1. A porous media burner, comprising:

the gas mixing device comprises a main body, wherein the main body comprises a cylindrical shell with an accommodating space inside, one end of the cylindrical shell is provided with an opening for mixed gas to enter, a partition is arranged inside the cylindrical shell and divides the accommodating space into a first gas flow space and a second gas flow space which are distributed along the axial direction of the cylindrical shell, the first gas flow space is communicated with the opening, the partition is provided with a first through hole, the first gas flow space is communicated with the second gas flow space through the first through hole, and the side wall of the cylindrical shell is also provided with a second through hole; and

the combustion mechanism is connected with the main body at two axial ends, is annularly arranged on the outer wall of the cylindrical shell and is arranged at intervals with the outer wall of the cylindrical shell to limit an airflow containing cavity, the airflow containing cavity is communicated with the containing space through the second through hole, a porous ceramic body is arranged in the combustion mechanism, and holes of the porous ceramic body are communicated with the airflow containing cavity.

2. The porous medium burner of claim 1, wherein the partition comprises a partition portion and a connecting portion, the partition portion is disposed in the middle of a radial cross section of the cylindrical shell, two ends of the connecting portion are respectively connected with the partition portion and the cylindrical shell, and an edge of the partition portion and an inner wall of the cylindrical shell are disposed at an interval.

3. The porous medium burner according to claim 2, wherein a cross section of the partition portion in a radial direction of the cylindrical shell and a radial cross section of the cylindrical shell are the same, and a ratio of an outer diameter of the partition portion to an inner diameter of the cylindrical shell is 2-3: 4.

4. The porous medium burner according to claim 3, wherein the partition is provided with a communication hole penetrating in a thickness direction of the partition, and a ratio of an area of the communication hole to an area of the partition is 1 to 3: 10.

5. The porous medium burner according to any one of claims 1 to 4, wherein the partition is plate-shaped, and an included angle between a surface of the partition adjacent to the opening and a radial direction of the cylindrical shell is not more than 30 °.

6. The porous-medium burner according to any one of claims 1 to 4, wherein the partition is provided in a middle portion in an axial direction of the cylindrical casing.

7. The porous medium burner of any one of claims 1 to 4, wherein the combustion mechanism comprises a support structure, the support structure is connected with the main body at two axial ends, the support structure is annularly arranged on the outer wall of the cylindrical shell and is arranged at intervals with the outer wall of the cylindrical shell so as to define the airflow accommodating cavity, the airflow accommodating cavity is communicated with the accommodating space through the second through hole, and the support structure is provided with a third through hole along the radial direction; the porous ceramic body is arranged outside the columnar shell in a surrounding mode, the porous ceramic body is fixed on the supporting structure, and holes of the porous ceramic body are communicated with the airflow containing cavity through the third through holes.

8. The porous medium burner as claimed in claim 7, wherein the supporting structure comprises two supporting blocks axially distributed along the cylindrical shell, each of the two supporting blocks has an annular bayonet, the annular bayonets of the two supporting blocks are oppositely arranged, two ends of the porous ceramic body are respectively clamped in the annular bayonets of the two supporting blocks, a fixing member is installed in the airflow accommodating cavity, and two ends of the fixing member in the radial direction are respectively connected with the joints of the cylindrical shell and the two supporting blocks.

9. The porous medium burner of claim 8, wherein the fixing member is disposed around an outer wall of the cylindrical housing and divides the airflow accommodating chamber into a first airflow passage and a second airflow passage, the first airflow passage is communicated with the first airflow space and isolated from the second airflow space, and the second airflow passage is communicated with the second airflow space.

10. A combustion device, comprising a mixed combustion mechanism and the porous medium burner as claimed in any one of claims 1 to 6, wherein the mixed combustion mechanism is used for mixing fuel gas and combustion-supporting gas, and the gas outlet end of the mixed combustion mechanism is communicated with the opening of the cylindrical shell.

Background

With the promotion of national environmental protection policies, emission standards of NOx generated in the combustion process are becoming more and more strict. Porous media combustion is a new combustion technology, and the application of porous media combustion in low-nitrogen combustion is increasingly emphasized.

