This invention relates to a body (2) located on the aircraft, at least one tank (T) located on the body (2) and allows fuel accumulation, at least one valve (3) that allows the water accumulated in the tank (T) to be discharged out of the body (2), at least one fastener (4) that enables the valve (3) to be mounted on the body (2), and a shell(S) located on the air-contacting surface of the body (2).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FLUID DISCHARGE SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    20.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    FLUID DISCHARGE SYSTEM

    SUZUKI YASUNORI | Europäisches Patentamt | 2020

    Freier Zugriff

    A FLUID DISCHARGE SYSTEM

    GOKMEN ERKAN | Europäisches Patentamt | 2023

    Freier Zugriff

    FLUID DISCHARGE DEVICE

    KOMATSUBARA YUSUKE / NINOMIYA HITOSHI / NAKAMURA TAKAHITO et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Fluid discharge device

    KOMATSUBARA YUSUKE / NINOMIYA HITOSHI / NAKAMURA TAKAHITO et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Fluid discharge device

    KOMATSUBARA YUSUKE / NINOMIYA HITOSHI / NAKAMURA TAKAHITO et al. | Europäisches Patentamt | 2022

    Freier Zugriff