The invention relates to an aircraft (41) comprising a fuselage (14) comprising a skin (15) and extending along a longitudinal axis (39) from a front end to a rear end (17) of the aircraft, and an engine (30) comprising an air intake (31) forming an opening in the skin (15), as wells as an exhaust (32) forming another opening in the skin (15), said engine being located in a rear fuselage section, in which the exhaust (32) is situated ahead of the air intake (31) along the longitudinal direction (39).


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    Titel :

    AIRCRAFT WITH A COMBUSTION ENGINE HAVING AN EXHAUST AHEAD OF ITS AIR INTAKE


    Weitere Titelangaben:

    FLUGZEUG MIT EINER BRENNKRAFTMASCHINE MIT EINEM AUSPUFF VOR SEINEM LUFTEINLASS
    AÉRONEF ÉQUIPÉ D'UN MOTEUR À COMBUSTION INTERNE AYANT UN ÉCHAPPEMENT EN AVANT DE SON ADMISSION D'AIR


    Beteiligte:

    Erscheinungsdatum :

    2024-05-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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