Combined cycle power plant with flue gas recirculation

Patent metadata

Field	Value
Publication number	US-9828912-B2
Application number	US-201113116486-A
Country	US
Kind code	B2
Filing date	May 26, 2011
Priority date	May 26, 2010
Publication date	Nov 28, 2017
Grant date	Nov 28, 2017

Abstract

An exemplary method for the operation of a CCPP with flue gas recirculation to reduce NOx emissions and/or to increase the CO2 concentration in the flue gases to facilitate CO2 capture from the flue gases as well as a plant designed to operate is disclosed. To allow a high flue gas recirculation ration (rFRG) an imposed combustion inhomogeneity ratio (ri) is used for flame stabilization. The imposed combustion inhomogeneity ratio (ri) is controlled as function of the flue gas recirculation rate (rFRG) and/or combustion pressure. Oxygen or oxygen enriched air to the gas turbine inlet gases or to the combustor is admixed to enhance operatability.

First claim

What is claimed is:

1. A method for operating a combined cycle power plant having a gas turbine and a heat recovery steam generator with a flue gas recirculation system, the method comprising:
controlling a combustion inhomogeneity ratio for operational burners receiving fuel to combust the fuel as a function of flue gas recirculation rate of flue gases recirculated into a compressor inlet gas of the gas turbine by the flue gas recirculation system, the combustion inhomogeneity ratio being one of:
(i) a calculated pilot ratio that is a ratio of fuel gas burned in a pilot flame relative to a total fuel gas mass flow injected into an operating burner of a combustor,
(ii) a calculated staging ratio that is one of (a) an equivalence ratio of a fuel gas mixture sent to one part of premixed injection locations and an overall equivalence ratio of an operating burner and (b) an equivalence ratio achieved in one group of operating burners of a combustor to an average equivalence ratio of all operating burners of the combustor, and
(iii) a combination of the calculated pilot ratio and the calculated staging ratio; and

controlling the combustion inhomogeneity ratio as a function of at least one of hot gas temperature of the combustor and a compressor pressure that is proportional to combustion pressure via a control band, the control band defining a maximum flue gas recirculation ratio and a minimum flue gas recirculation ratio to only allow adjustment of flue gas recirculation to the compressor inlet via the flue gas recirculation system such that a rate of flue gas recirculation is set so that the flue gas recirculation ratio is within the control band to impose an allowable inhomogeneity ratio as a function of at least one of the combustion pressure and the hot gas temperature of the combustor, the flue gas recirculation ratio being a ratio between flue gas mass flow from the gas turbine that is recirculated to the compressor inlet and total flue gas mass flow of the gas turbine.

2. The method according to claim 1 , comprising:
adjusting the combustion inhomogeneity ratio as a function of measured CO and/or unburned hydrocarbon emissions; and
adjusting an admixing of oxygen or oxygen enriched air with compressor inlet gases as a function of measured CO and/or unburned hydrocarbon emissions; and
adjusting the combustion inhomogeneity ratio as a function of measured combustor pulsations.

3. The method according to claim 1 , comprising:
admixing oxygen or oxygen enriched air to at least one of compressor inlet gases of a gas turbine compressor of the gas turbine and to a combustor of the gas turbine to allow a higher flue gas recirculation rate.

4. The method according to claim 1 , comprising:
providing a target oxygen concentration in compressor inlet gas with compressor inlet gases as a function of the imposed combustion inhomogeneity ratio; and
controlling oxygen concentration in the inlet gas by at least one of variation of the flue gas recirculation rate and admixing of oxygen or oxygen enriched air.

5. The method according to claim 1 , comprising:
adjusting the combustion inhomogeneity ratio and/or adjusting an admixing of oxygen or oxygen enriched air with compressor inlet gases as a function of measured CO and/or unburned hydrocarbon emissions.

6. The method according to claim 1 , comprising:
adjusting the combustion inhomogeneity ratio as a function of measured combustor pulsations.

7. The method according to claim 1 , comprising:
maintaining the flue gas recirculation rate above a minimum value to assure a minimum flow through a CO 2 capture system.