The cylindrical burner has the advantages of small volume and large combustion specific surface area, and the gas distribution condition of the premixed gas in the cylindrical burner influences the stability of the combustion state.

Disclosure of Invention

An object of the embodiment of this application is to provide a porous medium combustor and burner, its effect that can even combustor gas mixture air current improves the gas mixture evenly distributed degree.

The embodiment of the application is realized as follows:

in a first aspect, embodiments of the present application provide a porous medium burner, including a main body, and a combustion mechanism;

the main body comprises a columnar shell with an accommodating space inside, one end of the columnar shell is provided with an opening for mixed gas to enter, a partition is arranged inside the columnar shell and divides the accommodating space into a first airflow space and a second airflow space which are distributed along the axial direction, the first airflow space is communicated with the opening, the partition is provided with a first through hole, the first airflow space is communicated with the second airflow space through the first through hole, and the side wall of the columnar shell is also provided with a second through hole;

the combustion mechanism is connected with the main part at axial both ends, and the outer wall of column casing and the outer wall interval setting of column casing are located to the combustion mechanism ring to inject the air current and hold the chamber, the air current holds the chamber and communicates through second through-hole and accommodation space, has the porous ceramic body among the combustion mechanism, and the hole and the air current of porous ceramic body hold the chamber intercommunication.

In the technical scheme, the applicant finds that the mixed gas enters the cylindrical combustor and is blown in through the action of the fan, when the mixed gas enters the cylindrical combustor, more mixed gas is concentrated at a position far away from the gas inlet end of the combustor, and therefore the gas is unevenly distributed in the combustor, and the stability of the combustion state is affected. In the scheme of this application embodiment, the separator separates into along the first air current space and the second air current space of axial direction distribution with the accommodation space of cylindricality casing, first air current space and opening intercommunication, and the air current gets into first air current space from the opening, and under the effect of blockking of separator, the gas mixture that gets into second air current space reduces for not setting up the separator occasionally, and the gas mixture in first air current space and the gas mixture evenly distributed degree in second air current space improve. The mixed gas in the first airflow space and the second airflow space enters the airflow containing cavity through the second through hole and then enters the holes of the porous ceramic body for combustion. Because the even distribution degree of the mixed gas in the first airflow space and the mixed gas in the second airflow space is improved, the mixed gas entering the holes of the porous ceramic body is more stable during combustion.

In a possible embodiment, the partition comprises a partition part and a connecting part, the partition part is arranged in the middle of the radial section of the cylindrical shell, two ends of the connecting part are respectively connected with the partition part and the cylindrical shell, and the edge of the partition part and the inner wall of the cylindrical shell are arranged at intervals.

In above-mentioned technical scheme, the separation part mainly plays the effect of blockking the air current, and under the effect of blockking of separation part, the air current enters into the second air current space from the clearance between the edge of separation part and the column casing, and the separation part sets up in the middle part of the radial cross-section of column casing, and the gas mixture can disperse in the region that is close to the edge in second air current space uniformly to can improve the even degree of the gas mixture that gets into the hole of porous ceramic body better.

In a possible embodiment, the cross section of the partition in the radial direction of the cylindrical shell and the radial cross section of the cylindrical shell are the same, and the ratio of the outer diameter of the partition to the inner diameter of the cylindrical shell is 2-3: 4.

In the above technical solution, the applicant has found that the above arrangement mode can better ensure the uniform distribution degree of the mixture in the first airflow space and the second airflow space.

In a possible embodiment, the partition is provided with a communicating hole penetrating through the thickness direction of the partition, and the ratio of the area of the communicating hole to the area of the partition is 1-3: 10.

In the above technical scheme, the occupation ratio of the communication hole to the partition part is small, a small part of the air flow can pass through the communication hole, most of the mixed gas can still be blocked by the partition part, and enters the second air flow space from the gap between the edge of the partition part and the columnar shell, so that the uniformity of the mixed gas entering the holes of the porous ceramic body can be improved.

In one possible embodiment, the partition is plate-shaped, and the angle between the surface of the partition close to the opening and the radial direction of the cylindrical shell is less than or equal to 30 degrees.

