襟翼驱动器输出加载系统建模与仿真  

Modeling and Simulation of the Flaps Actuator Output Loading System

作　　者：陈斌[1] 吴惠东[1] 于之靖[1] 

机构地区：[1]中国民航大学航空地面特种设备研究基地,天津300300

出　　处：《机床与液压》2017年第13期143-145,158,共4页Machine Tool & Hydraulics

摘　　要：介绍一套飞机襟翼驱动器的故障检测和性能测试系统,该系统采用比例阀控制液压马达,模拟襟翼驱动器的输出加载部分。并对它进行了数学建模和仿真,可以作为相关研究和实验的参考。A set of fault detection and performance testing system for aircraft flap actuator was introduced, in which the output loading part of the flap actuator was simulated through the hydraulic motor controlling proportional valve. The mathematical modeling and simulation were completed, which could be used as a reference for relevant researches and experiments.

关 键 词：襟翼驱动器 加载系统 阀控马达 建模和仿真 

分 类 号：TH137[机械工程—机械制造及自动化]