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Lightweight, Opto-Electronic Engine Control System for Aerospace Turbine Engines

1993-04-01
931442
AlliedSignal Controls and Accessories (ASCA) in cooperation with Pratt & Whitney Government Engine and Space Propulsion (PW GESP) have demonstrated a lightweight opto-electronic engine control system that features a lightweight fuel throttling valve, lightweight inlet guide vane servoactuator, and an opto-electronic controller with lightweight enclosure. The engine control system was built and tested in support of the first phase of the government sponsored Integrated High Performance Turbine Engine Technology (IHPTET) Initiative. Both the fuel throttling valve and inlet guide vane servoactuator utilize fiber-optic position feedback sensors, low power, high force lightweight piezoelectric actuated direct drive servovalves, and advanced lightweight materials such as AA-8090 aluminum-lithium, silicon nitride ceramic, carbon fiber composite, and AA-8009 high temperature aluminum.
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