Electric rocket device

Abstract

The invention discloses an electric rocket device. The device comprises a cylindrical shell, an electric driving mechanism is arranged at the lower end of the cylindrical shell, an automatic opening mechanism is arranged at the upper end of the cylindrical shell, and a linkage triggering mechanism is arranged on one side of the automatic opening mechanism. The electric rocket device disclosed by the invention has the beneficial effects that the device can have small wind resistance during capturing under the action of the automatic opening mechanism, and the stability of the device is improved; through the design of the electric driving mechanism and the overall structure, the moving speed of the equipment can be increased, the capturing precision is improved, and misoperation can be avoided through the action of the linkage triggering mechanism.

Description

technical field [0001] The invention relates to the technical field of electric rockets, and more specifically, relates to an electric rocket device. Background technique [0002] With the continuous maturity of remote sensing technology, navigation technology and electronic technology, small unmanned aerial vehicles have brought convenience to industry, agricultural production or other fields, but they have also brought certain hidden dangers to public safety; A no-fly zone has been established, and relevant management measures have been gradually introduced, but there are always incidents of aircraft out of control or malicious intrusion, and small unmanned aerial vehicles need to be captured or intercepted forcibly; [0003] Due to the small size and flexible flight routes of low-altitude small unmanned aerial vehicles, it is not suitable for general military ground-to-air interception devices, especially in densely populated areas. There are several types such as carryi...

AI Technical Summary

Problems solved by technology

[0002] With the continuous maturity of remote sensing technology, navigation technology and electronic technology, small unmanned aerial vehicles have brought convenience to industry, agricultural production or other fields, but they have also brought certain hidden dangers to public safety; A no-fly zone has been established, and relevant management measures have been gradually introduced, but there are always incidents of aircraft out of control or malicious intrusion, and small unmanned aerial vehicles need to be captured or intercepted forcibly;

[0003] Due to the small size and flexible flight routes of low-altitude small unmanned aerial vehicles, it is not suitable for general military ground-to-air interception devices, especially in densely populated areas. There are several types such as carrying capture nets and electronic interference. For example, the patent number is CN201921756372.1, and the patent name is a patent for a low-damage capture device for drones. Issues of short interception effective distance, slow capture speed, low reliability and high cost of use

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