WO2006076549A1 - Matrix means for reducing combustion volume - Google Patents

Matrix means for reducing combustion volume Download PDF

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Publication number
WO2006076549A1
WO2006076549A1 PCT/US2006/001185 US2006001185W WO2006076549A1 WO 2006076549 A1 WO2006076549 A1 WO 2006076549A1 US 2006001185 W US2006001185 W US 2006001185W WO 2006076549 A1 WO2006076549 A1 WO 2006076549A1
Authority
WO
WIPO (PCT)
Prior art keywords
steam generating
matrix means
oxidant
fuel
generating boiler
Prior art date
Application number
PCT/US2006/001185
Other languages
French (fr)
Inventor
Joseph Robert Strempek
Ronald C. Lenzer
Original Assignee
The Babcock & Wilcox Company
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to PL06718277T priority Critical patent/PL1836439T3/en
Application filed by The Babcock & Wilcox Company filed Critical The Babcock & Wilcox Company
Priority to BRPI0606693-3A priority patent/BRPI0606693B1/en
Priority to JP2007551388A priority patent/JP5232474B2/en
Priority to CA2594739A priority patent/CA2594739C/en
Priority to AU2006204840A priority patent/AU2006204840B2/en
Priority to ES06718277.4T priority patent/ES2546645T3/en
Priority to EP06718277.4A priority patent/EP1836439B1/en
Priority to CN200680005070XA priority patent/CN101120208B/en
Priority to DK06718277.4T priority patent/DK1836439T3/en
Priority to KR1020077017063A priority patent/KR101362671B1/en
Priority to MX2007008516A priority patent/MX2007008516A/en
Publication of WO2006076549A1 publication Critical patent/WO2006076549A1/en
Priority to NO20073886A priority patent/NO340477B1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C6/00Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • F23C6/045Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D3/00Burners using capillary action
    • F23D3/40Burners using capillary action the capillary action taking place in one or more rigid porous bodies
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F22STEAM GENERATION
    • F22BMETHODS OF STEAM GENERATION; STEAM BOILERS
    • F22B21/00Water-tube boilers of vertical or steeply-inclined type, i.e. the water-tube sets being arranged vertically or substantially vertically
    • F22B21/34Water-tube boilers of vertical or steeply-inclined type, i.e. the water-tube sets being arranged vertically or substantially vertically built-up from water tubes grouped in panel form surrounding the combustion chamber, i.e. radiation boilers
    • F22B21/341Vertical radiation boilers with combustion in the lower part
    • F22B21/343Vertical radiation boilers with combustion in the lower part the vertical radiation combustion chamber being connected at its upper part to a sidewards convection chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/84Flame spreading or otherwise shaping
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D17/00Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2201/00Staged combustion
    • F23C2201/40Intermediate treatments between stages
    • F23C2201/401Cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2900/00Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • F23C2900/06041Staged supply of oxidant
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2203/00Gaseous fuel burners
    • F23D2203/10Flame diffusing means
    • F23D2203/102Flame diffusing means using perforated plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2203/00Gaseous fuel burners
    • F23D2203/10Flame diffusing means
    • F23D2203/105Porous plates
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2203/00Gaseous fuel burners
    • F23D2203/10Flame diffusing means
    • F23D2203/106Assemblies of different layers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00003Fuel or fuel-air mixtures flow distribution devices upstream of the outlet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00012Liquid or gas fuel burners with flames spread over a flat surface, either premix or non-premix type, e.g. "Flächenbrenner"
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/14Special features of gas burners
    • F23D2900/14582Special features of gas burners with outlets consisting of layers of spherical particles

