Quick dismounting and mounting design scheme for load and body of small unmanned aerial vehicle

Abstract

The invention relates to the design of a quick load mounting and dismounting mode of an unmanned aerial vehicle and the power supply and data transmission reliability design. The unmanned aerial vehicle structure manufactured under the guide of the scheme is convenient to mount and dismount, high in environmental adaptability, high in function extensibility and good in man-machine working efficiency. With the adoption of the design scheme, a lot of time for mounting and dismounting a small unmanned aerial vehicle system in a war can be saved, and the effect of the system of the small unmanned aerial vehicle can be played better; the load and body connecting operation process of the unmanned aerial vehicle can be simplified through the mature structure processing production technology and the electrical communication interface design technology; on the basis of the mature design technology, the use requirement on quick mounting and dismounting of an aerial vehicle can be ensured through a buckling type physical inserting manner and an elastic needle type electric connecting manner. The design highlights the quickness of the structure connection and the reliability of the electrical connection.

Description

technical field [0001] The invention relates to the design of the fast installation and disassembly mode of the unmanned aerial vehicle load and the reliability design of power supply and data transmission. Guided by this plan, the completed UAV structure has the characteristics of convenient installation and disassembly, strong environmental adaptability, strong function expansion, and good ergonomics, which is conducive to the use of small UAV systems in wartime and saves a lot of assembly and disassembly time, so that the combat effectiveness of the small unmanned aerial vehicle system can be brought into play to a greater extent. technical background [0002] The development of UAV technology is an important direction for the development of the world's aviation industry. In addition to the rapid improvement of aircraft flight performance and load information post-processing technology, the reliability and stability of aircraft structure installation, functional module st...

AI Technical Summary

Problems solved by technology

[0003] The installation of each functional module of the traditional small unmanned aerial vehicle system aircraft is fixed by screw standard parts or locking devices of different specifications and models, and the electrical communication system is completed by the traditional and more complicated connector communication connection method. There are the following disadvantages: the assembly and disassembly takes a long time, which is not conducive to wartime use; the maintenance process is complicated, and special tools are required; the number of disassembled parts is large, and it is not easy to keep; the maintenance and use costs are high

It is difficult to meet the growing demand for the use of military digital equipment

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