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Proceedings Paper

Use of optical sensors and signal processing in gas turbine engines
Author(s): Ian Davinson
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Paper Abstract

The application of optical measurement techniques to aircraft engine testing is described including measurement systems for turbine blade tip clearance compressor blade vibration fan blade profile turbine blade temperature and flow diagnostics. The signal and data processing associated with these techniques is emphasised and the prospects for further extending the use of optical methods on ground test and flight engines is discussed. The possibility of applying optical processing techniques is also briefly discussed.

Paper Details

Date Published: 1 February 1991
PDF: 15 pages
Proc. SPIE 1374, Integrated Optics and Optoelectronics II, (1 February 1991); doi: 10.1117/12.24975
Show Author Affiliations
Ian Davinson, Rolls Royce plc (United Kingdom)


Published in SPIE Proceedings Vol. 1374:
Integrated Optics and Optoelectronics II
Ka Kha Wong, Editor(s)

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