Apparatus for reducing gas turbine engines emissions

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

Reexamination Certificate

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Details

C060S725000

Reexamination Certificate

active

06883301

ABSTRACT:
A combustion control system controls a turbine engine that includes a fuel manifold and a plurality of fuel injectors. The control system includes a fuel pulsator and a controller. The fuel pulsator is coupled in flow communication with the plurality of injectors and the fuel manifold. The controller is coupled to the fuel pulsator such that the pulsator is between the controller and the fuel manifold. The controller is variably selectable and configured to facilitate promoting stable combustion.

REFERENCES:
patent: 5349811 (1994-09-01), Stickler et al.
patent: 5797266 (1998-08-01), Brocard et al.
patent: 6205765 (2001-03-01), Iasillo et al.
patent: 6336806 (2002-01-01), Paschereit et al.

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