Definitions

  • the present invention relates generally to fossil fuel combustion, and in particular, to a new and useful method and apparatus for gaseous fuel combustion in a steam generating boiler.
  • Fossil fuel burners convert chemical energy stored in fossil fuels to thermal heat by combusting the fossil fuel in the presence of an oxidant.
  • thermal heat may be transferred to water in order to produce steam for driving electricity producing turbines.
  • thermal heat can be transferred to any number of conceivable objects or processes.
  • Conventional steam generating boilers generally comprise of one or more burners, one or more fuel injection points, one or more oxidant injection points, and a means for propelling the injected fuel and oxidant into a combustion furnace.
  • a combustion envelope 4 is formed comprising a flame 3 and an oxidant/fuel mixing zone 2 between the flame 3 and the burner 1.
  • FIGS 2 and 3 are schematic representations of conventional steam generating boilers utilizing a single and multiple burner(s) respectively.
  • the interior wails comprise a plurality of steam generating tubes 6 fluidly connected to a boiler bank (not shown). Thermal energy produced within the combustion envelope 4 radiantly heats the tubes 6 which in turn coduct thermal energy to the water in the tubes 6 for the purpose of generating steam.
  • combustion furnace 5 In many steam generating boilers, the length and width of the combustion envelope 4 play an integral role in the design of the combustion furnace 5.
  • the combustion furnace 5 In FM boilers, for example, the combustion furnace 5 is preferably designed sufficiently large enough to avoid excessive contact of the combustion envelope 4 with the furnace walls 10. Also known as flame impingement, seen in Fig 3, excessive flame 3 contact with a furnace wall 10 may result in incomplete combustion, leading to higher emissions of CO and other combustion byproducts, or premature degradation, leading to costly repairs and boiler downtime. Accordingly, combustion furnaces 5 are generally designed to accommodate a given burner combustion envelope 4 while minimizing the possibility of flame impingement.
  • Conventional burners generally utilize flow control mechanisms to control the axial and radial expansion of the combustion envelope 4. Radial expansion of the combustion envelope 4 is generally a function of swirl and the natural expansion of the fuel, oxidant, and flame. Some conventional burner designs utilize flow control mechanisms to restrict the natural radial expansion of the combustion envelope 4, resulting in a longer narrower flame. Shearing forces created by flow control mechanisms may also be used to influence the extent of oxidant/fuel mixing prior to combustion, thereby having an effect on emissions such as CO and NOx.
  • the present invention solves the aforementioned problems and provides a steam generating boiler capable of firing liquid fuels, gaseous fuels, or any combination thereof.
  • An objective of the present invention is to provide a compact steam generating boiler.
  • Another objective of the present invention is to provide a steam generating boiler with a radially wider and axially shorter combustion envelope than that of conventional steam generating boilers.
  • Another objective of the present invention is to provide a low NOx and low CO steam generating boiler.
  • Another objective of the present invention is to provide a steam generating boiler capable of passively maintaining a constant ignition source.
  • a steam generating boiler according to the present invention comprises a combustion furnace, an oxidant inlet, a fuel inlet, a matrix means, and steam tubes.
  • FIG. 1 is a schematic representation of a combustion envelope.
  • FIG. 2 is a schematic representation of a conventional industrial boiler utilizing a single burner.
  • FIG. 3 is a schematic representation of a conventional industrial boiler utilizing more than one burner.
  • FIG. 4 is a schematic representation of an undesirable combustion envelope wherein excessive flame contact occurs along the length and width of the combustion furnace.
  • FIG. 5 is an embodiment of the present invention, wherein a matrix means is retrofitted into the combustion furnace of an existing steam generating boiler.
  • FIG. 6 is an illustration of an embodiment of the present invention wherein a fuel and an oxidant are introduced upstream of the a matrix means.
  • FIG. 7 is an illustration of an embodiment of the present invention wherein a fuel and an oxidant are introduced in the sides of a matrix means.
  • FIG. 8 is an illustration of an embodiment of the present invention wherein a fuel and an oxidant are introduced in both the front and the side(s) of a matrix means.
  • Fig 9. is a preferred embodiment of a matrix means according to the present invention, wherein matrix cross sections are illustrated.
  • Figure 10 is a graphic representation of an embodiment of the present invention where two matrix means are used to facilitate staged combustion.
  • Fig 11 is a graphic representation of a staged combustion embodiment of the present invention wherein interstaged cooling is used in a two matrix means staged combustion boiler.
  • Fig. 12 is a graphical illustration of an alternative embodiment of a matrix means according to the present invention.
  • Fig. 13 is a graphical illustration of another alternative embodiment of a matrix means according to the present invention.
  • the present invention utilizes a combination of features to improve upon the design of conventional oil and gas fired steam generating boilers.
  • Conventional oil and gas fired steam generating boilers include, but are not limited to: FM, High Capacity FM, PFM, PFI, PFT, SPB, and RB; all of which are described in Chapter 27 of Steam/its Generation and v Use, 41th Edition, Kitto and Stultz, Eds., ⁇ 2005 The Babcock & Wilcox Company, the text of which is hereby incorporated by reference as though fully set forth herein.
  • schematic views of FM boiler are used herein. However, as one of ordinary skill in the art can appreciate, the intent of utilizing FM boiler schematics is merely for reason of example and not intended to limit the present invention to that of FM boiler embodiments.
  • FIG. 2 and 3 schematic representations of prior art FM boilers are shown.
  • a baffle wall 20 separates a combustion furnace 5 from a boiler bank (not shown).
  • Combustion envelope 4 is located inside the combustion furnace 5. Fuel and oxidant are delivered to burner 1 , producing a combustion envelope 4 upon ignition.
  • the interior walls 10 of the combustion furnace comprise a series of tubes 6 fluidly connected to a steam drum 7, producing steam used for process of electrical generation purposes.
  • the conically diffusing shape of the combustion envelope 4 results in significant unused combustion furnace volume along side the combustion envelope 4 as it expands.
  • An object of the present invention is to reduce unused combustion furnace volume.
  • the present invention provides a matrix 8, placed either within or prior to the flame of the combustion envelope. Referring to Figure 5, a retrofit embodiment of the present invention is shown. Matrix 8 is placed with combustion furnace 5 downstream of the burner 1. Fuel and oxidant enter matrix 8, wherein the cross sectional design of matrix 8 provides a means for passively mixing gaseous streams and radially dispersing the resulting combustion envelope 9.
  • gaseous fuel stream Provided to the matrix 8 is at least one gaseous fuel stream and at least one gaseous oxidant stream, or combinations thereof.
