Power generation and distribution for vehicle propulsion

• US 10,017,266 B2
• Filed: 09/21/2017
• Issued: 07/10/2018
• Est. Priority Date: 09/22/2016
• Status: Active Grant

• Current Assignee: Istari Digital Incorporated
• Original Assignee: Top Flight Technologies, Inc.
• Inventors: Phan, Long N., Duong, Luan H., Nayfeh, Samir, Sweetland, Matthew
• Primary Examiner(s): Ellis, Christopher P
• Application Number:
  US15/711,175
• Publication Number:
  US 20180079516A1
• Time in Patent Office: 292 Days
• CPC Class Codes: B64D 27/026 comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine Hybrid electric aircraft B64D27/33
• CPC Class Codes: B64D 27/10 of gas-turbine type jet aircraft B64D27/16
• CPC Class Codes: B64D 27/24 using steam or spring force jet aircraft B64D27/16
• CPC Class Codes: B64U 50/11 using internal combustion piston engines
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: F01D 15/10 Adaptations for driving, or combinations with, electric generators
• CPC Class Codes: F05D 2220/76 an electrical generator
• CPC Class Codes: H02J 2310/44 for aircrafts
• CPC Class Codes: H02J 7/1415 with a generator driven by a prime mover other than the motor of a vehicle
• CPC Class Codes: H02K 7/1823 structurally associated with turbines or similar engines
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

An aerial vehicle includes a hybrid power generation system comprising an engine; a generator mechanically coupled to the engine; and a propulsion system comprising an electric motor electrically coupled to the generator and a rotational mechanism coupled to the electric motor.

Claims

1. An aerial vehicle comprising:

a hybrid power generation system comprising;

a combustion engine; and

a generator mechanically coupled to the combustion engine;

a plurality of propulsion systems, each propulsion system located remote from the hybrid power generation system, each propulsion system comprising;

an electric motor electrically coupled to the generator; and

a rotational mechanism coupled to the electric motor;

an electronic control unit configured to control operations for the combustion engine; and

a plurality of electronic speed controllers configured to control operations for the plurality of propulsion systems, respectively,

wherein controlling operations of the combustion engine is independent of controlling the plurality of propulsion systems,

wherein controlling operations of at least one propulsion system is independent of controlling the remainder of the plurality of propulsion systems, and

wherein the combustion engine is controlled to produce a single rotational output that is provided to the mechanically coupled generator.

2. The aerial vehicle of claim 1, wherein the rotational mechanism comprises a propeller.

3. The aerial vehicle of claim 1, wherein the rotational mechanism comprises a fan.

4. The aerial vehicle of claim 1, wherein the generator is configured to convert mechanical energy from the engine into electrical energy.

5. The aerial vehicle of claim 4, wherein the electric motor is configured to convert the electrical energy from the generator into rotational mechanical energy.

6. The aerial vehicle of claim 5, wherein the rotational mechanism is configured to be driven by the rotational mechanical energy from the electric motor.

7. The aerial vehicle of claim 1, wherein one or more of the plurality of propulsion system is located on a wing of the aerial vehicle and the hybrid power generation system is located on a body of the aerial vehicle.

8. The aerial vehicle of claim 1, each of the plurality of propulsion systems comprising:

an electric motor electrically coupled to the generator; and

a rotational mechanism coupled to the electric motor.

9. The aerial vehicle of claim 8, wherein each electric motor is configured to operate independently of each other electric motor.

10. The aerial vehicle of claim 1, comprising a battery electrically coupled to the generator and to the electric motor.

11. The aerial vehicle of claim 1, comprising one or more of a sensing subsystem, a computing subsystem, and a communications subsystem electrically coupled to the generator.

12. A method comprising:

in a hybrid power generation system of an aerial vehicle;

generating mechanical energy in a combustion engine; and

converting the generated mechanical energy into electrical energy in a generator mechanically coupled to the combustion engine;

at an electronic control unit, controlling operations of the combustion engine such that the combustion engine operates to produce a single rotational output that is provided to the mechanically coupled generator;

at each of a plurality of electronic speed controllers, controlling operations of at least one of a plurality of propulsion systems, respectively;

at the plurality of propulsion systems of the aerial vehicle, each propulsion system located remote from the hybrid power generation system;

converting the electrical energy into rotational mechanical energy to drive rotation of a rotational mechanism of each propulsion system;

driving rotation of the rotational mechanism in each propulsion system independently of the rotation of the rotational mechanism in each other propulsion system,

wherein controlling operations of the combustion engine at the electronic control unit is independent of controlling the plurality of propulsion systems, and

wherein controlling operations of the plurality of propulsion systems is independent of controlling operations of the combustion engine.

13. The method of claim 12, comprising driving rotation of a first rotational mechanism in a first direction and driving rotation of a second rotational mechanism in a second direction, the first direction different from the second direction.

14. The method of claim 12, comprising driving rotation of a first rotational mechanism at a first speed and driving rotation of a second rotational mechanism at a second speed, the first speed different from the second speed.

15. The method of claim 12, comprising storing at least some of the electrical energy in a battery.

16. The method of claim 12, comprising providing at least some of the electrical energy to one or more of a sensing subsystem, a computing subsystem, and a communications subsystem.