Novel heat flux sensor for SiC-SiC ceramic matrix composite engine components
Silicon carbide-silicon carbide ceramic matrix composites (SiC-SiC CMC’s) are being used in gas turbine engine hot sections due to their refractory nature and excellent toughness at high temperatures. A novel heat flux sensor was developed for SiC-SiC CMC based engine components, which can survive t...
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Published in | Sensors and actuators. A. Physical. Vol. 345; p. 113771 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
Lausanne
Elsevier B.V
01.10.2022
Elsevier BV |
Subjects | |
Online Access | Get full text |
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Summary: | Silicon carbide-silicon carbide ceramic matrix composites (SiC-SiC CMC’s) are being used in gas turbine engine hot sections due to their refractory nature and excellent toughness at high temperatures. A novel heat flux sensor was developed for SiC-SiC CMC based engine components, which can survive temperatures up to 550 °C. The heat flux sensor consists of platinum thin films that forms a thermocouple junction with the SiC-SiC CMC which utilizes the bulk thermoelectric properties of the SiC-SiC CMC for its operation. This novel Pt:SiC-SiC CMC heat flux sensor generates a thermoelectric voltage that is directly proportional to the temperature gradient along the through thickness direction of the CMC component onto which it was deposited and has a calibration factor of 0.0266 µV/(W/m2). Fabrication details, experimental results and implementation challenges are discussed.
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•A Pt:SiC ceramic matrix composite sensor that measures heat-flux was developed.•The calibration factor of the sensor was linear and 0.0266μV/(W/m2).•Upon repeated thermal cycling, the output of the sensor drifted by only 15μV.•Thermal conductivity is 0.323Wm−1K−1 to 1.054Wm−1K−1 with a mullite coating.•Thermal conductivity is 0.496Wm−1K−1 to 1.444Wm−1K−1 without a mullite coating. |
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ISSN: | 0924-4247 1873-3069 |
DOI: | 10.1016/j.sna.2022.113771 |