Flying vehicle systems and methods

Patent metadata

Field	Value
Publication number	US-11485518-B2
Application number	US-202117223538-A
Country	US
Kind code	B2
Filing date	Apr 6, 2021
Priority date	Apr 6, 2020
Publication date	Nov 1, 2022
Grant date	Nov 1, 2022

Abstract

An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, and a winch mounted to the chassis. The winch includes a reel and a motor. The reel has a line wound thereon, the line having a free end. The reel includes a circumferential channel in which a wound portion of the line is wound onto the reel. The circumferential channel includes an inner portion, an outer portion, and a passage connecting the inner portion and the outer portion. The motor is operable to rotate the reel under control of the control system to thereby cause the line to wind onto and off of the reel, thereby causing the free end of the line to raise and lower.

First claim

What is claimed is:

1. An unmanned aerial vehicle, comprising:
a chassis;
a power supply mounted to the chassis;
a control system operable to receive power from the power supply;
at least one rotor operable to generate lift under control of the control system; and
a winch mounted to the chassis, the winch comprising:
a reel having a line wound thereon, the line having a free end, wherein the reel comprises a circumferential channel in which a wound portion of the line is wound onto the reel, wherein the circumferential channel comprises an inner portion, an outer portion, and a passage connecting the inner portion and the outer portion; and
a motor operable to rotate the reel under control of the control system to thereby cause the line to wind onto and off of the reel, thereby causing the free end of the line to raise and lower;

wherein the passage has a passage width;
wherein the inner portion has an inner portion width; and
wherein the passage width is less than the inner portion width.

2. The unmanned aerial vehicle of claim 1 , wherein the outer portion tapers inward from an outer portion maximum width to an outer portion minimum width, and wherein the outer portion minimum width is defined between the outer portion maximum width and the passage.

3. The unmanned aerial vehicle of claim 1 , wherein the reel comprises a circumferential ridge that at least partially defines the passage.

4. The unmanned aerial vehicle of claim 3 , wherein the reel further comprises a circumferential groove facing an apex of the circumferential ridge, the circumferential groove further defining the passage.

5. The unmanned aerial vehicle of claim 4 , wherein the reel further comprises:
a first portion comprising the circumferential ridge; and
a second portion comprising the circumferential groove;
wherein the first portion and the second portion are coupled to one another.

6. The unmanned aerial vehicle of claim 1 , wherein the reel is rotatable about a vertical rotational axis.

7. The unmanned aerial vehicle of claim 1 , further comprising a gravity hook coupled to the free end of the line.

8. The unmanned aerial vehicle of claim 1 , wherein the passage surrounds the inner portion and is surrounded by the outer portion.

9. An unmanned aerial vehicle, comprising:
a chassis;
a power supply mounted to the chassis;
a control system operable to receive power from the power supply;
at least one rotor operable to generate lift under control of the control system; and
a winch mounted to the chassis, the winch comprising a reel having a line wound thereon, the line having a free end, wherein the reel comprises a circumferential channel in which a wound portion of the line is wound onto the reel;
wherein the reel is rotatable about a reel axis defining an axial direction;
wherein the circumferential channel comprises:
an annular inner portion having a first width in the axial direction; and
an annular passage surrounding the annular inner portion, the annular passage having a second width in the axial direction, wherein the second width is less than the first width.

10. The unmanned aerial vehicle of claim 9 , wherein the circumferential channel further comprises an annular outer portion surrounding the passage.

11. The unmanned aerial vehicle of claim 10 , wherein the annular outer portion has a third width in the axial direction; and
wherein the third width is greater than the second width.

12. The unmanned aerial vehicle of claim 9 , wherein the reel comprises an annular ridge that at least partially defines the annular passage.

13. The unmanned aerial vehicle of claim 12 , wherein the reel further comprises an annular groove facing an apex of the annular ridge, the annular groove further defining the annular passage.

14. The unmanned aerial vehicle of claim 9 , wherein the winch further comprises a motor operable to rotate the reel under control of the control system.

15. The unmanned aerial vehicle of claim 9 , wherein the reel further comprises:
a first portion rotatable about the reel axis and partially defining the circumferential channel; and
a first portion rotatable about the reel axis and further defining the circumferential channel;
wherein the first portion and the second portion are releasably coupled to one another.

Assignees

• Workhorse Group Inc

Inventors

• Ratajczak Jay
• Wei Wei
• Zhang Haonan
• Bort Thaddeus

Classifications

• B64U20/70

  Constructional aspects of the UAV body · CPC title

• B64U80/86

  Land vehicles · 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

• B64U80/70

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

• B64U70/30

  for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net · CPC title