1. Field of the Invention
The present invention relates to a combined-cycle power plant and a steam thermal power plant, which are installed near medium- or small-scaled gas fields and oil fields. More particularly, the present invention relates to a fuel line, a power generating system, and an operating method, which are used for burning raw fuel produced from gas fields and oil fields in a combined-cycle power plant or a steam thermal power plant.
2. Description of the Related Art
In view of environmental pollution in worldwide scale, regulations on exhaust gases from various engines have been urged in progress. Under such situations, natural gas is worthy of note as fuel giving less influence upon environments. Natural gas is transported from a gas field to a consuming area, as shown in
However, progresses are not so noticeable in utilization of accompanying gases produced from medium- or small-scaled or overage gas fields and oil fields that have a difficulty in developing business by using pipelines or liquefying natural gas. In the case where those gas fields and oil fields are far away from markets and invested funds are hard to recover by the method of using pipelines or liquefying natural gas, one effective method is to generate power immediately at a source well, i.e., near a gas field and an oil field, and to supply generated electricity to the consuming area. Also, it is proved that, among various types of power generating systems, combined-cycle power generation has the highest efficiency at the present, shows high reliability and a high availability factor in long-term operation, and is superior in environmental friendliness and economy.
In many cases, raw fuel produced from the source well contains a gas component and a liquid component in a mixed state.
Burning the raw fuel as it is in the gas-liquid mixed state causes problems to be overcome in points of fuel flow control and stable combustion. If the raw fuel is burnt in the gas-liquid mixed state, the combustion temperature rises locally due to a difference in amount of heat generated per unit volume between a liquid and gas to such an extent that constructive parts may be damaged and an amount of generated nitrogen oxides may be increased, thus resulting in deterioration of both reliability and environmental friendliness. In current situations, therefore, raw fuel is required to be burnt in a gas-alone state or a liquid-alone state. One solution of meeting such a requirement is to separate raw fuel produced from the source well into a gas component and a liquid component. This solution enables the separated gas component to be used as fuel for a combined-cycle gas turbine. When using the gas component as the fuel, ingredients harmful to high-temperature constructive parts, such as heavy metals and hydrogen sulfide, must be removed from the gas component. Also, although the remaining liquid component can be refined and separated into volatile oil, naphtha, lamp oil, light oil, heavy oil, etc., it is not economically reasonable to install a refining facility for a medium- or small-scaled source well. On the other hand, because the liquid component is able to generate a very large amount of heat, effective utilization of the liquid component is desired.
It is an object of the present invention to provide a combined-cycle power plant, a steam thermal power plant, and a method for operating the power plant, which are capable of effectively utilizing raw fuel produced from medium- or small-scaled gas fields and oil fields.
To achieve the above object, the combined-cycle power plant of the present invention includes a combined-cycle power generating system comprising a gas turbine, a steam generator, and a steam turbine which are installed in the vicinity of a gas field or an oil field, wherein raw fuel produced from the gas field or the oil field is separated into gas and a liquid, and electricity is generated by using the separated gas as fuel for the gas turbine and the separated liquid as fuel for the steam generator, the generated electricity being supplied to a consuming area.
According to the present invention, it is possible to effectively utilize fuel produced from medium- or small-scaled gas fields and oil fields.
As a basic feature, a combined-cycle power plant of the present invention includes a combined-cycle power generating system comprising a gas turbine, a steam generator, and a steam turbine which are installed in the vicinity of a gas field or an oil field. Raw fuel produced from the gas field or the oil field is separated into gas and a liquid. Electricity is generated by using the separated gas as fuel for the gas turbine and the separated liquid as fuel for the steam generator. The generated electricity is supplied to a consuming area.
Embodiments of the present invention will be described in detail below with reference to the drawings, taking as an example the case of application to raw fuel produced from a gas field.
