CN108426247B - Fuel nozzle cooling structure of heat accumulation combustor - Google Patents

Fuel nozzle cooling structure of heat accumulation combustor Download PDF

Info

Publication number
CN108426247B
CN108426247B CN201711212217.9A CN201711212217A CN108426247B CN 108426247 B CN108426247 B CN 108426247B CN 201711212217 A CN201711212217 A CN 201711212217A CN 108426247 B CN108426247 B CN 108426247B
Authority
CN
China
Prior art keywords
exhaust
fuel nozzle
burner
heat accumulation
flow path
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
CN201711212217.9A
Other languages
Chinese (zh)
Other versions
CN108426247A (en
Inventor
河本祐作
北村和也
川端健介
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.)
Chugai Ro Co Ltd
Original Assignee
Chugai Ro Co 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 Chugai Ro Co Ltd filed Critical Chugai Ro Co Ltd
Publication of CN108426247A publication Critical patent/CN108426247A/en
Application granted granted Critical
Publication of CN108426247B publication Critical patent/CN108426247B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/48Nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/72Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/78Cooling burner parts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00Combustion apparatus characterised by arrangements for air supply
    • F23C7/02Disposition of air supply not passing through burner
    • F23C7/06Disposition of air supply not passing through burner for heating the incoming air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING 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
    • F23L15/00Heating of air supplied for combustion
    • F23L15/02Arrangements of regenerators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2209/00Safety arrangements
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/34Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Abstract

The invention provides a fuel nozzle cooling structure of a heat accumulation burner, which can reduce the equipment cost and the required installation space required by cooling a fuel nozzle by using an exhaust blower for exhausting in an exhaust operation mode, and has simple arrangement of a pipeline and the like. The heat accumulation burner alternately repeats an exhaust mode and a combustion mode, and the fuel nozzle cooling structure of the heat accumulation burner includes: a hollow cylindrical fuel nozzle which is provided inside the burner body and which injects fuel mixed with combustion air from a tip end thereof to generate a flame; a cooling pipe provided so as to surround an outer periphery of the fuel nozzle, and having a communication portion for communicating with an exhaust system and an opening portion that opens to the atmosphere; and a connection pipe that connects the communication portion and the exhaust system, and cools the fuel nozzle by the atmosphere that flows toward the communication portion through the opening portion by an exhaust suction action of the exhaust system via the connection pipe.

