Methods and apparatus for gas turbine engine lean blowout...

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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C060S039270

Reexamination Certificate

active

10930491

ABSTRACT:
A method of monitoring and controlling the combustion dynamics of a gas turbine engine system is provided. The system includes at least one gas turbine that includes at least one combustor can. The method includes receiving a signal from a gas turbine engine sensor that is indicative of combustion dynamics in at least one of the combustor cans, processing the received signal to determine a probability of lean blowout for at least one combustor can, and controlling the gas turbine engine system to facilitate reducing a probability of a lean blowout (LBO) event using the determined probability of lean blowout.

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“Optical and Acoustic Sensing of Lean Blowout Precursors” by T.M. Muruganandam, S. Nair, Y. Neumeier, T. Lieuwen, J.M. Seitzman, 38thAIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Jul. 7-10, 2002.
“Acoustic Characterization of a Piloted, Premixed Flame Under Near Blowout Conditions,” by S. Nair, T.M. Muruganandam, R. Hughes, L. Wu, J. Seitzman, and T. Lieuwen, 38thAIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Jul. 7-10, 2002.
“Evaluation of Chemiluminescence as Sensor for Lean Premixed Combustion,” by Laurent Zimmer, Shigeru Tachibana, Takeshi Yamamoto, Yohji Kurosawa, and Kazuo Suzuki, National Aerospace Laboratory of Japan.

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