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Portable Linked Wing Military Unmanned Aerial Vehicle

A technology of unmanned aerial vehicles and joint wings, which is applied in the field of unmanned aerial vehicles, can solve the problems of inappropriate long-distance reconnaissance and strike, lack of individual equipment, poor penetration capabilities, etc., to achieve good flight performance and penetration capabilities, Easy to carry and low trim resistance

Inactive Publication Date: 2017-09-29
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although the existing fixed-wing aircraft have excellent performance, long range, and strong penetration capabilities, they do not have the requirements for individual equipment due to their huge size; for multi-axis aircraft, although they are easy to carry, most of them have low speed and poor penetration capabilities. , the voyage is small, it is not suitable for long-distance reconnaissance and strike, so it is still not suitable as an individual reconnaissance / strike equipment

Method used

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  • Portable Linked Wing Military Unmanned Aerial Vehicle
  • Portable Linked Wing Military Unmanned Aerial Vehicle
  • Portable Linked Wing Military Unmanned Aerial Vehicle

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Embodiment Construction

[0027] In order to make the purpose and technical solutions of the embodiments of the present invention more clear, the technical solutions of the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings of the embodiments of the present invention. Apparently, the described embodiments are some, not all, embodiments of the present invention. Based on the described embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative work all belong to the protection scope of the present invention:

[0028] figure 1 Shown: It shows the aircraft view of the portable joint-wing military unmanned aerial vehicle when it is flying in the air. This flight state has the advantages of large lift-to-drag ratio, high structural strength, and small trim resistance.

[0029] figure 2 As shown, it shows the aircraft view of the portable joint-wing military unmanned aerial v...

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Abstract

The invention relates to an unmanned aerial vehicle, in particular to a portable joint-wing military unmanned aerial vehicle. The fuselage of the portable joint-wing military unmanned aerial vehicle is provided with a wing reinforcement and a slider; Hinged, the other end of the front wing of the wing is hinged with one end of the rear wing; the other end of the rear wing is hinged with the slider; the slider slides along the rear end of the fuselage to the side close to the wing reinforcement, thereby driving the wing toward the aircraft The body is close to; the vertical tail is hinged with the fuselage, and the vertical tail can be placed on the tail end of the fuselage or vertically stand on the tail end of the fuselage. The portable joint-wing military unmanned aerial vehicle provided by the invention can give full play to the portability of the multi-axis aircraft and the good flight performance of the fixed-wing aircraft. The aircraft can be folded into a backpack for easy carrying, which fully reflects the portability of being easy to carry. Take it out of the backpack before flying, and take off by hand throwing. During the hand throwing process, the wings and vertical tail pop up to the flying state, and land in the form of taxiing.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle, in particular to a portable joint-wing military unmanned aerial vehicle. Background technique [0002] With the progress of modern warfare, special forces are increasingly playing an increasingly important role, and how to integrate fixed-wing aircraft into the individual equipment of special forces is the original intention of the present invention. Considering that special forces sometimes go deep behind enemy lines alone, they need to conduct reconnaissance and identification within a few kilometers of the surrounding area, or carry out some blasting tasks in unfamiliar areas. Although the existing fixed-wing aircraft have excellent performance, long range, and strong penetration capabilities, they do not have the requirements for individual equipment due to their huge size; for multi-axis aircraft, although they are easy to carry, most of them have low speed and poor penetration capabilities. , ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C3/56
CPCB64C3/56B64U10/25B64U30/12
Inventor 邢宇徐相荣谷长河周士杰屠强祝雯生苟能亮
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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