|Table of Contents|

Design of high-temperature vacuum fiber optic absolute pressure sensor for near-space vehicles(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2024年03期
Page:
118-123
Research Field:
目次
Publishing date:

Info

Title:
Design of high-temperature vacuum fiber optic absolute pressure sensor for near-space vehicles
Author(s):
ZHANG Yutong1; 2; 3;  JIANG Yi1; 2;  YANG Shuiwang4;  ZHANG Dayou5
1.School of Optics and Photonics, Beijing Institute of Technology, Beijing 100081, China; 2.Key Laboratory of Photonic Information Technology, Ministry of Industry and Information Technology, Beijing 100081, China; 3.School of Physical Science and Technology, Baotou Teachers' College, Baotou 014030, China; 4.Beijing Zhenxing Institute of Metrology and Measurement, Beijing 100074, China; 5.Beijing Aerospace Institute for Metrology and Measurement Technology, Beijing 100076, China
Keywords:
optical fiber pressure sensors;  extrinsic Fabry-Perot interferometer;  sapphire wafer;  absolute pressure measurement
PACS:
TP212
DOI:
10.3969/j.issn.1672-9374.2024.03.013
Abstract:
A sapphire-based extrinsic Fabry-Perot interferometer(EFPI)fiber optic absolute pressure sensor for near-space vehicles in high-temperature environment is developed and experimentally demonstrated. The sapphire wafer sensor head is composed of three sapphire wafers with different thicknesses bonded to form composite Fabry-Perot(FP)cavities, which can realize the simultaneous measurement of temperature and absolute pressure. By monitoring the temperature in real time, the pressure measurement is compensated to eliminate the influence of temperature on the pressure measurement. Experiment results show that the optical cavity length of the sealed FP cavity varies linearly within the applied pressure at each temperature point below 900 ℃. At room temperature, the pressure sensitivity is 11.6 nm/kPa and increases slightly with the increase of temperature. The resolution of the pressure measurement is 86 Pa.

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