Startup method and mechanism for a burner having a perforated flame holder
10077899 ยท 2018-09-18
Assignee
Inventors
- DOUGLAS W. KARKOW (DES MOINES, WA, US)
- JOSEPH COLANNINO (BELLEVUE, WA, US)
- Igor A. Krichtafovitch (Kirkland, WA)
- Christopher A. Wiklof (Everett, WA)
Cpc classification
F27D11/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N2227/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/38
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N2900/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2900/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2208/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2203/104
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E20/34
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F23N1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2203/102
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2203/1023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/406
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/446
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N1/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N2221/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/74
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C9/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/145
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C6/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N5/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/42
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/84
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T50/60
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F23D11/383
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/448
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N5/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2203/105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C99/001
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2207/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2201/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N5/265
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D2203/1012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F23L7/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/74
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/42
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/44
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/38
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D11/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C6/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C9/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N5/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C99/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23N5/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/84
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27D11/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
According to an embodiment, a combustion system is provided, which includes a nozzle configured to emit a diverging fuel flow, a flame holder positioned in the path of the fuel flow and that includes a plurality of apertures extending therethrough, and a preheat mechanism configured to heat the flame to a temperature exceeding a startup temperature threshold.
Claims
1. A burner, comprising: a primary nozzle having a longitudinal axis and configured to emit a fuel flow; a primary flame holder having first and second faces and a plurality of apertures extending through the flame holder from the first face to the second face, positioned with the first face toward the nozzle and intersecting the longitudinal axis of the nozzle; and a preheat mechanism configured to preheat the primary flame holder, the preheat mechanism including: a preheat nozzle; a secondary flame holder configured to support a flame at a position between the primary nozzle and the first face of the primary flame holder and to introduce turbulence into the fuel flow emitted by the primary nozzle; and a mechanism configured to move the secondary flame holder between an operative and an inoperative position.
2. The burner of claim 1, wherein the secondary flame holder is movable between the operative position, in which the secondary flame holder introduces turbulence into the fuel flow, and the inoperative position, in which the secondary flame holder is spaced away from a path of the fuel flow.
3. The burner of claim 1, comprising a controller configured to switch the burner from a preheat condition to an operative condition.
4. The burner of claim 3, wherein the controller is configured to hold the burner in the preheat condition for a first time period, and to switch the burner from the preheat condition to the operative condition at the end of the first time period.
5. The burner of claim 3, wherein the controller is configured to receive a signal indicative of a temperature of the primary flame holder, and to switch the burner from the preheat condition to the operative condition while the temperature of the primary flame holder is above a temperature threshold.
6. The burner of claim 3, wherein the controller is configured to regulate an operating level of the burner.
7. A method, comprising: performing a burner startup procedure, including applying thermal energy to a primary flame holder by supporting a preheat flame at a position between a primary nozzle and the primary flame holder with a preheat nozzle and a secondary flame holder, the secondary flame holder being positioned between the primary nozzle and the primary flame holder; terminating the burner startup procedure after a temperature of a portion of the primary flame holder is above a startup temperature threshold; emitting a flow of fuel from the primary nozzle at an operational rate; introducing turbulence into the flow of fuel with the secondary flame holder; supporting a flame within a plurality of apertures extending through the primary flame holder; and moving the secondary flame holder between an operative position and an inoperative position with a mechanism.
8. The method of claim 7 wherein the terminating the burner startup procedure includes reducing a concentration of oxygen in a flow of oxidizer fluid.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
(12) In the following detailed description, reference is made to the accompanying drawings, which form a part hereof. In the drawings, similar symbols typically identify similar components, unless context dictates otherwise. The illustrative embodiments described in the detailed description and drawings are not meant to be limiting. Other embodiments may be utilized, and other changes may be made, without departing from the spirit or scope of the subject matter presented here.
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(14) The term air refers to a fluid, typically gaseous, that includes oxygen in a form that can support combustion. While ambient air is the most common oxidizer fluid, many combustion systems employ a mixture that can include other additives, selected, generally, for the purpose of modifying the combustion in some way. For example, in many cases, flue gases are recirculated and mixed with ambient air to reduce the oxygen concentration in the oxidizer fluid, in order to reduce harmful emissions, according to very well known principles and processes. For the purpose of the present specification and claims, the term air is to be construed as referring to any such fluid or mixture of fluids, unless explicitly limited or defined otherwise.
