Small unpowered unmanned aerial vehicle mounting device

Abstract

The invention provides a small unpowered unmanned aerial vehicle mounting device. The small unpowered unmanned aerial vehicle mounting device comprises a base, a loading carbon rod, a steering engineplug and a rubber bandage, wherein the upper end of the loading carbon rod is fixed in the middle of the base, a spring is arranged in a sleeve mode outside a carbon fiber cylindrical rod, the upper end of the spring is fixed onto the base, the lower end of the spring is fixedly provided with a limiting and fixing device which is internally provided with hole allowing the carbon fiber cylindricalrod to penetrate through, the lower surface of the limiting and fixing device is provided with a groove matched in shape with the surface of an unmanned aerial vehicle to be mounted, one end of the rubber bandage is fixed onto the base and on one side of the loading carbon rod, and the other end of the rubber bandage is a free end; the steering engine plug is fixed onto the base and on the other side of the loading carbon rod for fixing or releasing the free end of the rubber bandage. By means of high-strength and low-weight materials and a relatively simple mounting structure, the small unpowered unmanned aerial vehicle mounting device effectively reduces the overall weight and increase the strength; the unmanned aerial vehicle is in a laminated mounting structure, so that the number of mounting can be effectively increased, and the loading size can be reduced.

Description

technical field [0001] The invention relates to the technical field of loading and launching control of aircraft loads, in particular to a small unpowered unmanned aerial vehicle mounting device. Background technique [0002] As we all know, UAV is an unmanned aircraft that can perform tasks autonomously only through radio remote control instructions and program control. It has many advantages such as high flexibility, low cost, and convenient use. It is widely used in civilian and military applications. and other fields. [0003] There are many ways for drones to take off, such as rocket launch, runway roll, and high-altitude drop. It can perform a variety of tasks, such as high-altitude target drones, military reconnaissance, and target strikes. For traditional mounting tasks, commonly used hanger forms are shown in Figure 1(a) and Figure 1(b), where Figure 1(a) is a single-point hanger and Figure 1(b) is a multi-point hanger shelf. Usually, the upper part of the pylon...

AI Technical Summary

Problems solved by technology

[0006] When the traditional mounting device mounts multiple loads, the multiple loads are all concentrated in one mounting plane, and for larger task loads, a set of racks can usually only mount one load, As a result, the number of mounts is small, and it seems powerless in applications that require a large number of mounts and small loads.

[0007] (2) The structure is more complicated and the weight is larger

[0008] Traditional delivery devices are generally made of metal materials (such as aluminum alloy), which are suitable for manned aircraft with heavy load and high structural strength. , therefore, the metal material delivery device is not suitable for applications that require the overall weight of the UAV to be light

[0009] (3) Traditional hangers are not suitable for mounting small UAVs

[0010] In some important military applications, the mounting task of UAVs is to mount smaller UAVs (hereinafter referred to as "mounted UAVs"). Compared with ordinary mission loads, the mounted UAVs The shape of the pylon is relatively complicated, and there is a certain aerodynamic shape, and the structural strength is not high. In this case, the traditional pylon cannot achieve stable and fixed mounting.

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