An integrated drain mast structure for use in draining fluids emanating from aircraft components, such as turbine engines and fuselages, for facilitating the detection of fluids leaking from said components. A self-supporting tube section including a plurality of generally aligned fluid passages each having a peripheral wall, at least a portion of which is common with at least a portion of another aligned adjacent fluid passage is connected to one or more of these aircraft components. An aerodynamic fairing includes a plurality of fairing fluid passages each connected to a respective fluid passage of the tube section and having respective fluid outlets. The tube section and fairing section can comprise a single integral structure.


    Access

    Download


    Export, share and cite



    Title :

    Integrated drain mast structure


    Contributors:

    Publication date :

    2020-07-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    INTEGRATED DRAIN MAST STRUCTURE

    PARKER MATTHEW / MISTRY SHAILESH / POSSERT ERIC | European Patent Office | 2024

    Free access

    INTEGRATED DRAIN MAST STRUCTURE

    PARKER MATTHEW / MISTRY SHAILESH / POSSERT ERIC | European Patent Office | 2019

    Free access

    INTEGRATED DRAIN MAST STRUCTURE

    PARKER MATTHEW J / MISTRY SHAILESH N / POSSERT ERIC M | European Patent Office | 2019

    Free access

    INTEGRATED DRAIN MAST STRUCTURE

    PARKER MATTHEW / MISTRY SHAILESH / POSSERT ERIC | European Patent Office | 2023

    Free access

    Drain mast

    LÜBBERT TIM / REMPE MICHAEL / SCHNEIDER FRANK | European Patent Office | 2024

    Free access