JP3491967B2 - Gas turbine exhaust gas temperature control device - Google Patents

Description

Detailed Description of the Invention

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a gas turbine exhaust gas temperature control device for controlling the exhaust gas temperature of a gas turbine in a combined cycle power plant.

[0002]

2. Description of the Related Art Generally, a combined cycle power plant is constructed by connecting a gas turbine and a steam turbine with one shaft and connecting a generator with this shaft.

That is, the air compressed by the air compressor is supplied to the combustor together with the fuel for combustion, and the combustion gas from the combustor drives the gas turbine. The exhaust gas that has finished its work in the gas turbine is guided to the exhaust heat recovery boiler, and is heat-exchanged with the exhaust heat recovery boiler to generate steam. Then, the steam drives the steam turbine.

In such a combined cycle power generation plant, since the steam supplied to the steam turbine is generated by the exhaust gas of the gas turbine, it is necessary to control the temperature of the exhaust gas of the gas turbine to be constant.

FIG. 6 shows a block diagram of a conventional gas turbine exhaust gas temperature control device. The gas turbine exhaust gas temperature control device has set value generation means, fuel flow rate control means, and air flow rate control means. First, the set value generating means is for obtaining an exhaust gas temperature set value, and comprises an exhaust gas temperature control set value function generator 21. That is, the discharge air pressure a input from the discharge air pressure sensor 10 of the air compressor is input to the exhaust gas temperature control set value function generator 21 to obtain the exhaust gas temperature set value b. Here, the exhaust gas temperature control set value function 21 is a function determined so that the gas turbine inlet temperature is operated in a temperature range in which the material of the gas turbine is allowed, and is the discharge air pressure a of the air compressor and the gas turbine. It is determined from the relationship between the exhaust gas temperature and the gas turbine inlet temperature.

Next, the fuel flow rate control means controls the fuel flow rate control valve (GCV) 1 so that the exhaust gas temperature j detected by the exhaust gas temperature sensor 11 becomes the exhaust gas temperature set value b. That is, the control of the fuel flow rate control valve 1 is performed as follows. The exhaust gas temperature j input from the exhaust gas temperature sensor 11 is subtracted from the exhaust gas temperature set value b, and the obtained exhaust gas temperature control deviation d is sent to the valve controller 25 via the PI controller 23. The valve controller 25 uses the opening command e of the fuel flow control valve 1 corresponding to the deviation.
Is output to control the fuel flow control valve 1 so that the exhaust gas temperature becomes the exhaust gas temperature set value b. In this case, the exhaust gas temperature decreases when the fuel flow rate is reduced, and the exhaust gas temperature increases when the fuel flow rate increases.

On the other hand, the air flow rate control means controls the inlet guide vanes 2 of the air compressor so that the exhaust gas temperature j detected by the exhaust gas temperature sensor 11 becomes a value g obtained by adding a bias value to the exhaust gas temperature set value b. To control. That is, the inlet guide vane (IGV) 2 of the air compressor is controlled as follows. A value obtained by subtracting the bias value f output from the bias generation circuit 22 from the exhaust gas temperature set value b is set as the set value g. Then, the deviation h obtained by subtracting the exhaust gas temperature j input from the exhaust gas temperature sensor 11 is input to the valve controller 26 via the PI controller 24, and the valve controller 26 outputs an opening command i corresponding to the deviation. , Control the inlet guide vanes (IGV) 2 of the air compressor. When the inlet guide vane (IGV) 2 opens, the amount of air flowing into the gas turbine increases, so the exhaust gas temperature decreases, and when the inlet guide vane (IGV) 2 closes, the exhaust gas temperature rises.

Here, the air flow rate control means suppresses the rise of the exhaust gas temperature by opening the inlet guide vane (IGV) 2 at first, and the fuel flow rate control valve 1 after the inlet guide vane (IGV) 2 is fully opened. Thus, the exhaust gas temperature is controlled.

The equipment downstream of the gas turbine is determined by the heat balance based on the amount of heat exhausted from the gas turbine. That is, the main steam temperature, the main steam pressure, the denitration catalyst inlet gas temperature, and the exhaust gas recovery boiler outlet gas temperature are determined by the exhaust heat amount of the gas turbine and are not individually controlled.

[0010]

However, in the gas turbine exhaust gas temperature control device for such a combined cycle power plant, the exhaust gas temperature control of the gas turbine is controlled so that the gas turbine inlet temperature does not exceed the allowable value. However, there is a possibility that a part of the equipment on the downstream side may reach a high temperature exceeding the design value. That is, if the heat balance changes due to the deterioration of the heat exchange performance in the exhaust heat recovery boiler over time, the temperature of the gas turbine exhaust gas does not change, but there may be places in the downstream equipment where the temperature exceeds the design value. In such a case, the service life of downstream equipment may be accelerated.

