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Flight body flight system and flight body flight method

机译:飞行体飞行系统和飞行体飞行方法

摘要

The vehicle body 3 is equipped with a power receiving apparatus 20 for receiving electric power by a non-contact power supply of a magnetic resonance system, and a thrust generating mechanism (power motor 255, a motor control device 254) for obtaining a thrust for the flight by electric power received by the receiving apparatus 20 During the flight of the line 3, electric power is transmitted to the receiving apparatus 20 by contactless power supply from the power transmission apparatus 10 spaced from the body 3.A sensor (an area sensor 15, a distance measuring sensor 16) for providing information used for judging whether or not the body 3 exists in a preset flight area 5 and an information processing device 14 are provided, and the information processing device 14 is based on the above information, and the flight body 14 is a flying body It is determined whether or not 3 exists in the flight area 5, and the power to be transmitted from the transmission apparatus 10 is lowered when it is determined that the body 3 is not present in the flight area 5.
机译:车身3具备:受电装置20,其通过磁共振系统的非接触电源接收电力;以及推力产生机构(动力马达255,马达控制装置254),该推力产生机构用于获得用于由接收设备20接收的电力进行的飞行在线路3的飞行过程中,电力通过与主体3隔开的动力传输设备10的非接触式电力传输到接收设备20。参照图15,提供了距离测量传感器16)和信息处理设备14,该距离测量传感器16提供用于判断在预定飞行区域5中是否存在物体3的信息,该信息处理设备14基于上述信息,并且飞行体14是飞行体,判断在飞行区域5中是否存在3,并且当从飞行装置14传输的动力降低时确定在飞行区域5中不存在身体3。

著录项

  • 公开/公告号JPWO2017203590A1

    专利类型

  • 公开/公告日2018-06-07

    原文格式PDF

  • 申请/专利权人 中国電力株式会社;

    申请/专利号JP20170503182

  • 发明设计人 沖段 和磨;

    申请日2016-05-24

  • 分类号H02J50/12;H02J7;B64C13/18;B64C39/02;B64D27/24;B64F1/12;B64C13/20;

  • 国家 JP

  • 入库时间 2022-08-21 13:06:57

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