CN113357626A - Gas burner system and working method thereof - Google Patents

Gas burner system and working method thereof Download PDF

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Publication number
CN113357626A
CN113357626A CN202110778125.7A CN202110778125A CN113357626A CN 113357626 A CN113357626 A CN 113357626A CN 202110778125 A CN202110778125 A CN 202110778125A CN 113357626 A CN113357626 A CN 113357626A
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CN
China
Prior art keywords
air
cylinder
flue gas
gas
caliber
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CN202110778125.7A
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Chinese (zh)
Inventor
刘永才
陈令清
刘刚
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Shenzhen Jiayuntong Electronics Co Ltd
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Shenzhen Jiayuntong Electronics Co Ltd
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Priority to CN202110778125.7A priority Critical patent/CN113357626A/en
Publication of CN113357626A publication Critical patent/CN113357626A/en
Pending legal-status Critical Current

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    • 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 
    • F23C9/00Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
    • F23C9/006Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber the recirculation taking place in the combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F23D14/04Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
    • 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
    • F23D14/58Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
    • 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
    • F23D14/62Mixing devices; Mixing tubes
    • F23D14/64Mixing devices; Mixing tubes with injectors
    • 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
    • F23L1/00Passages or apertures for delivering primary air for combustion 
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23NREGULATING OR CONTROLLING COMBUSTION
    • F23N3/00Regulating air supply or draught
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2203/00Gaseous fuel burners
    • F23D2203/007Mixing tubes, air supply regulation

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

The invention discloses a gas burner system and a working method thereof. The gas burner system comprises: the device comprises an air supply channel, a flue gas backflow mixing cylinder, an inner cylinder, a bluff body, a 1 st fuel supply system and a 2 nd fuel supply system; the air supply duct comprises an air outlet cylinder; the flue gas backflow mixing cylinder is sleeved outside the air outlet cylinder, and a flue gas backflow channel is formed by a channel between the flue gas backflow mixing cylinder and the air outlet cylinder; the inner cylinder is sleeved in the air outlet cylinder, and an air nozzle is formed by a channel between the inner cylinder and the air outlet cylinder; the bluff body is arranged at the downstream of the inner cylinder; the 1 st fuel supply system is arranged in the air supply channel and comprises two groups of branch pipes which are respectively positioned inside and outside the inner cylinder, and the tail ends of the two groups of branch pipes are respectively connected with an inner support nozzle and an outer support nozzle; the 2 nd fuel supply system is arranged outside the air supply duct and comprises two groups of outer nozzles which spray fuel towards the center at different angles. The present invention mixes the fuel gas with the inert combustion products before combustion occurs, greatly reducing the peak temperature of the composition, thereby inhibiting the formation of NOx in industrial gas burners.