8. The method according to claim 1 , comprising:
providing a target compressor inlet temperature of the gas turbine as a function of relative load and in that the compressor inlet temperature is controlled by adjusting a re-cooling temperature.

9. The method of claim 1 , wherein the compressor pressure is an exit pressure of the compressor.

10. A combined cycle power plant, comprising:
a gas turbine;
a heat recovery steam generator (HRSG) that receives fluid from the gas turbine;
a steam turbine that receives steam from the HRSG;
a flue gas recirculation line with a recirculation flue gas re-cooler, the flue gas recirculation line connecting a downstream end of the heat recovery steam generator to an inlet of a compressor of the gas turbine;
at least one of:
a measurement device to measure at least one of compressor exit pressure and compressor exit temperature,
at least one measurement device to measure at least one of oxygen and CO 2 positioned between a mixing point of recirculated flue gas and ambient air and a compressor of the gas turbine,
at least one measurement device to measure at least one of oxygen and CO 2 positioned downstream of the gas turbine and combustor, and
at least one measurement device to measure at least one of CO and unburned hydrocarbon positioned downstream of the gas turbine and combustor; and

a fuel distribution system configured to impose a controlled flame inhomogeneity for operational burners receiving fuel to combust the fuel by controlling fuel distribution as a function of flue gas recirculation rate of flue gases recirculated into the inlet of the compressor of the gas turbine by the flue gas recirculation line based on a combustion inhomogeneity ratio, the combustion inhomogeneity ratio being one of:
(i) a calculated pilot ratio that is a ratio of fuel gas burned in a pilot flame relative to a total fuel gas mass flow injected into a burner of a combustor,
(ii) a calculated staging ratio that is one of:
(a) an equivalence ratio of a fuel gas mixture sent to one part of premixed injection locations and an overall equivalence ratio of a burner and
(b) an equivalence ratio achieved in one group of burners of a combustor to an average equivalence ratio of all burners of the combustor, and

(iii) a combination of the calculated pilot ratio and the calculated staging ratio, the combustion inhomogeneity ratio being controlled as a function of at least one of hot gas temperature of the combustor and a compressor pressure via a control band that is defined to impose an allowable inhomogeneity ratio as a function of at least one of the combustion pressure and the hot gas temperature of the combustor, the control band configured to define a maximum flue gas recirculation ratio and a minimum flue gas recirculation ratio to limit adjustment of flue gas recirculation to the inlet of the compressor via the flue gas recirculation line such that a rate of flue gas recirculation is set so that the flue gas recirculation ratio is within the control band to impose an allowable inhomogeneity ratio as a function of at least one of the combustion pressure and the hot gas temperature of the combustor, the flue gas recirculation ratio being a ratio between flue gas mass flow from the gas turbine that is recirculated to the compressor inlet and total flue gas mass flow of the gas turbine.

11. The combined cycle power plant according to claim 10 , wherein the gas turbine comprises at least one of:
a pilot stage in at least one burner, and
at least one burner with staged premixed gas injection.

12. The combined cycle power plant according to claim 10 , wherein the gas turbine comprises:
at least one combustor with staged burner groups.

13. The combined cycle power plant according to claim 10 , wherein the gas turbine has a design compressor pressure ratio that is proportional to a temperature of gas exiting the compressor.

14. The combined cycle power plant according to claim 10 , wherein the gas turbine is a sequential combustion g

Assignees

• De La Cruz Garcia Marta
• Lachaux Thierry
• Burdet Andre
• Hellat Jaan
• Ansaldo Energia Switzerland AG

Inventors

• De La Cruz Garcia Marta
• Lachaux Thierry
• Burdet Andre
• Hellat Jaan

Classifications

• F02C3/28

  using a separate gas producer for gasifying the fuel before combustion · CPC title

• F02C9/24

  Control of the pressure level in closed cycles · CPC title

• Y02E20/326

  Cross-Sectional Technologies · mapped topic

• F02C3/34 Primary

  with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle · CPC title

• Y02E20/16

  Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT] · CPC title