CAJ | 학술논문

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。
설계료비궤결구건강감공모의가재시험계통，포괄가재평태계통、대응변측시정도시험험증모괴화관건부위모의시험모괴，용우연구전감기부설방법대측시정도적영향，위광섬전감기술재비궤결구감측중적응용연구제공기술기출화이론의거。
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.