EP3177872B1 - Brenner mit einstellbarer luft- oder gasinjektion - Google Patents

Brenner mit einstellbarer luft- oder gasinjektion Download PDF

Info

Publication number
EP3177872B1
EP3177872B1 EP15756185.3A EP15756185A EP3177872B1 EP 3177872 B1 EP3177872 B1 EP 3177872B1 EP 15756185 A EP15756185 A EP 15756185A EP 3177872 B1 EP3177872 B1 EP 3177872B1
Authority
EP
European Patent Office
Prior art keywords
primary air
burner
radial
air
gas
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
EP15756185.3A
Other languages
English (en)
French (fr)
Other versions
EP3177872A1 (de
Inventor
Louis Ricci
Gaël Le Piver
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fives Pillard SA
Original Assignee
Fives Pillard SA
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
Application filed by Fives Pillard SA filed Critical Fives Pillard SA
Priority to DE15756185.3T priority Critical patent/DE15756185T1/de
Publication of EP3177872A1 publication Critical patent/EP3177872A1/de
Application granted granted Critical
Publication of EP3177872B1 publication Critical patent/EP3177872B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
    • F23C7/006—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes adjustable
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/60—Devices for simultaneous control of gas and combustion air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/005—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or pulverulent fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/21—Burners specially adapted for a particular use

Definitions

  • the present invention relates to the field of burners of any field and of any fuel, and in particular but not limited to burners for rotary kilns (or rotary kilns), such as cement kilns or lime kilns.
  • secondary air arrives at very high temperature (between 600 to 1200 ° C) and low speed (between 4 and 10m / s), after being used as cooling air for hot material falling from the oven.
  • this hot secondary air represents between 80 and 95% of the combustion air in the kiln.
  • Complementary air is the air injected directly into the burner at a lower temperature (temperature close to ambient temperature in most cases) but at high speed.
  • Rotary oven burners are generally characterized by their primary air pulse which is the force generated by the expansion of the air primary in the furnace (primary air mass flow x primary air expansion speed) divided by the calorific power of the burner.
  • the primary air at high pressure and low temperature impacts the energy balance of the process by the electrical consumption necessary for its pressurization as well as by the introduction of cold air into the process.
  • the primary air injections at the end of the rotary oven burners generally consist of at least two primary air outlets, at least one of which is axial and the other radial (or rotational), as in the patent FR 2 780 489 and FR 2 901 852 .
  • the adjustment of the proportion between the flow and / or the axial and radial air pressure allows the adjustment of the overall radial component of the primary air and varies the flame shape.
  • These burners are therefore generally equipped with devices for adjusting the axial and / or radial pressure which reduces the pressure and consequently the expansion speed of these airs at the end of the burner. They thereby reduce the burner pulse which is proportional to the expansion speed.
  • the injection of pulverized fuel (coal, petcoke, etc., which are the main fuels in the rotary kiln) is sandwiched between the primary external axial air and the internal radial air. Therefore, at primary air pulse, this radial outlet does not fully participate in the absorption of secondary air in the flame. It will therefore take more primary air impulse to achieve an equivalent result.
  • the arrangement of the radial air inside the pulverized fuel circuit increases the risk of fuel being ejected from the flame, which can create unfavorable operating conditions (deterioration of the cooking quality of the product , operational difficulties, reduction in the life of the brickwork lining the furnace, etc.) and increases NOx emissions, because the fuel concentration is too low at the center of the flame, which prevents the phenomenon of NOx-reducing re-combustion. .
  • Controlling the flame diameter is more difficult in burners with a single primary air outlet with adjustable radial component. Indeed, if in burners with two or more outlets, the axial outlet is generally located at the periphery of the burner to control and stabilize the divergence of the flow and allow a more efficient and finer adjustment of the flame diameter, this advantage does not exist on single outlet burners, making it more difficult to adjust the diameter. Too large a flame diameter which can have serious consequences on the conditions of operation of the process (affecting the nature of the material to be cooked and / or the operating conditions) and or the lifetime of the refractory linings of the oven.
  • part of the combustion air can also be rotated to ensure turbulence and a better mixture of air and fuel.
  • the present invention also applies to these burners, whether the air is called primary air, combustion air or radial air or rotational air, or staged air.
  • this portion of combustion air will be referred to as primary air.
  • the object of the present invention is to provide a burner which makes it possible to gradually and linearly adjust the radial component of the primary air or of the gas and to avoid adjustment by reducing the pressure (and therefore the expansion speed). ) of a radial or axial component and therefore of retaining the maximum pulse of the primary air or of the gas.
  • the burner according to the invention comprises a primary air or gas pipe of axis X delimited by an outer wall and a concentric inner wall and pipes for injecting primary air or radial gas, it is characterized in that that the primary air or gas duct comprises a ring movable in rotation and having axial protrusions constituting distributors which cooperate with the primary air or radial gas injection ducts disposed at the end of the burner on the part outer peripheral of the inner wall and form two channels of different angles in each primary air or gas injection duct radial.
  • the rotation of the crown will allow the section of the primary air or radial gas ducts to be divided into two series of interposed channels.
  • the crown is also movable in translation.
  • the translation of the crown will make it possible to modify the passage section of the primary air or radial gas injection conduits.
  • the passage section is the sum of the sections of the conduits constituting the primary air or gas conduit, and it is smaller than the outlet section, the passage section is therefore adjustable.
  • a first series of channels has a small radial primary air injection angle (generally between -10 and + 30 °) while the other series has a greater radial primary air injection angle than the previous series (generally between +10 and + 60 °).
  • the injection angle of the radial primary air or of the resulting gas is the combination of the air jets from the two series of interleaved channels, one at a small angle and the other at a large angle.
  • the rotation adjustment of the crown around the X axis makes it possible to vary the section distribution, and therefore the flow of primary air or gas between these two series of intercalated channels and therefore to adjust the injection angle. radial air.
  • This cross-sectional distribution between the two series of interleaved channels is carried out at constant total cross-section, which greatly simplifies the adjustment of the burner.
  • the adjustment is located just at the end of the burner, at the level of the exit of the primary air or the gas in the furnace, by this position of the adjustment at the end one maximizes the exit speed of the air or gas and therefore the pulse.
  • the two channels are formed by a flared shape complementary to the distributor and the primary radial air ducts and the sum of the sections of said channels is constant in a plane perpendicular to X, whatever the angular position of the crown (3).
  • the distributors and the primary air or radial gas injection conduits are of complementary flared shape which form channels of constant section.
  • the adjustment is made by modifying the outlet angle of the radial component with a constant outlet section which greatly simplifies the adjustment of the burner.
  • the distributors and the primary air or radial gas injection conduits have walls with parallel edges.
  • the distributors and the primary air or radial gas injection conduits have curvilinear edges. This form makes it possible to limit the pressure drops.
  • the movable crown has at least one inclined groove and it is actuated in rotation by a movable ring in translation to which it is connected by a nut sliding in said groove.
  • the translation of the ring thus allows the rotation of the crown.
  • the movable ring is actuated by a jack.
  • the cylinder can be hydraulic, or mechanical, or pneumatic.
  • the radial primary air ducts and the distributors are chamfered upstream.
  • the chamfer is in a tangent plane or in a vertical plane relative to the air flow, and it allows a progressive entry and acceleration of the air in the channels and therefore a limited pressure drop.
  • the burner also includes axial primary air ducts.
  • the primary air or radial gas injection pipe is sandwiched between the fuel pipes and the axial primary air pipe.
  • the axial primary air and radial primary air injection conduits are supplied by the same supply.
  • This is very advantageous, especially in the case of a burner with two primary air outlets (one axial and the other radial), located outside the fuel circuits as this makes it possible to lighten the burner and limit the pressure losses in the supply circuits, to have a burner whose settings are simple.
  • We can thus adjust the rotation of the crown to increase the radial component and act on the flame diameter and adjust the air pressure upstream of the burner to adjust the pulse.
  • This makes it possible to limit the maximum rotation by a constant proportion between the external axial circuit and the internal circuit with adjustable radial component and to limit the maximum flame diameter and thus protect the refractories of the ovens from false operations and / or incorrect adjustment.
  • the number of primary air or radial gas injection ducts is a multiple of the number of axial primary air duct or of a group of axial primary air ducts.
  • the primary air or radial gas injection conduits and the axial primary air conduits are arranged on the same radii.
  • the number of outlet ports in the radial air circuit, or with a tangential component, can be matched with the number of holes (or group of holes) in the axial air circuit, so that the primary air pulse from the two circuits best contributes to the absorption of secondary air.
  • the angular location of the axial and radial air orifices is important and the arrangement with the axial and radial orifices (or group of orifices) on the same radius is advantageous, that is to say that the radial air or gas injection ducts are located radially directly below the axial air injection ducts.
  • the inclination and the length of the groove is proportional to the rotation of the crown.
  • the groove may have a length of 50 to 300mm and a slight inclination of 1 to 15 ° relative to the X axis. The combination of a long groove and a small angle makes it possible to obtain high adjustment precision.
  • the duct has an outlet section, this outlet section varies according to the movement of a wall relative to the other, the inner radial face of the distributors and the outer radial face of the notches make an angle ⁇ with the axis X and the inner radial face of the outer ring makes an angle ⁇ with the axis X.
  • the outlet section can be adjusted to maintain a pressure and therefore a maximum injection speed of the primary air or gas at the end of the burner.
  • This modification of section is obtained by relative displacement along the X axis of the inner and outer tubes of the circuit and by an inclined shape along the X axis of the distributors mounted on the movable ring and the notches of primary radial air or of gases arranged on the outer peripheral part of the inner tube of the circuit.
  • the primary air or radial gas injection pipe is disposed outside of fuel circuits (pulverized solid, liquid or other gas). This limits any risk of projection of liquid or solid fuel at the periphery of the flame when the radial component of the air or gas is increased.
  • this arrangement makes it possible to reduce NOx by a staged combustion effect, by concentrating the fuel in the center of the flame.
  • the primary air or radial gas injection pipe is sandwiched between an axial air pipe and the center of the burner comprising the combustible pipes (pulverized solid , liquid or gaseous) and possibly the flame stabilizer.
  • the distributors and the primary air or radial gas injection conduits are of complementary flared shape forming two channels and the sum of the sections of which is variable in a plane perpendicular to X, whatever the angular position of the crown. .
  • the outlet section must be adjustable to maintain a pressure and therefore a maximum injection speed of the primary air or gas at the end of the burner. This section modification is obtained by a relative displacement along the axis X of the movable crown and radial primary air or gas notches arranged on the outer peripheral part of the inner tube of the circuit.
  • the burner 1 comprises at least one primary air or gas duct 22 comprised between an outer wall 52 and an inner wall 23 of axis X and constituting concentric tubes of cylindrical shape, surrounding the center of the burner 10 in which can be several other primary air or fuel ducts 100, 101 or a stabilizer 8 are installed.
  • the end of this duct on the furnace side is closed by an inner end ring 2 and an outer end ring 5, which can be as follows the embodiments, two separate parts to facilitate machining or the same part.
  • the primary air or gas duct has a crown 3, itself surrounded by a ring 4.
  • the downstream end of the duct is encircled by the ring 5.
  • the inner ring 2 connected to the inner tube of the wall 23 has on its periphery notches 20 which have two faces 200 and 201 flared relative to each other (or V-shaped), which are closed on their peripheral part by the ring 5 and thus constitutes conduits 21 for injecting radial primary air or gas.
  • the outer ring 5 comprises conduits 50 for primary air with an axial component.
  • Crown 3 (cf. figures 1 , 2 and 7 ) has protrusions 30 of flared or V shape which are arranged in the notches 20 and constitute air distributors 30.
  • Each protrusion 30 has two faces 300 and 301 which join downstream and which are respectively parallel to the faces 200 and 201 of the notch 20.
  • the V shape therefore has its point arranged downstream.
  • the crown 3 rotates around the axis X on the main conduit between two extreme positions, in which the distributor 30 is in abutment on the face 200 of the notch 20 or on the face 201 of said notch 20.
  • the crown 3 has at least one groove 31 disposed in an inclined manner relative to the axis X.
  • the ring 4 slides from upstream to downstream on the wall 23 along the axis X.
  • the ring 4 comprises a stud, nut or key 42 which slides in the groove 31.
  • the ring 4 is fixed to the at least one control arm or bar 43 connected to a piston (not shown) in order to slide the ring 4 from upstream to downstream and vice versa.
  • Each air distributor 30 makes it possible to separate the flow of primary air or gas which arrives in the conduit 21 for injecting radial primary air or gas and to give it a tangential angular component by dividing it into two channels 210 and 211 with different angles. These channels 210 and 211 generate two jets which recombine into a single jet at the outlet and whose mean angle is practically proportional to the outlet angle of each V weighted by the flow rate of each jet.
  • the sectional distribution between the two channels 210 and 211 is varied, the overall section of the channels 210 and 211 being constant over the entire setting and therefore the flow rate in each of the branches of the V to obtain a variation of the exit angle of the air flow 6 without decreasing the ejection speed and keeping the flow constant.
  • the channels 210 and 211 are curved, to reduce the pressure drop in the channels by the progressive increase in speed according to the tangential component and allow greater aerodynamic stability of the jet.
  • the curved shape gives the underside of the jet a slightly lower expansion speed than that at the underside of the jet. It makes it less turbulent the mixture of the two jets at different angles and therefore more stable the resulting flow and more optimal the average speed of the jet.
  • the distributor 30 is placed substantially in the middle, the amount of air which passes through the two channels is substantially identical.
  • the distributor 30 is pressed against the wall 200 and the majority of the air passes through the more inclined channel 210, the air flow 6 is therefore more strongly inclined.
  • the distributor 30 is pressed against the wall 201 and the majority of the air passes through the channel 211 less inclined, the air flow 6 is therefore very slightly inclined.
  • chamfers 303, 203 are provided at the inlet of the air distributor 30 as well as at the inlet of the channels 210 and 211 in a tangent plane or in a vertical plane.
  • the burner comprises an outer protective concrete 7, the outer ring 5 with axial ducts 50, the inner ring 2 with the ducts 21 for injecting radial primary air or gas, and the center of the burner 10 delimited outside by the wall 23 comprising a pulverulent and / or gaseous fuel conduit 100, and other combustible conduits 101 and a central stabilizer 8.
  • This type of burner can be used both if it has a primary air or single gas outlet with only the primary air ducts 21 or multiple with the primary air or gas ducts 21 and 50.
  • conduits 50 and 21 can be supplied with primary air by a single primary air duct 22 or by separate primary air circuits, generally concentric or almost concentric with respect to the 'X axis.
  • FIGS 9 to 11 show different radial arrangements of the primary air or gas conduits according to the invention and of the annular fuel duct (s) (pulverulent, gaseous fuels).
  • the figure 9 shows an arrangement with, from the center of the burner, at the stabilizing center 8, fuel conduits 101 in the stabilizer, a pulverulent fuel line 100, primary air or radial gas injection lines 21, one of the axial lines50.
  • the figure 10 shows an arrangement with, from the center of the burner, at the stabilizing center 8, a fuel duct 101 in the stabilizer, primary air or radial gas injection ducts 21, a pulverulent fuel duct 100, axial ducts 50.
  • the figure 11 shows an arrangement with, from the center of the burner, at the stabilizing center 8, a fuel duct 101 in the stabilizer, a pulverulent fuel duct 100, one of the primary air or radial gas injection ducts 21 without axial duct .
  • the primary radial air or gas duct 22, the minimum section of the radial component in the plane 216 can be adjusted at the end of the burner to maintain a pressure and therefore a maximum injection speed of the primary air or gas at the end of the burner.
  • This section modification is obtained by the displacement along the axis X of one of the walls 23 or 52 relative to the other, of the inclination of angle ⁇ of the inner radial face 315 of the distributors 30 and the outer radial face 215 of the primary radial air or gas notches 20 relative to the axis X, as well as a divergent angle ⁇ on the inner radial face 51 of the outer ring 5.
  • the inner wall 23 is movable and the outer wall 52 is fixed.
  • the crown 3 also translates along the axis X on the main conduit between two extreme positions, in which the face 310 of the distributor 30 is in abutment on the face 220 to obtain a minimum passage section.
  • the distributor 30 can be moved back for an increased passage section.
  • the translation of the crown 3 or the rotation of the latter can be done by two relative movements independent.
  • the adjustment of the section can also be carried out by a translation and / or a rotation of the crown.
  • the section of the radial component in the radial primary air or gas duct 22, can be adjusted at the end of the burner 1 to maintain a pressure and therefore a maximum injection speed of the primary air or gas at the end of the burner.
  • This section modification is obtained by the translation along the axis X of the crown 30 linked to the control bar 43.
  • figures 14 , 16b and 17 the section of the channels 210, 211 are maximum, while when they are pushed, figure 15 , 16a and 18 , the section of the channels 210, 211 are minimum.
  • the optimal arrangement for the suction of secondary air into the flame is the installation of this primary air duct outside the fuel ducts and in particular the pulverulent fuel duct. This arrangement limits the projection of solid fuels outside the flame and reduces the formation of nitrogen oxides.
  • this device located just outside the combustible duct as illustrated figure 2 , in particular the pulverulent fuel conduit (coal, pet coke ...), and generally between the pulverulent fuel conduit and the axial conduit, allows it to be rotated to activate its combustion but also to benefit from an arrangement of the orifices outlet of the primary air duct with tangential component close to the secondary air, in order to benefit from the impulse of this duct for the absorption of the secondary air in the flame.
  • the pulverulent fuel conduit coal, pet coke
  • the number of ducts 21 is a multiple of the number of axial ducts 50 or group of axial ducts 50, to improve the absorption of secondary air.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Gas Burners (AREA)

Claims (14)

  1. Brenner (1), umfassend einen Primärluft- oder Gaskanal (22) mit X-Achse, der durch eine Außenwand (52) und eine konzentrische Innenwand (23) begrenzt ist, und Kanäle (21) für radiale Gas- oder Primärluftinjektion, dadurch gekennzeichnet, dass der Luft- oder Gaskanal (22) einen Ring (3) umfasst, der drehbeweglich ist und axiale Vorsprünge aufweist, die Verteiler (30) darstellen, die mit den radialen Primärluftkanälen (21), die auf dem äußeren Umfangsteil der Innenwand angeordnet sind, zusammenwirken und zwei Durchlässe (210, 211) mit unterschiedlichen Winkeln in jedem Kanal (21) für radiale Gas- oder Primärluftinjektion bilden.
  2. Brenner (1) nach dem vorhergehenden Anspruch, dadurch gekennzeichnet, dass der Ring (3) translatorisch beweglich ist.
  3. Brenner (1) nach Anspruch 1, dadurch gekennzeichnet, dass die zwei Durchlässe (210, 211) durch ergänzende erweiterte Formen des Verteilers (30) und der radialen Gas- oder Primärluftkanäle (21) gebildet sind und dass die Summe der Abschnitte der Durchlässe der Kanäle in einer senkrecht zu X verlaufenden Ebene konstant ist, ungeachtet der Winkelposition des Ringes (3).
  4. Brenner (1) nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Verteiler (30) und die radialen Gas- oder Primärluftkanäle (21) Wände (200, 300; 201, 301) mit parallelen Kanten aufweisen.
  5. Brenner (1) nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Verteiler (30) und die radialen Gas- oder Primärluftkanäle (21) krummlinige Kanten aufweisen.
  6. Brenner (1) nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass die radialen Primärluftkanäle (21) und die Verteiler (30) am stromaufwärtigen Ende abgeschrägt sind.
  7. Brenner (1) nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass er axiale Primärluftkanäle (50) umfasst.
  8. Brenner (1) nach dem vorhergehenden Anspruch, dadurch gekennzeichnet, dass der radiale Primärluftkanal (21) sandwichartig zwischen den Kraftstoffkanälen und dem axialen Primärluftkanal angeordnet ist.
  9. Brenner (1) nach dem vorhergehenden Anspruch, dadurch gekennzeichnet, dass der axiale Primärluft- und radiale Primärluftkanal (50, 21) aus derselben Zuführung (22) gespeist werden.
  10. Brenner (1) nach Anspruch 7, dadurch gekennzeichnet, dass die Anzahl von Gas- oder von radialen Primärluftkanälen (21) ein Vielfaches der Anzahl axialer Kanäle oder einer Gruppe von axialen Kanälen (50) ist.
  11. Brenner (1) nach dem vorhergehenden Anspruch, dadurch gekennzeichnet, dass der Gas- oder der radiale Primärluft- und axiale Luftkanal (50, 21) auf demselben Radius angeordnet sind.
  12. Brenner (1) nach einem der Ansprüche 5 und 6, dadurch gekennzeichnet, dass der Ring (3) mindestens einen Schlitz (31) aufweist, der in einer Neigung zur X-Achse angeordnet ist, und dass die Neigung und die Länge des Schlitzes (31) proportional zur Drehung des Ringes (3) sind.
  13. Brenner (1) nach Anspruch 3, dadurch gekennzeichnet, dass der Kanal (21) einen Auslassabschnitt (216) aufweist, dass dieser Auslassabschnitt (216) in Abhängigkeit von der Bewegung einer Wand (52, 23) gegenüber der anderen (23, 52) variiert, dass die radiale Innenfläche (315) der Verteiler (30) und die radiale Außenfläche (215) der Einschnitte (20) einen Winkel α mit der X-Achse bilden und dass die radiale Innenfläche (51) des äußeren Rings (5) einen Winkel ß mit der X-Achse bildet.
  14. Brenner (1) nach Anspruch 2, dadurch gekennzeichnet, dass die Verteiler (30) und die radialen Primärluftkanäle (21) eine ergänzende erweiternde Form aufweisen, wobei sie zwei Durchlässe (210) und (211) bilden, deren Summe der Abschnitte in einer senkrecht zu X verlaufenden Ebene variabel ist, ungeachtet der Winkelposition des Rings (3).
EP15756185.3A 2014-08-06 2015-06-25 Brenner mit einstellbarer luft- oder gasinjektion Active EP3177872B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE15756185.3T DE15756185T1 (de) 2014-08-06 2015-06-25 Brenner mit einstellbarer luft- oder gasinjektion

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1401811A FR3024765B1 (fr) 2014-08-06 2014-08-06 Bruleur a injection d'air ou de gaz ajustable
PCT/FR2015/051726 WO2016020587A1 (fr) 2014-08-06 2015-06-25 Brûleur a injection d'air ou de gaz ajustable

Publications (2)

Publication Number Publication Date
EP3177872A1 EP3177872A1 (de) 2017-06-14
EP3177872B1 true EP3177872B1 (de) 2020-05-27

Family

ID=52273197

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15756185.3A Active EP3177872B1 (de) 2014-08-06 2015-06-25 Brenner mit einstellbarer luft- oder gasinjektion

Country Status (10)

Country Link
US (1) US10234137B2 (de)
EP (1) EP3177872B1 (de)
CN (1) CN106796025B (de)
BR (1) BR112017002300B1 (de)
DE (1) DE15756185T1 (de)
DK (1) DK3177872T3 (de)
ES (1) ES2648462T3 (de)
FR (1) FR3024765B1 (de)
RU (1) RU2678466C2 (de)
WO (1) WO2016020587A1 (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190113225A1 (en) * 2016-05-11 2019-04-18 Dynamis Engenharia E Comércio Ltda. Method to Enhance Burner Efficiency and Burner
EP3455554A4 (de) * 2016-05-11 2019-11-20 Dynamis Engenharia E Comércio Ltda. Verfahren zur verbesserung der brennereffizienz und brenner
CN108895446B (zh) * 2018-07-27 2024-04-16 岳阳恒盛石化科技有限公司 一种奇数循环引火高效节能超低nox气体燃烧器

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3527262A (en) * 1968-04-16 1970-09-08 Jerry C Fuchs Rotating piston chamber engine
SU1145211A1 (ru) * 1983-06-03 1985-03-15 Запорожский индустриальный институт Горелка
FR2572463B1 (fr) * 1984-10-30 1989-01-20 Snecma Systeme d'injection a geometrie variable.
DE3520781A1 (de) * 1985-06-10 1986-12-11 Stubinen Utveckling AB, Stockholm Verfahren und vorrichtung zum verbrennen fluessiger und/oder fester brennstoffe in pulverisierter form
SU1377514A1 (ru) * 1986-09-22 1988-02-28 Харьковский Институт Инженеров Железнодорожного Транспорта Им.С.М.Кирова Газова горелка
DE4110507C2 (de) * 1991-03-30 1994-04-07 Mtu Muenchen Gmbh Brenner für Gasturbinentriebwerke mit mindestens einer für die Zufuhr von Verbrennungsluft lastabhängig regulierbaren Dralleinrichtung
JP2666117B2 (ja) * 1994-06-10 1997-10-22 財団法人石油産業活性化センター 予蒸発予混合燃焼器
FR2780489B1 (fr) * 1998-06-24 2000-09-08 Pillard Chauffage Perfectionnement aux bruleurs comportant au moins trois conduits d'alimentation en air, dont deux axial et en rotation, concentriques avec au moins une alimentation-en combustible, et un stabilisateur central
US6315551B1 (en) * 2000-05-08 2001-11-13 Entreprise Generale De Chauffage Industriel Pillard Burners having at least three air feed ducts, including an axial air duct and a rotary air duct concentric with at least one fuel feed, and a central stabilizer
DE102005053819A1 (de) * 2005-11-11 2007-05-16 Khd Humboldt Wedag Gmbh Drehofenbrenner
FR2901852B1 (fr) * 2006-05-30 2010-10-22 Egci Pillard Conduite annulaire a double flux et bruleur comportant une telle conduite
FR2919043A1 (fr) * 2007-07-20 2009-01-23 Pillard Chauffage Bruleur comportant une conduite annulaire d'alimentation en air
FR2930626B1 (fr) * 2008-04-28 2010-05-21 Fives Pillard Bruleur a points peripheriques d'injection d'air a flux axial

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
EP3177872A1 (de) 2017-06-14
RU2017104450A3 (de) 2018-11-13
ES2648462T3 (es) 2021-04-26
WO2016020587A1 (fr) 2016-02-11
CN106796025A (zh) 2017-05-31
CN106796025B (zh) 2019-10-29
FR3024765A1 (fr) 2016-02-12
RU2678466C2 (ru) 2019-01-29
DK3177872T1 (da) 2017-10-16
RU2017104450A (ru) 2018-09-06
US20170219206A1 (en) 2017-08-03
DE15756185T1 (de) 2018-02-22
BR112017002300B1 (pt) 2022-03-03
FR3024765B1 (fr) 2016-07-29
BR112017002300A2 (pt) 2018-01-16
ES2648462T1 (es) 2018-01-03
US10234137B2 (en) 2019-03-19
DK3177872T3 (da) 2020-08-31

Similar Documents

Publication Publication Date Title
CA2443407C (fr) Procede de combustion comportant des injections separees de combustible et d'oxydant et ensemble bruleur pour la mise en oeuvre de ce procede
US8015821B2 (en) Apparatus and method for a gas turbine entrainment system
EP3177872B1 (de) Brenner mit einstellbarer luft- oder gasinjektion
CA2299530C (fr) Perfectionnements apportes aux bruleurs a flamme plate
CN102713434A (zh) 用于玻璃熔化系统的非对中的氧-燃料燃烧器
CN108884763A (zh) 燃烧器以及燃气轮机
CN108458366A (zh) 一种可调节燃烧区空气流量的衬套组件
CN102721059A (zh) 低热值燃气燃烧器及燃烧技术
EP3105506B1 (de) Brennermodul im strom
RU131455U1 (ru) Горелочное устройство
EP3671038B1 (de) Anordnung und verfahren für die injektion von gasförmigem brennmittel
EP2212620A2 (de) Verbrennungsverfahren und -system
EP2283277B1 (de) Brenner
CN113606577A (zh) 叶片可调型旋流燃烧器及烟气脱硝系统
RU2642997C2 (ru) Газовая горелка с низким содержанием оксидов азота и способ сжигания топливного газа
WO2013046708A1 (ja) 管状火炎バーナー
EP1045203B1 (de) Mehrstoffbrenner
WO2024141509A1 (fr) Bruleur a precombustion
FR3091331A1 (fr) Brûleur a flamme ajustable
WO2023057722A1 (fr) Dispositif d'injection de dihydrogène et d'air
EP0162761B1 (de) Brenner mit Schaufeln und ausgeglichener Zweitluftzufuhr
FR3127988A1 (fr) Dispositif d’injection de dihydrogène et d’air
BE494848A (de)
FR2564181A1 (fr) Bruleur pour foyer a grande souplesse de fonctionnement

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20170131

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
REG Reference to a national code

Ref country code: DE

Ref legal event code: R210

Ref document number: 602015053372

Country of ref document: DE

Ref country code: DE

Ref legal event code: R210

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20190821

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

INTC Intention to grant announced (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20200206

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1274933

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200615

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602015053372

Country of ref document: DE

REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

Effective date: 20200827

REG Reference to a national code

Ref country code: FI

Ref legal event code: FGE

REG Reference to a national code

Ref country code: SE

Ref legal event code: TRGR

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: FIVES PILLARD

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200928

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200927

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200828

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200827

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20200527

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200827

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602015053372

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200625

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20200630

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2648462

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20210426

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200727

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200630

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200630

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200625

26N No opposition filed

Effective date: 20210302

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200630

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20200527

REG Reference to a national code

Ref country code: AT

Ref legal event code: UEP

Ref document number: 1274933

Country of ref document: AT

Kind code of ref document: T

Effective date: 20200527

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20230523

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20230523

Year of fee payment: 9

Ref country code: ES

Payment date: 20230703

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20240521

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DK

Payment date: 20240521

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: AT

Payment date: 20240523

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20240522

Year of fee payment: 10

Ref country code: FI

Payment date: 20240521

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: TR

Payment date: 20240527

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20240701

Year of fee payment: 10