Multifunctional unmanned aerial vehicle provided with flexible stamping parafoil

A drone and multi-purpose technology, applied in the direction of motor vehicles, ultra-light aircraft, hang glider, etc., can solve the problems of short flight distance and functional gap, and achieve the effect of large load, various launch methods and small size

Inactive Publication Date: 2013-02-06
武汉南沙工贸有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the flight distance of this remote-controlled power flexible ram parafoil is short, and it can only fly within the visible range. There is still a huge gap

Method used

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  • Multifunctional unmanned aerial vehicle provided with flexible stamping parafoil
  • Multifunctional unmanned aerial vehicle provided with flexible stamping parafoil
  • Multifunctional unmanned aerial vehicle provided with flexible stamping parafoil

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Embodiment Construction

[0037] Embodiments of the present invention will be described below in conjunction with the accompanying drawings.

[0038] figure 1 It is an oblique view of the multi-purpose flexible stamping parafoil UAV in the vehicle state of an embodiment of the present invention, figure 2 It is a structural schematic diagram of a multi-purpose flexible stamping parafoil drone according to an embodiment of the present invention. see figure 1 and figure 2 , the multi-purpose flexible stamping parafoil UAV of the present embodiment comprises: flexible stamping parafoil 1, cabin body 2, propeller 12 and skid type landing gear 15; 2. A control mechanism 13, a modular mission cabin 14 and an engine 11 are installed inside the cabin body 2; the propeller 12 is installed at the tail of the cabin body 2; Equipped with the equipment needed to complete different purposes; the control mechanism 13 includes: GPS navigation system, which guides the drone to fly autonomously and land in the targ...

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Abstract

The invention provides a multifunctional unmanned aerial vehicle provided with a flexible stamping parafoil, which mainly comprises the flexible stamping parafoil (1), a cabin body (2), a propeller (12) and a skid type landing gear (15); the lower part of the flexible stamping parafoil (1) is connected with the cabin cabin (2) through parafoil ropes (10); a control mechanism (13), a modularized mission cabin (14) and an engine (11) are mounted inside the cabin body (2); the propeller (12) is mounted at the tail part of the cabin body (2); the skid type landing gear (15) is mounted at the lower part of the cabin body (2); and equipment required for different purposes is carried in the modularized mission cabin. The multifunctional unmanned aerial vehicle provided with the flexible stamping parafoil has the benefits of safety, reliability, multiple launching manners, long cruise time, wide flying range, small size, light weight, convenience in use, and wide field of use, and is an ideal unmanned aircraft.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to an improved multipurpose flexible ram parafoil unmanned aerial vehicle. Background technique [0002] The wings of traditional drones are all fixed wings. This kind of drone is expensive, relatively small in load, complex in maintenance and use, requires a large number of supporting facilities, and requires long-term professional training for operators. Therefore, the traditional UAVs are generally used for special purposes such as high-altitude military reconnaissance. [0003] In order to adapt to various demands, various aircrafts have been researched and manufactured. Invention patent ZL 93202125.5 (authorized announcement number CN 2204774Y) of the Airborne Forces Research Institute of the Chinese People's Liberation Army discloses a powered flight flexible stamped parafoil, which is used for flight performances, advertising, border patrols and recreational flights ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C31/036B64F1/10
Inventor 郭海军陈勇贺应平马启明田入东祝远程薛富利李琦余刚
Owner 武汉南沙工贸有限公司
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