(15) The flame holder 104 of the combustion system 100 is preferably made from a refractory material, such as, e.g., ceramic, and includes a plurality of apertures 112, that extend from a first face 114 to a second face 116 of the flame holder.
(16) The flame holder is positioned with the first face 114 toward the nozzle 102 and spaced away from the nozzle by a distance D.sub.1. In the embodiment shown, the first and second faces 114, 116 of the flame holder 104 are planar, and lie substantially parallel to a plane that is perpendicular to a longitudinal axis of the nozzle 102. According to alternative embodiments, the flame holder 104 can include faces that are non-planar, or that lie at different angles with respect to each other or to the longitudinal axis of the nozzle 102.
(17) In operation, a stream of fuel 118 is ejected from the nozzle 102 toward the first face 114 of the flame holder 104. The fuel stream 118 disperses from the nozzle 102 in a conical spray at an angle that is typically about 7.5 degrees from the longitudinal axis, resulting in a solid conical angle of about 15 degrees. As the fuel stream 118 disperses, it entrains air, and eventually reaches a flammable proportion of fuel and air. By selection of the nozzle and the pressure at which fuel is ejected, the velocity at which the fuel stream 118 is ejected from the nozzle 102 is preferably selected to be much higher than the flame propagation speed of the particular type of fuel employed, so that, on the one hand, the fuel stream is prevented from supporting a flame near the nozzle, and on the other hand, by the time the dispersing fuel stream 118 has slowed to near the flame propagation speed, the fuel stream has entrained enough air that the mixture is too lean for combustion at the temperature of the fuel stream.
(18) However, the flame holder 104 is held at a much higher temperature because of ongoing combustion. The higher temperature of the flame holder 104 is sufficient to maintain combustion of the lean fuel mixture. A stable flame can thus be maintained by the flame holder 104. The flame is held primarily within the apertures 112, although the flame may extend a short distance beyond either or both faces 114, 116 of the flame holder 104. The fuel stream 118 is able to continually feed the combustion, and the flame holder 104 is able to support a leaner flame than could be maintained in a conventional burner system. The distance D.sub.1 is selected, in part, according to a desired fuel-to-air ratio of the fuel stream 118 at the point at which the fuel stream contacts the flame holder 104.
(19) The inventors have recognized that, although while in operation, the flame holder 104 is able to support combustion with a very lean fuel mixture, startup of the combustion system 100 is problematic. Because the fuel mixture at the distance D.sub.1 is flammable only at elevated temperatures, and because the flame holder 104 may be at ambient temperature at startup, conventional ignition methods or devices are not generally effective for startup of the combustion system 100.
(20) The inventors have developed various systems and methods for efficient startup of combustion systems that employ perforated flame holders. In the embodiments described hereafter, elements that are described with reference to previous embodiments, and that are referenced by a same reference number, are generally not described in detail.
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(22) The nozzle 122 is configured to be translatable along its longitudinal axis. As shown, the nozzle 122 includes inner and outer telescoping elements 134, 136. The inner telescoping element 134 is fixed, while the outer telescoping element 136, which includes a nozzle orifice 138, is movable between a retracted position, as shown in
(23) The fuel supply 128 is coupled to the nozzle via a fluid line 142. The fuel control valve 130 is coupled in the fluid line 142 and configured to control the flow of fuel from the fuel supply 128 to the nozzle 122.
(24) The temperature sensor 132 is positioned and configured to detect a temperature of the flame holder 104, and to transmit a signal representative of the detected temperature to the system control unit 126 via connector 144. As shown in
(25) The system control unit 126 is operatively coupled to the temperature sensor 132, the fuel control valve 130, and the nozzle position controller 124 via connectors 144, and is configured to receive data from the temperature sensor and to control operation of the fuel control valve and the nozzle position controller.
