An aircraft propulsion system is provided that includes a turbine engine and an exhaust gas condenser. The exhaust gas condenser includes a housing, a nozzle, inlet and outlet air scoops, and an exhaust gas conduit bank. The housing has an interior cavity, top and bottom sides, and first and second lateral sides. The exhaust gas conduit bank is disposed in the interior cavity of the housing. The exhaust gas conduit bank includes a plurality of exhaust gas conduits and bypass air passages that are disposed in an alternating configuration. The exhaust gas conduits extend axially between the forward and aft ends, are open at the forward end and at the nozzle. The bypass air passages receive bypass air from the inlet air scoop and direct the bypass air laterally across the condenser to the outlet air scoop.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft propulsion system with turbine engine and exhaust condenser


    Beteiligte:
    SMITH SCOTT (Autor:in) / STRATTON RUSSELL (Autor:in)

    Erscheinungsdatum :

    03.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST CONDENSER

    SMITH SCOTT / STRATTON RUSSELL | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft propulsion system with turbine engine and exhaust condenser

    SMITH SCOTT / STRATTON RUSSELL | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft propulsion system with turbine engine and exhaust condenser

    SMITH SCOTT / STRATTON RUSSELL | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST CONDENSER

    SMITH SCOTT / STRATTON RUSSELL | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM WITH TURBINE ENGINE AND EXHAUST CONDENSER

    SMITH SCOTT / STRATTON RUSSELL | Europäisches Patentamt | 2024

    Freier Zugriff