期刊
IEEE SENSORS JOURNAL
卷 16, 期 17, 页码 6596-6603出版社
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/JSEN.2016.2586586
关键词
Aircraft engine tests; fibre Bragg grating sensors; total temperature sensing
资金
- Bundesministerium fur Forschung und Technology [FKZ 170 10X 11]
- Bayrische Forschungsstiftung [AZ-1146-14]
The suitability of using fiber Bragg gratings (FBG) as sensor elements in total temperature probes for turbine compressor applications is shown. A series of five FBG-based probes was built and characterized experimentally in the harsh environment of an open-jet test bench at air stream velocities of up to Mach 0.8. The performances of the FBG-based probes were compared with that of a conventional thermocouple-based total temperature sensor. All fiber-optic probes showed good mechanical robustness and recovery factors in the range of 0.79-0.99. Employing fiber-optic sensor elements allowed a significant reduction of the diameters of the stagnation tubes of the transducers. Because of the smaller probe design and thinner signal transmission cables, less distortion of the air stream is expected with the fiber-optic sensors, when compared with the conventional instrumentation.
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