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Intelligent flexible inflatable wing unmanned aerial vehicle structure

An intelligent flexible and inflatable technology, applied in the direction of wings, wing adjustment, fuselage, etc., can solve the problems of poor flexibility, low energy reserve, high loading and transportation requirements, and achieve the effect of convenient storage

Active Publication Date: 2019-10-25
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The wings of traditional fixed-wing UAVs are bulky, large in size, complex in structure, high in loading and transportation requirements, poor in concealment performance, poor in flexibility, low in energy reserves, high in energy consumption, small in flight radius, short in cruise time, low in efficiency, and reliable poor sex
In the face of ever-changing and diverse battlefield environments in modern warfare, UAVs have poor adaptability, especially in special combat environments such as jungle operations, canyon operations, and other special areas.

Method used

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  • Intelligent flexible inflatable wing unmanned aerial vehicle structure
  • Intelligent flexible inflatable wing unmanned aerial vehicle structure
  • Intelligent flexible inflatable wing unmanned aerial vehicle structure

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Embodiment Construction

[0041] The present invention will be further described in detail below in conjunction with the accompanying drawings.

[0042] An intelligent flexible inflatable wing UAV structure proposed by the present invention, combined with the accompanying drawings below Figure 1 to Figure 6 And examples, the specific embodiment of the present invention is described further.

[0043] see figure 1 , an intelligent flexible inflatable wing UAV structure proposed by the present invention, comprising: intelligent flexible inflatable wing (1), internal braces (11), flexible film airfoil (12), propeller (2), Body (3), landing gear (4), support bar (41), pulley (42), protective cover (5), empennage (6), horizontal empennage (61), vertical empennage (62), empennage rudder surface (63 ), high-pressure gas cylinders (7), air pressure valves (71), gas pipes (72), missiles and other weapons (8), other general components (9), power supplies (91), flight control boards (92), motors (93 ), cable ...

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Abstract

The invention provides an intelligent flexible inflatable wing unmanned aerial vehicle structure, which comprises intelligent flexible inflatable wings, a propeller, a body, a landing gear, a protective cover, an empennage, a high-pressure gas storage bottle, a missile weapon, other universal parts (9) and the like. The intelligent flexible inflatable wing unmanned aerial vehicle structure can befoldable and is small in size, light in weight, simple in structure, low in energy consumption, long in cruising time and higher in rapid maneuverability and anti-interference characteristic; the flexible inflatable wings can be quickly unfolded under a high-pressure inflation condition; the defects of a fixed-wing unmanned aerial vehicle are greatly made up under a condition that the requirementsfor the usability of the unmanned aerial vehicle are met, and the performance of the intelligent unmanned aerial vehicle is well exerted; the minimization of unmanned aerial vehicle is realized, thestorage, carrying and transportation are facilitated, and various functional advantages such as rapid reconnaissance, observation, emergency communication, disaster situation monitoring, rescue, intelligence gathering, fast enemy response and fight and the like of the unmanned aerial vehicle on a target area can be realized.

Description

technical field [0001] The invention relates to the technical field of flexible inflatable aircraft, in particular to an intelligent flexible inflatable wing UAV structure. The structure of the flexible inflatable UAV is relatively simple, and the folded state is small in size, which is convenient for storage, transportation and maintenance. The flexible inflatable and deployable wings enable UAVs to be carried by individual soldiers and transported in small vehicles, providing more possibilities for the application scenarios of smart UAVs. Background technique [0002] The rapid development of unmanned aerial vehicles in today's world, the impact on a country and an army cannot be ignored. For unmanned aerial vehicles, it must meet the requirements of precise combat and achieve the effect of concealed combat. The wings of traditional fixed-wing UAVs are bulky, large in size, complex in structure, high in loading and transportation requirements, poor in concealment performa...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/30B64C3/56B64C1/00
CPCB64C1/0009B64C3/30B64C3/56B64C2001/0063
Inventor 刘龙斌勇良江振宇许秋平龚明书
Owner NAT UNIV OF DEFENSE TECH
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