1. Field of the Invention
The present invention relates to a gas turbine plant used in a power generation plant and to a method of controlling such a gas turbine plant.
2. Description of the Related Art
FIG. 9 shows the general structure of a conventional single-shaft combined plant (i.e., gas turbine plant).
In the shown single-shaft combined plant, reference numeral 101 indicates a compressor for absorbing and compressing the air, reference numeral 102 indicates a combustor to which combustion oil and combustion air (which has been compressed in the compressor 101) are supplied, reference numeral 103 indicates a gas turbine which rotates when receiving a combustion gas generated by the combustor 102, reference numeral 104 indicates a steam turbine coupled with the gas turbine 103, and reference numeral 105 indicates a generator.
The above gas turbine 103, compressor 101, steam turbine 104, and generator 105 are coupled with each other via a coupling shaft 106.
The drive source for the steam turbine 104 is an exhaust heat recovery boiler 108. The exhaust heat recovery boiler 108 generates steam by using heat collected from the high-temperature exhaust gas output from the gas turbine 103, and introduces the generated steam into the steam turbine 104. Reference numeral 107 indicates a condenser into which exhaust steam from the steam turbine 104 is introduced. The condenser 107 condenses the introduced steam and returns condensate (i.e., condensed water) to the exhaust heat recovery boiler 108.
Reference numeral 109 indicates a fuel valve for controlling the amount of fuel supplied to the combustor 102. This fuel valve 109 is controlled by a controller 110.
The combustor 102 has a structure shown in FIG. 10. In FIG. 10, reference numeral 112 indicates a main combustor, and reference numeral 113 indicates a tail pipe of the main combustor. Fuel is supplied to the main combustor 112 via the fuel valve 109, and air 114 is also supplied to the main combustor 112 from the compressor 101, thereby combusting the fuel.
Reference numeral 115 indicates a bypass valve which is controlled by the controller 110. Depending on the degree of opening of the bypass valve 115, the distribution of air from the compressor 101, that is, the ratio of air supplied to the main combustor 112 to air supplied to the tail pipe 113, is determined.
In the combined plant explained above, when the frequency of the electric power system is changed due to a load change, the frequency must be stabilized by controlling the generated power. The above controller 110 controls the fuel valve 109 so as to recover a suitable frequency, thereby controlling the output of the gas turbine 103.
A concrete example of such a control will be explained below.
In FIG. 11, reference symbol S1 indicates a governor CSO (control signal output) signal output by the controller 110 to the fuel valve 109 so as to control the output of the gas turbine 103.
As shown by reference symbol xe2x80x9caxe2x80x9d, in the normal state, the controller 110 suitably varies the governor CSO signal S1 (corresponding to the output of the gas turbine 103) so as to fix the frequency.
When the amount of load suddenly decreases, the relevant revolution speed suddenly increases, and thus the frequency also increases. In this case, as shown by reference symbol b1, the controller 110 decreases the level of the governor CSO signal S1 so as to avoid a sudden increase of the revolution speed.
On the other hand, when the amount of load suddenly increases, the relevant revolution speed suddenly decreases, and thus the frequency also decreases. In this case, as shown by reference symbol c1, the controller 110 increases the level of the governor CSO signal S1 so as to avoid a sudden decrease of the revolution speed.
However, if the governor CSO signal S1 is suddenly increased, the temperature of the gas turbine 103 suddenly increases. It is not preferable because the gas turbine 103 should have a stress. Therefore, the controller 110 calculates, in advance, a load-limiting CSO signal S2 shown by reference symbol S2. In the normal state, the load-limiting CSO signal S2 has a level higher than that of the governor CSO signal S1 by a predetermined tracking width TW. When the governor CSO signal S1 suddenly increases or decreases, the load-limiting CSO signal S2 is increased or decreased by a specific rate. The controller 110 uses the load-limiting CSO signal S2 as an upper-limit value of the governor CSO signal S1.
Therefore, when the governor CSO signal S1 suddenly decreases, the level of the load-limiting CSO signal S2 is never less than the level of the governor CSO signal S1 (refer to reference symbol b1xe2x80x2); however, when the governor CSO signal S1 suddenly increases, the level of the load-limiting CSO signal S2 may be higher than the level of the governor CSO signal S1 (refer to reference symbol c1xe2x80x2). Therefore, the governor CSO signal S1 is limited so as not to increase with a rate higher than the above-explained specific rate (refer to reference symbol d1).
If the load suddenly increases immediately after a sudden decrease of the load, then the governor CSO signal S1 is controlled in a manner such that the signal suddenly decreases, and then suddenly increases (see FIG. 12).
That is, when the load suddenly decreases, as shown by reference symbol b2, the governor CSO signal S1 decreases without limitation, and the load-limiting CSO signal S2 decreases by a specific rate (see reference symbol b2xe2x80x2).