In the above technical solution, the applicant has found that, when an included angle between the partition and the cylindrical shell in the radial direction is not greater than 30 °, the mixture in the first airflow space and the second airflow space is more favorably and uniformly distributed.

In one possible embodiment, the partition is provided in the middle of the cylindrical housing in the axial direction.

In the above technical solution, through research and discovery by the applicant, the partition is disposed in the middle of the accommodating space, which is more beneficial to uniformly distribute the mixture of the first airflow space and the second airflow space.

In a possible embodiment, the combustion mechanism comprises a supporting structure, the supporting structure is connected with the main body at two axial ends, the supporting structure is annularly arranged on the outer wall of the cylindrical shell and is arranged at intervals with the outer wall of the cylindrical shell so as to define an airflow containing cavity, the airflow containing cavity is communicated with the containing space through a second through hole, and the supporting structure is provided with a third through hole along the radial direction; the porous ceramic body is annularly arranged outside the columnar shell, the porous ceramic body is fixed on the supporting structure, and holes of the porous ceramic body are communicated with the airflow containing cavity through the third through holes.

In above-mentioned technical scheme, bearing structure provides the support for the porous ceramic body, and the gas mixture in first air current space and second air current space all gets into the air current through the second through-hole and holds the chamber, and the air current holds the chamber and communicates through the hole of third through-hole and porous ceramic body, and then the gas mixture holds the hole that the chamber got into the porous ceramic body from the third through-hole through the air current and burns.

In a possible embodiment, the supporting structure comprises two supporting blocks axially distributed along the columnar shell, the two supporting blocks are respectively provided with an annular bayonet, the annular bayonets of the two supporting blocks are oppositely arranged, two ends of the porous ceramic body are respectively clamped in the annular bayonets of the two supporting blocks, a fixing part is installed in the airflow containing cavity, and two ends of the fixing part in the radial direction are respectively connected with the columnar shell and the joint of the two supporting blocks.

In above-mentioned technical scheme, through establishing the annular bayonet socket at two supporting shoes with the porous ceramic body card, can fix the porous ceramic body better, two supporting shoes of bearing structure pass through the mounting and are connected with the column casing for two supporting shoes are more stable.

In a possible embodiment, the fixing member is annularly arranged on the outer wall of the columnar shell and divides the airflow containing cavity into a first airflow channel and a second airflow channel, the first airflow channel is communicated with the first airflow space and is separated from the second airflow space, and the second airflow channel is communicated with the second airflow space.

In the above technical scheme, the fixing member divides the airflow containing cavity into the first airflow channel and the second airflow channel, the mixed gas in the first airflow space can flow into the first airflow channel, the mixed gas in the second airflow space can flow into the second airflow channel, and the first airflow channel and the second airflow channel are divided by the fixing member, so that the mixed gas entering the porous ceramic body from the first airflow channel and the second airflow channel is distributed more uniformly.

In one possible embodiment, the main body includes a first connecting plate and a second connecting plate provided at both ends in the axial direction of the cylindrical housing, the first connecting plate being connected with the cylindrical housing and the support structure and sealing the accommodation space and one end of the airflow accommodation chamber; the outer wall of the columnar shell is connected with a connecting piece, the second connecting plate is connected with the supporting structure and seals the other end of the airflow containing cavity, and the second connecting plate is detachably connected with the connecting piece.

In above-mentioned technical scheme, it is fixed with column casing and bearing structure's one end through first connecting plate, thereby be connected bearing structure and column casing's the other end fixedly through second connecting plate and connecting piece, because the second connecting plate can be dismantled with the connecting piece and be connected, then can conveniently dismantle the condition of inspection column casing and bearing structure.

In a second aspect, the embodiment of the present application provides a combustion apparatus, including a mixed combustion mechanism and the porous medium burner of the embodiment of the first aspect, the mixed combustion mechanism is used for mixing fuel gas and combustion-supporting gas, and an air outlet end of the mixed combustion mechanism is communicated with an opening of the cylindrical shell.

In the above technical scheme, the gas and the combustion-supporting gas are mixed through the mixed combustion mechanism, and then the mixed combustion mechanism is introduced into the cylindrical shell, and the mixed gas in the first airflow space and the mixed gas in the second airflow space are uniformly distributed to a higher degree, so that the mixed gas entering the holes of the porous ceramic body is more stable during combustion.

