Lightweight, Opto-Electronic Engine Control System for Aerospace Turbine Engines
Document Number: 931442
Date Published: April 1993
Author(s):
Bradley J. McRoberts - Allied Signal Controls and Accessories
Charles T. Walejewski - Allied Signal Controls and Accessories
Abstract:
Allied Signal Controls and Accessories (ASCA) in cooperation with Pratt and 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 van 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. Using these advanced lightweight materials, and employing innovative control techniques and advanced electromechanical interface devices, an overall weight savings of 25% was achieved over baseline YF119 components. The engine control system has completed over 100 hours of testing on the USAF's JTDE XTE 65-1B engine with additional testing scheduled for the latter part of 1993. In addition, the components have amassed a total of 50 hours of component acceptance and design verification testing in the laboratory
File Size: 1616K
Product Status: In Stock
See other papers presented at Aerospace Atlantic Conference & Exposition, April 1993, Dayton, OH, USA, Session: Aerospace Atlantic Conference & Exposition
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