Aerial devices capable of controlled flight

Patent metadata

Field	Value
Publication number	US-10875641-B2
Application number	US-201615578532-A
Country	US
Kind code	B2
Filing date	May 27, 2016
Priority date	Jun 1, 2015
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

An aerial device (100) capable of controlled flight has a body (110), a rotor (120) arranged to rotate relative to the body; and a deployable sheet (130), the sheet having an undeployed configuration in which the sheet is folded against the body and a deployed configuration in which the sheet is at least partially unfolded away from the body.

First claim

The invention claimed is:

1. An aerial device capable of controlled flight, the aerial device comprising:
a body;
a rotor arranged to rotate relative to the body; and
a deployable sheet, the sheet having an undeployed configuration in which the sheet is folded against the body and a deployed configuration in which the sheet is at least partially unfolded away from the body,
wherein the sheet comprises at least one crease, and wherein the at least one crease of the sheet is scored or perforated.

2. The aerial device of claim 1 , wherein the sheet comprises a plurality of creases that define a tessellated surface thereof, and wherein the tessellated surface comprises a plurality of parallelograms defined by the creases.

3. The aerial device of claim 1 , wherein the rotor is arranged to rotate in a plane and wherein, in the deployed configuration, the sheet is at least partially unfolded away from the body in a direction parallel to the plane.

4. The aerial device of claim 1 further comprising an actuator operable to deploy the sheet from the undeployed configuration to the deployed configuration and/or to undeploy the sheet from the deployed configuration to the undeployed configuration.

5. The aerial device of claim 4 further comprising a controller arranged to operate the actuator, and at least one sensor for generating sensor data relating to a surrounding environment in which the aerial device is controllably flown, wherein the controller is arranged to operate the actuator based on the sensor data.

6. The aerial device of claim 5 , wherein the sensor data includes data relating to a distance between the aerial device and a potential obstacle and the controller is arranged to operate the actuator based on the data relating to the distance.

7. The aerial device of claim 5 , the aerial device further comprising an energy store, and wherein the controller is arranged to operate the actuator based on an energy level of the energy store.

8. The aerial device of claim 1 , wherein the body defines a space for the rotor to rotate within.

9. The aerial device of claim 8 , wherein the space is defined by a duct portion of the body, and further wherein at least a portion of the duct portion is moveable relative to the body so that, when the rotor rotates relative to the body and the at least a portion of the duct portion is moved, a fluid flow through the duct portion is changed.

10. An aerial device capable of controlled flight, the aerial device comprising:
a body;
a rotor arranged to rotate relative to the body; a rotor guard arranged to define a space for the rotor to rotate within; and
one or more deployable structures, each structure having an undeployed configuration in which that structure is compressed against the rotor guard and a deployed configuration in which that structure extends away from the rotor guard,
wherein at least a portion of the rotor guard is arranged to rotate relative to the body and relative to the rotor.

11. The aerial device of claim 10 , wherein the rotor is a first rotor, the aerial device further comprising a second rotor arranged to rotate relative to the body, wherein the rotor guard is arranged to define a space for both the first and second rotors to rotate within.

12. The aerial device of claim 10 , wherein an outer perimeter of the rotor guard has one or more radiused corners and at least one of the one or more deployable structures is fixed to one of the radiused corners.

13. The aerial device of claim 10 , wherein the deployable structure is a sheet and wherein, in the undeployed configuration, the sheet is folded against the rotor guard and, in the deployed configuration, the sheet is at least partially unfolded away from the rotor guard.

14. The aerial device of claim 13 , wherein the rotor is arranged to rotate in a plane and wherein, in the deployed configuration, the sheet is at least partially unfolded away from the body in a direction parallel to the plane.

15. The aerial device of claim 10 , wherein the one or more deployable structures comprises a plurality of deployable structures, and wherein each deployable structure is fixed to a respective portion of an outer perimeter of the rotor guard.

16. The aerial device of claim 10 , further comprising an actuator operable to deploy the structure from the undeployed configuration to the deployed configuration and/or to undeploy the structure from the deployed configuration to the undeployed configuration.

17. The aerial device of claim 10 , wherein the body defines a space for the rotor to rotate within.

18. The aerial device of claim 17 , wherein the space is defined by a duct portion of the body, and further wherein at least a portion of the duct portion is moveable relative to the body so that, when the rotor rotates relative to the body and the at least a portion of the duct portion is moved, a fluid flow through the duct portion is changed.

Assignees

• Imperial College Sci Tech & Medicine

Inventors

• Kovac Mirko
• Sareh Pooya

Classifications

• B64U50/14

  ducted or shrouded · CPC title

• B64U30/26

  Ducted or shrouded rotors · CPC title

• B64U10/14

  with four distinct rotor axes, e.g. quadcopters · CPC title

• B64U50/13

  using external fans or propellers · CPC title

• B64C2203/00

  Flying model aircraft, flying toy aircraft · CPC title