Exhaust control damper system for dual-cycle power plants.

Abstract

To provide a damper system for controlling gas turbine exhaust parameters for a heat recovery system.SOLUTION: An exhaust control damper system 140 for a power plant includes a frame 142 configured to be fluidly coupled to an exhaust flow path from a gas turbine (GT) system 108 to a heat recovery system 112. The damper system includes at least two sets of louvered dampers 150 in the frame and collectively covering the exhaust flow path. Each set of louvered dampers includes a plurality of blades 152 collectively angularly positionable in one of a fully open position, a fully closed position and a partially open position. An air insertion system 160 is coupled to the frame and configured to insert an airflow into the exhaust flow path to control the exhaust temperature entering the heat recovery system. The exhaust control damper system can be modulated to control the exhaust flow distribution and the mass flow to the heat recovery system.SELECTED DRAWING: Figure 2

Description

[Technical Field]

[0001] The present disclosure relates generally to dual-cycle power plants, and more particularly to a damper system including a louvered damper set and an air insertion system for controlling gas turbine exhaust parameters for a heat recovery system. [Background technology]

[0002] A dual-cycle power plant includes a power generation system that produces excess heat that can be used for other purposes. For example, a cogeneration plant produces both electrical power and excess heat that can be used for other purposes. Similarly, a combined cycle power plant (CCPP) includes a gas turbine (GT) system that produces electrical power and excess heat that can be used to generate steam for a steam turbine (ST) system, which also produces electrical power. In simple-cycle operation of a CCPP, the GT system operates alone to generate electrical power, and exhaust from the GT system is routed through a bypass exhaust stack via a diverter or bypass damper. The bypass exhaust stack can include any of a variety of environmental exhaust treatment systems that treat the exhaust gases before exhausting to the atmosphere. In combined-cycle operation of a CCPP, the hot exhaust from the GT system is routed by a bypass damper to a heat recovery system, such as a heat recovery steam generator to generate steam for the ST system, before being exhausted to the atmosphere. In a combined cycle, both the GT system and the ST system generate electrical power.

[0003] Start-up of an ST system ideally involves gradually increasing the temperature of the system to prevent damage to the system. The temperature of the ST system is increased by, among other things, controlling the amount of steam generated by the heat recovery system and applied to the ST system. The bypass dampers used to redirect the GT system exhaust from the exhaust stack to the heat recovery system can include single or dual blade closure or flap valves. The blades rotate or slide open and closed at an end pivot point (the latter is sometimes called a guillotine damper). The bypass dampers are typically designed to be in an open or closed position.

[0004] During operation, the GT system produces hot exhaust gas, and when the ST system is ready to start, the bypass damper is opened, exposing the heat recovery system to the hot exhaust gas to produce steam for the ST system. This all-or-nothing approach can make a gradual, controlled start-up of the ST system difficult and expose components upstream of and within the heat recovery system to severe thermal stresses from rapid temperature increases. Severe stresses can shorten the useful life of these components.

[0005] To address these challenges, one approach involves controlling the exhaust temperature by controlling the output of the GT system, but this approach can undesirably reduce plant output and power availability. In another approach, a bypass damper is used to attempt to control the mass flow rate of the exhaust to the heat recovery system, among other aspects, by placing the bypass damper in a partially open position, such as 10%, 20%, etc. This method and structure presents several drawbacks. In particular, the blade bypass damper does not provide sufficient control of the exhaust flow because it actually contains only one or two blades that can only be in either an open or closed position. In either partially open position, the one or two blades lack sufficient control of the application of backpressure in the GT system, which is advantageous for fast startup or cycling operation. Furthermore, between closed and open settings, current bypass dampers can cause backflow or turbulence of the exhaust, among other issues, causing uneven heat transfer in the heat recovery system. Thus, controlling the temperature of the ST system during start-up, for example, becomes a difficult task, since the current bypass damper is unable to control the heating rate of the heat recovery system.