  • the gaseous streams may enter the matrix 8 from any side.
  • Fig. 6 illustrates a preferred embodiment where the fuel stream 12 and oxidant stream 11 are introduced upstream of the matrix 8.
  • the gaseous streams 11 , 12 may enter the matrix 8 from the side(s) only or a combination of the front and side(s) of the matrix 8.
  • the combustion apparatus is a matrix 8 comprising at least one layer of spheres.
  • the spheres may be arranged in either a random or ordered manner within the matrix 8.
  • the spheres may be hollow, solid, or porous in nature, or any combination thereof.
  • the spheres may vary in size or be of a substantially similar size.
  • the spheres preferably comprise a high temperature metal or ceramic capable of withstanding the extreme temperatures to which the matrix 8 may be exposed during the combustion of fossil fuels, however, spheres comprising any known material may be used.
  • Plane 1 is approximately 46 percent open
  • plane two is approximately 31 percent open
  • plane 3 is about 9 percent open
  • plane 4 is about 58 percent open.
  • An object of the present invention is improved mixing of the gaseous streams. Improved mixing is achieved in the presence of a matrix 8 comprising at least two cross sectional planes having different percentages of open area, such that a first cross sectional plane possesses a greater percentage of open area for gaseous flow than a second cross sectional plane.
  • Plane 1 and plane 2 of Fig. 9 are two cross sectional planes having different percentages of open area for gaseous flow.
  • Another object of the present invention is to radially disperse the combustion envelope. Radial dispersion is achieved in the presence of matrix 8 comprising at least two cross sectional planes having different percentages of open area, wherein the two planes are taken from different axes, and a first cross sectional plane possesses a greater percentage of open area for gaseous flow than a second cross sectional plane.
  • Plane 3 and plane 4 of Fig. 9 are cross sectional planes of different axes having different percentages of open area for gaseous flow.
  • the present invention provides a combustion apparatus that allows for improved steam generating boiler designs while retaining similar heat output.
  • a schematic representation of the present invention retrofitted into a convention FM boiler is shown.
  • the present invention radially expands the combustion envelope 4, resulting in a shorter combustion envelope 9, wherein unused combustion volume is shifted downstream of the combustion envelope 9.
  • additional steam generating equipment can be placed in the unused combustion volume, thereby maximizing energy generation potential.
  • a benefit of reducing the depth of a combustion furnace is the ability to develop new compact boiler designs without sacrificing heat output.
  • Combustion furnaces 5 in steam generating boilers are generally designed to accommodate a given combustion envelope 4 while minimizing risk of flame impingement. Shortening the combustion envelope 4 allows for significant furnace depth reduction at any given heat output. Use of the present invention reduces boiler size, thus weight, as shorter boilers utilize considerably less raw materials to make boiler walls and tubes 6.
  • a matrix 8 according to the present invention may be placed anywhere within the combustion envelope 4.
  • the matrix 8 is placed within the mixing zone 2 and will be of a depth sufficient to allow combustion to begin within the matrix 8 and combustion flames 3 to exit the matrix 8 downstream of where fuel and oxidant are introduced.
  • flame width is maximized as ignition of the combustible stream creates expansive forces, enabling further radial expansion within the matrix 8.
  • an additional benefit of the present invention is passively maintaining a constant ignition source.
  • the matrix 8 is comprised of a material capable of retaining thermal heat. When a flame would otherwise lose ignition due to excessive velocities or fluctuations in fuel and/or oxidant streams, the thermal heat retained within the matrix elements provides a thermal reservoir sufficient to maintain ignition; thereby avoiding undesirable situations associated with delayed re- ignition.
  • a steam generating boiler may utilize more than one matrix 8.
  • Figure 10 is a graphic representation of an embodiment of the present invention where two matrixes are used to facilitate staged combustion.
  • a second matrix 14 is located downstream of a first matrix 8.
  • the first matrix 8 is provided with a fuel stream 18 and substoichiometric oxidant 17 to inhibit the production of undesirable combustion byproducts such as NOx.
  • a second oxidant stream 13, providing sufficient oxygen to burn remaining fuel, is provided downstream of the first matrix 8 and upstream of the second matrix 14.
  • Fig 11 illustrates an alternative two matrix staged combustion embodiment according to the present invention.
  • cooling tubes 15 are placed between the two matrixes 8, 14 for the purpose of controlling flame temperature and the formation of thermal NOx.
  • a perforated plate 150 may also be placed upstream of the first matrix 8, serving the function of acting as a flame arrestor and/or pre distributing the substoichiometric oxidant 17.
  • a sensor 16 may be placed within the combustion furnace for observing the combustion process within the combustion furnace 5.
  • a igniter 160 may be placed within the combustion furnace for preheating the matrix 8 or igniting a fuel and oxidant.
  • Fig. 12 provides a graphical representation of another embodiment of the present invention.
  • the matrix 8 comprises a random or ordered block of fibers or interlaced particles. Between the fibers and particles of this embodiment are series of internal passage having cross sections of varying open area for gaseous flow providing a means for gaseous fuel and oxidant streams to passively mix and radially disperse within the matrix 8.
  • Section A-A provides a cross section view of the present embodiment.
  • Fig. 13 provides a graphical representation of another embodiment of the present invention.
  • the matrix 8 comprises fired or fitted tiles with venturi holes 19.
  • An expanded view of a Section B-B of this embodiment is shown where the cross sectional dimensions of the venturi holes 19 are shown varying along the depth of the matrix 8.
  • oxidant and/fuel may be fed to the matrix 8 in multiple streams.
  • the matrix 8 can comprise of non-spherical elements or a combination of spherical and non-spherical elements arranged in either an ordered or non-ordered fashion.
  • the spheres or alternatively shaped elements may be coated with any number of chemical substrates known to one of ordinary skill in the art for the purpose of altering the chemistry of the fuel, enhancing combustion, and reducing pollutant emissions.
  • the matrix 8 itself can be rectangular, circular, or of any other geometric design.
  • the matrix 8 elements of the present invention are held captive by a suitable apparatus for preventing movement between the spheres. Examples of suitable apparatus are, but are not limited to, wire frames and/or chemically or mechanically bonding the matrix 8 elements to one another.
  • multiple matrixes may be arranged in parallel within a boiler.
  • multiple fuels may be combusted simultaneously, thereby providing combustion fuel flexibility to boiler designs.
  • forced air or recirculation fans may be utilized to create a pressure differential across the matrix 8 to either promote or restrict gaseous flow there through.

