Battery, aircraft with battery and battery control method

Abstract

The invention discloses a battery which comprises a power supply and a power supply circuit, wherein the power supply circuit is electrically connected with the power supply and comprises an electronic switch and an input device; the electronic switch is electrically connected with an output pole of the power supply and used for controlling on and off of the power supply; and the input device is electrically connected with the electronic switch and controls an on / off state of the electronic switch. The electronic switch controls the on and off of the power supply, so that the problem of electric spark in a power-on process can be avoided, and the normal use of the battery and safety of an aircraft are ensured. Correspondingly, the invention further provides the battery, the aircraft with the battery, and a battery control method.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a battery, an aircraft with the battery and a control method for the battery. Background technique [0002] In the field of model aircraft, most aircraft use batteries as power sources. When users use them, except for a few applications that use switches as discharge control devices, most of them use the interface between the battery and the equipment to be powered. to control device power-on. During the connection of the interfaces of two devices or during the closing of a mechanical switch, at the last connected contact position, sparks are generated. [0003] The electric spark during the power-on process has two great hazards. First, the electric spark will bring an instantaneous high voltage, which is often 2 to 3 times higher than the battery voltage. This voltage will damage the equipment to be powered. Second, the electric spark will ablate the contact point, resulting in an inc...

AI Technical Summary

Problems solved by technology

[0003] The electric spark during the power-on process has two great hazards. First, the electric spark will bring an instantaneous high voltage, which is often 2 to 3 times higher than the battery voltage. This voltage will damage the equipment to be powered.

Second, the electric spark will ablate the contact points, resulting in increased resistance or poor contact, which is a very serious safety hazard for flying model aircraft

[0004] At the same time, because the current is usually very large, and there is no charge and discharge protection function, the battery is often damaged due to over-discharge, and there is a certain probability that the battery will explode or bulge due to over-charging.

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