(26) The combustion system 120 is shown in
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(28) According to another embodiment, the system control unit 126 includes a timer by which transition from startup mode to operational mode is controlled. I.e., when startup is initiated, the system control unit 126 starts the timer, and when a selected time period has passed, the nozzle 122 is retracted and the fuel flow is increased, as described above. The time period is selected according to a predetermined period necessary to ensure that the flame holder 104 has reached the startup temperature threshold.
(29) The movable nozzle 122 can also be employed in combustion systems that may be required to operate on a variety of fuels. As is well known in the art, the fuel-to-air ratio at which the mixture is combustible varies according to the type of fuel, as does flame propagation speed within a flow of fuel. Thus, an optimal operating distance D.sub.1 will vary according to the type of fuel. The combustion system 120 of
(30) According to an alternate embodiment, the flame holder 104 is configured to be translatable along the longitudinal axis A of the nozzle. This enables adjustments in the distance D between the nozzle and flame holder without changing the position of the nozzle. According to an embodiment, the combustion system 120 includes a flame holder that is translatable along the axis A and also a nozzle that is movable or translatable along the axis A. With such a configuration, a user can, for example, move the flame holder to a position that is more or less permanent, in order to establish a desired distance D on the basis of combustion characteristics of a particular fuel. Meanwhile, the nozzle can be configured to be moved for startup purposes, as described above, or for some other reason.
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(32) The first electrode 152 is in the shape of a torus, positioned just downstream of the nozzle 102 and centered on the longitudinal axis A of the nozzle so that the fuel stream 118 passes through the first electrode. The second electrode 154 is positioned between the first face 114 of the flame holder 104 and the nozzle. The second electrode 154 is movable from an extended position, as shown in solid lines in
(33) In operation, when the combustion system 150 is in startup mode, i.e., when startup is initiated, the system control unit 126 controls the electrode position control 156 to move the second electrode 154 to the extended position. The system control unit 126 controls the voltage supply 128 to transmit a first voltage signal to the first electrode 152. As the fuel stream 118 passes through the first electrode 152, an electrical charge having a first polarity is imparted to the fuel stream. Meanwhile, the system control unit 126 transmits a second voltage signal from the voltage supply 158 to the second electrode 154. The second voltage signal has a polarity that is opposite that of the charge imparted to the fuel stream, and therefore attracts the oppositely-charged fuel stream. Ignition is initiated within the fuel stream 118, whereupon a startup flame 148 is held between the first and second electrodes 152, 154, in spite of the high velocity of the fuel stream. This method of holding a flame within a fuel flow is sometimes referred to as electrodynamic combustion control.
(34) According to an embodiment, the system control unit 126 controls the voltage supply 158 to apply a voltage signal to the second electrode 154 while connecting the first electrode 152 to ground. According to an embodiment, the voltage signal applied to the first and/or second electrode is an AC signal.
(35) With the startup flame 148 held below the first surface 114 of the flame holder 104, a portion of the flame holder 104 is quickly heated to the startup temperature threshold. When the startup temperature threshold is surpassed, the system control unit 126 controls the voltage supply 158 to remove the voltage signals from the first and second electrodes, and controls the electrode position controller 156 to move the second electrode 154 to the retracted position. When the voltage signals are removed from the electrodes, the startup flame is no longer held, and blows out. As previously described, when the uncombusted fuel and air mixture reaches the flame holder 104, the primary flame auto-ignites in the preheated portions of the flame holder, and normal operation quickly follows.
(36) Although embodiments are described as including a system control unit that is configured to control transition between a startup mode and an operational mode, alternative embodiments are operated manually. For example, According to an embodiment, the combustion system 150 is configured such that an operator manually switches the electrode position controller 156 to move the second electrode. According to another embodiment, the operator manually extends and retracts the second electrode. Additionally, according to an embodiment, an operator manually switches a voltage signal to the first and second electrodes 152, 154, and switches the signals off when the flame holder 104 exceeds the startup threshold.
