EP3168434B1 - Method of controlling a steam turbine and steam turbine plant - Google Patents
Method of controlling a steam turbine and steam turbine plant Download PDFInfo
- Publication number
- EP3168434B1 EP3168434B1 EP16199217.7A EP16199217A EP3168434B1 EP 3168434 B1 EP3168434 B1 EP 3168434B1 EP 16199217 A EP16199217 A EP 16199217A EP 3168434 B1 EP3168434 B1 EP 3168434B1
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- European Patent Office
- Prior art keywords
- temperature
- rotor
- steam turbine
- stress
- spt
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- 238000000034 method Methods 0.000 title claims description 15
- 238000009826 distribution Methods 0.000 claims description 27
- 230000001052 transient effect Effects 0.000 claims description 23
- 238000012937 correction Methods 0.000 claims description 17
- 238000012545 processing Methods 0.000 claims description 7
- 230000035882 stress Effects 0.000 description 39
- 239000007789 gas Substances 0.000 description 10
- 238000011084 recovery Methods 0.000 description 3
- 238000013459 approach Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000004393 prognosis Methods 0.000 description 2
- 206010063493 Premature ageing Diseases 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000002547 anomalous effect Effects 0.000 description 1
- 238000009529 body temperature measurement Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K7/00—Steam engine plants characterised by the use of specific types of engine; Plants or engines characterised by their use of special steam systems, cycles or processes; Control means specially adapted for such systems, cycles or processes; Use of withdrawn or exhaust steam for feed-water heating
- F01K7/16—Steam engine plants characterised by the use of specific types of engine; Plants or engines characterised by their use of special steam systems, cycles or processes; Control means specially adapted for such systems, cycles or processes; Use of withdrawn or exhaust steam for feed-water heating the engines being only of turbine type
- F01K7/165—Controlling means specially adapted therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D19/00—Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D19/00—Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
- F01D19/02—Starting of machines or engines; Regulating, controlling, or safety means in connection therewith dependent on temperature of component parts, e.g. of turbine-casing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
- F01K13/00—General layout or general methods of operation of complete plants
- F01K13/02—Controlling, e.g. stopping or starting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/81—Modelling or simulation
Definitions
- the steam turbine 5 which in the example described comprises a high pressure section 5a and a medium-low pressure section 5b, receives a flow of high-pressure steam Q HP and a flow of medium-low pressure steam Q IP from the heat-recovery boiler 10 and supplies a flow of steam to the condenser 11 through the exhaust of the medium-low pressure section 5b and through a bypass system of a known type and not shown here for simplicity.
- the gas turbine regulator 16 receives the partial power reference W TG and acts on the actuator assembly 13 so that the gas turbine 5 provides the required power.
- the steam turbine regulator 17 is based on the use of a simplified model of the rotor 5c of the steam turbine 5 to determine the temperature distribution and the stress distribution.
- the rotor 5c is represented by the simplified model M in the form of a homogeneous and isotropic cylinder (a cross-section of which is shown in figure 2 ) with uniform thermal conductivity, immersed in a steam flow with working temperature TW set at a distance DB from the axis A of the rotor 5c itself.
- the rotor 5c may be represented with a radius R0 given by an average of the distance of the rotor blades from the axis A in the high pressure section 5a.
- the approximate values of the stresses determined on the basis of the simplified model M described are in a constant ratio with the values of the same stresses as determined accurately using, for example, finite element methods.
- the actual values of the stresses can be obtained with good approximation by the values calculated with the simplified model M of the rotor 5c by applying a correction factor which is constant and independent of temperature.
- the use of the simplified model M to determine temperature distributions and stress distributions does not represent a significant increase as regards the processing capacity of the entire system. It is therefore possible to monitor in real time conformity of instantaneous stresses with the defined threshold criteria.
- the correction factor may be determined once and for all during the design phase.
- the value of the corrected maximum instantaneous stress ⁇ MAXC is then compared by the comparison module 27 with the stress threshold ⁇ TH received from section 21c of the memory 21.
