- Conference Article
- 10.2514/6.2009-4974
High-Temperature Pressure Sensor Using Optical Stress Birefringence for Distributed Engine Control
- Aug 02, 2009
- Jeffrey Mackey + 2 more +2
Accurate pressure measurements in harsh environments are necessary to accommodate distributed jet engine control using various feedback schemes communicating with the Full Authority Digital Engine Control (FADEC) unit. Active combustion control requires feedback to the engine control system in order to adjust the quantity, timing, and placement of fuel charges. Understanding the complex interaction of air and fuel during combustion will help scientists design and construct quieter, safer, faster and more powerful aircraft engines and other propulsion systems. Current state-of-the-art pressure measurement instruments used in jet engines may employ MEMS-based silicon or silicon carbide sensors arranged in a variety of configurations, some of which may be coupled to optical fibers. Although the measurement signals are generally not distorted by the engine's electromagnetic fields, measurements obtained through current methods may be compromised due the high temperature range, its rapid rate of change, g-levels and lifespan issues. Alternatively, intrinsic optical fiber properties may be exploited because a silica fiber acts as a pre-stressed optically anisotropic force-deformation element when subjected to an applied load. Pre-stressing the fiber during the drawing process enables positive (tension) and negative (compression) forces to be quantified. In this paper we present a technique to perform static and fast transient pressure measurements using a single optical fiber as a pressure-sensing element. Since fused silica has a frequency response on the order of 100 kHz and an annealing temperature in excess of 1100 o C, optical fiber makes an excellent candidate for combustion engine applications. Linearly polarized light is phase-modulated and then transmitted through the optical fiber, which has a reflective coating sputtered onto the terminating surface. The polarization state of the transmitted and reflected light is altered through the silica fiber by the intrinsic static birefringence inherent in fused silica and by an additional amount determined by the applied load. By examining the interaction of polarized light with the silica fiber, the amount of molecular deformation and thus the applied pressure may be obtained. Phase modulation creates an infinite series of sine waves so that a Fourier-Bessel expansion may be used to separate signals of interest from noise using offset homodyning signal recovery techniques. Ratio analysis of the dc and harmonic signals yields the optical phase retardance and mathematically relates this quantity to the applied pressure by the Stress-optic rule. Several prototype phase-modulated stress-induced birefringence based fiber-optic high-temperature pressure sensors were recently developed at NASA Glenn Research Center to operate at temperatures in excess of 600 o C for an absolute pressure range from 14 psia to 1029 psia. This paper presents the design theory, fabrication methods and laboratory test results obtained with these prototypes.
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