A fuel tank (102) system for an aircraft has a vent system. The system has a conduit opening (108) into the fuel section. The system has a member (122) connected to the conduit (104) at a proximal end. The member has a seal plate (132) within the conduit (104) sealing the opening (108) into the fuel section when a buoyant section at a distal end rises along with the seal plate through the member (122) with a rise in fluid (124) level within the fuel section.


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    Title :

    Pressure regulating float valve


    Additional title:

    Druckregelschwimmerventil
    Soupape à flotteur de régulation de pression


    Contributors:

    Publication date :

    2020-03-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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