个人信息Personal Information
副教授
博士生导师
硕士生导师
性别:男
毕业院校:北京航空航天大学
学位:博士
所在单位:力学与航空航天学院
学科:飞行器设计. 航空航天力学与工程. 工程力学
办公地点:综合实验1号楼409B
联系方式:+86 411 84706213
电子邮箱:yangl@dlut.edu.cn
The Performance of a Surface-bonded PZT Sensor Based Rocket Tanks SHM System under the Cryogenic Temperature Operating Environment
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论文类型:会议论文
发表时间:2015-01-01
收录刊物:CPCI-S
页面范围:2945-2953
摘要:A series of tests have been conducted to determine the survivability and functionality of a PZT sensor-based guide wave structural health monitoring (GWSHM) technology under the operating conditions of typical liquid rocket tanks such as cryogenic temperature. The performance of a typical piezoelectric sensor (PZT-5A) and different low temperature adhesives under cryogenic temperature was first investigated. The GWSHM sensor system for liquid rocket tanks was exposed to flight various environments from room temperature (10 degrees C) to cryogenic temperature (-180 degrees C) to evaluate the physical robustness of the sensor- adhesives system as well as operational survivability and functionality. Test results demonstrated that the developed sensors system can withstand operational levels of vibration and shock energy on a representative rocket tanks duct assembly, and is functional under the combined cryogenic temperature and vibration environment.