In a possible embodiment, mix and fire the mechanism and include the hybrid tube, the gas pipe with help the gas pipe, the one end of gas pipe is followed the length direction setting of hybrid tube in the hybrid tube, the inner wall of hybrid tube and the outer wall of gas pipe pass through annular seal plate sealing connection, the tip that stretches into the hybrid tube of gas pipe is sealed, the lateral wall of gas pipe has the gas hole, the inside of gas hole intercommunication gas pipe and the inside of hybrid tube, help giving vent to anger the end of gas pipe and the inside intercommunication of hybrid tube, the hybrid tube internally mounted has the whirl piece that is used for the mist to pass through.

Among the above-mentioned technical scheme, the gas is from the gas pipe inside the gas hole enters into the mixing tube, combustion-supporting gas gets into the mixing tube from combustion-supporting gas pipe inside, gas and combustion-supporting gas mix at the mixing tube inside, because the gas pipe is the lateral wall that sets up at the gas pipe, then the gas distributes around the gas pipe, be favorable to gas and combustion-supporting gas homogeneous mixing, mixing tube internally mounted has the spinning disk, the spinning disk can restrict the gas mixture and disperse relatively evenly in the inside of mixing tube, strengthen the gas and the homogeneous mixing degree of combustion-supporting gas.

In a possible embodiment, the rotational flow plate comprises a plurality of blades, and the rotational flow angle of each blade is 32-45 degrees.

In the technical scheme, the applicant researches and discovers that when the swirl angle of the blade is 32-45 degrees, the uniform mixing of the fuel gas and the combustion-supporting gas is facilitated.

In a possible embodiment, the gas pipe is arranged coaxially with the mixing pipe.

In the technical scheme, the gas pipe and the mixing pipe are coaxially arranged, so that the uniform distribution degree of the gas in the mixing pipe can be enhanced, and the uniform mixing degree of the gas and the combustion-supporting gas is more favorable.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present application and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained from the drawings without inventive effort.

FIG. 1 is a schematic structural view of a porous medium burner according to an embodiment of the present application;

FIG. 2 is a cross-sectional view A-A of FIG. 1;

FIG. 3 is a cross-sectional view taken along line B-B of FIG. 1;

FIG. 4 is a cross-sectional view of C-C of FIG. 1;

FIG. 5 is a schematic structural diagram of a support member according to an embodiment of the present application;

FIG. 6 is a schematic structural diagram of a support member according to an embodiment of the present disclosure from another perspective;

FIG. 7 is a simulated flow velocity distribution in the first and second gas flow spaces of a porous media burner according to an embodiment of the present disclosure;

fig. 8 is a simulated view of the flow velocity distribution of the first gas flow space and the second gas flow space in which the partition member of the present application is not provided;

FIG. 9 is a schematic structural view of a combustion apparatus according to an embodiment of the present application;

fig. 10 is a cross-sectional view of D-D in fig. 9.

Icon: 100-a combustion device; 10-a porous medium burner; 11-a body; 111-a cylindrical shell; 111 a-opening; 1111-a first airflow space; 1112-a second gas flow space; 1113-second via; 112-a separator; 1121 — a first through hole; 1122-a divider; 1123-connecting part; 113-a first connection plate; 114-a second connecting plate; 115-connecting piece; 12-a support structure; 121-a third via; 122-a support block; 122 a-a support; 1221-annular bayonet; 123-a fixing piece; 13-an airflow accommodating cavity; 131-a first air flow channel; 132-a second airflow channel; 14-a porous ceramic body; 20-a co-combustion mechanism; 21-a mixing tube; 22-a gas pipe; 23-a combustion-supporting gas pipe; 231-gas holes; 24-an annular seal plate; 25-a spinning disk; 251-blade.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are some embodiments of the present application, but not all embodiments. The components of the embodiments of the present application, generally described and illustrated in the figures herein, can be arranged and designed in a wide variety of different configurations.

