Burner and gas stove
By designing a vent pipe with shrinking ports, expansion and contraction parts, and optimizing the shape and position of the air outlet, the problem of flow velocity loss during the flow of the mixed gas is solved, and the uniformity of combustion and smoothness of gas flow are improved.
Patent Information
- Application Number
- CN202411466179.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-21
- Publication Date
- 2025-05-16
- Estimated Expiration
- 2044-10-21
AI Technical Summary
In existing burners, the flow rate loss of the mixed gas during flow in the outer fire channel is large, affecting the combustion uniformity.
A burner is designed, and its induction pipe forms a shrinking section with a gradually shrinking cross-sectional area, an expansion part with a gradually increasing cross-sectional area, and a shrinking part with a gradually shrinking cross-sectional area, and is arranged through the shape and position of the air outlet to ensure that the mixed gas occupies the lower space of the outer fire channel at the moment of ejection.
It effectively reduces the flow velocity loss of the mixed gas during the flow of the outer fire channel, extends the length of the flow path, thereby improving the uniformity of combustion, reducing spoilers and disturbances, and improving the smoothness of the gas flow.
Smart Images

Figure CN119022300B_ABST
Abstract
Description
Technical Field
[0001] The invention relates to a burner and a gas stove, belonging to the technical field of kitchen appliances. Background Art
[0002] The burner and the ejector tube are important components of the gas stove. The burner is the part of the stove that directly generates flames, which determines the distribution of the flame and the combustion efficiency. The most common burner suitable for kitchens is the double-ring fire style. The interior of the burner has a ring-shaped outer fire cavity. The ejector tube is used to transport gas. The gas is sprayed into the ejector tube at a high speed, thereby injecting air into the ejector tube and mixing with the gas to form a mixed gas. After the mixed gas is sprayed into the outer fire cavity, it is ignited and burned at the fire hole of the outer fire cover of the burner.
[0003] After the mixed gas formed by the gas and air is injected into the outer fire cavity by the injector tube, it will diffuse rapidly in the outer fire cavity. This diffusion process will cause the kinetic energy of the mixed gas to be lost, which is not conducive to the high-speed flow of the mixed gas in the outer fire cavity, and then affect the combustion uniformity; in addition, the mixed gas will also produce turbulence and disturbance during the diffusion process, thereby affecting the smoothness of the flow. Summary of the invention
[0004] The technical problem to be solved by the present invention is to provide a burner and a gas stove, which can effectively reduce the flow velocity loss of the mixed gas during the flow in the external fire cavity, which is beneficial to extend the flow path length of the mixed gas in the external fire cavity, thereby improving the uniformity of combustion.
[0005] The present invention is achieved through the following technical solutions.
[0006] A burner, comprising:
[0007] A shell body having an annular outer fire cavity inside;
[0008] The ejection pipe is arranged on the shell, and an air inlet and an air outlet are respectively provided at the head end and the tail end thereof. The ejection pipe is formed with a contraction section with a gradually decreasing cross-sectional area, an expansion section with a gradually increasing cross-sectional area, and a contraction section with a gradually decreasing cross-sectional area in sequence along the direction of the air path. The cross-sectional shape of the ejection pipe gradually changes from the shape of the air inlet to the shape of the air outlet along the direction of the air path.
[0009] As a further improvement of the present invention, the level of the air outlet is higher than the level of the air inlet.
[0010] As a further improvement of the present invention, the ejection pipe includes an upper half pipe and a lower half pipe, the upper half pipe is provided with a first point, and the lower half pipe is provided with a second point and a third point in sequence along the direction of the gas path, the upper half pipe is gradually raised from the head end to the first point along the direction of the gas path, and the horizontal height is maintained unchanged from the first point to the tail end, and the lower half pipe of the ejection pipe is gradually lowered from the head end to the second point along the direction of the gas path, gradually raised from the second point to the third point, and the horizontal height is maintained unchanged from the third point to the tail end.
[0011] As a further improvement of the present invention, along the gas path direction of the injection pipe, the first site is located between the second site and the third site, the second site is located at the expansion part, the third site is located at the contraction part, and the first site is located at the expansion part, or at the contraction part, or at the junction of the expansion part and the contraction part.
[0012] As a further improvement of the present invention, the cross-sectional shape of the upper half of the pipe gradually changes from the air inlet along the air path direction and suddenly changes to the shape of the air outlet at the first position, and the cross-sectional shape of the lower half of the pipe gradually changes from the air inlet along the air path direction and gradually changes to the shape of the air outlet at the third position.
[0013] As a further improvement of the present invention, both sides of the inner wall of the upper half pipe have convex corner structures formed by protrusions at the first position, so that the cross-sectional shape of the upper half pipe changes suddenly at the first position.
