红外与激光工程, 2018, 47 (7): 0722002, 网络出版: 2018-08-30
光纤法珀压力传感系统设计与风洞初步实验
Design and preliminary experiment of optical fiber F-P pressure sensing system working in wind tunnel
光纤法珀 大气压力 风洞 温度补偿 数值模拟 optical fiber F-P atmospheric pressure wind tunnel temperature compensation numerical simulation
摘要
针对航空领域对大气压力的测量需求, 基于光纤法珀传感和低相干干涉技术, 搭建了光纤法珀多通道压力传感系统。介绍了系统解调算法及工作原理, 对光纤法珀压力传感器的标定和温度补偿方法进行理论分析, 将非恒温条件下的传感器拟合误差降低至0.134% F.S.。在风洞环境中, 在侧滑角-4°~4°变化范围内, 对飞机实体模型的三个监测点进行压力测量实验, 并将压力测量结果与Ansys-Fluent软件模拟仿真结果做对比。结果显示, 光纤法珀压力传感系统与模拟仿真数据变化趋势相同, 全量程误差为0.38% F.S., 证明此系统能够提供可靠的压力数据, 真实反映飞机模型被监测位置在风洞中的受力情况。
Abstract
In order to meet the requirement of atmospheric pressure measurement in the aviation field, based on the principle of the optical fiber Fabry-Perot (F-P) sensing and low coherence interference, an optical fiber F-P multi-channel pressure sensing system was proposed. First of all, the demodulation algorithm and basic principle were introduced, the calibration method and temperature compensation of the optical fiber F-P pressure sensor were analyzed in theory. The fitting error of the sensor under non-constant temperature condition was reduced to 0.134% F.S.. Then, in the wind tunnel environment within -4°-4° sideslip angle range, the pressure measurement experiment was carried out on three monitoring points of the aircraft model. The results were compared with the simulation results using Ansys-Fluent software. In conclusion, the results show that the system using the optical fiber F-P pressure sensor and the Ansys-Fluent numerical simulation have the same trend of demodulation results, with the full range error of 0.38% F.S.. The experiments confirm that the system can provide reliable pressure data accurately and reflect the pressure of the aircraft model′s monitoring points in the wind tunnel.
刘畅, 王双, 梁应剑, 江俊峰, 梅运桥, 刘琨, 齐晓光, 李鑫, 李元耀, 刘铁根. 光纤法珀压力传感系统设计与风洞初步实验[J]. 红外与激光工程, 2018, 47(7): 0722002. Liu Chang, Wang Shuang, Liang Yingjian, Jiang Junfeng, Mei Yunqiao, Liu Kun, Qi Xiaoguang, Li Xin, Li Yuanyao, Liu Tiegen. Design and preliminary experiment of optical fiber F-P pressure sensing system working in wind tunnel[J]. Infrared and Laser Engineering, 2018, 47(7): 0722002.