Abstract

A steam generating boiler having a matrix means (8) for reducing combustion volume. Matrix means (8) is placed in the combustion furnace (5) of a steam generating boiler, preferably downstream of fuel and oxidant stream (11, 12). Matrix means produces a shorter combustion envelope than that of a conventional boiler, allowing for reduced volume steam generating boilers.

Description

MATRIX MEANS FOR REDUCING COMBUSTION VOLUME
[001] Field of the Invention
[002] The present invention relates generally to fossil fuel combustion, and in particular, to a new and useful method and apparatus for gaseous fuel combustion in a steam generating boiler.
[003] Background of the Invention
[004] Fossil fuel burners convert chemical energy stored in fossil fuels to thermal heat by combusting the fossil fuel in the presence of an oxidant.
In power generating applications, thermal heat may be transferred to water in order to produce steam for driving electricity producing turbines.
In non power generating applications, thermal heat can be transferred to any number of conceivable objects or processes.
[005] Conventional steam generating boilers generally comprise of one or more burners, one or more fuel injection points, one or more oxidant injection points, and a means for propelling the injected fuel and oxidant into a combustion furnace. Upon ignition of the oxidant/fuel mixture (Fig .1 ) a combustion envelope 4 is formed comprising a flame 3 and an oxidant/fuel mixing zone 2 between the flame 3 and the burner 1.
[006] Figures 2 and 3 are schematic representations of conventional steam generating boilers utilizing a single and multiple burner(s) respectively. The interior wails comprise a plurality of steam generating tubes 6 fluidly connected to a boiler bank (not shown). Thermal energy produced within the combustion envelope 4 radiantly heats the tubes 6 which in turn coduct thermal energy to the water in the tubes 6 for the purpose of generating steam.
[007] In many steam generating boilers, the length and width of the combustion envelope 4 play an integral role in the design of the combustion furnace 5. In FM boilers, for example, the combustion furnace 5 is preferably designed sufficiently large enough to avoid excessive contact of the combustion envelope 4 with the furnace walls 10. Also known as flame impingement, seen in Fig 3, excessive flame 3 contact with a furnace wall 10 may result in incomplete combustion, leading to higher emissions of CO and other combustion byproducts, or premature degradation, leading to costly repairs and boiler downtime. Accordingly, combustion furnaces 5 are generally designed to accommodate a given burner combustion envelope 4 while minimizing the possibility of flame impingement.
[008] Conventional burners generally utilize flow control mechanisms to control the axial and radial expansion of the combustion envelope 4. Radial expansion of the combustion envelope 4 is generally a function of swirl and the natural expansion of the fuel, oxidant, and flame. Some conventional burner designs utilize flow control mechanisms to restrict the natural radial expansion of the combustion envelope 4, resulting in a longer narrower flame. Shearing forces created by flow control mechanisms may also be used to influence the extent of oxidant/fuel mixing prior to combustion, thereby having an effect on emissions such as CO and NOx.
[009] The availability of oxidant and fuel and their ability to mix prior to combustion influences the length of a combustion envelope 4 within a combustion furnace 5. Longer flames generally result from an insufficient supply of oxidant or inadequate mixing of the oxidant and fuel within the combustion envelope 4. Shorter flames generally result from a sufficient supply of oxidant and adequate mixing of the oxidant and fuel within the combustion envelope 4. Flame length may also be influenced by the velocity at which fuel and/or oxidant streams enter the combustion envelope 4. Excessive velocities or momentary interruptions of fuel and/or oxidant streams may cause the burner flame 3 to lose ignition. Such loss of ignition is especially undesirable, as it may result in an accumulation of combustibles susceptible to violent explosion upon reignition.
[0010] The U.S Department of Energy has articulated that a long felt need exists to reduce the size and weight of steam generator boilers such as industrial boilers. Conventional steam generating boilers are built to accommodate the size of the combustion envelope 4 produced. Accordingly, a long felt need exists to develop a combustion envelope 4 capable of producing sufficient thermal energy for steam production in a significantly smaller volume, thereby allowing the production of smaller, lighter, and more compact steam generating boiler designs.
[0011] Summary of the Invention
[0012] The present invention solves the aforementioned problems and provides a steam generating boiler capable of firing liquid fuels, gaseous fuels, or any combination thereof.
[0013] An objective of the present invention is to provide a compact steam generating boiler.
[0014] Another objective of the present invention is to provide a steam generating boiler with a radially wider and axially shorter combustion envelope than that of conventional steam generating boilers.
[0015] Another objective of the present invention is to provide a low NOx and low CO steam generating boiler.
[0016] Another objective of the present invention is to provide a steam generating boiler capable of passively maintaining a constant ignition source.
[0017] Yet another objective of the present invention is to provide a means for designing a steam generating boiler of reduced size and weight as compared to that of a conventional steam generating boiler. [0018] The present invention discloses a steam generating boiler. A steam generating boiler according to the present invention comprises a combustion furnace, an oxidant inlet, a fuel inlet, a matrix means, and steam tubes.
[0019] The various features of novelty which characterize the present invention are pointed out with particularity in the claims annexed to and forming a part of this disclosure. For a better understanding of the invention, its operating advantages and specific objects attained by its uses, reference is made to the accompanying drawings and descriptive matter in which the preferred embodiments of the invention are illustrated.
[0020] Brief Description of The Drawings
[0021] In the accompanying drawings, forming a part of this specification, and in which reference numerals shown in the drawings designate like or corresponding parts throughout the same:
