An aircraft propulsion system comprises first and second propulsors. An epicyclic reduction gearbox is coupled to an input shaft. The reduction gearbox comprises a sun gear coupled to the input shaft, a plurality of planet gears which mesh with the sun gear and are mounted to a planet carrier, and a ring gear which meshes with the plurality of planet gears. The first propulsor is located upstream of the second propulsor The first propulsor is coupled to the sun gear, and the second propulsor is coupled to one of the planet carrier and the ring gear.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT PROPULSION SYSTEM


    Contributors:

    Publication date :

    2020-03-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / F16H Getriebe , GEARING



    AIRCRAFT PROPULSION SYSTEM

    YANG JINGBIN | European Patent Office | 2024

    Free access

    AIRCRAFT PROPULSION SYSTEM

    KITA AKINORI / MATSUMOTO TAKESHI | European Patent Office | 2023

    Free access

    Aircraft propulsion system

    HARVEY GILES E | European Patent Office | 2022

    Free access

    AIRCRAFT PROPULSION SYSTEM

    KITA AKINORI / MATSUMOTO TAKESHI / TSUTSUMI DAIKO | European Patent Office | 2022

    Free access

    AIRCRAFT PROPULSION SYSTEM

    KITA AKINORI / MATSUMOTO TAKESHI / TSUTSUMI DAIKO | European Patent Office | 2022

    Free access