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airplane wing, airplane, flap system for an airplane wing, and method for adjusting the position of an airplane wing flap

机译:飞机机翼,飞机,飞机机翼的襟翼系统以及调节飞机机翼襟翼位置的方法

摘要

1/1 overview “airplane wing, airplane, wing flap system, and method for adjusting the position of a wing flap” an airplane wing comprises a main wing and a flap system that has a flap on the trailing edge of the main wing. an elongated flap tracking member is connected to the main wing in such a way that it can be moved substantially in its longitudinal direction and is guided by supporting bearing elements relative to the main wing between a retracted forward position and an extended backward position. the flap is rotatably connected to the rear end of the flap tracking member in such a way that it can rotate about a rotational geometry axis extending substantially parallel to the trailing edge of the main wing. , such that the flap moves together with the flap tracking member when the flap tracking member is moved and so that the flap can be rotated mechanically about the rotational axis. independent of flap tracking member movement. The flap system comprises an actuator system with two actuators. The first actuator is connected to the main wing and has a snap member that engages the flap or flap tracking member to move the flap together with the flap tracking member so that the flap tracking member is movable. between your retracted position and your extended position. The second actuator is connected to the flap tracking member so that the second actuator moves together with the flap tracking member when the flap tracking member is moved through the first actuator. The second actuator has a coupling member that engages the flap to rotate the flap around the rotational geometry axis.
机译:1/1概述“飞机机翼,飞机,机翼襟翼系统以及调节机翼襟翼位置的方法”飞机机翼包括主翼和襟翼系统,襟翼系统在主翼的后缘具有襟翼。细长的襟翼跟踪构件以这样的方式连接到主翼,即,该主翼可以基本上在其纵向方向上移动,并且由支撑轴承元件相对于主翼在回缩的向前位置和延伸的向后位置之间引导。襟翼可旋转地连接到襟翼跟踪构件的后端,使得其可以绕基本平行于主翼后缘延伸的旋转几何轴线旋转。因此,当襟翼跟踪构件移动时,襟翼与襟翼跟踪构件一起移动,并且使得襟翼能够绕旋转轴线机械地旋转。与襟翼跟踪成员的移动无关。襟翼系统包括具有两个致动器的致动器系统。第一致动器连接到主翼并且具有卡扣构件,该卡扣构件与襟翼或襟翼跟踪构件接合以使襟翼与襟翼跟踪构件一起移动,使得襟翼跟踪构件是可移动的。在缩回位置和伸展位置之间。第二致动器连接到襟翼跟踪构件,使得当襟翼跟踪构件移动通过第一致动器时,第二致动器与襟翼跟踪构件一起移动。第二致动器具有接合构件,该接合构件接合挡板以使挡板绕旋转几何轴线旋转。

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