An aircraft is provided that defines a longitudinal centerline and extends between a forward end and an aft end. The aircraft includes a fuselage extending between a forward end of the aircraft and an aft end of the aircraft; a wing assembly extending laterally outward from a portion of the fuselage relative to the longitudinal centerline; a ductless turbofan engine, the ductless turbofan engine including a ductless fan defining a fan diameter; and a pylon fairing connecting the ductless turbofan engine to the wing assembly, the pylon fairing defining a leading edge and including a first inflection point along the leading edge, the first inflection point defining a first radius of curvature that is less than 5 times and greater than 0.1 times the fan diameter.

    提供了一种飞行器,飞行器限定纵向中心线并且在前端和后端之间延伸。飞行器包括:机身,机身在飞行器的前端和飞行器的后端之间延伸;机翼组件,机翼组件相对于纵向中心线从机身的一部分侧向向外延伸;无管道涡轮风扇发动机,无管道涡轮风扇发动机包括限定风扇直径的无管道风扇;和吊架整流罩,吊架整流罩将无管道涡轮风扇发动机连接到机翼组件,吊架整流罩限定前缘并且包括沿着前缘的第一拐点,第一拐点限定第一曲率半径,第一曲率半径小于风扇直径的5倍且大于风扇直径的0.1倍。


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    Titel :

    Open rotor hanger fairing


    Weitere Titelangaben:

    开式转子吊架整流罩



    Erscheinungsdatum :

    19.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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