None.
1. Field of the Invention
The present invention relates generally to a combined cycle power plant, and more specifically to a power plant with a dirty fuel combustor and a gas turbine engine.
2. Description of the Related Art including information disclosed under 37 CFR 1.97 and 1.98
Combined cycle power plants are well known in which a gas turbine engine drives an electric generator to produce electrical energy. The turbine exhaust is typically at around 400 degrees F., and in a non-combined cycle engine this hot gas exhaust is passed directly to the atmosphere through the stack. In a combined cycle engine, the hot exhaust gas is passed through a heat exchanger to pre-heat inlet air that is passed into the compressor, and thus improves the overall efficiency of the engine. Gas turbine engines are being integrated into regular power plant that uses another fuel, such as coal or natural gas, to produce steam to drive a steam turbine. One major problem with using a gas turbine engine with another power generating fuel is that the fuel, such as coal, produces contaminants that will block film cooling holes in the turbine vanes and blades and cause thermal damage. Another problem is that the combustion of the dirty fuel will also cause corrosion damage to the turbine parts.
A combined cycle power plant with a gas turbine engine integrated with a dirty fuel combustor in the turbine exhaust and the hot gas stream from the dirty combustor is mixed together and then passed through a heat recovery steam generator to produce steam, the steam being passed through a steam turbine to drive a second electric generator. Some of the turbine exhaust is passed directly into the HRSG while the remaining turbine exhaust is passed into the combustor and burned with the dirty fuel.
A combined cycle power plant is shown in
The feature of the present invention is the use of a second combustor 17 that can burn a dirty fuel which is considered a fuel that is not good for burning within the gas turbine engine because of particulates such as coal or other contaminants. Some of the turbine 14 exhaust is diverted through bypass passage 16 to be used to burn with the dirty fuel 18 within the second combustor 17 and produce a hot gas flow 19. A fan 23 is used to increase the pressure of the hot gas flow from the combustor 17 so that the turbine exhaust from line 15 will not flow toward the combustor 17 but into the HRSG 20. The fan 23 can be located in other sections of the flow from the turbine 14 outlet to the HRSG 20 inlet. The hot gas flow 19 is then mixed with the remaining turbine 14 exhaust from passage 15 and delivered into the HRSG to produce the steam for the steam turbine 21. In this particular embodiment, the gas turbine engine can be a large industrial gas turbine (IGT) engine in the order of 200 MWatts while the second combustor can be in the order of 20 MWatts. The second combustor 17 produces a hot gas flow that is mixed with the cooler turbine exhaust in order to prevent the combustion gases from the second combustor 17 from entering into the gas turbine engine. The second combustor 17 allows for a second fuel source to be used in the combined cycle power plant and also increases the efficiency of the gas turbine engine and steam turbine combination.
This application claims the benefit to U.S. Provisional Patent Application Ser. No. 61/153,918 filed on Feb. 19, 2009 and entitled COMBINED CYCLE POWER PLANT.
Number | Name | Date | Kind |
---|---|---|---|
4362013 | Kuribayashi | Dec 1982 | A |
4729217 | Kehlhofer | Mar 1988 | A |
6141956 | Iijima et al. | Nov 2000 | A |
6351935 | Bronicki et al. | Mar 2002 | B1 |
6572674 | Avart et al. | Jun 2003 | B1 |
20050268594 | Kurihara et al. | Dec 2005 | A1 |
Number | Date | Country | |
---|---|---|---|
61153918 | Feb 2009 | US |