EP2679899B1 - Combustion device - Google Patents

Combustion device Download PDF

Info

Publication number
EP2679899B1
EP2679899B1 EP11859242.7A EP11859242A EP2679899B1 EP 2679899 B1 EP2679899 B1 EP 2679899B1 EP 11859242 A EP11859242 A EP 11859242A EP 2679899 B1 EP2679899 B1 EP 2679899B1
Authority
EP
European Patent Office
Prior art keywords
burner
furnace
combustion
combustion gas
wind box
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
EP11859242.7A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP2679899A1 (en
EP2679899A4 (en
Inventor
Yusuke Ochi
Kouji Kuramashi
Kenji Kiyama
Hirofumi Okazaki
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.)
Mitsubishi Power Ltd
Original Assignee
Mitsubishi Power Ltd
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 Mitsubishi Power Ltd filed Critical Mitsubishi Power Ltd
Priority to PL11859242T priority Critical patent/PL2679899T3/pl
Publication of EP2679899A1 publication Critical patent/EP2679899A1/en
Publication of EP2679899A4 publication Critical patent/EP2679899A4/en
Application granted granted Critical
Publication of EP2679899B1 publication Critical patent/EP2679899B1/en
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
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D1/00—Burners for combustion of pulverulent fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D1/00—Burners for combustion of pulverulent fuel
    • F23D1/005—Burners for combustion of pulverulent fuel burning a mixture of pulverulent fuel delivered as a slurry, i.e. comprising a carrying liquid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L1/00—Passages or apertures for delivering primary air for combustion 
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L3/00—Arrangements of valves or dampers before the fire
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L9/00—Passages or apertures for delivering secondary air for completing combustion of fuel 
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M9/00—Baffles or deflectors for air or combustion products; Flame shields
    • F23M9/02—Baffles or deflectors for air or combustion products; Flame shields in air inlets
    • 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 
    • F23C2201/00—Staged combustion
    • F23C2201/10—Furnace staging
    • F23C2201/101—Furnace staging in vertical direction, e.g. alternating lean and rich zones

Definitions

  • the present invention relates to a combustion device such as a pulverized coal burning boiler having a pulverized coal burner.
  • a combustion method using a pulverized coal burner of a pulverized coal burning boiler there is adopted a two-stage combustion method that combusts a fuel in an air insufficient state and then complete burning air is supplied from an after air port in order to reduce an emission rate of a nitride oxide (which will be referred to as NOx hereinafter) in a combustion exhaust gas.
  • NOx nitride oxide
  • the furnace installing position of the after-air port may be the same as that in the conventional example, this position is provided on a lower (upstream) side in the furnace as compared with the conventional examples even if a combustion temperature of the burner flames becomes high, and hence an exhaust gas temperature at the outlet of the furnace can be the same as that in the conventional examples.
  • Japanese Unexamined Patent Application Publication No. 2008-121924 discloses a burner having a movable nozzle.
  • the nozzle is movable in a portion that faces a furnace and has high radiant heat, consideration must be given to damage due to falling of clinkers adhering to the inside of the furnace or securement of movability.
  • Japanese Unexamined Patent Application Publication No. 2002-147713 Japanese Unexamined Patent Application Publication No. S54 3924 A , EP 2 273 193 A1 or Japanese Unexamined Utility Model Application Publication No. S61 101226 U 27 disclose a burner that changes a direction of flames (a combustion region) by deviating an air flow rate in a circumferential direction of a burner.
  • a first aspect of the present invention provides a combustion device comprising a plurality of burners 19 arranged on a furnace wall 10 of a furnace 18, each burner 19 comprising: a cylindrical fuel nozzle 3 that injects a mixture of a fuel and a carrier gas therefor into the furnace 18; one or more cylindrical combustion gas nozzles 8, 11 that are provided on the outer circumference of the fuel nozzle 3 and inject a combustion gas into the furnace 18; and a wind box 12 that supplies the combustion gas to the combustion gas nozzles 8, 11, wherein the wind box 12 has a combustion gas inflow opening portion 12a, 12b into which the combustion gas flows from one direction, vertical to the axial direction of the burner 19 and is partitioned to form a plurality of parallel flow paths through which the combustion gas flows in from the combustion gas inflow opening portion 12a, 12b, wherein one duct 16 through which the combustion gas is collectively supplied to the plurality of wind boxes 12 from the outside of the furnace 18, which is installed on the outer side of the furnace wall 10 on which the wind boxes 12 are installed, where
  • a second aspect of the present invention provides the combustion device according to the first aspect, wherein second flow rate adjusting means 17 for adjusting a flow rate of the combustion gas that flows into each burner 19 on the upstream side of the first flow rate adjusting means 15 is provided in each wind box 12.
  • the first flow rate adjusting means 15 for adjusting a combustion gas flow rate is provided to each of the plurality of combustion gas nozzles 8 and 11, when an opening degree of the first flow rate adjusting means 15 is adjusted, a momentum of the combustion gas injected into the furnace from the burner 19 can be independently adjusted on each of upper and lower sides.
  • a momentum an air injection flow rate of the air flow rate from the lower side can be higher than that from the upper side of the burner 19, flames can be deflected to a downward direction.
  • the flames can be deflected, and the thermal absorption of the furnace can be controlled.
  • a temperature controller on the rear heat transfer surface of the furnace 18 can be eliminated.
  • the NOx reduction technology based on the change in the after-air port installing position and the air excess ratio can be applied without changing a steam temperature and a metal temperature of the rear heat transfer surface in the conventional example.
  • the combustion region of the burner 19 can be shifted to the lower side, the detention time of the NOx reduction region between the burner 19 and the after-air port 24 can be increased to be longer than that in a case where the injecting direction of the flames is horizontal, and the NOx concentration in the exhaust gas can be reduced as compared with the conventional example.
  • the combustion gas supplied to the wind box 12 provided on the outer side of one furnace wall surface 10 can be collectively supplied from one duct 16, and the combustion gas supply system for the plurality of burners 19 can have a simple configuration.
  • the plurality of wind boxes 12 are aligned and installed on the outer side of the furnace wall 10 inside the one duct 16, construction of the plurality of wind boxes 12 and the duct 16 can be facilitated.
  • the first flow rate adjusting means 15 provided to one wind box 12 can deviate the momentum of the combustion gas on each of the upper and lower sides of the burner 19, and providing the second flow rate adjusting means 17 on the upstream side of the first flow rate adjusting means 15 enables facilitating adjustment of an amount of the combustion gas supplied to each burner 19.
  • FIG. 1 shows a pulverized coal boiler system according to the present invention
  • FIG. 2 is a cross-sectional view of a pulverized coal burner 19 concerning the pulverized coal boiler system in FIG. 1
  • FIG. 3 is a perspective view ( FIG. 3(a) ) of a wind box 12 of the pulverized coal burner 19 and a view ( FIG. 3(b) ) showing a wind tunnel test result concerning the wind box 12.
  • a fuel in the present invention is not restricted to pulverized coal, and a solid fuel pulverized so that it can be carried using an air current can be used without regard to its type or composition.
  • air is mainly used as a fuel carrying gas and a combustion gas
  • the present invention is not necessarily restricted to air alone, and it is possible to adopt any gas that can be used as the fuel carrying gas and the combustion gas for a combustion device such as a boiler, e.g., a combustion exhaust gas or a mixed gas of air or oxygen and the combustion exhaust gas without regard to its type or composition.
  • pulverized coal and combustion air are supplied to burners 19 provided on a plurality of stages on a furnace wall 10 of a boiler furnace 18, the pulverized coal is combusted, and a non-illustrated water wall constituting the furnace wall 10 and a heat exchanger such as a non-illustrated superheater provided in the furnace are heated, thereby generating water vapor.
  • the pulverized coal supplied to each burner 19 is obtained by pulverizing coal in a bunker 20 with use of a mill 21, and the pulverized coal is carried on an air current and supplied to each burner 19 by using a blower 23. Further, the combustion air supplied to each burner 19 and each after-air port 24 is supplied through a duct 16 by a blower 25, and the combustion air is supplied to each pulverized coal burner 19 from each wind box 12 arranged on the outer side of the boiler furnace wall 10.
  • An oil spraying nozzle 7 is arranged at a central axis of the pulverized coal burner 19, a fuel nozzle 3 through which a gas-particle flow 1 of the pulverized coal and the carrying air is arranged at an outer periphery of the oil spraying nozzle 7, and a secondary air nozzle 8 and a tertiary air nozzle 11 that inject the combustion air 2 are provided at an outer periphery of the fuel nozzle 3.
  • an outer peripheral wall of the tertiary air nozzle 11 is formed of the wind box 12.
  • the oil spraying nozzle 7 is used for auxiliary combustion at the time of starting up or low-load combustion of each burner 19.
  • a venturi tube 6 configured to narrow a nozzle inner diameter of the fuel nozzle 3 is arranged on an inner peripheral wall of the fuel nozzle 3, and a pulverized coal concentrator 5 is provided on the outer periphery of the oil spraying nozzle 7 near an outlet portion of the fuel nozzle 3.
  • a flame stabilizer 4 is provided at an end of a partition wall (an outlet portion of each of the nozzles 3 and 8) that partitions the fuel nozzle 3 and the secondary air nozzle 8, and a guide sleeve 13 that directs a fluid toward a diffusing direction from the central axis of the burner 19 is provided at an end of a partition wall (an outlet portion of each of the nozzles 8 and 11) that partitions the secondary air nozzle 8 and the tertiary air nozzle 11.
  • each burner 19 is formed of the oil spraying nozzle 7, the fuel nozzle 3, the secondary air nozzle 8, the tertiary air nozzle 11, and the wind box 12 constituting the outer peripheral wall of the tertiary air nozzle 11, and this burner 19 is installed on the furnace wall 10 of the furnace 18.
  • FIG. 3(a) shows a perspective view of the wind box 12 of the pulverized coal burner 19 according to this embodiment
  • FIG. 4 shows a cross-sectional view ( FIG. 4(a) ) taken along a line A-A in FIG. 2 and a cross-sectional view ( FIG. 4(b) ) taken along a line B-B in FIG. 2 .
  • each dark arrow shown in FIG. 4 and subsequent drawings represents an inflow direction of the combustion air.
  • a heavy oil nozzle 7 and the pulverized coal nozzle 3 are not shown in FIG. 4 , and the heavy oil nozzle 7 and the pulverized coal nozzle 3 are arranged in a cylindrical through hole of the wind box 12.
  • a furnace wall of the through hole constitutes an outer wall of the secondary air nozzle 8.
  • the wind box 12 having combustion air inlet openings 12a and 12b provided in a direction vertical to a central axis direction of the pulverized coal burner 19, and the secondary air nozzle 8 is arranged as if it is inserted in the through hole provided in the wind box 12.
  • the two combustion air inlet openings 12a and 12b are provided in the wind box 12, a partition plate 14 that partitions the two combustion air inlet openings (combustion gas opening portions) 12a and 12b is provided, and the partition plate 14 is connected to the outer side of a portion that divides the outer wall of the secondary air nozzle 8 constituting the through hole of the wind box 12 into two parts.
  • Upper and lower dampers 15a and 15b each of which has a rotary shaft in a direction cutting across a flow of the combustion air introduced into the wind box and changes an area through which the combustion air flows, are provided near the combustion air inlet openings 12a and 12b in the wind box 12 divided into upper and lower parts by the partition plate 14, and separately adjusting respective rotation angles of the two dampers 15a and 15b enables deviating a momentum of the combustion air injected from the pulverized coal burner 19 depending on each of upper and lower sides in the wind box 12.
  • each of the dampers 15a and 15b is arranged in the wind box 12 to be retracted by a length L1 from the inlet opening portion of the wind box 12.
  • FIG. 3 (b) shows a result of a tertiary air flow path outlet velocity distribution at the time of flame downward deflection realized by conducting a test for deviating a momentum of tertiary air injected from the tertiary air nozzle 11 into the furnace depending on each of the upper and lower sides of the burner 19 based on the wind tunnel test. It was confirmed from this wind tunnel test that the momentum of the combustion air on the lower side of the burner 19 can be increased by adjusting a revolving angle of each of the upper and lower revolving dampers 15a and 15b. In case of deflecting flames into the furnace 18 on the upper side of the burner 19, the upper revolving damper 15a is opened, and the lower revolving damper 15b is closed.
  • the combustion air can be gradually injected.
  • Two upper and lower opening portions 8a are provided at the outer peripheral portion of the secondary air nozzle 8, and it is desirable to provide an air capacity adjusting mechanism such as slide type dampers 9a and 9b that adjust an amount of air supplied into the secondary air nozzle 8 from the opening portions 8a as shown in FIG. 2 .
  • the air can be prevented from flowing into the upper secondary air nozzle 8 and the tertiary air nozzle 11 by fully closing the upper opening portion 8a of the secondary air nozzle 8 with use of the slide type damper 9a, and the momentum of the air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained in the circumferential direction, thereby keeping flame stabilizing properties.
  • the momentum of the air injected from the secondary air nozzle 8 into the furnace 18 can be substantially evenly maintained along the circumferential direction of the secondary air nozzle 8 only if the combustion air flows into the secondary nozzle 8 from any position irrespective of whether the upper opening portion 8a of the secondary air nozzle 8 is fully closed by using the slide type damper 9a, but the upper opening portion 8a of the secondary air nozzle 8 must be fully closed by using the slide type damper 9a if softening the deflection of the flames in the furnace 18 toward the lower side is undesirable.
  • a direction of the flames in the furnace 18 can be deflected by just deviating the momentum of the combustion air in each of the upper half portion and the lower half portion in the burner 19 while maintaining flame stabilizing properties by adjusting an inflow amount of the combustion air.
  • the combustion air inlet openings 12a and 12b obtained by dividing the inside of the wind box shown in FIG. 5 into two parts by the partition plate 14 is further divided into two parts and dampers 15aa and 15ab and dampers 15ba and 15bb are provided to the respective combustion air inlet openings 12a and 12b, the momentum of the combustion air is deviated in each of the upper half and the lower half of the burner 19, whereby a direction of flames in the furnace 18 can be deflected.
  • the burners 19 each having the wind box 12 are installed on the furnace wall 10 of the boiler furnace 18, and the combustion air is supplied into the burners 19 from the duct 16 provided on the outer side of the furnace wall 10.
  • arrangement of the duct 16 is dependent on a boiler configuration and an installation angle of the burner 19 relative to the furnace wall 10.
  • the burners 19 each having the wind box 12 are arranged in the duct 16 as shown in FIG. 7 , and the momentum of the combustion air in each of the upper half and the lower half of each burner 19 can be deviated, and a direction of flames in the furnace 18 can be deflected.
  • a wind box 12 into which combustion air flows only from the upper side that is vertical to a central axis direction of a burner 19 is provided, and a plurality of partition plate 14 and revolving dampers 15 are provided in the wind box 12 so that the momentum of the combustion air injected into a furnace can be deviated depending on each of upper and lower sides by adjusting the dampers 15.
  • the partition plates 14 are provided so as to divide into three parts the wind box 12 into which the combustion air flows from one direction, i.e., either upper combustion air inlet opening 12a or 12b vertical to the central axis direction of the burner 19.
  • the dampers 15a, 15b, and 15b as air capacity adjusters are provided on the upstream side of trifurcated air inflow paths in the wind box 12, respectively. Therefore, air flows into the upper side of the burner 19 from a central portion of the wind box 12, and air flows into the lower side of the burner 19 from left and right portions of the wind box 12.
  • two partition plates 14 are provided so as to divide into four parts a wind box 12 into which the combustion air flows from one direction, i.e., either upper combustion air inlet opening 12a or 12b vertical to the central axis direction of the burner 19. Furthermore, the combustion air inlet opening 12a at a central portion of the wind box 12 is divided into two parts, and dampers 15aa, 15ab, and 15b as air capacity adjusters are provided on the upstream side of respective air inflow paths. Therefore, also when shown in Fig. 9 , air flows into the upper side of the burner 19 from an upper central portion of the wind box 12, and air flows into the lower side of the burner 19 from left and right portions of the wind box 12.
  • the momentum on the lower side of the burner 19 in the furnace 18 can be increased by adjusting an amount of the combustion air flowing into the wind box 12 by using three or four dampers 15. Performing an operation opposite to the above-described operation can cope with deflection of flames toward the upper side of the burner 19 in the furnace.
  • a secondary air nozzle 8 having a guide sleeve 13 at an end thereof is provided in the wind box 12 so that the combustion air can be gradually injected.
  • An opening portion 8a is provided in an outer wall of the secondary air nozzle 8, and it is desirable to use an air capacity adjusting mechanism such as slide type dampers 9a and 9b shown in FIG. 2 that can adjust an amount of air supplied into the secondary air nozzle 8 in order to adjust an opening degree of the opening portion 8a.
  • an air capacity adjusting mechanism such as slide type dampers 9a and 9b shown in FIG. 2 that can adjust an amount of air supplied into the secondary air nozzle 8 in order to adjust an opening degree of the opening portion 8a.
  • the flames can be deflected by just deviating the momentum of the tertiary air depending on each of the upper and lower sides of the burner 19 while maintaining the flame stabilizing properties by the above-described operation. According to these structures and the operating method, even when the combustion air inlet opening 12a in the central portion of the wind box 12 is divided into two portions as shown in FIG. 9 and the dampers 15aa and 15ab are provided near these divided portions, the same effect can be obtained by a damper adjustment method.
  • This embodiment provides a configuration that burners 19 each having the wind box 12 are installed on the outer side of the furnace wall 10 of the boiler furnace 18 and the combustion air is put into a duct 16 connected to each wind box 12 from an illustrated inflow direction.
  • arrangement of the duct 16 is dependent on a boiler configuration and an installation angle of the burner 19 relative to the furnace wall 10.
  • the burners 19 each having the wind box 12 are arranged in the duct 16 as shown in FIG. 11 , and the operation method can be executed.
  • This embodiment shown in FIG. 12 and FIG. 13 has a configuration that a wind box 12 into which combustion air flows only from lower combustion air inlet openings 12a and 12b vertical to a central axis of the burner 19 is provided, the inside of the wind box 12 is partitioned by a plurality of partition plates 14, dampers 15b, 15a, and 15b or 15b, 15aa, 15ab, and 15b are provided in respective combustion air nozzles in the wind box 12 partitioned by the partition plates 14, and the momentum of the combustion air injected into a furnace 18 from the burner 19 is deviated depending on each of upper and lower sides of the burner 19 by adjusting opening/closing degrees of the dampers 15b, 15a, and 15b or 15b, 15aa, 15ab, and 15b.
  • the partition plates 14 and 14 are provided so as to divide the wind box 12, into which the combustion air flows from only one lower direction which is a direction vertical to the central axis direction of the burner 19, into three portions.
  • dampers 15b, 15a, and 15b as air capacity adjusters are provided on upstream portions of trifurcated air inflow paths 12b, 12a, and 12b of the wind box 12. Therefore, air from a combustion air inlet opening 12a at a central portion of the wind box 12 flows into the lower side of the burner 19, and air flows into the upper side of the burner 19 from the left and right combustion air inlet openings 12b and 12b of the wind box 12.
  • the momentum on the lower side of the burner 19 can be increased by adjusting opening/closing degrees of the three dampers 15b, 15a, and 15b, and performing an operation opposite to the above-described operation can cope with deflection of flames toward the upper side of the burner 19 in the furnace 18.
  • a secondary air nozzle 8 having a guide sleeve 13 is provided in the wind box 12 so that the combustion air can be injected along a spreading direction from an outlet of the burner 19. Further, an opening portion 8a ( FIG. 2 ) is provided in the secondary air nozzle 8, and it is desirable to adjust an air inflow amount from the opening portion 8a by providing a slide type damper 9 shown in FIG. 2 .
  • the flames can be deflected by just adjusting a tertiary air injection amount to deviate the momentum of the air depending on each of the upper and lower sides of the burner 19 while maintaining the flame stabilizing properties by the above-described operation.
  • the combustion air inlet openings 12b and 12b are provided on both sides of the lower side of the wind box 12
  • the combustion air inlet opening 12a in the central portion is divided into two portions, and the dampers 15b, 15aa, 15ab, and 15b are provided on the upstream side of the respective air inflow paths as shown in FIG. 13
  • the same effect can be obtained by adjustment methods of the dampers 15b, 15aa, 15ab, and 15b.
  • This embodiment is characterized in that the burners 19 each having the wind box 12 are installed on the boiler furnace wall 10 and the combustion air is supplied into the burners 19 from a duct 16 provided on the outer side of the furnace wall 10.
  • arrangement of the duct 16 is dependent on a boiler configuration and an installation angle of the burner 19.
  • the burners 19 each having the wind box 12 are arranged in the duct 16 as shown in FIG. 15 , and the operation method can be carried out.
  • This embodiment provides a configuration where a second damper 17 as a supply air capacity adjuster for each burner 19, which is configured to adjust a flow rate of combustion air flowing into each burner 19, is provided on the upstream side of a damper 15 in addition to the configurations of Embodiments 1 to 3.
  • combustion air flow rate can be adjusted by a first damper 15 alone if its opening degree is adjusted in accordance with each burner 19, when the first damper 15 provided for the purpose of deviating a momentum of the combustion air on each of upper and lower sides of each burner 19 has a function of adjusting the combustion air flow rate consistent with the fuel supply amount, controlling this damper becomes difficult.
  • the first damper 15 and the second damper 17 that share the two different functions are independently provided.
  • FIG. 16 and FIG. 17 shows a configuration where, in addition to first dampers 15a and 15b configured to deviate an air momentum on each of upper and lower sides of the burner 19 described in Embodiment 1 ( FIGS. 4 and 5 ), second dampers 17a and 17b for adjusting a flow rate of the combustion air flowing into each burner 19 are provided on the upstream side of the first dampers 15a and 15b.
  • the flow rate of the combustion air flowing into each burner 19 can be individually adjusted without suppressing a deviation of the momentum of the combustion air on each of the upper and lower sides of the burner 19.
  • first dampers 15a and 15b which are adjusters that deviate the momentum of the combustion air on each of the upper and lower sides of each burner 19 in each wind box 12, on the downstream side of the second dampers 17a and 17b can suffice, and the second dampers 17a and 17b can be arranged at any positions.
  • each of the first dampers 15a and 15b and the second dampers 17a and 17b a member that adjusts an opening area by sliding a plurality of laminated porous plates may be used in place of the illustrated butterfly type damper, and it can have any structure as long as it has a gas flow rate adjusting function.
  • such a secondary air nozzle 8 having the guide sleeve 13 as shown in FIG. 2 is provided in the wind box 12, and the combustion air is injected into the furnace 18 from the outlet of the burner 19 in a spreading manner.
  • the opening portion 8a is provided in the secondary air nozzle 8, and it is desirable to provide the slide type damper 9 that can adjust an air capacity flowing into the secondary air nozzle 8.
  • the combustion air can be prevented from flowing into the tertiary air nozzle 11 on the upper side in the wind box 12 by fully closing the opening portion 8a of the secondary air nozzle 8 provided on the upper side in the wind box 12 with use of the slide type damper 9a, and the momentum of the combustion air injected into the furnace 18 from the secondary air nozzle 8 can be substantially homogeneously maintained along the circumferential direction of the burner 19, thereby holding the flame stabilizing properties.
  • the damper adjustment method for dividing each of the combustion air inlet openings 12a and 12b in the wind box 12 into two parts and providing the first dampers 15aa, 15ab, 15ba, and 15bb and the second dampers 17aa, 17ab, 17ba, and 17bb to the respective combustion air inlet openings 12a and 12b as shown in FIG. 17 enables individually adjusting the flow rate of the combustion air flowing into each burner 19 without suppressing a deviation of the momentum of the combustion air on each of the upper and lower sides of the burner 19.
  • the burners 19 each having the wind box 12 are arranged in the duct 16.
  • An air capacity of each of the plurality of burners 19 arranged on the furnace wall 10 along the horizontal direction in line can be adjusted by providing the second dampers 17 (17a, 17b and 17aa, 17ab; and 17ba, 17bb) shown in FIG. 16 and FIG. 17 in each wind box 12.
  • the burners 19 each having the wind box 12 shown in FIG. 16 and FIG. 17 may be installed on the outer side of the furnace wall 10 of the boiler so that the combustion air from the outside of the furnace 18 can be supplied into the burners 19 each having the wind box 12 through the duct 16.
  • the industrial applicability can be further enhanced.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Supply (AREA)
EP11859242.7A 2011-02-22 2011-02-22 Combustion device Active EP2679899B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL11859242T PL2679899T3 (pl) 2011-02-22 2011-02-22 Urządzenie do spalania

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2011/000976 WO2012114370A1 (ja) 2011-02-22 2011-02-22 燃焼装置

Publications (3)

Publication Number Publication Date
EP2679899A1 EP2679899A1 (en) 2014-01-01
EP2679899A4 EP2679899A4 (en) 2018-01-24
EP2679899B1 true EP2679899B1 (en) 2021-04-07

Family

ID=46720199

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11859242.7A Active EP2679899B1 (en) 2011-02-22 2011-02-22 Combustion device

Country Status (8)

Country Link
US (1) US20130340659A1 (pl)
EP (1) EP2679899B1 (pl)
JP (1) JP5743115B2 (pl)
KR (1) KR101582729B1 (pl)
AU (1) AU2011360560B2 (pl)
CA (1) CA2827903C (pl)
PL (1) PL2679899T3 (pl)
WO (1) WO2012114370A1 (pl)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10375901B2 (en) 2014-12-09 2019-08-13 Mtd Products Inc Blower/vacuum
CN105202568B (zh) * 2015-10-14 2017-05-10 北京高能时代环境技术股份有限公司 生活垃圾炉排炉的二次风装置
CN108087867A (zh) * 2018-01-11 2018-05-29 西安热工研究院有限公司 一种用于平衡低负荷氮氧化物与汽水参数的低氮燃烧***及方法
CN109185871B (zh) * 2018-10-17 2023-09-15 烟台龙源电力技术股份有限公司 一种锅炉二次风***
CN109185872B (zh) * 2018-10-17 2023-09-19 烟台龙源电力技术股份有限公司 一种锅炉二次风***
JP7141574B1 (ja) * 2021-08-10 2022-09-26 コロナ株式会社 送風バーナ装置

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS543924A (en) * 1977-06-09 1979-01-12 Kobe Steel Ltd Combustion method and system for small nitrogen oxide production
US4551090A (en) * 1980-08-25 1985-11-05 L. & C. Steinmuller Gmbh Burner
JPS61101226U (pl) * 1984-12-04 1986-06-27
JPH0729335B2 (ja) * 1989-04-24 1995-04-05 キタノ製作株式会社 歯ブラシなどのハンドルの成形方法および成形型
JP3054420B2 (ja) * 1989-05-26 2000-06-19 株式会社東芝 ガスタービン燃焼器
JPH0543924A (ja) * 1991-08-15 1993-02-23 Kobe Steel Ltd ２次燃焼吹錬方法
JPH0735302A (ja) * 1993-07-22 1995-02-07 Ishikawajima Harima Heavy Ind Co Ltd 石炭焚ボイラのミル常時ウォーミング方法
JPH09101015A (ja) * 1995-10-03 1997-04-15 Babcock Hitachi Kk 燃焼装置とそのスラグ付着除去装置
JPH09133345A (ja) * 1995-11-06 1997-05-20 Mitsubishi Heavy Ind Ltd バーナ
JP3009370B2 (ja) * 1997-03-07 2000-02-14 株式会社日立製作所 微粉炭バーナ、微粉炭ボイラ及び微粉炭燃焼方法
JP4301422B2 (ja) 2000-11-07 2009-07-22 バブコック日立株式会社 燃焼用バーナ、該バーナを備えた燃焼装置及び前記バーナを用いる燃焼方法
US6699031B2 (en) * 2001-01-11 2004-03-02 Praxair Technology, Inc. NOx reduction in combustion with concentrated coal streams and oxygen injection
JP2003254510A (ja) * 2002-02-28 2003-09-10 Babcock Hitachi Kk 燃焼装置ならびにウインドボックス
JP4898393B2 (ja) 2006-11-09 2012-03-14 三菱重工業株式会社 バーナ構造
JP4969464B2 (ja) * 2008-01-08 2012-07-04 三菱重工業株式会社 バーナ構造
WO2009125566A1 (ja) * 2008-04-10 2009-10-15 バブコック日立株式会社 固体燃料バーナ、固体燃料バーナを用いた燃焼装置とその運転方法
JP5344897B2 (ja) * 2008-12-12 2013-11-20 三菱重工業株式会社 旋回燃焼ボイラ
JP2010249362A (ja) * 2009-04-13 2010-11-04 Ihi Corp バーナ
JP2011033287A (ja) * 2009-08-04 2011-02-17 Mitsubishi Heavy Ind Ltd 微粉炭バーナ
WO2012098848A1 (ja) * 2011-01-21 2012-07-26 バブコック日立株式会社 固体燃料バーナおよび前記バーナを用いる燃焼装置

Non-Patent Citations (1)

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

Also Published As

Publication number Publication date
JP5743115B2 (ja) 2015-07-01
EP2679899A1 (en) 2014-01-01
PL2679899T3 (pl) 2021-07-05
CA2827903C (en) 2016-07-12
JPWO2012114370A1 (ja) 2014-07-07
EP2679899A4 (en) 2018-01-24
CA2827903A1 (en) 2012-08-30
KR20140008407A (ko) 2014-01-21
WO2012114370A1 (ja) 2012-08-30
US20130340659A1 (en) 2013-12-26
AU2011360560B2 (en) 2015-11-05
KR101582729B1 (ko) 2016-01-05

Similar Documents

Publication Publication Date Title
EP2679899B1 (en) Combustion device
US5806443A (en) Pulverized coal burner and method of using same
JP5374404B2 (ja) 燃焼バーナおよびこの燃焼バーナを備えるボイラ
EP2837889B1 (en) Sequential combustion with dilution gas mixer
US8726819B2 (en) Burner
AU2007205567A1 (en) Pulverized coal-fired boiler and pulverized coal combustion method
JP2009079794A (ja) 固体燃料バーナ、固体燃料バーナを用いた燃焼装置とその運転方法
EP4094017A1 (en) Nozzle assembly for a solid fuel burner and method of operating a nozzle assembly for a solid fuel burner
JP5797238B2 (ja) 燃料バーナ及び旋回燃焼ボイラ
CA2959134C (en) Low nox turbine exhaust fuel burner assembly
CA2645680A1 (en) In-furnace gas injection port
AU2011332718B2 (en) Pulverized fuel fired boiler equipment
JP2010270990A (ja) 燃料バーナ及び旋回燃焼ボイラ
JP2011052871A (ja) 燃焼装置
KR101595678B1 (ko) 관형상 화염 버너
KR20120103620A (ko) 유동 제어 디바이스
JP6476217B2 (ja) Ｔｄｒダンパー
WO2023120395A1 (ja) アンモニア燃焼バーナ及びボイラ
Whelan et al. Low NO x turbine exhaust fuel burner assembly
JP2005265394A (ja) 混焼型ボイラ
JP2019039612A (ja) ガスバーナ
KR100964307B1 (ko) 미분탄 버너
PL207762B1 (pl) Zespolony pyłowy palnik strumieniowy do spalania pyłu węglowego w kotłach energetycznych

Legal Events

Date Code Title Description
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

17P Request for examination filed

Effective date: 20130802

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

DAX Request for extension of the european patent (deleted)
RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: MITSUBISHI HITACHI POWER SYSTEMS, LTD.

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: MITSUBISHI HITACHI POWER SYSTEMS, LTD.

RA4 Supplementary search report drawn up and despatched (corrected)

Effective date: 20171222

RIC1 Information provided on ipc code assigned before grant

Ipc: F23C 6/04 20060101ALI20171215BHEP

Ipc: F23L 9/00 20060101AFI20171215BHEP

Ipc: F23D 1/00 20060101ALI20171215BHEP

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

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20190206

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: 20201112

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: MITSUBISHI POWER, LTD.

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

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1380156

Country of ref document: AT

Kind code of ref document: T

Effective date: 20210415

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602011070643

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: FI

Ref legal event code: FGE

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20210407

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1380156

Country of ref document: AT

Kind code of ref document: T

Effective date: 20210407

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

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: 20210407

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: 20210407

Ref country code: AT

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: 20210407

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: 20210707

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: 20210407

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

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: 20210807

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: 20210407

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: 20210708

Ref country code: SE

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: 20210407

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: 20210407

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: 20210809

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: 20210707

Ref country code: ES

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: 20210407

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602011070643

Country of ref document: DE

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

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: 20210407

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: 20210407

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: 20210407

Ref country code: DK

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: 20210407

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: 20210407

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: 20210407

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

26N No opposition filed

Effective date: 20220110

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

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: 20210807

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: 20210407

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

Ref country code: IT

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: 20210407

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602011070643

Country of ref document: DE

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: 20210407

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20220228

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20220222

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: 20220222

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: 20220228

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

Ref country code: LI

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

Effective date: 20220228

Ref country code: IE

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

Effective date: 20220222

Ref country code: GB

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

Effective date: 20220222

Ref country code: DE

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

Effective date: 20220901

Ref country code: CH

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

Effective date: 20220228

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: 20220228

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

Ref country code: HU

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

Effective date: 20110222

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: 20210407

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: 20210407

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

Ref country code: FI

Payment date: 20240213

Year of fee payment: 14

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

Ref country code: PL

Payment date: 20240104

Year of fee payment: 14

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

Ref country code: TR

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: 20210407