The invention relates to a splitting type undercarriage for a helicopter model. The splitting type undercarriage comprises a first bracket and a second bracket, wherein the bottom ends of the first bracket and the second bracket are fixedly connected with a connection ring; the connection ring is provided with a supporting rod; the supporting rod is in sleeve joint with the connection ring; the connection ring is provided with a fixing device for fixing the supporting rod in the connection ring; the first bracket and the second bracket are in bolt connection with a connection plate which is fixedly connected with a helicopter fuselage; a floating plate for promoting buoyancy force when a helicopter falls into the water is arranged in the connection plate; alarming lamps are fixedly connected with the two ends of the supporting rod and the supporting rod is internally provided with a power supply device for supplying power to the alarming lamps; and a pressure switch for controlling the alarming lamps to be turned on and off is arranged at the bottom of the supporting rod. The splitting type undercarriage for the helicopter model is provided with the connection plate with the floating plate and the automatic alarming lamps, so that the safety of the helicopter model is greatly improved.


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    Titel :

    Splitting type undercarriage for helicopter model


    Beteiligte:
    ZHANG LI (Autor:in)

    Erscheinungsdatum :

    29.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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