[0006] Another drawback of current bypass dampers is that they provide minimal control over the mass flow rate of exhaust air entering the heat recovery system. Lack of better mass flow control can also make it difficult to control the heating of the heat recovery system and the amount of steam it generates. Summary of the Invention

[0007] One aspect of the present disclosure provides an exhaust control damper system for a combined cycle power plant, the damper system including: a frame configured to be fluidly coupled to an exhaust flow path from a gas turbine (GT) system to a heat recovery system; at least two louver-type damper sets within the frame that collectively cover the exhaust flow path, each including a plurality of blades that can be collectively positioned at one of a fully open position, a fully closed position, and a partially open position; and an air insertion system operably coupled to the frame and configured to insert airflow into the exhaust flow path.

[0008] Another aspect of the present disclosure provides a power plant including a gas turbine (GT) system, a steam turbine (ST) system, a heat recovery steam generator operably coupled to the GT system and the ST system, and an exhaust control damper system, the exhaust control damper system including: a frame configured to fluidly couple to an exhaust flow path from the GT system to the heat recovery steam generator; at least two louver-type damper sets within the frame that collectively cover the exhaust flow path, each including a plurality of blades, the angles of which can be collectively positioned to one of a fully open position, a fully closed position, and a partially open position; and an air insertion system operably coupled to the frame and configured to insert airflow into the exhaust flow path.

[0009] The exemplary aspects of the present disclosure are designed to solve the problems described herein and / or other problems not discussed.

[0010] These and other features of the present disclosure will be more readily understood from the following detailed description of the various aspects of the disclosure, taken in conjunction with the accompanying drawings which illustrate various embodiments of the present disclosure. [Brief explanation of the drawings]

[0011] [Figure 1]1 illustrates a schematic diagram of an exemplary power plant including an exhaust control damper system according to an embodiment of the present disclosure. [Figure 2] 1 illustrates a perspective view of an exhaust control damper system according to an embodiment of the present disclosure. [Figure 3] 1 illustrates an end view of an exhaust control damper system according to an embodiment of the present disclosure. [Figure 4] 1 illustrates an enlarged perspective view of a louvered damper set of an exhaust control damper system according to an embodiment of the present disclosure. [Figure 5] 1 illustrates a schematic diagram of an exemplary power plant including an exhaust control damper system in place of a bypass damper according to an embodiment of the present disclosure. [Figure 6] 1 illustrates an enlarged perspective view of two louvered damper sets of an exhaust control damper system according to an embodiment of the present disclosure. DETAILED DESCRIPTION OF THE INVENTION

[0012] It should be noted that the drawings of the present disclosure are not necessarily to scale. The drawings are intended to depict only typical aspects of the disclosure and therefore should not be considered limiting of the scope of the disclosure. In the drawings, like numbers represent like elements between the drawings.

[0013] As an initial matter, a clear explanation of the subject matter of this disclosure may require the selection of specific terminology when referring to and describing relevant mechanical components within a power plant. Wherever possible, common industry terminology will be used and utilized in a manner consistent with its generally accepted meaning. Unless otherwise indicated, such terminology should be accorded the broadest interpretation consistent with the context of this application and the scope of the appended claims. Those skilled in the art will recognize that in many cases, several different or overlapping terms may be used to refer to a particular component. Content described herein as a single component may include multiple components and may be referred to as consisting of multiple components in other contexts. Alternatively, content described herein as including multiple components may be referred to as a single component elsewhere.

[0014] Additionally, several descriptive terms may be used periodically herein, and it will prove useful to define these terms at the beginning of this section. These terms and their definitions are as follows, unless otherwise stated: As used herein, "downstream" and "upstream" are terms that describe a direction relative to a fluid flow, such as the exhaust from a gas turbine or the flow of exhaust from, for example, a damper system toward a heat exchanger. The term "downstream" corresponds to the direction of fluid flow, and the term "upstream" refers to the direction opposite to the flow (i.e., the direction from which the fluid is flowing). The terms "forward" and "aft" refer to directions, unless otherwise specified, with "forward" referring to the front end or compressor end of the engine and "aft" referring to the aft portion of the turbomachine.

