The invention relates to the technical field of flight equipment, and provides a pedal adjusting structure and an aircraft pedal system. The pedal adjusting structure comprises a support; a left brake assembly and a right brake assembly are symmetrically arranged relative to the support, the right brake assembly comprises a right brake oil cylinder, a right brake pedal and a right connecting piece, the first end of the right brake oil cylinder is rotatably connected to the support, and the second end of the right brake oil cylinder is rotatably connected to the first end of the right brake pedal. The right connecting piece is connected with the second end of the right brake pedal and the support, and the support and the second end of the right brake pedal are both rotationally connected with the right connecting piece. And the driving assembly is installed on the support and connected with the right connecting piece, and the driving assembly is suitable for driving the right connecting piece to rotate. According to the pedal adjusting structure, the position of the brake pedal can be adjusted, the adjustable range between a driver and a pedal system is widened, and the requirements of more users can be met.
本申请涉及飞行设备技术领域,提供一种脚蹬调节结构及飞机脚蹬系统。脚蹬调节结构包括:支架;关于支架对称设置有左刹车组件和右刹车组件,右刹车组件包括右刹车油缸、右刹车踏板和右连接件,右刹车油缸的第一端可转动连接于支架,右刹车油缸的第二端可转动连接于右刹车踏板的第一端,右连接件连接右刹车踏板的第二端和支架,支架和右刹车踏板的第二端均与右连接件可转动连接;驱动组件,安装于支架,驱动组件与右连接件连接,驱动组件适于带动右连接件转动。根据本申请实施例的脚蹬调节结构,实现了刹车踏板的位置可调,增加了驾驶员与脚蹬系统之间的可调范围,可以满足更多用户的需求。
Pedal adjusting structure and airplane pedal system
脚蹬调节结构及飞机脚蹬系统
2024-07-30
Patent
Electronic Resource
Chinese
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