首页> 外国专利> Component for use in e.g. fuselage, of aircraft, has fiber-reinforced plastic part and fiber e.g. optical glass fiber, for guiding electrical or electromagnetic and/or optical signal such as light signal through component

Component for use in e.g. fuselage, of aircraft, has fiber-reinforced plastic part and fiber e.g. optical glass fiber, for guiding electrical or electromagnetic and/or optical signal such as light signal through component

机译:例如用于飞机的机身具有纤维增强的塑料部件和纤维,例如玻璃光纤,用于通过组件引导电或电磁和/或光信号,例如光信号

摘要

The component (10) has a fiber-reinforced plastic part and a fiber (12) e.g. optical glass fiber, for guiding an electrical or electromagnetic and/or optical signal (13) such as light signal through the component. The fiber extends transverse through the component and communicates with a transmitter at an end and a receiver at another end. A processor monitors and evaluates signal received from the receiver. The transmitter comprises a light source i.e. LED, and the receiver comprises a light sensor for receiving the signals. Independent claims are also included for the following: (1) a system for detecting a position of defect of an aircraft (2) a method for detecting a position of defect of an aircraft.
机译:部件(10)具有纤维增强的塑料部件和例如纤维(12)的纤维(12)。光学玻璃纤维,用于引导电或电磁和/或光信号(13),例如光信号通过组件。光纤横向延伸穿过组件,并与一端的发送器和另一端的接收器通信。处理器监视并评估从接收器接收到的信号。发射器包括光源,即LED,并且接收器包括用于接收信号的光传感器。还包括以下方面的独立权利要求:(1)用于检测飞机的缺陷位置的系统(2)用于检测飞机的缺陷位置的方法。

著录项

  • 公开/公告号DE102008026781A1

    专利类型

  • 公开/公告日2009-12-10

    原文格式PDF

  • 申请/专利权人 HARDUNG HEIMO VON;

    申请/专利号DE20081026781

  • 发明设计人 HARDUNG HEIMO VON;

    申请日2008-06-04

  • 分类号G01M13/00;G01M11/08;G01M5/00;

  • 国家 DE

  • 入库时间 2022-08-21 18:28:56

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