[0015] It is often necessary to describe components located at various radial positions relative to the central axis. The term "radial" refers to movement or position perpendicular to the axis. For example, if a first component is located closer to the axis than a second component, the first component is referred to herein as being "radially inward" or "inboard" of the second component. On the other hand, if a first component is located farther from the axis than the second component, the first component can be referred to herein as being "radially outward" or "outboard" of the second component. The term "axial" refers to movement or position parallel to the axis. Finally, the term "circumferential" refers to movement or position around the axis. It will be understood that such terms can be applied in relation to the central axis of the turbine.

[0016] Additionally, as explained below, certain descriptive terms may be used periodically herein: the terms "first," "second," and "third" may be used interchangeably to distinguish one component from another, and are not intended to denote the location or importance of the individual components.

[0017] The terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the disclosure. As used herein, the singular forms "a," "an," and "the" are intended to include the plural forms as well, unless expressly stated otherwise. It will be further understood that the terms "comprise" and / or "comprising," when used herein, specify the presence of stated features, integers, steps, operations, elements, and / or components, but do not exclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and / or sets thereof. "Optional" or "optionally" means that the event or circumstance described following the word may or may not occur, and the component or element described following the word may or may not be present, and that the description includes cases where such event occurs or where such element is present, as well as cases where such event does not occur or where such element is absent.

[0018] When an element or layer is referred to as being "on," "engaged," "connected," or "coupled" to another element or layer, it can be directly on, engaged, connected, or coupled to the other element or layer, or intervening elements or layers may be present. In contrast, when an element is referred to as being "directly on," "directly engaged," "directly connected," or "directly coupled" to another element or layer, there may not be intervening elements or layers. Other terms used to describe relationships between elements should be interpreted in a similar manner (e.g., "between" versus "directly between," "adjacent to" versus "directly adjacent to," etc.). As used herein, the term "and / or" includes any and all combinations of one or more of the associated listed items.

[0019] An embodiment of the present disclosure provides an exhaust control damper system for a power plant, such as a cogeneration plant or combined cycle power plant (CCPP). The damper system includes a frame configured to fluidly couple to an exhaust flow path from a gas turbine (GT) system to a heat recovery system. The damper system includes at least two louver-type damper sets within the frame that collectively cover the exhaust flow path. Each louver-type damper set includes a plurality of blades that can be collectively positioned at an angle in one of a fully open position, a fully closed position, and a partially open position. The louver-type damper sets can be adjusted to control the distribution of gas flow to a heat recovery system, such as a heat recovery steam generator. Furthermore, the damper system provides improved control of the mass flow rate of exhaust to the heat recovery system by controlling the positions of the different louver-type damper sets. The damper system can be added to a conventional bypass system or can replace a conventional bypass system in a retrofit situation.

[0020] An air insertion system is operably coupled to the frame and configured to insert an air flow into the exhaust flow path. The air insertion system can mix air with the exhaust flow to the heat recovery system to control the exhaust temperature entering the heat recovery system. The air insertion system enables reduced thermal stress on components and provides controlled temperature start-up of the ST system without reducing the efficiency of the GT system. Thus, the GT system can be started in a simple cycle mode, and thereafter the heat recovery system can be started at a controlled gas temperature and mass flow rate according to the requirements of the heat recovery system and the ST system (e.g., gradually increasing temperatures, low thermal stress, etc.).

[0021] FIG. 1 illustrates a power plant 100 according to one embodiment of the present disclosure. The power plant 100 may include a gas turbine (GT) system 102 and a steam turbine (ST) system 134. The GT system 102 may include a compressor 104, a combustor 106, and a gas turbine 108. The power plant 100 may further include a bypass stack 110 and a heat recovery system 112. While FIG. 1 illustrates a single component, embodiments of the present disclosure are not so limited and may include multiple compressors, combustors, turbines, bypass stacks, and / or heat recovery systems connected in series and / or parallel. In one embodiment, the GT system 102 is a 7HA.03 engine commercially available from General Electric Company of Greenville, South Carolina. The present disclosure is not limited to any particular GT system and may be implemented in connection with other engines, such as, for example, other HA, F, B, LM, GT, TM, and E-class engine models from General Electric Company, as well as engine models from other manufacturers.