Description

Gas burner system and working method thereof
Technical Field
The invention relates to the technical field of burners, in particular to a gas burner system and a working method thereof.
Background
National environmental protection policy is becoming stricter and the requirement for boiler nitrogen oxide emission is becoming higher and higher. For combustion of fuel gases, the mechanism of formation of NOx is primarily of the thermodynamic type, i.e. when the flame temperature is high enough, the covalent bond of N2 is broken to obtain free N ions, which combine with oxygen atoms to form NOx.
Disclosure of Invention
It is a primary object of the present invention to provide a gas burner system and method of operation thereof for mixing gas with inert combustion products prior to combustion by technical means which substantially reduces the peak temperature of the composition and thereby inhibits NOx formation in industrial gas burners.
In order to achieve the purpose, the invention adopts the technical scheme that:
in a first aspect, there is provided a gas burner system comprising:
the air supply duct is composed of a large-caliber air duct, a reduced pipe with a contracted caliber and a small-caliber air outlet duct, wherein the large end of the reduced pipe is connected with the air duct, and the small end of the reduced pipe is connected with the air outlet duct;
the flue gas backflow mixing cylinder is sleeved outside the air outlet cylinder and consists of a backflow part with a contracted caliber, a throat part with a small caliber and a diffuser with an expanded caliber, the upstream of the throat part is connected with the outlet of the backflow part, and the downstream of the throat part is connected with the inlet of the diffuser; a flue gas backflow channel is formed by a channel between the flue gas backflow mixing cylinder and the air outlet cylinder;
the inner cylinder is hollow and is sleeved in the air outlet cylinder; a channel between the inner cylinder and the air outlet cylinder forms an air nozzle;
a bluff body disposed downstream of the inner barrel;
the 1 st fuel supply system is arranged in the air supply channel and comprises a main pipe and two groups of branch pipes connected to the downstream of the main pipe, wherein the two groups of branch pipes comprise an inner branch pipe entering the inner cylinder and an outer branch pipe entering the outer part of the inner cylinder and the inner part of the flue gas backflow mixing cylinder, the tail end of the inner branch pipe is connected with an inner branch nozzle, an injection pipe is sleeved outside the inner branch nozzle, and the tail end of the outer branch pipe is connected with an outer branch nozzle;
the 2 nd fuel supply system is arranged outside the air supply duct and comprises an air collecting bag, the air collecting bag is connected with a plurality of external nozzles through branch pipes, and the external nozzles at least partially surround the flue gas backflow mixing cylinder; the outer nozzles are divided into two groups, wherein the injection ports of the outer nozzles of the first group are oriented to inject fuel to the central direction at a first angle relative to the longitudinal axis of the air supply duct, the injection ports of the outer nozzles of the second group are oriented to inject fuel to the central direction at a second angle relative to the longitudinal axis of the air supply duct, and the first angle is not equal to the second angle.
Optionally, the inner cylinder is composed of a large-caliber straight cylinder section, a caliber-contracted necking section, a small-caliber throat and a caliber-expanded flaring section, the large end of the necking section is connected with the straight cylinder section, the small end of the necking section is connected with the small-caliber throat, and the outlet of the small-caliber throat is connected with the small end of the flaring section.
Optionally, the outlet of the air outlet cylinder is not more than the outlet of the backflow part.
Optionally, the position of the spray hole of the outer support nozzle exceeds the outlet of the throat part of the flue gas backflow mixing cylinder.
Optionally, the overall shape of the blunt body is wide in the front and narrow in the rear, and the wide end faces the inner cylinder.
Optionally, the blunt body is hollow, and the outer wall surface is streamlined.
Optionally, the ejection outlet direction of each ejection pipe and the longitudinal axis of the air supply duct form an angle which is radially outward, and the angle range is 0-80 degrees.
Optionally, two sets of external nozzles of the 2 nd fuel supply system surround the flue gas backflow mixing cylinder, the second set of external nozzles are arranged on the periphery of the first set of external nozzles, and the two sets of external nozzles are respectively and uniformly distributed outside the flue gas backflow mixing cylinder in the circumferential direction.
