A multi-spar lift surface (30) is disclosed that includes a multi-spar torsion box (32) having a corner reinforcement (25), a movable control surface, and an axial lever fitting (40). The movable control surface comprises a movable element (1), an articulated connection (6.1) linked to the movable element (1), and an axial lever (7) linking the articulated connection (6.1) to the rear spar (5) of the multi-spar torsion box (32). The axial rod fitting (40) is configured to connect the axial rod (7) with the multi-spar torsion box (32); and comprising a longitudinal profile (10) abutting against the rear spar (5), and a lug (20) joined at one end to the longitudinal profile (10) and at the other end to the axial rod (7); the lug (20) defines a plane comprising a longitudinal axis of the axial rod (7). The multi-spar lift surface (30) is capable of supporting lateral forces without any additional structure.

    披露了一种多翼梁升力面(30),该多翼梁升力面包括具有拐角加强部(25)的多翼梁抗扭箱(32)、可移动操纵面和轴向杆配件(40)。可移动操纵面包括可移动元件(1)、连结到可移动元件(1)的铰接连接件(6.1)、以及将铰接连接件(6.1)连结到多翼梁抗扭箱(32)的后翼梁(5)的轴向杆(7)。轴向杆配件(40)被配置成将轴向杆(7)与多翼梁抗扭箱(32)连结;并且包括抵靠后翼梁(5)的纵向型材(10)、以及在一端处连结到纵向型材(10)并且在另一端处连结到轴向杆(7)的凸耳(20);凸耳(20)限定包括轴向杆(7)的纵向轴线的平面。该多翼梁升力面(30)能够支撑侧向力而无需任何附加结构。


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    Titel :

    Multi-spar lifting surface


    Weitere Titelangaben:

    多翼梁升力面


    Beteiligte:

    Erscheinungsdatum :

    2023-06-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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