A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. In one illustrative embodiment, an apparatus includes a transport member. The transport member is configured for use in the fluid transport system. The transport member includes a material configured to reduce voltages and currents, induced in response to an electromagnetic event, along the transport member.


    Access

    Download


    Export, share and cite



    Title :

    Composite tubes for a fluid transport system



    Publication date :

    2020-04-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60R Fahrzeuge, Fahrzeugausstattung oder Fahrzeugteile, soweit nicht anderweitig vorgesehen , VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR / B63B Schiffe oder sonstige Wasserfahrzeuge , SHIPS OR OTHER WATERBORNE VESSELS / F16L PIPES , Rohre / F17D Rohrleitungssysteme , PIPE-LINE SYSTEMS / H05F STATIC ELECTRICITY , Statische Elektrizität



    Composite tubes for a fluid transport system

    JOHNSON BENJAMIN A / IRWIN JAMES PATRICK / MINTEER DAVID WILLIAM et al. | European Patent Office | 2021

    Free access

    Composite tubes for a fluid transport system

    IRWIN JAMES PATRICK / MINTEER DAVID WILLIAM / AXTELL JOHN THOMAS et al. | European Patent Office | 2017

    Free access

    COMPOSITE TUBES FOR A FLUID TRANSPORT SYSTEM

    European Patent Office | 2020

    Free access

    Composite Tubes for a Fluid Transport System

    IRWIN JAMES PATRICK / MINTEER DAVID WILLIAM / AXTELL JOHN THOMAS et al. | European Patent Office | 2017

    Free access

    COMPOSITE TUBES FOR A FLUID TRANSPORT SYSTEM

    IRWIN JAMES PATRICK / MINTEER DAVID WILLIAM / AXTELL JOHN THOMAS et al. | European Patent Office | 2017

    Free access