[0022] FIG. 1 is a schematic representation of a combustion envelope.
[0023] FIG. 2 is a schematic representation of a conventional industrial boiler utilizing a single burner.
[0024] FIG. 3 is a schematic representation of a conventional industrial boiler utilizing more than one burner. [0025] FIG. 4 is a schematic representation of an undesirable combustion envelope wherein excessive flame contact occurs along the length and width of the combustion furnace.
[0026] FIG. 5 is an embodiment of the present invention, wherein a matrix means is retrofitted into the combustion furnace of an existing steam generating boiler.
[0027] FIG. 6 is an illustration of an embodiment of the present invention wherein a fuel and an oxidant are introduced upstream of the a matrix means.
[0028] FIG. 7 is an illustration of an embodiment of the present invention wherein a fuel and an oxidant are introduced in the sides of a matrix means.
[0029] FIG. 8 is an illustration of an embodiment of the present invention wherein a fuel and an oxidant are introduced in both the front and the side(s) of a matrix means.
[0030] Fig 9. is a preferred embodiment of a matrix means according to the present invention, wherein matrix cross sections are illustrated. [0031] Figure 10 is a graphic representation of an embodiment of the present invention where two matrix means are used to facilitate staged combustion.
[0032] Fig 11 is a graphic representation of a staged combustion embodiment of the present invention wherein interstaged cooling is used in a two matrix means staged combustion boiler.
[0033] Fig. 12 is a graphical illustration of an alternative embodiment of a matrix means according to the present invention.
[0034] Fig. 13 is a graphical illustration of another alternative embodiment of a matrix means according to the present invention.
[0035] Description of the Preferred Embodiments
[0036] The present invention utilizes a combination of features to improve upon the design of conventional oil and gas fired steam generating boilers. Conventional oil and gas fired steam generating boilers include, but are not limited to: FM, High Capacity FM, PFM, PFI, PFT, SPB, and RB; all of which are described in Chapter 27 of Steam/its Generation and v Use, 41th Edition, Kitto and Stultz, Eds., © 2005 The Babcock & Wilcox Company, the text of which is hereby incorporated by reference as though fully set forth herein. [0037] For the purposes of explaining the present invention, schematic views of FM boiler are used herein. However, as one of ordinary skill in the art can appreciate, the intent of utilizing FM boiler schematics is merely for reason of example and not intended to limit the present invention to that of FM boiler embodiments.
[0038] Referring to Figures 2 and 3, schematic representations of prior art FM boilers are shown. Within the FM boiler a baffle wall 20 separates a combustion furnace 5 from a boiler bank (not shown). Combustion envelope 4 is located inside the combustion furnace 5. Fuel and oxidant are delivered to burner 1 , producing a combustion envelope 4 upon ignition.
[0039] The interior walls 10 of the combustion furnace comprise a series of tubes 6 fluidly connected to a steam drum 7, producing steam used for process of electrical generation purposes. The conically diffusing shape of the combustion envelope 4 results in significant unused combustion furnace volume along side the combustion envelope 4 as it expands.
[0040] An object of the present invention is to reduce unused combustion furnace volume. The present invention provides a matrix 8, placed either within or prior to the flame of the combustion envelope. Referring to Figure 5, a retrofit embodiment of the present invention is shown. Matrix 8 is placed with combustion furnace 5 downstream of the burner 1. Fuel and oxidant enter matrix 8, wherein the cross sectional design of matrix 8 provides a means for passively mixing gaseous streams and radially dispersing the resulting combustion envelope 9.
[0041] Provided to the matrix 8 is at least one gaseous fuel stream and at least one gaseous oxidant stream, or combinations thereof. The gaseous streams may enter the matrix 8 from any side. Fig. 6 illustrates a preferred embodiment where the fuel stream 12 and oxidant stream 11 are introduced upstream of the matrix 8. Alternatively, as shown in Fig. 7 and Fig. 8, the gaseous streams 11 , 12 may enter the matrix 8 from the side(s) only or a combination of the front and side(s) of the matrix 8.
[0042] Referring to Fig. 9, a preferred embodiment of a matrix 8 according to the present invention is illustrated. In this embodiment, the combustion apparatus is a matrix 8 comprising at least one layer of spheres. The spheres may be arranged in either a random or ordered manner within the matrix 8. The spheres may be hollow, solid, or porous in nature, or any combination thereof. The spheres may vary in size or be of a substantially similar size. The spheres preferably comprise a high temperature metal or ceramic capable of withstanding the extreme temperatures to which the matrix 8 may be exposed during the combustion of fossil fuels, however, spheres comprising any known material may be used.
[0043] Referring to Figure 9, four cross sectional matrix planes are identified to schematically represent variations in open area for gaseous flow across the matrix 8. Plane 1 is approximately 46 percent open, plane two is approximately 31 percent open, plane 3 is about 9 percent open, and plane 4 is about 58 percent open.
[0044] An object of the present invention is improved mixing of the gaseous streams. Improved mixing is achieved in the presence of a matrix 8 comprising at least two cross sectional planes having different percentages of open area, such that a first cross sectional plane possesses a greater percentage of open area for gaseous flow than a second cross sectional plane. Plane 1 and plane 2 of Fig. 9 are two cross sectional planes having different percentages of open area for gaseous flow. As the gaseous streams pass between the two planes, a pressure differential is encountered forcing the gas streams to compress or expand; thereby creating shearing forces and mixing the gaseous streams. The superior mixing provided by the matrix 8, minimizes CO and excess air need to complete combustion.