Description

Fuel nozzle cooling structure of heat accumulation combustor
Technical Field
The present invention relates to a fuel nozzle cooling structure for a regenerative combustor, which can reduce the equipment cost and the required installation space required for cooling a fuel nozzle and simplify the arrangement of piping and the like by using an exhaust blower for exhausting in an exhaust operation mode.
Background
Various furnaces using regenerative burners are known (see patent document 1), and in this case, a structure for cooling the regenerative burners is also known (see patent documents 2 and 3). The "industrial furnace, method for energy-saving operation of the industrial furnace, and method for modifying the industrial furnace" of patent document 1 includes: an exhaust pipe connecting the combustion chamber with the chimney; an intake on-off valve that opens to introduce external Air (ATM) into the exhaust pipe; and an impeller connected to a suction blower functioning as a generator (generator), and configured to generate power by being rotated by external air introduced from the open intake opening/closing valve and flowing through the exhaust pipe. In patent document 1, the combustion operation and the exhaust operation of a pair of two regenerative burners are alternately switched.
The "low NOx burner for high-temperature air" of patent document 2 is configured such that a Baffle (pocket) is fitted externally to a tip end portion of a fuel nozzle for injecting fuel, a slit-shaped secondary air supply hole is formed in an outer periphery of the Baffle, the fuel nozzle is configured as a double pipe having an inner periphery portion as a fuel passage and an outer periphery portion as a cooling air passage, a fuel and cooling air ejection hole is provided in a center of the Baffle, a plurality of primary air supply holes having an angle of 30 to 50 ° are provided in a plane having the same pitch circle diameter from an inlet toward an outlet in an outer periphery side of the ejection hole, and ejection holes for fuel, cooling air, and primary air are formed in outlets of the ejection hole and the primary air supply hole. In the burner of patent document 2, air for cooling the fuel nozzle is discharged into the furnace.
In the "cooling device for a regenerative burner fuel nozzle pipe" of patent document 3, there is a problem that the introduced air is not discharged into the furnace but is used only for cooling the cooling air pipe, and the cooling air pipe is cooled while reciprocating forward and forward, thereby effectively preventing overheating of the cooling air pipe. In patent document 3, a blower is required to be provided to send the introduced air to the air cooling pipe without discharging the introduced air for cooling into the furnace.
Prior art documents
Patent document
Patent document 1: japanese patent laid-open publication No. 2016-133255
Patent document 2: japanese laid-open patent publication No. 10-185128
Patent document 3: japanese patent laid-open publication No. 2001 and 182915
Disclosure of Invention
Problems to be solved by the invention
In view of the fact that the furnace atmosphere heated by the regenerative burner is preferably homogeneous without fluctuation, it is preferable to use the double-tube structure of patent document 3 in which the introduced air is not discharged into the furnace as the cooling structure of the fuel nozzle provided in the regenerative burner.
However, patent document 3 does not disclose how to supply the introduced air to the air-cooling duct. In general, it is considered that a blower is newly or additionally provided, and the introduced air is supplied from the blower to the air supply pipe. When a blower is newly installed, there are problems that equipment costs including piping are incurred and installation space needs to be secured.
The present invention has been made in view of the above-described conventional problems, and an object thereof is to provide a fuel nozzle cooling structure for a regenerative combustor, which can reduce the equipment cost and installation space required for cooling the fuel nozzle and simplify the layout of piping and the like by using an exhaust blower that exhausts in an exhaust operation mode.
Means for solving the problems
In a fuel nozzle cooling structure of a heat storage burner according to the present invention, the heat storage burner alternately repeats an exhaust mode in which in-furnace exhaust gas sucked from a burner port of a burner main body by an exhaust suction action of an exhaust system having an exhaust blower is circulated to a heat storage portion to store waste heat, and a combustion mode in which a flame generated from combustion air heated by circulating the combustion air to the heat storage portion is ejected from the burner port of the burner main body into a furnace, the fuel nozzle cooling structure of the heat storage burner includes: a hollow cylindrical fuel nozzle which is provided inside the burner main body and which injects fuel mixed with combustion air from a tip end thereof to generate a flame; a cooling pipe provided so as to surround an outer periphery of the fuel nozzle, and having a communication portion for communicating with the exhaust system and an opening portion that opens to the atmosphere; and a connection pipe that connects the communication portion and the exhaust system, and cools the fuel nozzle by the atmosphere that flows toward the communication portion through the opening portion by an exhaust suction action of the exhaust system via the connection pipe.
Further, in the fuel nozzle cooling structure of the heat accumulating burner of the present invention, the heat accumulating burner alternately repeats an exhaust mode in which an exhaust valve for opening and closing an exhaust system having an exhaust blower is opened and an air supply valve for opening and closing an air supply system having an air supply blower is closed, furnace exhaust gas sucked from a burner port of a burner main body by an exhaust suction action of the exhaust system is circulated to a heat accumulating portion to accumulate waste heat and is discharged to the exhaust system via the exhaust valve, and a combustion mode in which the exhaust valve is closed and the air supply valve is opened, combustion air supplied to the burner main body by the air supply action of the air supply system is circulated to the heat accumulating portion to be heated, and flame generated by the heated combustion air is ejected into a furnace from the burner port of the burner main body, the fuel nozzle cooling structure of the regenerative combustor is characterized by comprising: a hollow cylindrical fuel nozzle which is provided inside the burner main body and which injects fuel mixed with combustion air from a tip end thereof to generate a flame; a cooling pipe provided so as to surround an outer periphery of the fuel nozzle, and having a communication portion for communicating with the exhaust system and an opening portion that opens to the atmosphere; and a connection pipe connecting the communication portion and the exhaust system at an intermediate position between the heat storage portion and the exhaust valve, wherein the fuel nozzle is cooled by atmospheric air flowing toward the communication portion through the opening portion by an exhaust suction action of the exhaust system via the connection pipe in an exhaust mode, and the fuel nozzle is cooled by combustion air bypassing the heat storage portion and flowing toward the opening portion through the communication portion via the connection pipe by an air supply action of the air supply system in a combustion mode.