- the stress threshold ⁇ TH may be determined based on a limit region, for example defined on the basis of Von Mises or Tresca criteria.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Control Of Turbines (AREA)
Description
- The present invention relates to a method of controlling a steam turbine and steam turbine plant.
- As is known, the start-up phase of a steam turbine may prove critical because of the forces induced on the rotor by both the inertia of the system and the considerable temperature fluctuations. The temperature fluctuations are due to the fact that the steam temperature should increase to a steady state value in a relatively short time, considering the mass and the geometry of the rotor.
- In order to prevent problems and conditions that could result in damage or premature ageing of the rotor, profiles for load acceptance and steam temperature increase during equipment start-up have been studied which ensure, at least theoretically, that dangerously high stresses are avoided. It is however appropriate to maintain monitoring of the rotor temperature during operation and implement control actions to reduce stress levels when necessary.
- A significant problem derives from the difficulty of detecting the temperature distribution in the rotor, which is not suitable to accommodate sensors. In order to overcome this, temperature estimates derived from measurements on the stator part are normally used. Estimates of this type are however not very precise and have a significant margin of error. Hence, on the one hand the limited precision makes it necessary to maintain a conservative approach in the design of the profiles for load acceptance and temperature increase, to the detriment, however, of equipment performance. On the other hand, even a reasonably conservative approach cannot prevent with sufficient confidence the occurrence of anomalous conditions as a result of which danger or damage may occur because of stresses inside the rotor. Control actions based on estimates derived from stator temperature measurements may thus not be sufficient to respond in a timely manner and to ensure that the machine is operated in conditions of safety.
- According to a method of controlling a steam turbine disclosed in
DE 10 2004 058171 A1JP H09 317404 A US 2005/085949 A1 . - The purpose of the present invention is therefore to provide a method of controlling a steam turbine and steam turbine plant that make it possible to overcome or at least mitigate the limitations described above.
- According to the present invention a method of controlling a steam turbine and steam turbine plant is provided as defined respectively in
claims - The present invention will now be described with reference to the accompanying drawings which illustrate a non-limiting embodiment example, wherein:
-
figure 1 is a simplified block diagram of a steam turbine plant in accordance with an embodiment of the present invention; -
figure 2 illustrates a simplified model used in the plant offigure 1 ; -
figure 3 shows a more detailed block diagram of a portion of the plant offigure 1 ; -
figure 4 is a graph that illustrates quantities relating to the plant offigure 1 . - As shown in
figure 1 , a combined cycle power plant for the production of electrical energy comprises a gas turbine set 3, asteam turbine 5, twogenerators steam turbine 5 and connected to a distribution network (not shown), a heat-recovery boiler 10, which operates as a steam generator, acondenser 11 and acontrol apparatus 12. Theplant 1 also has anactuator assembly 13 and anactuator assembly 14, on both of which thecontrol apparatus 12 acts so as to respectively control the gas turbine set 3 and thesteam turbine 5. - The gas turbine set 3 produces a flow of hot exhaust gases, which is conveyed to the heat-
recovery boiler 10 and is used for the production of steam. - The
steam turbine 5, which in the example described comprises ahigh pressure section 5a and a medium-low pressure section 5b, receives a flow of high-pressure steam QHP and a flow of medium-low pressure steam QIP from the heat-recovery boiler 10 and supplies a flow of steam to thecondenser 11 through the exhaust of the medium-low pressure section 5b and through a bypass system of a known type and not shown here for simplicity. - The
condenser 11 cools the steam received from the steam turbine, causing the steam to condense. - The
control apparatus 12 comprises aplant regulator 15, agas turbine regulator 16, asteam turbine regulator 17 and adata acquisition interface 18, for receiving measurements from sensors and transducers of theplant 1 indicating the status of theplant 1 itself. Through thedata acquisition interface 18, in particular, thecontrol apparatus 12 receives from a sensor assembly 20: a temperature signal ST, indicating the steam temperature at an inlet to thehigh pressure section 5a of thesteam turbine 5; a pressure signal SP, indicating the steam pressure at an inlet to thehigh pressure section 5a; and a flow signal SMF, indicating the flow rate QHP of steam supplied to thehigh pressure section 5a of thesteam turbine 5. - In order to control the
