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Dual-mode unmanned aerial vehicle working method and dual-mode unmanned aerial vehicle

A working method and technology of unmanned aerial vehicles, which are applied in the directions of unmanned aerial vehicles, motor vehicles, wing adjustment, etc., can solve the problem that fixed-wing unmanned aerial vehicles have high lifting and lowering site requirements, short flight time and short flight distance. and other problems, to achieve the effect of improving wind resistance and maneuverability, reducing energy consumption and prolonging flight time

Inactive Publication Date: 2019-04-09
CHENGDU AOCTER TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The above-mentioned unmanned aerial vehicles have been widely used, but each has some shortcomings; fixed-wing unmanned aerial vehicles have relatively high requirements for landing sites, especially high requirements for landing sites, which are prone to landing and breaking, and are greatly affected by wind direction during flight. ; During the flight process of the helicopter propeller UAV, it needs to rely on the lifting of the propeller to keep it in the air, so its flight time is short and the flight distance is relatively short

Method used

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  • Dual-mode unmanned aerial vehicle working method and dual-mode unmanned aerial vehicle
  • Dual-mode unmanned aerial vehicle working method and dual-mode unmanned aerial vehicle
  • Dual-mode unmanned aerial vehicle working method and dual-mode unmanned aerial vehicle

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Embodiment Construction

[0050] Embodiment of the present invention is described below with accompanying drawing as example:

[0051] exist Figure 1 to Figure 7 middle:

[0052] 1 is the folding main wing; 2 is the dual-mode UAV fuselage, which is equipped with a propeller direction adjustment servo motor; 3 is a propeller direction regulator, which is also equipped with a propeller driving motor or an internal combustion engine; 4 is a propeller limiter; 5 is a Foldable propeller; 6 is the propeller installation hole and installation shaft; 7 is the propeller drive shaft; 8 is the folding main wing installation hole or the folding main wing installation shaft; 9 is the U-shaped shell of the folding main wing or the U-shaped folding main wing at the outermost layer Structural layer; 10 is the rib plate or U-shaped structure layer of the folded main wing; 11 is the flexible material layer of the folded main wing; 12 is the innermost rib plate or the innermost U-shaped structure layer or the flat O-sh...

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Abstract

The invention discloses a dual-mode unmanned aerial vehicle working method and a dual-mode unmanned aerial vehicle. The two-mode unmanned aerial vehicle is mainly composed of an unmanned aerial vehicle body, propellers, folding main wings, a folding tail wing and a shock absorbing frame. According to the dual-mode unmanned aerial vehicle working method, the dual-mode unmanned aerial vehicle can realize vertical lifting and lowering, horizontal driving flight or horizontal gliding flight, and has the characteristics that the dual-mode unmanned aerial vehicle is easy to lift and lower, is less affected by wind direction and has long flight time and long flight distance.

Description

technical field [0001] The invention relates to a dual-mode unmanned aerial vehicle working method and a dual-mode unmanned aerial vehicle, which belong to the field of unmanned aerial vehicle technology or leisure sports equipment. Background technique [0002] Among the existing UAV technology solutions, there are mainly the following categories: [0003] 1. Fixed-wing UAV; [0004] 2. Helicopter UAV; [0005] The above-mentioned unmanned aerial vehicles have been widely used, but each has some shortcomings; fixed-wing unmanned aerial vehicles have relatively high requirements for landing sites, especially high requirements for landing sites, which are prone to landing and breaking, and are greatly affected by wind direction during flight. ; During the flight process of the helicopter propeller UAV, it needs to rely on the lifting of the propeller to keep it in the air, so its flight time is short and the flight distance is relatively short. Contents of the invention ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/56B64C29/00
CPCB64C3/56B64C29/0025B64U10/25B64U50/19B64U70/80B64U30/12B64U30/20B64U2201/20B64U50/13
Inventor 耿直
Owner CHENGDU AOCTER TECH CO LTD
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