beam and the third support beam.

13. The UAV of claim 11 , wherein the first attachment device and the second attachment device are each electrically controllable to open and close so as to be releasably coupled to the first cable and the second cable.

14. The UAV of claim 9 , wherein the first cable and the second cable each comprise a sling cable.

15. The UAV of claim 8 , wherein the control unit has instructions stored in memory that are executed by a processor to perform functions of:
coupling the attachment device to the first portion of the cable;
operating the at least four laterally-arranged rotors on the UAV to cause the UAV to elevate to an initial operating height, the initial operating height being less than a length of the cable such that that UAV does not support the cargo;
operating the rotors to further elevate the UAV and controlling navigation of the UAV; and
releasing the first portion of the cable from the attachment device.

16. The UAV of claim 8 , wherein the cable has a predetermined length of at least 25 feet.

17. An unmanned aerial vehicle (UAV) comprising:
a rotorcraft having at least four laterally-arranged rotors;
a landing gear structure affixed to an underside of the UAV;
a support beam structure comprising a plurality of support beams affixed to an underside of the UAV, wherein at least one of the plurality of support beams projects away from the landing gear structure;
a first attachment device coupled to at least one of the plurality of support beams, the first attachment device being electrically controllable;
a first cable having a first portion and a second portion, the first portion being releasably coupled to the first attachment device and the second portion being secured to a cargo;
a second attachment device coupled to at least one of the plurality of support beams, the second attachment device being electrically controllable; and
a second cable extending from the second attachment device to the cargo,
wherein the first attachment device and the second attachment device are each electrically controllable to open and close so as to be releasably coupled to the first cable and the second cable.

18. The UAV of claim 17 , further comprising:
a plurality of lateral arresting cable portions extending between the first cable and the second cable to prevent interference of the first cable or the second cable with the landing gear structure.

19. The UAV of claim 17 , wherein the plurality of support beams comprises a first support beam affixed to the underside of the UAV and extending away from the UAV, and a second support beam attached to the first support beam at a first end and to the landing gear structure at a second end.

20. The UAV of claim 17 , further comprising:
a control unit having instructions stored in memory that are executed by a processor to perform functions of:
operating the at least four laterally-arranged rotors on the UAV to cause the UAV to elevate to an initial operating height, the initial operating height being less than a length of the first cable such that that UAV does not support the cargo;
operating the rotors to further elevate the UAV a

Assignees

• Boeing Co

Inventors

• Jarvis Joshua B
• Lacy Roger W
• Gray Brian Charles
• Mason David H
• Mikita Douglas
• Rogers Justin Fowler
• Brown Brandon
• Hathaway Eric
• Schulze Eric J
• Seidel Corey

Classifications

• B64U2201/10

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

• B64U10/16

  with five or more distinct rotor axes, e.g. octocopters · CPC title

• B64U2101/64

  for parcel delivery or retrieval · CPC title

• B64U30/24

  Coaxial rotors · CPC title

• B64U60/50

  with landing legs · CPC title