After that, when the load suddenly increases, the governor CSO signal S1 suddenly increases (see reference symbol c2). In this case, the load-limiting CSO signal S2 continuously decreases-until the load-limiting CSO signal S2 obtains a level 5% higher than that of the governor CSO signal S1 (see reference symbol b2xe2x80x2). The load-limiting CSO signal S2 then enters an increase phase, where the increase is performed at a specific rate because of a sudden increase of the governor CSO signal S1 (see reference symbol c2xe2x80x2). Accordingly, the governor CSO signal S1 is limited so as not to increase with a rate higher than the specific rate (see reference symbol d2), that is, the load-limiting CSO signal S2 functions as an upper-limit level of the governor CSO signal S1.
In the above operation as shown in FIG. 12, in a time period t2 (i.e., before the increase of the governor CSO signal S1 is limited), fuel is also suddenly increased so that the gas turbine 103 has a stress.
In addition, the combustor 102 operates according to the variation of the governor CSO signal S1, as follows: when the load suddenly decreases, the controller 110 limits the amount of fuel supplied to the main combustor 112 by suitably closing the fuel valve 109, thereby suppressing the increase of the relevant revolution speed. In this process, the controller 110 opens the bypass valve 115 so as to maintain a suitable fuel-air ratio, so that the amount of air supplied from the bypass valve 115 to the tail pipe 113 of the combustor increases. Accordingly, the amount of air supplied to the main combustor 112 is decreased, and the suitable fuel-air ratio is maintained.
However, in the conventional combined plant, the opening/closing speed of the bypass valve 115 is fixed. Therefore, the operation of opening the bypass valve 115 cannot follow the sudden closing of the fuel valve 109, so that an excessive amount of air is introduced into the main combustor 112, and this situation causes unstable combustion or the like.
In consideration of the above circumstances, an objective of the present invention is to provide a gas turbine plant and a method of controlling a gas turbine plant, for limiting a sudden increase of the load of the gas turbine, that is, a sudden increase of the amount of fuel, and suppressing a stress imposed on the gas turbine. Another objective of the present invention is to provide a gas turbine plant and a method of controlling a gas turbine plant, for maintaining a suitable fuel-air ratio.
Therefore, the present invention provides a gas turbine plant comprising:
a gas turbine;
a combustor for supplying a combustion gas to the gas turbine;
a fuel valve for controlling an amount of fuel supplied to the combustor, and a controller for controlling the fuel valve, including:
a governor control signal calculating section for calculating a governor control signal for controlling the degree of opening of the fuel valve, based on a revolution speed of the gas turbine;
a load-limiting control signal calculating section for calculating a load-limiting control signal for following the governor control signal, wherein when the governor control signal decreases, the load-limiting control signal is larger than the governor control signal by a predetermined value, while when the governor control signal increases, the increase rate of the load-limiting control signal has a predetermined upper limit; and
a limiting section, into which the governor control signal and the load-limiting control signal are input, for limiting the upper value of the governor control signal by using the load-limiting control signal as an upper limit of said upper value, thereby controlling the fuel valve.
In this gas turbine plant, when the level of the governor control signal (corresponding to the governor CSO signal in the embodiment explained below) decreases (even when the signal suddenly decreases), the load-limiting control signalxe2x96xa1(corresponding to the load-limiting CSO signal in the embodiment explained below) follows the governor CSO signal. When the governor control signal suddenly increases, the load-limiting CSO signal increases at an increase rate having the predetermined upper limit, so that the level of the governor control signal may be larger than that of the load-limiting control signal. Therefore, the limiting section limits the governor control signal by using the load-limiting control signal as the upper limit, thereby avoiding a sudden increase of the output of the gas turbine. As the load-limiting control signal follows the governor control signal during a sudden decrease of the governor control signal, the limitation of the increase rate of the governor control signal becomes quickly effective even when the output of the gas turbine suddenly increases immediately after a sudden decrease of the gas turbine output. This is a distinctive feature in comparison with the conventional example shown by FIG. 12.
The present invention also provides a method of controlling a gas turbine plant comprising a gas turbine, a combustor for supplying a combustion gas to the gas turbine, and a fuel valve for controlling an amount of fuel supplied to the combustor, the method comprising the steps of:
calculating a governor control signal for controlling the degree of opening of the fuel valve, based on a revolution speed of the gas turbine;
calculating a load-limiting control signal for following the governor control signal, wherein when the governor control signal decreases, the load-limiting control signal is larger than the governor control signal by a predetermined value, while when the governor control signal increases, the increase rate of the load-limiting control signal has a predetermined upper limit; and
controlling the fuel valve based on a control signal for limiting the upper value of the governor control signal by using the load-limiting control signal as an upper limit of said upper value.
Also according to this method, the governor control signal is limited by using the load-limiting control signal as the upper limit and the limited signal is output to the fuel valve, thereby avoiding a sudden increase of the output of the gas turbine. In addition, when the level of the governor control signal suddenly decreases, the load-limiting control signal follows it, so that also in this method, the limitation of the increase rate of the governor control signal becomes quickly effective even when the output of the gas turbine suddenly increases immediately after a sudden decrease of the gas turbine output.
