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NONINTRUSIVE TRANSCEIVER AND METHOD FOR CHARACTERIZING TEMPERATURE AND VELOCITY FIELDS IN A GAS TURBINE COMBUSTOR

United States Patent Application

20150260611
A1
View the Complete Application at the US Patent & Trademark Office
An acoustic transceiver is implemented for measuring acoustic properties of a gas in a turbine engine combustor. The transceiver housing defines a measurement chamber and has an opening adapted for attachment to a turbine engine combustor wall. The opening permits propagation of acoustic signals between the gas in the turbine engine combustor and gas in the measurement chamber. An acoustic sensor mounted to the housing receives acoustic signals propagating in the measurement chamber, and an acoustic transmitter mounted to the housing creates acoustic signals within the measurement chamber. An acoustic measurement system includes at least two such transceivers attached to a turbine engine combustor wall and connected to a controller.
DeSilva, Upul P. (Oviedo, FL), Claussen, Heiko (North Brunswick, NJ)
14/ 341,924
July 28, 2014
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT [0010] Temperature mapping portions of this invention were made with government support under contract DE-FC26-05NT42644 awarded by the U.S. Department of Energy. The government may have certain rights in the invention.