USPatent applicationPatented

Combined cycle power plant

Granted 8 Jan 2013 · no office action yet

Application· this page
12/708,371
filed 18 Feb 2010
Publication
Not published
not published
Patent
US 8,347,634
granted 8 Jan 2013

Life of the application

11 dated events
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Abstract

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.

Description

6 parts
›CROSS-REFERENCE TO RELATED APPLICATIONS

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.

›FEDERAL RESEARCH STATEMENT

None.

›BACKGROUND OF THE INVENTION

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.

›BRIEF SUMMARY OF THE INVENTION

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.

›BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

FIG. 1 shows a cross section view of the combined cycle power plant of the present invention.

›DETAILED DESCRIPTION OF THE INVENTION

A combined cycle power plant is shown in FIG. 1 and includes an electric generator 11 connected to a gas turbine engine that includes a compressor 12 , a combustor 13 and a turbine 14 that drives the electric generator 11 and produces electrical power. The turbine 14 exhaust is connected by a passage 15 to a heat recovery steam generator (HRSG) 20 that converts water into steam using the heat from the turbine exhaust 15 . The steam generated is supplied to a steam turbine 21 that is connected to a second generator 22 to produce electrical power.

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.

Claims as granted

8 claims

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Classifications

4 codes
IPC · International Patent Classification
Section F — Mechanical engineering; lighting; heating; weapons
  • F02C1/00
USPC · US Patent Classification
60/77260/39.18260/39.5

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File wrapper

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Pendency
2.9 y
1,055 days filing → grant
Office actions
0
none on record
Examiner
Phutthiwat Wongwian
art unit 3741 · TC 3700
Citations: 6 back · 0 forward

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