The invention discloses a wing deformation folding transmission locking mechanism, and particularly relates to the field of aircrafts. Comprising two fixing bases, the two fixing bases are connected with a main wing butt joint beam through bolts, a sliding groove is formed between the two fixing bases, a locking sliding block is slidably connected into the sliding groove, a first limiting block is integrally formed on one side of the locking sliding block, and a driving assembly used for driving the locking sliding block to slide is arranged on the locking sliding block; a rotating shaft is rotationally connected between the two fixing bases, a second limiting block is arranged on one side of the rotating shaft, a fixing plate is integrally formed on one side of the rotating shaft and is in bolted connection with the aileron butt-joint cross beam, a connecting shaft block is arranged on the other side of the fixing plate, and a folding driving piece is slidably connected to the connecting shaft block; a rotating assembly installed on the fixed base is arranged on the folding driving piece and used for driving the folding driving piece to rotate. By the adoption of the technical scheme, the problem that an existing airplane occupies space in the transportation process is solved, and the space occupied by the airplane in the transportation process can be reduced.
本发明专利公开了一种机翼变形折叠传动锁定机构,具体涉及飞行器领域。包括两个固定底座,两个固定底座与主翼对接横梁螺栓连接,两个固定底座之间设有滑槽,滑槽内滑动连接有锁定滑块,锁定滑块的一侧一体成型有第一限位块,锁定滑块上设有用于驱动锁定滑块滑动的驱动组件,两个固定底座之间转动连接有转轴,转轴的一侧设有第二限位块,转轴的一侧一体成型有固定板,固定板与副翼对接横梁螺栓连接,固定板的另一侧设有连接轴块,连接轴块上滑动连接有折叠驱动件,折叠驱动件上设有安装在固定底座上的转动组件,转动组件用于带动折叠驱动件转动。采用本发明技术方案解决了现有的飞机在运输途中占用空间的问题,有利于减小飞机运输途中所占用的空间。
Wing deformation folding transmission locking mechanism
一种机翼变形折叠传动锁定机构
2024-12-24
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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