An over-pressure vent (OPV) system (150) is provided for a fuel tank (102) of an aircraft (800). The OPV system (150) includes an OPV valve (152) configured to be coupled in fluid communication with a supply line (104) of a nitrogen enriched air distribution system (NEADS) (100) such that the OPV valve (152) is configured to vent pressure from the supply line (104). The OPV valve (152) is configured to be coupled in fluid communication with the supply line (104) upstream from an outlet (136) of the supply line (104) from which the NEADS (100) delivers nitrogen enriched gas to the fuel tank (102). The OPV valve (152) is configured to sense a pressure within the supply line (104) upstream from the outlet (136) of the supply line (104).


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    Titel :

    OVER-PRESSURE VENT SYSTEM FOR AN AIRCRAFT FUEL TANK


    Weitere Titelangaben:

    ÜBERDRUCKENTLÜFTUNGSSYSTEM FÜR EINEN FLUGZEUGKRAFTSTOFFTANK
    SYSTÈME D'ÉVENT DE SURPRESSION POUR RÉSERVOIR DE CARBURANT D'AÉRONEF


    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 :

    13.09.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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