飞机结构健康监控模拟加载试验系统的设计

Design of Simulated Loading Test System for Aircraft Structure Health Monitoring

设计了飞机结构健康监控模拟加载试验系统,包括加载平台系统、大应变测试精度试验验证模块和关键部位模拟试验模块,用于研究传感器敷设方法对测试精度的影响,为光纤传感技术在飞机结构监测中的应用研究提供技术基础和理论依据。

The simulated loading test system for aircraft structure health monitoring was designed. The system consists of loading terrace system, large strain testing accuracy verification module, and key part simulated test module. The system can be used in studying influence of laying method of sensor on test accuracy. The purpose was to provide technique basis, theory and technique for application of fiber-optical sensor techniques in aircraft structure health monitoring.