A module between a dihydrogen tank and an engine in an aircraft. The module comprises outer and inner boxes, a pipeline between the tank and the engine through the boxes, pressure limiters mounted on the pipeline and the inner box, an exhaust pipeline between the pressure limiters and the outside, shut-off valves mounted on the pipeline at the outer box, a detector for detecting a leak of the pipeline or of the outer box and a controller configured to control each shut-off valve as a function of the information delivered by the detector.


    Access

    Download


    Export, share and cite



    Title :

    MODULE FOR A DIHYDROGEN SUPPLY SYSTEM FOR AN AIRCRAFT ENGINE


    Contributors:

    Publication date :

    2024-09-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Dihydrogen supply system for an aircraft engine

    MARTIN PIERRE-OLIVIER / CZAPLA LIONEL / BELLEVILLE MATHIEU | European Patent Office | 2024

    Free access

    Dihydrogen supply system for an aircraft engine

    MARTIN PIERRE-OLIVIER / CZAPLA LIONEL / BELLEVILLE MATHIEU | European Patent Office | 2025

    Free access

    DIHYDROGEN SUPPLY SYSTEM FOR AN AIRCRAFT ENGINE

    MARTIN PIERRE-OLIVIER / CZAPLA LIONEL / BELLEVILLE MATHIEU | European Patent Office | 2024

    Free access

    AIRCRAFT COMPRISING A DIHYDROGEN SUPPLY SYSTEM AND A DIHYDROGEN HEAT TREATMENT SYSTEM

    MILLIERE JÉRÔME / VERSEUX OLIVIER / LANDOLT JONATHAN et al. | European Patent Office | 2025

    Free access

    MODULE FOR AIRCRAFT COMPRISING A DIHYDROGEN PROCESSING SYSTEM

    MILLIERE JÉRÔME / CZAPLA LIONEL / JOUBERT ROMAIN | European Patent Office | 2025

    Free access