plant 1, thecontrol apparatus 12 acts on theactuator assembly 13 of the gas turbine set 3, which may comprise fuel feed valve actuators and inlet guide vane (IGV) actuators, and on theactuator assembly 14 of thesteam turbine 5, which may compriseinlet valve actuators stages steam turbine 5,bypass valve actuators 14c andboiler attemperators 14d. - The
plant regulator 15 determines a general power reference (set-point) WM for theentire plant 1 and, furthermore, determines a partial power reference WTG for the gas turbine 3, by subtracting the power supplied by thesteam turbine 5 from the general power reference WM (thesteam turbine 5 normally operates in sliding pressure conditions and is not choked). - The
gas turbine regulator 16 receives the partial power reference WTG and acts on theactuator assembly 13 so that thegas turbine 5 provides the required power. - The
steam turbine regulator 17 supervises the operating conditions of thesteam turbine 5 and intervenes in the start-up phases of theplant 1 or as a result of abnormal operating conditions, as described below, in order to maintain the desired pressure, temperature and flow rate conditions for the steam fed to thesteam turbine 5. - With reference to
figure 2 , thesteam turbine regulator 17 is based on the use of a simplified model of therotor 5c of thesteam turbine 5 to determine the temperature distribution and the stress distribution. Therotor 5c is represented by the simplified model M in the form of a homogeneous and isotropic cylinder (a cross-section of which is shown infigure 2 ) with uniform thermal conductivity, immersed in a steam flow with working temperature TW set at a distance DB from the axis A of therotor 5c itself. Therotor 5c may be represented with a radius R0 given by an average of the distance of the rotor blades from the axis A in thehigh pressure section 5a. Furthermore, the working temperature TW is variable in time, for example according to a programmed profile. The working temperature TW, which defines a boundary condition for calculating the temperature distribution of therotor 5c via the simplified model M, is determined on the basis of the temperature signal ST of the steam at an inlet of thehigh pressure section 5a of thesteam turbine 5. - It has also been observed by the inventors that the approximate values of the stresses determined on the basis of the simplified model M described are in a constant ratio with the values of the same stresses as determined accurately using, for example, finite element methods. In other words, the actual values of the stresses can be obtained with good approximation by the values calculated with the simplified model M of the
rotor 5c by applying a correction factor which is constant and independent of temperature. The use of the simplified model M to determine temperature distributions and stress distributions does not represent a significant increase as regards the processing capacity of the entire system. It is therefore possible to monitor in real time conformity of instantaneous stresses with the defined threshold criteria. The correction factor may be determined once and for all during the design phase. - The
steam turbine regulator 17 is configured to determine the temperature distribution in therotor 5c on the basis of the distance from the axis A and of the steam temperature TB, to determine the stresses (σ) inside therotor 5c on the basis of the temperature distribution, to determine a critical region of maximum stress and to compare the maximum stress in the critical region with a reference threshold. - With reference to
figure 3 , thesteam turbine regulator 17 comprises amemory unit 21 and aprocessing unit 22. - The
memory unit 21 comprises various sections, in which information is stored for use during operation of thesteam turbine regulator 17, including: - a
parameters section 21a containing the parameters of the simplified model M of therotor 5c for the calculation of the temperature distribution and the stress distribution (for example, and not exhaustively, radius, elastic modulus, density, thermal conductivity of the rotor); - a
correction section 21b, containing a correction factor σCF for the calculation of stresses; - a
threshold section 21c, containing a stress threshold σTH; and - a
profiles section 21d, containing at least one transient profile SPT(t), representing a series of values of steam temperature references SPT(tK) for theactuator assembly 14 of thesteam turbine 5 during a transient (in particular, a start-up transient; theprofiles section 21d may contain additional transient profiles for different transient situations that may occur during operation of thesteam turbine 5, other than profiles for load acceptance, in addition to the temperature profiles). - The
processing unit 22 comprises acontrol module 23, acalculation module 25, acorrection module 26 and acomparison module 27. - The
