A battery constant temperature device for a multi-rotor UAV

Abstract

The invention discloses a battery constant temperature device for a multi-rotor UAV, which comprises a UAV battery tank, a circular groove is opened at the bottom of the UAV battery tank, and a circular groove matching the circular groove is arranged in the circular groove. A heating plate, and the side wall of the heating plate is fixedly connected with the groove wall of the circular groove, the upper side of the heating plate is provided with a U-shaped heat conducting plate, and the side wall of the U-shaped heat conducting plate is fixed to the groove wall of the UAV battery groove Connection, the lower side of the U-shaped heat conducting plate is attached to the upper side of the heating plate, the inner side of the U-shaped heat conducting plate is provided with a U-shaped heat-insulating plate, and the outer side of the U-shaped heat-conducting plate is fixed to the inner side of the U-shaped heat-conducting plate connection, the upper side of the battery tank of the drone is provided with a horizontal baffle, and the upper front and rear side walls of the battery tank of the drone are provided with a horizontal chute, and the inner side of the slider is fixed to both sides of the baffle connected, the upper front side of the baffle and the upper wall of the battery slot of the drone are provided with serrated protrusions, so that the battery of the drone can maintain a constant temperature.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a battery constant temperature device for a multi-rotor unmanned aerial vehicle. Background technique [0002] UAV is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but it is equipped with autopilot, program control device and other equipment. Radar and other equipment, for tracking, positioning, remote control, telemetry and digital transmission, can take off like an ordinary plane under radio control or launch it with a booster rocket, and can also be brought into the air by the mother plane. However, its battery is due to Under the influence of low temperature, the power supply is often unstable, which makes the UAV fall accidents. Therefore, we propose a battery constant temperature device for multi-rotor UAVs to solve the above problems. Contents of the invention [0003] The purpo...

AI Technical Summary

Problems solved by technology

[0002] UAV is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but it is equipped with autopilot, program control device and other equipment. Radar and other equipment, for tracking, positioning, remote control, telemetry and digital transmission, can take off like an ordinary plane under radio control or launch it with a booster rocket, and can also be brought into the air by the mother plane. However, its battery is due to Under the influence of low temperature, the phenomenon of unstable power supply often occurs, which makes the drone fall accidently. Therefore, we propose a battery constant temperature device for multi-rotor drones to solve the above problems.

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