Optionally, the angle between the injection ports of the first group of outer nozzles of the 2 nd fuel supply system and the longitudinal axis of the air supply duct is 0-15 °; the jet ports of the second group of outer nozzles form an angle of 5-20 degrees with the longitudinal axis of the air supply duct.
In a second aspect, there is provided a method of operating a gas burner system as described above, the method comprising:
combustion air is supplied through an air supply duct, most of the combustion air passes through an air nozzle, and a small part of the combustion air passes through the inner barrel; high-speed combustion air passing through the air nozzle forms a low-pressure area in the flue gas backflow mixing cylinder to suck inert combustion products in the hearth through a flue gas backflow channel, and the combustion air and the inert combustion products are primarily mixed at the throat part of the backflow mixing cylinder;
a small part of required gas quantity is supplied through a 1 st fuel supply system, wherein a part of gas is sprayed into the injection pipe through an internal branch nozzle on the internal branch pipe, mixed with combustion-supporting air sucked from the inner cylinder and combusted in the injection pipe, and flame is sprayed out through an outlet of the injection pipe to form stable flame due to the blocking of a blunt body; wherein the other part of the fuel gas is sprayed into the flue gas backflow mixing cylinder through an outer support nozzle on an outer support pipe and is combusted with combustion air mixed with inert combustion products in a diffusion part of the backflow mixing cylinder;
and supplying most of the required gas quantity of the burner system through a 2 nd fuel supply system, wherein one part of gas is sprayed from the first group of external nozzles to the direction of the longitudinal axis of the gas burner system, the other part of gas is sprayed from the second group of external nozzles to the direction of the longitudinal axis of the gas burner system, and high-speed gas jet flow formed by spraying drives inert combustion products in a boiler furnace to follow and completes mixing before entering a combustion zone for combustion.
According to the technical scheme, the embodiment of the invention has the following advantages:
1. the mixing of air and inert combustion products in the smoke and the mixing of fuel gas and the inert combustion products are respectively completed before combustion, so that the flame peak value can be greatly reduced, the emission of nitrogen oxides is effectively reduced, and compared with the smoke external circulation technology, the performance of the combustor in the aspects of flame length, regulation ratio and stability is not sacrificed.
2. The central flame stabilizing zone adopts lean premixed combustion, so that the stability of combustion is ensured, the flame peak value can be reduced, and the generation of nitrogen oxides is effectively inhibited.
3. The invention may further provide a turndown ratio of 10:1 to 20: 1.
Drawings
In order to more clearly illustrate the technical solution of the embodiment of the present invention, the following briefly introduces the embodiment and the drawings used in the description of the prior art.
FIG. 1 is a cross-sectional view of a gas burner system provided by an embodiment of the present invention;
FIG. 2 is a perspective view of a gas burner system provided by an embodiment of the present invention;
FIG. 3 is a front view of a gas burner system provided by an embodiment of the present invention;
fig. 4 is a schematic diagram of the operation of a gas burner system according to an embodiment of the present invention.
Detailed Description
In order to make the technical solutions of the present invention better understood, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The terms "first," "second," "third," and the like in the description and in the claims, and in the above-described drawings, are used for distinguishing between different objects and not for describing a particular order. Furthermore, the terms "include" and "have," as well as any variations thereof, are intended to cover non-exclusive inclusions. In addition, the terms "inlet", "outlet", "upstream", "downstream" are defined in terms of the direction of gas flow.
The following are detailed descriptions of the respective embodiments.
Referring to fig. 1 to 4, an embodiment of the invention provides a gas burner system.
The gas burner system includes: an air supply duct 110, a flue gas reflux mixing cylinder 140, an inner cylinder 150, a bluff body 160, a 1 st fuel supply system 120, and a 2 nd fuel supply system 130.
The air supply duct 110 is composed of a large-caliber wind cylinder 111, a reduced pipe 112 with a contracted caliber and a small-caliber wind cylinder 113, wherein the large end of the reduced pipe 112 is connected with the wind cylinder 111, and the small end is connected with the wind cylinder 113.