control module 23 receives the transient profile SPT(t) and sets a series of values of steam temperature references SPT(tK) for the steam fed to thehigh pressure section 5a of thesteam turbine 5 in accordance with the transient profile SPT(t). In addition, based on the temperature signal ST, the pressure signal SP and the flow signal SMF received from thedata acquisition interface 18, thecontrol module 23 acts on theactuator assembly 14 of thesteam turbine 5, to obtain operating conditions in accordance with the transient profile SPT(t). - The
calculation module 25 receives the parameters of the simplified model M of therotor 5c from theparameters section 21a of thememory unit 21 and the temperature signal ST from thedata acquisition interface 18. Thecalculation module 25 is configured to determine the temperature distribution inside therotor 5c (represented as a homogeneous and isotropic cylinder) starting from the temperature of the steam measured via the temperature signal ST, which is assigned as the working temperature TW. The calculation of the temperature distribution may be based on a solution of the heat equation for a homogeneous and isotropic cylindrical body. - The
calculation module 25 is further configured to determine a distribution of the stresses from the calculated temperature distribution and the load condition of therotor 5c. Thecalculation module 25 further determines a critical region of therotor 5c in which there is a maximum instantaneous stress σMAX and iteratively calculates the value of the maximum instantaneous stress σMAX. - The value of the maximum instantaneous stress σMAX is supplied to the
correction module 26, which receives the correction factor σCF fromsection 21c of thememory 21. Thecorrection module 26, for example a multiplier module, determines a value of the corrected maximum instantaneous stress σMAXC from the value of the maximum instantaneous stress σMAX and the correction factor σCF. - The value of the corrected maximum instantaneous stress σMAXC is then compared by the
comparison module 27 with the stress threshold σTH received fromsection 21c of thememory 21. The stress threshold σTH may be determined based on a limit region, for example defined on the basis of Von Mises or Tresca criteria. - If the value of the corrected instantaneous maximum stress σMAXC exceeds the stress threshold σTH, intervention occurs on the
control module 23, for example to correct or stop the control action, so as to avoid operating conditions that are inappropriate or that could potentially cause damages to therotor 5c. In particular, knowledge of the instantaneous stress state also allows correction of the steam attemperation in real time in order to optimise start-up. The corrections make it possible to react to any unexpected deviations with respect to the stored and selected transient profiles. - The processing of transient profiles may be advantageously performed off-line once again using the simplified model M of the
rotor 5c. In particular, it has been observed that, when therotor 5c has a uniform temperature (and is therefore in a condition of low stress), the metallic material of which it is constituted can be placed in contact with steam at a significantly higher temperature. On the other hand, when therotor 5c is in conditions of high stress, i.e. with a high internal temperature gradient, contact with hot steam must be avoided. Furthermore, for very low steam flow rates, the heat transfer coefficient already assumes values that are so high that the temperature of the metal surface of therotor 5c is close to the temperature of the steam. For this reason, limitation of the steam flow rate is not very effective in controlling thermomechanical stress, while control of the steam temperature has practically immediate effects on the surface temperature and thus on the thermal stress of therotor 5c. Also in the light of the comments just made, various transient profiles SPT(t) may be defined and, after verifying the internal stress distributions and the compatibility with stress thresholds for each temperature reference SPT(tK) defining the transient profiles SPT(t) (i.e. checking that the maximum stress corresponding to each temperature reference SPT(tK) of the transient profile SPT(t) is lower than the threshold stress σTH), one or more optimal profiles may be selected that make it possible to combine a large margin of safety and reduced transient times. The response of the equipment can thus be improved without impacting safety. Selected profiles may then be stored in thememory 21 and recalled when needed. -
Figure 4 shows a comparison between maximum instantaneous stresses during the steam turbine start-up phase carried out in a conventional way (dashed line) and those with steam temperature control according to a given profile as described above (solid line). The conventional start-up causes a peak of high stress, albeit of short duration, while starting up with temperature control according to the invention is smoother and has a much lower maximum stress value. Taking into account that the life expended for low cycle fatigue depends mainly on the maximum value attained by the stress, start-up with the temperature control described is much less onerous for the rotor. - Alternatively, using a different profile, it is possible to reduce load acceptance times without causing critical stresses inside the rotor.