Thus, the following detailed description of the embodiments of the present application, presented in the accompanying drawings, is not intended to limit the scope of the claimed application, but is merely representative of selected embodiments of the application. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.

It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.

In the description of the present application, it should be noted that the terms "middle", "left", "right", "inside", "outside", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings or orientations or positional relationships that the products of the application usually place when in use, and are used only for convenience in describing the present application and for simplicity in description, and do not indicate or imply that the devices or elements being referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present application. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.

In the description of the present application, it is also to be noted that, unless otherwise explicitly specified or limited, the terms "disposed" and "connected" are to be interpreted broadly, e.g., as being either fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present application can be understood in a specific case by those of ordinary skill in the art.

The present embodiment provides a porous medium burner 10, please refer to fig. 1, which includes a main body 11, a supporting structure 12 and a porous ceramic body 14.

The main body 11 includes a cylindrical housing 111 having an accommodating space therein, and one end of the cylindrical housing 111 has an opening 111a for the mixed gas to enter. Illustratively, the cylindrical housing 111 may be a cylindrical housing 111, or may be a polygonal cylindrical housing 111 such as a square or a hexagon.

The inside of the cylindrical housing 111 is provided with a partition 112 (refer to fig. 1 and 3), and the partition 112 partitions the accommodation space into a first airflow space 1111 and a second airflow space 1112 distributed in the axial direction. The first airflow space 1111 is communicated with the opening 111a, the partition 112 is provided with a first through hole 1121, the first airflow space 1111 is communicated with the second airflow space 1112 through the first through hole 1121, and the side wall of the cylindrical housing 111 is further provided with a second through hole 1113. Illustratively, the first airflow space 1111 is located to the right of the second airflow space 1112.

In the research of the applicant, the mixed gas is blown in by the action of the fan when entering the cylindrical burner, and when the mixed gas enters the cylindrical burner, more mixed gas is concentrated at a position far away from the gas inlet end of the burner, so that the gas is unevenly distributed in the burner, and the stability of the combustion state is affected. In the scheme of this application embodiment, the holding space that the separator 112 will become the cylindricality casing is divided into first air current space 1111 and the second air current space 1112 along axial direction distribution, first air current space 1111 and opening 111a intercommunication, and the air current gets into first air current space 1111 from opening 111a, and under the blocking effect of separator 112, the gas mixture that gets into second air current space 1112 reduces to some extent when not setting up separator 112, and the gas mixture homogeneous distribution degree of first air current space 1111 and second air current space 1112 improves.

Illustratively, the partition 112 is plate-shaped, and an angle between a surface of the partition 112 near the opening 111a and the radial direction of the cylindrical housing 111 is ≦ 30 °, for example, 30 °, 20 °, 10 °, 5 °, or 0 °. The applicant researches and discovers that when the included angle between the partition 112 and the radial direction of the cylindrical shell 111 is less than or equal to 30 degrees, the mixed gas of the first gas flow space 1111 and the second gas flow space 1112 can be more favorably and uniformly distributed.

In one possible embodiment, the separator 112 includes a partition portion 1122 and a connection portion 1123, the partition portion 1122 is disposed in the middle of the radial cross section of the cylindrical case 111, both ends of the connection portion 1123 are connected to the partition portion 1122 and the cylindrical case 111, respectively, and the edge of the partition portion 1122 and the inner wall of the cylindrical case 111 are disposed at intervals.

The partition 1122 mainly functions to block the airflow, the airflow enters the second airflow space 1112 from the gap between the edge of the partition 1122 and the cylindrical case 111 by the blocking function of the partition 1122, the partition 1122 is provided in the middle of the radial cross section of the cylindrical case 111, and the air-fuel mixture can be uniformly dispersed in the area near the edge of the second airflow space 1112.

Alternatively, the cross section of the partition 1122 in the radial direction of the cylindrical housing 111 and the radial cross section of the cylindrical housing 111 are the same, for example, both are circular, square. The ratio of the outer diameter of the partition 1122 to the inner diameter of the cylindrical case 111 is 2 to 3: 4.

The applicant finds that the arrangement mode can better ensure the uniform distribution degree of the mixed gas of the first airflow space 1111 and the second airflow space 1112.

