CN214147874U - Cylindrical atmospheric burner and gas water heating equipment - Google Patents
Cylindrical atmospheric burner and gas water heating equipment Download PDFInfo
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- CN214147874U CN214147874U CN202022178384.XU CN202022178384U CN214147874U CN 214147874 U CN214147874 U CN 214147874U CN 202022178384 U CN202022178384 U CN 202022178384U CN 214147874 U CN214147874 U CN 214147874U
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Abstract
The utility model relates to a tube-shape atmosphere formula combustor and gas hot water equipment, tube-shape atmosphere formula combustor include base, first ware body, first reposition of redundant personnel section of thick bamboo, second ware body and ejector. The base is provided with a first mixing cavity and a second mixing cavity at intervals. The first device body is arranged on the base, and the second device body is superposed on the first device body. Because the mist that lets in respectively in first mixing chamber and the second mixing chamber can flow from different height positions finally, consequently, effectively satisfies the demand that the different load of user burns, realizes the sectional combustion of combustor. The tubular atmospheric burner skillfully changes the flow direction of mixed airflow by arranging the first splitter barrel in the tubular atmospheric burner, realizes tubular layered combustion, and overcomes the problem of overhigh temperature rise of the whole water heater under small load. This tube-shape atmosphere formula combustor embeds a plurality of hybrid chambers and reposition of redundant personnel chamber, guarantees gas and air intensive mixing before flowing for flame burning is more stable, is favorable to promoting the user to experience the use of water heater complete machine.
Description
Technical Field
The utility model relates to a hot water equipment technical field especially relates to tube-shape atmosphere formula combustor and gas hot water equipment.
Background
The burner device is a device for burning gas and air mixture. According to different combustion forms, the burner can be divided into a fully premixed burner and an atmospheric burner. The full premix burner has a cylindrical shape, a plate shape, a fiber mesh shape, and the like.
Traditional atmospheric type combustor is formed by the combination of a plurality of combustor monolithic usually, and different load burning demands then need the combustor monolithic of different quantity to make up the stack, and the structure is comparatively complicated, is subject to design factors such as service environment, cost, has reduced combustion characteristic and user's use and has experienced.
The cylindrical combustor on the existing market is mostly a full premix combustion mode, is limited by the structure, easily appears the problem that gas and air mix are uneven, is difficult for carrying out combustor segmentation structural design, and is handling the problem that the water heater complete machine small load temperature rise is too high and brings the difficulty.
SUMMERY OF THE UTILITY MODEL
The utility model provides a first technical problem that solve provides a drum formula stratified combustion of tube-shape atmosphere formula combustor, overcomes the too high problem of water heater complete machine light load temperature rise, simultaneously, does benefit to the gas mixture and distributes balancedly, improves the stability of flame burning.
The utility model provides a second technical problem who solves provides a gas hot water equipment, uses cylinder atmospheric burner, and the burning of cylinder formula layering is overcome the too high problem of water heater complete machine little load temperature rise, simultaneously, is favorable to the gas mixture to distribute balanced, improves the stability of flame burning, promotes the user and experiences the use of water heater complete machine.
The first technical problem is solved by the following technical scheme:
a tubular atmospheric burner, the tubular atmospheric burner comprising: the gas mixing device comprises a base, a gas mixing device and a gas mixing device, wherein a first mixing cavity and a second mixing cavity for introducing mixed gas are arranged on the base at intervals, and an air inlet is also formed in the base; the first device body is fixed on the base, a first shunt cavity communicated with the first mixing cavity is arranged in the first shunt cylinder, the first shunt cylinder is sleeved in the first device body, a second shunt cavity is formed between the first shunt cylinder and the first device body and communicated with the second mixing cavity, a first fire hole communicated with the second shunt cavity is formed in the first device body, and the air inlet is positioned on the periphery of the first device body; the second device body is stacked on the first device body, a third shunt cavity communicated with the first shunt cavity is arranged in the second device body, a second fire hole communicated with the third shunt cavity is formed in the second device body, and one end, back to the first device body, of the third shunt cavity is closed; the ejector is positioned on one side, back to the first ejector body, of the base, and the first mixing cavity and the second mixing cavity are communicated with at least one ejector.
