A propulsion assembly for an aircraft, which has a propulsion system with a combustion chamber surrounded by a casing, a supply pipe that conveys dihydrogen to the combustion chamber through the casing via injectors, and a housing fastened to the casing in a sealed manner around the latter, wherein the supply pipe has a downstream part housed inside the housing and wherein the injectors are also housed inside the housing.


    Access

    Download


    Export, share and cite



    Title :

    ENSEMBLE PROPULSIF POUR AÉRONEF


    Additional title:

    PROPULSION ASSEMBLY FOR AIRCRAFT
    ANTRIEBSEINHEIT FÜR EIN FLUGZEUG


    Contributors:

    Publication date :

    2025-07-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    ENSEMBLE PROPULSIF POUR AÉRONEF

    CZAPLA LIONEL / VARDELLE EMMANUEL | European Patent Office | 2024

    Free access

    ENSEMBLE PROPULSIF POUR AERONEF

    HURLIN HERVE / CARUEL PIERRE | European Patent Office | 2016

    Free access

    ENSEMBLE PROPULSIF POUR AÉRONEF

    CZAPLA LIONEL / AMARGIER RÉMI | European Patent Office | 2025

    Free access

    ENSEMBLE PROPULSIF POUR AERONEF

    FAUGERAS JOSE | European Patent Office | 2022

    Free access

    ENSEMBLE PROPULSIF POUR AÉRONEF

    FAUGERAS JOSE | European Patent Office | 2018

    Free access