Retrievable electric rocket used for intercepting small aircrafts

A return type, electric power technology, applied in the field of aircraft, can solve the problems of high use cost, short effective distance, slow capture speed, etc., and achieve the effect of strong applicability and low use cost

Active Publication Date: 2017-03-15
SOUTH CHINA AGRI UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There are several types of existing small aircraft interception devices, such as ground-launched capture nets, drone-carried capture nets, and

Method used

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  • Retrievable electric rocket used for intercepting small aircrafts
  • Retrievable electric rocket used for intercepting small aircrafts
  • Retrievable electric rocket used for intercepting small aircrafts

Examples

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Embodiment 1

[0025] A returnable electro-powered rocket for intercepting small aircraft, such as figure 1 , figure 2 , image 3 As shown, it includes fairing 1, distance sensor 2, rocket shell 3, wing arm 4, air inlet 5, rocket wing 6, tail rudder motor 7, tail rudder 8, connecting rib 9, image recognizer 10, capture Net 11, high-pressure air chamber 12, electrical control chamber 13, release valve 14, partition 15, first plane joint 16, second plane joint 17, third plane joint 18, pull rod 19, pull plate 20, lead screw 21, Lead screw drive motor 22, motor support 23, secondary thrust motor 24, secondary propeller 25, primary thrust motor 26, primary propeller 27 and return spring 28.

[0026] The external structure of the returnable electric powered rocket is: the top of the cylindrical rocket shell 3 is plugged with a conical fairing 1, and the fairing 1 and the rocket shell 13 are connected by a return spring 28; A distance sensor 2 and an image recognition device 10 are symmetrical...

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Abstract

The invention discloses a retrievable electric rocket used for intercepting small aircrafts. The retrievable electric rocket comprises a fairing, a distance sensor, a rocket shell, wing arms, an air inlet, rocket wings, tail vane motors, tail vanes, a connecting rib, an image recognizer, a capturing net, a high-pressure air cabin, an electric control cabin, a relief valve, a partition plate, a first plane joint, a second plane joint, a third plane joint, pull rods, a pull plate, a lead screw, a lead screw driving motor, a motor support, a second-stage thrust motor, a second-stage propeller, a first-stage thrust motor, a first-stage propeller and a reset spring. The retrievable electric rocket can work independent of fuel, safe to use, capable of automatically searching for, tracking and capturing targets, high in applicability and low in use cost.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a returnable electric power rocket for intercepting small aircraft. Background technique [0002] With the continuous maturity of remote sensing technology, navigation technology and electronic technology, the production cost of small unmanned aerial vehicles has gradually decreased, and its application scope and scale have expanded rapidly. 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. Relevant departments have set up no-fly zones for small unmanned aerial vehicles and gradually introduced relevant management measures. However, there are always incidents of aircraft out of control or malicious intrusion, and small unmanned aerial vehicles need to be captured or intercepted. Due to their small size, low cost, and flexible flight routes, low-altitude small un...

Claims

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Application Information

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IPC IPC(8): F41H11/02F42B12/36F42B15/00F42B15/01
CPCF41H11/02F42B12/36F42B15/00F42B15/01
Inventor 闫国琦
Owner SOUTH CHINA AGRI UNIV
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