JP2011038531A - Dual axis gas turbine, control device and control method therefor - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To effectively solve the resonance problem caused by frequency change of a gas generator shaft in a dual axis gas turbine. <P>SOLUTION: The dual axis gas turbine comprises a gas generator including a compressor 7 provided with an inlet guide vane 11 on the air intake side, a combustor 8 for producing a combustion gas by mixing and burning a fuel with compressed air from the compressor, and a high pressure turbine 9 driven and rotated with the combustion gas from the combustor for generating a driving force of the compressor. A controlling means for the inlet guide vane has a first control mode for adjusting the opening degree of the inlet guide vane based on a modified rotational frequency of the gas generator shaft according to the atmospheric temperature at low speed rotation of a gas generator shaft, and a second control mode for adjusting the opening degree of the inlet guide vane for constantly maintaining the actual rotational frequency of the gas generator shaft at high speed rotation of the gas generator shaft. <P>COPYRIGHT: (C)2011,JPO&INPIT

Description

  The present invention relates to a two-shaft gas turbine and a control device and control method thereof, and more particularly to control of a gas generator in a two-shaft gas turbine.

  Generally, a two-shaft gas turbine includes a gas generator including a compressor, a combustor, and a high-pressure turbine, and a low-pressure turbine (power turbine) connected to a load. ) Are separated from the rotational axis of the low-pressure turbine. In the gas generator, the compressor generates compressed air, and in the combustor, fuel is mixed and burned with the compressed air from the compressor to generate combustion gas. The combustion gas generated in the combustor is a high-pressure turbine. Is driven to generate the driving force of the compressor, and then sent to the low-pressure turbine to drive it.

  In such a two-shaft gas turbine, control for adjusting the IGV (Inlet Guide Vane) opening in the compressor based on the corrected rotational speed of the gas generator shaft, that is, the IGV opening control corresponding to the corrected rotational speed is performed. The conventional general gas generator control is applied uniformly regardless of the operation state of the gas generator.

  As for the two-shaft gas turbine, examples disclosed in, for example, Patent Literature 1 to Patent Literature 3 are known.

JP 2007-40171 A JP-A-8-82228 JP 63-212725 A

  As described above, in the conventional two-shaft gas turbine, the IGV opening corresponding to the corrected rotational speed is controlled by the gas generator. In this case, the IGV opening is correlated with the atmospheric temperature as shown in FIG. Therefore, since the operating line changes as shown in FIG. 7B, the rotational speed of the gas generator shaft changes depending on the atmospheric temperature. Further, since the position on the operation line changes, the rotational speed of the gas generator shaft also changes due to the load and the deterioration of the turbine.

  Such a change in the rotation speed of the gas generator shaft causes a resonance problem. That is, the change in the rotation speed of the gas generator shaft increases the possibility that the rotation speed of the gas generator shaft approaches the resonance rotation speed. As the rotational speed approaches the resonance, resonance is generated and the shaft vibration increases. Such a resonance problem is particularly serious in the state of high-speed rotation under high load operation, and the resonance in the high-speed rotation state increases the possibility of damaging the rotor blades of the turbine and the compressor. For this reason, in the control system that uniformly applies the IGV opening control corresponding to the corrected rotation speed, it is necessary to give a structure that can avoid resonance at the assumed rotation speed, or to give the rotor blade a structure that can withstand resonance, This would cause an increase in cost.

  The present invention has been made in the background as described above, and the problem thereof is that a resonance problem associated with a change in the number of revolutions of the gas generator shaft, particularly the state where the gas generator shaft is rotating at a high speed, for a two-shaft gas turbine. It is to be able to effectively solve the resonance problem.

  The corrected engine speed corresponding IGV opening control is effective in avoiding the surging of the compressor. However, the compressor is more stable in the region where the shaft rotation speed, that is, the rotation speed of the gas generator shaft is more than a certain value, and surging does not become a big problem. Therefore, although the IGV opening corresponding to the corrected rotational speed is required when the gas generator shaft is in the low speed rotation, the IGV opening corresponding to the corrected rotational speed is not necessarily required in the state where the gas generator shaft is in the high speed rotation such as the compressor stable region. Does not require control. On the other hand, the resonance problem becomes large when the gas generator shaft is in a high speed rotation such as a compressor stable region.

  Therefore, in an operation state where the gas generator shaft rotates at a low speed (this occurs during start-up operation, stop operation, and low-load operation where the load is below a certain level), the IGV opening control corresponding to the corrected rotation speed is used. In an operation state (high load operation state) in which the shaft rotates at a high speed, control is performed to adjust the IGV opening so as to keep the rotation speed of the gas generator shaft constant, that is, constant shaft rotation speed IGV opening control.

