JP3947153B2 - Multi-pipe once-through boiler - Google Patents

Description

  The present invention relates to an improvement of a boiler having a combustion chamber, in particular, a multi-tube type once-through boiler in which the combustion chamber is formed by a water-cooled wall composed of a plurality of water pipes and fins, and lowers NOx, lowers CO and absorbs heat to the water-cooled wall. The present invention relates to a multi-tube type once-through boiler capable of improving the rate.

In general, in a multi-pipe once-through boiler equipped with a premixed diffusion combustion burner, a method of supplying combustion air in multiple stages, a method of exhaust gas recirculation that recirculates part of the exhaust gas to the burner, etc. It has been practiced to reduce NOx emissions. In particular, in the gas-fired diffusion combustion using gas as fuel, the concentration combustion method by diversifying the fuel injection nozzle is adopted to reduce NOx, and in the oil-fired diffusion combustion using oil as fuel. NOx reduction is achieved by atomizing spray of oil fuel.
In these diffusion combustion methods, combustion air is pumped around the fuel ejected from the nozzle, both are forcibly mixed, and this combustion gas is burned in the combustion chamber, so a larger combustion chamber is required. Will be. In addition, the shape of the combustion chamber is restricted by the shape of the flame, and the combustion air rectification and the flame stabilization mechanism are required. As a result, in a multi-tube type once-through boiler equipped with a premixed diffusion combustion burner, there is a problem that the size of the boiler inevitably increases.

  On the other hand, in the case of a multi-tube type once-through boiler equipped with a premixed surface combustion burner that is basically gas-fired, the premixed surface combustion burner is a premixed gas obtained by premixing gas fuel and combustion air. Is supplied to a premixed gas dividing plate made of a porous material such as ceramic, and is uniformly diffused to the premixed gas dividing plate to burn on its surface, so that the flame is divided into premixed gas Many fine divided flames are dispersed on the surface of the plate. As a result, the premixed surface combustion burner has advantages such as being able to shorten the flame compared to the premixed diffusion combustion burner and greatly reducing NOx emissions, and so on. This burner is suitable for boiler miniaturization.

On the other hand, in the field of once-through boilers, miniaturization has been progressing more and more. Recently, in the case of a small once-through boiler with an evaporation amount of 2 t / h class, the furnace load reaches 5000 kW / m ³ h, and premix diffusion The size of the flame of the combustion burner has almost reached the limit due to the performance of the blower.
Therefore, in recent years, premixed surface combustion burners have been mounted in once-through boilers in order to reduce the size (for example, see Patent Document 1 and Patent Document 2).

However, even in a multi-tube once-through boiler equipped with a premixed surface combustion burner, if the supply of premixed gas to the premixed gas dividing plate is not uniform, the combustion temperature is not stable and the surface combustion region is In this case, a local high temperature is generated. As a result, there is a problem that thermal NOx is generated and NOx cannot be reduced.
In addition, since the premixed gas dividing plate is generally formed of a porous material such as ceramic, the premixed gas dividing plate may be distorted or cracked due to a temperature difference generated on the premixed gas dividing plate, or There is also a problem of causing clogging.
Japanese Patent Laid-Open No. 7-12301 JP 11-294702 A

  The present invention has been made in view of such problems, and its purpose is to reduce NOx and CO, and to increase the amount of heat absorption per unit area of the water-cooled wall. It is to provide a multitubular once-through boiler.

In order to achieve the above object, the invention of claim 1 of the present invention forms a combustion chamber by an inner water cooling wall having a circular cross-sectional shape composed of a plurality of water pipes and fins, and an outer peripheral position of the inner water cooling wall. The outer water cooling walls having a circular cross-sectional shape consisting of a plurality of water pipes and fins are arranged concentrically to form an annular gas passage between the inner water cooling wall and the outer water cooling wall, In a multi-tube type once-through boiler in which the upper and lower ends of each water pipe are connected to the upper header and the lower header, respectively, a premixed gas in which gas fuel and combustion air are mixed at the bottom of the combustion chamber A premixed gas supply unit that uniformly distributes the gas to the cross section of the combustion chamber is provided, and a number of ceramic particles or metal particles that allow the premixed gas to pass through the premixed gas supply unit while stirring are stacked in a point contact state. to form a primary particle layer formed by The space surrounded by the primary particle layer above the inner water wall and the primary combustion chamber, also supplied by a plurality of secondary air supply pipe which is arranged in equal intervals in the primary combustion chamber to an intermediate portion of the combustion chamber A plate-like secondary air distributor made of a porous ceramic material or metal material that uniformly distributes the secondary air to the cross section of the combustion chamber is provided, and the secondary air distributor is provided on the secondary air distributor from the primary combustion chamber. Forming a secondary particle layer formed by laminating a large number of ceramic particles or metal particles in a point contact state through which the primary combustion gas and the secondary air from the secondary air distributor are passed with stirring and mixing. The space surrounded by the inner water cooling wall above the bed is used as the secondary combustion chamber, and the inner combustion gas that uniformly flows out the secondary combustion gas in the secondary combustion chamber to the annular gas passage at the upper end of the inner water cooling wall Characterized by the formation of an outlet .

