Abstract
The chapter describes an innovative IR sensor properly conceived for real-time measurements of the gas turbine inlet temperature. The sensor is based on the measurements of the radiation emitted in a given wavelength band by the CO2 molecules present in the combustion gas. Experimental results relevant to laboratory tests aimed at characterizing the techniques will be presented.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Similar content being viewed by others
Reference
G.A. Hornbeck, Optical methods of temperature measurement. Appl. Opt. Vol.5, No.2, 179 (1966).
Acknowledgments
This work has been financed by the Research Fund for the Italian Electrical System under the Contract Agreement between RSE (formerly known as ERSE) and the Ministry of Economic Development—General Directorate for Nuclear Energy, Renewable Energy, and Energy Efficiency stipulated on July 29, 2009, in compliance with the Decree of March 19, 2009.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2014 Springer International Publishing Switzerland
About this paper
Cite this paper
Golinelli, E., Musazzi, S., Perini, U., Barberis, F. (2014). Nonintrusive IR Sensor for Real-Time Measurements of Gas Turbine Inlet Temperature. In: Di Natale, C., Ferrari, V., Ponzoni, A., Sberveglieri, G., Ferrari, M. (eds) Sensors and Microsystems. Lecture Notes in Electrical Engineering, vol 268. Springer, Cham. https://doi.org/10.1007/978-3-319-00684-0_4
Download citation
DOI: https://doi.org/10.1007/978-3-319-00684-0_4
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-00683-3
Online ISBN: 978-3-319-00684-0
eBook Packages: EngineeringEngineering (R0)