Paper
30 June 1998 Miniature fiber optic pressure sensors for turbomachinery applications
William N. MacPherson, James M. Kilpatrick, James S. Barton, Julian D. C. Jones
Author Affiliations +
Abstract
Development of pressure sensor for the instrumentation of experimental aerodynamic facilities has traditionally concentrated on electrical techniques. Such transducers have temporal and spatial resolutions that are currently insufficient to provide the accurate measurement of turbulent flows behind turbine rotor stages, for example. We present result obtained in a turbine test rig form a simple fiber optic pressure sensor based upon the interferometric response of an extrinsic cavity formed between the interrogation fiber and a reflective diaphragm. We discuss the design trade-offs, optical interrogation and temperature sensitivity of such a configuration, and demonstrate the success of the design in small-scale shock tube experiments. We then describe the application of the sensor in a full scale turbine test facility.
© (1998) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
William N. MacPherson, James M. Kilpatrick, James S. Barton, and Julian D. C. Jones "Miniature fiber optic pressure sensors for turbomachinery applications", Proc. SPIE 3478, Laser Interferometry IX: Techniques and Analysis, (30 June 1998); https://doi.org/10.1117/12.312947
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CITATIONS
Cited by 5 scholarly publications.
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KEYWORDS
Sensors

Aerodynamics

Fiber optics sensors

Fiber optics

Spatial resolution

Optical fibers

Reflectivity

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