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An easy-to-lift UAV

An unmanned aerial vehicle, a convenient technology, applied in vertical take-off and landing aircraft, unmanned aerial vehicles, gyrocopters, etc., can solve problems such as inflexible lifting, and achieve the effects of good structural stability, energy saving, and structural stability

Active Publication Date: 2018-08-03
广州三飞航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, the drones currently used in various aspects require relatively harsh terrain, and the lifting is very inflexible.

Method used

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  • An easy-to-lift UAV
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  • An easy-to-lift UAV

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0029] Such as Figure 1-5 As shown, a kind of easy-to-lift unmanned aerial vehicle includes a fixed-wing unmanned aerial vehicle body 1 and a vertical lift wing 2. The fixed-wing unmanned aerial vehicle body 1 is provided with a first mortise 3, and the fixed-wing unmanned aerial vehicle The machine body 1 is provided with three inclined mounting holes 4 whose ends communicate with each other. The inclined mounting holes 4 are connected with insertion openings 5, and the insertion openings 5 ​​are distributed in a triangular shape. The vertical elevating wing 2 includes connecting pipes 6 , elbow 7, motor 8, electric adjustment 9 and lifting propeller 10, the connecting pipe 6 is provided with a first tenon 11 matching with the first mortise 3 and a shape memory alloy strip matching with the inclined mounting hole 4 12. By setting the vertical lift 2, the fixed-wing UAV body 1 can take off and land vertically. Compared with the traditional UAV, it is flexible in lifting and l...

Embodiment 2

[0032] Such as Figure 1-9As shown, a kind of easy-to-lift unmanned aerial vehicle includes a fixed-wing unmanned aerial vehicle body 1 and a vertical lift wing 2. The fixed-wing unmanned aerial vehicle body 1 is provided with a first mortise 3, and the fixed-wing unmanned aerial vehicle The machine body 1 is provided with three inclined mounting holes 4 whose ends communicate with each other. The inclined mounting holes 4 are connected with insertion openings 5, and the insertion openings 5 ​​are distributed in a triangular shape. The vertical elevating wing 2 includes connecting pipes 6 , elbow 7, motor 8, electric adjustment 9 and lifting propeller 10, the connecting pipe 6 is provided with a first tenon 11 matching with the first mortise 3 and a shape memory alloy strip matching with the inclined mounting hole 4 12. The fixed-wing UAV body 1 includes a fuselage 13, wings 14, empennage 15, a power system, a control system, and a battery. The power system consists of a brush...

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PUM

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Abstract

The invention discloses a convenient lifting UAV, which includes a fixed-wing UAV body and a vertical lift wing. The fixed-wing UAV body is provided with a first mortise, and the fixed-wing UAV body is provided with a first mortise. There are three inclined mounting holes connected to each other at the ends, and the inclined mounting holes are connected with insertion openings, and the insertion openings are distributed in a triangular shape. The vertical lifting wing includes connecting pipes, elbows, motors, electric regulators and lifting propellers. The connecting pipe is provided with a first mortise that matches the first mortise and a shape memory alloy strip that matches the inclined mounting hole; the easy-to-lift UAV is less affected by the terrain when it goes up and down.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle with convenient lifting. Background technique [0002] Unmanned aircraft, referred to as "UAV", is the use of radio An unmanned aircraft operated by remote control equipment and self-contained program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote control with a parachute or a block. Can be used repeatedly. ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/22B64C27/08B64C29/02
CPCB64C27/08B64C27/24B64C29/02B64U10/25B64U70/80B64U30/20
Inventor 何智杰
Owner 广州三飞航空科技有限公司
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