[0022] The gas turbine 108 may be coupled to the compressor 104 and / or the generator 114 via one or more shafts 116. During operation, the compressor 104 may receive air via an inlet filter 118, compress the air, and provide the compressed air to the combustor 106. In the combustor 106, a fuel, such as natural gas, may be introduced and burned to generate hot combustion gases. The combustion gases are discharged to the gas turbine 108, and the expansion of the combustion gases may drive the gas turbine 108 to rotate. The rotation of the gas turbine 108 may be used to rotate the generator 114 via the shaft 116 to generate electricity.

[0023] The gas turbine 108 may be coupled to the exhaust bypass stack 110 and the heat recovery system 112 via an exhaust duct 120. The exhaust duct 120 may include an inlet coupled to an exhaust outlet of the gas turbine 108 for receiving hot exhaust gases from the gas turbine 108. The exhaust duct 120 may include a first outlet coupled to the exhaust bypass stack 110 and a second outlet coupled to the heat recovery system 112. The exhaust bypass stack 110 may receive the hot exhaust gases and direct them outside of the power plant 100, for example, through any currently known or later developed purification system.

[0024] The heat recovery system 112 receives high-temperature exhaust gas (hereinafter, "exhaust"), recovers heat from the exhaust, heats water, and generates steam. The heat recovery system may sometimes be referred to as a heat recovery steam generator (HRSG). The heat recovery system 112 may include a boiler 122 for generating steam. In one embodiment, the heat recovery system 112 may include an auxiliary fired duct burner 124 in the boiler 122. The steam may be directed to a steam turbine system 134 configured to rotate with the steam. Rotation of a steam turbine 126 in the ST system 134 may rotate a generator 128 via a shaft 130 to generate additional electricity. In other embodiments, the steam from the heat recovery system 112 may be used for other purposes (e.g., heating or desalination).

[0025] As shown in FIG. 1 , the exhaust duct 120 may include a bypass damper 132 inside the exhaust duct 120. The bypass damper 132 may be a sandwich-type flap with independently expandable double-skinned blades. The blades may be actuated by a toggle lever system and powered by a hydraulic control. The bypass damper 132 and drive components for the bypass damper 132 may be fabricated from materials that can withstand the exhaust gas environment. The bypass damper 132 may be controlled to direct the exhaust flow to the exhaust bypass stack 110 or the heat recovery system 112. The bypass damper 132 may be configured to completely block the flow of exhaust gas to the exhaust bypass stack 110 or the heat recovery system 112. For example, the controller 136 may control the position of the bypass damper 132 to a first position (vertical) to block the flow of exhaust to the heat recovery system 112. The controller 136 may control the position of the bypass damper 132 to a second position (horizontal) to block the flow of exhaust to the exhaust bypass stack 110.

[0026] 1, embodiments of the present disclosure are not so limited, and other types of dampers may be used to stop the flow of exhaust air to the exhaust bypass stack 110 and / or the heat recovery system 112. For example, a biplane damper may be installed at the outlet of the exhaust duct 120 and / or at the inlet to the exhaust bypass stack 110 and / or the heat recovery system 112. In another embodiment, a guillotine damper or blanking plate may be used to control the flow of exhaust air.

[0027] The power plant 100 may include one or more sensors 138 for monitoring the operation of the power plant. The sensors 138 may monitor temperature, moisture, flow rate, and / or exhaust composition. A controller 136 of the power plant 100 may receive data from the sensors 138, analyze the data to determine the operating status of the power plant, and cause control of the power plant based on the data received from the sensors 138.

[0028] The power plant 100 may further include an exhaust control damper system 140 (hereinafter "damper system 140") to provide further control over the exhaust air before it enters the heat recovery system 112. Figure 2 shows a perspective view, Figure 3 shows an end view, and Figure 4 shows an enlarged perspective view of the damper system 140 fluidly coupled to the exhaust duct 120.

