An aircraft vibration detecting device applicable to an aircraft having a moving surface to be driven by an actuator includes a difference calculating unit for calculating a difference between a target value of an angle of the moving surface and an actual measured value of the angle of the moving surface, a threshold value determining unit for determining whether an absolute value of the difference is equal to or greater than a threshold value, and a vibration determining unit for determining that the moving surface is vibrating if the absolute value of the difference is equal to or greater than the threshold value.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT VIBRATION DETECTING DEVICE, AIRCRAFT VIBRATION DETECTING METHOD, AND NON-TRANSITORY COMPUTER-READABLE STORAGE MEDIUM STORING THEREON PROGRAM FOR AIRCRAFT VIBRATION DETECTION


    Beteiligte:
    OGAWA TAKASHI (Autor:in) / TANIMOTO TAKASHI (Autor:in)

    Erscheinungsdatum :

    02.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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




    AIRCRAFT VIBRATION DETECTING DEVICE, AIRCRAFT VIBRATION DETECTING METHOD, AND PROGRAM FOR AIRCRAFT VIBRATION DETECTION

    OGAWA TAKASHI / TANIMOTO TAKASHI | Europäisches Patentamt | 2025

    Freier Zugriff


    Aircraft vibration

    Constant, H. | Engineering Index Backfile | 1932


    Aircraft Vibration

    Constant, H. | TIBKAT | 1935