A UAV projectile device applying a new generation of information technology

Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to an unmanned aerial vehicle ejection device applying a new generation of information technology. The opening connecting inside and outside, the bottom of the chamber is fixedly connected with a compression mechanism, the upper end of the compression mechanism is fixedly connected with a lifting mechanism, the upper end of the lifting mechanism is fixedly connected with a moving plate, one end of the sliding mechanism is fixedly connected with one end of the lifting mechanism, and the sliding mechanism is connected with the other end of the lifting mechanism. The lifting mechanism is arranged in communication, and the inner walls of the front and rear ends of the chamber are vertically provided with a first chute, and a matching slider is provided in the first chute, and the opposite side walls of the two sliders are respectively connected with the moving plate. The side walls at the front and rear ends are fixedly connected. The advantage is that the invention can reduce the dependence of the fixed-wing UAV on the space environment such as the runway, so that it can be used normally in an environment similar to the take-off of the rotor UAV.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to an unmanned aerial vehicle ejection device applying a new generation of information technology. Background technique [0002] Unmanned aircraft, referred to as unmanned aerial vehicle, is an unmanned aircraft controlled by radio remote control equipment and self-contained program control device, or is completely or intermittently operated autonomously by on-board computer. With the development of information technology, unmanned It has also begun to gradually use the new generation of information technology to develop a new generation of drone use platform. [0003] UAVs are generally divided into two types of take-off methods, that is, the vertically ascending rotorcraft and the fixed-wing aircraft that take off by taxiing or gliding. Compared with the rotorcraft, the fixed-wing aircraft has a larger load capacity, and the use of technology is more m...

AI Technical Summary

Problems solved by technology

[0003] UAVs are generally divided into two types of take-off methods, that is, the vertically ascending rotorcraft and the fixed-wing aircraft that take off by taxiing or gliding. Compared with the rotorcraft, the fixed-wing aircraft has a larger load capacity, and the use of technology is more mature and the flight is more stable. advantages, but its disadvantage is that it needs a long enough runway and has high requirements for the take-off environment. Therefore, for fixed-wing UAVs, the field problem is usually an important factor that limits its popularity.

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