An unmanned aircraft includes a circuit board with an inertia sensor, a vibration damper configured to attenuate vibration of the inertia sensor, a weight block configured to provide support for positioning the circuit board, and a housing assembly configured to form an inner chamber to accommodate the circuit board and the weight block. The vibration damper includes a first vibration-attenuation cushion and a second vibration-attenuation cushion bonded respectively to a first side and a second side of the circuit board. The weight block is disposed between the first vibration-attenuation cushion and the circuit board.


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    Titel :

    INERTIA MEASUREMENT MODULE FOR UNMANNED AIRCRAFT


    Beteiligte:
    WANG TAO (Autor:in) / ZHAO TAO (Autor:in)

    Erscheinungsdatum :

    2022-07-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16F SPRINGS , Federn / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS



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