Combustion device with pulsed fuel split

Patent metadata

Field	Value
Publication number	US-9822710-B2
Application number	US-201113879056-A
Country	US
Kind code	B2
Filing date	Sep 30, 2011
Priority date	Oct 13, 2010
Publication date	Nov 21, 2017
Grant date	Nov 21, 2017

Abstract

It is described a combustion device control unit and a combustion device, e.g. a gas turbine, which determine on the basis of at least one operating parameter whether the combustion device is in a predefined operating stage. In response hereto, there is generated a control signal configured for setting a ratio of at least two different input fuel flows to a predetermined value (psc 1 , psc 3 ) for a predetermined time (dt) in case the combustion device is in the predefined operating stage.

First claim

The invention claimed is:

1. A control unit of a combustion device, comprising:
a control input for receiving at least one operating parameter indicating an operation of the combustion device; and
a control output for outputting a control signal for controlling at least two different input fuel flows to the combustion device;
wherein the control unit is configured to determine whether the combustion device is in a predefined operating stage based on the at least one operating parameter,
wherein the control unit is configured to generate the control signal to set a ratio of the at least two different input fuel flows to a predetermined value for a predetermined time in case the combustion device is in the predefined operating stage,
wherein the ratio of the at least two different input fuel flows is set to the predetermined value by changing the ratio of the at least two different input fuel flows from a present value to the predetermined value in a stepwise manner, and
wherein the ratio of the at least two different input fuel flows is set to the predetermined value for the predetermined time comprising a pulse shaped temporal change of the ratio of the at least two different input fuel flows.

2. The control unit according to claim 1 , wherein after the predetermined time the ratio of the at least two different input fuel flows is set to a value that corresponds to a control regime applied before setting the ratio of the at least two different input fuel flows to the predetermined value.

3. The control unit according to claim 1 , wherein the at least two different input fuel flows include:
a main fuel flow to a main combustion region of a combustor of the combustion device; and
a pilot fuel flow to a pilot region of the combustor of the combustion device.

4. The control unit according to claim 1 , wherein the at least one operating parameter comprises at least one of a temperature and a pressure.

5. A combustion device, comprising:
a combustor; and
a control unit according to claim 1 .

6. The combustion device according to claim 5 , further comprising a fuel split device for controllably splitting a supply fuel flow into the at least two different input fuel flows to the combustor.

Assignees

• Brickwood Gavin
• Bulat Ghenadie
• Siemens Ag

Inventors

• Brickwood Gavin
• Bulat Ghenadie

Classifications

• F23N2241/20

  Gas turbines · CPC title

• F23R2900/00013

  Reducing thermo-acoustic vibrations by active means · CPC title

• F23R3/34

  Feeding into different combustion zones · CPC title

• F23R2900/03281

  Intermittent fuel injection or supply with plunger pump or other means therefor · CPC title

• F02C9/28 Primary

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