CN216619818U - Combustor subassembly and gas heater - Google Patents
Combustor subassembly and gas heater Download PDFInfo
- Publication number
- CN216619818U CN216619818U CN202121505420.7U CN202121505420U CN216619818U CN 216619818 U CN216619818 U CN 216619818U CN 202121505420 U CN202121505420 U CN 202121505420U CN 216619818 U CN216619818 U CN 216619818U
- Authority
- CN
- China
- Prior art keywords
- gas
- combustion chamber
- combustion
- air
- assembly
- 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
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract description 451
- 239000007789 gas Substances 0.000 claims abstract description 422
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 91
- 239000002737 fuel gas Substances 0.000 claims abstract description 35
- 238000002156 mixing Methods 0.000 claims description 25
- 230000001105 regulatory effect Effects 0.000 claims description 13
- 230000001276 controlling effect Effects 0.000 claims description 9
- MWUXSHHQAYIFBG-UHFFFAOYSA-N Nitric oxide Chemical compound O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 33
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 19
- 239000003546 flue gas Substances 0.000 description 18
- 230000000694 effects Effects 0.000 description 14
- 239000001301 oxygen Substances 0.000 description 11
- 229910052760 oxygen Inorganic materials 0.000 description 11
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 10
- 239000000446 fuel Substances 0.000 description 10
- 238000009826 distribution Methods 0.000 description 8
- 230000002093 peripheral effect Effects 0.000 description 8
- 239000003344 environmental pollutant Substances 0.000 description 7
- 238000002347 injection Methods 0.000 description 7
- 239000007924 injection Substances 0.000 description 7
- 231100000719 pollutant Toxicity 0.000 description 7
- 230000009471 action Effects 0.000 description 6
- 239000000376 reactant Substances 0.000 description 6
- 230000003247 decreasing effect Effects 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 4
- 239000000779 smoke Substances 0.000 description 4
- 239000000243 solution Substances 0.000 description 4
- 230000002269 spontaneous effect Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000003595 mist Substances 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000003032 molecular docking Methods 0.000 description 2
- 238000004321 preservation Methods 0.000 description 2
- 238000000197 pyrolysis Methods 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 230000036632 reaction speed Effects 0.000 description 2
- 238000003287 bathing Methods 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002912 waste gas Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery
Abstract
The utility model discloses a burner assembly and a gas water heater, wherein the burner assembly comprises: the combustion body is provided with a first combustion chamber and a second combustion chamber which are sequentially communicated; the premixer is communicated with the first combustion chamber and the second combustion chamber in sequence and is used for conveying mixed gas to the first combustion chamber and the second combustion chamber; the gas inlet assembly is provided with a gas inlet, a first gas outlet and a second gas outlet, the gas inlet of the gas inlet assembly is connected with gas, the first gas outlet of the gas inlet assembly is communicated with the gas inlet of the premixer, and the second gas outlet of the gas inlet assembly is communicated with the second combustion chamber; the air inlet assembly is used for respectively conveying fuel gas to the premixer and the first combustion chamber, and can control the flow rate of the fuel gas conveyed to the second combustion chamber.
Description
Technical Field
The utility model relates to the technical field of high-temperature air combustion, in particular to a burner assembly and a gas water heater.
Background
High temperature air combustion (high temperature air combustion) is called MILD and deep low oxygen dilution combustion, and is called a novel combustion mode for short, namely MILD combustion. The main characteristics of the combustion are: the chemical reaction mainly takes place in a high-temperature low-oxygen environment, the temperature of the reactants is higher than the autoignition temperature of the reactants, the maximum temperature rise in the combustion process is lower than the autoignition temperature of the reactants, and the volume fraction of oxygen is diluted by combustion products to an extremely low concentration, usually 3-10%. Compared with conventional combustion, in the combustion state, the pyrolysis of fuel is inhibited, the flame thickness is thickened, and the flame front surface disappears, so that the temperature of the whole hearth is very uniform during the combustion, and the emission of pollutants NOx and CO is greatly reduced.
Although high-temperature air combustion has the advantages, at present, it is difficult to meet the combustion conditions in the combustion gas water heater and generate a good combustion effect.
SUMMERY OF THE UTILITY MODEL
The main purpose of the present invention is to propose a burner assembly and a gas water heater aimed at reducing the emission of pollutants (CO and NOx) and reducing the noise of the gas water heater.
To achieve the above object, the present invention provides a burner assembly comprising:
the combustion device comprises a combustion main body, a first combustion chamber and a second combustion chamber, wherein the first combustion chamber and the second combustion chamber are sequentially communicated; the premixer is sequentially communicated with the first combustion chamber and the second combustion chamber and is used for conveying mixed gas to the first combustion chamber and the second combustion chamber; and (c) a second step of,
the gas inlet assembly is provided with a gas inlet, a first gas outlet and a second gas outlet, the gas inlet of the gas inlet assembly is connected with gas, the first gas outlet of the gas inlet assembly is communicated with the gas inlet of the premixer, and the second gas outlet of the gas inlet assembly is communicated with the second combustion chamber; wherein,
the air inlet assembly is used for respectively conveying fuel gas to the premixer and the first combustion chamber, and can control the flow rate of the fuel gas conveyed to the second combustion chamber.
Optionally, the air intake assembly comprises:
the gas pipeline is communicated with the gas inlet, the first gas outlet and the second gas outlet;
the first gas flow adjusting device is arranged on the gas pipeline and used for adjusting the gas flow output to the premixer and the second combustion chamber.
Optionally, the first gas flow regulating device comprises:
the gas valve is arranged between the gas inlet and the first gas outlet and/or the second gas outlet.
Optionally, the first gas flow regulating device further comprises:
the fuel gas proportional valve is arranged between the fuel gas valve and the premixer in series;
and/or the fuel gas proportional valve is arranged between the fuel gas valve and the second combustion chamber in series.
Optionally, the premixer comprises:
an air inlet and a gas inlet;
the first gas inlet of the Venturi tube is communicated with the first gas outlet of the first gas flow regulating device, and the second gas inlet of the Venturi tube is communicated with the air inlet;
and the mixing cavity is communicated with the Venturi tube, the first combustion chamber and the second combustion chamber.
Optionally, the premixer further comprises:
the fan is arranged between the air inlet and the Venturi tube in series;
or the fan is arranged in series between the venturi tube and the mixing cavity.
Optionally, the burner assembly further comprises:
and the flow dividing assembly is arranged between the premixer and the first combustion chamber and is used for dividing the air flow of the premixer and conveying the air flow to the first combustion chamber and the second combustion chamber respectively.
Optionally, the combustion body comprises:
a combustion case in which the first combustion chamber and the second combustion chamber are formed; and
the air inlet shell is covered on one side of the combustion shell and forms the mixing cavity with the combustion shell in an enclosing manner;
the combustion shell is provided with a first air inlet communicated with the mixing cavity and the first combustion chamber and a second air inlet communicated with the mixing cavity and the second combustion chamber.
Optionally, the number of the gas passages formed between the second gas outlet of the first gas flow regulating device and the second combustion chamber is multiple.
Optionally, the first combustion chamber is a preheat combustion chamber and the second combustion chamber is a high temperature air combustion chamber.
Optionally, the burner assembly further comprises:
and the electric control assembly is electrically connected with the air inlet assembly and used for controlling the air inlet assembly to respectively convey gas to the first combustion chamber and the second combustion chamber and controlling the flow rate of the gas conveyed to the second combustion chamber, so that the mixed gas is heated in the first combustion chamber to a preset target temperature, then conveyed to the second combustion chamber and subjected to high-temperature air combustion with the gas output to the second combustion chamber by the air inlet assembly.
