A UAV take-off aid

Abstract

The invention relates to the field of UAV auxiliary equipment, in particular to an UAV take-off auxiliary device, which includes a base on which a booster mechanism with adjustable inclination is arranged, and the booster mechanism is provided with a device for clamping and fixing the UAV. The clamping mechanism, the booster mechanism is also provided with a pneumatic thrust mechanism for accelerating the UAV, and the booster mechanism is provided with a trigger mechanism for simultaneously releasing the pressure of the pneumatic thrust mechanism and unlocking the clamping mechanism. This kind of drone take-off auxiliary device plays an auxiliary role in the take-off of the drone through the booster mechanism and the pneumatic thrust mechanism, thereby effectively improving the take-off speed of the drone and improving the operating efficiency of the drone, without the need to build a special runway , reduce the cost of use, and can meet the problem of heavy load of the UAV when it takes off, and use the clamping mechanism to clamp and fix the UAV to ensure that the UAV remains stable on the slide rail, thereby ensuring that the whole device is safe for no one. The stability and reliability of the aircraft-assisted take-off process.

Description

technical field [0001] The invention relates to the field of auxiliary equipment for unmanned aerial vehicles, in particular to an auxiliary device for unmanned aerial vehicle take-off. Background technique [0002] UAV is an unmanned aircraft operated by radio remote control equipment and self-contained program control device. The development of drones is becoming more and more mature, and its application fields are becoming more and more extensive. [0003] When the UAV is performing take-off operations, compared with the UAV with the screw wing, the UAV using the fixed wing structure and the turbine as the power needs to reach a certain speed for take-off, and use the air lift to make it rise. It requires a very long run-up field. The requirements for the use of this type of UAV are relatively high, and the input cost is correspondingly high. Moreover, when the UAV is carrying out heavy-duty operations, there is a large energy consumption during the take-off process. In...

AI Technical Summary

Problems solved by technology

[0003] When the drone is taking off, compared with the screw-wing drone, the drone that uses the fixed wing structure and the turbine as the power needs to reach a certain speed for take-off, and use the air lift to make it rise. It requires a very long run-up field. The requirements for the use of this type of UAV are relatively high, and the input cost is correspondingly high. Moreover, when the UAV is carrying out heavy-duty operations, there is a large energy consumption during the take-off process. In view of this, we propose a UAV take-off assisting device

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