轴向应变放大式谐振温度传感器研究
Research on resonant temperature sensor with axial strain amplification
滕飞1
作者信息
- 1. 中国飞行试验研究院,陕西西安 710089
- 折叠
摘要
试验机专用改装系统成为开展民机适航、审定试飞的重要手段之一.为进一步提升系统性能,满足高精度高可靠性要求,该文提出一种基于轴向应变放大结构的谐振式温度传感器.基于应变放大结构建立频率-温度模型,推导频率温度系数作为衡量灵敏度的物理量.为降低理论模型与仿真模型的相对误差,该文进行仿真分析与误差修正,将二者误差降低至 0.5%.测试结果表明,当外界温度在 273～293 K范围内变化时,器件的频率温度系数为13104×10-6 K-1,仿真结果为 12935×10-6 K-1,二者相比,相对误差为 1.3%.与以往谐振式温度传感器比较,相对灵敏度最大提高了83倍.该结构可用于高灵敏度谐振式温度传感器的优化设计,满足试验机改装系统的应用需求.
Abstract
The special modification system of the testing machine becomes one of the important means to carry out civil aircraft airworthiness and certification test flight.In order to further improve the system performance and meet the requirements of high accuracy and reliability,a resonant temperature sensor based on axial strain amplification structure is proposed.In this paper,a frequency-temperature model is established based on strain amplification structure,and the frequency-temperature coefficient is derived as a physical quantity to measure sensitivity.In order to reduce the relative error of theoretical model and simulation model,simulation analysis and error correction are carried out,and the relative error of both is reduced to 0.5%.The test results show that when the external temperature changes in the range of 273-293 K,the frequency-temperature coefficient of the device is 13104×10-6 K-1,while the simulation result is 12935×10-6 K-1,the relative error between the two is 1.3%,and the sensitivity is increased by 83 times compared with the previous resonant temperature sensor.The structure can be used to optimize the design of high sensitivity resonant temperature sensor and meet the application requirements of testing machine modification system.
关键词
轴向应变放大/频率温度系数/谐振式温度传感器/高灵敏度Key words
axial strain amplification/frequency-temperature coefficient/resonant temperature sensor/high sensitivity引用本文复制引用
出版年
2024
NETL
NSTL
万方数据