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UAV power component management system, management method and UAV

A technology for component management and machine power supply, applied in aircraft parts, transportation and packaging, etc., can solve the problem of inability to achieve emergency return and landing of drones, and achieve the effect of improving flight reliability.

Active Publication Date: 2021-04-02
HIWING AVIATION GENERAL EQUIP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The present invention provides a UAV power supply component management system, management method and UAV, which can solve the technical problem in the prior art that it is impossible to realize the emergency return and landing of UAVs without auxiliary power supply and emergency power supply

Method used

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  • UAV power component management system, management method and UAV
  • UAV power component management system, management method and UAV
  • UAV power component management system, management method and UAV

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Embodiment Construction

[0022] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. The following description of at least one exemplary embodiment is merely illustrative in nature and in no way taken as limiting the invention, its application or uses. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0023] It should be noted that the terminology used here is only for describing specific implementations, and is not intended to limit t...

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Abstract

The invention provides an unmanned aerial vehicle power supply assembly management system, a management method and the unmanned aerial vehicle. The unmanned aerial vehicle power supply assembly management system comprises a power supply confluence unit, a power supply assembly, a power distribution center unit and a center control and management unit; a generator and a battery pack are arranged onthe power supply confluence unit in parallel; the power distribution center unit is connected with the power supply confluence unit; a plurality of electric devices are connected with the power distribution center unit through a second switch group; the central control and management unit is connected with the power supply confluence unit and controls connection and disconnection between the generator and the power supply confluence unit, the charging and discharging state of the battery pack and connection and disconnection between the plurality of electric devices and the power distributioncenter unit according to the voltage of the power supply confluence unit and the working state of the generator. By applying the technical scheme provided by the invention, the technical problem thatemergency return and landing of the unmanned aerial vehicle without an auxiliary power supply and an emergency power supply cannot be realized in the prior art is solved.

Description

technical field [0001] The invention relates to the technical field of electrical systems of unmanned aerial vehicles, in particular to a management system and method for power supply components of unmanned aerial vehicles and unmanned aerial vehicles. Background technique [0002] As an important component system of the UAV, the power supply system is of great significance to the safe and autonomous flight of the UAV. In general, in order to improve the flight reliability of the UAV, its power supply system includes main power supply, auxiliary power supply and emergency power supply. However, for drones without auxiliary power and emergency power, it is also necessary to consider the emergency return and landing of the drone when the main power fails. However, in the prior art, for drones without auxiliary power and emergency power, there is no corresponding power management method for power management to realize emergency return and landing of the drone. Contents of th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D47/00
Inventor 邢艳丽田晓威周维民
Owner HIWING AVIATION GENERAL EQUIP