An over-pressure vent (OPV) system is provided for a fuel tank of an aircraft. The OPV system includes an OPV valve configured to be coupled in fluid communication with a supply line of a nitrogen enriched air distribution system (NEADS) such that the OPV valve is configured to vent pressure from the supply line. The OPV valve is configured to be coupled in fluid communication with the supply line upstream from an outlet of the supply line from which the NEADS delivers nitrogen enriched gas to the fuel tank. The OPV valve is configured to sense a pressure within the supply line upstream from the outlet of the supply line.


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    Titel :

    OVER-PRESSURE VENT SYSTEM FOR AN AIRCRAFT FUEL TANK


    Beteiligte:
    JOJIC IVANA (Autor:in) / JOHNSON TIMOTHY ANDREW (Autor:in) / JOHNSON ANDREW T (Autor:in) / RYAN DAVID A (Autor:in) / PILLA MELISSA A (Autor:in) / GIRI BIPIN (Autor:in) / ADKINS II DAVID ALLEN (Autor:in)

    Erscheinungsdatum :

    17.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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