Tube-shape atmosphere formula combustor, compare produced beneficial effect with the background art: during the use, gas and air mixture can be alternatively or simultaneously introduced into the first mixing cavity and the second mixing cavity. When the mixed gas is introduced into the first mixing cavity for mixing, the mixed gas flow flows into the first shunting cavity and flows into the third shunting cavity under the action of the first shunting cavity; the airflow flowing into the third branch flow cavity finally flows out of the second fire hole of the second device body. When the mixed gas is introduced into the second mixing cavity for mixing, the mixed gas flow flows into the second shunting cavity and flows out of the first fire hole on the first device body under the action of the second shunting cavity. Because the second device body is overlapped on the first device body, mixed gas respectively introduced into the first mixing cavity and the second mixing cavity finally flows out from different height positions, the requirements of users on different loads for combustion are effectively met, and the sectional combustion of the combustor is realized. The tubular atmospheric burner skillfully changes the flow direction of mixed airflow by arranging the first splitter barrel in the tubular atmospheric burner, realizes tubular layered combustion, and overcomes the problem of overhigh temperature rise of the whole water heater under small load. This tube-shape atmosphere formula combustor embeds a plurality of hybrid chambers and reposition of redundant personnel chamber, guarantees gas and air intensive mixing before flowing for flame burning is more stable, is favorable to promoting the performance of product.
In one embodiment, the inner diameter of the first shunt cylinder is firstly reduced and then increased from the end of the first shunt cylinder close to the base to the end of the first shunt cylinder close to the second device body, or is firstly reduced, then is unchanged and then is increased.
In one embodiment, the outer diameter of the first shunt cylinder is firstly reduced and then increased or is firstly reduced and then unchanged and then increased from the end of the first shunt cylinder close to the base to the end of the first shunt cylinder close to the second device body, and one side surface of the first device body facing the second shunt cavity is a cylindrical surface.
In one of them embodiment, tube-shape atmospheric burner still includes the top cap, the top cap seals the third reposition of redundant personnel chamber dorsad the one end of first ware body, the top cap includes installation department and bellying, the bellying sets up on the installation department, the installation department is installed on the second ware body, the bellying stretches into in the third reposition of redundant personnel chamber, the bellying be used for with the air current in the third reposition of redundant personnel chamber is to water conservancy diversion all around.
In one embodiment, the cross section of the boss taken in a plane perpendicular to the axis of the boss increases in area from the end of the boss remote from the mounting portion to the end of the boss closer to the mounting portion.
In one embodiment, the cylindrical atmospheric burner further comprises a second shunt cylinder, the second shunt cylinder is sleeved in the second burner body and divides the third shunt cavity into a first shunt cavity and a second shunt cavity, a shunt hole is formed in the shunt cylinder, the first shunt cavity is communicated with the second shunt cavity through the shunt hole, the first shunt cavity is communicated with the first shunt cavity, and the second fire hole is communicated with the second shunt cavity.
In one embodiment, the second mixing chamber is disposed around a periphery of the first mixing chamber.
In one embodiment, a sealing gasket is arranged between the first device body and the base, a first flow through hole and a second flow through hole are formed in the sealing gasket, at least two second flow through holes are arranged around the periphery of the first flow through hole at intervals, the first mixing cavity is communicated with the first shunting cavity through the first flow through hole, and the second mixing cavity is communicated with the second shunting cavity through the second flow through hole.
In one embodiment, the first shunt cylinder includes a cylinder body and a first end plate disposed at one end of the cylinder body, the cylinder body is sleeved in the first device body, the first end plate is supported at an end of the first device body, the second device body is disposed on the first end plate, the cylinder body is provided with the first shunt cavity, and the second shunt cavity is formed between the cylinder body and the first device body.
In one embodiment, the sum of the hole areas of all the second fire holes in the second body is larger than the sum of the hole areas of all the first fire holes in the first body.
In one embodiment, the tubular atmospheric burner further comprises an ignition assembly mounted on the base.
The second technical problem is solved by the following technical solutions:
a gas water heating device comprises the cylindrical atmospheric burner.
Gas hot water equipment, compare produced beneficial effect with the background art: by adopting the cylindrical atmospheric burner, in the using process, the mixed gas of gas and air can be alternatively or simultaneously introduced into the first mixing cavity and the second mixing cavity. When the mixed gas is introduced into the first mixing cavity for mixing, the mixed gas flow flows into the first shunting cavity and flows into the third shunting cavity under the action of the first shunting cavity; the airflow flowing into the third branch flow cavity finally flows out of the second fire hole of the second device body. When the mixed gas is introduced into the second mixing cavity for mixing, the mixed gas flow flows into the second shunting cavity and flows out of the first fire hole on the first device body under the action of the second shunting cavity. Because the second device body is overlapped on the first device body, mixed gas respectively introduced into the first mixing cavity and the second mixing cavity finally flows out from different height positions, the requirements of users on different loads for combustion are effectively met, and the sectional combustion of the combustor is realized. The tubular atmospheric burner skillfully changes the flow direction of mixed airflow by arranging the first splitter barrel in the tubular atmospheric burner, realizes tubular layered combustion, and overcomes the problem of overhigh temperature rise of the whole water heater under small load. This tube-shape atmosphere formula combustor embeds a plurality of hybrid chambers and reposition of redundant personnel chamber, guarantees gas and air intensive mixing before flowing for flame burning is more stable, is favorable to promoting the performance of product.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this application, are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification.
