Method of controlling combustion apparatus
US-2016363348-A1 · Dec 15, 2016 · US
US9459008B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9459008-B2 |
| Application number | US-52313508-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 15, 2008 |
| Priority date | Jan 15, 2007 |
| Publication date | Oct 4, 2016 |
| Grant date | Oct 4, 2016 |
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A method of controlling a fuel split of a pilot fuel flow and a main fuel flow in a gas turbine combustor during a load reduction is provided. The rate of change of fuel flow demand is monitored and an additional pilot fuel flow is added. The amount of additional pilot fuel flow depends on the rate of the change in fuel flow demand.
Opening claim text (preview).
The invention claimed is: 1. A method of controlling a fuel split into a pilot fuel flow and a main fuel flow in a gas turbine combustor during a load reduction, the method comprising: monitoring a rate of change of a fuel flow demand; and adding an additional pilot fuel flow, wherein an amount of the additional pilot fuel flow depends on the rate of change of the fuel flow demand. 2. The method of controlling a fuel split as claimed in claim 1 , wherein the additional pilot fuel flow is reduced to zero after the load reduction. 3. The method of controlling a fuel split as claimed in claim 2 , wherein a rate limit is applied to the pilot fuel flow when the amount of the additional pilot fuel flow is reduced to zero. 4. The method of controlling a fuel split as claimed in claim 1 , wherein the additional pilot fuel flow is added when a rate of fuel flow demand is less than a given value. 5. The method of controlling a fuel split as claimed in claim 4 , wherein the given value is a negative value. 6. The method of controlling a fuel split as claimed in claim 1 , further comprising subtracting the additional pilot fuel from the main fuel flow in order to keep a total amount of fuel flow constant. 7. The method of controlling a fuel split as claimed in claim 1 , wherein the load reduction is a rapid load reduction.
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Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion (ignition in gas-turbine plants F02C7/264; pilot flame igniters F23Q9/00) · CPC title
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