That is, although the amount of steam generated in the exhaust heat recovery boiler is reduced due to the deterioration of the heat exchange performance, the temperature of the gas turbine exhaust gas does not change, so the temperature of the main steam supplied to the steam turbine becomes high and the steam turbine The allowable temperature is exceeded. Further, when the performance of the heat exchanger deteriorates, the temperature of the exhaust gas does not decrease, so the temperature of the exhaust gas entering the denitration device exceeds the design point of the denitration catalyst, and the life of the denitration catalyst is consumed.

On the other hand, since the denitration performance of the denitration catalyst changes depending on the temperature, the denitration performance is lowered at a temperature exceeding the design point. Further, the gas temperature at the exhaust heat recovery boiler outlet also rises, which exceeds the design point of the chimney and consumes the life of the chimney.

An object of the present invention is to provide a gas turbine exhaust gas temperature control device which does not consume the life of such equipment downstream of the gas turbine.

[0014]

According to a first aspect of the present invention, air compressed by an air compressor is supplied to a combustor together with a fuel for combustion, and a combustion gas from the combustor drives a gas turbine. Gas that controls the exhaust gas temperature of the gas turbine of the combined cycle power generation plant that guides the exhaust gas that has finished work in the gas turbine to the exhaust heat recovery boiler and drives the steam turbine with the steam generated in the exhaust heat recovery boiler In a turbine exhaust gas temperature control device, a set value generating means for generating a first exhaust gas temperature set value of the gas turbine based on a discharge pressure of the air compressor, and a process amount downstream of the gas turbine exceeds a specified value. The second exhaust gas temperature set value from the set value generating means is corrected based on the process amount measured by the device so as not to A setting value correcting means for outputting a flue gas temperature setting value, the exhaust gas temperature and the second of said gas turbine
Fuel flow rate control means for controlling the flow rate of fuel to be supplied to the combustor based on the deviation from the exhaust gas temperature set value, and the exhaust gas temperature of the gas turbine and the second exhaust gas temperature set value including a bias value. The air flow rate control means for controlling the flow rate of the air supplied to the combustor based on the deviation from the exhaust gas temperature set value of No. 3 is provided.

The invention of claim 2 is characterized in that the steam temperature generated in the exhaust heat recovery boiler is used as the process amount downstream of the gas turbine.

The invention of claim 3 is characterized in that the inlet gas temperature of the denitration device in the exhaust heat recovery boiler is used as the process amount downstream of the gas turbine.

The invention of claim 4 is characterized in that the outlet gas temperature of the exhaust heat recovery boiler is used as the process amount downstream of the gas turbine.

The invention of claim 5 is characterized in that the steam pressure generated in the exhaust heat recovery boiler is used as the process amount in the downstream of the gas turbine.

According to a sixth aspect of the present invention, as the process amount in the downstream of the gas turbine, the steam temperature generated in the exhaust heat recovery boiler, the steam pressure generated in the exhaust heat recovery boiler, and the inlet gas temperature of the denitration device in the exhaust heat recovery boiler are used. Detecting a process amount of any two or more of the exhaust gas temperatures of the exhaust heat recovery boiler, and correcting the exhaust gas temperature set value from the set value generation means so that any detected process amount does not exceed the specified value. The feature is that the value is added.

[0020]

According to the present invention, the temperature and pressure, which are the process quantities of the temperature-limited part of the equipment downstream of the gas turbine, are measured, and the exhaust gas temperature set value from the set value generation means is set so as not to exceed the limit value. The gas turbine exhaust gas temperature control is performed by adding the correction value to. As a result, it becomes possible to operate the equipment downstream of the gas turbine without consuming excessive life.

[0021]

EXAMPLES Examples of the present invention will be described below. First, FIG. 5 shows a system configuration diagram of a combined cycle power generation plant to which the present invention is applied. The air is taken into the air compressor 33 via an inlet guide vane (IGV) 2 provided at the inlet of the air compressor 33. The air compressed by the air compressor 33 is sent to the combustor 34.

On the other hand, the fuel is a fuel flow control valve (GCV) 1
And is taken into the combustor 34. And the combustor 3
At 4, the fuel and air are mixed and burned, and the combustion gas is sent to the gas turbine 35, and the combustion gas drives the gas turbine 35. The combustion gas that has finished its work in the gas turbine 35 becomes high-temperature exhaust gas, and the exhaust heat recovery boiler (H
After being guided to the RB) 36 and exchanging heat with the feed water, it is discharged to the atmosphere from the chimney 38 through the denitration catalyst 37 of the denitration device.

