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, the ductless fan defining a plurality of fan wakes; and a pylon fairing connecting the ductless turbofan engine to the wing assembly, the pylon fairing defining pylon fairing curved blades, where the pylon fairing curved blades are in a direction opposite to an associated shear profile when incoming fan flow swirls and fan wake flow reach the pylon leading edge.

    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无管道风扇,无管道风扇限定多个风扇尾流;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,吊架整流罩限定吊架整流罩弯叶片,其中吊架整流罩弯叶片在与进入风扇流旋流和风扇尾流到达吊架前缘时的相关联的剪切轮廓相对的方向上。


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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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