A stable multi-axis drone

A drone and stable technology, applied in the field of drones, can solve the problems of drones, such as large size, inconvenient packaging and transportation, and easy damage during transportation, and achieve the effect of easy folding and opening, convenient packaging, and avoiding damage

Active Publication Date: 2018-05-25
GUANGZHOU REDBIRD HELICOPTER REMOTE SENSING TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the technical problems of large volume, inconvenient packaging and transportation, and easy damage during transportation, and provide a foldable, stable multi-axis UAV with high reliability.

Method used

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  • A stable multi-axis drone
  • A stable multi-axis drone
  • A stable multi-axis drone

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Embodiment Construction

[0057] The preferred embodiments of the present invention will be described below in conjunction with the accompanying drawings. It should be understood that the preferred embodiments described here are only used to illustrate and explain the present invention, and are not intended to limit the present invention.

[0058] Such as Figure 1 to Figure 12 As shown, the stable multi-axis UAV of the present invention includes a fuselage, and the fuselage is provided with six arms 1, and the six arms 1 are arranged symmetrically about the fuselage. In this embodiment, the fuselage is It is circular, and the six machine arms 1 are evenly distributed on the circumference of the fuselage, but the fuselage in the present invention is not limited to circular, and can also be other polygons. The end of the arm 1 far away from the fuselage is provided with a drive motor through a motor mount 11 , and a blade is provided on a rotating shaft of the drive motor.

[0059] Such as Figure 5 A...

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Abstract

The invention discloses a stable multi-axis unmanned aerial vehicle, comprising a fuselage, on which several arms are arranged; a drive motor is arranged at the end of the arm far away from the fuselage, and the rotating shaft of the drive motor is Blades are arranged on the top; the machine arm is connected to the fuselage through a connecting mechanism; the connecting mechanism includes a machine arm connecting seat and a machine arm folding seat, and one end of the machine arm folding seat is hinged to the machine arm to connect on the seat; the arm connecting seat is provided with a folding mechanism; the folding mechanism is movably connected with the other end of the folding seat of the arm; the folding mechanism includes an outer handle and an inner handle; one end of the inner handle is hinged on The other end of the connecting seat of the machine arm is movably provided with an outer handle rotating shaft; one end of the outer handle is hinged on the rotating shaft of the outer handle; part; the inner handle is also provided with a locking mechanism for locking the inner handle.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a stable multi-axis unmanned aerial vehicle. Background technique [0002] Unmanned aerial vehicle (unmanned aircraft), which has the advantages of flexible maneuverability, quick response, unmanned flight, and low operation requirements. It is loaded with multiple types of sensors, such as cameras, to realize real-time image transmission. Gaocheng area Detection and other functions are widely used in firefighting, military, transportation, police, exploration and meteorological fields to achieve cruise shooting and monitoring of designated areas. [0003] At present, most UAVs are multi-axis UAVs, such as four-axis, six-axis, etc., because the arm is set radially outward relative to the fuselage, the volume is large, and the transportation is inconvenient. At the same time, the structure of the arm may be damaged during transportation. During the co...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/30B64C27/08B64C25/10B64D47/00
CPCB64C1/30B64C25/10B64C27/08B64D47/00B64U2101/00
Inventor 徐鹏
Owner GUANGZHOU REDBIRD HELICOPTER REMOTE SENSING TECH
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