Airborne unmanned aerial vehicle charging

• US 10,099,561 B1
• Filed: 09/25/2015
• Issued: 10/16/2018
• Est. Priority Date: 09/25/2015
• Status: Active Grant

• Current Assignee: Amazon Technologies, Inc. (Amazon.com, Inc.)
• Original Assignee: Amazon Technologies, Inc. (Amazon.com, Inc.)
• Inventors: Ananthanarayanan, Peruvemba Ranganathan Sai, Dron, Anuj, Napoles, Adrian, Sammeta, Rohit, Zheng, Ming
• Primary Examiner(s): Grant, Robert
• Application Number:
  US14/866,740
• Time in Patent Office: 1,117 Days
• Field of Search: 320109
• CPC Class Codes: B60L 2200/10 Air crafts
• CPC Class Codes: B60L 2260/32 Auto pilot mode
• CPC Class Codes: B60L 5/005 without mechanical contact between the collector and the power supply line
• CPC Class Codes: B60L 50/53 in combination with an external power supply, e.g. from overhead contact lines
• CPC Class Codes: B60L 53/12 Inductive energy transfer
• CPC Class Codes: B60L 53/126 Methods for pairing a vehicle and a charging station, e.g. establishing a one-to-one relation between a wireless power transmitter and a wireless power receiver
• CPC Class Codes: B60L 53/32 by charging in short intervals along the itinerary, e.g. during short stops
• CPC Class Codes: B60L 53/36 by positioning the vehicle
• CPC Class Codes: B60L 53/38 specially adapted for charging by inductive energy transfer
• CPC Class Codes: B60L 53/80 Exchanging energy storage elements, e.g. removable batteries
• CPC Class Codes: B60L 9/00 Electric propulsion with power supply external to the vehicle electric propulsion for monorail vehicles, suspension vehicles or rack railways B60L13/00; in combination with batteries or fuel cells within the vehicle B60L50/53
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 2101/00 UAVs specially adapted for particular uses or applications
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/34 In-flight charging photovoltaics B64U50/31
• CPC Class Codes: B64U 50/37 Charging when not in flight
• CPC Class Codes: B64U 50/39 Battery swapping
• CPC Class Codes: B64U 70/20 for releasing or capturing UAVs in flight by another aircraft
• CPC Class Codes: B64U 70/30 : for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
• CPC Class Codes: B64U 70/90 : Launching from or landing on platforms
• CPC Class Codes: B64U 80/25 : for recharging batteries; for refuelling
• CPC Class Codes: B64U 80/82 : Airborne vehicles
• 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
• CPC Class Codes: Y02T 90/14 : Plug-in electric vehicles

Abstract

This disclosure describes a power unmanned aerial vehicle (UAV) that may generate a current from a conductor of an overhead power line carrying an AC power signal. The power UAV has a receptor that includes a secondary coil. Current is generated by the secondary coil of the receptor from magnetic fields emanating from the overhead power lines while the power UAV is flying. The generated current may be used to fly the power UAV, recharge an energy storage device of the power UAV, or be provided to another UAV. In various implementations, while the power UAV is flying, the power UAV may receive another UAV, recharge the other UAV, and then release the UAV to resume flying. In various implementations, the power UAV may also monitor characteristics of the power delivery system.

Claims

1. A power unmanned aerial vehicle (UAV), comprising:

a flight system having control electronics to control a flight of the power UAV and a flight mechanism to provide lift to the power UAV;

a receptor positioned to generate a current from a magnetic field emanating from a conductor of an overhead power line while the power UAV is flying proximate to the conductor;

a first shielding substrate disposed between at least a portion of the control electronics and the receptor;

a frame coupled to the receptor, the flight mechanism, and the first shielding substrate;

wherein the power UAV, while the power UAV is flying, is configured to at least;

engage a second UAV; and

provide a charging current to the second UAV; and

wherein a position of the first shielding substrate is configured to at least be adjustable with respect to the frame while the power UAV is flying.

2. The power UAV of claim 1, further comprising:

an energy storage device, wherein at least a portion of the current generated by the receptor is provided to the energy storage device for storage.

3. The power UAV of claim 1, further comprising:

a platform coupled to the frame to support the second UAV when a flight mechanism of the second UAV is deactivated.