Alternatively, the partition 1122 has a communication hole penetrating the partition 1122 in the thickness direction, and the ratio of the area of the communication hole to the area of the partition 1122 is 1-3: 10.

The communication hole has a small occupancy ratio with respect to the partition 1122, a small portion of the air flow can pass through the communication hole, and a large portion of the air-fuel mixture is still blocked by the partition 1122 and enters the second air flow space 1112 through a gap between the edge of the partition 1122 and the cylindrical case 111.

Illustratively, the spacer 112 is provided in the middle of the cylindrical housing in the axial direction.

The applicant has found that the partition 112 is disposed in the middle of the accommodating space, which is more beneficial to uniformly distribute the mixture of the first airflow space 1111 and the second airflow space 1112. The partition 112 is arranged in the middle of the accommodating space, which means that the partition 112 is arranged in a space between 1/3-2/3 intervals of the accommodating space in the axial direction.

In addition, the applicant tested that when the partition 112 was provided at 1/2 in the axial direction of the cylindrical case, and the partition 112 included the partition 1122 and the connection portion 1123, the ratio of the outer diameter of the partition 1122 to the inner diameter of the cylindrical case 111 was 2:3, and the included angle between the face of the partition 112 close to the opening 111a and the radial direction of the cylindrical case 111 was 0 ° (refer to fig. 3), the flow rates of the first air flow space 1111 and the second air flow space 1112 were both around 5, and the mixture distribution was relatively uniform (refer to fig. 7). In contrast, the flow rates of the first airflow space 1111 and the second airflow space 1112 are different from each other in the same manner except that the partition 112 is not provided (see fig. 8).

Wherein, the combustion mechanism is connected with main part 11 at axial both ends, and the combustion mechanism ring is located the outer wall of column casing 111 and is set up with the outer wall interval of column casing 111 to inject the air current and hold chamber 13, the air current holds chamber 13 and communicates with accommodation space through second through-hole 1113, has porous ceramic body 14 in the combustion mechanism, and the hole of porous ceramic body 14 holds chamber 13 with the air current and communicates.

The mixture of the first air flow space 1111 and the second air flow space 1112 enters the air flow accommodating chamber 13 through the second through hole 1113 and then enters the holes of the porous ceramic body 14 for combustion. Since the mixture of the first air flow space 1111 and the mixture of the second air flow space 1112 are uniformly distributed, the mixture entering the holes of the porous ceramic body 14 is more stably combusted.

Further, in a possible embodiment, the combustion mechanism includes a supporting structure 12, the supporting structure 12 is connected to the main body 11 at two ends in the axial direction, the supporting structure 12 is disposed around the outer wall of the cylindrical housing 111 and spaced from the outer wall of the cylindrical housing 111 to define an airflow accommodating chamber 13 (refer to fig. 1 and 2), the airflow accommodating chamber 13 is communicated with the accommodating space through a second through hole 1113, and the supporting structure 12 is opened with a third through hole 121 in the radial direction.

Illustratively, the main body 11 includes a first connecting plate 113 and a second connecting plate 114 provided at both ends in the axial direction of the cylindrical housing 111. As shown in fig. 1, the first connection plate 113 is disposed on the left side, the second connection plate 114 is disposed on the right side, and the first connection plate 113 is connected to the cylindrical housing 111 and the support structure 12 and seals the accommodation space and one end of the airflow accommodating chamber 13. The outer wall of the cylindrical housing 111 is connected to a connector 115, the second connecting plate 114 is connected to the support structure 12 and seals the other end of the airflow accommodating chamber 13, and the second connecting plate 114 is detachably connected to the connector 115.

The one end of column casing 111 and bearing structure 12 is fixed through first connecting plate 113, thereby be connected through second connecting plate 114 and connecting piece 115 with bearing structure 12 fixed with the other end of column casing 111, because second connecting plate 114 can dismantle with connecting piece 115 and be connected, then can conveniently dismantle the condition of inspection column casing 111 and bearing structure 12. Illustratively, the connecting member 115 has a first bolt hole, the second connecting plate 114 has a second bolt hole, and the connecting member 115 and the second connecting plate 114 can be fixed by bolts passing through the first bolt hole and the second bolt hole.