[0014] As a further improvement of the present invention, the shape of the gas outlet matches the lower part of the cross-sectional shape of the outer fire cavity, so that the mixed gas ejected from the gas outlet instantaneously occupies the lower space of the outer fire cavity.
[0015] As a further improvement of the present invention, the air outlet includes a top edge, a bottom edge and two side edges, the bottom edge of the air outlet is defined by the bottom plate of the shell, and the two side edges of the air outlet are respectively defined by the outer ring and the middle ring of the shell.
[0016] As a further improvement of the present invention, the shape of the air inlet is set to be circular, so that the air is introduced into the introduction pipe in a state of surrounding the gas and mixed with the gas.
[0017] As a further improvement of the present invention, at least two ejection pipes are provided and are centrally symmetrical with respect to the center of the shell.
[0018] A gas stove comprises the burner.
[0019] Beneficial effects of the present invention:
[0020] 1. The shape and position of the gas outlet can effectively reduce the velocity loss of the mixed gas in the process of flowing in the outer fire cavity, which is conducive to extending the flow path length of the mixed gas in the outer fire cavity, thereby improving the uniformity of combustion; in addition, it can also reduce the turbulence and disturbance caused by the need for diffusion of the ejected mixed gas, thereby improving the smoothness of gas flow;
[0021] 2. The gradual change of the cross-sectional shape of the ejector pipe can not only gradually adjust the cross-sectional shape of the ejector pipe to the shape of the gas outlet, so that the mixed gas can occupy the lower space of the outer fire cavity at the moment of ejection; but also reduce the turbulence generated when the mixed gas flows in the ejector pipe, which is conducive to the smooth flow and transportation in the ejector pipe;
[0022] 3. The cross-sectional area of the ejector pipe gradually decreases, increases, and decreases along the gas path. The gradually increasing cross-sectional area can gradually increase the static pressure of the mixed gas, prolong the mixing time, thereby facilitating the molecular diffusion and mixing between the gas and the air, optimizing the mixing process of the gas and the air, and helping to form a more uniform mixed gas, thereby enhancing the mixing efficiency of the mixed gas; the gradually decreasing cross-sectional area gradually increases the flow rate of the mixed gas, and is ejected from the gas outlet in the direction tangent to the outer fire cavity at the highest flow rate, thereby further improving the combustion uniformity of the outer fire ring and avoiding the problem of excessive or weak local combustion intensity on the outer fire cover;
[0023] 4. The change in the horizontal height of the upper half of the pipe along the gas path direction is slower than that of the lower half of the pipe, and the upper half of the ejector pipe is located in the internal space of the shell, which is beneficial to the smooth flow of the mixed gas in the outer fire cavity. The lower half of the ejector pipe will not affect the smooth flow of the mixed gas in the outer fire cavity. Therefore, the change in the horizontal height of the lower half of the ejector pipe is coordinated with the upper half of the pipe to adapt to the change in the cross-sectional area of the ejector pipe;
[0024] 5. In the part where the cross-sectional area gradually decreases along the gas path direction, the cross-sectional area gradually decreases less in the first half from the second point to the first point than in the second half from the first point to the third point, so as to achieve the effect of buffering fluid changes;
[0025] 6. The change in horizontal height of the upper half of the pipe is more gradual than that of the lower half of the pipe. Therefore, the cross-sectional shape of the upper half of the pipe is suddenly changed into the shape of the air outlet at the first position, so that the shape of the upper part of the ejector pipe is adjusted to match the shape of the air outlet in advance and will not cause too much influence on the flow state of the mixed gas; the change in horizontal height of the lower half of the pipe is more steep than that of the upper half of the pipe. Therefore, the cross-sectional shape of the upper half of the pipe is gradually changed into the shape of the air outlet at the third position, so that the change in the cross-sectional shape of the upper half of the pipe is more gradual, which is conducive to stabilizing the flow state of the mixed gas. BRIEF DESCRIPTION OF THE DRAWINGS
[0026] The preferred embodiments of the present invention will be described in detail below with reference to the accompanying drawings to help understand the purpose and advantages of the present invention, wherein:
[0027] Figure 1 is a schematic diagram of a burner from a top-down perspective;
[0028] Figure 2 It is a schematic diagram of the burner when viewed from an upward perspective;
[0029] Figure 3 is a schematic diagram of a burner in a three-dimensional perspective;
[0030] Figure 4 for Figure 2 Schematic diagram after cutting the outer structure along the dotted line Figure 1 ;
[0031] Figure 5 for Figure 2 Schematic diagram after cutting the outer structure along the dotted line Figure 2 ;
[0032] Figure 6 for Figure 2 Schematic diagram after cutting the outer structure along the dotted line Figure 3 ;
[0033] Figure 7 for Figure 2 Schematic diagram after cutting the outer structure along the dotted line Figure 4 ;
[0034] Figure 8 is a cross-sectional schematic diagram of the burner at the air inlet;
[0035] Fig. 9 is a cross-sectional schematic diagram of the burner at the air outlet;
[0036] Fig.10 is a cross-sectional schematic diagram of a burner at a first position;
[0037] Fig.11 Schematic diagram of the burner after removing the outer fire cover;
[0038] Fig.12 It is a schematic diagram of the fire distributor;
[0039] Fig.13 A schematic diagram of the cover.