The fuel nozzle cooling structure for a regenerative combustor is characterized in that the communication portion and the opening portion of the cooling pipe are formed on a base end portion side on a side opposite to a tip end portion of the fuel nozzle, and the cooling pipe includes: a first flow path that surrounds the periphery of the fuel nozzle, is formed from a distal end side to a proximal end side in a longitudinal direction thereof, and communicates with the communication portion; a second flow path that surrounds the periphery of the first flow path, is formed from a distal end side to a proximal end side in a longitudinal direction of the fuel nozzle, and communicates with the opening; and a connection flow path that connects the first flow path and the second flow path on a front end side of the fuel nozzle.
The fuel nozzle cooling structure for a regenerative combustor is characterized by comprising a pair of regenerative combustors, one of which is operated in a combustion mode and the other of which is operated in an exhaust mode, wherein the exhaust systems of the regenerative combustors are joined at a junction, and a single exhaust blower is provided downstream of the junction.
Effects of the invention
In the fuel nozzle cooling structure of the regenerative combustor according to the present invention, the exhaust blower that exhausts gas in the exhaust operation mode is used, so that the facility cost and the installation space required for cooling the fuel nozzle can be reduced, and the arrangement of piping and the like can be simplified.
Drawings
Fig. 1 is a configuration diagram showing a first embodiment of a fuel nozzle cooling structure of a regenerative combustor of the present invention.
Fig. 2 is a structural view showing a second embodiment of a fuel nozzle cooling structure of the regenerative combustor of the present invention.
Description of the reference numerals
1L, 1R regenerative burners; 2L and 2R fire holes; a 3L, 3R burner body; 3a the other end of the burner body; 4L, 4R heat storage portions; 4a one end of the heat storage portion; 4b the other end of the heat storage portion; 5, furnace; 6L, 6R fuel nozzles; 6a the front end of the fuel nozzle is open; 6b base end of fuel nozzle; 8L, 8R cooling pipes; 9L, 9R fuel on-off valve; 10 a fuel supply system; 11 an air supply blower; 12L, 12R air supply valves; 13 an air supply system; 13a combustion air supply pipe; 13b a combustion air merging portion; 13c a combustion air supply main pipe; 14 an exhaust blower; 15L, 15R exhaust valves; 16 an exhaust system; 16a an exhaust pipe; 16b an exhaust merging section; 16c an exhaust main pipe; a 17L, 17R connecting tube; 19 an inner tube; 19a closed end plate; 20 an outer tube; 20a first sealed end plate; 20b a second sealed end plate; 21 an opening part; 22 a communication part; 23 a first flow path; 24 a second flow path; 25 connecting the flow path; 26L, 26R connecting pipes; e, exhausting; f, flame.
Detailed Description
Hereinafter, preferred embodiments of a fuel nozzle cooling structure of a regenerative combustor according to the present invention will be described in detail with reference to the accompanying drawings. Fig. 1 is a structural view showing a fuel nozzle cooling structure of the regenerative combustor of the first embodiment.
As shown in fig. 1, the regenerative burners 1L and 1R include, as is well known in the art: burner bodies 3L, 3R having burners 2L, 2R at one end facing the inside of the furnace 5; and heat accumulating portions 4L and 4R provided adjacent to and directly connected to the burner bodies 3L and 3R at the other ends 3a of the burner bodies 3L and 3R, wherein the heat accumulating burners 1L and 1R are operated so that a pair of opposed combustion modes in which a flame F is ejected from the ports 2L and 2R of the burner bodies 3L and 3R into the furnace 5 to heat the inside of the furnace 5 (for example, about 1000 ℃) and an exhaust mode in which the exhaust gas E in the furnace 5 is sucked and discharged from the ports 2L and 2R are alternately and repeatedly switched.
In the heat storage burners 1L and 1R, in the exhaust mode, the exhaust gas E is sucked from the furnace 5 by the exhaust gas suction action of the exhaust system 16 having the exhaust blower 14, and the sucked exhaust gas E flows to the heat storage portions 4L and 4R, whereby the waste heat of the exhaust gas E is stored in the heat storage portions 4L and 4R, so that the exhaust gas E having passed through the heat storage portions 4L and 4R is cooled (for example, about 200 ℃) and discharged to the exhaust system 16, and thereafter, when the operation is switched from the exhaust mode to the combustion mode, the combustion air flows to the heat storage portions 4L and 4R by the air supply action of the air supply system 13 having the air supply blower 11, and the combustion air is preheated (heated) by the waste heat of the exhaust gas E stored in the heat storage portions 4L and 4R.
The preheated combustion air is supplied to the burner bodies 3L and 3R, and is mixed with fuel gas supplied through the fuel nozzles 6L and 6R provided inside the burner bodies 3L and 3R and burned, whereby the burner bodies 3L and 3R generate flames F through an energy-saving operation using waste heat.
In the case of using the regenerative burners 1L, 1R, the burners 1L, 1R are used in a pair so that the furnace temperature does not fluctuate with mode switching between the combustion mode and the exhaust mode.
The operation control is performed such that when one of the heat accumulation burners 1L (1R) is in the combustion mode, the other heat accumulation burner 1R (1L) is operated in the exhaust mode, and when the former is switched to the exhaust mode, the latter is switched to the combustion mode.
In the illustrated example, a pair of burner bodies 3L and 3R are provided on the left and right furnace side walls facing each other among the furnace walls constituting the furnace 5 having a rectangular cross section. The pair of burner bodies may be disposed adjacent to the same wall surface.