The porous ceramic body 14 is disposed around the exterior of the cylindrical housing 111, the porous ceramic body 14 is fixed to the supporting structure 12, and the holes of the porous ceramic body 14 are communicated with the airflow accommodating chamber 13 through the third through holes 121.

The mixed gas of the first gas flow space 1111 and the second gas flow space 1112 enters the gas flow accommodating cavity 13 through the second through hole 1113, the gas flow accommodating cavity 13 is communicated with the holes of the porous ceramic body 14 through the third through hole 121, and then the mixed gas enters the holes of the porous ceramic body 14 from the third through hole 121 through the gas flow accommodating cavity 13 for combustion. Since the mixture of the first air flow space 1111 and the mixture of the second air flow space 1112 are uniformly distributed, the mixture entering the holes of the porous ceramic body 14 is more stably combusted.

Referring to fig. 1-6, in a possible embodiment, the supporting structure 12 includes two supporting blocks 122 axially distributed along the cylindrical shell 111, the two supporting blocks 122 are axially arranged, each of the two supporting blocks 122 has an annular bayonet 1221, the annular bayonets 1221 of the two supporting blocks 122 are oppositely arranged, two ends of the porous ceramic body 14 are respectively clamped in the annular bayonets 1221 of the two supporting blocks 122, the airflow accommodating cavity 13 is internally provided with a fixing member 123, and two ends of the fixing member 123 along a radial direction are respectively connected with joints of the cylindrical shell 111 and the two supporting blocks 122.

The porous ceramic body 14 can be well fixed by clamping the porous ceramic body 14 at the annular bayonets 1221 of the two supporting blocks 122, and the two supporting blocks 122 of the supporting structure 12 are connected with the cylindrical shell 111 through the fixing pieces 123, so that the two supporting blocks 122 are more stable.

Alternatively, the supporting block 122 includes a plurality of supporting pieces 122a (refer to fig. 5 and 6), and the plurality of supporting pieces 122a are spliced with each other to form the supporting block 122. Illustratively, the supporting block 122 includes a bridge body and a base, the bridge body is annularly disposed outside the cylindrical housing, the base protrudes from the bridge body, and the annular bayonet 1221 is concavely disposed on the base. Illustratively, the support blocks 122 may be selected from a material having a low thermal conductivity and high temperature resistance to facilitate heat dissipation during combustion, for example, the support blocks 122 may be made of alumina fiber board.

Further, referring to fig. 1, in a possible embodiment, the fixing member 123 is disposed around an outer wall of the cylindrical housing 111 and divides the airflow accommodating chamber 13 into a first airflow channel 131 and a second airflow channel 132, the first airflow channel 131 is communicated with the first airflow space 1111 and is isolated from the second airflow space 1112, and the second airflow channel 132 is communicated with the second airflow space 1112.

The fixing member 123 divides the airflow accommodating chamber 13 into a first airflow channel 131 and a second airflow channel 132, the mixed gas in the first airflow space 1111 can flow into the first airflow channel 131, the mixed gas in the second airflow space 1112 can flow into the second airflow channel 132, and the first airflow channel 131 and the second airflow channel 132 are separated by the fixing member 123, so that the mixed gas from the first airflow channel 131 and the second airflow channel 132 respectively enters the porous ceramic body 14, and the mixed gas entering the porous ceramic body 14 is distributed more uniformly.

Referring to fig. 9, the combustion apparatus 100 further includes a mixed combustion mechanism 20 and the porous medium burner 10 of the embodiment of the present application, the mixed combustion mechanism 20 is used for mixing fuel gas and combustion-supporting gas, and an air outlet end of the mixed combustion mechanism 20 is communicated with the opening 111a of the cylindrical housing 111.

The gas and the combustion-supporting gas are mixed by the co-combustion mechanism 20, and then introduced into the cylindrical shell 111 from the co-combustion mechanism 20, and since the uniform distribution degree of the mixture gas in the first gas flow space 1111 and the mixture gas in the second gas flow space 1112 is improved, the mixture gas entering the holes of the porous ceramic body 14 is more stable during combustion.