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
FIG. 1 is a schematic structural view of a cylindrical atmospheric burner according to an embodiment;
FIG. 2 is an exploded view of a cylindrical atmospheric burner according to an embodiment;
FIG. 3 is a sectional view of a cylindrical atmospheric burner according to an embodiment;
FIG. 4 is a schematic view of the gas flow in the tubular atmospheric burner according to one embodiment;
fig. 5 is a schematic view of a base structure according to an embodiment.
Reference numerals:
100. a burner; 110. a base; 111. a first mixing chamber; 112. a second mixing chamber; 113. an air inlet; 120. a first body; 121. a first fire hole; 122. flanging; 123. expanding the edge; 130. a first splitter drum; 131. a cartridge body; 132. a first end plate; 133. a second end plate; 134. a laryngeal opening; 135. a first diversion chamber; 136. a second diversion cavity; 140. a second body; 141. a second fire hole; 142. edge covering; 150. A top cover; 151. an installation part; 152. a boss portion; 153. a round and smooth part; 154. contact step surfaces; 160. a second shunt cylinder; 161. a shunt hole; 162. a third shunting cavity; 1621. a first molecular cavity; 1622. a second lumen; 170. an ignition assembly; 180. an ejector; 190. a gasket; 191. a first flow through hole; 192. A second flow through hole.
Detailed Description
In order to make the above objects, features and advantages of the present invention more comprehensible, embodiments of the present invention are described in detail below with reference to the accompanying drawings. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. The present invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein, as those skilled in the art will be able to make similar modifications without departing from the spirit and scope of the present invention.
In one embodiment, referring to fig. 1 to 3, a tubular atmospheric burner 100, the tubular atmospheric burner 100 includes: a base 110, a first body 120, a first shunt cylinder 130, a second body 140 and an injector 180. The base 110 is provided with a first mixing chamber 111 and a second mixing chamber 112 at an interval for introducing the mixed gas. The base 110 is also provided with an air inlet 113. The first body 120 is fixed to the base 110. The first splitter cylinder 130 is provided with a first splitter cavity 135 communicated with the first mixing cavity 111, the first splitter cylinder 130 is sleeved in the first device body 120, and a second splitter cavity 136 is formed between the first splitter cylinder 130 and the first device body 120. The second branch chamber 136 communicates with the second mixing chamber 112. The first body 120 is provided with a first fire hole 121 communicated with the second diverging chamber 136. The air inlet 113 is located at the periphery of the first body 120. The second body 140 is stacked on the first body 120, a third diverging chamber 162 communicating with the first diverging chamber 135 is provided in the second body 140, and a second fire hole 141 communicating with the third diverging chamber 162 is provided in the second body 140. The end of the third branch chamber 162 facing away from the first body 120 is closed. The injector 180 is located on a side of the base 110 opposite to the first body 120. The first mixing chamber 111 and the second mixing chamber 112 are in communication with at least one eductor 180.
In the tubular atmospheric burner 100, the gas and air mixture may be introduced into the first mixing chamber 111 and the second mixing chamber 112 alternatively or simultaneously during use. When the mixed gas is introduced into the first mixing chamber 111 for mixing, the mixed gas flows into the first diversion chamber 135 and flows into the third diversion chamber 162 under the action of the first diversion chamber 135; the air current flowing into the third branch chamber 162 finally flows out of the second fire hole 141 of the second body 140. When the mixed gas is introduced into the second mixing chamber 112 for mixing, the mixed gas flows into the second branch chamber 136, and flows out of the first fire hole 121 of the first body 120 under the action of the second branch chamber 136. Because the second device body 140 is stacked on the first device body 120, the mixed gas respectively introduced into the first mixing cavity 111 and the second mixing cavity 112 finally flows out from different height positions, thereby effectively meeting the requirements of users on different loads and realizing the staged combustion of the combustor 100. The tubular atmospheric burner 100 skillfully changes the flow direction of mixed airflow by arranging the first splitter cylinder 130 in the burner, realizes tubular layered combustion, and overcomes the problem of overhigh temperature rise of the whole water heater under small load. This tube-shape atmosphere formula combustor 100 embeds a plurality of hybrid chambers and reposition of redundant personnel chamber, guarantees gas and air intensive mixing before flowing for flame burning is more stable, is favorable to promoting the performance of product.