The flue gas backflow mixing cylinder 140 is composed of a backflow part 141 with a contracted caliber, a throat part 142 with a small caliber and a diffuser 143 with an expanded caliber, the upstream of the throat part 142 is connected with the outlet of the backflow part 141, and the downstream of the throat part is connected with the inlet of the diffuser 143; the flue gas reflux mixing cylinder 140 is sleeved outside the air outlet cylinder 113 of the air supply duct 110; the outlet of the air outlet cylinder 113 does not exceed the outlet of the return part 141, and is preferably flush with the outlet of the return part 141; the channel formed between the flue gas reflux mixing cylinder 140 and the air outlet cylinder 113 of the air supply duct 110 is a flue gas reflux channel.
The inner cylinder 150 is composed of a large-caliber straight cylinder section 151, a caliber-contracted necking section 152, a small-caliber throat 153 and a caliber-expanded flaring section 154, wherein the large end of the necking section 152 is connected with the straight cylinder section 151, the small end of the necking section is connected with the small-caliber throat 153, and the outlet of the small-caliber throat 153 is connected with the small end of the flaring section 154. The inner cylinder 150 is hollow and sleeved in the air outlet cylinder 113 of the air supply duct 110, and the outlet of the inner cylinder exceeds the throat 142 of the flue gas reflux mixing cylinder 140. The passage between the inner cylinder 150 and the outlet cylinder 113 constitutes an air nozzle.
The bluff body 160 is wide in front and narrow in back, one wide end faces the inner cylinder 150, the middle of the bluff body is hollow, the outer wall surface is in a streamline shape similar to a wing, and the bluff body is placed at the downstream of the inner cylinder 150.
A 1 st fuel supply system 120, which is disposed inside the air supply duct 110, supplies fuel to the central flame, and is composed of a main pipe 121, two sets of branch pipes, and nozzles; downstream of the main pipe 121 there are connected two sets of branch pipes, 3 each, namely 3 inner branch pipes 122 and 3 outer branch pipes 124. The inner branch pipe 122 enters the inner cylinder 150, the outer branch pipe 124 enters the outer part of the inner cylinder 150 and the flue gas flows back into the mixing cylinder 140. The ends of the two groups of branch pipes are respectively connected with a nozzle, the end of the inner branch pipe 122 is connected with an inner support nozzle 123, and the end of the outer branch pipe 124 is connected with an outer support nozzle 125. The spray holes of the outer support nozzle 125 are positioned beyond the outlet of the throat 142 of the flue gas recirculation mixing drum 140 in a radially outward direction. Each inner support nozzle 123 is externally sleeved with an injection pipe 126, the side surface of each injection pipe 126 is provided with an opening for air inlet, the direction of the injection outlet of each injection pipe 126 and the longitudinal axis of the air supply duct 110 form a certain angle which is radially outward, the angle range is 0-80 degrees, the preferred angle range is 10-45 degrees, and the further preferred angle range is 15-30 degrees.
The 2 nd fuel supply system 130 is configured outside the air supply duct 110 and comprises an air collecting bag 131, a branch pipe 132 and two groups of external nozzles 133, wherein the air collecting bag 131 is connected with a series of external nozzles 133 arranged outside the flue gas backflow mixing cylinder 140 through the branch pipe 132, and the two groups of external nozzles are uniformly distributed outside the flue gas backflow mixing cylinder 140 in the circumferential direction. Among them, it is preferable that the second group of external nozzles 133b is at the periphery of the first group of external nozzles 133 a. The injection ports of the first set of outer nozzles 133a are oriented to inject fuel toward the center at a first angle with respect to the longitudinal axis of the air supply duct 110; the injection ports of the second set of outer nozzles 133b are oriented to inject fuel toward the center at a second angle with respect to the longitudinal axis of the air supply duct 110, the first angle being unequal to the second angle. The first angle is, for example, between 0-15, preferably between 0-10, and the second angle is, for example, between 5-20, preferably between 8-15, so that the two sets of outer nozzles 9133 are fired at different angles in a central direction.
The embodiment of the invention also provides a working method of the gas burner system, which comprises the following steps:
a) combustion air is supplied through the air supply duct 110, most of the combustion air (about 55-80% by volume) passes through the air nozzles, and a small part of the combustion air (about 20-45% by volume) passes through the inner cylinder 150; high-speed combustion air passing through the air nozzle forms a low-pressure area in the flue gas backflow mixing cylinder 140 to suck inert combustion products in the hearth through the flue gas backflow channel, and the combustion air and the inert combustion products are primarily mixed in the throat 142;
