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A flat-convex-wing unmanned aerial vehicle with integrated battery

A technology for integrating batteries and drones, which is applied to wings, aircraft parts, transportation and packaging, etc. It can solve the problem that integrated batteries are inconvenient for users to replace, and achieve the effects of saving internal space, reducing volume, and improving battery life

Active Publication Date: 2020-12-25
安徽中骄创新技术发展有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide an integrated battery flat convex wing drone, which is easy to install and disassemble by being provided with a clamping device, a limiting device, a clamping plate, a limiting groove, a sliding groove, a fixing block and a clamping groove The integrated battery solves the problem that the existing drone is inconvenient for users to replace when it is urgently used and cannot wait for the charging time to replace the integrated battery

Method used

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  • A flat-convex-wing unmanned aerial vehicle with integrated battery
  • A flat-convex-wing unmanned aerial vehicle with integrated battery
  • A flat-convex-wing unmanned aerial vehicle with integrated battery

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Embodiment Construction

[0029]The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.

[0030]In the description of the present invention, it should be understood that the terms "opening", "upper", "lower", "thickness", "top", "middle", "length", "inner", "around", etc. The indication of the orientation or position relationship is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the component or element referred to must have a specific orientation...

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Abstract

The invention discloses an integral battery convex wing unmanned aerial vehicle and relates to the technical field of unmanned aerial vehicles. The integral battery convex wing unmanned aerial vehiclecomprises a machine body, wherein wings are arranged on both sides of the machine body; clamping bases are fixed at the bottoms of the inner cavities of the wings; integral batteries are arranged atthe tops of the clamping bases; cover plates are arranged at the tops of the wings; a limiting device is fixed on one side of the top of the inner cavity of each wing; a plurality of clamping devicespenetrate through one side of each cover plate in parallel. Due to adoption of the clamping devices, limiting devices, clamping plates limiting grooves, sliding grooves, fixing blocks and clamping grooves, integral batteries can be conveniently mounted and dismounted, the integral batteries can be conveniently replaced when the integral batteries need to be used urgently and cannot wait for a recharge time, meanwhile as the integral batteries are mounted on the wings, the space inside the machine body is saved, and energy consumption of the unmanned aerial vehicle is reduced; due to adoption of holding grooves, clamping blocks and grooves, the problem that flying is obstructed by too much air when the unmanned aerial vehicle flies is avoided.

Description

Technical field[0001]The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to an integrated battery flat convex wing unmanned aerial vehicle.Background technique[0002]Unmanned aircraft is abbreviated as unmanned aerial vehicle. It is an unmanned aircraft operated by radio remote control equipment and its own program control device. It has no cockpit on board, but is equipped with autopilot and program control devices. It is widely used in the air. Reconnaissance, surveillance, communications, anti-submarine, electronic interference, etc.[0003]Traditional flat-lobe UAVs have integrated batteries installed inside the fuselage. However, excessive waste of fuselage space and inconvenient installation of other components result in the unmanned aerial vehicle being too large and consume unnecessary power. At the same time, the integrated battery is installed. Inside the body, there will be a problem of inconvenience to install and remove the b...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C3/00B64C3/34
CPCB64C3/00B64C3/34
Inventor 王兴生
Owner 安徽中骄创新技术发展有限公司
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