Method and system for controlling fuel supply in a combustion turbine engine

A combustion turbine engine having a combustor including an inlet, an outlet, a primary combustion zone and at least one further combustion zone, means for supplying primary fuel to said primary combustion zone, means for supplying other fuel to said at least one further combustion zone, said primary and said other fuel being together the total fuel, and means for regulating the fuel ratio of said primary fuel to said total fuel, said regulating means being arranged to regulate the fuel ratio by:

• a) determining the inlet and outlet temperatures at the inlet and outlet of said combustor;
• b) determining a first value representing a first predetermined property of said combustor from said inlet and outlet temperature;
• c) determining a second value representing a second predetermined property of the primary combustion zone from the current value of said fuel ratio and said first value;
• d) determining the temperature at the outlet of the primary combustion zone from the inlet temperatures and said second value;
• e) comparing the temperature at the outlet of the primary combustion zone with a predetermined temperature, thereby to derive a difference value and generating a control signal dependent on said difference value, and
• f) varying the primary fuel, thereby to vary said fuel ratio the varying of the primary fuel being such as to vary said control signal corresponding to a reduction in said difference value, wherein said first predetermined property is one of:
• the total enthalpy rise in said combustor, the equivalence ratio of said combustor, the fuel/air ratio of said combustor, the temperature rise across said combustor, the fuel flow through said combustor;
• and said second predetermined property is the corresponding one of:
• the enthalpy rise in said primary combustion zone, the equivalence ratio of said primary combustion zone, the fuel/air ratio of said primary combustion zone;
• the temperature rise across said primary combustion zone, or the fuel flow through the primary combustion zone.

A method of scheduling fuel flow to a combustion turbine engine, comprising the steps of putting a plurality of engine fuel flow governors in parallel with each other, letting the governor which outputs the lowest fuel demand signal be the one which schedules the total fuel flow to the engine, characterised in that there are a plurality of combustion stages, defining predetermined temperature limits for the combustion process in each stage of combustion, and individually scheduling fuel flows to the plurality of combustion stages to achieve the lowest fuel flows consistent with the predetermined temperature limits for the corresponding stages of combustion;

• wherein said engine has a combustor including an inlet, an outlet, a primary combustion zone and at least one further combustion zone, the total fuel supplied to the combustor being divided between primary fuel supplied to said primary combustion zone and other fuel supplied to said at least one further combustion zone;
• and the method further includes repeatedly and at predetermined intervals:
• a) determining the inlet and outlet temperatures at the inlet and outlet of said combustor;
• b) determining a first value representing a first predetermined property of said combustor from said inlet and outlet temperature;
• c) determining a second value representing a second predetermined property of the primary combustion zone from the current value of said fuel ratio and said first value;
• d) determining the temperature at the outlet of the primary combustion zone from the inlet temperatures and said second value;
• e) comparing the temperature at the outlet of the primary combustion zone with a predetermined temperature, thereby to derive a difference value and generating a control signal dependent on said difference value, and
• f) varying the primary fuel, thereby to vary said fuel ratio the varying of the primary fuel being such as to vary said control signal corresponding to a reduction in said difference value, wherein
• said first predetermined property is one of:
• the total enthalpy rise in said combustor, the equivalence ratio of said combustor, the fuel/air ratio of said combustor, the temperature rise across said combustor, the fuel flow through said combustor;
• and said second predetermined property is the corresponding one of:
• the enthalpy rise in said primary combustion zone, the equivalence ratio of said primary combustion zone, the fuel/air ratio of said primary combustion zone, the temperature rise across said primary combustion zone, or the fuel flow through the primary combustion zone.