b) a small part (the volume ratio is about 15-40%) of the gas quantity required by the gas burner system is supplied through the 1 st fuel supply system 120, wherein a part (10-15%) of the gas is sprayed into the ejector pipe 126 through the inner branch nozzle 123 on the inner branch pipe 122, mixed with combustion-supporting air sucked from the inner cylinder 150 and combusted in the ejector pipe 126, and the flame is sprayed out through the outlet of the ejector pipe 126 to form stable flame due to the blocking of the blunt body 160; wherein another part of the fuel gas (the volume ratio is about 10-20%) is sprayed into the flue gas backflow mixing cylinder 140 through the outer nozzle 125 on the outer branch pipe 124 and is combusted with the air mixed with the inert combustion products in the diffuser 143 of the flue gas backflow mixing cylinder 140;
c) supplying a majority (about 60-85% by volume) of the amount of gas required by the gas burner system through the 2 nd fuel supply system 130, wherein a portion of the gas is injected from the first set of outer nozzles 133a at a first angle toward the main combustion zone and another portion of the gas is injected from the second set of outer nozzles 133b at a second angle toward the main combustion zone; these high velocity gas jets formed by the injection will cause the inert combustion products in the furnace to follow and mix with the combustion products prior to entering the combustion zone for combustion.
The nitrogen reduction principle of the gas burner system provided by the embodiment of the invention is as follows:
after the combustion air passes through the air nozzle at a high speed, a low-pressure area is formed in the flue gas backflow mixing cylinder 140, so that inert combustion products in the hearth are sucked through the flue gas backflow channel, and the combustion air and the inert combustion products are preliminarily mixed in the throat portion 142. The gas sprayed by the outer branch pipe 124 and the outer branch nozzle 125 and the combustion air mixed with inert combustion products are combusted in the diffusion part 143 of the flue gas backflow mixing cylinder 140, so that the flame peak value in the area can be greatly reduced, and the emission of nitrogen oxides can be effectively reduced.
The high-speed gas jet flow supplied by the No. 2 fuel supply system 130 can drive inert combustion products in the hearth to follow and mix with the inert combustion products before entering the main combustion zone for combustion, so that the flame peak value of the main combustion zone can be greatly reduced, and the emission of nitrogen oxides is effectively reduced.
The gas (about 10-15 vol.%) supplied through the inner branch pipe 122 is mixed with the combustion air (about 20-45 vol.%) sucked into the inner tube 150 for combustion, and the combustion of the central flame is lean premixed combustion, so that the combustion temperature is low.
To sum up, the embodiment of the invention discloses a gas burner system and a working method thereof. According to the technical scheme, the embodiment of the invention has the following advantages:
1. the mixing of air and inert combustion products in the smoke and the mixing of fuel gas and the inert combustion products are respectively completed before combustion, so that the flame peak value can be greatly reduced, the emission of nitrogen oxides is effectively reduced, and compared with the smoke external circulation technology, the performance of the combustor in the aspects of flame length, regulation ratio and stability is not sacrificed.
2. The central flame stabilizing zone adopts lean premixed combustion, so that the stability of combustion is ensured, the flame peak value can be reduced, and the generation of nitrogen oxides is effectively inhibited.
3. The invention may further provide a turndown ratio of 10:1 to 20: 1.
The technical solution of the present invention is explained in detail by the specific embodiments above. In the above embodiments, the descriptions of the respective embodiments have respective emphasis, and for parts that are not described in detail in a certain embodiment, reference may be made to the related descriptions of other embodiments.
It should be understood that the above embodiments are only used for illustrating the technical solutions of the present invention, and not for limiting the same. The technical solutions described in the above embodiments can be modified or part of the technical features can be equivalently replaced by those skilled in the art; and the modifications or the substitutions do not make the essence of the corresponding technical solutions depart from the spirit and the scope of the technical solutions of the embodiments of the present invention.

