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Electric rocket device

A rocket and electric technology, applied in defensive devices, offensive equipment, etc., can solve the problems of short interception effective distance, out-of-control aircraft, malicious intrusion, etc., to improve the capture accuracy, improve the moving speed, and avoid misoperation.

Pending Publication Date: 2020-11-27
中科星控(天津)信息技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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

Method used

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Embodiment Construction

[0030] The present invention is specifically described below in conjunction with accompanying drawing, as Figure 1-12 As shown, an electric rocket device includes a cylindrical casing 1, the lower end of the cylindrical casing 1 is provided with an electric drive mechanism, the upper end of the cylindrical casing 1 is provided with an automatic opening mechanism, and one side of the automatic opening mechanism is provided with a linkage trigger mechanism;

[0031]The electric drive mechanism includes air inlets 2 on both sides of the cylindrical shell 1, an S-shaped air passage 3 is installed on one side of the air inlet 2, a sealed bearing-4 is installed on the lower end of the S-shaped air passage 3, and a sealed bearing-4 is installed on the outer ring of the sealed bearing-4. Rotating ring 5, sealed bearing 2 6 is installed on the lower end side surface of rotating ring 5, straight air channel 7 is installed on the inner ring of sealed bearing 2 6, the lower end of straigh...

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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...

Claims

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Application Information

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IPC IPC(8): F41H11/04
CPCF41H11/04
Inventor 李洁栗洁
Owner 中科星控(天津)信息技术有限公司
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