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Aircraft avionics system Simultaneous bidirectional bus for numerical data communication between aircraft avionics equipment, and avionics equipment

机译:飞机航空电子系统同时双向总线,用于飞机航空电子设备与航空电子设备之间的数值数据通信

摘要

The system has a pair of equipments comprising electrical interfaces connected using electrical communication bus. The equipments exchange information through an optical communication bus connected to the interfaces. A connector (30) is provided at ends of the optical communication bus. The connector has a conversion component (45) e.g. LED, laser diode, for converting electrical signals into optical signals, and conversion component (46) e.g. phototransistor, for converting optical signals into electrical signals. Independent claims are also included for the following: (1) a bidirectional bus for communicating data in the form of digital signals between avionic equipments (2) an avionic equipment.
机译:该系统具有一对设备,该对设备包括使用电通信总线连接的电接口。设备通过连接到接口的光通信总线交换信息。在光通信总线的端部设有连接器(30)。该连接器具有转换部件(45),例如。 LED,用于将电信号转换成光信号的激光二极管以及转换组件(46),例如,光电晶体管,用于将光信号转换为电信号。还包括以下方面的独立权利要求:(1)双向总线,用于在航空电子设备之间以数字信号的形式传送数据(2)航空电子设备。

著录项

  • 公开/公告号BRPI0615037A2

    专利类型

  • 公开/公告日2016-09-13

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号BR2006PI15037

  • 发明设计人 TOURNIER GILLES;

    申请日2006-08-31

  • 分类号G02B6/42;G06F13/38;H04B10/2581;

  • 国家 BR

  • 入库时间 2022-08-21 14:26:56

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