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A vertical take-off and landing UAV with foldable wings

A technology of vertical take-off and landing and unmanned aerial vehicles, which is applied in the direction of rotorcraft, motor vehicles, aircraft parts, etc., can solve the problems of long running distance, inability to effectively monitor the enemy, and difficulty in finding the runway, etc., to achieve the effect of eliminating the wake vortex

Active Publication Date: 2016-08-17
XIAMEN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

But it is not easy for conventional UAVs to adapt to the rapidly changing requirements of the war environment
[0003] First of all, conventional drones need to have a complete runway to take off, and the running distance is long, so it is difficult to find a suitable runway when fighting in the field
Secondly, conventional drones cannot hover in the air, they can only hover around the target, and cannot effectively monitor the enemy
Finally, when multiple drones fly intensively, the wake vortex of the front plane will affect the rear drones, causing accidents

Method used

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  • A vertical take-off and landing UAV with foldable wings
  • A vertical take-off and landing UAV with foldable wings
  • A vertical take-off and landing UAV with foldable wings

Examples

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Embodiment Construction

[0018] The following embodiments will further illustrate the present invention with reference to the accompanying drawings.

[0019] see Figure 1~4 , the embodiment of the present invention is provided with left wing 1, right wing 2, main wing 3, left wing propeller engine 41, right wing propeller engine 42, main propeller engine 43, left camera 61, right camera 62, main camera 63, left rudder surface 71, right rudder surface 72, main rudder surface 73.

[0020] Described left wing 1 and right wing 2 are connected with main wing 3 respectively, and left wing propeller engine 41 is arranged on the inner side of left wing 1 just above, and right wing propeller engine 42 is located at the inner side of right wing 2 just above. Above, the main propeller engine 43 is located on the inside of the main wing 3 just above; the left camera 61 is located on the outer side of the left wing 1, the right camera 62 is located on the outer side of the right wing 2, and the main camera 63 is...

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Abstract

The invention discloses a vertical take-off and landing unmanned aerial vehicle with foldable aerofoils, and relates to foldable unmanned aerial vehicles. The vertical take-off and landing unmanned aerial vehicle with foldable aerofoils is provided with a left aerofoil, a right aerofoil, a main aerofoil, a left aerofoil propeller engine, a right aerofoil propeller engine, a main propeller engine, a left camera, a right camera, a main camera, a left control plane, a right control plane and a main control plane; the left aerofoil and the right aerofoil are respectively connected with the main aerofoil; the left aerofoil propeller engine is arranged deadly above the inner side of the left aerofoil; the right aerofoil propeller engine is arranged deadly above the inner side of the right aerofoil; the main propeller engine is arranged deadly above the main aerofoil; the left camera is arranged on the outer side edge of the left aerofoil; the right camera is arranged on the right side edge of the right aerofoil; the main camera is arranged on the outer side of the main aerofoil; the left control plane is arranged on the lower part of the left aerofoil; the right control plane is arranged on the lower part of the right aerofoil; the main control surface is arranged on the lower part of the main aerofoil; the left aerofoil, the right aerofoil and two sides of the top of the main aerofoil are respectively provided with support rods.

Description

technical field [0001] The present invention relates to a foldable unmanned aerial vehicle, in particular to a vertical take-off and landing unmanned aerial vehicle with foldable wings, which is particularly suitable for taking off and landing in a harsh environment without a runway in the wild, and at the same time flying in different modes in the air. Background technique [0002] With the development of technology, the role of drone technology in the aviation field, especially the military field, is becoming more and more obvious. Modern warfare requires soldiers to conduct small-unit or even individual combat in harsh environments, and drones, as one of the most effective weapons for obtaining enemy information, play an increasingly important role. However, it is not easy for conventional UAVs to adapt to the rapidly changing requirements of the war environment. [0003] First of all, conventional UAVs need to have a complete runway to take off, and the running distance...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/22B64D47/08
Inventor 朱睿刘锦生傅向向
Owner XIAMEN UNIV