The invention belongs to the technical field of wing folding and flattening mechanism driving design, and particularly relates to a wing folding and flattening mechanism driving system and a control method thereof.The wing folding and flattening mechanism driving system comprises a hydraulic electromagnetic valve, an actuator cylinder, a fusiform valve, a high-pressure gas cylinder, an air pressure electromagnetic valve, an inflation valve and an in-place switch; the hydraulic electromagnetic valve is connected with a hydraulic source through an oil inlet pipeline and an oil return pipeline and is connected with a rod cavity and a rodless cavity of the actuating cylinder through pipelines, a fusiform valve is arranged on the pipeline for connecting the rod cavity and the rodless cavity, and a piston rod of the actuating cylinder is connected with the wing folding and flattening mechanism; the two fusiform valves are connected with a high-pressure gas cylinder through pipelines, and a gas pressure electromagnetic valve is arranged on the pipeline through which the two fusiform valves are connected with the high-pressure gas cylinder; the inflation valve is connected with a high-pressure gas cylinder through a pipeline and connected with a high-pressure gas source. The two in-place switches are connected to a cylinder body of the actuating cylinder and used for detecting whether the wings are folded and flattened in place or not.
本申请属于机翼折叠展平机构驱动设计技术领域,具体涉及一种机翼折叠展平机构驱动系统及其操控方法,其中,机翼折叠展平机构驱动系统,包括:液压电磁阀、作动筒、梭形活门、高压气瓶、气压电磁阀、充气活门、到位开关;液压电磁阀通过进油、回油管路连接液压源,以及通过管路连接作动筒的有杆腔、无杆腔,连接有杆腔、无杆腔的管路上设置梭形活门,作动筒的活塞杆连接机翼折叠展平机构;两个梭形活门通过管路连接高压气瓶,两个梭形活门连接高压气瓶的管路上设置气压电磁阀;充气活门通过管路连接高压气瓶,连接高压气源;到位开关有两个,连接在作动筒筒体上,分别用以检测机翼折叠、展平是否到位。
Wing folding and flattening mechanism driving system and control method thereof
一种机翼折叠展平机构驱动系统及其操控方法
2025-04-04
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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