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Portable multitask rotor individual combat unmanned aerial vehicle

A single-soldier, multi-task technology, applied in the field of unmanned aerial vehicles, can solve problems affecting the flight safety of rotor-wing single-soldier combat unmanned aerial vehicles, bird collisions, unmanned aerial vehicle collisions, etc., to improve safety, prevent damage, reduce The effect of resistance

Inactive Publication Date: 2019-09-06
杭州木书科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the existing problem in the prior art that during the flight of individual combat UAVs, the propellers are prone to collide with flying birds during the rotation process, and then the flying birds will be rolled into the propellers, which affects the The flight of the rotor single-soldier combat UAV is safe, but its outriggers cannot buffer it when it lands, which will cause a large collision between the UAV and the ground. A convenient multi-task rotor single-soldier combat drone

Method used

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  • Portable multitask rotor individual combat unmanned aerial vehicle
  • Portable multitask rotor individual combat unmanned aerial vehicle
  • Portable multitask rotor individual combat unmanned aerial vehicle

Examples

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Embodiment 1

[0029] refer to Figure 1-6, a portable multi-task rotor single-soldier combat UAV, including a fuselage 1 and a radar, the radar is fixedly installed on the fuselage 1, the radar is electrically connected to a receiving module, the receiving module is electrically connected to a single-chip microcomputer, and the single-chip electromechanical The strike module is connected, and the single-chip electromechanical connection is connected with the launch module. The top of the fuselage 1 is fixedly installed with two drive motors 2 arranged symmetrically. The output shaft of the drive motor 2 is welded with a propeller 3. The top of the fuselage 1 is detachable and fixed. Two protective nets 4 arranged symmetrically are installed, and the two propellers 3 are respectively located in the two protective nets 4, a riser 5 is fixedly installed on the middle position of the top of the fuselage 1, and a drainage plate is fixedly installed on the top of the riser 5 6. The bottom of the ...

Embodiment 2

[0038] refer to Figure 1-6 , a portable multi-tasking rotor single-soldier combat UAV, including a fuselage 1 and a radar, the radar is fixedly mounted on the fuselage 1 by screws, the radar is electrically connected to a receiving module, the receiving module is electrically connected to a single-chip microcomputer, and the single-chip microcomputer The strike module is electrically connected, and the single-chip motor is electrically connected to the launch module. The top of the fuselage 1 is fixed with two symmetrical drive motors 2 by screws, and the output shaft of the drive motor 2 is welded with a propeller 3. The top is detachable and fixed with two protective nets 4 arranged symmetrically by screws, and the two propellers 3 are respectively located in the two protective nets 4, and the middle position of the top of the fuselage 1 is fixed with a vertical plate 5 by screws. The top of 5 is fixed with a drainage plate 6 by screws, and the bottom of the fuselage 1 is f...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicles and in particular relates to a portable multitask rotor individual combat unmanned aerial vehicle. For problems that a propeller of an existing individual combat unmanned aerial vehicle is very easily to collide with a flying bird in the rotating process in the flying process of the existing individual combat unmanned aerialvehicle to affect the flying safety of the rotor individual combat unmanned aerial vehicle and outriggers of the existing individual combat unmanned aerial vehicle cannot buffer during landing, the following scheme is provided; the portable multitask rotor individual combat unmanned aerial vehicle comprises an unmanned aerial vehicle body and a radar; the radar is fixedly mounted on the unmanned aerial vehicle body; a receiving module is electrically connected to the radar; a single chip microcomputer is electrically connected to the receiving module; and an attacking module is electrically connected with the single chip microcomputer. According to the portable multitask rotor individual combat unmanned aerial vehicle, the unmanned aerial vehicle body can perform investigation and attacking on surrounding environments; and meanwhile, in the rotating process of the propeller, a protective net can prevent the propeller from colliding with the flying bird so that the flying safety of theunmanned aerial vehicle body is enhanced; and during landing, the outriggers can prevent the unmanned aerial vehicle body from suffering larger collision with the ground to be damaged during landing.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a portable multi-task rotor single-soldier combat unmanned aerial vehicle. Background technique [0002] An unmanned aircraft is an unmanned aircraft operated by radio remote control equipment and its own program control device. UAV is actually a general term for unmanned aerial vehicles. From a technical point of view, it can be divided into: unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paraglider etc. Compared with manned aircraft, it has the advantages of small size, low cost, convenient use, low requirements for combat environment, and strong battlefield survivability. Since unmanned aircraft is of great significance to future air combat, all major military countries in the world are stepping up the development of unmanned aircraft. [0003] Dur...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/62B64D45/00
CPCB64C25/62B64D45/00B64U2101/15B64U10/10
Inventor 拓守廷徐志勇
Owner 杭州木书科技有限公司
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