The measurement of engine emissions is important for their monitoring and control. However, the ability to measure these emissions in-situ is limited. We are developing a family of high temperature gas sensors which are intended to operate in harsh environments such as those in an engine. The development of these sensors is based on progress in two types of technology: 1) The development of SiC-based semiconductor technology. 2) Improvements in micromachining and microfabricarion technology. These technologies are being used to develop point-contact sensors to measure gases which are important in emission control especially hydrogen, hydrocarbons, nitrogen oxides, and oxygen. The purpose of this paper is to discuss the development of this point-contact sensor technology. The detection of each type of gas involves its own challenges in the fields of materials science and fabrication technology. Of particular importance is sensor sensitivity, selectivity, and stability in long-term, high temperature operation. An overview is presented of each sensor type with an evaluation of its stage of development. It is concluded that this technology has significant potential for use in engine applications but further development is necessary.
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ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition
June 2–5, 1997
Orlando, Florida, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7871-2
PROCEEDINGS PAPER
Development of High Temperature Gas Sensor Technology
Gary W. Hunter,
Gary W. Hunter
NASA Lewis Research Center, Cleveland, OH
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Liang-Yu Chen,
Liang-Yu Chen
NASA Lewis Research Center, Cleveland, OH
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Philip G. Neudeck,
Philip G. Neudeck
NASA Lewis Research Center, Cleveland, OH
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Dak Knight,
Dak Knight
NASA Lewis Research Center, Cleveland, OH
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C. C. Liu,
C. C. Liu
Case Western Reserve University, Cleveland, OH
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Q. H. Wu,
Q. H. Wu
Case Western Reserve University, Cleveland, OH
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H. J. Zhou
H. J. Zhou
Case Western Reserve University, Cleveland, OH
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Gary W. Hunter
NASA Lewis Research Center, Cleveland, OH
Liang-Yu Chen
NASA Lewis Research Center, Cleveland, OH
Philip G. Neudeck
NASA Lewis Research Center, Cleveland, OH
Dak Knight
NASA Lewis Research Center, Cleveland, OH
C. C. Liu
Case Western Reserve University, Cleveland, OH
Q. H. Wu
Case Western Reserve University, Cleveland, OH
H. J. Zhou
Case Western Reserve University, Cleveland, OH
Paper No:
97-GT-494, V004T15A038; 7 pages
Published Online:
December 24, 2014
Citation
Hunter, GW, Chen, L, Neudeck, PG, Knight, D, Liu, CC, Wu, QH, & Zhou, HJ. "Development of High Temperature Gas Sensor Technology." Proceedings of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award. Orlando, Florida, USA. June 2–5, 1997. V004T15A038. ASME. https://doi.org/10.1115/97-GT-494
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