UNMANNED AERIAL VEHICLES

• US 20180194463A1
• Filed: 07/22/2015
• Published: 07/12/2018
• Est. Priority Date: 07/23/2014
• Status: Active Grant

• Current Assignee: Airbus Defence and Space Limited
• Original Assignee: Airbus Defence and Space Limited
• Inventors: HASINSKI, Julian, TURTON, Brian
• Granted Patent: US 10,618,650 B2
• Time in Patent Office: Days
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64C 39/028 Micro-sized aircraft
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/26 Ducted or shrouded rotors
• CPC Class Codes: B64U 50/14 ducted or shrouded

Abstract

Unmanned aerial vehicles (1), and methods of flying such, comprising at least four rotors (2) arranged such that the plane of rotation of each rotor (2) is co-planar with a face of a notional polyhedron, and wherein each face of the notional polyhedron is co-planar with the plane of rotation of at least one rotor (2). Such methods comprise: a first step of flying the vehicle (1) using a first rotor set (2a-c) to provide lift; and, a second step using a second rotor set (2d-f) to provide lift; wherein, the second rotor set (2d-f) includes at least one rotor (2) that is not used to provide lift in the first step or that operates so that airflow through the rotor (2) is in the opposite direction to that through the rotor (2) during the first step; and, wherein at least one of the first and second sets (2a-c, 2d-f) comprises a plurality of rotors (2).

Claims

1. An unmanned aerial vehicle, wherein

the unmanned aerial vehicle comprises at least four rotors, each rotor having a plane of rotation,

the at least four rotors are arranged such that the plane of rotation of each rotor is co-planar with a face of a notional polyhedron, and

each face of the notional polyhedron is co-planar with the plane of rotation of at least one rotor.

2. An unmanned aerial vehicle according to claim 1, wherein the notional polyhedron is a convex polyhedron.

3. An unmanned aerial vehicle according to claim 1, wherein the notional polyhedron is a cube.

4. An unmanned aerial vehicle according to claim 1, wherein the area of any one face of the notional polyhedron is not more than 150% of the area of any other face of the notional polyhedron.

5. An unmanned aerial vehicle according to claim 1, wherein for each rotor the diameter of the circular disc-shape that is swept out by the rotor when rotated is not less than 25% of the longest dimension of the face of the notional polyhedron coplanar with the rotor.

6. An unmanned aerial vehicle according to claim 1, where all of the at least four rotors are substantially the same size.

7. An unmanned aerial vehicle according to claim 1, wherein the unmanned aerial vehicle comprises a body, and wherein each of the at least four rotors is surrounded by the body in the rotational plane of the rotor.

8. An unmanned aerial vehicle according to claim 1, wherein the unmanned aerial vehicle comprises a body in the form of an exoskeleton structure which both provides the supporting structure of the UAV and surrounds and protects each of the rotors in the rotational plane of the rotor.

9. An unmanned aerial vehicle according to claim 1, wherein the unmanned aerial vehicle comprises a body having at least four faces, wherein each of the at least four rotors is recessed into one of the at least four faces of the body.

10. An unmanned aerial vehicle according to claim 1, wherein each of the at least four rotors is driven by a circumferential drive.

11. An unmanned aerial vehicle according to claim 1, wherein the volume of the notional polyhedron is less than 200,000 cm³.

12. An unmanned aerial vehicle according to claim 1, wherein the unmanned aerial vehicle comprises at least four sensors, and wherein each sensor is located in the region of a vertex of the notional polyhedron.

13. An unmanned aerial vehicle according to claim 12, wherein at least one sensor is positioned in the region of every vertex of the notional polyhedron.

19. A unmanned aerial vehicle according to claim 1, wherein the at least four rotors are configured and arranged such that in any orientation of the vehicle there will be at least one rotor positioned such that its axis of rotation is oriented less than 60 degrees to the vertical, and such that the vehicle is arranged to be able to fly in any orientation of the vehicle.

20. An unmanned aerial vehicle according to claim 1, wherein the unmanned aerial vehicle comprises a main body, wherein each of the rotors is arranged at the periphery of the main body, and wherein the main body is so shaped as to define a space within the centre of the body which facilitates the flow of air to or from each of the rotors.

14. (canceled)

15. A method of flying an unmanned aerial vehicle, the vehicle comprising at least four independently controllable rotors, wherein the method comprises:

a first step of flying the vehicle using a first set of the rotors to provide lift; and

,

a second step of flying the vehicle using a second set of the rotors to provide lift;

wherein, the second set of rotors used in the second step includes at least one rotor that is not used to provide lift in the first step or that operates so that the airflow through the rotor is in the opposite direction to that of the airflow through the rotor during the first step; and

,

wherein at least one of the first set and the second set comprises a plurality of rotors.

16. A method of flying an unmanned aerial vehicle according to claim 15, wherein the method additionally comprises:

a third step of flying the vehicle using a third set of the rotors to provide lift;

wherein the third set of rotors used in the third step includes at least one rotor that is not used to provide lift in the first step or that operates so that the airflow through the rotor is in the opposite direction to that of the airflow through the rotor during the first step.

17. A method of flying an unmanned aerial vehicle in order to capture data from an environment, the unmanned aerial vehicle comprising a plurality of sensors mounted at different locations on the vehicle to capture such data, wherein the method comprises a step of flying the vehicle so that it assumes a first orientation in space at which first data is captured by the sensors, rotating the vehicle by at least +90 degrees about a substantially horizontal axis so as to assume a second different orientation in space at which second data is captured by the sensors.

18. A method of flying an unmanned aerial vehicle according to claim 17, wherein the method additionally comprises rotating the vehicle by at least +90 degrees about the same or a different substantially horizontal axis so as to assume a third different orientation in space at which third data is captured by the sensors.

23. A method of flying an unmanned aerial vehicle according to claim 17, wherein

each of the plurality of sensors mounted at different locations is an imaging sensor,

the method includes imaging an area using the unmanned aerial vehicle,

the unmanned aerial vehicle comprises at least four rotors, each rotor having a plane of rotation,

the at least four rotors are arranged such that the plane of rotation of each rotor is co-planar with a face of a notional polyhedron,

each face of the notional polyhedron is co-planar with the plane of rotation of at least one rotor,

each imaging sensor is located in the region of a vertex of the notional polyhedron.

21-22. -22. (canceled)