As shown in fig. 1, in the fuel nozzle cooling structure of the heat accumulation burner of the present embodiment, a pair of left and right heat accumulation burners 1L and 1R each include: burner bodies 3L, 3R in the form of passages having ports 2L, 2R open into the furnace 5 at one end; heat storage portions 4L, 4R having one ends 4a connected to the other ends 3a of the burner main bodies 3L, 3R; hollow and simple fuel nozzles 6L, 6R which are provided so as to penetrate the other end 3a side of the burner bodies 3L, 3R and be inserted from the outside into the burner bodies 3L, 3R, have tip end openings 6a facing the ports 2L, 2R, and eject fuel such as fuel gas mixed with combustion air from the tip end openings 6a toward the ports 2L, 2R to generate flames F; cooling pipes 8L and 8R provided so as to surround the outer peripheries of the fuel nozzles 6L and 6R, penetrating the other ends 3a of the burner bodies 3L and 3R, and extending from the outer portions thereof into the burner bodies 3L and 3R to the front end openings 6a of the fuel nozzles 6L and 6R or the vicinity thereof; a fuel supply system 10 having on-off valves 9L and 9R for fuel (in the figure, white open is shown as open, and black solid is shown as closed) for controlling supply/stop of fuel, and connected to the fuel nozzles 6L and 6R on the side of the base ends 6b of the fuel nozzles 6L and 6R opposite to the front end opening 6a on one end side in the longitudinal direction, so as to supply fuel toward the front end openings 6a of the fuel nozzles 6L and 6R; an air supply system 13 which has an air supply blower 11 for supplying combustion air to the burner bodies 3L and 3R and air supply valves 12L and 12R (white open and black solid are shown as open and closed in the figure) which are openable and closable to control supply and stop of the combustion air, and which is connected to the other end 4b of each heat storage portion 4L and 4R to supply the combustion air to the heat storage portions 4L and 4R; and an exhaust system 16 having an exhaust blower 14 for sucking the exhaust gas E from the furnace 5 through the ports 2L and 2R and discharging the exhaust gas E to the outside of the furnace 5, and openable and closable exhaust valves 15L and 15R (in the figure, white open is shown as open, and black solid is shown as closed) for controlling the discharge and stop of the exhaust gas E, and connected to the other ends 4b of the heat storage portions 4L and 4R so as to allow the exhaust gas E flowing out of the heat storage portions 4L and 4R to flow therethrough.
In detail, the air supply system 13 includes: a pair of combustion air supply pipes 13a directly connected to the heat storage portions 4L and 4R of the pair of heat storage burners 1L and 1R, respectively, and through which the combustion air supplied to the heat storage portions 4L and 4R flows, respectively; a combustion air merging portion 13b for merging the combustion air supply pipes 13 a; and a combustion air supply main pipe 13c connected to each combustion air supply pipe 13a via a combustion air merging portion 13b, wherein an air supply blower 11 is provided in the combustion air supply main pipe 13c to supply combustion air to both the pair of regenerative burners 1L and 1R, and air supply valves 12L and 12R are provided in the combustion air supply pipe 13a to individually switch the operation mode of the pair of regenerative burners 1L and 1R.
In the heat storage combustor 1R (1L) in the combustion mode, the exhaust valve 15R (15L) is closed and the air supply valve 12R (12L) is opened, and the combustion air fed by the air supply action of the air supply system 13 flows to the heat storage portion 4R (4L) through the air supply valve 12R (12L), and is further supplied from the heat storage portion 4R (4L) toward the burner port 2R (2L) of the combustor main body 3R (3L).
In detail, the exhaust system 16 includes: a pair of exhaust pipes 16a directly connected to the heat storage portions 4L and 4R of the pair of heat storage burners 1L and 1R, respectively, and through which the exhaust gas E discharged from the heat storage portions 4L and 4R flows, respectively; an exhaust merging portion 16b for merging the exhaust pipes 16a with each other; and an exhaust main pipe 16c connected to the exhaust pipes 16a via an exhaust merging portion 16b, the exhaust main pipe 16c being provided with an exhaust blower 14 for discharging the exhaust E from both of the pair of heat accumulation burners 1L, 1R, and the exhaust pipes 16a being provided with exhaust valves 15L, 15R for individually switching the operation modes of the pair of heat accumulation burners 1L, 1R.
In the heat storage combustor 1L (1R) in the exhaust mode, the exhaust valve 15L (15R) is opened and the air supply valve 12L (12R) is closed, and the exhaust gas E sucked by the exhaust suction action of the exhaust system 16 flows from the burner port 2L (2R) of the combustor main body 3L (3R) to the heat storage portion 4L (4R), and is further discharged from the heat storage portion 4L (4R) to the exhaust system 16 via the exhaust valve 15L (15R).
When the heat accumulation burners 1L and 1R are in the combustion mode, the fuel on-off valves 9L and 9R are opened to supply fuel to the fuel nozzles 6L and 6R, and when in the exhaust mode, the fuel on-off valves 9L and 9R are closed to stop the supply of fuel.
When the heat accumulation burners 1L and 1R are in the combustion mode, the air supply valves 12L and 12R are opened to supply combustion air to the ports 2L and 2R of the burner bodies 3L and 3R through the heat accumulation portions 4L and 4R, and when the exhaust mode is in the exhaust mode, the air supply valves 12L and 12R are closed to stop the supply of combustion air.
When the heat storage burners 1L, 1R are in the exhaust mode, the exhaust valves 15L, 15R are opened to suck the exhaust gas E in the furnace 5 from the ports 2L, 2R of the burner main bodies 3L, 3R through the heat storage portions 4L, 4R, and when in the combustion mode, the exhaust valves 15L, 15R are closed to stop the suction of the exhaust gas E. The air supply blower 11 and the air exhaust blower 14 are normally operated at all times during the operation of the furnace 5.
In the present embodiment, in contrast to the basic configuration of the heat accumulating burners 1L, 1R described above, each of the heat accumulating burners 1L, 1R includes a cooling structure that is disposed so as to face the high- temperature fire ports 2L, 2R and cools the fuel nozzles 6L, 6R through which the high-temperature exhaust gas E flows around the cooling structure. The cooling structure of the fuel nozzles 6L, 6R mainly includes the cooling pipes 8L, 8R and the connection pipes 17L, 17R that connect the cooling pipes 8L, 8R to the exhaust system 16.