The utility model also provides a gas water heater, which comprises the burner assembly.
Optionally, the gas water heater further comprises:
and one end of the heat exchanger is communicated with the cold water inlet pipe, the other end of the heat exchanger is communicated with the hot water outlet pipe, and the heat exchanger is used for absorbing heat generated by combustion of the first combustion chamber and the second combustion chamber of the burner assembly and exchanging the absorbed heat with water in the heat exchanger.
The gas inlet assembly is arranged, so that the gas inlet assembly divides the output gas into at least two gas flow paths to output under the gas shunting action of the gas inlet assembly, one gas flow path is output to the premixer, part of gas and air are mixed and then enter the first combustion chamber, high-temperature flue gas is formed after the combustion of the first combustion chamber, the other part of gas is directly injected into the second combustion chamber, the high-temperature flue gas formed by the combustion of the first combustion chamber is sucked by the high-speed gas injected into the second combustion chamber, and therefore the high-temperature air combustion is finally realized after the gas injected into the second combustion chamber is diluted with the preheated high-temperature air, and the emission of CO and NOx of the gas water heater is reduced. In the utility model, the air inlet assembly is used for completing high-temperature air combustion, after the mixed gas is properly distributed to the two-stage combustion chambers, the air inlet assembly can also output another path of fuel gas to the second combustion chamber, and more air can be preheated in the first combustion chamber under the condition of a certain air-fuel ratio, so that the air excess ratio of the first combustion chamber can be improved, namely more air participates in the combustion of the first combustion chamber and is directly heated, the preheating effect is favorably improved, a water heater is more easily in a high-temperature air combustion state, and the lower emission of NOx and CO is favorably realized.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
FIG. 1 is a schematic structural view of an embodiment of a burner assembly of the present invention;
FIG. 2 is a schematic structural view of another embodiment of a burner assembly of the present invention;
FIG. 3 is a schematic structural view of yet another embodiment of a burner assembly of the present invention;
FIG. 4 is a schematic structural view of yet another embodiment of a burner assembly according to the present invention;
FIG. 5 is a schematic structural view of yet another embodiment of a burner assembly according to the present invention;
FIG. 6 is a functional block diagram of one embodiment of the novel burner assembly of the present invention;
FIG. 7 is a functional block diagram of another embodiment of the novel burner assembly of the present invention;
FIG. 8 is a schematic view of a partially exploded view of the burner assembly of FIG. 1;
FIG. 9 is a partially exploded view of the housing of FIG. 1;
FIG. 10 is a schematic gas flow diagram of one embodiment of the burner assembly of the present invention.
The implementation, functional features and advantages of the objects of the present invention will be further explained with reference to the accompanying drawings.
The reference numbers illustrate:
Detailed Description
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 utility model aims to design a novel burner assembly by utilizing the combustion characteristic of high-temperature air and apply the novel burner assembly to a gas water heater, so that the gas water heater can effectively reduce the emission of pollutants (CO and NOx) and reduce the noise of the gas water heater.
Preheating the MILD intake air and increasing the speed of the MILD intake air are critical in order to create MILD combustion within the combustion chamber of the water heater. Therefore, how to distribute the gas to the two combustion chambers becomes a research direction for realizing high-temperature air combustion.
The utility model provides a burner assembly which is suitable for gas water heaters and related products and equipment such as gas wall-mounted furnaces and the like which use high-temperature hot water generated by gas combustion for household bathing, heating and the like.
As shown in fig. 1 to 10, in an embodiment of the present invention, the burner assembly includes:
a combustion body 100, the combustion body 100 having a first combustion chamber 20 and a second combustion chamber 30 which are communicated in sequence;
a premixer 200 sequentially communicating with the first combustion chamber 20 and the second combustion chamber 30, the premixer 200 being configured to deliver a mixture gas to the first combustion chamber 20 and the second combustion chamber 30; and the number of the first and second groups,
the intake assembly 300 is provided with a gas inlet 31a, a first gas outlet 31b and a second gas outlet 31c, the gas inlet 31a of the intake assembly 300 is connected with gas, the first gas outlet 31b of the intake assembly 300 is communicated with the gas inlet 31a of the premixer 200, and the second gas outlet 31c of the intake assembly 300 is communicated with the second combustion chamber 30; wherein,
the air intake assembly 300 is configured to deliver fuel gas to the premixer 200 and the first combustion chamber 20, respectively, and is capable of controlling the flow rate of the fuel gas delivered to the second combustion chamber 30.
It can be understood that the main features of high temperature air combustion are: the chemical reactions need to occur in a high temperature, low oxygen environment, with the reactants at a temperature above their auto-ignition temperature and the maximum temperature rise during combustion below their auto-ignition temperature, with the oxygen volume fraction being diluted to a very low concentration by the combustion products. Compared with conventional combustion, in the combustion state, the pyrolysis of fuel is inhibited, the flame thickness is thickened, and the flame front surface disappears, so that the temperature of the whole hearth is uniform, the combustion peak temperature is low, the noise is low, and the emission of pollutants NOx and CO is greatly reduced. However, achieving high temperature air combustion requires certain conditions: the oxygen concentration in most areas in the furnace is required to be ensured to be lower than a certain value, generally lower than 5% -10%, the gas is ensured to be fully combusted and uniformly combusted, the temperature is higher than the self-ignition point of the fuel, and the self-ignition is maintained. In addition, the following conditions are also achieved, and the high-temperature preheating of air and the matching of high-speed jet flow are the main modes for realizing high-temperature air combustion; the technical key of maintaining high-temperature air combustion is to entrain high-temperature flue gas and dilute combustion air jet flow, so that the scheme of the utility model can realize reasonable gas distribution for the two combustors and realize the purpose of stably performing high-temperature air combustion.
The combustion main body 100 includes a housing formed with the first combustion chamber 20 and the second combustion chamber 30, and in the present embodiment, the shape of the housing of the combustion main body 100 may be square, cylindrical, and the like, and may be selected and designed according to actual requirements, and is not particularly limited herein. The shell is also provided with a smoke outlet, and after the gas is burnt at high temperature in the second combustion chamber 30, the burnt heat is discharged through the smoke outlet, so that the heat can be exchanged with a heat exchanger of the gas water heater to realize the preparation of hot water. The gas water heater further comprises a preheating burner installed in the first combustion chamber 20; a heat exchanger located between the exhaust port and the second combustion chamber 30; the burner assembly further comprises an electric control assembly 500, and the gas water heater further comprises a water inlet pipe for introducing water into the gas water heater, a hot water outlet pipe for providing hot water to the outside, a smoke exhaust pipe connected with a smoke exhaust port, a gas inlet pipeline for connecting gas and an air inlet valve. Wherein the preheating burner is used for heating the gas of the MILD combustion chamber. The preheating burner may be a honeycomb structure effective to prevent backfire during combustion, for example, the gas water heater may further include an igniter for igniting the gas injected from the preheating burner. The gas water heater further includes an electric control assembly 500 for controlling the preheating burner to perform combustion operation when the gas water heater is started, and the gas and the air entering the first combustion chamber 20 are ignited and ignited by the preheating burner, so that the mixed gas mixed with the gas and the air is combusted to heat the air in the first combustion chamber 20, thereby forming high-temperature flue gas. It is understood that the air in the first combustion chamber 20 can be heated to the target temperature, i.e., the above-mentioned preset temperature, by controlling the heating temperature, so that the high-temperature preheating of the air is realized. After the high-temperature gas subjected to high-temperature preheating is sent into the second combustion chamber 30, the gas is sprayed into the second combustion chamber 30, the gas is combined with the high-temperature gas, and the high-temperature gas ignites the gas, so that MILD combustion is formed in the second combustion chamber 30. Wherein the first combustor 20 is a preheating combustor, and the second combustor 30 is a high temperature air combustor.
