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Sensor and Actuator Needs for More Intelligent Gas Turbine EnginesThis paper provides an overview of the controls and diagnostics technologies, that are seen as critical for more intelligent gas turbine engines (GTE), with an emphasis on the sensor and actuator technologies that need to be developed for the controls and diagnostics implementation. The objective of the paper is to help the "Customers" of advanced technologies, defense acquisition and aerospace research agencies, understand the state-of-the-art of intelligent GTE technologies, and help the "Researchers" and "Technology Developers" for GTE sensors and actuators identify what technologies need to be developed to enable the "Intelligent GTE" concepts and focus their research efforts on closing the technology gap. To keep the effort manageable, the focus of the paper is on "On-Board Intelligence" to enable safe and efficient operation of the engine over its life time, with an emphasis on gas path performance
Document ID
20100029602
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Garg, Sanjay
(NASA Glenn Research Center Cleveland, OH, United States)
Schadow, Klaus
(Schadow Technology San Clemente, CA, United States)
Horn, Wolfgang
(MTU Aero Engines G.m.b.H. Munich, Germany)
Pfoertner, Hugo
(MTU Aero Engines G.m.b.H. Munich, Germany)
Stiharu, Ion
(Concordia Univ. Montreal, Quebec, Canada)
Date Acquired
August 25, 2013
Publication Date
July 1, 2010
Subject Category
Instrumentation And Photography
Report/Patent Number
GT2010-22685
E-17323
NASA/TM-2010-216746
Report Number: GT2010-22685
Report Number: E-17323
Report Number: NASA/TM-2010-216746
Meeting Information
Meeting: Turbo Expo 2010
Location: Glasgow, Scotland
Country: United Kingdom
Start Date: June 14, 2010
End Date: June 18, 2010
Funding Number(s)
WBS: WBS 736466.08.01.03.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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