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Wing flap mechanism for adjusting an aerodynamic wing flap associated with a wing

机译:机翼襟翼机构,用于调节与机翼相关的空气动力学机翼襟翼

摘要

A wing flap mechanism for adjusting an aerodynamic wing flap (3), in particular a lift flap, assigned to a wing (1) by means of a drive device (10), the wing flap mechanism being attached to at least one of a plurality of flap beams (5) fastened to the wing (1) is mounted, wherein the wing flap mechanism for load-bearing and kinematic guidance of the wing flap (3) comprises an actuating device (4), wherein the actuating device (4) designed as a crank gear mechanism (12), wherein the transmission device (12) two mutually adjacent joints on the flap carrier (5) and is preferably designed as a four-bar linkage and wherein the actuating device (4) acted upon driving means (10) with a about a drive axis (13) rotating drive arm (14) is provided, characterized in that the wing flap (2) on a Klappenst cap (15) is mounted such that the flap support (15) has a front, to the wing (1) indicative flap support portion (16) which is pivotally connected to the drive arm (14), and that the flap support (15) has a rear, from The wing (1) has rearwardly facing flap support portion (17) on which, the front flap support portion adjacent, a joint (21) is provided in which a steering lever (22) of the transmission device (12) is pivotally coupled.
机译:一种用于调节通过驱动装置(10)分配给机翼(1)的空气动力学机翼襟翼(3),尤其是升力襟翼的机翼襟翼机构,该机翼襟翼机构附接至多个机翼襟翼机构中的至少一个安装有固定在机翼(1)上的襟翼梁(5),其中用于承载和运动引导机翼襟翼(3)的机翼襟翼机构包括致动装置(4),其中致动装置(4)传动装置(12)构造为曲柄齿轮机构(12),其中,传动装置(12)在襟翼支架(5)上两个彼此相邻的接头,并且优选地设计为四连杆机构,其中,操纵装置(4)作用在驱动装置上(10)具有绕驱动轴(13)旋转的驱动臂(14),其特征在于,在Klappenst盖(15)上安装的机翼襟翼(2)使得襟翼支撑(15)的前部翼片指示翼片支撑部分(16)可枢转地连接到驱动臂(14),并且翼片支撑部分(15)具有后部,从机翼(1)具有向后的襟翼支撑部分(17),在该襟翼支撑部分(17)上,邻近前襟翼支撑部分,设有接头(21),其中变速器的转向杆(22)装置(12)可枢转地联接。

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