Wired power multiple rotor wing unmanned aerial vehicle

A multi-rotor unmanned, wired power supply technology, applied in aircraft parts, power plant types, ground devices for mooring aircraft, etc. effect of life

Inactive Publication Date: 2014-04-30
张家港锐泰智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Unmanned aerial vehicles contain many high-precision, high-sensitivity electric motors and other electronic co

Method used

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  • Wired power multiple rotor wing unmanned aerial vehicle
  • Wired power multiple rotor wing unmanned aerial vehicle

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Embodiment Construction

[0016] The present invention is described in further detail now in conjunction with accompanying drawing. These drawings are all simplified schematic diagrams, which only illustrate the basic structure of the present invention in a schematic manner, so they only show the configurations related to the present invention.

[0017] like figure 1 Or as shown in 2, a multi-rotor unmanned aerial vehicle with wired power supply of the present invention includes a multi-rotor unmanned aerial vehicle 1 and a ground power supply device 2, and the described multi-rotor unmanned aerial vehicle 1 is equipped with a high voltage power supply device 2 The AC power is converted into a DC low-voltage power conversion system 3 suitable for the multi-rotor unmanned aerial vehicle 1. The power conversion system 3 is electrically connected to the ground power supply device 2 through a cable 4, and the power conversion system 3 is also connected. A power supply assembly for distributing electric en...

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Abstract

The invention relates to a wired power multiple rotor wing unmanned aerial vehicle comprising a multiple rotor wing unmanned aerial vehicle and a ground power unit. A power converter for converting high-pressure alternating current of the ground power unit to direct current low tension suitable for the multiple rotor wing unmanned aerial vehicle is arranged on the multiple rotor wing unmanned aerial vehicle, the power converter is electrically connected with the ground power unit via cables, and the power converter is provided with a power supply assembly for allocating power to each functional module of the multiple rotor wing unmanned aerial vehicle. Compared with the flying scheme of batteries in the existing multiple rotor wing unmanned aerial, the wired power multiple rotor wing unmanned aerial vehicle can greatly increase flying time of the aerial vehicle without limit in the acceptable range of aerial vehicle motors and other equipment.

Description

technical field [0001] The invention relates to the technical field of aircraft power supply equipment, in particular to a multi-rotor unmanned aircraft with wired power supply. Background technique [0002] Multi-axis and multi-rotor unmanned aerial vehicles are used more and more in civil and engineering fields. Due to the unique flight performance of multi-axis and multi-rotor unmanned aerial vehicles, this type of aircraft is suitable for aerial photography and monitoring. However, the current multi-axis multi-rotor unmanned aerial vehicle also has its disadvantages. The existing products and designs all use lithium batteries to power this type of aircraft. Since the lift of the multi-axis multi-rotor aircraft is completely provided by the electric motor, the energy consumption is large. Power consumption is very fast. The larger the battery capacity carried, the less the payload. The flight time of multi-axis and multi-rotor unmanned aerial vehicles in the prior art is...

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Application Information

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IPC IPC(8): B64D27/24B64F1/36B64F3/02
CPCY02T50/60
Inventor 杨华东许剑吴奇才
Owner 张家港锐泰智能科技有限公司
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