It should be noted that the present embodiment is not limited to two-stage combustion, and may also be designed to be a three-stage, four-stage, or even more-stage combustion manner, but as long as the structures of the first body 120, the second body 140, and the first splitter cylinder 130 and the structural relationship among the three are involved, the present invention falls into the protection scope of the present application. In addition, when the tubular atmospheric burner 100 needs to burn in more than three stages, it is only necessary to add corresponding structures on the basis of the original structure, for example: at least one mixing cavity is additionally arranged on the base 110, at least one device body is stacked on the second device body 140, and at least one shunt tube is sleeved in the first shunt tube 130. In addition, the first diversion cavity 135, the second diversion cavity 136, and the third diversion cavity 162 are all straight-through cavities, i.e., both ends are open. Of course, in other embodiments, openings may be formed at two ends of the first branch chamber 135, the second branch chamber 136, and the third branch chamber 162, respectively, to achieve the air passage communication. Meanwhile, the first and second bodies 120 and 140 are each a cylindrical structure.
It should be noted that, when the first mixing cavity 111 and the second mixing cavity 112 are both communicated with the same ejector 180, the ejector 180 may be provided with a control valve, such as a three-way valve, to realize an air supply function of the ejector 180; when the first mixing cavity 111 and the second mixing cavity 112 are respectively communicated with the two ejectors 180 correspondingly, the ejectors 180 can be provided with valve structures such as a proportional valve to adjust the flow.
It should be noted that, in this embodiment, the shape of the first diversion cavity 135 is not particularly limited, and it is only necessary that the mixed airflow in the first diversion cavity 135 can stably flow into the third diversion cavity 162. For example, the first branch chamber 135 may have a cylindrical shape, an inverted trapezoidal shape, a circular truncated cone shape, a venturi shape, or the like.
Alternatively, the first fire holes 121 may be circular holes, strip-shaped holes, elliptical holes, three-sided holes, or other polygonal holes; of course, the first fire holes 121 may be a combination of holes having various shapes. Similarly, the second fire holes 141 may be circular holes, strip-shaped holes, elliptical holes, three-sided holes, or other polygonal holes; of course, the second fire holes 141 may be a combination of holes having various shapes. In addition, the arrangement of the first fire holes 121 on the first container body 120 may be variously implemented as long as the outflow of the air current is satisfied.
Specifically, the number of the first fire holes 121 on the end of the first body 120 adjacent to the second body 140 is less than the number of the first fire holes 121 on the end of the first body 120 adjacent to the base 110. In addition, the first and second bodies 120 and 140 are each of a cylindrical structure.
Further, referring to fig. 3, the inner diameter of the first shunt cylinder 130 is first decreased and then increased or first decreased and then increased from the end of the first shunt cylinder 130 close to the base 110 to the end of the first shunt cylinder 130 close to the second body 140. It can be seen that the first branch chamber 135 of the present embodiment is shaped like a venturi or a similar venturi, that is, a throat 134 with a smaller cross section is disposed between two opposite openings of the first branch chamber 135. When the mixed gas flows into the first diversion cavity 135, the gas flow velocity is increased first and then decreased or increased first, then unchanged and then decreased and reaches the maximum in the throat 134 area, so that pressure difference and flow velocity difference are generated at two sides of the throat 134, the gas flow velocity is ensured to be changed rapidly in the first diversion cavity 135, the gas flow flows out of the first diversion cavity 135 and then enters the third diversion cavity 162 in a mode of diffusing all around, the gas flow is favorably and uniformly distributed in the third diversion cavity 162, and the combustion of flame is ensured to be more stable.
It should be further noted that, referring to fig. 3, the inner diameter of the first shunt cylinder 130 of the present embodiment is understood as: the cross section of the first shunt cylinder 130 at a side surface facing the first shunt chamber 135 is a circle having a diameter equal to the inner diameter of the first shunt cylinder 130. For the sake of easy understanding, taking fig. 3 as an example, the inner diameter of the first shunt cylinder 130 is S in fig. 30The size of the representation.
In one embodiment, referring to fig. 3, the outer diameter of the first shunt cylinder 130 is first decreased and then increased or first decreased and then increased from the end of the first shunt cylinder 130 close to the base 110 to the end of the first shunt cylinder 130 close to the second body 140, and the side of the first body 120 facing the second shunt chamber 136 is a cylindrical surface. Therefore, the outer side surface of the first flow dividing cylinder 130 is also in a venturi shape, so that the first flow dividing cylinder 130 enables the second flow dividing cavity 136 to be increased and then reduced, different pressure differences and different flow speeds are generated by internal airflow, airflow diffusion and mixing of the second flow dividing cavity 136 are facilitated, and flame combustion is more stable.
