A supply system for an aircraft arranged between two dihydrogen tanks and an engine. The supply system includes a supply module that assures the flow of dihydrogen between the tanks and an outlet pipe and two heaters mounted in series on a main pipe connected to the engine. The supply system also includes a network of pipes and solenoid valves that, in the event of a problem in one of the components of the supply system, enable dihydrogen to be redirected so as to reach the engine. Also an aircraft with such a supply system.


    Access

    Download


    Export, share and cite



    Title :

    Dihydrogen supply system for an aircraft engine


    Contributors:

    Publication date :

    2024-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / 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 | 2025

    Free access

    DIHYDROGEN SUPPLY SYSTEM FOR AN AIRCRAFT ENGINE

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

    Free access

    MODULE FOR A DIHYDROGEN SUPPLY SYSTEM FOR AN AIRCRAFT ENGINE

    MILLIERE JÉRÔME / CZAPLA LIONEL / PISSAVIN ALEXIS | 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

    Aircraft with dihydrogen-based cooling system and engine

    ZERBIAN MICHAEL / BERGERET DANIEL | European Patent Office | 2022

    Free access