[0045] Another object of the present invention is to radially disperse the combustion envelope. Radial dispersion is achieved in the presence of matrix 8 comprising at least two cross sectional planes having different percentages of open area, wherein the two planes are taken from different axes, and a first cross sectional plane possesses a greater percentage of open area for gaseous flow than a second cross sectional plane. Plane 3 and plane 4 of Fig. 9 are cross sectional planes of different axes having different percentages of open area for gaseous flow. As the gaseous streams approach plane 3, resistance is encountered due to the relatively low open area for gaseous flow across plane 3, forcing a portion of gas to change its vector towards a plane of lower flow resistance, such as plane 4; thereby axially suppressing and radially dispersing the combustion envelope.
[0046] The present invention provides a combustion apparatus that allows for improved steam generating boiler designs while retaining similar heat output. Referring back to Figs. 5, a schematic representation of the present invention retrofitted into a convention FM boiler is shown. The present invention radially expands the combustion envelope 4, resulting in a shorter combustion envelope 9, wherein unused combustion volume is shifted downstream of the combustion envelope 9. In retrofit applications, additional steam generating equipment can be placed in the unused combustion volume, thereby maximizing energy generation potential.
[0047] A benefit of reducing the depth of a combustion furnace is the ability to develop new compact boiler designs without sacrificing heat output. Combustion furnaces 5 in steam generating boilers are generally designed to accommodate a given combustion envelope 4 while minimizing risk of flame impingement. Shortening the combustion envelope 4 allows for significant furnace depth reduction at any given heat output. Use of the present invention reduces boiler size, thus weight, as shorter boilers utilize considerably less raw materials to make boiler walls and tubes 6. [0048] A matrix 8 according to the present invention may be placed anywhere within the combustion envelope 4. Preferably the matrix 8 is placed within the mixing zone 2 and will be of a depth sufficient to allow combustion to begin within the matrix 8 and combustion flames 3 to exit the matrix 8 downstream of where fuel and oxidant are introduced. In this embodiment, flame width is maximized as ignition of the combustible stream creates expansive forces, enabling further radial expansion within the matrix 8.
[0049] An additional benefit of the present invention is passively maintaining a constant ignition source. In this embodiment, the matrix 8 is comprised of a material capable of retaining thermal heat. When a flame would otherwise lose ignition due to excessive velocities or fluctuations in fuel and/or oxidant streams, the thermal heat retained within the matrix elements provides a thermal reservoir sufficient to maintain ignition; thereby avoiding undesirable situations associated with delayed re- ignition.
[0050] In another embodiment of the present invention, a steam generating boiler may utilize more than one matrix 8. Figure 10 is a graphic representation of an embodiment of the present invention where two matrixes are used to facilitate staged combustion. In this embodiment, a second matrix 14 is located downstream of a first matrix 8. The first matrix 8 is provided with a fuel stream 18 and substoichiometric oxidant 17 to inhibit the production of undesirable combustion byproducts such as NOx. A second oxidant stream 13, providing sufficient oxygen to burn remaining fuel, is provided downstream of the first matrix 8 and upstream of the second matrix 14.
[0051] Fig 11 illustrates an alternative two matrix staged combustion embodiment according to the present invention. In this embodiment, cooling tubes 15 are placed between the two matrixes 8, 14 for the purpose of controlling flame temperature and the formation of thermal NOx. A perforated plate 150 may also be placed upstream of the first matrix 8, serving the function of acting as a flame arrestor and/or pre distributing the substoichiometric oxidant 17.
[0052] In another embodiment of the present invention, a sensor 16 may be placed within the combustion furnace for observing the combustion process within the combustion furnace 5.
[0053] In another embodiment of the present invention, a igniter 160 may be placed within the combustion furnace for preheating the matrix 8 or igniting a fuel and oxidant.
[0054] Fig. 12 provides a graphical representation of another embodiment of the present invention. In this embodiment, the matrix 8 comprises a random or ordered block of fibers or interlaced particles. Between the fibers and particles of this embodiment are series of internal passage having cross sections of varying open area for gaseous flow providing a means for gaseous fuel and oxidant streams to passively mix and radially disperse within the matrix 8. Section A-A provides a cross section view of the present embodiment.
[0055] Fig. 13 provides a graphical representation of another embodiment of the present invention. In this embodiment the matrix 8 comprises fired or fitted tiles with venturi holes 19. An expanded view of a Section B-B of this embodiment is shown where the cross sectional dimensions of the venturi holes 19 are shown varying along the depth of the matrix 8.
[0056] In another embodiment of the present invention, oxidant and/fuel may be fed to the matrix 8 in multiple streams.
[0057] In another embodiment of the present invention, the matrix 8 can comprise of non-spherical elements or a combination of spherical and non-spherical elements arranged in either an ordered or non-ordered fashion.
[0058] In yet another embodiment of the present invention, the spheres or alternatively shaped elements may be coated with any number of chemical substrates known to one of ordinary skill in the art for the purpose of altering the chemistry of the fuel, enhancing combustion, and reducing pollutant emissions. [0059] In yet another embodiment of the present invention, the matrix 8 itself can be rectangular, circular, or of any other geometric design. Generally, the matrix 8 elements of the present invention are held captive by a suitable apparatus for preventing movement between the spheres. Examples of suitable apparatus are, but are not limited to, wire frames and/or chemically or mechanically bonding the matrix 8 elements to one another.
[0060] In yet another embodiment of the present invention, multiple matrixes may be arranged in parallel within a boiler. In such an embodiment, multiple fuels may be combusted simultaneously, thereby providing combustion fuel flexibility to boiler designs.
[0061] In yet another embodiment of the present invention, forced air or recirculation fans may be utilized to create a pressure differential across the matrix 8 to either promote or restrict gaseous flow there through.

