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 and including a leading edge section defining a leading edge arc that varies along the length direction of the pylon fairing.

    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并且包括前缘区段,前缘区段限定前缘弧,前缘弧沿着吊架整流罩的长度方向变化。


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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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