[0029] The damper system 140 includes a frame 142 configured to fluidly couple to an exhaust flow path from the GT system 108 ( FIG. 1 ) to the heat recovery system 112. The exhaust flow path may include any now known or later developed duct or enclosed passage. The frame 142, which may be configured to direct the exhaust flow between the bypass damper 132 ( FIG. 1 ) and the heat recovery system 112, houses a portion of the damper system 140. The frame 142 may be located adjacent to and downstream of the bypass damper 132. The frame 142 may be included in the exhaust duct 120 or the heat recovery system 112.

[0030] As shown in FIG. 2, the frame 142 can provide the outermost portion of the exhaust duct 120, i.e., inserted as part of the exhaust duct 120, or as shown in FIGS. 3, 4, and 6, the frame 142 can be attached to the interior of a portion of the exhaust duct 120, for example, by supports 148, at a distance. In either case, the frame 142 can include any number of plate members 144 configured to form a duct of the same or similar shape and dimensions as the location where the frame 142 is located. For example, in FIG. 2, one plate member 144 forms each of the bottom and top of the frame 142, and three plate members 144 form each of the side surfaces of the frame 142. The frame 142 can be made of any material that can withstand the exhaust environment.

[0031] The frame 142 may be coupled to a new power plant 100 or may be retrofitted to an existing power plant 100. To this end, the frame 142 may have an adjustment member 146 configured to allow adjustment of the size of the frame. The adjustment member 146 allows the frame 142 to have different sizes to accommodate different sizes of exhaust ducts 120 and / or heat recovery systems 112. can any The structure In one example, but not limited to, an adjustment member 146 teeth , can include a selection from a variety of different length plate members.

[0032] Additionally, the damper system 140 includes at least two louver-type damper sets 150 within a frame 142 that collectively cover the exhaust flow path. Each louver-type damper set 150 includes a plurality of blades or vanes 152 that can be collectively positioned at one of a fully open position (shown in the outer two of FIG. 2 ), a fully closed position (shown in the outer two of FIG. 3 ), and a partially open position (shown in the middle two of FIG. 2 ). The partially open position can include any angular position of the blades 152 between the fully open and fully closed positions, such as 25%, 50%, 75%, and so on. Several louver-type damper sets 150 can have the same or different settings. Each louver-type damper set 150 can include a position transmitter 154 configured to adjust the angular position of each of the plurality of blades 152 independently of the other louver-type damper sets 150. The position transmitter 154 may include any now known or later developed mechanism for simultaneously changing the angular position of multiple blades 152, such as, but not limited to, an elongated member pivotally coupled to each vane and capable of linear movement to change the angular position.

[0033] Additionally, each louvered damper set 150 may include an actuator 156 configured to control operation of the position transmitting device 154 to position the respective louvered damper set 150 in one of a fully open position, a fully closed position, and a partially open position. The controller 136 may control each actuator 156 to, among other things, control the mass flow rate of exhaust air through the frame 142. The actuator 156 may include any suitable powered actuator capable of moving the position transmitting device 154, such as an electric, hydraulic, or pneumatic actuator. For example, the actuator 156 may be a rotary actuator (shown in FIG. 4 ) pivotally coupled to the position transmitting device 154 and capable of linearly moving the position transmitting device 154 vertically to change the angular position of the blades 152, or a linear actuator coupled to the position transmitting device 154 and capable of linearly moving the position transmitting device 154 vertically to change the angular position of the blades 152. Various other actuators may also be used depending on the type of position transmitting device 154.

[0034] 2-4 show four louver-type damper sets 150, but any number of sets can be used. For example, at least two or at least three louver-type damper sets 150 can be used. The plurality of blades 152 of each louver-type damper set 150 includes any number capable of providing the desired mass flow control of the exhaust. That is, the blades 152 are in sufficient number to provide something more than simply opening and closing a passageway, i.e., to provide a controlled flow restriction that can control the mass flow of the exhaust to the heat recovery system 112 and the backpressure to the GT system 102. In one example, without limitation, the plurality of blades 152 includes at least 10 vertically spaced damper blades, but any number sufficient to provide the desired flow restriction is possible.

