An aircraft propulsion system (10) comprises first and second propulsors (13a, 13b). An epicyclic reduction gearbox (25) is coupled to an input shaft (24). The reduction gearbox (25) comprises a sun gear (27) coupled to the input shaft (24), a plurality of planet gears (28) which mesh with the sun gear (27) and are mounted to a planet carrier (30), and a ring gear (29) which meshes with the plurality of planet gears (28). The first propulsor (13a) is located upstream of the second propulsor (13b). The first propulsor (13a) is coupled to the sun gear (27), and the second propulsor (13b) is coupled to one of the planet carrier (30) and the ring gear (29).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft propulsion system


    Erscheinungsdatum :

    2018-10-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    AIRCRAFT PROPULSION SYSTEM

    TASKER RICHARD / RIX ANDREW | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft propulsion system

    Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft propulsion system

    SWANN PETER | Europäisches Patentamt | 2019

    Freier Zugriff

    Aircraft propulsion system

    Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft propulsion system

    PETER SWANN | Europäisches Patentamt | 2018

    Freier Zugriff