  By using different control modes in accordance with the operating state in this way, the resonance problem can be effectively solved, and the surging of the compressor can be effectively dealt with. That is, when the gas generator shaft rotates at a high speed, where the resonance problem becomes particularly large, the rotational speed of the gas generator shaft is kept constant by controlling the IGV opening with a constant shaft rotational speed. The approaching situation can be effectively avoided, and therefore the resonance problem can be effectively solved. On the other hand, when the gas generator shaft rotates at a low speed, where the surging of the compressor becomes a problem, the surging of the compressor can be avoided by the IGV opening control corresponding to the corrected rotation speed.

  The present invention solves the above problems based on the above-described concept. Specifically, a compressor provided with inlet guide vanes on the air intake side, a combustor that generates combustion gas by mixing and burning fuel with compressed air from the compressor, and rotation by the combustion gas from the combustor In a two-shaft gas turbine having a gas generator including a high-pressure turbine that is driven to generate the driving force of the compressor, the control means for the inlet guide vane is responsive to the atmospheric temperature during low-speed rotation of the gas generator shaft. A first control mode for adjusting the opening degree of the inlet guide vane based on the corrected rotation speed of the gas generator shaft, and the actual rotation speed of the gas generator shaft is kept constant during high-speed rotation of the gas generator shaft. And a second control mode for adjusting the opening degree of the inlet guide vane.

  In other words, the control means for the inlet guide vane includes a first control mode for adjusting an opening degree of the inlet guide vane so as to avoid surging of the compressor when the gas generator shaft rotates at a low speed, and the gas generator shaft. And a second control mode for adjusting the opening degree of the inlet guide vanes so as to avoid resonance of the compressor during high-speed rotation.

  In a state where the rotational speed of the gas generator shaft is large and the IGV opening is small, separation of the air flow is likely to occur at the blades of the compressor, and the performance is likely to deteriorate, and icing is likely to occur. Therefore, it is preferable to avoid such a state. Therefore, in the present invention, in the above-described two-shaft gas turbine, the third control mode can be interposed during the mode transition between the first control mode and the second control mode. In the third control mode, the IGV opening is kept constant regardless of the rotation speed of the gas generator shaft.

  According to the present invention as described above, the resonance problem in the state where the gas generator shaft is rotating at high speed can be effectively solved in the two-shaft gas turbine, and the surging of the compressor can be effectively dealt with. Can do.

1 is a diagram illustrating a configuration of a two-shaft gas turbine according to a first embodiment. FIG. It is a figure which shows the structure of the IGV opening degree control part in 1st Embodiment. It is a figure which shows the relationship between the IGV opening degree in 1st Embodiment, a correction rotation speed, and each actual rotation speed. It is a figure which shows the structure of the 2-shaft type gas turbine by 2nd Embodiment. It is a figure which shows the structure of the IGV opening degree control part in 2nd Embodiment. It is a figure which shows the relationship between the IGV opening degree in 2nd Embodiment, a correction rotation speed, and each real rotation speed. It is a figure which shows the relationship between the IGV opening degree in the case of the conventional gas generator control, a correction rotation speed, and an actual rotation speed.

  Hereinafter, modes for carrying out the present invention will be described. FIG. 1 schematically shows the configuration of a two-shaft gas turbine 1 according to the first embodiment. The two-shaft gas turbine 1 includes a gas generator 2 and an output turbine 3.

  The output turbine 3 includes a low-pressure turbine 4 and a load 5 as main elements, and the load 5 is connected to the low-pressure turbine 4 via an output turbine shaft 6 that is also a rotor thereof.

  On the other hand, the gas generator 2 includes a compressor 7, a combustor 8, a high-pressure turbine 9, and a gas generator control device 10 as main elements.

  The compressor 7 compresses air taken in from the atmosphere to generate compressed air. The compressor 7 is provided with an IGV (inlet guide vane) 11 on the air intake side. The opening degree of the IGV 11 can be changed by the IGV driving device 12, thereby changing the air intake amount of the compressor 7.

  The combustor 8 mixes and burns the fuel 15 supplied from the fuel supply source 13 via the fuel control valve 14 with the compressed air 16 from the compressor 7 to generate combustion gas 17.

  The high-pressure turbine 9 can transmit a driving force to the compressor 7 via a gas generator shaft 18 that is also a rotor, and is driven to rotate by the combustion gas 17 from the combustor 8 to generate the driving force of the compressor 7. To do. The combustion gas 17 whose pressure has been reduced by rotating the high-pressure turbine 9 is sent from the high-pressure turbine 9 to the low-pressure turbine 4 to rotate it.

  The gas generator control device 10 includes a fuel control unit 19 and an IGV opening control unit 20.