Claims (10)

1. A gas burner system, comprising:
the air supply duct (110) is composed of a large-caliber air duct (111), a reduced pipe (112) with a contracted caliber and a small-caliber air outlet duct (113), the large end of the reduced pipe (112) is connected with the air duct (111), and the small end of the reduced pipe is connected with the air outlet duct (113);
the flue gas backflow mixing cylinder (140) is sleeved outside the air outlet cylinder (113) and consists of a backflow part (141) with a contracted caliber, a throat part (142) with a small caliber and a diffuser (143) with an expanded caliber, the upstream of the throat part (142) is connected with the outlet of the backflow part (141), and the downstream of the throat part is connected with the inlet of the diffuser (143); a flue gas backflow channel is formed by a channel between the flue gas backflow mixing cylinder (140) and the air outlet cylinder (113);
the inner cylinder (150) is hollow and sleeved in the air outlet cylinder (113); a channel between the inner barrel (150) and the air outlet barrel (113) forms an air nozzle;
a bluff body (160) disposed downstream of the inner barrel (150);
the 1 st fuel supply system (120) is arranged in the air supply duct (110) and comprises a main pipe (121) and two groups of branch pipes connected to the downstream of the main pipe (121), the two groups of branch pipes comprise an inner branch pipe (122) entering the inner barrel (150) and an outer branch pipe (124) entering the outer part of the inner barrel (150) and the inner part of the flue gas backflow mixing barrel (140), the tail end of the inner branch pipe (122) is connected with an inner branch nozzle (123), an injection pipe (126) is sleeved outside the inner branch nozzle (123), and the tail end of the outer branch pipe (124) is connected with an outer branch nozzle (125);
the 2 nd fuel supply system (130) is arranged outside the air supply duct (110) and comprises an air collecting bag (131), the air collecting bag (131) is connected with a plurality of external nozzles (133) through branch pipes (132), and the external nozzles (133) at least partially surround the flue gas backflow mixing cylinder (140); the outer nozzles (133) are divided into two groups, wherein the injection ports of the outer nozzles (133a) of the first group are oriented to inject fuel towards the central direction at a first angle relative to the longitudinal axis of the air supply duct (110), and the injection ports of the outer nozzles (133b) of the second group are oriented to inject fuel towards the central direction at a second angle relative to the longitudinal axis of the air supply duct (110), and the first angle is not equal to the second angle.
2. The gas burner system of claim 1, wherein the inner barrel (150) is composed of a straight barrel section (151) with a large caliber, a reducing section (152) with a contracted caliber, a small caliber throat (153) and an expanding section (154) with an expanded caliber, the large end of the reducing section (152) is connected with the straight barrel section (151), the small end is connected with the small caliber throat (153), and the outlet of the small caliber throat (153) is connected with the small end of the expanding section (154).
3. Gas burner system according to claim 1, characterized in that the outlet of the chimney (113) does not exceed the outlet of the return (141).
4. The gas burner system of claim 1, wherein the outer support nozzle (125) has an orifice location beyond the exit of the throat (142) of the flue gas recirculation mixing drum (140).
5. The gas burner system of claim 1, wherein the bluff body (160) has an overall shape that is wide at the front and narrow at the back, with the wide end facing the inner barrel (150).
6. The gas burner system of claim 5, wherein the bluff body (160) is hollow and the outer wall surface is streamlined.
7. The gas burner system according to claim 1, wherein each of said injector pipes (126) has an injection outlet directed radially outwardly at an angle in the range of 0 ° to 80 ° to the longitudinal axis of said air supply duct (110).
8. The gas burner system according to claim 1, characterized in that the 2 nd fuel supply system (130) has two sets of external nozzles (130) all around the flue gas recirculation mixing drum (140), and a second set of external nozzles (133b) is arranged at the periphery of the first set of external nozzles (133a), and the two sets of external nozzles (130) are respectively circumferentially and uniformly distributed outside the flue gas recirculation mixing drum (140).
9. The gas burner system according to claim 1, wherein the injection ports of the first set of outer nozzles (133a) of the 2 nd fuel supply system (130) are at an angle of 0 ° -15 ° to the longitudinal axis of the air supply duct (110); the jet ports of the second group of outer nozzles (133b) form an angle of 5-20 degrees with the longitudinal axis of the air supply duct (110).
10. A method of operating a gas burner system as claimed in claim 1, characterized in that the method comprises:
combustion air is supplied through the air supply duct (110), most of the combustion air passes through the air nozzle, and a small part of the combustion air passes through the inner barrel (150); high-speed combustion air passing through the air nozzle forms a low-pressure area in the flue gas backflow mixing cylinder (140) to suck inert combustion products in the hearth through a flue gas backflow channel, and the combustion air and the inert combustion products are primarily mixed at the throat (142) of the backflow mixing cylinder (140);
a small part of the required gas quantity is supplied through a 1 st fuel supply system (120), wherein a part of the gas is sprayed into an ejector pipe (126) through an inner branch nozzle (123) on an inner branch pipe (122), mixed with combustion air sucked from an inner barrel (150) and combusted in the ejector pipe (126), and the flame is sprayed out through an outlet of the ejector pipe (126) to form stable flame due to the blockage of a blunt body (160); wherein another part of the fuel gas is sprayed into the flue gas backflow mixing cylinder (140) through an outer branch nozzle (125) on an outer branch pipe (124) and is combusted with combustion air mixed with inert combustion products in a diffusion part (143) of the backflow mixing cylinder (140);
most of the gas quantity required by the burner system is supplied through a 2 nd fuel supply system (130), wherein one part of gas is sprayed from a first group of external nozzles (133a) to the direction of the longitudinal axis of the gas burner system, the other part of gas is sprayed from a second group of external nozzles (133b) to the direction of the longitudinal axis of the gas burner system, and high-speed gas jet flows formed by spraying drive inert combustion products in a boiler furnace to follow and complete mixing before entering a combustion area for combustion.
CN202110778125.7A 2021-07-09 2021-07-09 Gas burner system and working method thereof Pending CN113357626A (en)

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CN202110778125.7A CN113357626A (en) 2021-07-09 2021-07-09 Gas burner system and working method thereof

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Application Number Priority Date Filing Date Title
CN202110778125.7A CN113357626A (en) 2021-07-09 2021-07-09 Gas burner system and working method thereof

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CN202110778125.7A Pending CN113357626A (en) 2021-07-09 2021-07-09 Gas burner system and working method thereof

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113757665A (en) * 2021-09-23 2021-12-07 深圳市佳运通电子有限公司 Gas burner system and working method thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113757665A (en) * 2021-09-23 2021-12-07 深圳市佳运通电子有限公司 Gas burner system and working method thereof

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