Claims

CLAIMSWe Claim:
1. A steam generating boiler, comprising:
a generating bank, an economizer located downstream of the generating bank, and a combustion furnace located upstream of the generating bank comprising a oxidant inlet for providing an oxidant, a fuel inlet for providing a fuel, a plurality of steam tubes attached to a wall of the combustion furnace, wherein the steam tubes are fluidly connected to a steam drum located downstream of the combustion chamber, and a matrix means for passively mixing the oxidant and the fuel.
2. The steam generating boiler of claim 1 , wherein the matrix means radially disperses a combustion envelope produced by igniting the fuel and the oxidant.
3. The steam generating boiler of claim 2, wherein the matrix means comprises a layer of spherical elements.
4. The steam generating boiler of claim 2, wherein the spherical elements are ceramic.
5. The steam generating boiler of claim 2, wherein the spherical elements are metallic.
6. The steam generating boiler of claim 2, wherein the matrix means comprises a first cross section having an open area for gaseous flow, a second cross section having an open area for gaseous flow, and the open area for gaseous flow across the first cross section is greater than the open area for gaseous flow across the second cross section.
7. The steam generating boiler of claim 6, wherein the matrix means further comprises a third cross section and the open area for gaseous flow across the third cross sectional area is substantially equal to the open area for gaseous flow across the first cross section.
8. The steam generating boiler of claim 6, wherein the matrix means further comprises a third cross section and the open area for gaseous flow across the third cross sectional area is greater than the open area for gaseous flow across the second cross section.
9. The steam generating boiler of claim 2, wherein the combustion envelope protrudes the matrix means downstream of the fuel injection inlet.
10. The steam generating boiler of claim 9, wherein the matrix means comprises a thermal reservoir capable of maintaining ignition of the fuel and oxidant.
11. The steam generating boiler of claim 2, wherein the fuel inlet is located within the matrix means.
12. The steam generating boiler of claim 2, wherein the oxidant inlet is located within the matrix means.
13. The steam generating boiler of claim 2, further comprising a perforated plate located upstream of the matrix means.
14. The steam generating boiler of claim 2, wherein an air heater is located downstream of the economizer.
15. A steam generating boiler comprising,
a generating bank, an economizer located downstream of the generating bank, and a combustion furnace located upstream of the generating bank comprising a first oxidant inlet for providing a first oxidant, a second oxidant inlet for providing a second oxidant, a fuel inlet for providing a fuel, a plurality of steam tubes attached to a wall of the combustion furnace, wherein the steam tubes are fluidly connected to a steam drum located downstream of the combustion chamber, a first matrix means for passively mixing the first oxidant and the fuel, and a second matrix means located downstream of the first oxidant means for passively mixing the second oxidant and the fuel.
16. The steam generating boiler of claim 17, further comprising an inter-stage cooling tube located between the first matrix means and the second matrix means.
17. The steam generating boiler of claim 17, further comprising a perforated plate located upstream of the first matrix means.
18. The steam generating boiler of claim 15, further comprising an air heater located downstream of the economizer.
19. The steam generating boiler of claim 16, further comprising an igniter located between the first matrix means and the second matrix means.
20. The steam generating boiler of claim 16, further comprising a scanner located between the first matrix means and the second matrix means.
PCT/US2006/001185 2005-01-12 2006-01-12 Matrix means for reducing combustion volume WO2006076549A1 (en)

