UAV hybrid power systems and methods

Patent metadata

Field	Value
Publication number	US-11228200-B2
Application number	US-201916704608-A
Country	US
Kind code	B2
Filing date	Dec 5, 2019
Priority date	Dec 31, 2015
Publication date	Jan 18, 2022
Grant date	Jan 18, 2022

Abstract

A hybrid power system comprises a power controller adapted to be in communication with a first power source, a second power source, and a load. The power controller is configured to: control discharging of the first power source without permitting discharging of the second power source to power the load when a power drawn by the load is greater than a predetermined threshold power for a time period; and control discharging of the second power source to power the load when the power drawn by the load is greater than the predetermined threshold power starting from when the time period ends.

First claim

What is claimed is:

1. A hybrid power system, comprising:
a power controller adapted to be in communication with a first power source, a second power source, and a load, wherein the power controller is configured to:
control discharging of the first power source without permitting discharging of the second power source to power the load when a power drawn by the load is greater than a predetermined threshold power for a time period; and
control discharging of the second power source to power the load when the power drawn by the load is greater than the predetermined threshold power starting from when the time period ends.

2. The hybrid power system of claim 1 , wherein the first power source is a fuel cell and the second power source is a super capacitor.

3. The hybrid power system of claim 1 , wherein the first power source is a fuel cell and the second power source is a lithium-ion battery.

4. The hybrid power system of claim 1 , wherein the first power source is a lithium-ion battery and the second power source is a super capacitor.

5. The hybrid power system of claim 1 , wherein:
the time period is less than or equal to a predetermined time period; and
the predetermined time period is determined based on a power density of the second power source.

6. The hybrid power system of claim 5 , wherein the second power source is configured to supplement the first power source to power the load starting from when the time period ends.

7. The hybrid power system of claim 1 , wherein:
when the power drawn by the load is greater than the predetermined threshold power for the time period, the power controller is configured to control the first power source to discharge a current to power the load for the time period.

8. The hybrid power system of claim 1 , wherein:
when the power drawn by the load is greater than the predetermined threshold power starting from when the time period ends, the power controller is configured to control the first power source to discharge a first current and the second power source to discharge a second current to power the load starting from when the time period ends.

9. The hybrid power system of claim 8 , wherein the second current is configured to supplement the first current to power the load.

10. The hybrid power system of claim 1 , wherein the power controller is configured to control the discharging of the second power source to power the load when the first power source is depleted.

11. The hybrid power system of claim 1 , wherein a power density of the second power source is higher than a power density of the first power source.

12. The hybrid power system of claim 1 , wherein an energy capacity density of the first power source is higher than an energy capacity density of the second power source.

13. The hybrid power system of claim 1 , further comprising:
one or more current sensors to detect whether and/or when the current drawn by the load exceeds the predetermined threshold power.

14. The hybrid power system of claim 13 , wherein the sensors are further configured to detect one or more discharging currents between the first power source, the second power source, and the load.

15. An unmanned aerial vehicle (UAV), comprising:
a load comprising at least one propulsion unit; and
a power controller adapted to be in communication with a first power source, a second power source, and the load, wherein the power controller is configured to:
control discharging of the first power source without permitting discharging of the second power source to power the load when a power drawn by the load is greater than a predetermined threshold power for a time period; and
control discharging of the second power source to power the load when the power drawn by the load is greater than the predetermined threshold power starting from when the time period ends.

16. The UAV according to claim 15 , wherein the first power source is a fuel cell and the second power source is a super capacitor.

17. The UAV according to claim 15 , wherein the first power source is a fuel cell and the second power source is a lithium-ion battery.

18. A method for controlling power delivery, comprising:
controlling, with aid of one or more processors, discharging of a first power source without permitting discharging of a second power source to power the load when a power drawn by the load is greater than a predetermined threshold power for a time period; and
controlling, with the aid of the one or more processors, discharging of the second power source to power the load when the power drawn by the load is greater than the predetermined threshold power starting from when the time period ends.

19. The method according to claim 18 , further comprising:
in response to the power drawn by the load being greater than the predetermined threshold power for the time period, controlling the first power source to discharge a current to power the load for the time period.

20. The method according to claim 18 , further comprising:
in response to the power drawn by the load being greater than the predetermined threshold power starting from when the time period ends, controlling the first power source to discharge a first current and the second power source to discharge a second current to power the load starting from when the time period ends.

Assignees

• Sz Dji Technology Co Ltd

Inventors

• Wang Lei
• Wang Wentao
• Zheng Dayang
• Zhan Juncheng
• Liu Yuancai

Classifications

• B64U50/31

  generated by photovoltaics · CPC title

• H02J7/34 Primary

  Parallel operation in networks using both storage and other DC sources, e.g. providing buffering (H02J7/14 takes precedence) · CPC title

• B64U30/20 Primary

  Rotors; Rotor supports · CPC title

• B64U10/14

  with four distinct rotor axes, e.g. quadcopters · CPC title

• B64U50/19

  using electrically powered motors · CPC title