A buoyancy system (10) for an aircraft (1), the buoyancy system (10) being provided with at least one inflatable float (15). The buoyancy system (10) has at least one inflator (25) and at least one actuator (30) interposed between the inflator (25) and a float (15), the actuator (30) having a cylinder (35) and a rod (40) partially received in the cylinder (35). The rod (40) is secured to a piston (50) defining a first chamber (61) within the cylinder (35) and in fluid flow communication with the inflator (25), and a second chamber (62) within the rod (40) and in fluid flow communication with the float (15), and the piston (50) has a channel (63) to put the first chamber (61) into fluid flow communication with the second chamber (62), the deployment device (20) having a shutter (70) for shutting the channel (63).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Buoyancy system for an aircraft


    Beteiligte:
    DELORME LOUIS (Autor:in) / LAMARCHE NICOLAS (Autor:in) / AYACHE DAVID (Autor:in) / CERTAIN BERNARD (Autor:in)

    Erscheinungsdatum :

    03.01.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Buoyancy system for aircraft, and aircraft

    BERNARD CERTAIN / DAVID AYACHE / NICOLAS LAMARCHE et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Buoyancy system for aircraft, and aircraft

    NICOLAS DIJAUX | Europäisches Patentamt | 2015

    Freier Zugriff

    Electric buoyancy aircraft

    DU JIAN | Europäisches Patentamt | 2020

    Freier Zugriff

    Photovoltaic buoyancy aircraft

    LYU HUAIMIN / LYU SHEN | Europäisches Patentamt | 2015

    Freier Zugriff

    AIRCRAFT PROVIDED WITH A BUOYANCY SYSTEM, AND A BUOYANCY METHOD

    DELORME LOUIS / PRUD'HOMME LACROIX PIERRE | Europäisches Patentamt | 2018

    Freier Zugriff