Paper
13 February 1990 Fiber Optic Speed Sensor For Gas Turbine Engine Control
Mark A. Overstreet, Victor J. Bird, Deepak Varshneya, John L. Maida
Author Affiliations +
Abstract
Allison Gas Turbine Division of General Motors Corporation, with Teledyne Ryan Electronics, has developed and demonstrated a fiber optic speed sensor (FOSS) for application to advanced fiber optic based control systems for gas turbine engines. The subject FOSS is capable of measuring turbine engine rotational speed throughout a speed range of 0-22,000+ rpm, which is equivalent to a sensor bandwidth of approximately 25 KHz. The principle of operation is based on directly sensing the pressure pulses generated by passing turbine blades via a pressure tube, a diaphragm at the top of the pressure tube, and a fiber optic microbend transducer affixed to the diaphragm. Transceiver electronics/optoelectronics are remotely located.
© (1990) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Mark A. Overstreet, Victor J. Bird, Deepak Varshneya, and John L. Maida "Fiber Optic Speed Sensor For Gas Turbine Engine Control", Proc. SPIE 1169, Fiber Optic and Laser Sensors VII, (13 February 1990); https://doi.org/10.1117/12.963068
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KEYWORDS
Fiber optics sensors

Sensors

Fiber optics

Fiber lasers

Laser optics

Electronics

Fiber optics tests

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