It should be noted that the outer diameter of the first splitter cylinder 130 of the present embodiment is understood as: the cross section of the side surface of the first splitter cylinder 130 facing the second splitter cavity 136 is circular, and the diameter of the circle is the outer diameter of the first splitter cylinder 130. For the sake of easy understanding, taking fig. 3 as an example, the outer diameter of the first splitter cylinder 130 is S in fig. 34The size of the representation.
Further, the distribution density of the first fire holes 121 in the first body 120 is decreased in a direction from the throat 134 of the first splitter cylinder 130 to an end of the first splitter cylinder 130 close to the second body 140, with the throat 134 of the first splitter cylinder 130 as a reference; meanwhile, the distribution density of the first fire holes 121 in the first body 120 decreases in a direction from the throat 134 of the first splitter cylinder 130 to an end of the first splitter cylinder 130 close to the base 110, thereby ensuring more uniform outflow of the mixed gas on the first body 120. Further, the number of the first fire holes 121 located above the throat 134 of the first splitter 130 is smaller than the number of the first fire holes 121 located below the throat 134 of the first splitter 130, based on the throat 134 of the first splitter 130.
In one embodiment, referring to fig. 3, the tubular atmospheric burner 100 further comprises a top cover 150. The top cover 150 closes an end of the third branch flow chamber 162 facing away from the first body 120, and the top cover 150 includes a mounting portion 151 and a protrusion 152. The boss 152 is provided on the mounting portion 151. The mounting portion 151 is mounted on the second body 140. The protrusion 152 extends into the third shunting cavity 162, and the protrusion 152 is used for guiding the airflow in the third shunting cavity 162 to the periphery. Therefore, when the mounting portion 151 is mounted on the second body 140, the protruding portion 152 extends into the third shunting cavity 162, so that not only is one end of the third shunting cavity 162 sealed, but also the airflow in the third shunting cavity 162 is guided, so that the airflow entering the third shunting cavity 162 is diffused all around under the action of the protruding portion 152, the airflow is guided to be uniformly distributed in the third shunting cavity 162, the phenomenon that the mixed gas is gathered inside to cause overlarge gas pressure is prevented, and the deterioration phenomenon that the flame is uneven or the combustor 100 is blackened is effectively avoided.
It should be noted that the shape of the protruding portion 152 is not particularly limited in this embodiment, and only a certain slope or a certain radian is required to be formed on the side surface of the protruding portion 152, for example, the protruding portion 152 is designed in an inverted triangular cone, an inverted truncated cone, an inverted trapezoid, an inverted hemisphere, or the like.
Further, referring to fig. 3, a cross section of the protruding portion 152 is obtained by cutting a plane perpendicular to an axis of the protruding portion 152, and an area of the cross section increases from an end of the protruding portion 152 away from the mounting portion 151 to an end of the protruding portion 152 close to the mounting portion 151, that is, the protruding portion 152 of the embodiment is a structure that gradually increases, or increases first, does not change, and then continues to increase when viewed from the airflow flowing direction. When the protruding portion 152 extends into the third shunting cavity 162, the space between the protruding portion 152 and the cavity wall of the third shunting cavity 162 gradually decreases or first decreases, then does not change, and then continuously decreases along with the airflow flowing direction, so that the airflow entering the third shunting cavity 162 is more easily diffused to the periphery of the third shunting cavity 162 under the guidance of the protruding portion 152, and the airflow flowing out of the second fire holes 141 is ensured to be uniformly distributed.
It should be noted that, in order to facilitate understanding of the axis and the cross section of the boss 152 in the present embodiment, taking fig. 3 as an example, the axis of the boss 152 is S in fig. 31A straight line of representation; the cross section is S in FIG. 32The indicated area.
Further, referring to fig. 3, the cross-sectional area gradually increases from the end of the protruding portion 152 away from the mounting portion 151 to the end of the protruding portion 152 near the mounting portion 151. Meanwhile, one end of the protruding portion 152, which is far away from the mounting portion 151, is provided with a smooth portion 153, so that when the air flow impacts the protruding portion 152, the impact force of the air flow on the protruding portion 152 is relieved by the smooth portion 153, and the air flow flows around the third shunting cavity 162 along the smooth portion 153.
Specifically, the rounded portion 153 is a circular arc surface. Meanwhile, the mounting portion 151 and the boss portion 152 are integrally formed.
