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Electric rotorcraft charging system

A rotorcraft and charging system technology, which is applied in the field of electric rotorcraft charging systems, can solve the problems of difficult automatic charging and inconvenient battery charging, and achieve the effects of small footprint, good protection and convenient use

Active Publication Date: 2015-06-24
深圳市多翼创新科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a charging system for an electric rotorcraft to solve the problems of inconvenient and difficult automatic charging when charging the batteries of the existing electric rotorcraft

Method used

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Embodiment Construction

[0032] In order to better illustrate the present invention, the present invention will be described in detail with a preferred embodiment and with accompanying drawings, specifically as follows:

[0033] The electric rotorcraft charging system provided in this embodiment includes: a charging platform 1 , a windbreak wall 2 , an onboard battery 3 and a power receiving device 4 .

[0034] like figure 1 As shown, the windbreak wall 2 in this embodiment includes four identical windbreak wall structures, and these four pieces of windbreak walls are erected around the charging platform, which can avoid the impact of the surrounding wind force on the landing of the electric rotorcraft. In addition, a visual mark 201 may also be provided on the outer surface of the windbreak wall, so as to highlight the charging system from the surrounding environment. Wherein, the visual mark 201 can be any easily identifiable characters, symbols, numbers or other simple patterns, and the visual mar...

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Abstract

The invention provides an electric rotorcraft charging system. The electric rotorcraft charging system comprises a charging part and an airborne part, wherein the charging part comprises a charging platform and a windbreaker, and the airborne part comprises an electric energy receiving device and an airborne battery. The electric rotorcraft charging system is suitable for charging batteries of various electric rotorcrafts capable of vertical take-off and landing. A conductive contact surface with good electrical conductivity arranged on the charging platform is convenient for the electric rotorcraft to make direct contact with the contact surface through an electric conductor to achieve conduction-type charging. Moreover, the arrangement of the charging platform capable of being folded enables the occupied space of the charging platform to be smaller, the protection of the front side or the back side of the conductive contact surface is facilitated, and the use of a heating resistor capable of heating further enables the charging platform to avoid the problem of a charging obstacle caused by ice or accumulated snow. When the electric rotorcraft charging system is used to charge, the charging of the airborne battery can be directly performed after the electric rotorcraft lands at the charging platform, and the use is very convenient.

Description

technical field [0001] The invention relates to a charging device for an electric rotorcraft, in particular to a charging system for an electric rotorcraft. Background technique [0002] When the existing electric rotorcraft needs to be charged, the battery must be disassembled from the aircraft for charging, and then the battery must be assembled on the electric rotorcraft after charging. This method of first disassembling the battery and then charging it is not only inconvenient to use but also difficult to realize automatic charging. Contents of the invention [0003] The purpose of the present invention is to provide a charging system for an electric rotorcraft to solve the problems of inconvenient and difficult automatic charging of the battery of the existing electric rotorcraft. [0004] To achieve the above object, the present invention provides a charging system for an electric rotorcraft, the charging system comprising: [0005] Charging platform: including a l...

Claims

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Application Information

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IPC IPC(8): H02J7/00
Inventor 王洋
Owner 深圳市多翼创新科技有限公司
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