A deployable emergency transmitter device is configured to be launched from an aircraft in an initial passive flight state. It comprise an internal chassis, and an inertial mass member, rotatable relative to the internal chassis, for stabilising flight during the initial passive flight state. It has a powered drive system, mounted to the internal chassis and configured for providing lift while the deployable emergency transmitter device is in an active flight state. It has a radio transmitter configured for transmitting an emergency signal after being launched from the aircraft. The device is configured to transition from the initial passive flight state to the active flight state, after being launched from the aircraft.


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    Title :

    EMERGENCY TRANSMITTER DEVICE


    Additional title:

    NOTFALLSENDER
    DISPOSITIF DE TRANSMISSION D'URGENCE



    Publication date :

    2025-07-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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