4. The power UAV of claim 1, further comprising:

a second shielding substrate configured to reduce the magnetic field from a near side of the second shielding substrate to a far side of the second shielding substrate by at least 90% to shield at least a portion of the control electronics of the second UAV while the receptor is generating current;

wherein the second shielding substrate is adjustable between a first position and a second position; and

wherein in the second position, the second shielding substrate is between at least the portion of the control electronics of the second UAV and the receptor.

5. A method to generate current with a power unmanned aerial vehicle (“

UAV”

), the method comprising;

flying the power UAV to a position along a conductor of an overhead power line such that a receptor coupled to the power UAV is at a location where a magnetic field emanating from the conductor of the overhead power line is present;

generating, with the receptor, a current from the magnetic field emanating from the conductor of the overhead power line;

adjusting, while the power UAV is in flight, a position of a shielding substrate with respect to a frame of the power UAV; and

wherein the current is generated while the power UAV is in flight.

6. The method of claim 5, further comprising:

determining that the current should be generated based on at least one of;

a price charged by an owner of the overhead power line for generating the current using the power UAV;

a level of charge associated with an energy storage device of the power UAV;

a request to provide a charge to a second UAV;

or

a second level of charge associated with a second energy storage device of the second UAV.

7. The method of claim 5, further comprising:

receiving from flight, on a platform of the power UAV and while the power UAV is flying, a second UAV; and

charging an energy storage device of the second UAV while the second UAV is on the platform of the power UAV and the power UAV is flying.

8. The method of claim 5, further comprising:

electrically coupling a second UAV to the power UAV; and

providing a charging current by the power UAV to the second UAV.

9. The method of claim 8, further comprising:

monitoring an amount of current provided by the power UAV to the second UAV; and

determining a fee to charge for power provided by the power UAV to the second UAV.

10. The method of claim 8, further comprising:

determining that the second UAV has received a sufficient amount of generated current; and

decoupling the second UAV from the power UAV such that the second UAV may resume flight.

11. The method of claim 5, further comprising:

determining at least one of;

a relative distance between the conductor and the receptor;

or

a relative orientation between the receptor and the conductor; and

adjusting a position of the receptor based on at least one of the relative distance or the relative orientation.

12. The method of claim 11, wherein the adjusting the position of the receptor is further based on at least one of wind data, humidity or precipitation.

13. The method of claim 5, further comprising:

determining a relative distance between the conductor and the receptor based at least in part by monitoring a magnitude of the current.

14. The method of claim 5, further comprising:

flying the power UAV to a plurality of different locations of a power delivery system; and

at least one of;

measuring electromagnetic energy emanating from a conductor at each of the plurality of different locations;

or

capturing an image including at least a portion of the power delivery system at each of the plurality of different locations.

15. The method of claim 5, further comprising:

determining an amount of power drawn from the conductor by the receptor; and

determining a fee for the amount of power drawn from the conductor.

16. The method of claim 5, further comprising:

determining the location along the conductor based at least in part on at least one of;

UAV traffic data;

a location of another power source for charging a UAV;

or

a cost of drawing power from the conductor at the location.

17. A power unmanned aerial vehicle (UAV), comprising:

a flight system for flying the power UAV, the flight system having control electronics and a flight mechanism;

a receptor configured to at least, while the power UAV is flying, generate a current from a magnetic field emanating from a conductor of an overhead power line cable; and

a shielding substrate that is configured to, while the power UAV is flying, at least be adjustable with respect to a frame of the power UAV.

18. The power UAV of claim 17,

wherein the shielding substrate includes a Faraday cage, the Faraday cage configured to shield at least one of:

1) electronics of the power UAV;

or

     2) electronics of a second UAV that is on the power UAV.

19. The power UAV of claim 17, further comprising:

a control element, wherein the receptor is attached to an adjustable member configured to at least, while the power UAV is flying, adjust a position of the receptor with respect to the frame in response to control signals from the control element.

20. The power UAV of claim 17, wherein the receptor includes at least one coil.

21. The power UAV of claim 17, further comprising a platform sized and configured for landing a second UAV thereupon while the power UAV is flying;

and

wherein at least a portion of the current is provided to the second UAV.

22. The power UAV of claim 17, further comprising a first current sensor coupled to the receptor, the first current sensor configured to output a signal indicative of a characteristic of the current.