Novel unmanned aerial vehicle

A kind of unmanned aerial vehicle, a new type of technology, applied in the field of unmanned aerial vehicles, can solve problems such as propeller failure, high flatness requirements, affecting flight, etc., to achieve the effect of ensuring normal use, improving stability, and ensuring stability

Pending Publication Date: 2019-08-23
FUYANG NORMAL UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Aiming at the deficiencies in the prior art, the present invention provides a new type of unmanned aerial vehicle, which has the advantages of taking off on a slope, etc., and solves the problem that the existing four-rotor UAV is not perfect enough for taking off on a slope. When taking off, the flatness of the ground is very high, and it cannot take off on a slope, so that the drone cannot adapt to various terrains in time, which brings inconvenience to the control of the drone and increases the preparation time for takeoff. At the same time, the traditional When the quadrotor drone is flying, because the quadrotor drone uses the rotation of the propeller to ensure the lift of the aircraft, when the quadrotor drone comes into contact with objects during flight, it is easy to cause the propeller to malfunction and affect the flight. The problem

Method used

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Embodiment Construction

[0021] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.

[0022] See Figure 1-3 , A new type of drone, including body 1, bladeless fan 2, mounting block 3, support rod 4, connecting block 5, electric push rod 6, rotating shaft 7, sliding block 8, sliding groove 9, stabilizer bar 10, buffer The spring 11, the stabilizing plate 12 and the anti-skid block 13, the outer wall of the body 1 is fixedly installed with a bladeless fan 2. The bladeless fan 2 is also called an air multiplier, which can p...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles, and discloses a novel unmanned aerial vehicle. The novel unmanned aerial vehicle comprises a fuselage, bladeless fans, mounting blocks, supporting rods, connecting blocks, electric push rods, rotating shafts, sliding blocks, sliding grooves, stabilization rods, buffer springs, stabilization plates and antiskid blocks. The bladeless fans are fixedly mounted on the outer wall of the fuselage. The mounting blocks are fixedly mounted at the bottom of the fuselage. The supporting rods are movably connected to the bottoms of the mounting blocks. The connecting blocks are fixedly mounted at the tops of the supporting rods. The electric push rods movably connected with the connecting blocks are fixedly mounted at the bottomsof the mounting blocks. According to the novel unmanned aerial vehicle, propellers of a traditional four-rotor unmanned aerial vehicle are changed into the bladeless fans, and therefore the stabilityof the unmanned aerial vehicle during flying is guaranteed better; even though the unmanned aerial vehicle collides with an object, the problem of traditional propeller damage cannot be generated; and the maintenance cost is reduced, normal use of the unmanned aerial vehicle is guaranteed better, and the stability of the unmanned aerial vehicle during flying is improved.

Description

Technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a new type of unmanned aerial vehicle. Background technique [0002] Unmanned aircraft is abbreviated as unmanned aerial vehicle. It is an unmanned aircraft that uses radio remote control equipment and self-provided program control devices, or is completely or intermittently operated by an onboard computer. Quadrotors can take off and land vertically, Hovering freely, and the fuselage is light and easy to control, it can adapt to various speeds and flight conditions of various flight profiles. These advantages determine that it is a high-tech equipment for both military and civilian use. [0003] The existing quad-rotor drones are not perfect for take-off on slopes. Traditional quad-rotor drones require very high ground flatness during take-off and cannot take off on slopes. As a result, the drone cannot respond to the Adaptation to this kind of terrain brings inconven...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02
CPCB64C39/02
Inventor 唐义甲张正豪赵发勇
Owner FUYANG NORMAL UNIVERSITY
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