  The fuel control unit 19 controls the fuel control valve 14 based on the data from the rotational speed detector 21 that detects the rotational speed of the output turbine shaft 6 and the load state data obtained for the load 5, so that the fuel supply source 13 The supply of fuel 15 to the combustor 8 is controlled.

  The IGV opening control unit 20 controls the opening of the IGV 11 through the control of the IGV driving device 12. In FIG. 2, the structural example of the IGV opening degree control part 20 is shown. The IGV opening control unit 20 in this example includes a first control unit 21, a second control unit 22, an operating state determination unit 23, and a mode selection unit 24.

The first control unit 21 performs control in the first control mode. In the first control mode, IGV opening control corresponding to the corrected rotational speed is performed, and the IGV opening is adjusted based on the corrected rotational speed of the gas generator shaft 18. Here, the corrected rotational speed of the gas generator shaft 18 is the actual rotational speed of the gas generator shaft 18 (which is given by the rotational speed detector 25 that detects the rotational speed of the gas generator shaft 18). It is obtained by standardization with a thermometer 26 for measuring temperature). Specifically, the correction rotational speed is Nt, the actual rotational speed is N, and the atmospheric temperature is T.
Nt = N · [288.15 / (273.15 + T)] ^1/2

  The second control unit 22 executes control in the second control mode. In the second control mode, the shaft rotational speed constant IGV opening degree control is performed, and the IGV opening degree is adjusted so as to keep the rotational speed of the gas generator shaft constant. Here, the rotation speed kept constant by the constant shaft rotation speed IGV opening control is, for example, the rated rotation speed.

  The driving state determination unit 23 determines the driving state based on load data and the like. Specifically, the first operation state (any one of the start operation state, the stop operation state, and the low load operation state) and the second operation state (an operation state other than the first operation state, that is, a high load operation state). It is judged whether it exists in. Here, the low load operation state and the high load operation state are distinguished using the IGV opening degree regarding the stable operation region of the compressed air 16 as a guide. That is, a target IGV opening degree for a stable operation region corresponding to the characteristics of the compressed air 16 is set, and it is determined whether the engine is in a low load operation state or a high load operation state based on the target IGV opening degree.

  The mode selection unit 24 selects a control mode according to the determination result in the operation state determination unit 23. Specifically, the first control unit 21 is activated when it is determined as the first operation state, and the second control unit 22 is activated when it is determined as the second operation state. That is, in the first operating state, the corrected rotational speed corresponding IGV opening control mode (first control mode) is used, and in the second operating state, the shaft rotational speed constant IGV opening control mode (second control mode) is used. Mode selection is performed so that

  As described above, the IGV opening control unit 20 selectively uses the corrected rotation speed corresponding IGV opening control mode and the constant shaft rotation speed IGV opening control mode according to the operating state. FIG. 3 shows the relationship between the corrected rotational speed of the gas generator shaft 18 and the IGV opening (FIG. 3A) in the case of such control by the IGV opening control section 20, and the actual rotational speed of the gas generator shaft 18. And the IGV opening degree relationship ((b) of FIG. 3). As can be seen, the operating line is the same regardless of the atmospheric temperature at low loads, but the corrected rotational speed varies with the atmospheric temperature at high loads. On the other hand, the operating line changes depending on the atmospheric temperature when the load is low, but the rotational speed of the gas generator shaft 18 is constant when the load is high.

  According to such control, the resonance problem, that is, the resonance problem that the possibility of damaging the rotor blades of the turbine or the compressor due to the resonance generated when the rotation speed approaches the resonance rotation speed during the high speed rotation of the gas generator shaft 18 is increased. It can be effectively eliminated, and it can effectively cope with the surging of the compressor at the time of low speed rotation. As a result, the design burden related to the resonance problem can be reduced, and the cost can be reduced.

  Hereinafter, a second embodiment will be described. FIG. 4 schematically shows the configuration of the two-shaft gas turbine 31 according to the second embodiment. The two-shaft gas turbine 31 of the present embodiment has the two-shaft of FIG. 1 except that the gas generator control device 10 includes an IGV opening controller 32 instead of the IGV opening controller 20 in FIG. This is the same as the type gas turbine 1. Therefore, the characteristic configuration of the two-shaft gas turbine 31 will be mainly described below, and the description above is used for the configuration common to the two-shaft gas turbine 1.

  As shown in FIG. 5, the IGV opening degree control unit 32 includes a first control unit 21, a second control unit 22, an operating state determination unit 23, and a mode selection unit 24 similar to those in FIG. 2. In addition to providing, a third control unit 33 is provided.