The feed water sent from the condenser 41 to the exhaust heat recovery boiler 36 by the feed water pump 43 enters the drum 42 after being heated by the economizer 52 and becomes steam in the evaporator 51. Return to drum 42. Further, the steam of the drum 42 becomes superheated steam in the superheater 50 and is guided to the steam turbine 40,
After driving the steam turbine 40 to perform work, the condenser 41
Then go back to the water.

Here, in order to detect the process amount downstream of the gas turbine 35, the main steam temperature sensor 12, the denitration device inlet gas temperature sensor 13, the exhaust heat recovery boiler outlet gas temperature sensor 14, and the main steam pressure sensor 15 are provided. It is provided.

FIG. 1 is a block diagram showing the first embodiment of the present invention. The first embodiment is different from the conventional one shown in FIG. 6 in that a set value correction means for adding a correction value o to the exhaust gas temperature set value b from the set value generation means is provided.

The set value correction means is the main steam temperature sensor 12
The deviation m between the main steam temperature k from the main steam temperature k and the main steam temperature specified value 1 from the signal generator 20 is input to the PI controller 28 via the limiter circuit 27 to obtain the correction value o. That is, the correction value o is set to the exhaust gas temperature set value b from the set value generation means so that the main steam temperature as the process amount downstream of the gas turbine 35 does not exceed the specified value.
Is added.

This will be described in detail below. The main steam temperature k input from the main steam temperature sensor 12 is subtracted from the main steam temperature specified value l given by the signal generator 20,
Get the deviation m. The limiter circuit 27 is set to cut off an input value of 0 or less, and outputs the main steam temperature deviation n when the deviation m is positive, that is, when the main steam temperature k exceeds the main steam temperature specified value l. . The PI controller 28 receives the signal n and outputs the correction value o which is the exhaust gas temperature control bias value.

On the other hand, using the exhaust gas temperature control set value p obtained by subtracting the correction value o from the exhaust gas temperature control set value b output from the exhaust gas temperature control set value function 21 of the set value generating means, the fuel flow control valve 1 And the inlet guide vanes (IGV) 2 of the air compressor.

In the first embodiment, the exhaust heat recovery boiler 3 is used as a process amount downstream of the gas turbine 35.
Although the temperature of the main steam generated in 6 is used, the same applies when the pressure of the main steam generated in the exhaust heat recovery boiler 36 is used.

As a result, when the main steam temperature k exceeds the main steam temperature specified value l, a negative bias is applied to the exhaust gas temperature control set value p, the exhaust gas temperature drops, and the main steam temperature k does not exceed the specified value l. To be driven.

Therefore, since the main steam temperature k is controlled so as not to exceed the specified value l, it becomes possible to operate the steam turbine 40 within a design allowable range and suppress excessive life consumption.

Next, FIG. 2 shows a second embodiment of the present invention. In the second embodiment, an exhaust gas temperature control bias function generator 29 is provided instead of the limiter circuit 27 and the PI controller 28 in the first embodiment shown in FIG.

Exhaust gas temperature control bias function generator 29
Is to calculate the amount of decrease in the exhaust gas temperature of the gas turbine required to make the deviation zero from the main steam temperature deviation m. In this embodiment, the exhaust gas temperature control bias value o is used as the exhaust gas temperature control value. It is configured to subtract from the set value b. As a result, the same effect as that of the first embodiment shown in FIG. 1 can be obtained.

FIG. 3 shows a third embodiment of the present invention. In the third embodiment, the inlet gas temperature of the denitration device in the exhaust heat recovery boiler 36 is used as the process amount downstream of the gas turbine 35. That is, the denitration catalyst inlet gas temperature sensor 13 is provided in place of the main steam temperature sensor 12 in the second embodiment shown in FIG. As a result, the exhaust gas temperature can be controlled so that the inlet gas temperature q of the denitration catalyst 37 does not exceed the specified value l, and excessive life consumption of the denitration catalyst 37 can be avoided.

FIG. 4 shows a fourth embodiment of the present invention. In the fourth embodiment, the outlet gas temperature of the exhaust heat recovery boiler 36 is used as the process amount downstream of the gas turbine 35. That is, in the fourth embodiment, the exhaust gas heat recovery boiler outlet gas temperature sensor 14 is provided in place of the main steam temperature sensor 12 in the second embodiment of FIG. As a result, the exhaust gas temperature can be controlled so that the outlet gas temperature t of the exhaust heat recovery boiler 36 does not exceed the specified value l, and excessive life consumption of the chimney can be avoided.

Further, as the process amount in the downstream of the gas turbine 35, the steam temperature generated in the exhaust heat recovery boiler 36, the steam pressure generated in the exhaust heat recovery boiler 36, the inlet gas temperature of the denitration device in the exhaust heat recovery boiler 36, A process amount of any two or more of the outlet gas temperatures of the exhaust heat recovery boiler 36 is detected, and the exhaust gas temperature set value from the set value generation means is corrected so that any detected process amount does not exceed the specified value. You may make it consider a value. In this case, excessive life consumption can be avoided for any equipment downstream of the gas turbine 35.

