An aircraft (10) including a fuselage (20) and an aft engine (200) is provided. The fuselage (20) extends from a forward end of the aircraft (10) towards an aft end (16) of the aircraft (10). The aft engine (200) is mounted to the fuselage (20) proximate the aft end (16) of the aircraft (10). The aft engine (200) includes a fan (222) rotatable about a central axis (220) of the aft engine (200), the fan (222) including a plurality of fan blades (228). The aft engine (200) also includes a nacelle (224) surrounding the plurality of fan blades (228) and defining an inlet (244). The inlet (244) defines a non-axis symmetric shape with respect to the central axis (220) of the aft engine (200) to, e.g., allow for a maximum amount of airflow into the aft engine (200).


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    Titel :

    NON-AXIS SYMMETRIC AFT ENGINE


    Weitere Titelangaben:

    NICHTACHSSYMMETRISCHER HINTERER MOTOR
    MOTEUR AFT À AXE NON SYMÉTRIQUE


    Beteiligte:

    Erscheinungsdatum :

    26.10.2022


    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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