In order to improve the combustion efficiency of the burner assembly, one embodiment of the present invention is to mix air and gas when providing air and gas for the first combustion chamber 20 and the second combustion chamber 30, for example, the present invention is applied to a fully premixed gas water heater, the fully premixed burner assembly is installed in the first combustion chamber, the air is sucked by the fan 220 and mixed with the gas, and then the mixed gas of the gas and the air is injected into the first combustion chamber 20 and the second combustion chamber 30.
Another embodiment of the present invention is to provide unmixed gas through different pipelines, and the unmixed gas is applied to a strong pumping type gas water heater, wherein the gas is injected into the first combustion chamber 20 and the second combustion chamber 30, and the strong drum type gas can be sucked by the fan 220 and then injected into the combustion chambers respectively. The supply of air and gas to the first and second combustion chambers 20 and 30 is accomplished by piping, and thus, in a specific embodiment, the flow rate of gas and air in the piping is controlled by installing a control valve, such as a solenoid valve, on each piping to distribute the gas and air flowing into the first and second combustion chambers 20 and 30.
In the present embodiment, the gas delivered to the first combustion chamber 20 and the second combustion chamber 30 is taken as an example of a mixed gas, the premixer 200 has a gas inlet and an air inlet, and the premixer 200 mixes the gas received from the gas inlet and the air output from the air intake assembly 300 and outputs the mixture to the first combustion chamber 20 and the second combustion chamber 30, thereby completing the preheating combustion and the high-temperature air combustion.
In the present embodiment, the air intake assembly 300 is provided, so that in the operation process of the burner assembly, the air intake assembly 300 divides the introduced gas into two parts to respectively deliver the gas to the premixer 200 and the second combustion chamber 30, specifically, the air intake assembly 300 delivers a part of the gas to the premixer 200, so that the premixer 200 mixes the introduced gas with air and then delivers the mixed gas to the first combustion chamber 20 and the second combustion chamber 30, and the air intake assembly 300 delivers another part of the gas to the second combustion chamber 30.
In this way, when the gas is supplied to the first combustion chamber 20, preheating of the gas and all air required for combustion of the high temperature air is completed, so that when the gas is injected again into the second combustion chamber 30 through the intake assembly 300, more mixture gas can be combined with the gas in the second combustion chamber 30, and the excess air in the high temperature gas is high enough to ignite the gas. And forms a entrainment effect in the second combustion chamber 30 and forms a jet combustion zone and a flue gas recirculation zone in the second combustion chamber 30, so that part of the high temperature flue gas (flue gas rich in N2 and CO 2) circulates the diluted reactants inside the second combustion chamber 30.
The gas is added into the second combustion chamber 30 in two ways through the gas inlet assembly 300, wherein one way directly leads the gas into the second combustion chamber 30 through the gas inlet assembly 300, the other way leads the gas into the first combustion chamber 20 and the second combustion chamber 30 after being premixed with the gas through the premixer 200, and then most of the air required by the preheating combustion and the high-temperature air combustion is preheated through the first combustion chamber 20. When the mixed gas and the fuel gas are introduced into the second combustion chamber 30, the preheated air in the mixed gas is fully diluted by the mixed gas and the fuel gas introduced into the second combustion chamber 30, so that a lower oxygen concentration is formed, the combustion reaction speed is reduced, the higher temperature of the second combustion chamber 30 is maintained, the temperature is higher than the spontaneous combustion point of the fuel, spontaneous combustion is realized, and high-temperature air combustion is realized.
It should be noted that the target temperature of the high-temperature preheated air cannot be too low, and generally, the target temperature is controlled to 1200 ℃, so that when the high-temperature gas contacts with the fuel gas in the second combustion chamber 30, better automatic combustion is realized, and ignition are not required any more. Wherein, the target temperature can be achieved by controlling the heating time, controlling the ratio of the fuel gas and the air, performing heat preservation, increasing the residence time of the high-temperature gas in the first combustion chamber 20, and the like. The injection speed and the flow rate of the fuel gas delivered to the second combustion chamber 30 by the air intake assembly 300 can be adjusted according to the requirement, specifically, the injection speed and the flow rate can be adjusted according to the preset temperature, the ambient temperature, the water intake flow rate, the water outlet temperature, the ambient pressure, and the like, and the adjustment proportion and the adjustment process can be predetermined and set.
It can be understood that, when the fuel gas and the air are mixed in advance, the premixing device 200 may be used to realize that a part of the mixed gas flow enters the first combustion chamber 20 for combustion and preheating combustion; another part of the mixed gas is injected into the second combustion chamber 30 to be combusted. Because the mixed gas containing the fuel gas and the air is provided by the premixer 200, the mixed gas is ignited and combusted by the preheating combustor, high-temperature preheating air is realized, the mixed gas of the fuel gas and the air is conveyed to the second combustion chamber 30, and then the fuel gas is conveyed to the second combustion chamber 30 by the air inlet assembly 300, so that more air can be preheated in the first combustion chamber 20, thereby generating entrainment effect in the second combustion chamber 30, leading the high-temperature flue gas to flow back, realizing heat preservation on one hand, leading the temperature to be higher than the spontaneous combustion point of the fuel, leading the fuel gas in the combustion chamber to be capable of spontaneous combustion, on the other hand, leading the oxygen concentration to be lower than a certain value by entraining the jet flow, realizing uniform combustion, thus leading the high-temperature air combustion in the combustion chamber to be realized, meeting the MILD combustion requirement and reducing the emission of CO and NOx. In order to achieve better preheating of the air and the fuel gas, different air excess coefficients, that is, air excess coefficients, may be set for the first combustion chamber 20 and the second combustion chamber 30, in this embodiment, the fuel gas is provided to the second combustion chamber 30 at least in two portions, and the air flowing to the first combustion chamber 20 and the second combustion chamber 30 is provided entirely through the premixer 200, so that more air can be preheated by the preheating burner in the first combustion chamber 20, that is, the air excess coefficient of the first combustion chamber 20 is higher than that of the second combustion chamber 30, so that more air participates in the combustion in the first combustion chamber 20 and is directly heated, and the preheating effect can be improved. The technical scheme of this embodiment is favorable to reaching above-mentioned two conditions that need satisfy that realize MILD burning simultaneously, realizes the high temperature air burning smoothly. And, the structure of this kind of combustor subassembly frame can be with the subassembly miniaturization that realizes the high temperature air burning for have more application space and value, the noise is low in addition, and the burning is abundant, and it is little to discharge waste gas pollution, when being applied to gas heater and including using gas combustion such as gas hanging stove to produce high temperature hot water and carry out relevant products and equipment that use such as family's shower and heating, not only satisfied the requirement, but also brought the abundant, the low pollutant of burning that the combustor subassembly did not possess in the current water heater effect.
