The present invention provides a water inflow prevention device for aircraft, working when landing in water, the device including: a blocking body for blocking a flow channel from an outside of the aircraft when landing in water, the flow channel allowing the inside and outside of the aircraft to communicate with each other, and a valve element of a pressure adjusting valve being positioned in the flow channel; and a connection part that is deformed when landing in water, wherein the blocking body is supported by a member constituting an end of the flow channel on a side outside the aircraft through the connection part, and the connection part is deformed in a direction so as to block the flow channel by the blocking body, with use of force of water acting on the blocking body when landing in water.


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    Titel :

    WATER INFLOW PREVENTION DEVICE FOR AIRCRAFT WORKING WHEN LANDING IN WATER, PRESSURE ADJUSTING VALVE, AND AIRCRAFT


    Beteiligte:
    KAWANO SHINGO (Autor:in) / UCHINO TAKASHI (Autor:in) / HAGINO SYUICHI (Autor:in) / URANO AKITAKA (Autor:in)

    Erscheinungsdatum :

    2016-09-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16K VALVES , Ventile



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