[0035] In the illustrated example, the blades 152 are spaced apart vertically and rotate about a horizontal axis. It will be readily understood that the blades 152 may also be spaced apart horizontally and rotate about a vertical axis, i.e., with the actuators 156 on the sides of the frame 142. As shown in Figures 4 and 6, for example, each louver-type damper set 150 may be separated by a portion 158 of the frame 142, although this is not necessary in all cases (see Figure 3).

[0036] Additionally, damper system 140 includes an air insertion system 160 ( FIGS. 2 and 3 ) operably coupled to frame 142 and configured to insert an air flow into the exhaust flow path. Air insertion system 160 may include an air pump 162 having an output and a conduit 164 fluidly coupling the output of air pump 162 to at least one opening 166 in frame 142 that is in fluid communication with the exhaust flow path. Conduit 164 may include any form of piping capable of withstanding the environment in power plant 100 and directing the air flow to a desired location. FIG. 2 illustrates one opening 166, while FIGS. 3 , 4 , and 6 illustrate multiple openings 166 spaced along at least a portion, e.g., one side, of frame 142. While a particular arrangement of openings is illustrated, any number of openings 166 may be provided in any arrangement around frame 142. Each opening 166 is configured to insert air flow from air pump 162 into the exhaust flow path.

[0037] In FIG. 2, the air pump 162 is located beside the frame 142, while in FIGS. 3, 4, and 6, the air pump 162 is attached to the frame 142. Any number of air pumps 162 can be used. FIGS. 2 and 3 show one air pump 162, while FIGS. 4 and 6 show a pair of air pumps 162. Air can be obtained from the atmosphere surrounding the power plant 100 or from the compressor 104 (FIG. 1). In one embodiment, a sensor 138 measures the temperature of the exhaust stream (gas). Based on the temperature, the controller 136 can control the air pump 162 to provide a quantity of air that, when mixed with the remainder of the exhaust stream within and / or downstream of the frame 142, produces a desired exhaust temperature for the heat recovery system 112.

[0038] 1 , the power plant 100 may further include an isolator 170 for isolating the air or air / gas mixture from the heat recovery system 112. The isolator 170 may be a guillotine damper or a blanking plate configured to isolate the bypass damper 132 and the damper system 140 from the heat recovery system 112. The isolator 170 may be located adjacent to the damper system 140 (shown) or the bypass damper 132. The isolator 170 may be included in the exhaust duct 120 or the heat recovery system 112. The isolator 170 may be a bolted plate supplied with the diverter bypass damper 132 and / or the damper system 140 and may remain in place until the heat recovery system 112 is operated, allowing the power plant 100 to operate in a simple cycle. In one embodiment, the isolator 170 may not provide thermal insulation.

[0039] During operation, the power plant 100 can be controlled to operate in a simple cycle, producing energy solely from the operation of the gas turbine 108, or in a combined cycle, producing energy from the operation of the gas turbine 108 and the heat recovery system 112. In the simple cycle, the bypass damper 132 can be controlled to be in a first position (vertical) to block the flow of exhaust to the heat recovery system 112. In the simple cycle, exhaust from the gas turbine 108 can flow via the exhaust duct 120 to the exhaust bypass stack 110.

[0040] In a combined cycle, the bypass damper 132 can be controlled to a second position (horizontal) to block the flow of exhaust to the exhaust bypass stack 110. In a combined cycle, exhaust from the gas turbine 108 can flow through the exhaust duct 120 to the damper system 140 and ultimately to the heat recovery system 112 to recover additional energy from the exhaust gas. A controller 136 of the damper system 140 is configured to control the position of the louvered damper set 150 and the operation of the air injection system 160 to control at least one of the temperature of the exhaust flow downstream of the frame 142, the mass flow rate of the exhaust downstream of the frame 142, and the backpressure upstream of the frame 142, i.e., to the GT system 108. The controller 136 can be part of a control system of the power plant 100 or can be a separate controller.

