A drive arrangement for an aircraft comprises a pair of propulsor units each having a fan and a fan shaft for driving the fan. A core engine has a turbine driving a core engine shaft. A mechanical connection connects the core engine shaft to drive the fan shafts for each of the propulsor units. An aircraft also has such an arrangement.


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    Titel :

    Double propulsor imbedded in aircraft tail with single core engine


    Beteiligte:
    SUCIU GABRIEL L (Autor:in) / CHANDLER JESSE M (Autor:in) / LORD WESLEY K (Autor:in) / EPSTEIN ALAN H (Autor:in) / O'FLARITY STEVEN M (Autor:in)

    Erscheinungsdatum :

    2019-09-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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