• CN: 11-2187/TH
  • ISSN: 0577-6686

Journal of Mechanical Engineering ›› 2019, Vol. 55 ›› Issue (18): 1-7.doi: 10.3901/JME.2019.18.001

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Research on Optical Fiber F-P Temperature Sensor and Its Signal Demodulation System Used in Aero-engine

LIN Qijing1,2,3,4, WU Zirong2, ZHAO Na2, TIAN Bian2, JIANG Zhuangde1,2   

  1. 1. Collaborative Innovation Center of High-End Manufacturing Equipment, Xi'an Jiaotong University, Xi'an 710054;
    3. State Key Laboratory of Mechanical Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an 710049;
    3. State Key Laboratory of Digital Manufacturing Equipment & Technology, Huazhong University of Science and Technology, Wuhan 430074;
    4. State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, Hangzhou 310027
  • Received:2018-09-04 Revised:2019-03-25 Online:2019-09-20 Published:2020-01-07

Abstract: Optical fiber F-P temperature sensor with the advantages of stable structure, high precision, small volume, anti-electromagnetic interference, light weight and low cost has potential application in the high temperature measurement of aerial engine. According to the high temperature condition of aero-engine, the F-P temperature sensor is designed based on multi-beam interference principle. The fabrication of optical fiber F-P temperature sensor is completed by means of face detection and microscopic measurement. In order to overcome the shortcomings of the traditional spectrometer demodulation system which is expensive and slow demodulation speed, the signal demodulation system of the sensor is designed with F-P filter and DSP as the core, which overcomes the limitation of the demodulation with traditional spectrometer. The hardware design of the system is carried out, including the principle design, simulation analysis and circuit production of the photoelectric conversion amplifier circuit. Then the sensor is calibrated by standard thermocouple in high temperature furnace with high control precision of temperature. The results show that the temperature response sensitivity of the sensor is 0.012 nm/℃, and the linearity is 0.996 from 30℃ to 1 000℃.

Key words: optical fiber sensor, high temperature measurement, aero-engine, signal demodulation, performance test

CLC Number: