EP3260776A1 - Systeme de lance, citerne comprenant un systeme de lance et procede de reduction de nox - Google Patents

Systeme de lance, citerne comprenant un systeme de lance et procede de reduction de nox Download PDF

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Publication number
EP3260776A1
EP3260776A1 EP16175167.2A EP16175167A EP3260776A1 EP 3260776 A1 EP3260776 A1 EP 3260776A1 EP 16175167 A EP16175167 A EP 16175167A EP 3260776 A1 EP3260776 A1 EP 3260776A1
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EP
European Patent Office
Prior art keywords
inner tube
outer tube
lance system
boiler
reducing agent
Prior art date
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Granted
Application number
EP16175167.2A
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German (de)
English (en)
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EP3260776B1 (fr
Inventor
Stefan Dr. Hamel
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Steinmueller Engineering GmbH
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Steinmueller Engineering GmbH
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Publication date
Application filed by Steinmueller Engineering GmbH filed Critical Steinmueller Engineering GmbH
Priority to RS20190734A priority Critical patent/RS58920B1/sr
Priority to PL16175167T priority patent/PL3260776T3/pl
Priority to EP16175167.2A priority patent/EP3260776B1/fr
Priority to PCT/EP2017/065077 priority patent/WO2017220571A1/fr
Publication of EP3260776A1 publication Critical patent/EP3260776A1/fr
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Publication of EP3260776B1 publication Critical patent/EP3260776B1/fr
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J15/00—Arrangements of devices for treating smoke or fumes
    • F23J15/02—Arrangements of devices for treating smoke or fumes of purifiers, e.g. for removing noxious material
    • F23J15/04—Arrangements of devices for treating smoke or fumes of purifiers, e.g. for removing noxious material using washing fluids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J15/00—Arrangements of devices for treating smoke or fumes
    • F23J15/003—Arrangements of devices for treating smoke or fumes for supplying chemicals to fumes, e.g. using injection devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J7/00—Arrangement of devices for supplying chemicals to fire
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23J—REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J2219/00—Treatment devices
    • F23J2219/20—Non-catalytic reduction devices

Definitions

  • the present invention relates to a lance system, a boiler system containing the lance system and a method for NOx reduction.
  • NO x nitrogen oxides
  • NO x The formation of NO x is subject to complex reaction mechanisms, the most important NO x sources being the oxidation of the nitrogen of the combustion air (thermal NO x ) and the oxidation of the fuel nitrogen (fuel NO x ).
  • Thermal NO x is formed essentially at temperatures greater than about 1200 ° C to 1500 ° C, because only at these temperatures the molecular oxygen present in the air changes noticeably into atomic oxygen (thermal oxidation) and with the nitrogen of the air combines.
  • the rate of formation of the thermal NO x depends exponentially on the temperature and is proportional to the oxygen concentration.
  • the primary nitrogen compounds contained in the fuel first disintegrate into secondary nitrogen compounds (simple amines and cyanides), which are competitively converted to either NO x or N 2 in the course of combustion.
  • secondary nitrogen compounds simple amines and cyanides
  • NO x is competitively converted to either NO x or N 2 in the course of combustion.
  • N 2 is preferred or the formation of NO x is suppressed or even reversed.
  • the formation of fuel NO x is only slightly dependent on temperature and proceeds even at low temperatures.
  • the reduction of NOx is carried out in the prior art by means of primary measures such as the air staging at the burner and above the combustion chamber height.
  • the air grading above the combustion chamber height is carried out in such a way that the burner belt area is usually operated under stoichiometry.
  • ABL burnout air
  • the remaining air needed for burnout is then usually added at a considerable distance above the burner belt.
  • OFA Over-Fire-Air
  • the addition takes place by means of so-called ABL nozzles.
  • ABL nozzles The two basic types of ABL nozzles are wall nozzles and ABL lances.
  • the wall nozzles are installed on one wall, two walls or even on all four walls. It is also customary in the prior art to admit the combustion air over several levels at different heights of the firebox. The aim is to achieve the best possible mixing between the rising flue gas and the burnout air added via the ABL nozzles. Due to the substoichiometric operation of the burner belt area, flue gas still contains unburned constituents, such as carbon monoxide, but also coke particles, etc., which are to be converted by means of the addition of air.
  • the second basic device for injecting the required combustion air are so-called lances. These protrude into the firebox or boiler and release the air into the flue gas via a multitude of small nozzles distributed over the lance length. By arranging a plurality of lances and the plurality of nozzles per lance system, a uniform distribution of the burnout air over the cross-sectional area is achieved.
  • lances are also often mounted in the area within the first heating surfaces, which are connected downstream of the furnace. This offers the practical advantage that the lances then no longer represent self-supporting elements, but can be deposited on the Schundunen. A static design is thus considerably simplified.
  • ABL wall nozzles are often combined in possibly several levels and, for example, as in the flue gas direction last stage running lances.
  • the invention relates to a method for the reduction of undesirable substances by injecting a reagent into a flue gas of a steam generator, in which the reagent is injected by means of lances in the combustion chamber of the steam generator. Furthermore, the invention relates to a lance or a lance system for the Injecting of reagent into a furnace of a steam generator for the reduction of undesirable substances in the flue gas. In addition, the invention also relates to a furnace of a steam generator with such a device.
  • the reactants are, for example, ammonia and / or urea, which can reduce the proportion of nitrogen oxides in the flue gas.
  • Corresponding processes are referred to as selective noncatalytic reduction (SNCR).
  • SNCR selective noncatalytic reduction
  • reducing agents in aqueous solution typically ammonia water, urea
  • gaseous ammonia
  • the optimum temperature range for the execution of the reactions described is dependent on the flue gas composition between 900 and 1100 ° C.
  • SNCR technology is successfully used in small and medium sized boilers and especially in waste incineration plants.
  • the flue gas is passed through one or two so-called empty passes.
  • the flue gas already gives off energy to the walls of these empty ducts and already reaches such a low temperature before entering the convective heating surfaces, for example to prevent corrosion problems in the heating surfaces (eg in biomass, waste wood and waste incineration boilers).
  • this often means that the temperature window relevant to the SNCR technology is reached within the empty trains. Together with the comparatively small dimensions, therefore, the SNCR technology is effective and optimized applicable here.
  • FACE Furnace Exit Gas Temperature
  • This temperature indicates the flue gas temperature when leaving the combustion chamber and when entering the convective heating surfaces and it usually depends on the ash softening behavior of the fuels used. The goal is to keep the FEGT below the asher softening point to minimize fouling of the convective heating surfaces.
  • These temperatures depend on the fuels used, but are typically in the range 1050 to 1150 ° C for lignite, typically in the range 1000 to 1300 ° C for hard coal, and in the range 1000 to 1100 ° C for large-scale boilers converted to woody biomass.
  • the temperature profile in the combustion chamber is additionally influenced by a large number of firing types and boiler geometries.
  • the DE 44 34 943 C2 describes the injection of the reducing agent by means of two-fluid nozzles with simultaneous measurement of the temperature profile of the boiler and the injection level, whereby the optimum temperature window is determined. By changing the position and the angle of the nozzles they can be aligned to the optimal temperature window.
  • the DE 10 2008 004 008 A1 discloses the direct atomization of aqueous reducing agent into the flue gas.
  • the EP 0 530 255 B1 discloses injecting a NOx reducing mixture of liquid and gas into the flue gas within a temperature optimal window for the reaction, the mixture being injected into liquid droplets that have evaporated before impinging on a surface.
  • the document also describes the use of the injection method by means of a lance placed between heating surface packages, which is equipped with a multiplicity of nozzles in order to achieve an even distribution over the cross section into the flue gas.
  • the DE 197 81 750 T1 ( WO 97/41947 A1 ) discloses an injection lance for injecting anhydrous NH 3 and air into a furnace.
  • the lance consists of three tubes, which are arranged one inside the other, whereby the ammonia is introduced into the inner tube, at the inner end enters the gap between the inner and middle tube, there also meets with the air and is mixed with this, the in the gap between the middle and outer tube is passed. Through a plurality of openings, the ammonia / air mixture flows from the interior of the middle tube through radial channels, which bridge the gap between the middle and outer tube, in the flue gas of the boiler.
  • the DE 10 2010 050 334 A1 discloses the atomization of liquid reducing agent into the flue gas, wherein the droplets are vaporized prior to any wall contact.
  • the device described provides a vertical lance introduced through the boiler ceiling, which atomises at the end horizontally or at an angle to the horizontal of -10 to 60 °.
  • the document DE 10 2004 026 697 A1 discloses a method of injecting reductant together with the upper air. This will be part of the combustion air introduced by means of first ABL nozzles in the flow direction, a further part of the Ausbandluft is introduced with a second nozzle within which the injection nozzle for introducing nitrogen oxide reducing agent is simultaneously located.
  • the DE 10 2012 110 962 A1 describes the injection of reducing agent via wall mounted multi-component nozzles.
  • process-required combustion air can be used as a so-called enveloping medium in order to initially shield the reducing agent from the flue gas and at the same time to achieve a greater penetration depth for preferably large furnace dimensions.
  • the EP 2 962 743 A1 discloses the introduction of reducing agent with control valves, a sensor for measuring NOx concentrations over the boiler cross-section and a controller that controls the amount of reducing agent to be introduced. Furthermore, the use of lances for injecting the reducing agent is described, in which one or more injectors are introduced for reducing agent and these lances also supplied, for example, combustion air. Here, it is proposed in particular to introduce a plurality of injectors with different penetration depth into the lances, which can then inject different amounts of reducing agent into the lance on the basis of the present measurement data.
  • the boiler cross-section can be virtually divided into segments, which can each be supplied with individual amounts of reducing agent.
  • the described technology of reducing agent addition via the ABL lances allows the distribution of the reducing agent across the cross section.
  • the amount of reducing agent in certain quadrants can be controlled individually. This is achieved by the fact that the reducing agent injectors protrude at different depths into the ABL lance. Injected there, the reducing agent leaves the lance through the nearest outlet openings of the lance in the flue gas. The atomization at the lances of the lance involves the risk of droplets escaping from the lance.
  • the US 5,342,592 discloses an injection lance of a complicated construction including an outer tubular jacket with a cooling circuit.
  • This outer tubular sheath has a plurality of openings along the sheath.
  • This tubular sheath also has an inner channel into which an injection lance is inserted.
  • This in turn consists of an inner tube and an outer tube, wherein a gap is formed.
  • the reducing agent is passed through the interior of the inner tube and the propellant through the gap.
  • the reducing agent passes from the interior of the inner tube and via the inner tube branching channels that bridge the gap directly into the flue gas stream.
  • the propellant meets at the nozzles, ie at the outlet of the branches of the inner tube channels, from the intermediate space with the reducing agent and enters the flue gas stream.
  • the US 2004/0201142 A1 discloses an injection lance for injecting a mixture of steam and ammonia gas with two nested tubes, wherein along the outer tube a plurality of openings are arranged, which are connected via channels to the interior of the inner tube.
  • a feed tube which projects into the outer end of the outer tube in this, has openings and supplies the space between the inner tube and the outer tube with the reducing agent / vapor mixture.
  • the mixture flows along the gap to the opposite closed end of the lance or the outer tube.
  • the mixture passes into the open end of the inner tube and via the channels branching off from the inner tube (which bridge the gap and are not in fluid communication with it) directly into the flue gas stream.
  • the US 5,281,403 describes an injection lance system having an inner tube and an outer tube forming a gap through which the reducing agent is passed.
  • the reducing agent is fed into a conduit located in the inner cavity of the inner tube, the conduit being provided with a plurality of nozzles.
  • a carrier gas is introduced in this inner cavity.
  • the nozzles of the arranged within the inner cavity line through a respective corresponding outlet opening in the injection lance system, the reagent in the flue gas, wherein the reagent is mixed simultaneously with the carrier gas, which in the inner cavity is passed and leaves the lance system also through said exit opening.
  • the technical object of the invention was to provide a simply constructed and cost-effective lance system to mix nitrogen oxide reducing agent as evenly distributed in a combustion gas. Furthermore, the object was to provide a lance with which the reducing agent can be injected in the vicinity of or between heating surface packages. In addition, the object when using reducing agent dissolved in water was that the heating surface pipes are not struck by liquid medium containing the reducing agent in order to reduce or avoid corrosion damage to the heating surfaces.
  • a lance system for introducing reducing agents into a boiler for selective noncatalytic reduction of nitrogen oxides in combustion gases, having an interior section designed to be located within the boiler, and an exterior section constructed to be located outside the boiler wherein the lance system comprises an inner tube and an outer tube, and at least along the inner portion of the lance system, the inner tube is disposed within the outer tube, thereby forming a gap between the outer wall of the inner tube and the inner wall of the outer tube, according to the invention
  • a plurality of first outlet openings in the peripheral wall of the inner tube is arranged, and along the outer tube a plurality of second outlet openings is arranged in the peripheral wall of the outer tube, the first outlet openings of the inner tube open into the intermediate space, the interior of the inner tube is in fluid communication with the intermediate space via the first outlet openings of the inner tube and the intermediate space is in fluid communication with the outer side via the second outlet openings of the outer tube.
  • nitrogen oxide reducing agent can be mixed into a combustion gas as evenly as possible. Furthermore, the design and operation of the lance system allows the reducing agent to be injected in the vicinity of or between heating surface packages, in a purely gaseous form, without the risk of liquid droplets.
  • the heating surface pipes are not struck by liquid medium containing the reducing agent.
  • this is achieved by a pipe-in-pipe combination, wherein the outer diameter of the inner tube is smaller than the inner diameter of the outer tube.
  • the ratio of inner diameter of the outer tube to the outer diameter of the inner tube of 1: 0.1 to 1: 0.9, preferably from 1: 0.3 to 1: 0.6.
  • only one (number 1) inner tube is mounted in the outer tube.
  • the inner tube preferably extends substantially over the entire length of the outer tube in the inner portion.
  • the end of the inner tube (inner end) located in the inner section of the lance system, which is preferably closed, can contact the end of the outer tube, which is also situated in the inner section, but will generally have a certain distance therefrom.
  • the inner tube within the outer tube extends from 50% to 100%, preferably from 60% to 100%, preferably from 70% to 100%, more preferably from 95% to 100%, particularly preferably from 98% to 100% , and particularly preferably from 99% to 100% of the inner section running distance of the outer tube.
  • the number and positioning of the second outlet openings depends on the arrangement or the division of the heating surfaces or Bank lakerohre mounted in the boiler.
  • the second outlet openings are arranged so that they do not flow directly to the heating surfaces or Edel lakerohre.
  • the number and arrangement of the second outlet openings according to the flow shape of the flue gas and at which point in the cross section of the combustion chamber which amounts of reducing agent or oxidant (burnout) is required. Accordingly, the number, arrangement and size of the second outlet openings may vary.
  • a multiplicity of second outlet openings in the peripheral wall of the outer tube here preferably means at least 4, 6, 8, 10, 20, 30, 40, 50, 60, 70, 80, 90, 100.
  • a plurality of pairs of second outlet openings are provided in the outer tube, in each case two second outlet openings are opposite, in particular in each case a pair of second outlet openings is positioned so that the outlet openings are aligned with a free space between the Edel vomrohren.
  • a pair of second outlet openings can be aligned in each free space between the Edel vomrohren. This embodiment is in FIG. 3 shown.
  • only every second free space between the Edel vomrohren be supplied with a pair of second outlet openings. This embodiment is in FIG. 4 shown. Since several lance systems are provided in one boiler, they can then be injected into the heating surfaces offset from each other (see FIG. 4 ).
  • the present flow field and the temperature field it is also possible to provide further embodiments, such as, for example, every third free space between the heating surface pipes, etc.
  • the second outlet openings or the pairs of second outlet openings can be arranged equidistantly or not equidistantly along the longitudinal axis of the lance system.
  • the first outlet openings preferably follow the scheme of the arrangement of the second outlet openings.
  • each second outlet opening and / or each pair of second outlet openings is associated with one or two first outlet openings.
  • the first outlet openings are preferably arranged with respect to the flow direction in the intermediate space (between the inner and outer tubes) upstream of the second outlet openings.
  • a great many, preferably at least 20, 40, 60, 80, 100, 200, 400 first outlet openings are arranged in the inner tube.
  • the inner tube can be referred to as perforated with first outlet openings. It is understood that even in the embodiment of a perforated inner tube according to the invention, areas of the inner tube are excluded from the perforation, the second outlet openings in the outer tube opposite.
  • a mixing chamber for mixing the reducing agent and the oxidizing agent preferably air
  • the mixture enters the interior of the inner tube.
  • the invention makes use of the gaseous medium (combustion air) required in the combustion process.
  • the design of the lance system according to the invention with the two nested tubes, inner tube and outer tube, represents a simple construction method. This results in lower costs for production and maintenance. With this construction, it can be avoided in particular that the lance system is damaged by distortion due to temperature fluctuations. Because the two nested tubes are preferably not firmly connected.
  • the diameter of the outer tube decreases in the direction of the inner end. This measure serves to maintain the velocity of the mass flow in the gap, and to reduce the weight of the lance system.
  • the rejuvenation of the outer tube can be done continuously or in stages.
  • the diameter of the inner tube can also be reduced in the direction of the inner end.
  • complete evaporation is achieved by first passing the reducing agent mixed with hot oxidizing agent (preferably air) into an inner tube, then into the space between the inner tube and the first via the first outlet openings Outer tube is transferred, there again with hot oxidizing agent (preferably air) is mixed and then leaves the lance system on the second outlet openings in the outer tube.
  • hot oxidizing agent preferably air
  • the intermediate stage of (residual) evaporation in the space between Inner tube and outer tube is inventively achieved in that the first outlet openings of the inner tube open into the intermediate space. This means that the second outlet openings of the outer tube are arranged offset with respect to the first outlet openings of the inner tube.
  • the "staggered" arrangement of the first to the second outlet openings according to this invention also has a functional significance.
  • a structurally offset arrangement, for example of radial bores as the first and second outlet openings, is usually functionally fulfilled the requirement that the mixture containing reducing agent from the inner tube is first passed into the space, so that there mixed with other gaseous oxidation medium and is completely evaporated.
  • the functional aspect of the "staggered” arrangement also means that, for example, a first outlet opening with an inclined tubular attachment (whose axis is not perpendicular to the longitudinal axis of the inner tube) is directed towards the inner wall of the outer tube and is not directed toward a second exit opening, also If the position of this second outlet opening relative to the first outlet opening radially and / or offset or displaced in the longitudinal direction.
  • the desired mixing of the reducing agent in the intermediate space with the additionally supplied there oxidizing agent depending on the distance to the second outlet opening and their dimensions may not be given because the emerging from the first outlet fluid would be at least partially gedüst directly through the second outlet opening , as is the case in the prior art. This is undesirable according to the invention, because the mixture coming from the interior of the inner tube is first to be evaporated completely in the intermediate space before it leaves the outer tube.
  • the first outlet openings in particular those in the form of nozzles, tubes or pipe sockets, not directed in the direction of or on the present in the immediate vicinity of the second openings.
  • the axes of the first outlet openings of the inner tube are directed to the inner wall of the outer tube.
  • the axes of each first outlet opening meet the inner wall of the outer tube at a closed wall portion of the outer tube. This measure will ensures that the first outlet openings of the inner tube open into the intermediate space.
  • first outlet openings of the inner tube and the second outlet openings of the outer tube are arranged so that the mixture emerging from the first outlet openings can not pass directly through the second outlet openings to the outside.
  • the first outlet openings of the inner tube and the second outlet openings of the outer tube are therefore offset from one another.
  • offset here means not only that any axis, for example, is perpendicular to the longitudinal axis of the inner tube, as would be the case in the simplest form of outlet openings - the radial bore - not simultaneously by a first and second outlet opening extends.
  • Offset also means also that, for example, in inclined outlet openings, and the axis of the first outlet opening does not extend through a second outlet opening, but the inner wall of the outer tube intersects.
  • the distance of the intersection of the axis of each first outlet opening (outlet opening of the inner tube) to the edge of the nearest second outlet opening (outlet opening of the outer tube) is at least 1.5 times, more preferably at least 2.0 times that Radius of the respective first outlet opening.
  • a gap between inner tube and outer tube is defined, which extends over the entire circumference of the inner tube. Furthermore, it is preferred that the gap between the outer wall of the inner tube and the inner wall of the outer tube extends over the entire length of the inner tube.
  • the inner end of the inner tube is usually preferably closed, or provided with one or more first openings. Again, this first outlet opening opens into the intermediate space.
  • the measure according to b), according to which further oxidizing agent is fed separately into the intermediate space between the inner tube and the outer tube, means that further oxidizing agent is not supplied via the inner tube, but via a feed of the outer tube.
  • this supply is arranged for the further oxidant for the gap in the outer portion of the lance system, which is designed to supply the space between the inner tube and the outer tube with a gaseous oxidant, preferably air.
  • the outer tube has an inner end and an outer end, the outer end being in fluid communication with a supply for introducing the gaseous oxidant into the gap.
  • a mixing chamber is in the outer portion of the lance system, which is in fluid communication with the interior of the inner tube and is designed to supply this interior with a fluid containing the reducing agent, wherein the mixing chamber, a supply for the reducing agent and a supply for a gaseous oxidizing agent, preferably air. More preferably, the mixing chamber and / or the reducing agent supply in the mixing chamber to a supply for a propellant.
  • the supply of the gaseous oxidant into the mixing chamber is preferably designed so that the gaseous oxidant tangentially into the mixing chamber flows. This measure serves the improved mixture of reducing agent and gaseous oxidizing agent.
  • means may be arranged in the mixing chamber, in particular baffles or swirl bodies, in order to improve the mixing of the fluid containing the reducing agent with the gaseous oxidizing agent.
  • the supply of the reducing agent can be carried out as a one-component nozzle, if only the reducing agent is introduced into the mixing chamber, or as two-component nozzles, if the reducing agent is introduced together with a blowing agent (preferably compressed air) into the mixing chamber.
  • a blowing agent preferably compressed air
  • the first outlet openings of the inner tube can be designed differently.
  • the first outlet openings are preferably selected from the group consisting of holes, nozzles, tubes and pipe sockets.
  • the design of the first outlet openings may be different and, in particular, serves to predetermine the mixture emerging from the inner tube, containing the reducing agent.
  • a preferred construction of the first outlet openings of the inner tube is a tangential with respect to the inner tube, so that the inflow into the enveloping outer tube, ie in the space between the inner and outer tube, an additional twisting and improved mixing with the introduced separately into the gap Oxidizing agent (preferably combustion air) causes.
  • the first outlet openings can be tangential and in the direction of the flow within the Aligned outer tube.
  • the individual first outlet openings can have individual and different opening dimensions. Thus, it is possible to deliver the exiting flow of material, for example over the length of the inner tube differently in the enveloping outer tube.
  • the first outlet openings can also be designed only as holes in the inner tube, which can then be present in a larger number. As the first outlet openings of the inner tube and radial bores in the shell or the wall of the inner tube can serve.
  • the mass flow passing through the interior of the inner tube and containing the reducing agent only when leaving the inner tube passes through the first outlet openings into the intermediate space with the further gaseous oxidizing agent separately conducted into the intermediate space between inner tube and outer tube.
  • the interior of the inner tube is in fluid communication only via the first outlet openings in the jacket or the wall of the inner tube and, if present, with the first outlet openings at the inner end of the inner tube with the intermediate space.
  • the second outlet openings of the outer tube can also be designed differently.
  • the second outlet openings are preferably selected from the group consisting of holes, nozzles, tubes and pipe sockets.
  • the respective axis of a second outlet opening of the outer tube is aligned radially at right angles to the longitudinal axis of the outer tube. If the lance system is arranged horizontally in the vessel, then the respective axis of a second exit opening will also be oriented horizontally or, preferably, inclined downwardly with respect to the horizontal, i. aligned inclined against the flow direction of the combustion gas stream. If the lance system is arranged vertically in the boiler, then the respective axis of a second outlet opening can be aligned horizontally.
  • the lance system Since the lance system is arranged to extend vertically, in particular in two-pass boilers, and in these boilers, the flow direction of the combustion gas flow at the position of the lance systems usually not upwards but horizontally or with respect to the horizontal at an angle of 0 to 80 °, it makes sense to align the axis of the second outlet openings of the lance system according to the main combustion gas flow inclined. If the lance system is arranged vertically in the vessel, then the respective axis of a second outlet opening is inclined relative to the flow direction of the combustion gas flow.
  • the inclination of the axes of the second exit port against the combustion gas flow is preferred. This measure serves to extend the residence time of the reducing agent in the correct temperature window of the combustion gas stream.
  • the measure "counter to the flow direction of the combustion gas flow” here means an angle of 0 to less than 90 ° C with respect to the flow direction of the combustion gas flow (contrary to this flow direction).
  • a further preferred embodiment of the lance system is designed so that the distance between inner tube and outer tube is maintained by spacers, these spacers are preferably selected from the group consisting of pins, rods, webs, baffles.
  • the inner tube and outer tube are preferably not fixed together, but the spacers are fixed either on the outside of the inner tube, and preferably not on the inside of the outer tube, or the spacers are on the inside of the outer tube attached, and preferably not on the outside of the inner tube.
  • baffles are arranged in the intermediate space such that the flow within the intermediate space is set into a rotation (twist) about the inner tube. The flow of the mixture around the inner tube causes a higher turbulence and better mixing.
  • the invention further provides a boiler having at least one fuel supply, at least one oxidizer supply, one or more levels of heating surfaces and at least one lance system of the invention as described above; wherein the inner portion of the lance system is disposed within the vessel, and the outer portion of the lance system is located outside the vessel.
  • the boiler fuel and combustion air are brought together to carry out the combustion.
  • the resulting flue gas or combustion gas flows through the furnace and then through the subsequently arranged in the flue gas flow heating surfaces.
  • the furnace is operated with air staging, so that the combustion air added to the burner is not sufficient for complete conversion of the fuel but substoichiometric.
  • combustion air is added, for example, below the convective heating surfaces by means of wall nozzles for further combustion.
  • one or more lance systems according to the invention is or are arranged, which supply the nitrogen oxide reducing agent.
  • the lance systems can be arranged horizontally or vertically in the boiler.
  • the reducing agent is mixed with a portion of the combustion air required for the combustion process and fed into the interior of the inner tube and passes through the first outlet openings in the inner tube in the space between the inner tube and outer tube.
  • the other part of the burnout air is also supplied via the lance system to the combustion gas by direct into the outer tube i. is passed into the space between the inner tube and outer tube. In the space the remaining liquid is evaporated.
  • the gas mixture containing the reducing agent passes through the second outlet openings in the outer tube into the flue gas stream.
  • the mixing chamber, the supply of the reducing agent into the mixing chamber, the supply of gaseous oxidizing agent are arranged in the mixing chamber outside the boiler.
  • a supply for a propellant is further arranged to distribute the reducing agent in the mixing chamber.
  • the boiler means are arranged in the mixing chamber, in particular baffles or swirl body to improve the mixing of the fluid containing the reducing agent with the other supplied gaseous oxidant.
  • baffles or swirl body are arranged in the mixing chamber, in particular baffles or swirl body to improve the mixing of the fluid containing the reducing agent with the other supplied gaseous oxidant.
  • the supply for the introduction of a gaseous oxidizing agent is arranged in the space between the inner tube and the outer tube outside the boiler.
  • the alignment of the lance systems in the boiler can be horizontal or vertical.
  • the heating surfaces are horizontal in the boiler, so that the lance systems according to the invention can be placed running horizontally on the heating surfaces or otherwise attached to the heating surfaces as mentioned above.
  • the heating surfaces can be placed hanging from above.
  • the tubes of the heating surfaces extend vertically, so that the lance systems according to the invention can not be deposited on the heating tubes.
  • appropriate brackets can be provided so that the lance systems can be mounted horizontally extending to the existing support tubes.
  • the lance systems in this type of boiler can also be installed vertically suspended from the ceiling wall of the system.
  • one or more lance systems according to the invention may be arranged.
  • a plurality of lance systems are distributed uniformly over the inner cross section of the boiler, so that each area of the combustion gas flow is achieved for the reducing agent.
  • the lance systems can also be arranged one above the other in one or more horizontal planes, in particular in the case of horizontal alignment of the lance systems. Between the several horizontal planes of the lance systems, but may not be, heating surfaces or one or more Schuvide or parts thereof may be arranged.
  • a plurality of lance systems are arranged parallel to one another, preferably at right angles to the panes of the adjacent heating surfaces.
  • the second outlet openings arranged parallel to the outer tubes ( FIG. 3 ) or combing ( FIG. 4 ).
  • the lance system or lance systems are arranged to mix the mixture containing the reducing agent and oxidizing agent into the combustion gases rising through the lanes of the heating surfaces.
  • the lance systems are located on a heating surface.
  • the mixture is mixed below the heating surface so that the reducing agent can flow through the lanes of the heating surfaces with the combustion gas upwards and can mix with this.
  • the lance systems are mounted below the heating surfaces.
  • the lance systems in the boiler can be arranged horizontally or vertically.
  • the respective axis of a second outlet opening is also aligned horizontally or preferably inclined downwardly with respect to the horizontal, i. against the flow direction of the combustion gas stream.
  • the orientation of the axes of the second outlet openings depends on the flow direction of the combustion gas flow.
  • the axes of the second outlet openings are inclined relative to the flow direction of the combustion gas stream.
  • the inclination of the axes of the second outlet opening is inclined relative to the combustion gas stream. This measure serves to extend the residence time of the reducing agent in the correct temperature window of the combustion gas stream.
  • a nitrogen-containing compound is used, selected from the group consisting of urea, ammonia, cyanuric acid, hydrazine, ethanolamine, biuret, triuret, ammelides, ammonium salts of organic and inorganic acids (for example, ammonium acetate, ammonium sulfate, ammonium bisulfite, ammonium bisulfite, Ammonium formate, ammonium carbonate, ammonium bicarbonate, ammonium nitrate, ammonium oxalate), preferably urea or ammonia.
  • the reducing agent is preferably in aqueous solution (eg ammonia water, or urea dissolved in water) or gaseous (ammonia) fed into the mixing chamber.
  • the gaseous oxidant is introduced tangentially into the mixing chamber.
  • the reducing agent is introduced into the mixing chamber with the aid of single-substance nozzles, or with the aid of two-substance nozzles together with a blowing agent (preferably compressed air).
  • the reducing agent and the oxidizing agent in the mixing chamber are further fluidized by means arranged in the mixing chamber, in particular baffles or swirl bodies, in order to improve the mixing of the fluid containing the reducing agent with the gaseous oxidizing agent.
  • the oxidant (preferably air) fed into the mixing chamber and the further oxidant (preferably air) fed separately into the gap independently of one another have a temperature of 200 ° C to 400 ° C.
  • the gaseous oxidizing agent or the mixture containing reducing agent and oxidizing agent in the intermediate space between inner tube and outer tube is set into a rotation (swirl) around the inner tube. This is preferably done by appropriately arranged baffles within the space. The flow of the mixture around the inner tube causes a higher turbulence and better mixing.
  • the gaseous oxidizing agent preferably air
  • the lance system in the interior of the inner tube and, separately, in the space between inner and outer tube
  • the gaseous oxidizing agent preferably air
  • the reducing agent at exit from the outer tube of the lance system meets combustion gas, which is a Temperature in the range of 900 ° C to 1100 ° C, preferably from 950 ° C to 1050 ° C.
  • FIG. 1 shows a schematic longitudinal section through a furnace or boiler 1.
  • the supply for fuel 2 and combustion air 3 are shown schematically, which are brought together to carry out the combustion.
  • the resulting combustion gas 4 flows through the furnace and subsequently arranged in the combustion gas flow heating surfaces 10, 11, 12.
  • the firing is operated with air staging. This means that the combustion air 3 added to the burner is not sufficient for complete conversion of the fuel 2.
  • combustion air 5 is added, for example, below the convective heating surfaces 10, 11, 12 by means of wall nozzles.
  • FIG. 1 shows a schematic longitudinal section through a furnace or boiler 1.
  • the supply for fuel 2 and combustion air 3 are shown schematically, which are brought together to carry out the combustion.
  • the resulting combustion gas 4 flows through the furnace and subsequently arranged in the combustion gas flow heating surfaces 10, 11, 12.
  • the firing is operated with air staging. This means that the combustion air 3 added to the burner is not sufficient for complete conversion of the fuel 2.
  • combustion air 5 is added, for example, below the convective heating surfaces 10, 11, 12
  • nitrogen oxide reducing agent is mixed together with blowing agent 8 for fine distribution with part of the combustion air 7 required in the combustion process in the mixing chamber 15 and guided into the interior 23 of the inner tube 16 via one or more horizontally extending lance systems according to the invention.
  • the other part of the oxidizing agent 6 (combustion air) is also supplied via the lance system 9 to the combustion gas by being conducted in the outer section 21 into the outer tube 17 and finally into the intermediate space 22 between inner tube 16 and outer tube 17.
  • the lance system 9 rests on the heating surface 10 in the illustrated embodiment.
