A split drone

Abstract

The invention is a split-type unmanned aerial vehicle. The body and the load compartment are connected by an annular connector and a spring latch, and can be quickly disassembled and assembled through a rotation operation. A spring pull rod is used between the hatch cover and the hatch shell to quickly compress and open. The quick-release hinges with embedded design can quickly assemble and separate the rudder surfaces on the wings and tail, and avoid the hinges being exposed to the outside and affecting the performance of the entire machine. The steering gear is built-in, which does not affect the aerodynamic performance of the drone and makes it easy to replace the steering gear. The canopy canopy locking structure adopts a built-in method to ensure the smoothness of the outside of the canopy canopy. The pipe fittings in the fuselage are connected using a quick plug-in method to facilitate the loading and unloading of pipe fittings. The drive motor is connected to the body through a motor mounting piece to facilitate the installation and removal of the propeller drive motor. The pitot tube and the wing are plugged and fixed for easy disassembly without affecting the aerodynamic performance of the entire aircraft.

Description

Technical field [0001] The invention relates to an unmanned aerial vehicle, in particular to a split unmanned aerial vehicle capable of carrying mission equipment for exploration. Background technique [0002] In recent years, electric drones have developed rapidly and are widely used in military, public security, agriculture, aerial photography and other fields. At present, most electric drones are powered by propellers. With the continuous heat dissipation of electric drones and the continuous introduction of new products, various types of drones are also emerging. The application in various occasions requires different The overall design is required. The existing split UAV can be improved in the way of assembly and the way of connection between the various components. [0003] There are roughly two common ways to install UAV rudder surfaces. One is to make the UAV rudder surface and the wing surface integrally, and then cut the rudder surface, leaving the upper or lower surfa...

AI Technical Summary

Problems solved by technology

One is to directly use the rudder plate of the steering gear to press the umbrella cover, the disadvantage is that the rudder plate must be exposed outside the body, and the steering gear needs enough installation space

The second is to use the overall umbrella bag with its own umbrella opening device. The disadvantage is that the drone needs to be equipped with enough installation space, which may affect the planning of the whole machine.

[0006] The conventional steering gear installation method needs to add installation card slots and other devices in the body, the structure is complex and the process is cumbersome, and the installation accuracy deviation is large

There is also a way to fix the steering gear on the carbon plate, and then fix the carbon plate on the wing surface, which affects the aerodynamic shape of the drone

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