Active combustion control for a turbine engine

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

Reexamination Certificate

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C060S776000, C060S746000, C060S747000, C060S725000, C060S039826, C431S114000

Reexamination Certificate

active

08028512

ABSTRACT:
A combustion control system for a turbine engine is disclosed. The combustion control system includes a fuel injector having a main fuel supply and pilot fuel supply coupled to a combustor of the turbine engine. The combustion control system also includes a sensor coupled to a transfer tube. The transfer tube is fluidly coupled to the combustor, and the sensor is configured to detect a pressure pulse in the combustor. A semi-infinite coil is also coupled to the transfer tube. The combustion control system also includes a controller electrically connected to the sensor. The controller is configured to compare an amplitude of the pressure pulse within a frequency range to a threshold amplitude, and adjust the pilot fuel supply in response to the comparison.

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Jayasuriya, Jeevan; Manrique, Arturo, Gas Turbine Combustor Lab Exercise, Royal Institute of Technology, Jan. 31, 2005, 9 pages, Stockholm.

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