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; and a pylon fairing connecting the ductless turbofan engine to the wing assembly, the pylon fairing defining a length direction, a leading edge, a trailing edge, and a chord extending from the leading edge to the trailing edge, the pylon fairing including a maximum thickness portion along the length direction of the pylon fairing located between 10% and 60% of the chord.

    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;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,吊架整流罩限定长度方向、前缘、后缘和从前缘延伸到后缘的弦,吊架整流罩包括位于弦的10%和60%之间的沿着吊架整流罩的长度方向的最大厚度部分。


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    Title :

    Open rotor hanger fairing


    Additional title:

    开式转子吊架整流罩



    Publication date :

    2024-07-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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