Claims (13)
- A method of controlling a steam turbine comprising:defining a simplified model (M) of a steam turbine rotor (5c);determining a stress distribution in the rotor (5c) from parameters of the simplified model (M) and from temperature values (ST) of steam (QHP) supplied to the steam turbine (5);comparing the stress determined in the rotor (5c) with a stress threshold (σTH); andcontrolling the steam turbine (5) based on the comparing the stress determined in the rotor (5c) and the stress threshold (σTH);characterized in that the simplified model (M) of the steam turbine rotor (5c) is in the form of a homogeneous and isotropic cylinder.
- The method according to claim 1, wherein determining the stress distribution comprises:determining a temperature distribution in the simplified model (M) of the rotor (5c) from the temperature values (ST) of the steam (QHP) supplied to the steam turbine (5);determining an approximate stress distribution in the simplified model (M) of the rotor (5c) from the temperature distribution in the simplified model (M) of the rotor (5c); andapplying a programmed correction factor (σCF) to the approximate stress determined, the correction factor being constant and independent of the temperature.
- The method according to claim 2, wherein the correction factor (σCF) is a multiplying factor.
- The method according to any one of the foregoing claims, wherein controlling the steam turbine (5) comprises:setting a temperature reference (SPT(tK)) for the steam (QHP) supplied to the steam turbine (5);detecting the temperature values (ST) of the steam (QHP) at an inlet of the steam turbine (5); andacting on an actuator assembly (14) of the steam turbine (5) to take the detected temperature values (ST) to the set temperature reference (SPT(tK)).
- The method according to claim 4, wherein determining a stress distribution in the rotor (5c) comprises iteratively determining a maximum instantaneous stress (σMAX) and controlling comprises acting on the actuator assembly (14) of the steam turbine (5) so as to limit the temperature of the steam (QHP) supplied to the steam turbine (5) if the maximum instantaneous stress (σMAX) is greater than the stress threshold (σTH).
- The method according to claim 5, wherein the actuator assembly (14) comprises boiler attemperators (14d) and acting on the actuator assembly (14) of the steam turbine (5) so as to limit the temperature of the steam (QHP) comprises acting on the boiler attemperators (14d).
- The method according to any one of claims 4 to 6, comprising:defining at least one transient profile (SPT(t)), comprising a sequence of temperature references (SPT(tK));determining the stress distribution in the rotor (5c) from the parameters of the simplified model (M) and from the temperature values (ST) of the steam (QHP) supplied to the steam turbine (5) for each temperature reference (SPT(tK)) of the transient profile (SPT(t));comparing the stress determined in the rotor (5c) for each temperature reference (SPT(tK)) of the transient profile (SPT(t)) with the stress threshold (σTH); andstoring the transient profile (SPT(t)) if the stress determined in the rotor (5c) for each temperature reference (SPT(tK)) of the transient profile (SPT(t)) is lower than the stress threshold (σTH).
- The method according to claim 7, wherein the temperature reference (SPT(tK)) is selected in accordance with the transient profile (SPT(t)).
