An aircraft system (10) for an aircraft (1) including a controller (100) configured to receive at least one signal during a take-off procedure of the aircraft. The signal includes information representative of at least one parameter of the aircraft. The controller is configured to determine whether a current or future aircraft climb rate associated with the take-off procedure meets a criterion, on the basis of the at least one signal. The controller is configured to determine at least one remedial action to be taken, such as performance of at least a portion of a procedure to retract a landing gear of the aircraft, when the controller determines that the aircraft climb rate does not meet the criterion.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft take-off system


    Beteiligte:
    KERR SEAN (Autor:in) / MARLES DAVID (Autor:in)

    Erscheinungsdatum :

    04.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aircraft take-off system

    JIANG ZHENYU / XU QIUPING / LI XIAOBIN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT VERTICAL TAKE-OFF SYSTEM

    DUROV DMITRIJ SERGEEVICH | Europäisches Patentamt | 2016

    Freier Zugriff


    AIRCRAFT TAKE-OFF AND LANDING SYSTEM

    NAM YONG HYUN / YIM CHUNG SIK / CHOI JAE YOUNG et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Vertical take-off aircraft

    Emerald Group Publishing | 2001