李 峥1 ,任宗金 1 ,林山2 ,李新阳 1 ,张军1 ,张巍2.压电式推力矢量测试系统传感器设计[J].航空发动机,2025,51(6):169-173
压电式推力矢量测试系统传感器设计
Design of Piezoelectric Sensor-Based Vectored Thrust Measurement System
  
DOI:
中文关键词:  推力矢量测试  压电传感器  标定  压电式测试系统  航空发动机
英文关键词:vectored thrust measurement  piezoelectric sensor  calibration  piezoelectric measurement system  aeroengine
基金项目:国家自然科学基金(52075079)资助
作者单位
李 峥1 ,任宗金 1 ,林山2 ,李新阳 1 ,张军1 ,张巍2 1.大连理工大学 机械工程学院辽宁大连 116024 2.中国航发沈阳发动机研究所沈阳 110015 
摘要点击次数: 2006
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中文摘要:
      为实现新一代发动机对于高动态推力矢量的测试需求,基于6组件的多分量卧式推力矢量测试系统,提出压电3向力传 感器的矢量推力测试方法,设计3向压电传感器、刚性连接结构以及测试系统。采用理论建模与仿真计算相结合的方式分析压电 式推力矢量测试系统的力传递规律,得到每个传感器3个方向的力传递系数,从理论上验证了方案的可行性。通过仿真计算对传 感器位置极限受力进行分析,基于分析结果设计了压电传感器量程及尺寸。开发了压电传感器并进行了静态标定、动态标定及刚 度测量试验,结果表明:各传感器3个方向线性误差及重复性误差均在1%以内,3向固有频率高达8701.1、8789.06、8457.03 Hz, 3 向刚度分别为709.9、718.1、1538.4 kN/mm。传感器动静态特性好、刚度高,满足了动态推力矢量的测试需求。
英文摘要:
      To meet the testing requirements of dynamic vectored thrust measurement in next-generation engines,a vectored thrust measurement method using piezoelectric triaxial load cells was proposed based on a six-component multi-axis vectored thrust measure? ment system mounted in an underslung (floor-mounted)thrust stand. Triaxial piezoelectric sensors, rigid connection structures, and the measurement system were designed.The force transmission characteristics of the piezoelectric vectored thrust measurement system were analyzed through theoretical modeling and simulation,obtaining force transmission coefficients for each sensor in three directions,theoreti? cally verifying the feasibility of the solution.The extreme loads at sensor positions were analyzed by simulation,and the ranges and dimen? sions of the piezoelectric sensors were designed based on the analysis results.Piezoelectric sensors were developed and subjected to tests including static calibration,dynamic calibration,and stiffness measurement.The results show that linearity errors and repeatability errors in all three directions of each sensor are within 1%.In three directions,the natural frequencies reach 8701.1,8789.06,and 8457.03 Hz, respectively, and the stiffness values are 709.9, 718.1 and 1538.4 kN/mm, respectively. The sensors exhibit excellent dynamic/static characteristics,as well as high stiffness,meeting the requirements for dynamic vectored thrust measurement.
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