According to a second aspect of the present invention, in the multitubular once-through boiler according to the first aspect, a partition wall is provided at a position below the secondary air distributor, and the secondary air distributor is separated from the secondary air distributor. forming an inlet space to the combustion chamber, also to form a annular gas passage primary combustion gas passes through between the inner side of the water-cooled wall of the primary combustion chamber forming part and the outer water wall, the A particle layer is formed by laminating a large number of ceramic particles or metal particles that allow the primary combustion gas to pass through the gas passage in a point contact state, and the primary combustion gas is placed at the lower end of the inner water cooling wall. A gas outlet for uniformly flowing into the gas passage is formed, and the primary combustion gas that has passed through the particle layer in the gas passage is uniformly distributed to the inlet space and the secondary air distributor at a portion facing the inlet space of the inner water cooling wall. It is characterized in that a gas inlet for inflow is formed .

In the multi-tube once-through boiler according to claim 1 of the present invention, the premixed gas is passed through the primary particle layer and burned under conditions of an air ratio of 0.7 to 0.8 in the primary combustion chamber. A large number of micro flames are formed in the primary combustion chamber and the flame temperature is maintained at 1200 ° C. to 1300 ° C., and a reducing atmosphere combustion region is formed in the primary combustion chamber. As a result, a significant reduction in NOx can be achieved.
In this multi-tube recirculation boiler, the primary combustion gas and the secondary air are stirred and mixed in the secondary particle layer and supplied to the secondary combustion chamber without any uneven mixing. Since the primary combustion gas is completely burned under the conditions of 1.2 to 1.3, the generation of CO can be suppressed, and a significant reduction in CO can be achieved.
Further, in this multitubular once-through boiler, heat absorption to the water-cooled wall in the primary combustion chamber is caused by ceramic particles or metal particles forming a primary particle layer in addition to flame radiation, a secondary air supply pipe and a secondary air supply pipe. It is performed by solid radiation of the secondary air distributor, and heat absorption to the water cooling wall in the secondary combustion chamber is performed by solid radiation of ceramic particles or metal particles forming a secondary particle layer in addition to flame radiation. Therefore, the heat absorption rate is greatly improved. As a result, the multi-pipe once-through boiler of the present invention can be reduced in size as compared with the conventional boiler in which heat absorption to the water cooling wall forming the combustion chamber is performed only by flame radiation.
The multi-tube type once-through boiler according to claim 2 of the present invention can have the following effects in addition to the above effects. That is, in this multitubular once-through boiler, the primary combustion gas passing through the particle layer gives heat to the inner water cooling wall and the outer water cooling wall and the ceramic particles or metal particles forming the particle layer, respectively. Heat is applied to the inner water-cooled wall and the outer water-cooled wall by the contact heat conduction caused by solid radiation and flow of the ceramic particles or metal particles forming the water, and thus heat absorption to the water-cooled wall is further promoted. Further, when the primary combustion gas passes through the particle layer, it is possible to earn a reduction convection time until the secondary combustion is started.

Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings.
FIG. 1 is a schematic longitudinal sectional view of a multitubular once-through boiler according to an embodiment of the present invention. The multitubular once-through boiler includes a plurality of water tubes 1a, 2a and fins 1b, 2b arranged concentrically. An inner water cooling wall 1 and an outer water cooling wall 2 having a circular cross-sectional shape, and an upper header 3 connected to the upper and lower ends of the water pipes 1a and 2a of the two water cooling walls 1 and 2 in communication with each other. And a lower header 4, a premixed gas supply unit 5 disposed at the bottom of the space surrounded by the inner water cooling wall 1, a primary particle layer 6 formed on the premixed gas supply unit 5, and an inner side A secondary air distributor 7 disposed in the middle of the space surrounded by the water cooling wall 1, a secondary air supply pipe 8 for supplying the secondary air A to the secondary air distributor 7, and secondary air A secondary particle layer 9 formed on the distributor 7, a primary combustion chamber 10 formed above the primary particle layer 6, and a secondary A secondary combustion chamber 11 formed above the sub-layer 9 and an annular gas passage 12 formed between the inner water cooling wall 1 and the outer water cooling wall 2, etc. The premixed gas G is subjected to primary combustion under the condition of an air ratio of 0.7 to 0.8, and the primary combustion gas G1 is secondary air A in the secondary combustion chamber 11 to a total air ratio of 1.2 to 1. The secondary combustion gas G2 in the secondary combustion chamber 11 is caused to flow into the gas passage 12 by performing secondary combustion under the condition .3.