[0040] Reference numerals: housing 1, fire distributor 11, outer fire cover 12, inner fire cover 13, bottom plate 1a, middle surrounding ring 1b, outer peripheral ring 1c, sinking section 1s;
[0041] Double-layer space r1, upper space r11, lower space r12, single-layer space r2, external fire cavity c;
[0042] The ejection pipe 2, the upper half pipe 2a, the lower half pipe 2b, the ejection section 21, the direction-changing section 22, the extension section 23, the constriction portion m1, the expansion portion m2, the contraction portion m3, the air inlet a1, the air outlet a2, the first point p1, the second point p2, and the third point p3;
[0043] Cover plate 3 , climbing section 31 , horizontal section 32 , inclined portion 33 . DETAILED DESCRIPTION
[0044] The present invention is further described in detail below based on the accompanying drawings and implementation examples.
[0045] The directional terms such as up, down, left, right, front, back, front, back, top, bottom, etc. mentioned or may be mentioned in this specification are defined relative to the structures shown in the drawings. The words "inside" and "outside" refer to the direction toward or away from the geometric center of a specific component, respectively. They are relative concepts, and therefore may change accordingly according to different locations and different usage conditions. Therefore, these or other directional terms should not be interpreted as restrictive terms.
[0046] Implementation Case 1:
[0047] Reference Figure 1-13 A burner comprises a shell 1 and an ejection pipe 2, wherein the shell 1 comprises an ignition divider 11, an outer fire cover 12 and an inner fire cover 13, wherein the ignition divider 11 comprises a bottom plate 1a and an inner surrounding ring, a middle surrounding ring 1b and an outer ring 1c connected to the bottom plate 1a, and the outer fire cover 12 is sealed on the middle surrounding ring 1b and the outer ring 1c, so that an annular space defined by the bottom plate 1a, the middle surrounding ring 1b, the outer ring 1c and the fire cover is formed inside the shell 1, and most of the space forms an outer fire cavity c, and the ejection pipe 2 injects a mixture of fuel gas and air into the outer fire cavity c, and an outer fire ring is formed on the fire hole 121 of the outer fire cover 12 through ignition by an igniter. In principle, an inner fire ring is formed on the fire hole 121 of the inner fire cover 13. Since the technical improvement of the present application does not involve this part, this part will not be described in detail in this implementation case.
[0048] In this embodiment, the head end and tail end of the ejection pipe 2 are respectively provided with an air inlet a1 and an air outlet a2. As for the structure of the ejection pipe 2, the ejection pipe 2 has an ejection section 21 and a redirection section 22 arranged in sequence along the gas path direction, wherein the ejection section 21 is used to inject air from the air inlet a1 and mix it with the gas, and the redirection section 22 is used to change the gas path direction, that is, the gas path direction of the ejection pipe 2 changes when passing through the ejection section 21 and the redirection section 22, and makes the ejection direction of the air outlet a2 tangent to the outer fire cavity c.
[0049] In this embodiment, an ejection section 21 and a redirecting section 22 are provided on the ejection pipe 2, wherein the ejection section 21 is equivalent to the ejection pipe 2 in the prior art, and the gas nozzle on the nozzle seat injects the gas from the gas inlet a1 of the ejection pipe 2, and the ejection section 21 utilizes the negative pressure difference formed by the high-speed flow of the gas to inject the air outside the ejection pipe 2 into the ejection section 21, and mixes with the gas to form a mixed gas, which can ensure that the gas can be fully burned during combustion. The redirecting section 22 can change the gas path direction of the ejection pipe 2 after passing through the ejection section 21 along the gas path direction, so that the mixed gas is finally injected into the outer fire cavity c from the gas outlet a2 along the direction tangent to the outer fire cavity c. By changing the orientation of the gas path direction of the injection pipe 2 through the redirecting section 22 and making it tangential to the outer fire cavity c, the mixed gas ejected from the gas outlet a2 can flow in an annular direction along the outer fire cavity c, and the kinetic energy loss caused by the mixed gas directly impacting the outer ring 1c can be avoided, thereby increasing the annular flow speed of the mixed gas in the outer fire cavity c and forming a circular flow, extending the flow path length of the mixed gas in the outer fire cavity c, and then being able to improve the uniformity of the distribution of the mixed gas in the outer fire cavity c, thereby improving the combustion uniformity of the outer fire ring.