- A steam turbine plant comprising:a steam turbine (5);a sensor assembly (20), configured to provide a temperature signal (ST), indicating a steam temperature at an inlet of the steam turbine (5);a memory unit (21), containing parameters of a simplified model (M) of a rotor (5c) of the steam turbine (5); anda processing unit (22) configured to determine a stress distribution in the rotor (5c) from the simplified model (M) and from the temperature signal (ST), to compare the stress determined in the rotor (5c) with a stress threshold (σTH) and to control the steam turbine (5) based on comparing the stress determined in the rotor (5c) with the stress threshold (σTH);characterized in that the simplified model (M) of the steam turbine rotor (5c) is in the form of a homogeneous and isotropic cylinder.
- The plant according to claim 9, wherein the processing unit (22) comprises:a calculation module (25), configured to determine a temperature distribution in the simplified model (M) of the rotor (5c) from the temperature signal (ST) and to determine an approximate stress distribution in the simplified model (M) of the rotor (5c) from the temperature distribution in the simplified model (M) of the rotor (5c); anda correction module (26), configured to apply a programmed correction factor (σCF) to the approximate stress determined, the correction factor being constant and independent of the temperature.
- The plant according to claim 9 or 10, wherein the processing unit (22) comprises a control module (23) configured to act on an actuator assembly (14) of the steam turbine (5) on the basis of a temperature reference (SPT(tK)) and of the temperature signal (ST).
- The plant according to claim 11, wherein the actuator assembly (14) comprises boiler attemperators (14d) and the control module (23) is configured to act on the boiler attemperators (14d) so as to limit the temperature of the steam (QHP) .
- The plant according to claim 11 or 12, wherein:the memory unit (21) comprises at least one transient profile (SPT(t)), defined by a sequence of temperature references (SPT(tK)) selected so that the stress determined in the rotor (5c) for each temperature reference (SPT(tK)) of the transient profile (SPT(t)) is lower than the stress threshold (σTH); andthe control module (23) is configured to select the temperature reference (SPT(tK)) in accordance with the transient profile (SPT(t)).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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ITUB2015A005614A ITUB20155614A1 (en) | 2015-11-16 | 2015-11-16 | METHOD OF CONTROL OF A STEAM TURBINE AND STEAM TURBINE SYSTEM |
Publications (2)
Publication Number | Publication Date |
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EP3168434A1 EP3168434A1 (en) | 2017-05-17 |
EP3168434B1 true EP3168434B1 (en) | 2021-09-22 |
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EP16199217.7A Active EP3168434B1 (en) | 2015-11-16 | 2016-11-16 | Method of controlling a steam turbine and steam turbine plant |
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EP (1) | EP3168434B1 (en) |
CN (1) | CN106703905B (en) |
IT (1) | ITUB20155614A1 (en) |
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US11428115B2 (en) * | 2020-09-25 | 2022-08-30 | General Electric Company | Control of rotor stress within turbomachine during startup operation |
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JPS59226211A (en) * | 1983-06-08 | 1984-12-19 | Hitachi Ltd | Controlling method of thermal power plant |
JP3673017B2 (en) * | 1996-05-23 | 2005-07-20 | 株式会社東芝 | Steam turbine start control device |
US6939100B2 (en) * | 2003-10-16 | 2005-09-06 | General Electric Company | Method and apparatus for controlling steam turbine inlet flow to limit shell and rotor thermal stress |
DE102004058171A1 (en) * | 2004-10-02 | 2006-04-06 | Abb Technology Ag | Method and module for the anticipatory start-up of steam turbines |
-
2015
- 2015-11-16 IT ITUB2015A005614A patent/ITUB20155614A1/en unknown
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2016
- 2016-11-16 EP EP16199217.7A patent/EP3168434B1/en active Active
- 2016-11-16 CN CN201611034275.2A patent/CN106703905B/en active Active
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Publication number | Publication date |
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EP3168434A1 (en) | 2017-05-17 |
CN106703905A (en) | 2017-05-24 |
ITUB20155614A1 (en) | 2017-05-16 |
CN106703905B (en) | 2020-10-27 |
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