In the embodiment, the gas inlet assembly 300 is arranged, so that the gas inlet assembly 300 divides the output gas into at least two gas flow paths to output, one gas flow path is output to the premixer 200, a part of gas and air are mixed and then enter the first combustion chamber 20, high-temperature flue gas is formed after the combustion in the first combustion chamber 20, the other part of gas is directly sprayed into the second combustion chamber 30, the high-temperature flue gas formed by the combustion in the first combustion chamber 20 is sucked by the high-speed gas sprayed into the second combustion chamber 30, and therefore, after the gas sprayed into the second combustion chamber 30 is diluted with the preheated high-temperature air, the combustion of the high-temperature air is finally realized, and the emission of CO and NOx of the gas water heater is reduced. In the utility model, the air intake assembly 300 is used for completing high-temperature air combustion, after the mixed gas is properly distributed to the two-stage combustion chambers, the air intake assembly 300 can also output another path of fuel gas to the second combustion chamber 30, and more air can be preheated in the first combustion chamber 20 under the condition of a certain air-fuel ratio, so that the excess air ratio of the first combustion chamber 20 can be improved, namely more air participates in the combustion of the first combustion chamber 20 and is directly heated, the preheating effect is improved, the water heater can enter a high-temperature air combustion state more easily, and the lower emission of NOx and CO is favorably achieved.
As shown in fig. 6 and 7, in one embodiment, the intake assembly 300 includes:
a gas pipeline 310 communicating the gas inlet 31a, the first gas outlet 31b and the second gas outlet 31 c;
the first gas flow regulating device 320 is disposed on the gas pipeline 310, and the first gas flow regulating device 320 is configured to regulate gas flow output to the premixer 200 and the second combustion chamber 30.
In this embodiment, the premixer 200 is communicated with the air inlet assembly 300 through a pipeline, an air inlet channel is further formed in the combustion main body 100, the mixing channel is sequentially communicated with the premixer 200, the gas channel and the air inlet channel, and the first gas flow rate adjusting device 320 can adjust the gas flow rate output to the premixer 200 and the second combustion chamber 30. Specifically, the first gas flow adjusting device 320 may control on/off of the gas output to the premixer 200 and the second combustion chamber 30, may also adjust the gas flow output to the premixer 200 and the second combustion chamber 30, may also adjust the gas ratio output to the premixer 200 and the second combustion chamber 30, and may be specifically set according to actual requirements, which is not limited herein. The air excess ratio of the first combustion chamber 20 can be adjusted by the first gas flow adjusting device 320, so that the air and the gas can be well preheated under the condition that the air-fuel ratio is not changed, and the air and the gas can be better in a high-temperature air combustion state.
As shown in fig. 6 and 7, in an embodiment, the first gas flow regulating device 320 includes:
a gas valve 321, the gas valve 321 being disposed between the gas inlet 31a and the first and second gas outlets 31b and 31 c;
a gas proportional valve 322, wherein the gas proportional valve 322 is arranged in series between the gas valve 321 and the premixer 200;
and/or the fuel gas proportional valve 322 is arranged between the fuel gas valve 321 and the second combustion chamber 30 in series.
In this embodiment, the gas valve 321 and the gas proportional valve 322 are respectively located in the main path and the branch 2 of the gas. Specifically, the gas proportional valve 322 is disposed in series between the gas valve 321 and the premixer 200, or between the gas valve 321 and the second combustion chamber 30, and the opening degree of the gas proportional valve 322 can be adjusted at different thermal loads, so as to achieve different excess air coefficients and achieve the optimal effect. The gas valve 321 may be an electromagnetic valve having only an open/close type, or may be a gas proportional valve 322 having a different opening degree. In other embodiments, of course, the gas proportional valve 322 may be replaced by an electromagnetic valve having only an open-close type, so as to achieve the purposes of higher excess air coefficient and good preheating effect of the first combustion chamber 20; the electromagnetic valve of the main circuit can be replaced by a proportional valve. Of course, in other embodiments, two valves may be disposed in any two of the main line (on the gas inlet 31 a), the branch line 1 (the line between the gas valve 321 and the premixer 200), and the branch line 2 (the line between the gas valve 321 and the second combustion chamber 30). For example, the gas valves 321 are respectively arranged between the branch 1 and the branch 2, that is, the gas valves 321 are arranged between the gas inlet 31a and the first gas outlet 31 b; the gas proportional valve 322 is disposed in series between the gas inlet 31a and the second combustion chamber 30.
In the present embodiment, the gas valve 321 is disposed between the gas inlet 31a and the first and second gas outlets 31b and 31c, and the gas proportional valve 322 is disposed in series between the gas valve 321 and the second combustion chamber 30, and the opening degree of the gas valve 321 is adjustable, so that the gas flow rate delivered to the first and second combustion chambers 20 and 30 can be adjusted by adjusting the opening degree of the gas valve 321, for example, when the opening degree of the gas valve 321 is increased, the gas output to the premixer 200 and the second combustion chamber 30 is increased. Conversely, if the opening degree of the gas valve 321 is decreased, the amount of gas output to the premixer 200 and the second combustor 30 is decreased. The gas flow rate ratio outputted to the premixer 200 and the second combustion chamber 30 can be adjusted by adjusting the opening degree of the gas proportional valve 322, for example, when the gas proportional valve 322 is disposed between the gas valve 321 and the second combustion chamber 30, the opening degree of the gas proportional valve 322 is increased, the gas proportion outputted to the second combustion chamber 30 is increased, and the gas proportion outputted to the premixer 200 is decreased. Conversely, when the opening degree of the gas proportional valve 322 is decreased, the proportion of the gas output to the second combustion chamber 30 is decreased, and the proportion of the gas output to the premixer 200 is increased. Similarly, when the gas proportional valve 322 is disposed between the gas valve 321 and the premixer 200, the gas proportion of the premixer 200 and the second combustion chamber 30 can also be adjusted. In this way, it is possible to ensure that the air flow rates output to the first combustion chamber 20 and the second combustion chamber 30 can satisfy the demand for the warm-up combustion in the first combustion chamber 20 and the high-temperature air combustion in the second combustion chamber 30, and the air excess ratio in the first combustion chamber 20 is increased.
As shown in fig. 6 and 7, in one embodiment, the premixer 200 includes:
an air inlet and a gas inlet;
a venturi tube 210, a first air inlet of the venturi tube 210 communicating with the first gas outlet 31b of the first gas flow regulating device 320, a second air inlet of the venturi tube 210 communicating with the air inlet;
a mixing chamber 10, wherein the mixing chamber 10 communicates the venturi 210 with the first combustion chamber 20 and the second combustion chamber 30.
In this embodiment, the burner assembly may further be provided with an air pipe, the venturi 210 is located between the air pipe and the gas pipe 310 and the mixing chamber 10, and the venturi 210, the air pipe and the gas inlet pipe together form the premixer 200 communicating with the mixing chamber 10. Air may enter the venturi 210 from the air inlet of the air line and form a vortex of air at the outlet of the venturi 210. But the gas that the air vortex was inhaled by the gas intake pipe entrainment to make gas and air carry out the intensive mixing in venturi 210, the gas of intensive mixing like this and the mist of air can realize abundant burning in gas heater, thereby can improve combustion efficiency, and can reduce the production of harmful substance such as nitrogen oxide (NOx) and carbon monoxide. In the present embodiment, the venturi 210 communicates with the air inlet and the mixing chamber 10 to output the mixed gas to the first and second combustion chambers 20 and 30.
As shown in fig. 6 and 7, in one embodiment, the premixer 200 further includes:
a fan 220, the fan 220 being arranged in series between the air inlet and the venturi 210;
alternatively, the fan 220 is disposed in series between the venturi 210 and the mixing chamber 10.
