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Glenn
Research Center
1991 Phase II
6H-SiC Pressure
Sensors for High
Temperature
Applications
Kulite
Semiconductor Products, Inc.
Leonia, NJ
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INNOVATION
A silicon carbide (SiC) pressure
sensor for use at temperatures as high as 500°C, which is approximately
100°C higher than can be withstood by presently available silicon
pressure sensors
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SiC Sensor Mounted on a Header
Optional Powerpoint
file
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ACCOMPLISHMENTS
- Prototype SiC pressure sensors
were developed in Phase II contract
- The pressure sensors were shown
to be capable of operating at 500°C for several hours
- Provided GRC with prototype
SiC pressure sensors
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COMMERCIALIZATION
- A high temperature pressure
sensor for engine aircraft development and test. Fast response
pressure measurements in the compressor hot section for stall
detection and control
- This pressure sensor can be
used for other high temperature turbine engine applications
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GOVERNMENT/SCIENCE
APPLICATIONS
- Phase III of $500K to provide
GRC with 6-10 prototype SiC pressure sensors. Funding provided by
Advanced High Temperature Engine Material Technology Program (HITEMP)
and Higher Operating Temperature Propulsion Components (HOTPC) Program.
- A prototype SiC pressure sensor
to be tested in the compressor of a gas turbine engine by
October 2000
- For use in military aircraft
and any other turbine engine, e.g., tanks
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