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drone

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

Active Publication Date: 2018-03-20
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 and figure 2 , in a preferred embodiment of the drone of the present invention, the drone also includes a battery (not shown in the figure), a control circuit assembly (not shown in the figure), multiple groups of paddle assemblies 200 and a fuselage 100, in figure 2 The fuselage 100a shown is the first specific implementation of the fuselage 100 of the preferred embodiment of the drone of the present invention. The fuselage 100a is provided with chambers for accommodating batteries and control circuit components. The batteries are accumulators, such as Lithium batteries are used to provide electrical energy to the relevant power-consuming parts of the drone. The control circuit components include multiple ...

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Abstract

The invention discloses an unmanned aerial vehicle, which includes 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 A motor electrically connected to the control circuit assembly, one end of each of the paddle arms is hinged to the fuselage; the UAV also includes a paddle spreading assembly corresponding to each of the paddle arms, and the paddle assembly Having a folded state and an unfolded state, the paddle spreader assembly unfolds the paddle assembly from the folded state to an unfolded state and maintains the paddle assembly in the unfolded state. As a result, the packaging structure for transportation and the volume of space occupied during storage are reduced. At the same time, the paddle assembly is driven by a motor to unfold 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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