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Security system for use in civilian airliner, has computing unit initiating automatic flight control system of aircraft to control aircraft at selected destination airport and land aircraft at airport after selection of airport

机译:用于民用飞机的安全系统,具有计算单元,该计算单元启动飞机的自动飞行控制系统,以控制选定目的地机场的飞机并在选择机场后控制机场的陆地飞机

摘要

The system (2) has an activating unit (4) activating emergency programs, and connected with a signal input of a computing unit (8). The activating unit selects a destination airport during operation of the computing unit. The computing unit initiates an automatic flight control system (12) of an aircraft to control the aircraft at the selected destination airport and to land the aircraft at the destination airport after selection of the destination airport. An UHF/VHF transmitter (16) sends an emergency signal during operation of the computing unit. An independent claim is also included for a method for implementing emergency programs after operation of activating units.
机译:系统(2)具有激活紧急程序的激活单元(4),并与计算单元(8)的信号输入连接。激活单元在计算单元的操作期间选择目的地机场。计算单元启动飞机的自动飞行控制系统(12)以控制飞机在选定的目的地机场并且在选择目的地机场之后使飞机降落在目的地机场。 UHF / VHF发射机(16)在计算单元的操作期间发送紧急信号。还包括一种用于在激活单元运行之后执行紧急程序的方法的独立权利要求。

著录项

  • 公开/公告号DE102008025404A1

    专利类型

  • 公开/公告日2009-12-17

    原文格式PDF

  • 申请/专利权人 AIRBUS DEUTSCHLAND GMBH;

    申请/专利号DE20081025404

  • 发明设计人 SCHWORMSTEDT BORIS;

    申请日2008-05-28

  • 分类号B64D45/00;

  • 国家 DE

  • 入库时间 2022-08-21 18:28:56

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