In one embodiment, referring to fig. 4, the tubular atmospheric burner 100 further comprises a second splitter cylinder 160. The second shunt tube 160 is disposed in the second body 140 and divides the third shunt cavity 162 into a first shunt cavity 1621 and a second shunt cavity 1622. The shunt cylinder is provided with a shunt hole 161. The first branch chamber 1621 communicates with the second branch chamber 1622 through the branch orifice 161, and the first branch chamber 135 communicates with the first branch chamber 1621. The second fire port 141 communicates with the second chamber 1622. It can be seen that as the gas stream exits the first mixing chamber 111, the gas stream first enters the first branch chamber 1621; through the flow orifice 161 into the second chamber 1622; finally, it flows out through the second fire holes 141 to be burned. In this embodiment, the second splitter cylinder 160 is additionally arranged in the second device body 140, so that the mixed gas uniformly flows into the second splitter chamber 1622, and stable combustion of flame on the second device body 140 is ensured.
Further, referring to fig. 4, the mounting portion 151 is mounted on the second body 140, and the protrusion 152 extends into the first housing chamber 1621. When the airflow flows into the first split cavity 1621, the airflow is guided by the protrusion 152 to spread around; the diffused gas flow uniformly flows into the second chamber 1622 from the diversion hole 161, so as to ensure the mixed gas to be fully mixed and the mixed gas flow to be uniformly distributed on the inner side wall of the second device body 140, so that the flame on the second device body 140 is more stable.
In one embodiment, referring to fig. 4, one end of the second split cylinder 160 is lower than one end of the second body 140. The top cover 150 is provided with an interference step surface 154, and the outer side surface of the top cover 150 is in interference fit with the inner side of the second container body 140. The interference step surface 154 interferes with one end of the second split sleeve 160, and the other end of the second split sleeve 160 interferes with the second end plate 132, so that the top cap 150 is stably mounted on the second body 140. At the same time, one end of the second chamber 1622 is closed by the interference step 154. In order to improve the sealing performance between the second body 140 and the top cover 150, solder may be filled between the second body 140 and the top cover 150, and the hermeticity between the second body 140 and the top cover 150 may be improved by welding.
Specifically, referring to fig. 4, the interference step surface 154 is disposed on the mounting portion 151 and surrounds the periphery of the protrusion 152.
In one embodiment, referring to fig. 5, the second mixing chamber 112 is disposed around the periphery of the first mixing chamber 111, i.e. the second mixing chamber 112 is an annular chamber, so as to ensure that the airflow flowing out from the second mixing chamber 112 is uniformly dispersed into the second branch chamber 136.
It should be noted that, when the tubular atmospheric burner 100 has more than three combustion modes, at least one mixing cavity needs to be additionally arranged on the base 110, at this time, the mixing cavities on the base 110 are in an annular structure, and the mixing cavities are arranged in a ring-by-ring manner.
Further, referring to fig. 2, a sealing gasket 190 is disposed between the first body 120 and the base 110 to improve the air tightness between the first body 120 and the base 110 and prevent the leakage of the fuel gas therebetween. Meanwhile, the gasket 190 is provided with a first flow hole 191 and a second flow hole 192. At least two second flow holes 192 are arranged around the periphery of the first flow hole 191 at intervals, the first mixing cavity 111 is communicated with the first shunting cavity 135 through the first flow hole 191, the second mixing cavity 112 is communicated with the second shunting cavity 136 through the second flow hole 192, and thus, through the first flow hole 191 and the second flow hole 192, airflow in the first mixing cavity 111 and the second mixing cavity 112 stably flows into the respective corresponding shunting cavities, and the smooth flowing of mixed gas is ensured. Meanwhile, the at least two second flow holes 192 are arranged around the first flow hole 191 and have a flow equalizing effect on the air flow in the second mixing cavity 112, so that the air flow in the second mixing cavity 112 uniformly and stably flows into the second shunting cavity 136, and the stable combustion of the flame on the first device body 120 is further ensured.
In one embodiment, referring to fig. 2, the first shunt cylinder 130 includes a cylinder body 131 and a first end plate 132 disposed at one end of the cylinder body 131. The cylinder body 131 is fitted in the first container 120. The first end plate 132 is supported at an end of the first body 120. The second body 140 is mounted on the first end plate 132. A first shunting cavity 135 is arranged in the cylinder body 131, and a second shunting cavity 136 is formed between the cylinder body 131 and the first device body 120, so that the first shunting cylinder 130 is ensured to be stably sleeved in the first device body 120.
Further, referring to fig. 2, the end of the first body 120 is provided with a flange 122, and the first end plate 132 is supported on the flange 122. The second container 140 is provided with a covering edge 142. The edge 142 wraps the first end plate 132 and the flange 122 to allow the first body 120, the first shunt tube 130 and the second body 140 to be stably connected.
