The invention provides a dual-drive flap control system and method, and belongs to the technical field of aviation systems, a first power drive device and a first mechanical line system form a first actuating system for controlling outer flaps on the left side and the right side, and a second power drive device and a second mechanical line system form a second actuating system for controlling inner flaps on the left side and the right side; the flap control computer calculates a flap control instruction according to the expected flap configuration position and the flap real-time position fed back by the first mechanical line system and the second mechanical line system, and sends the flap control instruction to the first power driving device and the second power driving device; the first power driving device moves, drives the first mechanical line system to move and controls the outer side flap to move; the second power driving device moves, drives the second mechanical line system to move and controls the inner side flap to move; according to the invention, the function availability of the high-lift system is improved, and the task reliability is higher.
本发明提供一种双驱动襟翼控制系统及控制方法,属于航空系统技术领域,第一动力驱动装置和第一机械线系统组成控制左右两侧外襟翼的第一作动系统,第二动力驱动装置和第二机械线系统组成控制左右两侧内襟翼的第二作动系统,襟翼控制计算机根据期望的襟翼构型位置和第一、第二机械线系统反馈的襟翼实时位置解算襟翼控制指令,并发送襟翼控制指令给第一动力驱动装置和第二动力驱动装置;第一动力驱动装置运动并带动第一机械线系统运动并控制外侧襟翼运动;第二动力驱动装置运动并带动第二机械线系统运动并控制内侧襟翼运动;本发明提高了高升力系统的功能可用性,任务可靠性更高。
Dual-drive flap control system and control method
一种双驱动襟翼控制系统及控制方法
2024-10-15
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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