Unlock instant, AI-driven research and patent intelligence for your innovation.

Quick assembly structure of unmanned aerial vehicle rotor and unmanned aerial vehicle

An unmanned aerial vehicle and rotor technology, which is applied in the directions of aircraft, rotorcraft, transportation and packaging, can solve the problems of troublesome installation or disassembly, and cannot realize the installation and disassembly and replacement of unmanned aerial vehicle rotors. Mobility, simple structure effect

Inactive Publication Date: 2016-08-24
FOSHAN AIRCAM UAV TECH CORP
View PDF1 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In some fields such as firefighting and emergency handling, unmanned aerial vehicles are required to be easy to carry and quickly deployed, and even required to perform tasks in the dark, so the mechanism of unmanned aerial vehicles is required to adopt a quick-loading structure in order to reduce the transportation volume and flight preparation time , but in the prior art, the rotor of the unmanned aerial vehicle is usually connected with the rotating shaft of the rotor motor by means of threaded connection, so the installation or disassembly is more troublesome, and the purpose of fast loading, unloading and replacement of the unmanned aerial vehicle rotor cannot be achieved

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Quick assembly structure of unmanned aerial vehicle rotor and unmanned aerial vehicle
  • Quick assembly structure of unmanned aerial vehicle rotor and unmanned aerial vehicle
  • Quick assembly structure of unmanned aerial vehicle rotor and unmanned aerial vehicle

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0029] like figure 1 Shown is the exploded view of the unmanned aircraft rotor quick-loading structure of the present invention, as can be seen from the figure, the unmanned aircraft rotor quick-installation structure of the present invention comprises: the mount 2 that is fixedly connected to the unmanned aircraft rotor 1; A connection assembly for a human aircraft motor; wherein, the connection assembly has a concave or protruding first lock; wherein, the mounting seat has a protruding or concave second lock that matches the connection assembly; wherein, by inserting the first The locking piece is locked with the second locking piece, and the unmanned aerial vehicle rotor and the unmanned aerial vehicle motor are quickly connected together.

[0030] Specifically, the UAV rotor quick-installation structure of the present invention includes the UAV rotor, the mounting base fixedly connected with the UAV rotor, the UAV motor and the connection assembly fixedly connected with th...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The present invention discloses a rapid installation structure of an unmanned aerial vehicle rotor wing. The rapid installation structure comprises: an installation base fixedly connected with an unmanned aerial vehicle rotor wing, and a connection assembly fixedly connected with an unmanned aerial vehicle motor, wherein the connection assembly is provided with a concave or convex first lock member, the installation base is provided with a convex or concave second lock member matched with the connection assembly, and the unmanned aerial vehicle rotor wing and the unmanned aerial vehicle motor are rapidly and integratedly connected through locking of the first lock member and the second lock member. The present invention further provides an unmanned aerial vehicle having the rapid installation structure. According to the present invention, with the rapid installation structure of the unmanned aerial vehicle rotor wing, the structure is simple, and the unmanned aerial vehicle rotor wing is rapidly installed on the unmanned aerial vehicle motor through the locking manner so as to achieve convenient disassembly with characteristics of no disassembly tool and no part disassembly, shorten the spreading time of the rotor wing, increase the flying maneuverability of the unmanned aerial vehicle, and perform rapid maintenance or replacement on the rotor wing.

Description

technical field [0001] The invention relates to the technical field of rotor unmanned aerial vehicles, in particular to a quick assembly structure capable of quickly mounting and dismounting the rotor of an unmanned aerial vehicle on a motor and an unmanned aerial vehicle with the quick assembly structure. Background technique [0002] In recent years, the technology of unmanned aerial vehicles has become more and more mature. It has a power device without carrying operators, its takeoff and landing, hovering are stable, and it has autonomous cruise capabilities. At the same time, it can also carry various mission equipment, so it has been widely used in military and civilian fields. Wide range of applications, especially in the civilian field, small unmanned aerial vehicles have begun a large number of application attempts of unmanned aerial vehicles in industries such as fire protection, security monitoring, surveying and mapping, and film and television shooting. [0003]...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/32
Inventor 罗国坤谭剑涛
Owner FOSHAN AIRCAM UAV TECH CORP