A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. The aerospace vehicle is operated. The fluid transport system in the aerospace vehicle is comprised of materials selected such that the fluid transport system has an electrical configuration. The intensity of the electrical discharge that occurs within the fluid transport system during operation of the aerospace vehicle is reduced to within selected tolerances by the electrical configuration of the fluid transport system.


    Access

    Download


    Export, share and cite



    Title :

    Fluid transport system for preventing electrical discharge



    Publication date :

    2015-10-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H05F STATIC ELECTRICITY , Statische Elektrizität / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16L PIPES , Rohre / F17D Rohrleitungssysteme , PIPE-LINE SYSTEMS



    FLUID TRANSPORT SYSTEM FOR PREVENTING ELECTRICAL DISCHARGE

    European Patent Office | 2020

    Free access

    FLUID TRANSPORT SYSTEM FOR PREVENTING ELECTRICAL DISCHARGE

    DAVID WILLIAM MINTEER / JAMES PATRICK IRWIN / BENJAMIN A JOHNSON et al. | European Patent Office | 2018

    Free access

    FLUID TRANSPORT SYSTEM FOR PREVENTING ELECTRICAL DISCHARGE

    MINTEER DAVID WILLIAM / IRWIN JAMES PATRICK / JOHNSON BENJAMIN A et al. | European Patent Office | 2017

    Free access

    FLUID TRANSPORT SYSTEM FOR PREVENTION OF ELECTRIC DISCHARGE

    MINTIER DEVID UILYAM / IRVIN DZHEJMS PATRIK / DZHONSON BENDZHAMIN A et al. | European Patent Office | 2018

    Free access