Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Military unmanned aerial vehicle with portable united wings

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, and poor penetration capabilities, achieving good flight performance and penetration capabilities, Easy to carry and low trim resistance

Inactive Publication Date: 2016-04-06
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
View PDF6 Cites 7 Cited by
  • 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

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Military unmanned aerial vehicle with portable united wings
  • Military unmanned aerial vehicle with portable united wings
  • Military unmanned aerial vehicle with portable united wings

Examples

Experimental program
Comparison scheme
Effect test

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...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention relates to an unmanned aerial vehicle, in particular to a military unmanned aerial vehicle with portable united wings. According to the military unmanned aerial vehicle with portable united wings, a wing stiffener and a sliding block are arranged on a fuselage, a propeller is arranged at the tail end of the fuselage, and a vertical tail is arranged at the tail end of the fuselage; one end of the front wing is hinged to the wing stiffener, and the other end of the front wing is hinged to one end of a rear wing; the other end of the rear wing is hinged to the sliding block; the sliding block slides along the tail end of the fuselage to one side close to the wing stiffener, so that the wings are driven to be close to the fuselage; the vertical tail is hinged to the fuselage, and can be levelly put at the tail end of the fuselage or perpendicular to tail end of the fuselage. According to the military unmanned aerial vehicle with portable united wings provided by the invention, the portability of a multiple-spindle aircraft and favorable flight performance of a fixed wing aircraft are fully used. The unmanned aerial vehicle is put in a knapsack after being folded, so that the unmanned aerial vehicle is convenient to carry, and the portability that the unmanned aerial vehicle is easy to carry is fully reflected. Before flight, the unmanned aerial vehicle is taken out from the knapsack, the unmanned aerial vehicle is thrown manually to fly, and in the manual throwing process, the wings and the vertical tails are ejected to be in the flight state, and land in the sliding manner.

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

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(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
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products