12 July 1993 Surface-mounted sensors for gas turbine research and development
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Abstract
In the development of gas turbine aeroengines, the high cost of development testing and market lead pressure to reduce program timescales has led to increasing use of advanced instrumentation. A growing interest has been the integration of sensors into the engine components, both to look outward at the behavior of the flow over the component, and to look inward at the temperature and strain of the component itself. This paper describes a range of pieso-resistive and thermal sensor applications developed by Rolls-Royce concluding with a view of this industry's future needs and sensor design challenges.
© (1993) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Peter Loftus, Richard Shepherd, Keith Stringfellow, "Surface-mounted sensors for gas turbine research and development", Proc. SPIE 1918, Smart Structures and Materials 1993: Smart Sensing, Processing, and Instrumentation, (12 July 1993); doi: 10.1117/12.148001; https://doi.org/10.1117/12.148001
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