Unmanned aerial vehicle with remote starting device

Abstract

The invention provides an unmanned aerial vehicle with a remote starting device, and solves the technical problem that an engine is liable to shut down when a small-sized unmanned aerial vehicle in the prior art flies. The unmanned aerial vehicle comprises an internal combustion engine, an electrical device and a starting motor, wherein the electrical device is electrically connected with the starting motor; the output shaft of the starting motor is in transmission connection with the rotary output end of the internal combustion engine through a transmission device; the electrical device is provided with a wireless signal receiving and sending module which remotely operates the starting motor to start and stop; and the electrical device is electrically connected with an inner power supply system of the small-sized unmanned aerial vehicle. According to the unmanned aerial vehicle provided by the invention, the remote starting device is arranged for the small-sized unmanned aerial vehicle, so that the technical effect that the engine is liable to shut down when the small-sized unmanned aerial vehicle flies in a bad environment is overcome; and the wireless signal receiving and sending module arranged in the electrical device is in signal connection with a control base station or a remote controller, so that start and stop of the starting motor are remotely and wirelessly operated, and therefore, powerful technical support is provided for wirelessly starting the internal combustion engine of the unmanned aerial vehicle.

Description

technical field [0001] The invention relates to the technical field of small unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a remote start device. Background technique [0002] In the prior art, the internal combustion engine used as an engine for drones is mainly developed for large-scale model airplanes. Because large-scale model airplanes are usually equipped with relatively complete safety facilities, they can make up for the inherent defects of the engine, and then can adapt to conditions with relatively harsh temperature, humidity and air pressure. flight environment. However, due to the structural size and weight of the above-mentioned safety facilities, they are usually abandoned in the structural design of small UAVs. Therefore, the reduced configuration brings certain safety hazards to the flight safety of small UAVs, especially When small unmanned aerial vehicles fly in the harsh environment of high altitude in mountainous areas, techn...

AI Technical Summary

Problems solved by technology

However, due to the structural size and weight of the above-mentioned safety facilities, they are usually abandoned in the structural design of small UAVs. Therefore, the reduced configuration brings certain safety hazards to the flight safety of small UAVs, especially When small UAVs fly in the harsh environment of high altitude in mountainous areas, it is very easy to have technical failures that cause the engine to stall

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