A fairing for a wing mounted engine, an aircraft comprising a wing having a longitudinal centerline axis, a leading edge, a trailing edge behind the leading edge, a wing thickness and a wing chord, an engine having a longitudinal axis vertically aligned with the wing chord and parallel to the longitudinal centerline axis, a pylon, and a fairing, a pylon connects the wing to the engine, and a fairing is received over the pylon. The fairing defines a horizontal plane, a first plane perpendicular to the longitudinal axis, and a second plane perpendicular to the longitudinal axis, the second plane behind the first plane, the longitudinal axis defining a reference line when projected onto the horizontal plane. The fairing includes a fairing body defining an aerodynamic surface having an outboard portion and an inboard portion, the inboard portion configured such that a first plane intersects a horizontal plane and the aerodynamic surface of the inboard portion at a first intersection point. The first intersection is laterally displaced by a first distance from the reference line. The second plane intersects the horizontal plane and the aerodynamic surface of the inboard portion at a second intersection point. The second intersection is laterally displaced by a second distance from the reference line. The second distance is greater than the first distance.

    用于机翼安装的发动机的整流罩,飞机包括机翼、发动机、挂架和整流罩,机翼具有纵向中心线轴线、前缘、在前缘后面的后缘、机翼厚度和机翼翼弦,发动机具有与机翼翼弦竖直对齐并平行于纵向中心线轴线的纵向轴线,挂架将机翼连接到发动机,整流罩被接收在挂架上方。整流罩限定水平平面、垂直于纵向轴线的第一平面和垂直于纵向轴线的第二平面,第二平面在第一平面的后面,纵向轴线在投影到水平平面上时限定参考线。整流罩包括整流罩主体,其限定具有外侧部分和内侧部分的空气动力学表面,内侧部分被配置为使得第一平面在第一交点处与水平平面和内侧部分的空气动力学表面相交。第一交点从参考线横向位移第一距离。第二平面在第二交点处与水平平面和内侧部分的空气动力学表面相交。第二交点从参考线横向位移第二距离。第二距离大于第一距离。


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    Titel :

    Fairing for wing-mounted engine


    Weitere Titelangaben:

    用于机翼安装的发动机的整流罩


    Beteiligte:
    SPINGHOW (Autor:in) / ZCC HOISINGTON (Autor:in)

    Erscheinungsdatum :

    2023-09-08


    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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