RECHARGING AN AIRCRAFT BATTERY

• US 20150097530A1
• Filed: 08/18/2014
• Published: 04/09/2015
• Est. Priority Date: 10/03/2013
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Scarlatti, David, Casado, Enrique, Maza, Ivan, Esteban Campillo, David, Caballero, Fernando
• Granted Patent: US 9,643,507 B2
• Time in Patent Office: Days
• US Class Current: 320/109
• CPC Class Codes: B60L 53/35 Means for automatic or assisted adjustment of the relative position of charging devices and vehicles
• CPC Class Codes: H02J 7/00 Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
• CPC Class Codes: H02J 7/00045 Authentication, i.e. circuits for checking compatibility between one component, e.g. a battery or a battery charger, and another component, e.g. a power source
• CPC Class Codes: Y02T 10/70 Energy storage systems for electromobility, e.g. batteries
• CPC Class Codes: Y02T 10/7072 Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
• CPC Class Codes: Y02T 90/12 Electric charging stations

Abstract

And aircraft recharging station is provided for recharging an aircraft provided with a rechargeable battery. The recharging station includes a parking surface with conductive tiles selectively connected to an electrical power supply. The recharging station also includes a controller configured to determine a position of the aircraft on the parking surface by connecting, including being configured to iteratively connect a different pair of tiles to the electrical power supply to provide a circuit including positive and negative tiles connected thereto, and test an electrical circuit condition of the circuit, until a closed circuit condition is determined, thereby indicating that the aircraft is positioned on the positive and negative tiles, and that the battery is thereby rechargeable by the electrical power supply.

Claims

1. An aircraft recharging station comprising:

a parking surface disposed for an aircraft provided with a battery to rest thereon, the battery being rechargeable, and the parking surface comprising conductive tiles;

a switching circuit configured to allow selectively an electrical connection between an electrical power supply and any two of the conductive tiles; and

a controller configured to determine a position of the aircraft on the parking surface to allow recharging of the battery by the electrical power supply, including the controller being configured to control the switching circuit to iteratively connect a different pair of the conductive tiles to the electrical power supply to provide a circuit including a positive tile and a negative tile connected to the electrical power supply, and test an electrical circuit condition of the circuit connected to the electrical power supply, until a closed circuit condition is determined, thereby indicating that the aircraft is positioned on the positive tile and the negative tile, and that the battery is thereby rechargeable by the electrical power supply.

2. The aircraft recharging station of claim 1, wherein each conductive tile of the conductive tiles is provided with an electrical connector and insulated from other, adjacent conductive tiles of the conductive tiles,

wherein the electrical power supply is provided with a positive output and a negative output, and

wherein the switching circuit being configured to allow selectively an electrical connection between the electrical power supply and any two of the conductive tiles includes being configured to allow selectively an electrical connection between the positive output and the electrical connector of any conductive tile of the conductive tiles, and allow selectively an electrical connection between the negative output and the electrical connector of any other conductive tile of the conductive tiles.

3. The aircraft recharging station of claim 2, wherein the aircraft is provided with a positive terminal and a negative terminal connected to the battery, the positive terminal and negative terminal both being arranged to be in contact with one or more of the conductive tiles when the aircraft is resting on the parking surface.

4. The aircraft recharging station of claim 3, wherein the controller being configured to determine the position of the aircraft includes being configured to at least:

control the switching circuit to connect the positive output of the electrical power supply to the electrical connector of a conductive tile of the conductive tiles, and connect the negative output of the electrical power supply to the electrical connector of another conductive tile of the conductive tiles, thereby making the conductive tile the positive tile and the other conductive tile the negative tile; and

test the electrical circuit condition between the positive output and negative output of the electrical power supply, and

wherein the controller is configured to iteratively control the switching circuit and test the electrical circuit condition until the closed circuit condition is determined, thereby indicating that the positive output of the electrical power supply is connected to the positive terminal of the aircraft via the positive tile, and the negative output of the electrical power supply is connected to the negative terminal of the aircraft via the negative tile.

5. The aircraft recharging station of claim 4, wherein the controller being configured to determine the position of the aircraft includes being configured to perform one or more iterations of an outer loop and an inner loop,

wherein the outer loop includes the controller being configured to control the switching circuit to iteratively connect either the positive output or the negative output of the electrical power supply to the electrical connector of different ones of the conductive tiles, thereby making the different ones of the conductive tiles the positive tile or the negative tile respectively,

wherein after each iteration of the controller making a conductive tile the positive tile or the negative tile, the inner loop includes the controller being configured to control the switching circuit to iteratively connect the other of the positive output or the negative output of the electrical power supply to the electrical connector of different ones of the conductive tiles other than the conductive tile made the positive tile or the negative tile, thereby making the different ones of the conductive tiles the other of the positive tile or the negative tile, and

wherein the controller is configured to perform the one or more iterations of the outer loop and the inner loop until the closed circuit condition is determined.

6. The aircraft recharging station of claim 5, wherein the conductive tiles are congruent and arranged in a repeating pattern, and

wherein the controller being configured to iteratively connect the other of the positive output or the negative output of the electrical power supply includes being configured to iteratively connect the other of the positive output or the negative output to the electrical connector of different ones of the conductive tiles adjacent to the conductive tile made the positive tile or the negative tile.

7. The aircraft recharging station of claim 1, wherein the parking surface comprises an array of the conductive tiles that are arranged to fill the parking surface.