The cooling pipes 8L, 8R include an inner pipe 19, an outer pipe 20, an opening 21, and a communicating portion 22, the inner pipe 19 surrounding the outer periphery of the fuel nozzles 6L, 6R and being formed in a tubular shape in the longitudinal direction from the front end opening 6a side to the base end portion 6b side, the base end portion of the fuel nozzles 6L, 6R outside the burner bodies 3L, 3R being closed by an annular closed end plate 19a joined to the outer peripheral surfaces of the fuel nozzles 6L, 6R and being open at the front end side close to the burner ports 2L, 2R, the outer pipe 20 surrounding the outer periphery of the inner pipe 19 and being formed in a tubular shape in the longitudinal direction of the fuel nozzles 6L, 6R from the front end opening 6a side to the base end portion 6b side, the base end portion of the fuel nozzles 6L, 6R outside the burner bodies 3L, 3R being sealed at the base end portion thereof by an annular first sealing end plate 20a joined to the outer peripheral surface of the inner pipe 19, the front end portion side of the inner tube 19 is covered from the burner 2L, 2R side at the position of the front end portion opening 6a of the fuel nozzle 6L, 6R that extends further toward the burner 2L, 2R side than the inner tube 19, and is sealed by an annular second seal end plate 20b that is joined to the outer peripheral surface of the fuel nozzle 6L, 6R, the opening portion 21 is formed in the outer tube 20 so as to be open to the atmosphere on the base end portion 6b side of the fuel nozzle 6L, 6R outside the burner main body 3L, 3R, and the communication portion 22 is formed in the inner tube 19 for communicating with the exhaust system 16.
The cooling pipes 8L and 8R are provided with: a first flow path 23 which surrounds the outer periphery of the fuel nozzles 6L and 6R, is formed from the front end opening 6a side to the base end 6b side in the longitudinal direction thereof, and communicates with the communication portion 22; a second flow path 24 which surrounds the outer periphery of the first flow path 23, is formed from the front end opening 6a side to the base end 6b side in the longitudinal direction of the fuel nozzles 6L and 6R, and communicates with the opening 21; and a connection flow path 25 that connects the first flow path 23 and the second flow path 24 so as to turn back on the side of the distal end opening 6a of the fuel nozzle 6L, 6R.
That is, the exhaust system 16, which functions as exhaust suction, is open to the atmosphere via the outer periphery of the fuel nozzles 6L, 6R. The communicating portions 22 of the cooling pipes 8L and 8R are connected to the exhaust system 16 via the connecting pipes 17L and 17R, and in the present embodiment, the communicating portions 22 of the cooling pipes 8L and 8R are connected to the exhaust main pipe 16c on which the exhaust blower 14 is provided singly, on the downstream side of the exhaust merging portion 16b where the exhaust pipes 16a from the respective heat storage portions 4L and 4R merge together. The connection positions of the connection pipes 17L, 17R of the regenerative burners 1L, 1R with respect to the exhaust system 16 may be connected at any positions as long as they are intermediate positions between the exhaust valves 15L, 15R and the exhaust blower 14.
Next, the operation of the fuel nozzle cooling structure of the regenerative combustor of the first embodiment will be described. During operation of the furnace 5, for example, as shown in fig. 1, in the regenerative burner 1R on one side (right side), the on-off valve 9R for fuel and the air supply valve 12R are opened and the exhaust valve 15R is closed to set a combustion mode, while in the regenerative burner 1L on the other side (left side), the on-off valve 9L for fuel and the air supply valve 12L are closed and the exhaust valve 15L is opened to set an exhaust mode. The operation of the regenerative burners 1L and 1R itself is known as described above.
The exhaust gas E, which flows through the heat storage portion 4L of the heat storage combustor 1L in the exhaust mode by the exhaust suction action of the exhaust blower 14, is stored in the heat storage portion 4L and cooled, reaches the exhaust blower 14 via the open exhaust valve 15L, and is discharged.
The exhaust suction action of the exhaust blower 14 acts on the communicating portion 22 of each of the cooling pipes 8L and 8R from the exhaust main pipe 16c via the two connecting pipes 17L and 17R. Since the communication portion 22 communicates with the opening 21 that is open to the atmosphere via the first flow path 23, the connection flow path 25, and the second flow path 24, the atmosphere flows through the opening 21 into the cooling pipes 8L and 8R on both sides toward the communication portion 22 by the exhaust suction action of the exhaust blower 14.
The ambient air at a temperature much lower than the temperature (about 1000 ℃) of the one end 4a of the heat accumulating portion 4L, 4R flows from the opening 21 on the base end side of the cooling pipe 8L, 8R of both the pair of heat accumulating burners 1L, 1R toward the second flow path 24 in the outer pipe 20 through the opening 6a at the tip end of the fuel nozzle 6L, 6R provided in both the pair of heat accumulating burners 1L, 1R in the combustion mode and the exhaust mode facing the burner 2L, 2R in the furnace 5 and in a high temperature state, and is further circulated through the first flow path 23 in the inner tube 19 after being folded back by the connecting flow path 25, the fuel nozzles 6L, 6R of the heat accumulating burners 1L, 1R are cooled, and after cooling, of course, the exhaust gas E is sucked and discharged from the communicating portion 22 to the exhaust system 16 through which the exhaust gas E flows by the exhaust suction action of the single exhaust blower 14 without flowing into the furnace 5.
Even if the left heat accumulation burner 1L is switched to the combustion mode and the right heat accumulation burner 1R is switched to the exhaust mode, the left and right fuel nozzles 6L, 6R are always cooled by the air introduced by the exhaust suction action during the operation of the exhaust blower 14.
In the fuel nozzle cooling structure of the heat storage combustor of the first embodiment described above, the heat storage combustor 1L, 1R alternately repeats an exhaust mode in which waste heat is stored by circulating furnace exhaust gas E sucked from the ports 2L, 2R of the combustor main bodies 3L, 3R by an exhaust suction action of the exhaust system 16 having the exhaust blower 14 to the heat storage portions 4L, 4R provided adjacent to and directly connected to the combustor main bodies 3L, 3R, and a combustion mode in which flames F generated from combustion air heated by circulating to the heat storage portions 4L, 4R are ejected from the ports 2L, 2R of the combustor main bodies 3L, 3R into the furnace 5, the heat storage combustor 1L, 1R including: hollow and simple fuel nozzles 6L and 6R which are provided inside the burner bodies 3L and 3R and which inject fuel mixed with combustion air into the furnace 5 from the tip end openings 6a thereof to generate flames F; cooling pipes 8L and 8R provided so as to surround the outer peripheries of the fuel nozzles 6L and 6R, and having a communication portion 22 for communicating with the exhaust system 16 and an opening portion 21 that opens to the atmosphere; and connection pipes 17L, 17R that connect the communication portion 22 with the exhaust system 16, and cool the fuel nozzles 6L, 6R through the opening portion 21 by the exhaust suction action of the exhaust system 16 via the connection pipes 17L, 17R, so that the fuel nozzles 6L, 6R can be cooled by flowing the cooling air into the cooling pipes 8L, 8R by the exhaust blower 14 that discharges the exhaust gas E in the exhaust mode, thermal deformation of the fuel nozzles 6L, 6R can be prevented, and further, the equipment required for cooling the fuel nozzles 6L, 6R only needs the cooling pipes 8L, 8R surrounding the fuel nozzles 6L, 6R and the connection pipes 17L, 17R that connect the cooling pipes 8L, 8R with the exhaust system 16, so that the equipment cost and the required installation space can be reduced, only the spatial extent of the tubes is required and the arrangement is therefore also simple.
