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UAV (Unmanned Aerial Vehicle) arm folding mechanism

A technology of folding mechanism and unmanned aerial vehicle, applied in the direction of fuselage, aircraft parts, aircraft control, etc., can solve the problems of poor stability, short life, inconvenient operation, etc., to increase stability, prolong service life, and eliminate gaps. Effect

Inactive Publication Date: 2016-06-22
郭根松
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to overcome the technical defects of inconvenient operation, poor stability, and short life of the above-mentioned arm folding mechanism, the present invention provides an unmanned aerial vehicle arm folding mechanism that is convenient to fold, stable to open and fixed, and good in stability.

Method used

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  • UAV (Unmanned Aerial Vehicle) arm folding mechanism
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  • UAV (Unmanned Aerial Vehicle) arm folding mechanism

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Embodiment Construction

[0028] 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.

[0029] like Figure 1 ~ Figure 4 As shown, the drone arm folding mechanism of the present invention includes the arm folding seat 12 and the arm connecting seat 17 arranged on the machine arm 1. The fuselage mounting lug 172 connected with the second mounting plate 21, its side opposite to the machine arm 1 and at the position of the second mounting plate 21 protrudes from the machine arm mounting lug 173, and the machine arm connecting seat 17 is A protrusion protrudes upwards from the surface, and a through hole 174 is formed on the protrusion. One end of the arm connecting seat 17 close to the through hole 174 protrudes toward the first mounting plate 2 with a po...

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Abstract

The invention discloses a UAV (Unmanned Aerial Vehicle) arm folding mechanism. The UAV arm folding mechanism comprises a UAV arm connection base and a UAV arm folding base arranged on a UAV arm, wherein one end of the UAV arm folding base is hinged to the UAV arm connection base; a folding mechanism is arranged on the UAV arm connection base; the folding mechanism is movably connected with the other end of the UAV arm folding base; the folding mechanism comprises an outer handle and an inner handle; one end of the inner handle is hinged to the UAV arm connection base; the other end of the inner handle is provided with an outer handle rotation shaft in a sleeved manner; one end of the outer handle is hinged to the outer handle rotation shaft; the other end of the outer handle is provided with a connection part which is movably connected with the UAV arm folding base; and the inner handle is further provided with a locking structure for locking the inner handle. The UAV arm folding mechanism is convenient for operation; double-locking is realized; and furthermore, an elastic component is arranged between the two metal components, so that a clearance between the metal components is eliminated; the stability is improved; and the service life is prolonged.

Description

technical field [0001] The invention belongs to the technical field of arm folding mechanisms, and in particular relates to an arm folding mechanism of an 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. 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 Applications(China)
IPC IPC(8): B64C1/30
CPCB64C1/30
Inventor 郭根松
Owner 郭根松
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