Li Yinan, Wang Junbo, Luo Zhenyu, Chen Deyong, Chen Jian
State Key Laboratory of Transducer Technology, Institute of Electronics, Chinese Academy of Sciences, Beijing 100190, China.
University of Chinese Academy of Sciences, Beijing 100049, China.
Sensors (Basel). 2015 Apr 29;15(5):10048-58. doi: 10.3390/s150510048.
Resonant pressure microsensors are widely used in the fields of aerospace exploration and atmospheric pressure monitoring due to their advantages of quasi-digital output and long-term stability, which, however, requires the use of additional temperature sensors for temperature compensation. This paper presents a resonant pressure microsensor capable of self-temperature compensation without the need for additional temperature sensors. Two doubly-clamped "H" type resonant beams were arranged on the pressure diaphragm, which functions as a differential output in response to pressure changes. Based on calibration of a group of intrinsic resonant frequencies at different pressure and temperature values, the functions with inputs of two resonant frequencies and outputs of temperature and pressure under measurement were obtained and thus the disturbance of temperature variations on resonant frequency shifts was properly addressed. Before compensation, the maximal errors of the measured pressure values were over 1.5% while after compensation, the errors were less than 0.01% of the full pressure scale (temperature range of -40 °C to 70 °C and pressure range of 50 kPa to 110 kPa).
谐振式压力微传感器因其准数字输出和长期稳定性的优点,在航空航天探索和大气压力监测领域得到广泛应用,然而,这需要使用额外的温度传感器进行温度补偿。本文提出了一种无需额外温度传感器即可实现自温度补偿的谐振式压力微传感器。两个双端固支“H”型谐振梁布置在压力膜片上,压力膜片响应压力变化起到差分输出的作用。基于对一组不同压力和温度值下的固有谐振频率进行校准,得到了以两个谐振频率为输入、温度和被测压力为输出的函数,从而妥善解决了温度变化对谐振频率偏移的干扰。补偿前,被测压力值的最大误差超过1.5%,而补偿后,误差小于满量程压力的0.01%(温度范围为-40°C至70°C,压力范围为50 kPa至110 kPa)。