The communicating portions 22 and the openings 21 of the cooling pipes 8L and 8R are formed on the base end portion 6b side opposite to the front end portion openings 6a of the fuel nozzles 6L and 6R, and the cooling pipes 8L and 8R include: a first flow path 23 which surrounds the outer periphery of the fuel nozzles 6L and 6R, is formed from the front end opening 6a side to the base end 6b side in the longitudinal direction thereof, and communicates with the communication portion 22; a second flow path 24 which surrounds the outer periphery of the first flow path 23, is formed from the front end opening 6a side to the base end 6b side in the longitudinal direction of the fuel nozzles 6L and 6R, and communicates with the opening 21; and a connection channel 25 that connects the first channel 23 and the second channel 24 to each other on the side of the distal end opening 6a of the fuel nozzle 6L, 6R, so that the atmosphere can be circulated and reciprocated from the second channel 24 to the first channel 23 in the longitudinal direction of the fuel nozzle 6L, 6R to ensure a cooling effect, and the atmosphere for cooling can be efficiently cooled without being released into the furnace 5, thereby preventing the atmosphere in the furnace from varying.
The heat storage burners 1L and 1R are provided with a pair of heat storage burners 1L and 1R that operate in the exhaust mode when one is in the combustion mode, and the exhaust systems 16 of the heat storage burners 1L and 1R are joined together at the exhaust joining portion 16b, and the single exhaust blower 14 is provided downstream of the exhaust joining portion 16b, so even in the furnace 5 that operates by the pair of heat storage burners 1L and 1R, it is possible to ensure the alternate combustion operation by cooling both the fuel nozzles 6L and 6R by the single exhaust blower 14.
In the description of the present embodiment, the case where the heat storage burners 1L and 1R are applied to a pair has been described, but the heat storage burners are not limited to a pair, and the above-described operational effects can be obtained even if the heat storage burners are single bodies.
Fig. 2 is a structural view showing a fuel nozzle cooling structure of the regenerative combustor of the second embodiment. The connecting pipes 26L, 26R of the second embodiment are different in connecting position with respect to the exhaust system 16, and thus different in function, as compared with the first embodiment described above.
In the first embodiment, the connection pipes 17L, 17R from the communication portion 22 are connected to the exhaust main pipe 16c, but in the second embodiment, the connection pipes 26L, 26R from the communication portion 22 are connected to intermediate positions between the heat storage portions 4L, 4R provided adjacent to and directly connected to the burner main bodies 3L, 3R and the exhaust valves 15L, 15R in the heat storage burners 1L, 1R, respectively. The other structure is the same as that of the first embodiment.
The operation of the fuel nozzle cooling structure of the regenerative combustor of the second embodiment will be described. As described above, the regenerative burners 1L, 1R are, in the combustion mode, at a higher temperature in the vicinity of the tip end opening 6a of the fuel nozzles 6L, 6R facing the ports 2L, 2R where the flames F are generated than in other portions of the fuel nozzles 6L, 6R, and in the exhaust mode, the flames F are extinguished, but high-temperature exhaust gas E flows around the fuel nozzles 6L, 6R.
Therefore, it is preferable that the cooling of the fuel nozzles 6L and 6R by the cooling pipes 8L and 8R be performed at a low temperature on the inner pipe 19 side in the combustion mode and at a low temperature on the outer pipe 20 side in the exhaust mode.
In the second embodiment, since the connection positions of the connection pipes 26L, 26R with respect to the exhaust system 16 are connected to the intermediate positions of the heat storage portions 4L, 4R and the exhaust valves 15L, 15R, in the exhaust mode (shown by the operation of the heat storage combustor 1L on the left in the figure), the atmospheric air that passes through the opening portion 21 by the exhaust suction action of the exhaust system 16 via the connection pipe 26L and flows toward the communication portion 22 first flows through the outer pipe 20 and then flows through the inner pipe 19, as in the first embodiment, whereby the outer pipe 20 exposed to the exhaust gas E can be cooled more efficiently by the atmospheric air at a lower temperature, and thus the fuel nozzle 6L can be cooled appropriately to prevent overheating.
On the other hand, in the combustion mode (shown by the operation of the heat accumulating combustor 1R on the right in the figure), unlike the first embodiment described above, among the combustion air supplied toward the heat accumulating portion 4R by the air supply action of the air supply system 13 having the air supply blower 11, a part of the combustion air bypasses the heat accumulating portion 4R, flows into the connecting pipe 26R through the exhaust system 16 (exhaust pipe 16a) in which the exhaust valve 15R is closed, then flows toward the opening portion 21 through the connecting pipe 26R and the communicating portion 22, and the part of the combustion air flows through the inner pipe 19 first and then flows through the outer pipe 20, whereby the inner pipe 19 exposed to the flame F can be cooled more efficiently by the combustion air of a lower temperature, and the fuel nozzle 6R can be cooled appropriately to prevent overheating.
That is, the flow direction in the cooling pipes 8L and 8R changes with respect to the switching of the operation conditions such as the combustion mode and the exhaust mode, and thus a good cooling effect of the fuel nozzles 6L and 6R can be ensured.
Further, since the connection pipes 26L and 26R are only required to be disposed between the burner bodies 3L and 3R and the heat storage portions 4L and 4R, which are directly connected to each other in an adjacent manner, it is not necessary to extend the connection pipes 17L and 17R at least to the downstream side of the exhaust valves 15L and 15R as in the first embodiment, and therefore, the space for the pipes can be reduced, and the cost of the equipment and the size of the equipment layout can be reduced.
In the second embodiment, the above-described operation and effect can be obtained not only by applying the heat accumulation burners 1L and 1R to a pair of heat accumulation burners but also by using only one heat accumulation burner. The second embodiment may have other operational effects of the first embodiment.