In a possible embodiment, the mixed combustion mechanism 20 includes a mixing pipe 21, a gas pipe 22 and a combustion-supporting gas pipe 23, one end of the gas pipe 22 is disposed in the mixing pipe 21 along the length direction of the mixing pipe 21, the inner wall of the mixing pipe 21 is connected with the outer wall of the gas pipe 22 through an annular sealing plate 24 in a sealing manner, the end of the gas pipe 22 extending into the mixing pipe 21 is sealed, the side wall of the gas pipe 22 is provided with a gas hole 231, and the gas hole 231 communicates the inside of the gas pipe 22 with the inside of the mixing pipe 21. Illustratively, the sidewall of the gas pipe 22 may be planar or may include an arc.

The gas outlet end of the combustion-supporting gas pipe 23 communicates with the inside of the mixing pipe 21, and a swirl plate 25 (see fig. 10) for passing the mixed gas is installed inside the mixing pipe 21. Illustratively, the oxidant gas pipe 23 extends from the side wall of the mixing pipe 21 into the interior of the mixing pipe 21.

Gas enters into mixing tube 21 inside from gas pipe 22 through gas hole 231, combustion-supporting gas is inside from combustion-supporting gas pipe 23 entering mixing tube 21, gas and combustion-supporting gas are at mixing tube 21 internal mixing, because gas pipe 22 is the lateral wall that sets up at gas pipe 22, then the gas distributes around gas pipe 22, be favorable to gas and combustion-supporting gas homogeneous mixing, mixing tube 21 internally mounted has spinning disk 25, spinning disk 25 can restrict the gas mixture and more evenly disperse in mixing tube 21's inside, strengthen the gas and the homogeneous mixing degree of combustion-supporting gas.

Optionally, the swirl plate 25 comprises a plurality of blades 251, and the swirl angle of the blades 251 is 32-45 degrees, such as 32 degrees, 34 degrees, 37 degrees, 38 degrees, 40 degrees, 42 degrees or 45 degrees.

The applicant researches and discovers that when the rotational flow angle of the blade 251 is 32-45 degrees, the uniform mixing of fuel gas and combustion-supporting gas is facilitated.

Illustratively, the gas pipe 22 is disposed coaxially with the mixing pipe 21. The gas pipe 22 and the mixing pipe 21 are coaxially arranged, and the gas distributed around the gas pipe 22 can be improved in the uniform distribution degree inside the mixing pipe 21, so that the uniform mixing degree of the gas and the combustion-supporting gas is more facilitated.

The operating principle of the combustion apparatus 100 according to the embodiment of the present application is:

inside gas entered into mixing pipe 21 from gas pipe 22 through gas hole 231, combustion-supporting gas entered into mixing pipe 21 from combustion-supporting gas pipe 23, and gas and combustion-supporting gas mix in mixing pipe 21 is inside, and mixing pipe 21 internally mounted has spinning disk 25, and spinning disk 25 can restrict the gas mixture and more evenly disperse in mixing pipe 21's inside, strengthens the misce bene degree of gas and combustion-supporting gas.

The mixed gas enters the first gas flow space 1111 from the mixing pipe 21 through the opening 111a of the cylindrical housing 111, and the mixed gas entering the second gas flow space 1112 is reduced to a certain extent by the blocking action of the partition 112 compared to the case where the partition 112 is not provided, and the degree of uniform distribution of the mixed gas in the first gas flow space 1111 and the mixed gas in the second gas flow space 1112 is improved. The mixed gas of the first gas flow space 1111 and the second gas flow space 1112 enters the gas flow accommodating cavity 13 through the second through hole 1113, the gas flow accommodating cavity 13 is communicated with the holes of the porous ceramic body 14 through the third through hole 121, and then the mixed gas enters the holes of the porous ceramic body 14 from the third through hole 121 through the gas flow accommodating cavity 13 for combustion. Since the mixture of the first air flow space 1111 and the mixture of the second air flow space 1112 are uniformly distributed, the mixture entering the holes of the porous ceramic body 14 is more stably combusted.

The above description is only a preferred embodiment of the present application and is not intended to limit the present application, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the present application shall be included in the protection scope of the present application.