Method of controlling a fuel split

US9459008B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9459008-B2
Application numberUS-52313508-A
CountryUS
Kind codeB2
Filing dateJan 15, 2008
Priority dateJan 15, 2007
Publication dateOct 4, 2016
Grant dateOct 4, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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.

First claim

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.

Assignees

Inventors

Classifications

  • for flame failures · CPC title

  • Joint control of separate flows to main and auxiliary burners · CPC title

  • Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title

  • using electronic means · CPC title

  • 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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What does patent US9459008B2 cover?
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.
Who is the assignee on this patent?
Skipper Dorian, Siemens Ag
What technology area does this patent fall under?
Primary CPC classification F23N1/00. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Oct 04 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).