When natural gas is produced in sufficient amount from the gas field, it is advantageous from the viewpoint of economical profits to transport the produced natural gas to the consuming area by using pipelines or liquefying natural gas, as shown in
In many cases, the raw fuel 2 is produced in a gas-liquid mixed state. However, burning the raw fuel 2 as it is in the gas-liquid mixed state in a combustor of the gas turbine 6 causes problems to be overcome in points of fuel flow control and stable combustion. In current situations, therefore, the raw fuel is required to be burnt in a gas-alone state or a liquid-alone state. Similarly, combustion in the steam generator 8 also requires to be performed in a gas-alone state or a liquid-alone state. If the raw fuel is burnt in the gas-liquid mixed state, pulsations occur in a flow of the fuel and the combustion temperature rises locally due to a difference in amount of heat generated per unit volume between a liquid and gas to such an extent that constructive parts may be damaged and an amount of generated nitrogen oxides may be increased, thus resulting in deterioration of both reliability and environmental friendliness. By separating the raw fuel 2 into the gas component 4 and the liquid component 5 and utilizing the separated gas component 4 as fuel for the gas turbine 6 and the separated liquid component 5 as fuel for the steam generator 8 as in the embodiment of
Raw fuel 2 produced from a gas field 1 is separated into a gas component 4 and a liquid component 5 by a separator 3. The gas component 4 contains water 20, corrosive gases 21 such as hydrogen sulfide, and metals 22 such as vanadium. Therefore, the water 20, the corrosive gases 21, and the metals 22 are removed from the gas component 4 by a removing unit 23. Gas fuel 24 obtained from the removing unit 23 is supplied to a gas turbine. In the gas turbine, atmospheric air 30 is sucked into a compressor 31 and pressurized by the compressor 31 to produce high-temperature and high-pressure air 32. The high-temperature and high-pressure air 32 and the gas fuel 24 are burnt in a combustor 33, and combustion gases are supplied to a turbine 34 to generate motive power. The motive power generated by the gas turbine drives a power generator 35 to generate electricity. Exhaust gases 36 exhausted from the turbine 34 is supplied to an exhaust-heat recovering boiler 40. High-pressure water 42 is also supplied to the exhaust-heat recovering boiler 40 by a water feed pump 41. The high-pressure water 42 is converted to steam 44 through heat exchange between the high-pressure water 42 and the exhaust gases 36, which is performed in a heat exchanger 43 disposed inside the exhaust-heat recovering boiler 40. Exhaust gases 49 having passed through the heat exchanger 43 are discharged to the atmosphere. The steam 44 is supplied to a steam turbine 45 to generate motive power for driving a power generator 46, to thereby generate electricity. The steam 47 exiting the steam turbine 45 is converted to water by a condenser 48, and the converted water is supplied to the water feed pump 41 for circulation. The liquid component 5 obtained from the separator 3 is supplied to a tank 50. The liquid component 5 exiting the tank 50 is burnt as fuel 51 in a burner 52 disposed upstream of the heat exchanger 43. Since burning the liquid component 5 in the burner 52 increases the temperature of the exhaust gases, it is possible to increase an amount of the steam 44 generated in the exhaust-heat recovering boiler 40 and to increase an output of the steam turbine 45.
