Method and apparatus for reduction of combustor dynamic...

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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C060S725000, C060S039281

Reexamination Certificate

active

06973791

ABSTRACT:
Methods and apparatus for operating a gas turbine engine without sustained detrimental levels of dynamic pressure are provided. The engine includes a combustor. The method includes determining the combustor acoustic level amplitude, comparing the acoustic level to a predetermined upper acoustic limit, and adjusting a fuel flow distribution to the combustor using a closed loop controller to facilitate reducing the acoustic level to a predetermined lower acoustic limit that is less than the upper acoustic limit.

REFERENCES:
patent: 5323604 (1994-06-01), Ekstedt et al.
patent: 5396760 (1995-03-01), Hines
patent: 5685157 (1997-11-01), Pandalai et al.
patent: 6354071 (2002-03-01), Tegel et al.
patent: 6742341 (2004-06-01), Ryan et al.

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