Claims (6)

1. A fuel nozzle cooling structure of a heat storage burner that alternately repeats an exhaust mode in which exhaust gas in a furnace, which is sucked from a burner port of a burner body by an exhaust suction action of an exhaust system having an exhaust blower, is circulated to a heat storage portion to store waste heat, and a combustion mode in which a flame generated from combustion air, which is circulated to the heat storage portion and heated, is ejected from the burner port of the burner body into the furnace,
the fuel nozzle cooling structure of the heat accumulation burner comprises: a hollow cylindrical fuel nozzle which is provided inside the burner main body and which injects fuel mixed with combustion air from a tip end thereof to generate a flame; a cooling pipe provided so as to surround an outer periphery of the fuel nozzle, and having a communication portion for communicating with the exhaust system and an opening portion that opens to the atmosphere; and a connection pipe connecting the communication portion with the exhaust system,
the fuel nozzle is cooled by the atmosphere flowing toward the communication portion through the opening portion by an exhaust suction action of the exhaust system via the connection pipe.
2. The fuel nozzle cooling structure of the regenerative combustor according to claim 1,
the communication portion and the opening portion of the cooling pipe are formed on a base end portion side opposite to the fuel nozzle tip portion, and the cooling pipe includes: a first flow path that surrounds the periphery of the fuel nozzle, is formed from a distal end side to a proximal end side in a longitudinal direction thereof, and communicates with the communication portion; a second flow path that surrounds the periphery of the first flow path, is formed from a distal end side to a proximal end side in a longitudinal direction of the fuel nozzle, and communicates with the opening; and a connection flow path that connects the first flow path and the second flow path on a front end side of the fuel nozzle.
3. The fuel nozzle cooling structure of the regenerative combustor according to claim 1 or 2,
the fuel nozzle cooling structure of the heat accumulation burner includes a pair of the heat accumulation burners operated in an exhaust mode when one of the heat accumulation burners is in a combustion mode, and the exhaust systems of the heat accumulation burners are joined to each other at a junction portion, and a single exhaust blower is provided downstream of the junction portion.
4. A fuel nozzle cooling structure of a heat accumulation burner that alternately repeats an exhaust mode in which an exhaust valve that opens and closes an exhaust system having an exhaust blower is opened and an air supply valve that opens and closes an air supply system having an air supply blower is closed, and that circulates in-furnace exhaust gas that is drawn from a burner port of a burner body by an exhaust suction action of the exhaust system to a heat accumulation portion to accumulate waste heat and discharges the waste heat to the exhaust system via the exhaust valve, and a combustion mode in which the exhaust valve is closed and the air supply valve is opened, and that circulates combustion air that is supplied to the burner body by an air supply action of the air supply system to the heat accumulation portion to be heated, and that ejects a flame generated from the heated combustion air from the burner port of the burner body into a furnace,
the fuel nozzle cooling structure of the heat accumulation burner comprises: a hollow cylindrical fuel nozzle which is provided inside the burner main body and which injects fuel mixed with combustion air from a tip end thereof to generate a flame; a cooling pipe provided so as to surround an outer periphery of the fuel nozzle, and having a communication portion for communicating with the exhaust system and an opening portion that opens to the atmosphere; and a connection pipe connecting the communication portion and the exhaust system at an intermediate position between the heat storage portion and the exhaust valve,
the fuel nozzle is cooled by the atmospheric air flowing through the opening toward the communicating portion by an exhaust suction action of the exhaust system via the connecting pipe in the exhaust mode, and is cooled by the combustion air bypassing the heat storage portion and flowing through the connecting pipe toward the opening via the communicating portion in the combustion mode by an air supply action of the air supply system.
5. The fuel nozzle cooling structure of the regenerative combustor according to claim 4,
the communication portion and the opening portion of the cooling pipe are formed on a base end portion side opposite to the fuel nozzle tip portion, and the cooling pipe includes: a first flow path that surrounds the periphery of the fuel nozzle, is formed from a distal end side to a proximal end side in a longitudinal direction thereof, and communicates with the communication portion; a second flow path that surrounds the periphery of the first flow path, is formed from a distal end side to a proximal end side in a longitudinal direction of the fuel nozzle, and communicates with the opening; and a connection flow path that connects the first flow path and the second flow path on a front end side of the fuel nozzle.
6. The fuel nozzle cooling structure of the regenerative combustor according to claim 4 or 5,
the fuel nozzle cooling structure of the heat accumulation burner includes a pair of the heat accumulation burners operated in an exhaust mode when one of the heat accumulation burners is in a combustion mode, and the exhaust systems of the heat accumulation burners are joined to each other at a junction portion, and a single exhaust blower is provided downstream of the junction portion.
CN201711212217.9A 2017-02-14 2017-11-27 Fuel nozzle cooling structure of heat accumulation combustor Active CN108426247B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2017-024772 2017-02-14
JP2017024772A JP6483169B2 (en) 2017-02-14 2017-02-14 Regenerative burner fuel nozzle cooling structure

