Portable foldable unmanned aerial vehicle

An unmanned aerial vehicle and portable technology, applied in the field of unmanned aerial vehicles, can solve the problems of unsuitable long-distance, long-term reconnaissance, unfavorable daily use, poor endurance, etc., and achieve good penetration ability, good flight performance, and low resistance. Effect

Active Publication Date: 2017-05-31
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the prior art, the fixed-wing aircraft has excellent performance, long range, and long battery life, but due to its huge size, it is not easy to carry and is not conducive to daily use; for multi-axis aircraft, although it is easy to carry, it has a small range and poor battery life. distance, long reconnaissance is still not suitable

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  • Portable foldable unmanned aerial vehicle
  • Portable foldable unmanned aerial vehicle
  • Portable foldable unmanned aerial vehicle

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Embodiment Construction

[0026] In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. Hereinafter, embodiments of the present invention will be described in detail, examples of which are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0027] Those skilled in the art can understand that, unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. It should als...

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Abstract

The embodiment of the invention discloses a portable foldable unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles. The portable foldable unmanned aerial vehicle comprises lifting wing flaps 1, ailerons 2, an engine 3, rib folding hinges 4, a wing 5, a wing 6, a wing 7, a wing 8, a wing 9, a wing 10, an equipment cabin 11, an equipment cabin 12, back beams 13, wing ribs 14, front beams 15, beam folding fixing bolts 16, an airbag cabin 17, an airbag skin 18 and a skin 26. The portable foldable unmanned aerial vehicle disclosed by the embodiment of the invention is put into backpacks in a folded manner to be convenient to carry; therefore, the portability of the portable foldable unmanned aerial vehicle is sufficiently represented. Meanwhile, through adoption of the aerodynamic layout of flying wings, the portable foldable unmanned aerial vehicle has the advantages of large lift-drag ratio, high structural strength, small resistance, convenient carrying, short takeoff time and simple structure.

Description

technical field [0001] The present invention relates to the technical field of unmanned aerial vehicles, in particular, to a portable and foldable unmanned aerial vehicle. Background technique [0002] Along with the continuous demand of people to reconnaissance equipment, how to bring a kind of portable fixed-wing aircraft into people's daily work is a technical problem to be solved. There are roughly two types of aircraft in daily life: fixed-wing aircraft and axial aircraft. In the prior art, the fixed-wing aircraft has excellent performance, long range and long battery life, but due to its huge size, it is not easy to carry and is not conducive to daily use; for multi-axis aircraft, although it is easy to carry, it has a small range and poor battery life. Distance, long reconnaissance is still not suitable. Contents of the invention [0003] The embodiments of the present invention give full play to the portability of the multi-rotor aircraft and the good flight perf...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/30
CPCB64C1/30B64U2101/00
Inventor 王宇邢宇刘东伟余雄庆
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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