A split drone

Abstract

The invention discloses a split-type unmanned aerial vehicle (UAV). A vehicle body and a load cabin are connected by circular-ring-shaped connectors and a spring bolt which can be quickly mounted and dismounted through a rotation operation. A spring pull rod is used to quickly compact and separate a cabin cover and a cabin case. Quick-assembly hinges with an embedded design allow quick assembly and detachment of control surfaces on wings and on an empennage, and avoid the influence on overall vehicle performance caused by the exposing of the quick-assembly hinges. Steering gears are mounted in an embedded way so that aerodynamic performance of a UAV is not affected, and the steering gears are easy to be replaced. A lock structure of a parachute cabin cover uses a built-in way to ensure the smoothness outside the parachute cabin cover. Pipe fittings of a fuselage part are in a quick inserted connection to facilitate the assembling and disassembling of the pipe fittings. A drive motor is connected with the vehicle body by a motor mounting part which facilitates the assembling and disassembling of a propeller drive motor. A pitot tube is in an inserted and fixed connection with one of the wings and is easy to be dismounted, and the aerodynamic performance of the UAV is not affected.

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

Images