论文部分内容阅读
阐述典型飞机防滑刹车系统的组成和工作原理。利用AMESim高级建模和仿真平台构建了系统主要液压附件仿真模型,在此基础上构建了系统仿真模型。完成了系统动态压力响应仿真试验以及系统在各种跑道情况下的动力仿真试验。仿真结果表明:所建立的飞机防滑刹车系统仿真模型可行,能反映飞机制动系统的真实试验情况,也可以有效地验证整个制动系统的性能。
Describes the composition and working principle of typical aircraft anti-skid braking system. Using AMESim advanced modeling and simulation platform, a simulation model of the main hydraulic attachments of the system was built, and a system simulation model was built. The simulation of system dynamic pressure response and the dynamic simulation of the system under various runway conditions were completed. The simulation results show that the established simulation model of the aircraft anti-skid braking system is feasible, which can reflect the actual test situation of the aircraft braking system and can also effectively verify the performance of the entire braking system.