  The third control unit 33 executes control in the third control mode. In the third control mode, the IGV opening constant holding control is performed to keep the IGV opening constant regardless of the rotation speed of the gas generator shaft 18. The third control mode (IGV opening constant holding control mode) by the third control unit 33 is used for mode transition between the first control mode and the second control mode. That is, the third control unit 33 is activated when the operation state determination unit 23 determines that the operation state transition has occurred with respect to the first operation state or the second operation state, and thereby the IGV opening constant holding control mode. The control at is executed.

  FIG. 6 shows the relationship between the corrected rotational speed of the gas generator shaft 18 and the IGV opening (FIG. 6A) in the case of control by the IGV opening control section 32, and the actual rotational speed of the gas generator shaft 18 and the IGV opening. The degree relationship ((b) of FIG. 6) is shown. As can be seen from this, the control in the IGV opening constant holding control mode can also be performed, so that the IGV opening can be prevented from being reduced when the rotation speed of the gas generator shaft is large. That is, in the state where the rotation speed of the gas generator shaft 18 is large and the IGV opening is small, air flow separation occurs in the blades of the compressor 7 and the performance is easily deteriorated, and icing is also likely to occur. By interposing the third control mode during the mode transition between the control mode and the second control mode, such a situation can be effectively avoided and the reliability can be improved.

  As mentioned above, although the form for implementing this invention was demonstrated, these are only representative examples, This invention can be implemented with various forms in the range which does not deviate from the meaning.

DESCRIPTION OF SYMBOLS 1, 31 Two-shaft gas turbine 2 Gas generator 7 Compressor 8 Combustor 9 High-pressure turbine 11 IGV
DESCRIPTION OF SYMBOLS 12 IGV drive device 15 Fuel 16 Compressed air 17 Combustion gas 20, 32 IGV opening degree control part 21 1st control part 22 2nd control part 23 Operation state determination part 24 Mode selection part 33 3rd control part

Claims (5)

Compressor provided with inlet guide vanes on the air intake side, a combustor for generating combustion gas by mixing fuel with compressed air from the compressor, and the compression driven by the combustion gas from the combustor In a two-shaft gas turbine comprising a gas generator comprising a high-pressure turbine that generates a driving force of the machine,
The control means for the inlet guide vanes includes a first control mode for adjusting an opening degree of the inlet guide vanes based on a corrected rotation speed of the gas generator shaft according to an atmospheric temperature when the gas generator shaft rotates at a low speed, and the gas A two-shaft gas turbine, comprising: a second control mode for adjusting an opening degree of the inlet guide blade so as to keep the actual rotational speed of the gas generator shaft constant during high-speed rotation of the generator shaft. Compressor provided with inlet guide vanes on the air intake side, a combustor for generating combustion gas by mixing fuel with compressed air from the compressor, and the compression driven by the combustion gas from the combustor In a two-shaft gas turbine comprising a gas generator comprising a high-pressure turbine that generates a driving force of the machine,
The inlet guide vane control means includes a first control mode for adjusting an opening degree of the inlet guide vane so as to avoid surging of the compressor during low speed rotation of the gas generator shaft, and high speed rotation of the gas generator shaft. A two-shaft gas turbine comprising a second control mode for adjusting an opening degree of the inlet guide vanes so as to avoid resonance of the compressor sometimes.   The inlet guide vane control means makes the opening degree of the inlet guide vane constant regardless of the number of rotations of the gas generator shaft during mode transition between the first control mode and the second control mode. 3. The two-shaft gas turbine according to claim 1, further comprising a third control mode that is adjusted so as to be maintained. 4. Compressor provided with inlet guide vanes on the air intake side, a combustor for generating combustion gas by mixing fuel with compressed air from the compressor, and the compression driven by the combustion gas from the combustor In a control device for a two-shaft gas turbine comprising a gas generator comprising a high-pressure turbine for generating a driving force of the machine,
A first control mode for adjusting an opening degree of the inlet guide vane based on a corrected rotational speed of the gas generator shaft according to an atmospheric temperature during low-speed rotation of the gas generator shaft; and the gas generator during high-speed rotation of the gas generator shaft A control apparatus for a two-shaft gas turbine, comprising a second control mode for adjusting an opening degree of the inlet guide vanes so as to keep the actual rotational speed of the shaft constant. Compressor provided with inlet guide vanes on the air intake side, a combustor for generating combustion gas by mixing fuel with compressed air from the compressor, and the compression driven by the combustion gas from the combustor In a control method for a two-shaft gas turbine provided with a gas generator including a high-pressure turbine for generating a driving force of the machine,
When the gas generator shaft rotates at a low speed, the opening degree of the inlet guide blade is adjusted based on the corrected rotation speed of the gas generator shaft according to the atmospheric temperature,
A control method for a two-shaft gas turbine, wherein the opening degree of the inlet guide vanes is adjusted so that the actual rotational speed of the gas generator shaft is kept constant when the gas generator shaft rotates at a high speed.

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