Method of operating a combined-cycle plant

• US 5,884,470 A
• Filed: 03/31/1997
• Issued: 03/23/1999
• Est. Priority Date: 04/22/1996
• Status: Expired due to Term

• Current Assignee: General Electric Technology GmbH (GE Aerospace)
• Original Assignee: Asea Brown Boveri AG (ABB Limited)
• Inventors: Frutschi, Hansulrich
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US08/831,016
• Time in Patent Office: 722 Days
• Field of Search: 60/39.05, 60/39.17, 60/39.182, 60/39.3, 60/39.53, 60/39.55, 60/728
• US Class Current: 60/783
• CPC Class Codes: F01K 21/047 having at least one combustion gas turbine
• CPC Class Codes: F01K 23/10 with exhaust fluid of one cycle heating the fluid in another cycle F01K17/025 takes precedence
• CPC Class Codes: F02C 6/003 Gas-turbine plants with heaters between turbine stages
• CPC Class Codes: F05D 2260/211 by intercooling, e.g. during a compression cycle
• CPC Class Codes: Y02E 20/16 Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

Abstract

In a method of operating a combined-cycle plant, which essentially comprises a gas-turbine group, a waste-heat steam generator (14) and a steam cycle equipped with a steam turbine (17), the gas-turbine group being operated according to sequential combustion (4, 9), at least one steam quantity (50) proportioned by a control (C) is extracted at a suitable point in terms of pressure in order to increase the operational output of the steam turbine (17). This steam quantity (50) is then fed to the gas-turbine group at a suitable point in such a way that, to maintain the output thus induced, at least the metering (D, E) of a fuel quantity (5, 10) at at least one combustion chamber (4, 9) is influenced.

Claims

1. A method of operating a combined-cycle plant, the plant including a gas-turbine group having a compressor unit, a least one combustion chamber, and at least one gas turbine, a waste-heat steam generator connected to receive exhaust gas from the at least one gas turbine, a steam cycle having at least one steam turbine, and a generator driven by the at least one gas turbine and the at least one steam turbine, the method comprising the steps of:

generating a flow of pressurized steam in the waste-heat steam generator;

feeding the pressurized steam to the at least one steam turbine;

extracting a quantity of partially expanded steam from the at least one steam turbine;

feeding the extracted steam to a combustion air flow in the gas turbine group upstream of the at least one gas turbine;

adjusting a quantity of fuel flow to the at least one combustion chamber for heating the extracted steam,

wherein an output of the gas turbine group is increased by the heated extracted steam, and wherein the exhaust gases of the turbine group provide additional heat to the steam generator to increase a quantity of steam generated in the steam generator; and

feeding the increased quantity of steam to the steam turbine for an increase in output of the steam turbine.

2. The method as claimed in claim 1, wherein the gas turbine group further includes an intercooler arranged between stages of the compressor unit, the method including the steps of controlling an amount of the extracted steam by adjusting a compressor guide-row, by controlling a degree of preheating of intake air to the compressor, and by adjusting a flow quantity of cooling water to the intercooler.

3. The method as claimed in claim 1, wherein the extracted steam is introduced into the gas-turbine group downstream of the compressor unit.

4. The method as claimed in claim 1, wherein the gas-turbine group includes a first combustion chamber upstream of a first turbine, and a second combustion chamber connected downstream of the first turbine and upstream of a second turbine, wherein the method includes the step of introducing exhaust gas from the first turbine into the second combustion chamber for combustion.

5. The method as claimed in claim 4, wherein the exhaust gases from the first turbine enter into the second combustion chamber at a temperature level which lies above the self-ignition temperature of a fuel injected into the second combustion chamber.