Publications (2)

Publication Number Publication Date
CN108426247A CN108426247A (en) 2018-08-21
CN108426247B true CN108426247B (en) 2020-09-01

Family

ID=63155804

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711212217.9A Active CN108426247B (en) 2017-02-14 2017-11-27 Fuel nozzle cooling structure of heat accumulation combustor

Country Status (4)

Country Link
JP (1) JP6483169B2 (en)
KR (1) KR102344215B1 (en)
CN (1) CN108426247B (en)
TW (1) TWI755441B (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN86104491A (en) * 1985-06-28 1986-12-31 中外炉工业株式会社 The combustion chamber
JPH08312910A (en) * 1995-05-23 1996-11-26 Daido Steel Co Ltd Cooling method of heat storage type radiant tube burner
JP2003185129A (en) * 2001-12-17 2003-07-03 Tokyo Gas Co Ltd Heat reserved combustion type flat frame burner
JP2003254509A (en) * 2002-03-04 2003-09-10 Chugai Ro Co Ltd Single end type heat accumulating radiant tube burner and its combustion method
RU2278325C1 (en) * 2004-12-14 2006-06-20 Общество С Ограниченной Ответственностью Научно-Производственная Фирма "Горелочный Центр" Method of heating furnaces
CN101749945A (en) * 2008-12-11 2010-06-23 中外炉工业株式会社 Combustion control method for regenerative-combustion heat treat furnace
CN101782326A (en) * 2009-01-16 2010-07-21 中外炉工业株式会社 Combustion control method for regenerative-combustion heating furnace
CN102636037A (en) * 2011-02-09 2012-08-15 中外炉工业株式会社 Energy recovery device

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0774693B2 (en) * 1992-11-02 1995-08-09 中外炉工業株式会社 Combustion control method for regenerative burner system
TW278124B (en) * 1994-10-14 1996-06-11 Toyota Motor Co Ltd
JP3590495B2 (en) 1996-12-26 2004-11-17 住友金属工業株式会社 Low NOx burner for high temperature air
JP2001182915A (en) * 1999-12-28 2001-07-06 Rozai Kogyo Kaisha Ltd Cooler of fuel nozzle tube of regenerative burner
JP3964270B2 (en) * 2002-06-18 2007-08-22 中外炉工業株式会社 Regenerative burner having an inert gas introduction path connected to a fuel supply path and its operating method
JP4405944B2 (en) * 2005-06-21 2010-01-27 中外炉工業株式会社 Regenerative burner installation furnace
JP6570836B2 (en) * 2015-01-19 2019-09-04 中外炉工業株式会社 Industrial furnace, energy-saving operation method of industrial furnace, and modification method of industrial furnace

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN86104491A (en) * 1985-06-28 1986-12-31 中外炉工业株式会社 The combustion chamber
JPH08312910A (en) * 1995-05-23 1996-11-26 Daido Steel Co Ltd Cooling method of heat storage type radiant tube burner
JP2003185129A (en) * 2001-12-17 2003-07-03 Tokyo Gas Co Ltd Heat reserved combustion type flat frame burner
JP2003254509A (en) * 2002-03-04 2003-09-10 Chugai Ro Co Ltd Single end type heat accumulating radiant tube burner and its combustion method
CN1442629A (en) * 2002-03-04 2003-09-17 中外炉工业株式会社 Single end heat storage type radiation pipe burner device and its burning method
RU2278325C1 (en) * 2004-12-14 2006-06-20 Общество С Ограниченной Ответственностью Научно-Производственная Фирма "Горелочный Центр" Method of heating furnaces
CN101749945A (en) * 2008-12-11 2010-06-23 中外炉工业株式会社 Combustion control method for regenerative-combustion heat treat furnace
CN101782326A (en) * 2009-01-16 2010-07-21 中外炉工业株式会社 Combustion control method for regenerative-combustion heating furnace
CN102636037A (en) * 2011-02-09 2012-08-15 中外炉工业株式会社 Energy recovery device

Also Published As

Publication number Publication date
KR20180093790A (en) 2018-08-22
TW201829964A (en) 2018-08-16
TWI755441B (en) 2022-02-21
JP6483169B2 (en) 2019-03-13
CN108426247A (en) 2018-08-21
KR102344215B1 (en) 2021-12-29
JP2018132222A (en) 2018-08-23

Similar Documents

Publication Publication Date Title
KR101568900B1 (en) Burner apparatus and combustion control method for burner apparatus
CN108426247B (en) Fuel nozzle cooling structure of heat accumulation combustor
KR101528807B1 (en) Super-low NOx eission combustion apparatus using coanda effect
TWI712762B (en) Burner device and heat treatment facility
JP4757596B2 (en) Thermal storage burner device and its operation method
JP2007101129A (en) Heat storage type burner device and its operation method
KR101107466B1 (en) Single end type regenerative radiant tube burner
JP4007835B2 (en) Thermal storage radiant tube combustion device
KR20190128548A (en) Recuperator and radiant tube type heating apparatus
JP2007278693A (en) Regenerative radiant tube combustion device
JP2768902B2 (en) Zonal flame burner
KR102065945B1 (en) Super-low NOx Emission Combustion Apparatus
KR101453859B1 (en) Super-low NOx Emission Combustion Apparatus Using Coanda Effect
TWI751217B (en) Regenerative burner device
JP4184304B2 (en) Direct fire type hot air generator
TWI746691B (en) Regenerative burner system
TW201740069A (en) Regenerative burner device
JP3320624B2 (en) Supply / exhaust guide device for radiant tube burner device
JPH06147464A (en) Method for controlling combution in heat accumulative type burner system
JPH06147462A (en) Method for contrtolling combution of heat accumulative burner system
JP2000266305A (en) Combustion method by means of collision and agitation
JP4126537B2 (en) Exhaust gas recirculation single heat storage burner
JP2001141233A (en) Regenerative burner system
JP2680982B2 (en) Method for purging residual oil in heat storage type oil burner system
JP6366281B2 (en) Thermal storage type alternating combustion device

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant