A quick disassembly and assembly mechanism for the tail of a small fixed-wing unmanned aerial vehicle and its application method

Abstract

The invention discloses a small-sized fixed-wing unmanned aerial vehicle tail quick disassembly mechanism and its use method, comprising a body, two horizontal tails and a vertical tail, the two horizontal tails are respectively located The straight empennage is located on the top of the fuselage, the vertical empennage is located between the two horizontal empennages, the first mounting block is fixedly installed on both sides of the fuselage, the first mounting block is provided with a third groove, and the The inner walls on both sides of the third groove are symmetrically provided with card slots, and a fixed block is fixedly installed on one side of the horizontal tail. The invention is simple to operate and can quickly install and disassemble the UAV tail, which solves the problem The installation of the UAV is complicated and requires a long installation time, which buys time for the special operation of the UAV, and this installation method is more stable than the previous installation method, preventing the UAV from loosening during the work and affecting its normal operation. .

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a quick disassembly and assembly mechanism for the tail of a small fixed-wing unmanned aerial vehicle and a method for using the same. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the...

AI Technical Summary

Problems solved by technology

[0003] The existing small fixed-wing UAV tail quick disassembly mechanism is complicated to disassemble the UAV tail, and it takes a lot of time to waste, and the installation is not stable enough. For some special operations of UAVs, time is life, so a kind of Small fixed-wing UAV tail quick disassembly mechanism, and has a high stability mechanism after installation

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