(37) According to an embodiment, a portion of the nozzle 102 is electrically conductive, and acts as the first electrode, with the connector 144 being coupled to the conductive portion of the nozzle. According to an embodiment, the second nozzle 154 is retracted by a telescoping mechanism similar to that described with reference to the nozzle of
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(39) In operation, when startup is initiated, the system control unit 126 controls the secondary fuel valve 164 to openthe primary fuel valve 130 is closedand ignites a stream of fuel that exits the secondary nozzle 162, producing a startup flame 148 that is directly adjacent to the first face 114 of the flame holder 104. The startup flame 148 heats a portion of the flame holder 104 to a temperature exceeding the startup threshold. When the system control unit 126 determines that a portion of the flame holder 104 exceeds the startup temperature thresholdvia, for example, a signal from a temperature sensor, as described previouslythe system control unit controls the secondary fuel valve 164 to close, while controlling the primary fuel control valve 130 to open, causing a fuel stream 118 to be ejected by the primary nozzle 102. When the fuel and air mixture of the fuel stream 118 reaches the flame holder 104, a primary flame is ignited and normal operation follows, substantially as described with reference to previously embodiments.
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(47) To move the startup flame holder 226 from the startup position to the retracted position, the operator grasps a handle 230 at the end of the rod 228, rotates the rod, which moves the startup flame holder substantially out of the path of the fuel stream 118, then pulls the rod outward, which translates the startup flame holder into a space that is fully out of the path of the fuel stream.
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(49) The air mixture control valve 244 includes a valve gate 247 and acts as a proportion control valve, configured to control a proportion of components of the air 246 that is introduced into the combustion volume 106. In the embodiment shown, the air mixture control valve 244 is configured to control the respective proportions of two components that are introduced via first and second valve input ports 248, 250. Pivoting of the valve gate 247 in, for example, a clockwise direction increases the proportion of a fluid entering via the first valve input port 248 while simultaneously reducing the proportion of fluid entering the valve via the second valve input port 250. Conversely, pivoting of the valve gate 247 in the counter-clockwise direction reduces the proportion from the first valve input port 248 and increases the proportion from the second valve input port 250.
(50) In the embodiment of
(51) As explained in more detail above with reference to
(52) According to an embodiment, the combustion system 240 is configured for normal operation with air that has a significantly lower oxygen content than is found in ambient air. Accordingly, as shown in
(53) While the introduction of recirculated flue gas can have beneficial effects with respect to the production of NOx, a system configured to operate with recirculated flue gas can have advantages related to startup, as well.
(54) In the embodiment described with reference to
(55) Various methods and devices can be used to enable operation of the combustion system 240. For example, an oxygen sensor can be positioned in the air conduit 242, with an output coupled to the controller 126, to enable the controller to monitor the air oxygen level of the air 246. A temperature sensor and/or a timer can be provided, as previously described, to enable the controller 126 to determine when to transition from the startup mode to the operation mode, etc.
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(60) The step of applying energy to the flame holder (step 302) can be accomplished via any of a number of different structures and devices, some examples of which are disclosed above. For example, the energy can be applied by means of an electrically resistive element, as described with reference to
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(63) In each of the above-referenced examples, deactivation procedures are also disclosed.
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(66) Structures configured to electrically connect components or assemblies shown in the drawings are depicted generically as connectors 144, inasmuch as electrical connectors and corresponding structures are very well known in the art, and equivalent connections can be made using any of a very wide range of different types of structures. The connectors 144 can be configured to carry high-voltage signals, data, control logic, etc., and can include a single conductor or multiple separately-insulated conductors. Additionally, where a voltage potential, control signal, feedback signal, etc., is transmitted via intervening circuits or structures, such as, for example, for the purpose of amplification, detection, modification, filtration, rectification, etc., such intervening structures are considered to be incorporated as part of the respective connector. Where other methods of signal or data transmission are used, such as via, e.g., fiber optics or wireless systems, such alternative structures are considered to be equivalent to the connectors 144 depicted here.
(67) The abstract of the present disclosure is provided as a brief outline of some of the principles of the invention according to one embodiment, and is not intended as a complete or definitive description of any embodiment thereof, nor should it be relied upon to define terms used in the specification or claims. The abstract does not limit the scope of the claims.
(68) While various aspects and embodiments have been disclosed herein, other aspects and embodiments are contemplated. The various aspects and embodiments disclosed herein are for purposes of illustration and are not intended to be limiting, with the true scope and spirit being indicated by the following claims.