An aircraft (100) equipped with a distributed unducted fan propulsion system (150) is provided. In one aspect, an aircraft (100) includes a body (102) defining a lateral centerline that separates the body (102) into a first side (114) and a second side (116). One or more first unducted fans (162A) are mounted to the first side (114) of the body (102). The one or more first unducted fans (162A) are rotatable in a first direction. One or more second unducted fans (172A) are mounted to the second side (116) of the body (102). The one or more second unducted fans (172A) are rotatable in a second direction that is opposite the first direction.


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    Titel :

    AIRCRAFT EQUIPPED WITH A DISTRIBUTED COUNTERROTATING UNDUCTED FAN PROPULSION SYSTEM


    Weitere Titelangaben:

    FLUGZEUG MIT VERTEILTER GEGENLÄUFIGER DIFFUSER GEBLÄSEANTRIEBSANLAGE
    AÉRONEF ÉQUIPÉ D'UN SYSTÈME DE PROPULSION À SOUFFLANTE NON CARÉNÉE À CONTRE-ROTATION RÉPARTI


    Beteiligte:

    Erscheinungsdatum :

    2022-03-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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