Vehicle

Patent metadata

Field	Value
Publication number	US-10899429-B2
Application number	US-201816637799-A
Country	US
Kind code	B2
Filing date	Aug 10, 2018
Priority date	Aug 15, 2017
Publication date	Jan 26, 2021
Grant date	Jan 26, 2021

Abstract

The present invention provides a vehicle comprising: a rotor and a stator; at least one planar control surface coupled to the rotor, wherein the rotor is configured to rotate relative to the stator such that, in use, the at least one planar control surface moves from a first position to a second position, and wherein in the first position the planar control surface is controllable to affect substantially only the pitch of the vehicle and in the second position the planar control surface is controllable to affect substantially both of the pitch and yaw of the vehicle, or substantially only the yaw, or in the first position the planar control surface is controllable to affect substantially only the yaw of the vehicle and in the second position the planar control surface is controllable to affect substantially both of the pitch and yaw of the vehicle, or substantially only the pitch of the vehicle. The present invention also provides a method of controlling a vehicle.

First claim

What is claimed is:

1. A vehicle comprising:
a rotor and a stator;
at least one planar control surface coupled to the rotor, such that the control surface extends perpendicularly from the periphery of the rotor, wherein the rotor is configured to rotate relative to the stator such that, in use, the at least one planar control surface moves from a first position to a second position, and wherein:
in the first position the planar control surface is controllable to affect only the pitch of the vehicle and in the second position the planar control surface is controllable to affect both of the pitch and yaw of the vehicle, or only the yaw; or
in the first position the planar control surface is controllable to affect only the yaw of the vehicle and in the second position the planar control surface is controllable to affect both of the pitch and yaw of the vehicle, or only the pitch of the vehicle; and
at least one actuator coupled to the rotor and to the stator, wherein the control surface is coupled to the rotor such that the control surface extends perpendicularly from the periphery of the rotor wherein, in use, when a first actuator is in a first configuration the rotor is rotated such that the planar control surface is arranged in the first position, and when the first actuator is in a second configuration the rotor is rotated such that the planar control surface rotates about the central axis of the rotor to be arranged in the second position, wherein the at least one actuator comprises a plurality of actuators arranged in pairs; and
first and second pistons, each pivotably connected to the rotor and to the stator;
wherein, in use, when the first piston is in a first configuration the rotor is rotated such that the planar control surface is arranged in the first position, and when the first piston is in a second configuration, the rotor is rotated such that the planar control surface rotates about the central axis of the rotor to be arranged in the second position; and
wherein, in use, when the first piston extends, the second piston retracts to cause rotation of the rotor.

2. The vehicle according to claim 1 , wherein a longitudinal axis of the vehicle and central axis of the stator are arranged in parallel.

3. The vehicle according to claim 1 , wherein in the first position the planar control surface is co-planar with the local horizontal plane of the vehicle and in the second position the planar control surface is arranged in a plane at 45 degrees to the local horizontal plane.

4. The vehicle according to claim 1 , wherein the plurality of actuators consists of only three pairs of actuators.

5. The vehicle according to claim 1 , wherein the plurality of actuators define an elongate space having the stator and rotor disposed at the longitudinal ends of the elongate space, and wherein the stator and rotor are annular.

6. The vehicle according to claim 5 , wherein an engine is disposed in the elongate space.

7. The vehicle according to claim 6 , wherein the at least one actuator is configured to incline the central axis of the rotor with respect to the central axis of the stator in order to vector the thrust of the engine;
wherein the inclination of the central axis is symmetric within a cone about the central axis.

8. The vehicle according to claim 5 , wherein, in use, when one actuator expands another actuator retracts to cause rotation of the rotor only about the central axis of the rotor.

9. The vehicle according to claim 1 , comprising a second rotor and a second stator, the second rotor being coupled to a second planar control surface, wherein the second rotor is configured to rotate relative to the second stator such that, in use, the second planar control surface moves from the first position to the second position, and wherein the rotor is arranged adjacent and parallel to the second rotor such that the planar control surface and the second planar control surface are arranged on opposite sides of the vehicle with respect to each other.

10. The vehicle according to claim 1 , wherein the vehicle is an aircraft.

11. The vehicle according to claim 10 , wherein the planar control surface is a tail plane; and
wherein the rotor is a tail cone.

12. The vehicle of claim 1 , wherein the rotor comprises an open-ring rotatable rotor member to which a rotor end of the actuators are attached, wherein an outside edge of the open-ring rotatable rotor member is coupled to an inner wall of a tail surface of the vehicle; and
the stator comprises an open-ring fixed stator member to which opposite, stator, ends of the actuators are attached, wherein an outside edge of the open-ring fixed stator member is coupled to an inner wall of a fuselage of the vehicle;
wherein an outer diameter of the open-ring rotatable rotor member is less than an outer diameter of the open-ring fixed stator member, whereby a flow is maintained.

13. The vehicle of claim 1 , wherein the actuators are coupled directly to an inside surface of a tail fairing; and
an opposite end of each actuator is coupled directly to an inside surface of a fuselage.

14. The vehicle of claim 1 , wherein the rotatable member comprises a baffle for coupling a tail fairing to a fuselage wherein the baffle is able to compress and expand to reduce radar cross section and to prevent gaps forming in the outside surface of the vehicle when the rotatable member pivots up, down, left or right with respect to the fuselage.

15. The vehicle according to claim 1 , wherein the plurality of actuators define an elongate space having the stator and rotor disposed at the longitudinal ends of the elongate space, and wherein the stator and rotor are annular; and
wherein an engine is disposed in the elongate space;
the engine surrounded by a cylindrical engine casing;
wherein the cylindrical engine casing comprises recesses whereby, when actuators surrounding the cylindrical engine casing are at maximum extension, midpoints of each fully extended actuator are accommodated by the recesses in the cylindrical engine casing;
whereby a clearance is maintained between moving and static parts, with clearance for emergency extension limits of the actuators without contact with equipment disposed between the plurality of actuators.

16. A method of controlling a vehicle comprising:
providing a rotating rotor relative to a stator, a planar control surface being coupled to the rotor, such that the planar control surface moves from a first position to a second position, such that the control surface extends perpendicularly from the periphery of the rotor, wherein:
in the first position the planar control surface is controllable to affect only the pitch of the vehicle and in the second position the planar control surface is controllable to affect both of the pitch and yaw of the vehicle, or only the yaw; or
in the first position the planar control surface is controllable to affect only the yaw of the vehicle and in the second position the planar control surface is controllable to affect both of the pitch and yaw of the vehicle, or only the pitch; and
at least one actuator coupled to the rotor and to the stator, wherein the control surface is coupled to the rotor such that the control surface extends perpendicularly from the periphery of the rotor wherein, in use, when a first actuator is in a first configuration the rotor is rotated such that the planar control surface is arranged in the first position, and when the first actuator is in a second configuration the rotor is rotated such that the planar control surface rotates about the central axis of the rotor to be arranged

Assignees

• Bae Systems Plc

Inventors

• White Andrew Charles

Classifications

• B64C3/42

  Adjusting about chordwise axes · CPC title

• F02K9/84

  using movable nozzles · CPC title

• B64C9/02

  Mounting or supporting thereof · CPC title

• B64C5/10 Primary

  adjustable · CPC title

• F02K1/006

  within one plane only · CPC title