In this embodiment, gas and air can advance into the venturi structure, and the mist reentrants fan 220 mixes, consequently this fan 220 need use explosion-proof fan 220 for the air gas has better mixed effect. Alternatively, the blower 220 may be positioned before the venturi device, and the blower 220 may draw air into the venturi 210 through the blower 220 using a common blower 220 to complete the mixing of the air and the gas in the venturi 210. The fan 220 adjusts the rotation speed to provide air or mixed gas with corresponding flow for the burner assembly under different working conditions, such as different heat load requirements, based on the control of the electric control assembly 500, so as to complete high-temperature air combustion.
As shown in fig. 6 and 7, in one embodiment, the burner assembly further comprises:
and a flow dividing assembly 400 disposed between the premixer 200 and the first combustion chamber 20, wherein the flow dividing assembly 400 is configured to divide the flow of the premixer 200 and deliver the flow to the first combustion chamber 20 and the second combustion chamber 30, respectively.
In the present embodiment, under the shunting action of the shunting assembly 400, a part of the gas enters the first combustion chamber 20 through the shunting assembly 400 for combustion; another portion of the gas is blocked by the flow splitting assembly 400 and is injected downward into the second combustion chamber 30 for combustion from a two-sided turbulent flow. Thus, in the process of the operation of the burner assembly, as the mixed gas containing the gas and the air is provided by the premixer 200, the preheating burner ignites and burns the mixed gas, high-temperature preheated air is realized, the flow dividing assembly 400 divides the gas delivered by the mixing cavity 10 to deliver the gas to the first combustion chamber 20 and the second combustion chamber 30 respectively, so as to complete the preheating of the gas and the air when delivering the gas to the first combustion chamber 20, and when injecting the gas to the second combustion chamber 30, the gas and the high-temperature gas can be combined, so that the high-temperature gas ignites the gas, and a entrainment effect is formed in the second combustion chamber 30, so that an injection combustion area and a flue gas recirculation area are formed in the second combustion chamber 30, part of the high-temperature flue gas circulates and dilutes the reactant in the second combustion chamber 30, and then the injected gas and the air are sufficiently diluted, lower oxygen concentration is formed, the combustion reaction speed is reduced, the higher temperature of the second combustion chamber 30 is maintained, the temperature is higher than the self-ignition point of fuel, the self-ignition is realized, the oxygen concentration can be lower than a certain value through the shunting of the shunting assembly 400, the uniform combustion is realized, and the high-temperature air combustion is realized. The electronic control assembly 500 may also control the preheat burner to cease operation when the MILD burner assembly temperature reaches above the MILD combustion light-off temperature while MILD combustion is occurring.
Referring to fig. 8-10, in one embodiment, the flow diversion assembly 400 includes:
a flow divider 410 including a baffle 411 disposed between the air intake chamber 10 and the first combustion chamber 20, wherein the baffle 411 is provided with a plurality of air holes 411a to form a first flow path for the gas in the air intake chamber 10 to flow into the first combustion chamber 20;
a second flow path for the gas in the intake chamber 10 to flow into the second combustion chamber 30 is formed between the side edge of the baffle 411 and the chamber wall of the intake chamber 10.
In this embodiment, as shown in fig. 5, a dashed line in fig. 5 indicates that the gas flowing out from the intake chamber 10 forms at least two flow paths under the action of the baffle 411, the baffle 411 may extend into the intake chamber 10, a gap is formed between the baffle 411 and the wall of the intake chamber 10, an air hole 411a is arranged in the middle of the baffle 411 or at a position corresponding to the first combustion chamber 20, and the gas output from the intake chamber 10 flows into the first combustion chamber 20 under the action of the air hole 411a to provide the air and the fuel gas required for preheating combustion for the first combustion chamber 20. A gas flow path which at least flows into the second combustion chamber 30 is defined between the side edge of the baffle 411 and the cavity wall of the air inlet cavity 10, and under the turbulent flow action of the baffle 411, the gas flows into the second combustion chamber 30 through a second flow path which is formed between the side edge of the baffle 411 and the cavity wall of the air inlet cavity 10, so that air and fuel gas which are required by high-temperature air combustion are provided for the second combustion. The number, position and aperture of the air holes 411a of the baffle 411, the area of the baffle 411, and the like may be set according to the type of the gas water heater to be used, so as to adjust the distribution of the gas flow rates flowing to the first combustion chamber 20 and the second combustion chamber 30, thereby achieving the MILD combustion state.
Referring to fig. 8 and 9, in an embodiment, a plurality of side plates 412 surround a side of the baffle 411 facing the intake chamber 10.
In this embodiment, the plurality of plates are disposed on one side of the baffle 411 facing the intake chamber 10, that is, on the side facing away from the first combustion chamber 20, the number of the side plates 412 may be two or four, when two side plates are disposed, two side plates 412 are disposed on two opposite sides of the side of the baffle 411, and when four side plates are disposed, four side plates 412 are disposed on four sides of the baffle 411. The height of the baffle 411 is adjustable, and the flow rate of the gas flowing into the second combustion chamber 30 is smaller as the height of the baffle 411 is higher, and the flow rate of the gas flowing into the second combustion chamber 30 is larger as the height of the baffle 411 is lower, so that the gas flow rate distribution ratio to the first combustion chamber 20 and the second combustion chamber 30 can be adjusted.
Referring to fig. 8 and 9, in an embodiment, the flow diversion assembly 400 further comprises:
a spoiler 420 disposed between the flow splitter 410 and the first combustion chamber 20 to disturb gas flowing into the first combustion chamber 20.
Specifically, the spoiler 420 is a porous spoiler, a plurality of spoiler through holes are formed in the porous spoiler, and the diameters of the spoiler through holes are smaller than the diameters of the air holes 411a of the splitter 410.
In this embodiment, the spoiler 420 may be implemented by a multi-hole spoiler or a comb-shaped structure, and in this embodiment, the spoiler 420 is selected to be a multi-hole spoiler, so that the gas flowing into the first combustion chamber 20 is more uniform, thereby ensuring that the gas can be uniformly mixed with the mixed gas and air in each region of the first combustion chamber 20. The aperture of the turbulent flow through hole is smaller than the aperture of the air hole 411a of the flow divider 410, the ratio of the aperture of the turbulent flow through hole to the aperture of the flow divider 410 is adjustable, and the distribution ratio of the gas flow to the first combustion chamber 20 and the second combustion chamber 30 can be adjusted by adjusting the aperture of the multi-hole turbulent flow plate. When the aperture of the turbulent flow through hole is larger, the flow rate of the gas flowing into the first combustion chamber 20 is larger, so that the gas is more uniform, and the velocity of the flow velocity of the gas flowing into the first combustion chamber 20 can be faster. When the aperture of the turbulent flow through hole is smaller, the gas flowing into the first combustion chamber 20 is more uniform, the speed of the gas flowing to the first combustion chamber 20 is also blocked, and the residence time of the gas in the gas inlet chamber is increased, so that more gas flows to the second combustion chamber 30. Wherein, the air hole 411a and the spoiler through hole of the splitter 410 can be set as circular through holes, or square through holes, or bar-shaped through holes, and the air hole 411a and the spoiler through hole of the splitter 410 can be set as the same or different.
Referring to fig. 8 and 9, in an embodiment, the burner assembly further comprises:
and a preheating burner mounted to the first combustion chamber 20 formed in the main body, for delivering the ignited mixture gas to the first combustion chamber 20 of the burner assembly 100 and preheating the first combustion chamber 20 to a target temperature. Wherein, the preheating combustor includes: a porous medium 430 disposed between the spoiler 300 and the first combustion chamber 20.
