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Power line communication system on aircraft

机译:飞机上的电力线通信系统

摘要

A method includes coupling a vehicle to an electrical umbilical comprising a supply end, a plug end and an electrical conductor extending therebetween, said plug end configured to mate with the vehicle such that power is supplied to the vehicle through the electrical conductor from the supply end; the method also uses a first interface device electrically coupled to the supply end and a network access point, the first interface device configured to: transmit and receive data carrier signals though the electrical conductor while power is supplied to the vehicle through the electrical conductor; and convert the data carrier signals from and to a predetermined data format on the network; and a second interface device electrically coupled to the plug end when the umbilical is coupled to the vehicle, said interface device configured to transmit and receive the data carrier signals with the first interface device while power is supplied to the aircraft through the electrical conductor.
机译:一种方法,包括将车辆联接至包括供应端,插头端和在其间延伸的电导体的电脐带,所述插头端构造成与车辆配合,从而通过电导体从供应端向车辆供应电力。 ;该方法还使用电耦合到供应端和网络接入点的第一接口设备,该第一接口设备被配置为:当通过电导体向车辆供电时,通过电导体发送和接收数据载体信号。将数据载波信号与网络上的预定数据格式相互转换;当脐带缆线连接至车辆时,第二接口装置电连接至插头端,所述接口装置构造成在通过电导体向飞机供电时与第一接口装置发送和接收数据载体信号。

著录项

  • 公开/公告号EP2475103B1

    专利类型

  • 公开/公告日2014-04-09

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20120163307

  • 发明设计人 DAVIS TERRY. L;PELTON SCOTT L.;

    申请日2008-02-05

  • 分类号H04B3/54;

  • 国家 EP

  • 入库时间 2022-08-21 15:49:29

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