[0041] During start-up of the power plant 100, the power plant can be set to a simple cycle or a combined cycle. For start-up in the simple cycle, the bypass damper 132 can be set to a first position (vertical) to block the flow of exhaust to the heat recovery system 112 and allow generated exhaust to flow to the exhaust bypass stack 110. After start-up of the gas turbine 108, the exhaust is introduced into the exhaust duct 120, and all of the exhaust flows outside the power plant 100 through the exhaust bypass stack 110. After predetermined conditions are met (e.g., predetermined time, temperature, exhaust gas composition), the bypass damper 132 can be controlled to transition to a second position (horizontal) to allow the flow of exhaust to the heat recovery system 112 and block the flow of exhaust to the exhaust bypass stack 110.

[0042] During the transition from the first position to the second position, a portion of the exhaust air may flow to the heat recovery system 112 and a portion of the exhaust air may flow to the exhaust bypass stack 110. By controlling the rate of the transition, the amount of exhaust air introduced into the heat recovery system 112 may be controlled in a limited manner by the bypass damper 132 to reduce stress on the components of the heat recovery system 112 due to the rapid temperature change. According to embodiments of the present disclosure, the damper system 140 may be operated to provide further control of the exhaust air flow to reduce stress on the components of the heat recovery system 112 both during and after the transition. Thus, the damper system 140 may reduce risks to the heat recovery system 112 of the power plant 100 caused by a lack of fine control of the bypass damper 132.

[0043] For example, damper system 140 can provide protection against excessive or too little pressure in exhaust duct 120. Additionally, damper system 140 can eliminate turbulence and better control the mass flow rate of exhaust air to heat recovery system 112. Air injection system 160 allows for control of exhaust air temperature, providing further protection against thermal stress to heat recovery system 112 or upstream components. Additionally, damper system 140 can also be controlled in conjunction with bypass damper 132 and stack damper 172 of heat recovery system 112 to reduce the possibility of excessive pressure in exhaust duct 120, for example.

[0044] In another embodiment shown in Figure 5, a damper system 140, possibly in combination with an isolator 170, can replace the bypass damper 132, thus eliminating any drawbacks that the bypass damper 132 presents. In another embodiment shown in Figure 6, only two louver-type damper sets 150 are used.

[0045] Embodiments of the present disclosure provide an exhaust control damper system 140 that can provide additional exhaust control to the heat recovery system 112. The damper system 140 can provide better backpressure control in the GT system 102 compared to the bypass damper 132, even compared to bypass dampers 132 that use multiple gates. For example, the system provides lower backpressure in the GT system 102 during fast startup or cycling operation. Therefore, the system enables rapid startup of the GT system 102 while reducing thermal stresses that may occur in the heat recovery system 112. Furthermore, the damper system 140 is more reliable compared to single-blade bypass dampers, which may experience turbulence or backflow when partially open. The damper system 140 also further improves control of the mass flow rate of exhaust to the heat recovery system 112, providing additional control over startup of the ST system 134. The damper system 140 is flexible, adjustable, and easily installed in any configuration or power plant framework, either as a newbuild or retrofit.

[0046] As used in this application throughout this specification and claims, approximation can be applied to modify any quantitative expression that can reasonably vary without resulting in a change in the basic function involved. Thus, values ​​modified by terms such as "approximately," "about," and "substantially" are not limited to the exact value specified. In at least some instances, approximation can correspond to the precision of the instrument used to measure the value. Here, and throughout this specification and claims, range limitations are combinable and / or interchangeable, and unless the context and language dictate otherwise, such ranges are identified and include all subranges encompassed therein. "About," as applied to a particular value in a range, applies to both endpoints and can indicate + / - 10% of the stated value, unless otherwise dependent on the precision of the instrument used to measure the value.