In this embodiment, a porous medium 430 combustion mode is adopted, the porous medium 430 is filled in the first combustion chamber 20, the heat exchange tube directly exchanges heat with the high-temperature porous medium 430 in the combustion chamber in a radiation and heat conduction manner, strong heat exchange is realized between the heat exchange tube at the periphery of the high-temperature flue gas and the porous medium 430, and the flue gas can be rapidly cooled to directly condense water vapor on the tube wall, so that heat exchange between the flue gas and water is facilitated, the exhaust gas temperature of the combustion chamber is greatly reduced, latent heat of the water vapor in the flue gas can be collected, and the heat efficiency is improved. The porous medium 430 may be a porous medium 430 material made of metal fibers, and has good heat conductivity and mechanical strength, which is beneficial to heat return, combustion space reduction and combustion strength and heat exchange strength enhancement.
As shown in fig. 3, 5, and 9, in one embodiment, the combustion body 100 includes:
a combustion case 110 in which the first combustion chamber 20 and the second combustion chamber 30 are formed; and
the air inlet shell 120 is covered on one side of the combustion shell 110, and the air inlet shell 120 and the combustion shell 110 enclose to form the mixing chamber 10;
the combustion housing 110 is provided with a first air inlet communicating the mixing chamber 10 and the first combustion chamber 20 and a second air inlet communicating the mixing chamber 10 and the second combustion chamber 30.
In this embodiment, the air inlet housing 120 may be a housing of the premixer 200, the premixer 200 may be fitted into the air inlet housing 120, or the air inlet housing 120 may also be formed as a gas distribution chamber. The combustion housing 110 forms the first combustion chamber 20 and the second combustion chamber 30, and simultaneously, the heat exchanger of the gas water heater can also be assembled in the combustion housing 110, and the combustion housing 110 and the air inlet housing 120 can be directly and fixedly connected through screws, buckles and the like. Under the shunting action of the shunting assembly 400, the gas in the mixing chamber 10 flows to the first air inlet and the second air inlet respectively, so that the air and the gas required for preheating combustion are provided to the first combustion chamber 20 through the first air inlet, and the air and the gas required for high-temperature air combustion are improved to the second combustion chamber 30 through the second air inlet.
As shown in fig. 8 and 9, in one embodiment, the combustion casing 110 includes:
a frame portion 111 having a first side and a second side opposite to each other, wherein the first combustion chamber 20 and the second combustion chamber 30 are sequentially disposed from the first side to the second side, the first side of the frame portion 111 is a frame opening, and at least one side frame of the frame portion 111 is provided with a gas connector 1114; and
a fixing plate 112, wherein the fixing plate 112 is covered on a first side of the housing 111, and the air inlet housing 120 is covered on a side of the fixing plate 112 facing away from the housing 111; the first gas inlet 121a is disposed at a position of the fixing plate 112 corresponding to the first combustion chamber 20, the second gas inlet 121b is disposed at a position of the fixing plate 112 corresponding to the gas connector 1114, and the gas connector 1114 is communicated with the gas inlet cavity 10 and the second combustion chamber 30.
In this embodiment, the first side of the housing 111 is fixedly connected to the air intake housing 120, the fixing plate 112 is sandwiched between the housing 111 and the air intake housing 120, the housing 111 may be provided with a screw hole, the air intake housing 120 and the fixing plate 112 are provided with a through hole at corresponding positions, and a screw passes through the through holes of the air intake housing 120 and the fixing plate 112 and is installed in the screw hole of the housing 111, so that the air intake housing 120, the fixing plate 112 and the housing 111 are fixed by the screw. The fixing plate 112 is covered on the frame opening, and at least two air inlets, that is, a first air inlet 121a and a second air inlet 121b, are disposed on the fixing plate 112, and further, a mounting portion is formed by protruding the fixing plate 112 to the first combustion chamber 20 corresponding to the peripheral edge of the first air inlet 121a, so that the spoiler 420 and the porous medium 430 are fixedly mounted. The size of the mounting portion, that is, the aperture of the first air inlet 121a, may be set according to the areas of the spoiler 420 and the porous medium 430.
As shown in fig. 8 and 9, in an embodiment, the housing portion 111 includes a first end cover 1111, a second end cover 1112 and a peripheral side plate 1113 connecting the first end cover 1111 and the second end cover 1112, the first end cover 1111 forms a first water chamber 111a therein, the second end cover 1112 forms a second water chamber 111b therein, and the first water chamber 111a and the second water chamber 111b are connected in series with each other through at least one heat absorbing pipe 500 to form a series water circuit.
In this embodiment, the water passage may be formed by providing the heat absorbing pipe 500, or the water passage may be designed inside the combustion body 100. The water passage may be formed entirely by the passage in the heat absorbing pipe 500 or entirely by the passage in the combustion body 100. It is also possible to have the water running channel formed partly by the channel in the heat absorbing pipe 500 and partly by the channel in the combustion body 100. The flow path of the water passage may extend only along a part of the wall surface of the combustion body 100, may be provided around the peripheral wall surface of the combustion body 100, or may be provided around the wall surface of the combustion body 100 in a spiral shape or in multiple layers. The flow path of the water passage is not particularly limited, and can be selected and designed according to actual requirements. By forming the first water chamber 111a in the first end cap 1111 and the second water chamber 111b in the second end cap 1112 and forming the water passing channel by connecting the heat absorbing pipes 500 in series with each other, the heat of the combustion body 100 and the heat of the first and second combustion chambers 20 and 30 can be taken away by the water flowing in the water passing channel and the heat of the combustion body 100 can be absorbed by the water, so that the effect of absorbing the heat of the combustion body 100 and the combustion chamber 11 by the whole water passing channel is better. The heat absorbing pipe 500 may be a straight pipe extending along the length direction of the combustion body 100. Through making form first water cavity 111a in the first end cover 1111, form second water cavity 111b in the second end cover 1112, then when not influencing the result of use of end cover, make full use of the interior space of end cover for the water route flows through inside first end cover 1111 and the second end cover 1112, makes the holistic cooling area bigger. Moreover, the heat absorbing pipe 500 is located in the combustion chamber 11, so that the heat exchange rate between the heat absorbing pipe 500 and the airflow in the combustion chamber 11 can be improved, the temperature in the combustion chamber 11 can be sufficiently reduced, heat radiation to the outside of the burner assembly 100 can be prevented, and the generation of pollutants can be reduced. The heat absorbing pipe 500 is made of a material with high temperature resistance and good heat conductivity. The first end cover 1111 is defined by a first sub-end cover 1111a and a first sub-end cover 1111b, and the first sub-end cover 1111a and the second sub-end cover 1111b define a first water chamber 111 a. Similarly, the first end cap 1112 is enclosed by the second sub-end cap 1112a and the second sub-end cap 1112b, and the second sub-end cap 1112a and the second sub-end cap 1112b enclose to form the first water chamber 111 b.
As shown in fig. 8 and 9, in an embodiment, the number of the peripheral side plates 1113 is two, and the two peripheral side plates 1113 are arranged oppositely;
the two peripheral side plates 1113 are respectively provided with a communicating gas connector 1114.
