Electric unmanned helicopter

An unmanned helicopter, electric technology, applied in the directions of unmanned aerial vehicles, fuselage, motor vehicles, etc., can solve the problems of difficult adjustment of the center of gravity, poor load capacity, troublesome disassembly and assembly, etc., to reduce weight, increase versatility and Interchangeability, simple and clear structure

Pending Publication Date: 2018-06-29
ZHUHAI ZIYAN UAV CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There are many problems in the traditional unmanned helicopter structure: complex structure, troublesome disassembly; low integration,

Method used

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  • Electric unmanned helicopter
  • Electric unmanned helicopter
  • Electric unmanned helicopter

Examples

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Embodiment Construction

[0025] Such as Figure 1 to Figure 4 As shown, in this embodiment, the present invention adopts a modular design, including a front-end module 1, a middle-end module 2, and a rear-end module 3 connected in sequence, and the front-end module 1 includes symmetrically arranged left carbon fiber plates 11 and right carbon fiber plates Plate 12, between the left carbon fiber plate 11 and the right carbon fiber plate 12, there is a picture number transmission device 13, an electric adjustment device 14 and a load installation plate 15, and the middle end module 2 includes an upper carbon fiber plate 21, which is arranged on The lower carbon fiber plate 22 below the upper carbon fiber plate 21 and the active power system 23 arranged on the upper carbon fiber plate 21 and the lower carbon fiber plate 22, the rear end module 3 includes a tailpipe 31 and is arranged on the Tail rotor system 32 at tail pipe 31 end. In this design, the main body of the whole machine is divided into three...

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Abstract

The invention discloses an electric unmanned helicopter, and aims to provide the electric unmanned helicopter having advantages of simple structure, easy disassembly and assembly, good interchangeability, high integration, good functionality, light weight, strong load capacity, long endurance, good stability, small vibration, adjustable gravity center and the like. The electric unmanned helicopterprovided by the invention comprises a front end module, a middle end module and a rear end module which are sequentially connected, wherein the front end module comprises a left carbon fiber board and a right carbon fiber board which are symmetrically arranged; an image and data transmission device, an electronic speed regulating device and a load mounting board are arranged between the left carbon fiber board and the right carbon fiber board; the middle end module comprises an upper carbon fiber board, a lower carbon fiber board arranged below the upper carbon fiber board, and main power systems arranged on the upper carbon fiber board and the lower carbon fiber board; the rear end module comprises a tail tube and a tail rotor system arranged at a tail end of the tail tube. The electricunmanned helicopter provided by the invention is applied to the technical field of electric unmanned helicopters.

Description

technical field [0001] The invention relates to the technical field of electric unmanned helicopters, in particular to an electric unmanned helicopter. Background technique [0002] At present, unmanned helicopters have played an irreplaceable important role in national defense construction, national economic construction and emergency response, and the application of unmanned helicopters has penetrated into all walks of life. Small unmanned helicopters have many advantages such as small size, good maneuverability, strong anti-interference ability, easy to carry, no need for runways, and are not affected by terrain. , Forest and oil fire patrols, search and rescue, light material transportation, border defense, customs patrol, anti-terrorism and stability maintenance, etc. have a very wide range of uses. [0003] With the continuous development of UAV technology, the market has higher and higher expectations for the performance of small unmanned helicopters. There are many...

Claims

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Application Information

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IPC IPC(8): B64C1/00B64C1/16B64D27/24B64D27/26B64C17/02
CPCB64C1/00B64C1/16B64C17/02B64D27/24B64D27/26B64C2001/0072B64U10/10Y02T50/60
Inventor 王江平刘一
Owner ZHUHAI ZIYAN UAV CO LTD
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