Disclosed is flap support (11) for supporting a flap (9) of a wing (5) for an aircraft (1), the flap support (11) comprising a load bearing fairing shell (13) and a reinforcement structure (31) at least partially received in the interior space (27) of the fairing structure (13) and mounted to the first and second side wall portions(21, 23) of the fairing shell (13), wherein the fairing shell (13) comprises a front attachment device (33) configured for attachment to a main wing (7), wherein the reinforcement structure (31) comprises an aft attachment device (63) configured for attachment to the main wing (7), and wherein the flap support (11) further comprises a hinge device (39) configured for forming an articulated connection to the flap (9). The object, to provide a particularly strong and at the same time lightweight flap support, is achieved in that the hinge device (39) forms part of the reinforcement structure (31).

    公开了一种用于对用于飞行器(1)的机翼(5)的襟翼(9)进行支承的襟翼支承件(11),该襟翼支承件(11)包括承受载荷的整流壳(13)并且包括加强结构(31),该加强结构被至少部分地接纳在整流结构(13)的内部空间(27)中并且安装至整流壳(13)的第一侧壁部分(21)和第二侧壁部分(23),其中,整流壳(13)包括构造成用于附接至主翼(7)的前附接装置(33),其中,加强结构(31)包括构造成用于附接至主翼(7)的后附接装置(63),并且其中,襟翼支承件(11)还包括铰接装置(39),该铰接装置构造成用于形成与襟翼(9)的铰接连接。通过使铰接装置(39)形成加强结构(31)的一部分而实现了提供特别坚固且同时轻量的襟翼支承件的目的。


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    Title :

    FLAP SUPPORT FOR SUPPORTING FLAP OF WING FOR AIRCRAFT


    Additional title:

    用于对飞行器机翼的襟翼进行支承的襟翼支承件


    Contributors:

    Publication date :

    2021-04-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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