[0050] In this embodiment, the ejector pipe 2 has an extension section 23, which is located downstream of the redirection section 22 along the gas path, so that the ejector pipe 2 is arranged in sequence as the ejector section 21, the redirection section 22 and the extension section 23 along the gas path. The extension section 23 can effectively extend the total length of the ejector pipe 2, so that the flow path of the mixed gas in the ejector pipe 2 is extended, so that the mixing of the gas and the air is more complete. The complete mixing can ensure that each gas molecule has enough oxygen for complete combustion, thereby improving the combustion efficiency and significantly reducing the emission of incomplete combustion products such as carbon monoxide CO and unburned hydrocarbons HC. In addition, the mixed gas obtained by fully mixing the gas and the air maintains a stable combustion flame during combustion to avoid flameout or deflagration.
[0051] In this embodiment, the gas path direction of the turning section 22 gradually changes along its extension direction, so that the turning section 22 presents an arc-shaped linear structure on the horizontal plane. The gradual change setting of the gas path of the turning section 22 provides a smoother transition, reduces the sudden turning of the mixed gas fluid during the flow process, and can reduce the friction resistance between the fluid and the pipe wall, thereby reducing the pressure loss and reducing the energy loss caused by turbulence.
[0052] In the present embodiment, the gas path direction at the head end of the extension section 23 is the same as the gas path direction at the tail end of the turning section 22 and the injection direction of the gas outlet a2. The mixed gas completes the adjustment process of the gas flow direction in the injection pipe 2 through the turning section 22. The gas flow direction of the extension section 23 is at least maintained consistent in the flow direction along the outer fire cavity c, so that the gas and air can be fully mixed with low friction resistance to reduce energy loss, and can reduce the degree of turbulence, so that the mixed gas ejected in the direction tangent to the outer fire cavity c has high stability and high flow rate.
[0053] In this embodiment, the gas path direction at the tail end of the ejection section 21 is the same as the gas path direction at the head end of the turning section 22, that is, the gas path direction of the turning section 22 is gradually adjusted and changed by the gas path direction at the tail end of the ejection section 21, so that the adjustment change of the gas path direction is relatively smooth, further reducing the energy loss caused by frictional resistance.
[0054] In this embodiment, for the structure of the ejection pipe 2, an expansion part m2 is formed on the ejection pipe 2, and the cross-sectional area of the expansion part m2 gradually increases along the gas path direction of the ejection pipe 2. For the position of the expansion part m2 on the ejection pipe 2, in the first embodiment, the expansion part m2 is formed at the rear section of the ejection section 21; in the second embodiment, the expansion part m2 is formed at the front section of the redirection section 22; in the third embodiment, the expansion part m2 extends from the rear section of the ejection section 21 to the front section of the redirection section 22. All of the above three embodiments are possible, and in all of the above three embodiments, after the ejection section 21 completes its ejection function, the gas and air are mixed and enter the expansion part m2. In the expansion part m2, as the cross-sectional area gradually increases along the gas path direction, the flow rate of the fluid formed by the gas and air will gradually decrease, and at the same time, the static pressure of the fluid will gradually increase, extending the mixing time, thereby facilitating the molecular diffusion and mixing between the gas and the air, optimizing the mixing process of the gas and the air, and helping to form a more uniform mixed gas, thereby enhancing the mixing efficiency of the mixed gas.
[0055] It should be noted that the cross sections in this embodiment all refer to the cross sections cut off by the vertical plane passing through the central axis of the housing 1 .
[0056] In this embodiment, with respect to the structural composition of the ejection pipe 2, a contraction portion m3 is formed on the ejection pipe 2, and the cross-sectional area of the contraction portion m3 gradually decreases along the gas path direction of the ejection pipe 2. With respect to the position of the contraction portion m3 on the ejection pipe 2, in the first embodiment, the contraction portion m3 is formed at the rear section of the turning section 22; in the second embodiment, the contraction portion m3 is formed at the front section of the extension section 23; in the third embodiment, the contraction portion m3 extends from the rear section of the turning section 22 to the front section of the extension section 23. All three of the above embodiments are applicable, and in the above three embodiments, the mixed gas formed by the mixture of fuel gas and air passes through the expansion portion m2 and the contraction portion m3 in sequence. In the process of passing through the contraction portion m3, since its cross-sectional area is continuously reduced along the gas path direction of the injection pipe 2, the flow velocity of the mixed gas gradually increases, and is ejected from the gas outlet a2 in the direction tangent to the outer fire cavity c at the highest flow velocity, thereby further improving the combustion uniformity of the outer fire ring and avoiding the problems of excessive local combustion intensity and weak local combustion intensity on the outer fire cover 12.
