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).


    Access

    Download


    Export, share and cite



    Title :

    FLUID DISCHARGE SYSTEM


    Contributors:

    Publication date :

    2025-02-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    FLUID DISCHARGE SYSTEM

    SUZUKI YASUNORI | European Patent Office | 2020

    Free access

    A FLUID DISCHARGE SYSTEM

    GOKMEN ERKAN | European Patent Office | 2023

    Free access

    FLUID DISCHARGE DEVICE

    KOMATSUBARA YUSUKE / NINOMIYA HITOSHI / NAKAMURA TAKAHITO et al. | European Patent Office | 2021

    Free access

    FLUID DISCHARGE APPARATUS

    KOMATSUBARA YUSUKE / NINOMIYA HITOSHI / NAKAMURA TAKAHITO et al. | European Patent Office | 2019

    Free access

    Fluid discharge device

    KOMATSUBARA YUSUKE / NINOMIYA HITOSHI / NAKAMURA TAKAHITO et al. | European Patent Office | 2024

    Free access