A split drone

A kind of unmanned aerial vehicle, split-type technology, applied in the direction of wings, aircraft accessories, aircraft assembly, etc., can solve the problems of large installation accuracy deviation, complex structure, cumbersome process, etc., and achieve convenient disassembly, convenient loading and unloading, and convenient replacement Effect

CN107010244BActive Publication Date: 2019-08-09BEIJING ZHAOYANG SCI TECH CULTURE
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Publication Date
2019-08-09

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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.
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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...

Examples

Embodiment Construction

[0070] In order to have a clearer understanding of the technical features, objectives and effects of the present invention, specific embodiments of the present invention will now be described with reference to the accompanying drawings. The term "connection" in the present invention includes not only the direct connection between two components, but also the connection between two components through at least one intermediate component. The location words (such as upper, lower, front, back, etc.) used in the present invention are only used to express the technical content more clearly in conjunction with the drawings, and are not specific limitations on the technical solutions of the present invention.

[0071] Such as Figure 1 to Figure 5 As shown, the present invention provides a split UAV 100, which includes a body 101 and a load bay 102. The body 101 includes an integral upper and lower parts. The lower part of the body 101 is a cylindrical shell with open ends. The front and...