Priority Applications (12)

Application Number Priority Date Filing Date Title
ES06718277.4T ES2546645T3 (en) 2005-01-12 2006-01-12 Matrix means to reduce combustion volume
BRPI0606693-3A BRPI0606693B1 (en) 2005-01-12 2006-01-12 STEAM GENERATION BOILER
JP2007551388A JP5232474B2 (en) 2005-01-12 2006-01-12 Matrix means for reducing combustion volume
CA2594739A CA2594739C (en) 2005-01-12 2006-01-12 Matrix means for reducing combustion volume
AU2006204840A AU2006204840B2 (en) 2005-01-12 2006-01-12 Matrix means for reducing combustion volume
PL06718277T PL1836439T3 (en) 2005-01-12 2006-01-12 Matrix means for reducing combustion volume
EP06718277.4A EP1836439B1 (en) 2005-01-12 2006-01-12 Matrix means for reducing combustion volume
KR1020077017063A KR101362671B1 (en) 2005-01-12 2006-01-12 Matrix means for reducing combustion volume
DK06718277.4T DK1836439T3 (en) 2005-01-12 2006-01-12 MATRIX ORGAN TO REDUCE COMBUSTION RANGE
CN200680005070XA CN101120208B (en) 2005-01-12 2006-01-12 Matrix means for reducing combustion volume
MX2007008516A MX2007008516A (en) 2005-01-12 2006-01-12 Matrix means for reducing combustion volume.
NO20073886A NO340477B1 (en) 2005-01-12 2007-07-24 Power supply device for reducing combustion volume

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US64321905P 2005-01-12 2005-01-12
US60/643,219 2005-01-12

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WO2006076549A1 true WO2006076549A1 (en) 2006-07-20

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KR (1) KR101362671B1 (en)
CN (1) CN101120208B (en)
AU (1) AU2006204840B2 (en)
BR (1) BRPI0606693B1 (en)
CA (1) CA2594739C (en)
DK (1) DK1836439T3 (en)
ES (1) ES2546645T3 (en)
HU (1) HUE027866T2 (en)
MX (1) MX2007008516A (en)
NO (1) NO340477B1 (en)
PL (1) PL1836439T3 (en)
PT (1) PT1836439E (en)
RU (1) RU2410599C2 (en)
WO (1) WO2006076549A1 (en)
ZA (1) ZA200705847B (en)

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HUE027866T2 (en) 2016-11-28
RU2410599C2 (en) 2011-01-27
PL1836439T3 (en) 2015-12-31
KR101362671B1 (en) 2014-02-12
EP1836439B1 (en) 2015-07-01
DK1836439T3 (en) 2015-09-28
MX2007008516A (en) 2007-09-19
ZA200705847B (en) 2008-07-30
CN101120208A (en) 2008-02-06
AU2006204840B2 (en) 2011-09-29
KR20070101868A (en) 2007-10-17
CA2594739A1 (en) 2006-07-20
EP1836439A4 (en) 2013-09-04
JP2008527310A (en) 2008-07-24
BRPI0606693A2 (en) 2009-07-14
EP1836439A1 (en) 2007-09-26
NO20073886L (en) 2007-10-08
ES2546645T3 (en) 2015-09-25
RU2007144255A (en) 2009-06-10
CN101120208B (en) 2010-05-19
BRPI0606693B1 (en) 2019-05-14
JP5232474B2 (en) 2013-07-10
NO340477B1 (en) 2017-05-02
PT1836439E (en) 2015-10-12
AU2006204840A1 (en) 2006-07-20
CA2594739C (en) 2014-03-25

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