In this embodiment, the mld intake cavities 10, i.e., the gas connectors 1114, are disposed on both the two peripheral side plates 1113, and the gas connectors 1114 and the combustion main body 100 may be integrally formed or may be separately formed. When the gas connector 1114 is separated from the combustion body 100, the gas connector and the combustion body can be fixedly connected by screws, welding, and the like. By forming the docking passage in the gas docking member 1114, gas output from the intake chamber 10 is enabled to flow from the second flow path formed by the flow divider assembly 400 and the wall of the intake chamber 10 into the second combustion chamber 30. The gas interface 1114 extends along the length of the combustion body 100. The gas connector 1114 has a tube body disposed facing one side of the gas inlet chamber 10 and having an opening (gas inlet 1114a), the gas inlet 1114a disposed facing the gas inlet chamber 10 is used for receiving the gas output from the gas inlet chamber 10, and at least one gas outlet on the other side of the tube body is communicated with the second combustion chamber 30. Two gas connectors 1114 are provided on both sides of the combustion body to deliver gas to the second combustion chamber 30 from both sides, which may make the gas flow into the second combustion chamber 30 more uniform. Of course, in other embodiments, the number of the gas connectors 1114 may be set to one, and is not limited herein.
As shown in fig. 8 and 9, in one embodiment, the gas connector 1114 is provided with a plurality of gas holes 1114b near one end of the second combustion chamber 30 for gas to flow into the second combustion chamber 30.
In this embodiment, after the gas that gets into from gas connection member 1114 is disturbed the flow by a plurality of gas holes 1114b, establish gas injection to second combustion chamber 30, the injection flow of a plurality of gas holes 1114b is more even, and can guarantee the gas velocity of flow that every gas hole 1114b sprays, and then realize that whole second combustion chamber 30's burning is more stable, in order to realize the entrainment high temperature flue gas and dilute, make second combustion chamber 30 gas and air misce bene, the oxygen concentration of second combustion chamber 30 also can be balanced like this, and be less than a definite value, not only the gas can obtain abundant burning during the burning, just so reduced the emission of pollutant, and, the gas also can the burning in the second combustion chamber 30 is even, the problem of local combustion too prosperous and noise production can not appear. In addition, the high-speed jet entrainment is realized through the gas holes 1114b on the two sides, the backflow of high-temperature flue gas is also realized, the temperature of the second combustion chamber 30 can be kept higher than the self-ignition point of fuel, and the combustion can be maintained as long as the gas is continuously introduced. The heat after combustion can exchange heat with the heat exchanger 50 of the gas water heater to realize the production of hot water. All set up gas through both sides on burning main part 100 width direction and plug into piece 1114, and make a plurality of gas holes 1114b of two gas plug into piece 1114 arrange in proper order on the length direction of burning main part 100, then can follow the relative both sides injection gas of burning main part 100 and/or air to the second combustion chamber 30 in, improve gas injection volume on the one hand, on the other hand makes the mist evenly distributed who is favorable to gas and air in the combustion chamber, combine to burn with high temperature air fully.
As shown in fig. 8 and 9, in an embodiment, a gap is formed between the flow divider 410 and the inner side wall of the intake housing 120, and the gap is a flow path for the gas in the intake chamber 10 to flow into the first combustion chamber 20 and the second combustion chamber 30.
A gap α is formed between the flow divider 410 and the fixed plate 112, and the gap is a flow path through which the gas in the intake chamber 10 flows into the first combustion chamber 20.
In this embodiment, the gap β formed between the flow divider 410 and the inner sidewall of the intake housing 120 is the second flow path, and the gap formed between the flow divider 410 and the fixing plate 112 is the flow path flowing into the first combustion chamber 20, that is, the gas output from the intake cavity 10 flows to the flow divider 410, and a part of the gas directly flows to the porous spoiler through the porous structure on the flow divider 410 and enters the first combustion chamber 20 through the porous medium 430 for combustion; another portion of the gas is blocked by the flow splitter 410, swirls downward from both sides, and is split again at the junction of the fixed plate 112 and the combustion housing 110, a portion flows toward the perforated spoiler and enters the first combustion chamber 20 through the porous medium 430 for combustion, and another portion is injected into the second combustion chamber 30 for combustion through the gas connector 1114, i.e., the MILD intake chamber 10. Of course, in other embodiments, the baffle 411 may not have the air holes 411a, and if there is no hole in the baffle, the gas is disturbed to the peripheral side of the baffle 411 directly after flowing from the inlet of the air intake chamber 10. The MILD combustion state can be achieved by adjusting the distribution of gas flow to the first and second combustion chambers 20, 30 by adjusting the size of the baffle 411, the number and distribution of the holes in the flow splitter 410, the distance α between the baffle and the intake housing 120, the distance β between the baffle and the fixed plate 112, and the size γ of the opening of the MILD intake chamber 10. The distance between the flow splitter 410 and the inner side wall of the air intake housing 120 is adjustable. The distance between the flow diverter 410 and the fixed plate 112 is adjustable.
In an embodiment, the baffle 411 may be driven by a driving member to move, so as to adjust a relative distance between the baffle 411 and the fixed plate 112, and adjust a relative distance α between the baffle 411 and the air intake housing 120, thereby adjusting the gap size and achieving distribution of the gas flow.
As shown in fig. 6 and 7, in an embodiment, the number of gas passages formed between the second gas outlet 31c of the first gas flow rate regulating device 320 and the second combustion chamber 30 is multiple.
In this embodiment, the first gas flow regulating device 320 is connected to the second combustion chamber 30 through a gas pipeline, and the number of the gas pipelines between the first gas flow regulating device 320 and the second combustion chamber 30 may be two or more. As shown in fig. 2, two gas pipelines, which are respectively labeled as 311 and 312, between the first gas flow regulator 320 and the second combustion chamber 30 are disposed at two opposite sides of the gas casing 110, so that the gas output to the second combustion chamber 30 is more uniform, which is beneficial to improving the combustion effect of high-temperature air combustion.
As shown in fig. 6 and 7, in one embodiment, the burner assembly further comprises:
and an electronic control assembly 500, where the electronic control assembly 500 is electrically connected to the air intake assembly 300, and is configured to control the air intake assembly 300 to respectively deliver air to the first combustion chamber 20 and the second combustion chamber 30, and control the flow rate of the gas delivered to the second combustion chamber 30, so that the mixed gas is heated to a preset target temperature in the first combustion chamber 20, then delivered to the second combustion chamber 30, and is subjected to high-temperature air combustion with the gas output by the air intake assembly 300 to the second combustion chamber 30.
In this embodiment, the electronic control assembly 500 includes an electronic control board, and a burner assembly control circuit disposed on the electronic control board, and the burner assembly control circuit can be realized by using a main controller, a gas valve driving circuit, a fan 220 driving circuit, a gas proportional valve driving circuit, etc., wherein the gas valve driving circuit, the fan driving circuit, and the gas proportional valve driving circuit can be realized by using a driving circuit composed of power tubes such as a relay, a MOS tube, and an IGBT. The main controller can receive control instructions input by a user through a wireless communication circuit, such as a Bluetooth module, an infrared induction circuit, a WIFI module and the like, and controls the work of the burner assembly according to the corresponding control instructions so as to meet the water demand of the user.
The utility model also provides a gas water heater. The gas water heater includes a burner assembly as described above. The detailed structure of the burner assembly can refer to the above embodiments, and is not described herein; it can be understood that, because the burner assembly is used in the gas water heater of the present invention, the embodiment of the gas water heater of the present invention includes all technical solutions of all embodiments of the burner assembly, and the achieved technical effects are also completely the same, and are not described herein again.
In one embodiment, the gas water heater further comprises:
and the heat exchanger (not shown) is communicated with a cold water inlet pipe at one end and a hot water outlet pipe at the other end, and is used for absorbing heat generated by combustion of the first combustion chamber 20 and the second combustion chamber 30 of the burner assembly and exchanging the absorbed heat with water in the heat exchanger.
