An Optical Acoustic Sensor Based on Grooved High-Q Ring Resonator Applied to Subatmospheric Pressure Environment

被引:0
作者
Chen, Jiamin [1 ]
Luo, Yifan [1 ]
Zheng, Yongqiu [1 ]
Bai, Jiandong [1 ]
Xue, Chenyang [1 ]
机构
[1] North Univ China, Key Lab Instrumentat Sci & Dynam Measurement, Minist Educ, Taiyuan 030051, Peoples R China
基金
中国国家自然科学基金;
关键词
High sensitivity; optical acoustic sensor; optical waveguide ring resonator (OWRR); subatmospheric pressure; SENSITIVITY;
D O I
10.1109/JSEN.2024.3436668
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Optical waveguide ring resonators (OWRRs) with high quality factor can greatly enhance the interaction between light and matter, which shows great advantages in optical sensing and has become a research hotspot in recent years. In this article, the change of acoustic signal is perceived by the evanescent field, which is induced by grooving in the ring waveguide region of SiO2 OWRR. The acoustic characteristics of the optical acoustic sensor based on SiO2 grooved OWRR under different atmospheric pressures are studied in detail. In the atmospheric pressure range of 41-101 kPa, the optical acoustic sensor always maintains a broadband acoustic response of 400 H-59 kHz, and the response flatness is less than +/- 2 dB. The sound pressure sensitivity increases with the decrease of atmospheric pressure. At 41 kPa, the sound pressure sensitivity is as high as 1040.44 mV/Pa, which is 1.35 times higher than that at 101 kPa. At the same time, the optical acoustic sensor can detect an acoustic signal as low as 5.03 dB at a subatmospheric pressure of 41 kPa. In addition, the fluctuation error of sound pressure sensitivity of the sensor is less than 3% when tested in different temperature and humidity environments. The excellent acoustic detection performance of the optical acoustic sensor in the subatmospheric pressure environment indicates that it is very suitable for acoustic monitoring and acoustic diagnosis under subatmospheric conditions such as high-altitude areas and aerospace fields.
引用
收藏
页码:28879 / 28888
页数:10
相关论文
共 43 条
[1]  
Lee H.M., Garg S., Lim K.M., Lee H.P., Comparison of cabin noise of turboprop and turbofan aircrafts, Appl. Acoust., 214, (2023)
[2]  
Bagherzadeh S.A., Salehi M., Assessment of cabin noise contributing factors of a turbo-propeller airplane using EMD and SSA signal decomposition methods, Appl. Acoust., 178, (2021)
[3]  
Li Z., Wang Y., Qiao B., Wen B., Chen X., Experimental investigation of aeroelastic instabilities in an aeroengine fan: Using acoustic measurements, Aerosp. Sci. Technol., 130, (2022)
[4]  
Cheng T., Zhang T., Zhong Y., Ji H., Zhang X., Design and experimental validation of active robust controller for the jet flame combustion oscillation, Int. J. Thermal Sci., 197, (2024)
[5]  
Bu H., Huang X., Zhang X., An overview of testing methods for aeroengine fan noise, Prog. Aerosp. Sci., 124, (2021)
[6]  
Kusuda S., Yamasaki N., Inoue C., Namba M., Aircraft engine fan tone noise due to back-pressure distortion caused by a downstream pylon under high-speed conditions, J. Sound Vibrat., 572, (2024)
[7]  
Xu X., Lu Y., Shao M., Lu J., Noise attenuation of frequencymodulated multi-rotor using sound field reproduction, Chin. J. Aeronaut., 36, 11, pp. 185-203, (2023)
[8]  
Li Z., Et al., The investigation of all-sapphire Fabry-Perot fiber acoustic sensor operating up to 800°C, IEEE Sensors J., 23, 23, pp. 28960-28968, (2023)
[9]  
Yang H., Et al., Micropascal-sensitivity ultrasound sensors based on optical microcavities, Photon. Res., 11, 7, (2023)
[10]  
Zhang S., Dong B., Chen Z., Huang W., Yang L., Shao Q., An allpolymer spring optomechanical microresonator for ultrahigh sensitivity and wideband ultrasonic detection, J. Lightw. Technol., 42, 7, pp. 2625-2631, (2024)