The invention provides an aircraft auxiliary display system capable of avoiding space disorientation. The aircraft auxiliary display system comprises a central processing unit, a sensing module, a starting display unit and an electronic optical visual unit. The central processing unit comprises a storage unit and is electrically connected to the starting display unit; the sensing module is electrically connected to the central processing unit and comprises a flight data sensing unit; the starting display unit is electrically connected to the electronic optical visual unit.

    本发明提供一种避免空间迷向的飞航器辅助显示系统,包含中央处理单元、感测模块、启动显示单元以及电子光学可视单元。中央处理单元包括储存单元且电性连接于启动显示单元;感测模块电性连接于中央处理单元且包括飞航数据感测单元;启动显示单元电性连接于电子光学可视单元。


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    Titel :

    Aircraft auxiliary display system capable of avoiding space disorientation


    Weitere Titelangaben:

    避免空间迷向的飞航器辅助显示系统


    Beteiligte:

    Erscheinungsdatum :

    05.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT AUXILIARY DISPLAY SYSTEM FOR AVOIDING SPATIAL DISORIENTATION

    LIN HUNG-HSIN | Europäisches Patentamt | 2023

    Freier Zugriff

    Disorientation

    NTIS | 1994



    Disorientation

    NTIS | 1994