[0047] For all means-plus-function or step-plus-function elements in the following claims, corresponding structure, materials, acts, and equivalents are intended to encompass any structure, material, or acts for performing that function in combination with elements recited in other claims as specifically claimed. The description of the present disclosure has been presented for purposes of illustration and description and is not intended to be exhaustive or to limit the disclosure to the precise form disclosed. Numerous modifications and variations will be apparent to those skilled in the art without departing from the scope and spirit of the disclosure. The embodiments have been chosen and described to best explain the principles and practical applications of the disclosure and to enable those skilled in the art to appreciate the disclosure in various embodiments that may be varied in various ways to suit the particular uses contemplated. [Explanation of symbols]

[0048] 100 Power Plants 102 Gas Turbine (GT) System 104 Compressor 106 Combustor 108 Gas Turbine, GT System 110 Exhaust Bypass Stack 112 Heat Recovery System 114 Generator 116 Shaft 118 Inlet filter 120 Exhaust duct 122 Boiler 124 Auxiliary combustion duct burner 126 Steam Turbine 128 Generator 130 shaft 132 Diverter bypass damper 134 Steam (ST) Turbine System 136 Controller 138 Sensors 140 Exhaust Control Damper System 142 frames 144 Plate member 146 Adjustment member 148 Support 150 Louver type damper set 152 Blades or vanes 154 Position transmission device 156 Actuator 158 Part of a Frame 160 Air Injection System 162 Air Pump 164 Conduit 166 Opening 170 Isolator 172 Stack Damper

Claims

1. An exhaust control damper system (140) for a combined cycle power plant (100), the exhaust control damper system (140) comprising: a frame (142) configured to fluidly couple to an exhaust flowpath from a gas turbine (108) (GT) system (102) to a heat recovery system (112); at least two louver-type damper sets (150) disposed within the frame (142) and jointly covering the exhaust flow path, each of the louver-type damper sets (150) including a plurality of blades (152), the angles of which can be collectively positioned at one of a fully open position, a fully closed position, and a partially open position; an air injection system (160) operably coupled to the frame (142) and configured to inject airflow into the exhaust flow path; wherein the frame has an adjustment member configured to allow adjustment of the size of the frame.

2. Each of the louver-type damper sets (150) a position transmitter (154) configured to adjust the angular position of each of the plurality of blades (152); an actuator (156) configured to control the operation of the position transmission device (154) to position each of the louver-type damper sets (150) in one of the fully open position, the fully closed position, and the partially open position; The exhaust control damper system (140) of claim 1, comprising:

3. An air insertion system (160) an air pump (162) having an output; a conduit (164) fluidly coupling the output of the air pump (162) to at least one opening (166) in the frame (142) in fluid communication with the exhaust flow path; Including, The exhaust control damper system (140) of claim 1, wherein the at least one opening (166) is configured to insert airflow from the air pump (162) into the exhaust flow path.

4. 4. The exhaust control damper system of claim 3, wherein the at least one opening comprises a plurality of openings spaced apart along at least a portion of the frame.

5. The exhaust control damper system (140) of claim 3, wherein the air pump (162) comprises a pair of air pumps (162).

6. The exhaust control damper system (140) of claim 1, wherein the at least two louvered damper sets (150) comprise at least three louvered damper sets (150).

7. 2. The exhaust control damper system of claim 1, wherein the plurality of blades of each louver-type damper set includes at least 10 vertically spaced damper blades.

8. 2. The exhaust control damper system of claim 1, further comprising a controller configured to control the position of the at least two louvered damper sets and the operation of the air insertion system to control at least one of a temperature of the exhaust flow downstream of the frame, a mass flow rate of the exhaust downstream of the frame, and a back pressure upstream of the frame.

9. The exhaust control damper system (140) of claim 1, wherein the frame (142) is mounted within a portion of an exhaust duct (120).

10. a gas turbine (108) (GT) system (102); a steam turbine (126) (ST) system (134); a heat recovery steam generator (112) operably coupled to the GT system (102) and the ST system (134); An exhaust control damper system (140) according to any one of claims 1 to 9; A power plant (100) comprising:

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