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 an aft end (17) of the aircraft, and an engine (30) comprising an air inlet (31) forming an opening in the skin (15) and an air outlet (32) forming another opening in the skin (15), said engine being located in an aft fuselage section, the exhaust port (32) is located in front of the intake port (31) in the longitudinal direction (39).

    本发明涉及一种飞行器(41),该飞行器(41)包括机身(14)和发动机(30),机身(14)包括蒙皮(15)并且沿着纵向轴线(39)从飞行器的前端部延伸至后端部(17),发动机(30)包括在蒙皮(15)中形成开口的进气口(31)以及在蒙皮(15)中形成另一开口的排气口(32),所述发动机位于后部机身部段中,其中,排气口(32)沿着纵向方向(39)位于进气口(31)的前方。


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    Titel :

    Aircraft having combustion engine with exhaust port in front of its intake port


    Weitere Titelangaben:

    具有在其进气口前方带有排气口的燃烧发动机的飞行器



    Erscheinungsdatum :

    2023-03-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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