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Modular miniature unmanned aerial vehicle

A drone, modular technology, applied in the direction of the fuselage, rotorcraft, motor vehicles, etc., can solve the problems of poor task load stability, poor compatibility of micro drones, etc., to achieve multi-functional use, enhanced compatibility, The effect of enhanced stability

Pending Publication Date: 2018-08-21
王瀚晨
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a modular micro-UAV to solve the technical problems of poor compatibility of the micro-UAV and poor stability of the task load of the micro-UAV due to the vibration of the fuselage in the prior art

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Embodiment Construction

[0030] In order to make the technical problems, technical solutions and beneficial effects to be solved by the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0031] It should be noted that when an element is referred to as being “fixed” or “disposed on” another element, it may be directly on the other element or be indirectly on the other element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or indirectly connected to the other element.

[0032] It is to be understood that the terms "length", "width", "top", "bottom", "front", "rear", "left", "right", "vertical", "horizontal", "top" , "bottom", "inner", "outer" and other indicated orientations...

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Abstract

The invention provides a modular miniature unmanned aerial vehicle, and belongs to the technical field of miniature unmanned aerial vehicles. The modular miniature unmanned aerial vehicle comprises abody. The body comprises an upper shell, a middle shell and a lower shell, and the heads and the tails of the upper shell, the middle shell and the lower shell are sequentially detachably connected with one another; mission payloads are arranged inside the lower shell; a first partition plate for completely separating the upper shell from the middle shell is arranged between the upper shell and the middle shell, and a second partition plate for completely separating the middle shell from the lower shell is arranged between the middle shell and the lower shell; a universal suspension is arranged on the upper portion of the upper shell, and a power device for driving propellers to rotate is arranged on the universal suspension. The modular miniature unmanned aerial vehicle has the advantagethat the problems of poor compatibility and poor mission payload stability due to vibration of existing bodies can be effectively solved by the aid of the modular miniature unmanned aerial vehicle.

Description

technical field [0001] The invention belongs to the technical field of micro drones, and more specifically relates to a modular micro drone. Background technique [0002] At present, the use of micro unmanned aerial vehicles is mostly reconnaissance. Its development is mainly divided into three categories: fixed wing, bionic flapping wing and multi-rotor. There are also single-rotor drones represented by helicopters. However, the current definition of micro drones is not very clear, and there are no strict restrictions on size and weight. While size and weight are important factors, modern micro-drones still prioritize practicality. [0003] Among the micro-UAVs, the fixed-wing UAVs are relatively mature. Most of them are palm-sized and can achieve long battery life and long range. Some models can also achieve hovering similar to "crane", but their wind resistance is poor. The weight of the carried load is small, which is not suitable for outdoor flying; the bionic oropter...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/06B64C27/06B64D27/26
CPCB64C1/061B64C13/00B64C27/10B64C27/14
Inventor 王瀚晨王玉柱刘贵君
Owner 王瀚晨
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