TY - GEN
T1 - Temperature measurement of gases using acoustic means
AU - Moss, Brian
AU - Leen, Gabriel
AU - Lewis, Elfed
AU - Bremer, Kort
AU - Niven, Andrew
PY - 2009
Y1 - 2009
N2 - Traditional temperature measurement devices such as bimetallic strips, thermocouples, RTDs, radiation devices (i.e. Infrared), silicon P-N junctions etc. all have limitations such as range or slow response times due to them having to 'reach' temperature. These limitations, while normally not an issue become so where high speed operation or large temperature ranges are either required and/or likely to be encountered. Kleppe [1, 2] and Stones[3] describe methods based on Acoustic Pyrometry for high speed high temperature measurement in flue gas flows and high pressure burner combustors. However most Acoustic Pyrometric schemes use active acoustics in that an acoustic wave of sufficient power and frequency (usually ultrasonic) is introduced into the medium to be received by an appropriate transducer a distance away. From the resultant time of flight (TOF) of the transmitted signal the speed of sound in that gas region can be determined. The aim of this paper is to discuss the use of passive acoustic sensors that utilise the self generating pressure pulses in a dynamic gas flow.
AB - Traditional temperature measurement devices such as bimetallic strips, thermocouples, RTDs, radiation devices (i.e. Infrared), silicon P-N junctions etc. all have limitations such as range or slow response times due to them having to 'reach' temperature. These limitations, while normally not an issue become so where high speed operation or large temperature ranges are either required and/or likely to be encountered. Kleppe [1, 2] and Stones[3] describe methods based on Acoustic Pyrometry for high speed high temperature measurement in flue gas flows and high pressure burner combustors. However most Acoustic Pyrometric schemes use active acoustics in that an acoustic wave of sufficient power and frequency (usually ultrasonic) is introduced into the medium to be received by an appropriate transducer a distance away. From the resultant time of flight (TOF) of the transmitted signal the speed of sound in that gas region can be determined. The aim of this paper is to discuss the use of passive acoustic sensors that utilise the self generating pressure pulses in a dynamic gas flow.
UR - http://www.scopus.com/inward/record.url?scp=67650517700&partnerID=8YFLogxK
U2 - 10.1109/SSD.2009.4956712
DO - 10.1109/SSD.2009.4956712
M3 - Conference contribution
AN - SCOPUS:67650517700
SN - 9781424443468
T3 - 2009 6th International Multi-Conference on Systems, Signals and Devices, SSD 2009
BT - 2009 6th International Multi-Conference on Systems, Signals and Devices, SSD 2009
T2 - 2009 6th International Multi-Conference on Systems, Signals and Devices, SSD 2009
Y2 - 23 March 2009 through 26 March 2009
ER -