An airplane off ground advisory system employs at least one position sensor attached for detection of an extended condition and a compressed condition of a main landing gear. A control system receives an input from the position sensor. The control system records a toggling of the input from an extended to a compressed to an extended condition and providing an output. At least one indicator is coupled to the control system to be activated by the output.


    Access

    Download


    Export, share and cite



    Title :

    Airplane off ground advisory system


    Contributors:

    Publication date :

    2015-12-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    Airplane off ground advisory system

    HERBERT KEITH B / JINADASA SUNIL J | European Patent Office | 2017

    Free access

    Airplane off ground advisory system

    HERBERT KEITH B / JINADASA SUNIL J | European Patent Office | 2015

    Free access


    Airplane ground flight verification system

    PAN TENGFEI / HOU WENLI / WU LIANG et al. | European Patent Office | 2015

    Free access

    Airplane ground power interface device and airplane ground power supply method

    LANG ZHEN / LIU LIANGLIANG / LI ZHENGHONG et al. | European Patent Office | 2023

    Free access