After the fuel for the gas turbine has been burnt, the resulting combustion gases pass, as turbine operating gases, through high-temperature constructive parts. Therefore, if the fuel contains a sulfur component and/or heavy metals such as vanadium, the high-temperature constructive parts of the gas turbine are corroded and damaged by those impurities. In particular, because a turbine rotor blade is subjected to centrifugal forces with rotations of the gas turbine, there is a risk that if corrosion of the blade is progressed, the blade is fallen off and excessive shaft vibrations are caused due to unbalance in turbine rotation, thus leading to shutdown of the plant. To avoid such a risk, the components adversely affecting the gas turbine are removed by the removing unit 23 to increase reliability of the gas turbine. Also, the operational life of each high-temperature part is prolonged and the interval for routine check can be set to a longer time. In addition, the probability of inevitable shutdown of the plant is reduced and operating efficiency of the plant is increased correspondingly. The liquid component 5 obtained from the separator 3 can be separated into volatile oils, naphtha, lamp oil, light oil, heavy oil, etc. However, oil refining equipment for separating the liquid component 5 requires a large cost and constructing such equipment is not advantageous from the viewpoint of economy. By burning the liquid component 5 as it is without separating the liquid component 5 like this embodiment, a cost increasing factor, e.g., the construction of the oil refining equipment, can be cut. Also, there is a possibility that the liquid component 5 contains metal-corroding components, such as sulfur and vanadium. However, the exhaust-heat recovering boiler 40 is operated under environments where the temperature is lower than that in the gas turbine and constructive parts are not subjected to centrifugal forces. Accordingly, if the corrosive components, such as sulfur and vanadium, are contained at a relatively low concentration, the liquid component 5 can be utilized as it is in the exhaust-heat recovering boiler 40. When the liquid component 5 contains the corrosive components at a relatively high concentration, a unit for removing sulfur, vanadium, etc. from the liquid component 5 may be additionally installed.
Further, since respective rotating shafts of the gas turbine and the steam turbine are of an independent multi-shaft structure, the plant can be operated in any of a mode using the gas turbine alone and a mode using the steam turbine alone. By constructing the tank 50 with a capacity capable of storing a sufficient amount of fuel, the sole operation of the steam turbine 45 can be performed even when a gas fuel supply line is shut off.
Because the corrosive components contained in the gas fuel 24 supplied to the gas turbine are removed by the removing unit 23 and held at a low concentration, corrosion of the exhaust-heat recovering boiler 40 subjected to the exhaust gases from the gas turbine is also suppressed. On the other hand, in the case of the liquid fuel 51 containing the corrosive components at a relatively high concentration, if the liquid fuel 51 is burnt in the exhaust-heat recovering boiler 40, this would raise the necessity of changing the material of the heat exchanger 43 to a highly corrosion-resistant material in order to suppress corrosion of the heat exchanger 43, and would push up the cost. By providing the separate boiler 60 dedicated for the liquid fuel 51 like this embodiment, an increase of the cost required for modifying the exhaust-heat recovering boiler 40 can be avoided. Further, because the rotating shafts of the gas turbine and the steam turbine are independent of each other, the sole operation of the steam turbine can be performed using the separate boiler 60 and the steam turbine 45. Accordingly, the power generation can be continued even during a check period of the gas turbine, and the operating efficiency can be increased correspondingly. Even when the supply of the gas fuel 24 is shut off, the sole operation of the steam turbine 45 can be performed with the liquid fuel 51, and the reliability of the power plant is increased.
With the gas fuel burner 81 and the liquid fuel burner 82 disposed independently of each other, fuel flow control is facilitated and a stable combustion state can be held. It is therefore possible to prevent constructive parts from being damaged with a local rise of the combustion temperature, and to suppress deterioration of both reliability and environmental friendliness, which may be caused with an increase in the amount of nitrogen oxides generated. When the liquid fuel contains the corrosive components at a relatively high concentration, a unit for removing sulfur, vanadium, etc. from the liquid fuel may be additionally installed.
Further, since the amount of the raw fuel and the ratio of the gas component to the liquid component differ depending on individual gas fields and oil fields, the capacities and number of the required gas turbines and steam turbines also differ depending on individual sites. In the case where the concentration of the corrosive components contained in the liquid fuel is so low as to be usable in a gas turbine and the liquid fuel is produced in larger amount than the gas fuel, not only the gas turbine dedicated for the gas fuel, but also a gas turbine dedicated for the liquid fuel may be both installed.
Number | Date | Country | Kind |
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2004-251225 | Aug 2004 | JP | national |
This application is a divisional application of U.S. application Ser. No. 11/213,724, filed Aug. 30, 2005, the entirety of which is incorporated herein by reference.
Number | Date | Country | |
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Parent | 11213724 | Aug 2005 | US |
Child | 12180941 | US |