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Inflatable hang glider unmanned aerial vehicle

An inflatable and unmanned aerial vehicle technology, applied in the direction of gliders, unmanned aircraft, wings, etc., can solve the problem of limited storage and transportation space, inability to change orbits quickly, and high rigidity of triangular ribs for hang glider drones problems such as limited storage and transportation space, inability to quickly change orbits, high rigidity, and strong collision energy absorption capacity

Active Publication Date: 2017-06-20
HARBIN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to solve the problem of limited storage and transportation space and inability to quickly change the orbit of the hang gliding UAV, and provides an inflatable hang gliding UAV. The technical solution is as follows:
[0005] The beneficial effects of the present invention are: the inflatable side wings can be quickly inflated and deployed and deflated and retracted during the advancing process of the UAV to realize track change, and can be repeatedly inflated and deployed and deflated and retracted, which solves the storage and transportation space of the gliding wing UAV The problem of limited and inability to quickly change orbits; the inflatable side wings adopt a rigid-flexible combination structure of flexible skin and ribs. The triangular ribs have high rigidity and strong collision energy absorption capacity, which can reduce accidents during operations such as flight, landing and transportation. Damage; The inflatable wing has unique advantages such as ultra-light weight, good folding performance, and low cost, which can provide a new technical approach for the expandable structure or variant structure technology in the aerospace field

Method used

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  • Inflatable hang glider unmanned aerial vehicle
  • Inflatable hang glider unmanned aerial vehicle
  • Inflatable hang glider unmanned aerial vehicle

Examples

Experimental program
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Effect test

specific Embodiment 1

[0016] Embodiment 1, the front end of each rib 2 - 1 is rotationally connected with the fuselage 1 along the opening and closing direction through the rotating shaft 4 .

specific Embodiment 2

[0017] Embodiment 2, the rear end of each rib 2-1 is rotationally connected with the central shaft 3-1 along the opening and closing direction through a hinge 5 .

specific Embodiment 3

[0018] Embodiment 3, the root of the X-shaped telescopic mechanism 3 is rotationally connected with the fuselage 1 along the opening and closing direction through the rotating shaft 4 or the hinge 5 .

[0019] Preferably, the flexible skin 2-2 is made of aramid fiber covered with aluminum foil. Aramid fiber is also called Kevlar, which acts as a force bearing, and the aluminum foil acts as an airtight effect.

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PUM

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Abstract

The invention provides an inflatable hang glider unmanned aerial vehicle and belongs to the technical field of unmanned aerial vehicles. The problems that the hang glider unmanned aerial vehicle storage and transportation space is limited, and rapid orbit transfer cannot be conducted are solved. The inflatable hang glider unmanned aerial vehicle comprises a fuselage and inflatable side wings arranged on the two sides of the fuselage. Each inflatable side wing is composed of a plurality of rib plates which are arranged in a fan-shaped mode and are in sealing connection through flexible skins. The flexible skins and the rib plates are bonded. Every two adjacent rib plates are sealed through the front-surface flexible skin, the back-surface flexible skin, the upper-surface flexible skin and the lower-surface flexible skin to form an air chamber. The width of each rib plate is gradually increased from the front end to the back end. The widths of the front ends of all the rib plates are the same. The widths of the back ends of all the rib plates of each inflatable side wing are gradually increased from the outer sides to the inner sides. Each rib plate adopts a triangular plate of a hollow structure. Air holes are formed in the side walls of the rib plates on the two sides of each air chamber. The front end of each rib plate is connected with a high-pressure gas cylinder and an inflating control system which are arranged in the fuselage. An exhaust electromagnetic valve is arranged at the back end of each air chamber.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to an inflatable gliding wing unmanned aerial vehicle. Background technique [0002] UAVs have obvious advantages such as no risk of casualties. With the rapid development of UAV technology, glider UAVs have been widely used; The space is not conducive to storage and transportation; and when the glider UAV encounters natural enemies such as birds, it cannot quickly change orbit to avoid it, and the safety hazard is relatively large; This program. Contents of the invention [0003] The purpose of the present invention is to solve the problem of limited storage and transportation space and inability to quickly change the orbit of the hang gliding UAV, and provides an inflatable hang gliding UAV. The technical solution is as follows: [0004] An inflatable hang gliding drone, which includes a fuselage and inflatable wings arranged on both sides of the f...

Claims

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Application Information

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IPC IPC(8): B64C3/30B64C31/02
CPCB64C3/30B64C31/02B64U10/00
Inventor 卫剑征谭惠丰甄铎
Owner HARBIN INST OF TECH
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