A disclosed aircraft propulsion system includes a gas turbine engine supported within an aircraft fuselage, a main drive driven by the gas turbine engine and an open rotor propeller system supported outside of the aircraft fuselage separately from the gas turbine engine. A secondary drive that is driven by the main drive drives the open rotor propeller system.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    CONTRA-ROTATING OPEN ROTOR DISTRIBUTED PROPULSION SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    08.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Contra-rotating open rotor distributed propulsion system

    VEILLEUX JR LEO J / RIBAROV LUBOMIR A | Europäisches Patentamt | 2017

    Freier Zugriff

    Contra-rotating open rotor distributed propulsion system

    VEILLEUX JR LEO J / RIBAROV LUBOMIR A | Europäisches Patentamt | 2016

    Freier Zugriff

    CONTRA-ROTATING OPEN FAN PROPULSION SYSTEM

    GOLSHANY SINA S / HUNTLY DAVID MILES / BLOM ADRIANA W et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Contra-rotating open fan propulsion system

    GOLSHANY SINA S / HUNTLY DAVID MILES / BLOM ADRIANA W et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Contra-rotating open fan propulsion system

    GOLSHANY SINA S / HUNTLY DAVID MILES / BLOM ADRIANA W et al. | Europäisches Patentamt | 2017

    Freier Zugriff