drone

A technology of unmanned aerial vehicle and fuselage, applied in the field of aircraft, can solve the problems of cumbersome and manual installation, and achieve the effect of reducing space volume and packaging structure

Active Publication Date: 2017-11-10
SICHUAN AEE AVIATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Most of the UAVs in the prior art have their paddle arms and fuselage integrally formed, and some of them divide the paddle arms into two parts: the first paddle arm and the second paddle arm, and the first paddle arm is integrated with the fuselage Forming, the detachable connection between the second section of the paddle arm and the first section of the paddle arm solves the problem of transportation and storage space to a certain extent, but it still needs manual installation when using it, which is more cumbersome

Method used

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Embodiment Construction

[0028] It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0029] The invention provides an unmanned aerial vehicle, which is a foldable rotor helicopter, see Figure 1 to Figure 3 , in a preferred embodiment of the drone of the present invention, the drone includes a battery (not shown in the figure), a control circuit assembly (not shown in the figure), multiple sets of paddle assemblies 200 and a fuselage 100, the machine The body 100 is provided with a chamber for accommodating a battery and a control circuit assembly. The battery is a storage battery, such as a lithium battery, used to provide electrical energy to the relevant components of the drone. The control circuit assembly includes a plurality of control modules, such as for controlling UAV flight attitude flight control module, Beidou module (such as GPS module) for navigating UAV, and data processing module for ...

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Abstract

The invention discloses an unmanned aerial vehicle, which comprises a battery, a control circuit assembly, multiple sets of paddle assemblies and a fuselage, the paddle assemblies are arranged around the circumference of the fuselage; the paddle assemblies include paddle arms, paddle blades and are electrically connected to the control circuit assembly One end of each paddle arm is hinged with the fuselage. The drone also includes a paddle lock assembly and air rods corresponding to each paddle arm. The arm body between the two ends of the paddle arm is connected to the fuselage through an air rod The paddle assembly has a folded state and an unfolded state, the paddle lock assembly keeps the paddle assembly in the folded state in the folded state, and the air bar expands the paddle assembly in the folded state to the unfolded state and maintains it in the unfolded state. As a result, the packaging structure for transportation and the volume of space occupied during storage are reduced, and the paddle assembly is deployed through the air rod without manual installation.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an unmanned aerial vehicle. Background technique [0002] In recent years, drones have received more and more attention due to their simple structure, convenient manipulation and high safety performance. Most of the UAVs in the prior art have their paddle arms and fuselage integrally formed, and some of them divide the paddle arms into two parts: the first paddle arm and the second paddle arm, and the first paddle arm is integrated with the fuselage Forming, the detachable connection of the second section of the paddle arm and the first section of the paddle arm solves the problem of transportation and storage space to a certain extent, but it still needs manual installation when it is used, which is more cumbersome. Contents of the invention [0003] The main purpose of the present invention is to provide an unmanned aerial vehicle, aiming at further saving transportation an...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C11/00
Inventor 张显志
Owner SICHUAN AEE AVIATION TECH CO LTD
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