[0037]

As described above, according to the present invention, when the temperature of the equipment downstream of the gas turbine is limited, the gas turbine exhaust gas can be operated so as not to exceed the limit value. It is possible to provide a temperature control device and avoid excessive lifetime consumption of equipment downstream of the gas turbine.

[Brief description of drawings]

FIG. 1 is a block configuration diagram showing a first embodiment of the present invention.

FIG. 2 is a block diagram showing a second embodiment of the present invention.

FIG. 3 is a block configuration diagram showing a third embodiment of the present invention.

FIG. 4 is a block diagram showing a fourth embodiment of the present invention.

FIG. 5 is a system configuration diagram of a combined cycle power generation plant to which the present invention is applied.

FIG. 6 is a block diagram showing a conventional example.

[Explanation of symbols]

1 Fuel flow control valve 2 Air compressor inlet guide vanes 10 Air compressor discharge air pressure sensor 11 Gas turbine exhaust gas temperature sensor 12 Main steam temperature sensor 13 DeNOx catalyst inlet temperature sensor 14 Exhaust heat recovery boiler outlet gas temperature sensor 15 Main steam pressure sensor 33 air compressor 34 Combustor 35 gas turbine 36 Exhaust heat recovery boiler 37 DeNOx catalyst 38 chimney 39 generator 40 steam turbine 41 condenser 42 drums 43 Water pump

Continuation of the front page (56) Reference JP-A-1-285608 (JP, A) JP-A-3-70804 (JP, A) JP-A-64-66405 (JP, A) JP-A-58-124010 (JP , A) JP 58-107805 (JP, A) (58) Fields investigated (Int.Cl. ⁷ , DB name) F01D 1/00-21/20 F01K 1/00-27/02 F02C 1/00 -9/58 F23R 3/00-7/00

Claims (6)

(57) [Claims] 1. The air compressed by an air compressor is supplied to a combustor together with a fuel for combustion, the combustion gas from the combustor drives a gas turbine, and exhaust gas exhausted from the gas turbine is exhausted. In a gas turbine exhaust gas temperature control device for controlling the exhaust gas temperature of the gas turbine of a combined cycle power plant, which guides to a heat recovery boiler, and drives a steam turbine with steam generated in the exhaust heat recovery boiler, the air compressor Set value generating means for generating the first exhaust gas temperature set value of the gas turbine based on the discharge pressure of the gas turbine, and the process amount in the downstream of the gas turbine has a specified value.
To the process amount measured by the equipment so as not to exceed
On the basis of the first exhaust gas temperature setting from the set value generating means.
Setting to output the second set value of exhaust gas temperature with the fixed value corrected
Value correction means, fuel flow rate control means for controlling the flow rate of fuel supplied to the combustor based on the deviation between the exhaust gas temperature of the gas turbine and the second exhaust gas temperature set value, and the exhaust gas temperature of the gas turbine the third exhaust gas temperature setting in consideration a bias value to the second exhaust gas temperature setting value
A gas turbine exhaust gas temperature control device , comprising: an air flow rate control unit that controls an air flow rate to be supplied to the combustor based on a deviation from a value . 2. The gas turbine according to claim 1, wherein the set value correcting means uses a steam temperature generated in the exhaust heat recovery boiler as a process amount downstream of the gas turbine. Exhaust gas temperature control device. 3. The set value correction means uses the inlet gas temperature of a denitration device in the exhaust heat recovery boiler as the process amount downstream of the gas turbine. Gas turbine exhaust gas temperature control device. 4. The gas turbine exhaust gas according to claim 1, wherein the set value correction means uses the outlet gas temperature of the exhaust heat recovery boiler as a process amount downstream of the gas turbine. Temperature control device. 5. The gas turbine according to claim 1, wherein the set value correction means uses the steam pressure generated in the exhaust heat recovery boiler as a process amount downstream of the gas turbine. Exhaust gas temperature control device. 6. The set value correction means, as a process amount in the downstream of the gas turbine, a steam temperature generated in the exhaust heat recovery boiler, a steam pressure generated in the exhaust heat recovery boiler, and an exhaust heat recovery boiler in the exhaust heat recovery boiler. Any two or more process amounts of the inlet gas temperature of the denitration device and the outlet gas temperature of the exhaust heat recovery boiler are detected, and the set value generating means is used to prevent any detected process amount from exceeding a specified value. 2. The gas turbine exhaust gas temperature control device according to claim 1, wherein a correction value is added to the exhaust gas temperature set value of.