8. The aircraft recharging station of claim 1, wherein the aircraft is configured to contact the parking surface through a plurality of landing feet, landing wheels, or extending members.

9. The aircraft recharging station of claim 8, wherein a landing event occurs when a portion of the aircraft makes contact with the landing pad, the landing event being detected using at least one of pressure sensitive switches, video monitoring, audio monitoring, and breaking a light beam.

10. The aircraft recharging station of claim 1, wherein the aircraft is a rotorcraft or a fixed-wing craft.

11. The aircraft recharging station of claim 1, wherein the aircraft is an unmanned aerial vehicle (UAV).

12. A system comprising:

an aircraft recharging station comprising a parking surface including conductive tiles in the shape of squares; and

an aircraft comprising a battery that is rechargeable and connected to a positive terminal and a negative terminal that are both arranged to be in contact with one or more of the conductive tiles when the aircraft is resting on the parking surface, the positive terminal being separated from the negative terminal by a distance greater than the length of a longest span across a conductive tile of the parking surface but less than twice the width of a conductive tile of the parking surface,

wherein the aircraft recharging station is configured to determine a position of the aircraft on the parking surface to allow recharging of the battery by an electrical power supply, including being configured to iteratively connect a different pair of the conductive tiles to the electrical power supply to provide a circuit including a positive tile and a negative tile connected to the electrical power supply, and test an electrical circuit condition of the circuit connected to the electrical power supply, until a closed circuit condition is determined, thereby indicating that the aircraft is positioned on the positive tile and the negative tile, and that the battery is thereby rechargeable by the electrical power supply.

13. The system of claim 12, wherein the positive terminal and negative terminal of the aircraft are in the form of landing feet, landing wheels, or extending members.

14. A method of recharging a battery of an aircraft using a recharging station comprising a parking surface disposed for the aircraft to rest thereon, the battery being rechargeable, the parking surface comprising conductive tiles, and the method comprising:

determining a position of the aircraft on the parking surface, including iteratively connecting a different pair of the conductive tiles to an electrical power supply of the recharging station to provide a circuit including a positive tile and a negative tile connected to the electrical power supply, and testing an electrical circuit condition of the circuit connected to the electrical power supply, until a closed circuit condition is determined, thereby indicating that the aircraft is positioned on the positive tile and the negative tile, and that the battery is thereby rechargeable by the electrical power supply; and

recharging the battery using the electrical power supply as connected to the aircraft via the positive tile and the negative tile.

15. The method of claim 14, wherein the electrical power supply is provided with a positive output and a negative output, and

wherein iteratively connecting a different pair of the conductive tiles to the electrical power supply includes iteratively connecting the positive output of the electrical power supply to a conductive tile to provide the positive tile, and the negative output of the electrical power supply to another conductive tile to provide the negative tile.

16. The method of claim 15, wherein the aircraft is provided with a positive terminal and a negative terminal connected to the battery, the positive terminal and negative terminal both being arranged to be in contact with one or more of the conductive tiles when the aircraft is resting on the parking surface,

wherein determining the position of the aircraft on the parking surface comprises:

connecting the positive output of the electrical power supply to a conductive tile of the conductive tiles, and connecting the negative output of the electrical power supply to another conductive tile of the conductive tiles, thereby making the conductive tile the positive tile and the other conductive tile the negative tile; and

determining the electrical circuit condition between the positive output and negative output of the electrical power supply, and

wherein connecting the positive output and negative output of the electrical power supply, and determining the electrical circuit condition, are iteratively performed until the closed circuit condition is determined, thereby indicating that the positive output of the electrical power supply is connected to the positive terminal of the aircraft via the positive tile, and the negative output of the electrical power supply is connected to the negative terminal of the aircraft via the negative tile.

17. The method of claim 16, wherein determining the position of the aircraft on the parking surface includes performing one or more iterations of an inner loop and an outer loop,

wherein the outer loop includes iteratively connecting either the positive output or the negative output of the electrical power supply to different ones of the conductive tiles, thereby making the different ones of the conductive tiles the positive tile or the negative tile respectively,

wherein after each iteration of making a conductive tile the positive tile or the negative tile, the inner loop includes iteratively connecting the other of the positive output or the negative output of the electrical power supply to different ones of the conductive tiles other than the conductive tile made the positive tile or the negative tile, thereby making the different ones of the conductive tiles the other of the positive tile or the negative tile, and

wherein the one or more iterations of the outer loop and the inner loop are performed until the closed circuit condition is determined.

18. The method of claim 17, wherein iteratively connecting the other of the positive output or the negative output of the electrical power supply includes iteratively connecting the other of the positive output or the negative output to the electrical connector of different ones of the conductive tiles adjacent to the conductive tile made the positive tile or the negative tile.

19. The method of claim 18, wherein in the outer loop, iteratively connecting either the positive output or the negative output of the electrical power supply includes in at least one iteration, selecting and connecting either the positive output or the negative output of the electrical power supply to a conductive tile adjacent to the tile made the positive tile or the negative tile in an immediately preceding iteration of the outer loop.

20. The method of claim 18, wherein in the inner loop, iteratively connecting the other of the positive output or the negative output of the electrical power supply includes in a plurality of iterations, selecting and connecting the other of the positive output or the negative output of the electrical power supply to different ones of the conductive tiles adjacent to the conductive tile made the positive tile or the negative tile, in turn in a clockwise or anti-clockwise direction.