  • FIG. 1 illustrated embodiment of the lance system. 9 has an outer tube 17 whose diameter decreases toward the inner end.
  • FIG. 2 represents a top view of that in the FIG. 1 Within a boiler 1 are heating surfaces 10 on which or in the vicinity above a lance system 9 is arranged.
  • the lance system has an inner tube 16 and an outer tube 17. According to the invention, only a single inner tube 16 is contained in an outer tube 17.
  • reducing agent 13 is distributed in the mixing chamber 15 located outside of the boiler 1 (in the outer section 21 of the lance system). If it is a reducing agent dissolved in a liquid, it is so atomized. At the same time, a portion of the fluid 7 required in the process is introduced into the mixing chamber 15, which in an advantageous embodiment is burnout air 7.
  • the supply of the burn-out air can, for example, also take place tangentially into the mixing chamber 15 in order to improve the mixing.
  • the mixed fluid consisting of propellant 14, reducing agent 13 and burnout 7 leaves the mixing chamber 15 and enters the inner tube 16.
  • the mixture leaves in the flow direction gradually through the Openings 18, the inner tube 16 and enters the gap 22 between the inner tube 16 and the outer tube 17.
  • the openings 18 in the inner tube 16 are dimensioned so that over the length of the inner tube 16 uniform distribution in the gap 22 between inner tube 16 and outer tube 17th he follows.
  • the outer tube 17 a part in the process required fluid 6 is also supplied, in which the mixture emerging from the inner tube 16 is introduced and thus mixed in the intermediate space 22, before the outer tube 17 together through the openings 19 provided in the surrounding combustion gas stream. 4 leaves.
  • the openings 19 of the outer tube 17 are dimensioned so that over the length of the outer tube 17 as uniform as possible outflow into the surrounding combustion gas 4 takes place.
  • the openings 18 of the inner tube 16 can also be performed tangentially from the inner tube 16 in order to achieve a better mixing in the space 22 between the outer and inner tube.
  • the openings 18 may also be a plurality of bores which, due to their multiplicity, achieve good mixing with the medium 6 flowing into the outer tube 17.
  • complete evaporation is achieved by first passing the reducing agent mixed with hot oxidizing agent (preferably air) into an inner tube 16, via which first outlet openings 18 are subsequently transferred into the gap 22 between the inner tube 16 and the outer tube 17 is there in the space 22 again with hot oxidizing agent (preferably air) is mixed and then leaves the lance system 9 via the second outlet openings 19 in the outer tube 17.
  • hot oxidizing agent preferably air
  • the first outlet openings 18 of the inner tube 16 open into the intermediate space 22.
  • the second outlet openings 19 of the outer tube 17 are offset with respect to the first outlet openings 18 of the inner tube 16 are.
  • the first outlet openings 18 are shown schematically in the form of tubes or nozzles, whose axes are perpendicular to the longitudinal axis of the inner tube 16 and the lance system 9. The axis of each first outlet opening 18 is directed to the inner wall of the outer tube 17.
  • each first exit port 18 intersects the inner wall of the outer tube 17 at a closed wall portion of the outer tube 17.
  • the distance of the intersection of the axis of a given or arbitrary first exit port 18 of the inner tube 16 to the edge of the nearest second outlet opening 19 of the outer tube 17 is at least 1.5 times the radius of the respective first outlet opening 18th
  • FIG. 3 shows a preferred arrangement of a plurality of lance systems 9 on or in the vicinity of Bankdom Sea Sea 10.
  • the outlet openings 19 of the outer tube 17 are arranged opposite one another, wherein the outlet openings 19 come to lie in the space between the individual Schuphilrohren.
  • FIG. 4 shows another preferred arrangement of a plurality of lance systems 9 on or in the vicinity of Bankdom Zellen 10.
  • the outlet openings 19 of the outer tube 17 are arranged offset (meshing) opposite.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Treating Waste Gases (AREA)
EP16175167.2A 2016-06-20 2016-06-20 Système de lance, citerne comprenant un système de lance et procédé de réduction de nox Active EP3260776B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
RS20190734A RS58920B1 (sr) 2016-06-20 2016-06-20 Sistem brizgalica, kotao sa sistemom brizgalica i postupak za redukciju nox
PL16175167T PL3260776T3 (pl) 2016-06-20 2016-06-20 Układ lancowy, kocioł zawierający układ lancowy oraz sposób redukcji NOx
EP16175167.2A EP3260776B1 (fr) 2016-06-20 2016-06-20 Système de lance, citerne comprenant un système de lance et procédé de réduction de nox
PCT/EP2017/065077 WO2017220571A1 (fr) 2016-06-20 2017-06-20 Système de lance, chaudière contenant un système de lance et procédé de réduction des oxydes d'azote

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP16175167.2A EP3260776B1 (fr) 2016-06-20 2016-06-20 Système de lance, citerne comprenant un système de lance et procédé de réduction de nox

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EP3260776A1 true EP3260776A1 (fr) 2017-12-27
EP3260776B1 EP3260776B1 (fr) 2019-05-15

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PL (1) PL3260776T3 (fr)
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CN111111405A (zh) * 2020-02-12 2020-05-08 山西华仁通电力科技有限公司 用于塔式锅炉的氨气sncr脱硝系统

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EP0440604A1 (fr) * 1988-10-31 1991-08-14 Dale Gordon Jones Procede et dispositifs pour nettoyer des gaz.