In this embodiment, the cold water inlet pipe is used for introducing cold water to the gas water heater from the outside, and sending the cold water into the heat exchanger, the heat exchanger absorbs heat generated by combustion of the preheating burner and combustion of the MILD and heats the cold water into hot water, and the hot water is led out of the gas water heater through the hot water outlet pipe.
The above description is only an alternative embodiment of the present invention, and not intended to limit the scope of the present invention, and all modifications and equivalents of the technical solutions of the present invention that are made by using the contents of the specification and the drawings or directly/indirectly applied to other related technical fields are included in the scope of the present invention.
Claims (13)
1. A burner assembly, comprising:
the combustion device comprises a combustion main body, a first combustion chamber and a second combustion chamber, wherein the first combustion chamber and the second combustion chamber are sequentially communicated; the premixer is sequentially communicated with the first combustion chamber and the second combustion chamber and is used for conveying mixed gas to the first combustion chamber and the second combustion chamber; and the number of the first and second groups,
the gas inlet assembly is provided with a gas inlet, a first gas outlet and a second gas outlet, the gas inlet of the gas inlet assembly is connected with gas, the first gas outlet of the gas inlet assembly is communicated with the gas inlet of the premixer, and the second gas outlet of the gas inlet assembly is communicated with the second combustion chamber; wherein,
the air inlet assembly is used for respectively conveying fuel gas to the premixer and the second combustion chamber and can control the flow rate of the fuel gas.
2. The burner assembly of claim 1, wherein the air intake assembly comprises:
the gas pipeline is communicated with the gas inlet, the first gas outlet and the second gas outlet;
the first gas flow adjusting device is arranged on the gas pipeline and used for adjusting the gas flow output to the premixer and the second combustion chamber.
3. The burner assembly of claim 2, wherein the first gas flow regulating device comprises:
the gas valve is arranged between the gas inlet and the first gas outlet and/or the second gas outlet.
4. The burner assembly of claim 3, wherein the first gas flow adjustment device further comprises:
the fuel gas proportional valve is arranged between the fuel gas valve and the premixer in series;
and/or the fuel gas proportional valve is arranged between the fuel gas valve and the second combustion chamber in series.
5. The combustor assembly of claim 1, wherein the premixer comprises:
an air inlet and a gas inlet;
the first air inlet of the Venturi tube is communicated with the first fuel gas outlet, and the second air inlet of the Venturi tube is communicated with the air inlet;
and the mixing cavity is communicated with the Venturi tube, the first combustion chamber and the second combustion chamber.
6. The combustor assembly of claim 5, wherein the premixer further comprises:
the fan is arranged between the air inlet and the Venturi tube in series;
or the fan is arranged in series between the venturi tube and the mixing cavity.
7. The burner assembly of claim 1, further comprising:
and the flow dividing assembly is arranged between the premixer and the first combustion chamber and used for dividing the air flow of the premixer and conveying the air flow to the first combustion chamber and the second combustion chamber respectively.
8. The burner assembly of claim 5, wherein the combustion body comprises:
a combustion case in which the first combustion chamber and the second combustion chamber are formed; and
the air inlet shell is covered on one side of the combustion shell and forms the mixing cavity with the combustion shell in an enclosing manner;
the combustion shell is provided with a first air inlet communicated with the mixing cavity and the first combustion chamber and a second air inlet communicated with the mixing cavity and the second combustion chamber.
9. The burner assembly of claim 2, wherein the number of gas passages formed between the second gas outlet of the first gas flow regulating device and the second combustion chamber is multiplexed.
10. The burner assembly of claim 1 wherein the first combustion chamber is a preheat combustion chamber and the second combustion chamber is a high temperature air combustion chamber.
11. The burner assembly of any of claims 1-10, further comprising:
and the electric control assembly is electrically connected with the air inlet assembly and used for controlling the air inlet assembly to respectively convey gas to the first combustion chamber and the second combustion chamber and controlling the flow rate of the gas conveyed to the second combustion chamber, so that the mixed gas is heated in the first combustion chamber to a preset target temperature, then conveyed to the second combustion chamber and subjected to high-temperature air combustion with the gas output to the second combustion chamber by the air inlet assembly.
12. A gas water heater comprising a burner assembly as claimed in any one of claims 1 to 11.
13. The gas water heater of claim 12, further comprising:
and one end of the heat exchanger is communicated with the cold water inlet pipe, the other end of the heat exchanger is communicated with the hot water outlet pipe, and the heat exchanger is used for absorbing heat generated by combustion of the first combustion chamber and the second combustion chamber of the burner assembly and exchanging the absorbed heat with water in the heat exchanger.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202121505420.7U CN216619818U (en) | 2021-06-30 | 2021-06-30 | Combustor subassembly and gas heater |
PCT/CN2022/103047 WO2023274381A1 (en) | 2021-06-30 | 2022-06-30 | Combustor assembly and gas water heater device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202121505420.7U CN216619818U (en) | 2021-06-30 | 2021-06-30 | Combustor subassembly and gas heater |
Publications (1)
Publication Number | Publication Date |
---|---|
CN216619818U true CN216619818U (en) | 2022-05-27 |
Family
ID=81681323
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202121505420.7U Active CN216619818U (en) | 2021-06-30 | 2021-06-30 | Combustor subassembly and gas heater |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN216619818U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2023274377A1 (en) * | 2021-06-30 | 2023-01-05 | 芜湖美的厨卫电器制造有限公司 | Burner and gas water-heating device |
WO2023274381A1 (en) * | 2021-06-30 | 2023-01-05 | 芜湖美的厨卫电器制造有限公司 | Combustor assembly and gas water heater device |
-
2021
- 2021-06-30 CN CN202121505420.7U patent/CN216619818U/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2023274377A1 (en) * | 2021-06-30 | 2023-01-05 | 芜湖美的厨卫电器制造有限公司 | Burner and gas water-heating device |
WO2023274381A1 (en) * | 2021-06-30 | 2023-01-05 | 芜湖美的厨卫电器制造有限公司 | Combustor assembly and gas water heater device |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN112682781B (en) | Combustor and gas water heater | |
CN216619819U (en) | Combustor subassembly and gas hot water equipment | |
CN216619818U (en) | Combustor subassembly and gas heater | |
CN218033135U (en) | Thick and thin combustor and gas household appliance | |
CN214307646U (en) | Combustor and gas water heater | |
CN214120027U (en) | Combustor and gas equipment | |
CN115560325A (en) | Combustor and gas water heating equipment | |
CN215808461U (en) | Burner, combustion assembly, combustor and water heater | |
CN115560324A (en) | Combustor subassembly and gas heater | |
CN115560326A (en) | Combustor subassembly and gas hot water equipment | |
WO2023274381A1 (en) | Combustor assembly and gas water heater device | |
CN218787555U (en) | Combustor and gas water heating equipment | |
CN214275723U (en) | Premixing device, burner and gas equipment | |
CN114688532A (en) | Combustor and gas water heater | |
WO2023274377A1 (en) | Burner and gas water-heating device | |
CN114459029A (en) | Combustor and gas equipment | |
CN114087607B (en) | Premixing device and gas water heater | |
CN216619817U (en) | Combustor and water heater | |
CN113864773B (en) | Burner and gas water heater | |
CN215723199U (en) | Combustor and gas equipment | |
CN115560323A (en) | Combustor and gas water heater | |
CN114484434A (en) | Combustor and water heater | |
CN115560320A (en) | Combustor and gas water heater | |
CN114459025A (en) | Combustor and gas equipment | |
CN112682950A (en) | High-temperature air burner and gas water heater |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |