IN-FLIGHT BATTERY RECHARGING SYSTEM FOR AN UNMANNED AERIAL VEHICLE

• US 20160325834A1
• Filed: 05/09/2016
• Published: 11/10/2016
• Est. Priority Date: 05/07/2015
• Status: Abandoned Application

• Current Assignee: Sonin Aerospace, LLC
• Original Assignee: Sonin Aerospace, LLC
• Inventors: Foster, Curtis Asa
• Application Number:
  US15/149,972
• Publication Number:
  US 20160325834A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64D 27/24 using steam or spring force jet aircraft B64D27/16
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 30/10 Wings
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/26 Ducted or shrouded rotors
• CPC Class Codes: B64U 50/12 using turbine engines, e.g. turbojets or turbofans
• CPC Class Codes: B64U 50/14 ducted or shrouded
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/34 In-flight charging photovoltaics B64U50/31

Abstract

An in-flight battery recharging system for Unmanned Aerial Vehicle (UAV). This invention converts byproducts of a multi-rotor unmanned aerial vehicle'"'"'s conventional propulsion system operation and airframe movements to generate electricity that, in turn, is used to power the propulsion system'"'"'s electric motors, power onboard electronic components, and recharge the battery that initially powers the propulsion system'"'"'s electric motors. Having this ability of recharging the battery in-flight gives an unmanned aerial vehicle a much improved flight time and range, thereby greatly increasing its utility.

Claims

1. An in-flight charging system for an unmanned aerial vehicle (UAV), comprising:

a hub portion,

a motor attached to the hub portion via a support arm,

a rotor rotationally driven by the motor to produce a thrust airflow; and

a prop oriented for rotational movement in the thrust airflow and operatively coupled to a generator via a generator shaft, the generator producing a first electrical charge responsive to the rotational movement of the prop with the thrust airflow.

2. The in-flight charging system of claim 1, further comprising:

a power conditioning circuit, coupled to the generator, and configured to produce a regulated direct current output from the first electrical charge.

3. The in-flight charging system of claim 2, further comprising:

a battery, operatively coupled to the power conditioning circuit, wherein an output of the power conditioning circuit charges the battery.

4. The in-flight charging system of claim 1, wherein the prop is coaxially aligned with the rotor.

5. The in-flight charging system of claim 2, wherein the power conditioning circuit further comprises:

an AC to DC rectifier coupled to the generator;

a voltage regulator coupled to the AC to DC rectifier;

a boost converter; and

a battery charger integrated circuit.

6. The in-flight charging system of claim 5, further comprising:

a storage capacitor operatively coupled to the voltage regulator.

7. The in-flight charging system of claim 2, further comprising:

a micro generator operatively coupled to a motor shaft, the micro generator adapted to produce a second electrical charge with rotation of the motor shaft.

8. The in-flight charging system of claim 7, wherein the power conditioner receives the second electrical charge.

9. The in-flight charging system of claim 1, further comprising:

an auxiliary generator operatively coupled to the hub portion, the auxiliary generator driven by an auxiliary prop oriented to receive an airflow across the hub.

10. The in-flight charging system of claim 1, wherein the motor comprises a ducted fan.

11. The in-flight charging system of claim 10, further comprising:

a flight control surface oriented subjacent to an outlet of the ducted fan.