COOLING A POWER SYSTEM FOR AN UNMANNED AERIAL VEHICLE

1 . An unmanned aerial vehicle comprising:

at least one rotor motor configured to drive at least one propeller to rotate;

a micro hybrid generator system configured to provide power to the at least one rotor motor, the micro hybrid generator system comprising:

a rechargeable battery configured to provide power to the at least one rotor motor;

a small engine configured to generate mechanical power; and

a generator motor coupled to the small engine and configured to generate electrical power from the mechanical power generated by the small engine; and

a cooling system configured to couple to the micro hybrid generator system, the cooling system comprising:

one or more plates; and

a plurality of fins extending from each of the one or more plates,

wherein the cooling system is configured to dissipate heat from the micro hybrid generator system.

2 . The unmanned aerial vehicle of claim 1 , wherein the one or more plates are configured to couple to the small engine.

3 . The unmanned aerial vehicle of claim 1 , wherein at least one of the plates and the corresponding plurality of fins is positioned substantially beneath one of the propellers.

4 . The unmanned aerial vehicle of claim 1 , wherein the plurality of fins extend in a perpendicular direction from the one or more plates.

5 . The unmanned aerial vehicle of claim 1 , wherein the plates are physically coupled to the small engine.

6 . The unmanned aerial vehicle of claim 1 , wherein the plates are coupled to the generator motor.

7 . The unmanned aerial vehicle of claim 1 , wherein the cooling system comprises an impeller.

8 . The unmanned aerial vehicle of claim 7 , wherein the impeller is coupled to the small engine.

9 . The unmanned aerial vehicle of claim 7 , wherein the impeller is coupled to the rotor motor.

10 . The unmanned aerial vehicle of claim 1 , wherein the plates are coupled to one or more exhaust pipes of the small engine.

11 . The unmanned aerial vehicle of claim 1 , wherein the plates are formed of metal.

12 . The unmanned aerial vehicle of claim 1 , wherein the fins comprise multiple groups of fins, each group of fins extending from a corresponding surface of one of the plates.

13 . The unmanned aerial vehicle of claim 1 , wherein the fins are spaced equally.

14 . The unmanned aerial vehicle of claim 1 , wherein fins located at the perimeter of each plate are fanned away from fins located in an interior region of the surface of the plate.

15 . The unmanned aerial vehicle of claim 1 , wherein the one or more plates are positioned below the at least one propeller.

16 . A method comprising:

operating a hybrid energy generation system to provide electrical energy to a rotor motor configured to drive rotation of a propeller of an unmanned aerial vehicle, comprising:

generating mechanical energy in an engine of the hybrid electrical energy generation system;

in a generator of the hybrid energy generation system, converting the mechanical energy into electrical energy;

providing at least some of the electrical energy produced by the generator to a rechargeable battery of the hybrid energy generation system; and

one or more of (i) providing at least some of the electrical energy produced by the generator to the rotor motor of the hybrid energy generation system and (ii) providing electrical energy from the rechargeable battery of the hybrid energy generation system to the rotor motor; and

cooling the hybrid energy generation by dissipation of heat to a cooling system, the cooling system comprising:

one or more plates; and

a plurality of fins extending from each of the one or more plates.