A multifunctional portable multi-rotor UAV

Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and provides a multifunctional portable multi-rotor unmanned aerial vehicle, comprising a frame, a tripod and at least 4 rotor assemblies; the frame includes an upper center plate and a lower center plate, and the upper part of the upper center plate is The flight control installation layer is equipped with the control system. The battery installation layer is between the upper center board and the lower center board. The battery is installed inside. The battery can be quickly positioned and fixed through the partition. The lower center board is equipped with a mission load installation layer. , the load equipment can be quickly connected and removed through the quick change device and the lower center plate; the rotor assembly is arranged around the frame and connected with the frame through a fast horizontal folding device; Pipe clips enable quick connection and removal. The invention provides a foldable, multi-layer arrangement, long battery life, small size, multi-function, fast disassembly and assembly, safety, and modular multi-rotor remote control aircraft, which is an industrial-grade unmanned aerial vehicle that can be rapidly expanded and applied to different working conditions solution.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and more specifically relates to a multifunctional portable multi-rotor unmanned aerial vehicle. Background technique [0002] At present, in the field of UAVs, multi-rotor UAVs have the characteristics of flexible maneuverability, fast response, unmanned driving, and low operating requirements. UAVs are equipped with various types of sensors, such as cameras, which can realize real-time image transmission and detection of high-risk areas. Functions, widely used in firefighting, military, traffic, police, exploration and meteorology, etc., to achieve cruising shooting and monitoring of designated areas. [0003] In the fuselage structure of a multi-rotor unmanned aerial vehicle, the arms are usually folded in the vertical direction, and the space occupied after folding is still a bit large, which brings inconvenience to packaging and transportation. At present, most of the multi...

AI Technical Summary

Problems solved by technology

[0003] In the fuselage structure of a multi-rotor unmanned aerial vehicle, the arms are usually folded in the vertical direction, and the space occupied after folding is still a bit large, which brings inconvenience to packaging and transportation

At present, most of the multi-rotor aerial photography UAVs on the market are of fixed layout structure, which is inconvenient to disassemble and assemble different loads, and has a single function, which makes it difficult to meet the requirements of the same customer in different periods, different occasions, and different purposes. At the same time, if the aircraft is flying in the air, if there is no navigation light and warning light, it is difficult to judge the flight direction of the aircraft with the naked eye, which may easily lead to accidents

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