In one embodiment, referring to fig. 2, an end of the first body 120 close to the base 110 is provided with a flared edge 123, and the flared edge 123 abuts against the sealing pad 190.
In one embodiment, referring to fig. 2, the first shunt cylinder 130 further includes a second end plate 133 disposed on the other end of the cylinder body 131, and the second end plate 133 abuts against the sealing gasket 190.
In one embodiment, referring to fig. 5, the number of the air inlets 113 is two or more. Two or more air inlets 113 are spaced around the periphery of the first body 120.
In one embodiment, referring to fig. 3, the length direction of the ejector 180 is intersected with the depth direction of the first mixing cavity 111 and the depth direction of the second mixing cavity 112, so as to prevent the airflow of the ejector 180 from directly flowing out of the first mixing cavity 111 and the second mixing cavity 112. Meanwhile, the flow velocity of the air flow is also reduced, so that the mixed gas can be fully mixed in the first mixing cavity 111 and the second mixing cavity 112.
In one embodiment, the sum of the hole areas of all the second fire holes 141 of the second body 140 is greater than the sum of the hole areas of all the first fire holes 121 of the first body 120, so that the gas flow flowing out of the second body 140 is greater than the gas flow flowing out of the first body 120, thereby meeting the different load combustion requirements of the product.
In one embodiment, referring to fig. 1, the tubular atmospheric burner 100 further comprises an ignition assembly 170. The ignition assembly 170 is mounted on the base 110. When the mixed gas flows out of the first fire hole 121 and the second fire hole 141, respectively, the ignition assembly 170 is activated so that the gas is rapidly ignited.
In one embodiment, please refer to fig. 1 to 3, a gas water heater includes a cylindrical atmospheric burner 100 in any one of the above embodiments.
In the gas water heating device, the cylindrical atmospheric burner 100 is adopted, and during use, gas and air mixed gas can be alternatively or simultaneously introduced into the first mixing cavity 111 and the second mixing cavity 112. When the mixed gas is introduced into the first mixing chamber 111 for mixing, the mixed gas flows into the first diversion chamber 135 and flows into the third diversion chamber 162 under the action of the first diversion chamber 135; the air current flowing into the third branch chamber 162 finally flows out of the second fire hole 141 of the second body 140. When the mixed gas is introduced into the second mixing chamber 112 for mixing, the mixed gas flows into the second branch chamber 136, and flows out of the first fire hole 121 of the first body 120 under the action of the second branch chamber 136. Because the second device body 140 is stacked on the first device body 120, the mixed gas respectively introduced into the first mixing cavity 111 and the second mixing cavity 112 finally flows out from different height positions, thereby effectively meeting the requirements of users on different loads and realizing the staged combustion of the combustor 100. The tubular atmospheric burner 100 skillfully changes the flow direction of mixed airflow by arranging the first splitter cylinder 130 in the burner, realizes tubular layered combustion, and overcomes the problem of overhigh temperature rise of the whole water heater under small load. This tube-shape atmosphere formula combustor 100 embeds a plurality of hybrid chambers and reposition of redundant personnel chamber, guarantees gas and air intensive mixing before flowing for flame burning is more stable, is favorable to promoting the performance of product.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", and the like, indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the present application, unless expressly stated or limited otherwise, the first feature may be directly on or directly under the second feature or indirectly via intermediate members. Also, a first feature "on," "over," and "above" a second feature may be directly or diagonally above the second feature, or may simply indicate that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature may be directly under or obliquely under the first feature, or may simply mean that the first feature is at a lesser elevation than the second feature.
It will be understood that when an element is referred to as being "secured to" or "disposed on" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "upper," "lower," "left," "right," and the like as used herein are for illustrative purposes only and do not denote a unique embodiment.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
The above-mentioned embodiments only represent some embodiments of the present invention, and the description thereof is specific and detailed, but not to be construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the appended claims.