The present invention also provides a gas turbine plant comprising:
a gas turbine;
a combustor to which fuel and air are supplied, including:
a main combustor into which the supplied fuel and air are introduced;
a tail pipe, to which a combustion gas is introduced from the main combustor, for introducing the combustion gas to the gas turbine; and
a bypass valve for introducing a portion of the air supplied to the main combustor into the tail pipe;
a fuel valve for controlling an amount of the fuel supplied to the combustor;
a bypass valve controller for controlling the bypass valve at an opening/closing speed according to a variation of the output of the gas turbine; and
a fuel valve controller for controlling the fuel valve.
According to this gas turbine plant, even when the variation of the output of the gas turbine is large, the opening/closing operation of the bypass valve can be quickly performed according to the sudden opening/closing operation of the fuel valve.
In this gas turbine plant, a single controller may function as both the bypass valve controller and the fuel valve controller.
Also in this gas turbine plant, preferably, the bypass valve controller includes:
a bypass valve opening-degree calculating section for calculating a set value of the degree of opening of the bypass valve corresponding to the output of the gas turbine;
an opening/closing speed calculating section for calculating a width of the variation of the output of the gas turbine, and calculating an opening/closing speed of the bypass valve based on the calculated width of the variation; and
a first change rate limiter for controlling the bypass valve by using the opening/closing speed calculated by the opening/closing speed calculating section as a change rate of the set value of the degree of opening of the bypass valve calculated by the bypass valve opening-degree calculating section.
In this structure, the bypass valve opening-degree calculating section calculates a suitable degree of opening of the bypass valve according to the output of the gas turbine. The opening/closing speed calculating section provides the opening/closing speed of the bypass valve, which is used when the degree of opening of the bypass valve is changed from the current degree to one indicated by the relevant set value. The larger the width of the variation of the output of the gas turbine, the higher the calculated opening/closing speed becomes. The first change rate limiter outputs a signal for controlling the bypass valve based on the obtained opening/closing speed.
Also preferably, the opening/closing speed calculating section includes:
a second change rate limiter, into which the output of the gas turbine is input, for converting an increase/decrease change rate of the output of the gas turbine into a predetermined change rate, and outputting a reference output having the predetermined change rate;
a subtracter, into which the output of the gas turbine and the reference output are input, for calculating a difference between the output of the gas turbine and the reference output; and
a change rate calculator for calculating the opening/closing speed of the bypass valve according to the calculated difference.
In this structure, when the output of the gas turbine greatly decreases, the second change rate limiter outputs a signal which decreases with a predetermined change rate (refer to FIGS. 7A and 7B in the embodiment explained below). The subtracter calculates a difference between the output from the second change rate limiter and the output of the gas turbine (refer to FIG. 7C in the embodiment explained below). The larger this difference, the higher the opening/closing speed of the bypass valve (calculated by the change rate calculator) becomes.
The present invention also provides a method of controlling a gas turbine plant which comprises:
a gas turbine;
a combustor to which fuel and air are supplied, including:
a main combustor into which the supplied fuel and air are introduced;
a tail pipe, to which a combustion gas is introduced from the main combustor, for introducing the combustion gas to the gas turbine; and
a bypass valve for introducing a portion of the air supplied to the main combustor into the tail pipe; and
a fuel valve for controlling an amount of the fuel supplied to the combustor, and wherein the method comprises the step of controlling the bypass valve at an opening/closing speed according to a variation of the output of the gas turbine.
Accordingly, even when the variation of the output of the gas turbine is large, the opening/closing operation of the bypass valve can be quickly performed according to the sudden opening/closing operation of the fuel valve.
In this method, the step of controlling the bypass valve may include:
calculating a width of the variation of the output of the gas turbine;
calculating an opening/closing speed of the bypass valve based on the calculated width of the variation; and
controlling the opening/closing operation of the bypass valve by using the calculated opening/closing speed.
When the degree of opening of the bypass valve is changed from the current value to a set value, the opening/closing speed of the bypass valve is necessary. According to this method, the larger the width of the variation of the output of the gas turbine, the higher the calculated opening/closing speed becomes.
In this method, the step of controlling the bypass valve may include:
converting an increase/decrease change rate of the output of the gas turbine into a predetermined change rate;
determining a reference output having the predetermined change rate;
calculating a difference between the output of the gas turbine and the reference output; and
determining the calculated difference as the width of the variation of the output of the gas turbine.
Also in this case, even when the output of the gas turbine greatly decreases, a reference output having the predetermined change rate is determined in advance (refer to FIGS. 7A and 7B in the embodiment explained below), and a difference between the reference output and the output of the gas turbine (corresponding to the difference between FIGS. 7A and 7B) is calculated. The larger this difference, the higher the opening/closing speed of the bypass valve becomes.
As explained above, according to the present invention, the upper value of the governor control signal is limited by the load-limiting control signal, thereby preventing a sudden increase of the temperature of the gas turbine. In addition, the limitation of the governor control signal by using the load-limiting control signal becomes quickly effective, thereby reducing the stress imposed on the governor control signal, in comparison with the conventional gas turbine plant.
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