US5281403A (en) 1991-09-27 1994-01-25 Noell, Inc. Method for converting urea to ammonia
US5342592A (en) 1989-07-04 1994-08-30 Fuel Tech Europe Ltd. Lance-type injection apparatus for introducing chemical agents into flue gases
EP0530255B1 (fr) 1990-05-21 1996-07-10 Nalco Fuel Tech GmbH Procede pour reduire au minimum des concentrations polluantes dans des gaz de combustion
WO1997041947A1 (fr) 1996-05-07 1997-11-13 Nebraska Public Power District Lance d'injection pour injecter uniformement du gaz ammoniac anhydre et de l'air dans une cavite de chaudiere
DE4434943C2 (de) 1994-09-30 1998-08-27 Krc Umwelttechnik Gmbh Verfahren zur Reduzierung des NO¶x¶-Gehaltes bei gleichzeitiger Minimierung des Reduktionsmittelschlupfes in Ab- bzw. Rauchgasen von Verbrennungs- und Produktionsprozessen
US20040201142A1 (en) 2003-04-14 2004-10-14 Robert Rumen Injection lance for uniformly injecting a steam/ammonia mixture into a fossil fuel combustion stream
DE102004026697A1 (de) 2003-06-05 2004-12-30 General Electric Co. Mehrere Zwischenkammern aufweisendes Oberluft- und N-Agensinjektionssystem und Verfahren zum Reduzieren von Stickoxiden in Rauchgas
EP1890081A2 (fr) * 2006-08-09 2008-02-20 MARTIN GmbH für Umwelt- und Energietechnik Buse destinée à l'introduction et au dosage d'une substance de traitement dans un flux de gaz d'échappement dans des processus de combustion
DE102008004008A1 (de) 2007-01-24 2008-07-31 General Electric Co. Verfahren und Einrichtung zur Reduktion von NOx-Emissionen aus gewerblichen Verbrennungsanlagen
US20080276842A1 (en) * 2007-05-10 2008-11-13 Alstom Technology Ltd. SYSTEM AND METHOD FOR DECREASING NOx EMISSIONS FROM A FLUIDIZED BED COMBUSTION SYSTEM
DE102010050334A1 (de) 2010-11-05 2012-05-10 Jörg Krüger Verfahren und Vorrichtung zur nicht-katalytischen Entstickung von Abgasen von Verbrennungsanlagen
DE102012110962A1 (de) 2012-11-14 2014-05-15 Babcock Borsig Steinmüller Gmbh Verfahren und Mehrstoffdüse zur Reduktion unerwünschter Substanzen in einem Rauchgas
EP2962743A1 (fr) 2014-07-04 2016-01-06 Alstom Technology Ltd Chaudière et procédé de commande d'émissions de NOx provenant d'une chaudière comprenant SNCR

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EP0440604A1 (fr) * 1988-10-31 1991-08-14 Dale Gordon Jones Procede et dispositifs pour nettoyer des gaz.
US5342592A (en) 1989-07-04 1994-08-30 Fuel Tech Europe Ltd. Lance-type injection apparatus for introducing chemical agents into flue gases
EP0530255B1 (fr) 1990-05-21 1996-07-10 Nalco Fuel Tech GmbH Procede pour reduire au minimum des concentrations polluantes dans des gaz de combustion
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US5281403A (en) 1991-09-27 1994-01-25 Noell, Inc. Method for converting urea to ammonia
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DE4434943C2 (de) 1994-09-30 1998-08-27 Krc Umwelttechnik Gmbh Verfahren zur Reduzierung des NO¶x¶-Gehaltes bei gleichzeitiger Minimierung des Reduktionsmittelschlupfes in Ab- bzw. Rauchgasen von Verbrennungs- und Produktionsprozessen
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WO1997041947A1 (fr) 1996-05-07 1997-11-13 Nebraska Public Power District Lance d'injection pour injecter uniformement du gaz ammoniac anhydre et de l'air dans une cavite de chaudiere
US20040201142A1 (en) 2003-04-14 2004-10-14 Robert Rumen Injection lance for uniformly injecting a steam/ammonia mixture into a fossil fuel combustion stream
DE102004026697A1 (de) 2003-06-05 2004-12-30 General Electric Co. Mehrere Zwischenkammern aufweisendes Oberluft- und N-Agensinjektionssystem und Verfahren zum Reduzieren von Stickoxiden in Rauchgas
EP1890081A2 (fr) * 2006-08-09 2008-02-20 MARTIN GmbH für Umwelt- und Energietechnik Buse destinée à l'introduction et au dosage d'une substance de traitement dans un flux de gaz d'échappement dans des processus de combustion
DE102008004008A1 (de) 2007-01-24 2008-07-31 General Electric Co. Verfahren und Einrichtung zur Reduktion von NOx-Emissionen aus gewerblichen Verbrennungsanlagen
US20080276842A1 (en) * 2007-05-10 2008-11-13 Alstom Technology Ltd. SYSTEM AND METHOD FOR DECREASING NOx EMISSIONS FROM A FLUIDIZED BED COMBUSTION SYSTEM
DE102010050334A1 (de) 2010-11-05 2012-05-10 Jörg Krüger Verfahren und Vorrichtung zur nicht-katalytischen Entstickung von Abgasen von Verbrennungsanlagen
DE102012110962A1 (de) 2012-11-14 2014-05-15 Babcock Borsig Steinmüller Gmbh Verfahren und Mehrstoffdüse zur Reduktion unerwünschter Substanzen in einem Rauchgas
EP2962743A1 (fr) 2014-07-04 2016-01-06 Alstom Technology Ltd Chaudière et procédé de commande d'émissions de NOx provenant d'une chaudière comprenant SNCR

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PL3260776T3 (pl) 2019-10-31
EP3260776B1 (fr) 2019-05-15
RS58920B1 (sr) 2019-08-30
WO2017220571A1 (fr) 2017-12-28

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