Claims (10)
1. A tubular atmospheric burner (100), characterized in that it comprises:
the gas mixing device comprises a base (110), wherein a first mixing cavity (111) and a second mixing cavity (112) for introducing mixed gas are arranged on the base (110) at intervals, and an air inlet (113) is also formed in the base (110);
the gas mixing device comprises a first device body (120) and a first shunt tube (130), wherein the first device body (120) is fixed on a base (110), a first shunt cavity (135) communicated with a first mixing cavity (111) is arranged in the first shunt tube (130), the first shunt tube (130) is sleeved in the first device body (120), a second shunt cavity (136) is formed between the first shunt tube (130) and the first device body (120), the second shunt cavity (136) is communicated with a second mixing cavity (112), a first fire hole (121) communicated with the second shunt cavity (136) is arranged on the first device body (120), and an air inlet (113) is positioned on the periphery of the first device body (120);
the second device body (140) is stacked on the first device body (120), a third shunt cavity (162) communicated with the first shunt cavity (135) is arranged in the second device body (140), a second fire hole (141) communicated with the third shunt cavity (162) is formed in the second device body (140), and one end, back to the first device body (120), of the third shunt cavity (162) is closed;
the ejector (180) is located on one side, back to the first body (120), of the base (110), and the first mixing cavity (111) and the second mixing cavity (112) are communicated with at least one ejector (180).
2. The tubular atmospheric burner as recited in claim 1, wherein the inner diameter of the first splitter cylinder (130) is first reduced and then increased or first reduced and then increased from the end of the first splitter cylinder (130) near the base (110) to the end of the first splitter cylinder (130) near the second body (140); and/or the presence of a gas in the gas,
the outer diameter of the first shunt tube (130) is firstly reduced and then increased or is firstly reduced and then increased from one end of the first shunt tube (130) close to the base (110) to one end of the first shunt tube (130) close to the second device body (140), and is not changed and then increased, and one side surface of the first device body (120) facing the second shunt cavity (136) is a cylindrical surface.
3. The cylindrical atmospheric burner as claimed in claim 1, wherein the cylindrical atmospheric burner (100) further comprises a top cover (150), the top cover (150) seals the third diversion chamber (162) back to the one end of the first body (120), the top cover (150) comprises an installation part (151) and a boss (152), the boss (152) is arranged on the installation part (151), the installation part (151) is arranged on the second body (140), the boss (152) extends into the third diversion chamber (162), and the boss (152) is used for guiding the airflow in the third diversion chamber (162) to the periphery.
4. The tubular atmospheric burner as claimed in claim 3, characterized in that a cross section of the boss (152) taken in a plane perpendicular to the axis of the boss (152) increases in area from an end of the boss (152) remote from the mounting portion (151) to an end of the boss (152) close to the mounting portion (151).
5. The tubular atmospheric burner according to claim 1, wherein the tubular atmospheric burner (100) further comprises a second shunt tube (160), the second shunt tube (160) is sleeved in the second device body (140), and separates the third shunt cavity (162) into a first shunt cavity (1621) and a second shunt cavity (1622), the shunt tube is provided with a shunt hole (161), the first shunt cavity (1621) is communicated with the second shunt cavity (1622) through the shunt hole (161), the first shunt cavity (135) is communicated with the first shunt cavity (1621), and the second fire hole (141) is communicated with the second shunt cavity (1622).
6. The tubular atmospheric burner as claimed in claim 1, characterized in that the second mixing chamber (112) is arranged around the periphery of the first mixing chamber (111).
7. The tubular atmospheric burner as recited in claim 6, characterized in that a gasket (190) is disposed between the first body (120) and the base (110), a first flow hole (191) and a second flow hole (192) are disposed on the gasket (190), at least two of the second flow holes (192) are disposed around the periphery of the first flow hole (191) at intervals, the first mixing chamber (111) is communicated with the first branch chamber (135) through the first flow hole (191), and the second mixing chamber (112) is communicated with the second branch chamber (136) through the second flow hole (192).
8. The tubular atmospheric burner as claimed in any one of claims 1 to 7, wherein the first splitter tube (130) comprises a tube body (131) and a first end plate (132) disposed at one end of the tube body (131), the tube body (131) is sleeved in the first body (120), the first end plate (132) is supported at an end of the first body (120), the second body (140) is disposed on the first end plate (132), the first splitter cavity (135) is disposed in the tube body (131), and the second splitter cavity (136) is formed between the tube body (131) and the first body (120).
9. The tubular atmospheric burner as claimed in any of claims 1 to 7, wherein the sum of the hole areas of all the second fire holes (141) in the second body (140) is greater than the sum of the hole areas of all the first fire holes (121) in the first body (120); and/or the presence of a gas in the gas,
the cylindrical atmospheric burner (100) further comprises an ignition assembly (170), and the ignition assembly (170) is arranged on the base (110).
10. A gas-fired water heating appliance, characterized by comprising a tubular atmospheric burner (100) according to any one of claims 1 to 9.
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CN202022178384.XU CN214147874U (en) | 2020-09-28 | 2020-09-28 | Cylindrical atmospheric burner and gas water heating equipment |
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CN202022178384.XU CN214147874U (en) | 2020-09-28 | 2020-09-28 | Cylindrical atmospheric burner and gas water heating equipment |
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