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- Data Not Current
For Information Purposes
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Glenn
Research Center
1991 Phase II
Turbomachinery
Flowfield Temperature Measurement Linear Imaging Diagnostics
Aerodyne
Research, Inc.
Billerica, MA
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INNOVATION
Non-intrusive measurement
of gas temperature and/or density for use in turbomachinery
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Linear Imaging Temperature
Measurement System Design
Optional Powerpoint
file
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ACCOMPLISHMENTS
- Demonstrated the feasibility
of non-intrusive measurement of temperature and density in a flowing
gas stream
- Developed an optical measurement
technique for use in compressor flow fields
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COMMERCIALIZATION
- $11K Phase III funding for further
development of the temperature measurement system at Glenn’s compressor
test facility
- A new approach for non-intrusive
measurement of gas temperature based on an O2-LIF technique has
been demonstrated at GRC as a result of the Phase III funding
- GRC may use additional Phase
III funds for demonstration tests in a compressor after reviewing
results in the final report
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GOVERNMENT/SCIENCE
APPLICATIONS
- This technique will be used
in the “Smart Green Engine” Program
- Will be used in the NASA Physics
and Process Modeling Program (PPM)
- Useful in turbomachinery research
over a temperature range of 300K-500K
- Useful in research applications
requiring non-intrusive measurement of gas temperature
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