Paper
27 November 1996 Multiplexing optical fiber-based pressure sensors for smart wings
Mark E. Jones, Paul Grems Duncan, Ricky Crotts, Kevin A. Shinpaugh, Jennifer L. Grace, Kent A. Murphy, Richard O. Claus, Wade J. Pulliam, Joseph A. Schetz
Author Affiliations +
Abstract
A novel, multiplexed optical fiber differential-pressure transducer is described for the real-time pressure measurement of airflow in applications involving actuator- and SMA-controlled airfoils and multi-parameter skin friction measurements. The design of the pressure transducer is based upon extrinsic Fabry-Perot interferometry (EFPI) and uses a micromachined silicon diaphragm to modulate the sensing cavity. The pressure transducer was designed to operate from minus 10 to 10 psig and have a resolution of greater than 0.01 psi. Ten pressure transducers were spatially multiplexed and tested for smart wing applications. Results are also reported for an integrated skin friction balance/optical fiber pressure transducer tested in Virginia Tech's Supersonic Tunnel (VTSST).
© (1996) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Mark E. Jones, Paul Grems Duncan, Ricky Crotts, Kevin A. Shinpaugh, Jennifer L. Grace, Kent A. Murphy, Richard O. Claus, Wade J. Pulliam, and Joseph A. Schetz "Multiplexing optical fiber-based pressure sensors for smart wings", Proc. SPIE 2838, Distributed and Multiplexed Fiber Optic Sensors VI, (27 November 1996); https://doi.org/10.1117/12.259803
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Cited by 4 scholarly publications.
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KEYWORDS
Transducers

Sensors

Optical fibers

Skin

Multiplexing

Fiber optics sensors

Silicon

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