The invention relates to a motion mechanism of a trailing edge of a flexible wing, comprising a support mounted on the flexible wing; the first end of the main connecting rod is pivotally connected to the support, the second end of the main connecting rod is pivotally connected to the rear edge moving part of the rear edge, and the transmission part section is fixedly connected to the main connecting rod; the rocker arm is provided with a first connecting point, so that the rocker arm can pivot relative to the first connecting point, and the transmission part section is connected with the rocker arm in a pivoted mode at a second connecting point of the rocker arm; one end of the constraint connecting rod is pivotally connected to the support, and the other end of the constraint connecting rod is pivotally connected to the rocker arm at a first connecting point of the rocker arm; the first end of the side connecting rod is pivotally connected with the rocker arm at a third connecting point of the rocker arm, the second end of the side connecting rod is pivotally connected to the rear edge movable part of the rear edge, and the distance between the second connecting point and the first connecting point is smaller than that between the third connecting point and the first connecting point.
本发明涉及一种柔性机翼的后缘的运动机构,包括支座,该支座安装在柔性机翼上;主连杆,其第一端可枢转地连接于支座,并且第二端可枢转地连接于后缘的后缘活动件,传动部段,该传动部段固定地连接于主连杆;摇臂,该摇臂具有第一连接点,使得摇臂能相对于第一连接点枢转,并且传动部段在摇臂的第二连接点处与摇臂可枢转地连接;约束连杆,该约束连杆的一端可枢转地连接于支座,并且约束连杆的另一端在摇臂的第一连接点处可枢转地连接于摇臂;以及侧连杆,其第一端在摇臂的第三连接点处与摇臂可枢转地连接,并且第二端可枢转地连接于后缘的后缘活动件,其中,第二连接点与第一连接点之间的距离小于第三连接点与第一连接点之间的距离。
Movement mechanism for trailing edge of flexible wing
一种用于柔性机翼的后缘的运动机构
08.12.2023
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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