[0057] In addition, the mixed gas maintains its maximum flow rate when it is ejected from the gas outlet a2, so that the mixed gas can form a certain negative pressure intensity, which can "suck" the unburned gas in the outer fire cavity c to enhance and increase the total amount of the mixed gas and achieve a better combustion effect.
[0058] It should be noted that the mixed gas maintains its maximum flow rate when it is ejected from the air outlet a2. Since the injection speed of the mixed gas is fast enough, the flame can be prevented from flowing back into the ejector pipe 2 and making noise when the burner is extinguished, that is, backfire noise can be avoided, and damage to the structure of the ejector pipe 2 at the air inlet a1 due to backfire can also be avoided.
[0059] In this embodiment, the ejection pipe 2 also has a constricted portion m1, the cross-sectional area of which gradually decreases along the gas path direction, and the air inlet a1 is located at the head end of the constricted portion m1, so that the ejection pipe 2 forms a trumpet-shaped structure at the air inlet a1. The setting of the constricted portion m1 can form a large pressure difference when the gas enters, so that the air is quickly introduced into the ejection pipe, and can facilitate the air to enter the ejection pipe 2 in an annular manner from the edge at the air inlet a1, play a role in converging the air and effectively increase the amount of air injected, so that the gas can be fully mixed with the air; in addition, the constricted portion m1 with a gradually decreasing diameter can make the air have a smooth transition area before entering the ejection pipe 2, thereby reducing turbulence and vortexes and improving the flow stability when the air and gas are mixed.
[0060] It should be noted that the constriction portion m1, the expansion portion m2, and the contraction portion m3 are arranged in sequence along the gas path direction, and any two adjacent portions may be connected or not connected. For example, the contraction portion m1 is connected to the expansion portion m2, the expansion portion m2 is connected to the contraction portion m3, there is a section between the contraction portion m1 and the expansion portion m2 whose cross-sectional area does not change, and there is a section between the expansion portion m2 and the contraction portion m3 whose cross-sectional area does not change.
[0061] Regarding the shape setting of the cross section of the ejector pipe 2, in the present embodiment, the cross section shape of the ejector pipe 2 gradually changes from the shape of the air inlet a1 to the shape of the air outlet a2 along the gas path direction. By gradually setting the cross section shape of the ejector pipe 2, not only can the cross section shape of the ejector pipe 2 be gradually adjusted to the shape of the air outlet a2, so that the mixed gas can occupy the lower space of the outer fire cavity c at the moment of ejection; but also, the turbulence generated when the mixed gas flows in the ejector pipe 2 can be reduced, which is beneficial to the smooth flow and transportation in the ejector pipe 2.
[0062] In the present embodiment, with respect to the shape setting and change of the injection pipe 2, the shape of the air outlet a2 is consistent with the lower part of the cross-sectional shape of the outer fire cavity c, so that the mixed gas ejected from the air outlet a2 can instantly occupy the lower space of the outer fire cavity c, so that the mixed gas ejected from the air outlet a2 can instantly occupy the lower space of the outer fire cavity c without diffusion, which can effectively reduce the flow velocity loss of the mixed gas as a fluid during the flow in the outer fire cavity c, and is beneficial to extend the flow path length of the mixed gas in the outer fire cavity c, thereby improving the uniformity of combustion; in addition, it can also reduce the turbulence and disturbance caused by the need for diffusion of the ejected mixed gas, thereby improving the smoothness of the gas flow.
[0063] More specifically, in this embodiment, the air outlet a2 includes a top edge, a bottom edge and two side edges. The bottom edge of the air outlet a2 is defined by the bottom plate 1a of the shell 1, and the two side edges of the air outlet a2 are respectively defined by the outer ring 1c and the middle ring 1b of the shell 1, so that the specific shape of the air outlet a2 is a quadrilateral, and the mixed gas is ejected from the air outlet a2 close to the outer ring 1c, the middle ring 1b and the bottom plate 1a.
[0064] As for the shape setting of the air inlet a1, in the present embodiment, the shape of the air inlet a1 is set to be circular, and the gas is injected into the center of the air inlet a1 at a high speed, so that the air can be introduced into the introduction pipe 2 in a state of surrounding the gas and mixed with the gas, thereby increasing the contact area between the air and the gas and thus enhancing the mixing effect. In addition, the circular air inlet a1 can reduce the possibility of turbulence and local vortex when the air enters, thereby making the air flow smoother and reducing noise.
[0065] In this embodiment, under the action of high-speed gas injection, air is introduced into the introduction section 21 of the introduction pipe 2, and the gas and air are gradually mixed into a mixed gas in the introduction section 21 along the gas path direction, and then the gas path direction of the mixed gas is gradually changed by the redirection section 22 until it is adjusted to be inclined to the direction of the outer fire cavity c, and then flows in the extension section 23 and extends the flow path length, and finally ejected from the gas outlet a2. During the flow process in the introduction pipe 2, it also successively undergoes the rapid introduction of air by the constriction part m1, the full mixing by the expansion part m2, and the speed-up effect by the contraction part m3, thereby the cross-sectional area of the introduction pipe 2 is also changed along the gas path direction, and the cross-sectional area of the introduction pipe 2 gradually decreases, increases, and decreases along the gas path direction. In addition, the horizontal height of the gas outlet a2 of the introduction pipe 2 is higher than the horizontal height of the gas inlet a1. More specifically, the gas inlet a1 of the introduction pipe 2 is located below the bottom plate 1a of the ignition distributor 11, and the gas outlet a2 is located above the bottom plate 1a of the ignition distributor 11.
[0066] Regarding the change in height of the ejection pipe 2 along the gas path direction, in this embodiment, the ejection pipe 2 includes an upper pipe 2a corresponding to the upper half and a lower pipe 2b corresponding to the lower half, wherein the upper pipe 2a is provided with a first point p1, and the lower pipe 2b is provided with a second point p2 and a third point p3 in sequence along the gas path direction. The upper pipe 2a of the ejection pipe 2 is gradually raised from the head end to the first point p1 along the gas path direction, and then the horizontal height is maintained from the first point p1 to the tail end, while the lower pipe 2b of the ejection pipe 2 is gradually lowered from the head end to the second point p2 along the gas path direction, and gradually raised from the second point p2 to the third point p3, and the horizontal height is maintained from the third point p3 to the tail end. It should be noted that for the upper pipe 2a and the lower pipe 2b, the head ends of both correspond to the position of the air inlet a1, and the tail ends correspond to the position of the air outlet a2.
[0067] In the present embodiment, the change in horizontal height of the upper half pipe 2a along the gas path direction is slower than that of the lower half pipe 2b, and the upper half pipe 2a of the ejector pipe 2 is located in the internal space of the shell 1, which is beneficial to the smooth flow of the mixed gas in the outer fire cavity c. The lower half pipe 2b of the ejector pipe 2 will not affect the smooth flow of the mixed gas in the outer fire cavity c. Therefore, the change in horizontal height of the lower half pipe 2b of the ejector pipe 2 cooperates with the upper half pipe 2a to adapt to the change in the cross-sectional area of the ejector pipe 2.
[0068] In this embodiment, along the gas path direction of the ejection pipe 2, the first point p1 is located between the second point p2 and the third point p3, the second point p2 is located at the expansion part m2, the third point p3 is located at the contraction part m3, and the first point p1 is located at the expansion part m2, or at the contraction part m3, or at the junction of the expansion part m2 and the contraction part m3. The first point p1 is set between the second point p2 and the third point p3, so that the cross-sectional area of the contraction part m3 from the second point p2 to the first point p1 in the first half is smaller than that in the second half from the first point p1 to the third point p3, so as to achieve the effect of buffering the fluid change.
[0069] In the present embodiment, the cross-sectional shape of the upper pipe 2a gradually changes from the air inlet a1 along the direction of the gas path and suddenly changes to the shape of the gas outlet a2 at the first point p1. The change in horizontal height of the upper pipe 2a is gentler than that of the lower pipe 2b. Therefore, the cross-sectional shape of the upper pipe 2a is suddenly changed to the shape of the gas outlet a2 at the first point p1, so that the shape of the upper half of the injection pipe 2 is adjusted in advance to match the shape of the gas outlet a2 and will not cause too much influence on the flow state of the mixed gas; the cross-sectional shape of the lower pipe 2b gradually changes from the air inlet a1 along the direction of the gas path and gradually changes to the shape of the gas outlet a2 at the third point p3. The change in horizontal height of the lower pipe 2b is steeper than that of the upper pipe 2a. Therefore, the cross-sectional shape of the upper pipe 2a is gradually changed to the shape of the gas outlet a2 at the third point p3, so that the cross-sectional shape of the upper pipe 2a changes more gently, which is conducive to stabilizing the flow state of the mixed gas.
[0070] More specifically, in this embodiment, both sides of the inner wall of the upper half pipe 2a have convex corner structures d formed by protrusions at the first position p1, so that the cross-sectional shape of the upper half pipe 2a suddenly changes at the first position p1.
[0071] As for the specific structural setting of the ejection pipe 2, in the present embodiment, the bottom plate 1a of the ignition distributor 11, i.e., the bottom plate 1a of the shell body 1, has a sinking section 1s extending circumferentially and recessed downward, the head of the sinking section 1s is provided with an opening and forms an air inlet a1 of the ejection pipe 2, i.e., the sinking area of the bottom plate 1a and a section of the bottom plate 1a extending from the tail of the sinking area constitute the lower half pipe 2b of the ejection pipe 2, a cover plate 3 is circumferentially arranged in the shell body 1, the cover plate 3 is connected to the bottom plate 1a of the shell body 1 by a section extending from the head end along the gas path direction, the cover plate 3 constitutes the upper half pipe 2a of the ejection pipe 2, the tail end of the cover plate 3 and the bottom plate 1a, the outer ring 1c, and the middle ring 1b of the shell body 1 define an air outlet a2 of the ejection pipe 2. Based on the above structural arrangement, the air inlet a1 and the front half of the ejection pipe 2 are located below the bottom plate 1a, and the air outlet a2 and the rear half of the ejection pipe 2 are located above the bottom plate 1a.
[0072] In this embodiment, the cover plate 3 extends circumferentially in the shell 1. Due to the arrangement of the cover plate 3, the space in the shell 1 is circumferentially divided into a double-layer space r1 corresponding to the cover plate 3, and a single-layer space r2 not layered by the cover plate 3, wherein the lower space r12 in the double-layer space r1 forms the injection pipe 2, and the upper space r11 of the double-layer space r1 and the single-layer space r2 form an annular outer fire cavity c.
[0073] In this embodiment, the space inside the shell 1 is layered by the cover plate 3, i.e., the upper half of the pipe 2a. The mixed gas is ejected from the lower space r12 in a direction inclined to the outer fire cavity c and enters the single-layer space r2. It flows along the annular direction of the outer fire cavity c at a high speed through the single-layer space r2 and then enters the upper space r11. This can greatly extend the flow path length of the mixed gas in the shell 1, thereby improving the uniformity of combustion. In addition, it should be noted that the mixed gas gradually burns after being ejected from the gas outlet a2, and the flow rate gradually decreases. When the mixed gas is ejected into the outer fire cavity c, the flow rate is the highest, thereby forming a negative pressure environment in the single-layer space r2, and the residual mixed gas that flows from the upper space r11 into the single-layer space r2, which is not burned and has a large flow rate loss, can be sucked in, thereby improving the flow rate of the mixed gas along the annular direction in the outer fire cavity c as a whole.
[0074] In this embodiment, the cross-sectional area of the upper space r11 of the double-layer space r1 gradually decreases along the gas path direction. The mixed gas is continuously burned as it flows in the outer fire cavity c. The gradual reduction in the cross-sectional area of the upper space r11 can reduce the pressure difference, which is beneficial to maintaining the flow rate of the mixed gas and the uniformity of combustion.
[0075] In this embodiment, more specifically, the cover plate 3, i.e., the upper half of the pipe 2a, is formed with a climbing section 31 along its extension direction, and the climbing section 31 is gradually raised along the gas path direction of the outer fire cavity c, so that the horizontal height of the tail end of the cover plate 3 is higher than the horizontal height of the head end. On the one hand, the gradually raised horizontal height of the climbing section 31 matches the continuously shrinking cross-sectional area of the upper space r11, and on the other hand, when the mixed gas flows in the upper space r11, it gradually rises along the climbing section 31, so that the flow path of the mixed gas in the shell 1 is in a spiral upward trend as a whole, which is conducive to its continuous combustion and maintaining the uniformity of combustion.
[0076] In this embodiment, the cover plate 3, i.e., the upper half of the pipe 2a, is formed with a horizontal section 32 along its extension direction. The horizontal section 32 maintains a constant horizontal height along the gas path direction of the outer fire chamber c, and the horizontal section 32 is connected to the climbing section 31 and extends to the middle and rear part of the cover plate 3. The connection point between the climbing section 31 and the horizontal section 32 is the first point p1.
[0077] In this embodiment, the cover plate 3 has an inclined portion 33, which is gradually raised from the inner side plate of the cover plate 3 to the outer side, and the cover plate 3 is formed with an inclined portion 33 near its rear end. The setting of the inclined section can make the mixed gas flowing into the upper space r11 closer to the fire hole 121 of the fire cover, which is conducive to combustion. It should be noted that the inclined portion 33 can cover the horizontal section 32, and can also continue to cover part of the climbing section 31 forward.
[0078] In this embodiment, two ejection pipes 2 are provided, and they are centrally symmetrical about the center of the housing 1. The number of ejection pipes 2 is set according to actual needs, and more than two ejection pipes can be provided.
[0079] Implementation Case 2:
[0080] A gas stove includes a burner, and the burner is as shown in implementation example 1.
[0081] Finally, it should be noted that the above implementation cases are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned implementation cases, those skilled in the art should understand that they can still modify the technical solutions recorded in the aforementioned implementation cases, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the implementation cases of the present invention.
Claims
1. A burner, characterized in that: include: A shell (1) having an annular outer fire cavity (c) inside; An ejection pipe (2) is arranged on the shell (1), and has an air inlet (a1) and an air outlet (a2) at its head end and tail end respectively; the ejection pipe (2) is formed with a contraction section (m1) with a gradually decreasing cross-sectional area, an expansion section (m2) with a gradually increasing cross-sectional area, and a contraction section (m3) with a gradually decreasing cross-sectional area in sequence along the direction of the air path; the cross-sectional shape of the ejection pipe (2) gradually changes from the shape of the air inlet (a1) to the shape of the air outlet (a2) along the direction of the air path; the ejection direction of the air outlet (a2) is tangent to the outer fire cavity (c); The ejector pipe (2) comprises an upper pipe (2a) and a lower pipe (2b), wherein the upper pipe (2a) is provided with a first point (p1), and the lower pipe (2b) is provided with a second point (p2) and a third point (p3) in sequence along the gas path direction; the upper pipe (2a) is gradually raised from the head end to the first point (p1) along the gas path direction, and the horizontal height is maintained from the first point (p1) to the tail end; the lower pipe (2b) of the ejector pipe (2) is gradually lowered from the head end to the second point (p2) along the gas path direction, and is gradually raised from the second point (p2) to the third point (p3), and the horizontal height is maintained from the third point (p3) to the tail end.
2. The burner according to claim 1, characterized in that The level of the air outlet (a2) is higher than the level of the air inlet (a1).
3. The burner according to claim 2, characterized in that: Along the gas path direction of the ejection pipe (2), the first point (p1) is located between the second point (p2) and the third point (p3), the second point (p2) is located at the expansion part (m2), the third point (p3) is located at the contraction part (m3), and the first point (p1) is located at the expansion part (m2), or at the contraction part (m3), or at the junction of the expansion part (m2) and the contraction part (m3).
4. The burner according to claim 3, characterized in that The cross-sectional shape of the upper half pipe (2a) gradually changes from the air inlet (a1) along the air path direction and suddenly changes to the shape of the air outlet (a2) at the first point (p1), and the cross-sectional shape of the lower half pipe (2b) gradually changes from the air inlet (a1) along the air path direction and suddenly changes to the shape of the air outlet (a2) at the third point (p3).
5. The burner according to claim 4, characterized in that Both sides of the inner wall of the upper half pipe (2a) have convex corner structures (d) formed by protrusions at the first position (p1), so that the cross-sectional shape of the upper half pipe (2a) changes suddenly at the first position (p1).
6. The burner according to any one of claims 1 to 5, characterized in that: The shape of the gas outlet (a2) matches the lower part of the cross-sectional shape of the outer fire cavity (c), so that the mixed gas ejected from the gas outlet (a2) instantly occupies the lower space of the outer fire cavity (c).
7. The burner according to claim 6, characterized in that The air outlet (a2) comprises a top edge, a bottom edge and two side edges, the bottom edge of the air outlet (a2) is defined by the bottom plate (1a) of the shell (1), and the two side edges of the air outlet (a2) are respectively defined by the outer ring (1c) and the middle ring (1b) of the shell (1).
8. The burner according to any one of claims 1 to 5, characterized in that: The shape of the air inlet (a1) is set to be circular, so that the air is introduced into the introduction pipe (2) in a state of surrounding the gas and mixed with the gas.
9. The burner according to any one of claims 1 to 5, characterized in that: At least two ejection pipes (2) are provided, and are centrally symmetrical with respect to the center of the shell (1).
10. A gas stove, characterized in that: Comprising the burner according to any one of claims 1 to 9.
Citation Information
Patent Citations
Energy-saving furnace end for kitchen range
CN115727327A
Injection pipe assembly and stove burner comprising same
CN210291875U
Ejecting pipe and combustor with same
CN219140772U