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Development of a Temperature Sensor for Jet Engine and Space Mission ApplicationsElectronics for Distributed Turbine Engine Control and Space Exploration Missions are expected to encounter extreme temperatures and wide thermal swings. In particular, circuits deployed in a jet engine compartment are likely to be exposed to temperatures well exceeding 150 C. To meet this requirement, efforts exist at the NASA Glenn Research Center (GRC), in support of the Fundamental Aeronautics Program/Subsonic Fixed Wing Project, to develop temperature sensors geared for use in high temperature environments. The sensor and associated circuitry need to be located in the engine compartment under distributed control architecture to simplify system design, improve reliability, and ease signal multiplexing. Several circuits were designed using commercial-off-the-shelf as well as newly-developed components to perform temperature sensing at high temperatures. The temperature-sensing circuits will be described along with the results pertaining to their performance under extreme temperature.
Document ID
20080047731
Document Type
Conference Paper
Authors
Patterson, Richard L. (NASA Glenn Research Center Cleveland, OH, United States)
Hammoud, Ahmad (ASRC Aerospace Corp. Cleveland, OH, United States)
Elbuluk, Malik (Akron Univ. Akron, OH, United States)
Culley, Dennis (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
May 12, 2008
Subject Category
Aircraft Stability and Control
Report/Patent Number
E-16795
Meeting Information
HiTEC 2008 High Temperature Electronics Conference/International Microelectronics and Packaging society (IMAPS)(Albuquerque, NM)
Funding Number(s)
CONTRACT_GRANT: NNC06BA07B
WBS: WBS 561581.02.08.03.17.03
Distribution Limits
Public
Copyright
Public Use Permitted.

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