  Therefore, in the multitubular once-through boiler, the heat absorption to the boiler water flowing in the water pipe 1a of the inner water cooling wall 1 is caused by the radiation heat transfer by the primary flame in the primary combustion chamber 10 and the secondary combustion chamber. 11, radiation heat transfer by the secondary flame, contact heat transfer (convection heat transfer) by the secondary combustion gas G <b> 2 flowing through the gas passage 12, particles of the primary particle layer 6, particles of the secondary particle layer 9, secondary The heat absorption to the boiler water that is performed by the solid radiation of the air distributor 7 and the secondary air supply pipe 8 and that flows in the water pipe 2a of the outer water cooling wall 2 is the secondary combustion gas G2 that flows in the gas passage 12. It is performed only by contact heat transfer (convection heat transfer).

The inner water cooling wall 1 is formed by connecting a plurality of water pipes 1a in a ring and connecting adjacent water pipes 1a with strip-like fins 1b extending in the vertical direction, and has a circular cross-sectional shape. It is configured with an airtight structure. The space surrounded by the inner water cooling wall 1 is divided into upper and lower parts by a secondary air distributor 7 and a secondary particle layer 9 disposed in the middle of the space, and the lower space is the primary combustion chamber. 10 and the upper space is the secondary combustion chamber 11.
Further, an inner gas outlet 13 is formed at the upper end portion of the inner water-cooling wall 1 so that the secondary combustion gas G2 in the secondary combustion chamber 11 flows out by cutting out the upper end portion of the fin 1b. The secondary combustion gas G2 in the combustion chamber 11 flows out uniformly from the inner gas outlet 13 to the annular gas passage 12.

The outer water cooling wall 2 is formed by connecting a plurality of water pipes 2a in a ring shape in parallel with the inner water cooling wall 1 and connecting adjacent water pipes 2a with strip-like fins 2b extending in the vertical direction. The cross-sectional shape is an airtight structure with a circular shape. This outer water cooling wall 2 is arranged concentrically with the inner water cooling wall 1 at the outer peripheral position of the inner water cooling wall 1, and has an annular shape through which the secondary combustion gas G 2 passes between the inner water cooling wall 1. A gas passage 12 is formed.
Further, an outer gas outlet 14 is formed at the lower end portion of the outer water cooling wall 2 so that the secondary combustion gas G2 in the gas passage 12 flows out by notching the lower end portion of the fin 2b. The secondary combustion gas G2 flowing through the gas is discharged from the outer gas outlet 14 to a flue (not shown).

  The upper header 3 and the lower header 4 are both formed in an annular hollow structure, and are connected to the upper and lower ends of the water pipes 1a and 2a of the inner water cooling wall 1 and the outer water cooling wall 2 in a continuous manner. Yes. The upper header 3 is connected with a steam pipe provided with a steam separator and the like, and the lower header 4 is connected with a water supply pipe provided with a water supply pump or the like (all not shown). The upper header 3 is provided with a refractory ceiling wall 15 that closes the upper surface of the secondary combustion chamber 11.

The premixed gas supply unit 5 is provided at the bottom of the primary combustion chamber 10 and uniformly distributes the premixed gas G, which is a mixture of gaseous fuel and combustion air, to the cross section of the primary combustion chamber 10. It is. The premixed gas supply unit 5 is formed of a perforated plate such as punching metal, a metal mesh, or the like, and is attached to the bottom of the primary combustion chamber 10 and to the lower header 4 in a horizontal posture.
Further, a wind box 16 that covers the lower surface side of the premixed gas supply unit 5 is provided at a position below the premixed gas supply unit 5, and the premixed gas G is distributed to the entire lower surface side of the premixed gas supply unit 5. It can be supplied at the same time.
Note that the premixed gas G supplied into the wind box 16 is a premixed gas G with high mixing accuracy that is sufficiently mixed with gas fuel and combustion air and has no uneven mixing. It is.

The primary particle layer 6 is formed by laminating a number of ceramic particles or metal particles having heat resistance on the premixed gas supply unit 5 in a point contact state, and between the ceramic particles or between the metal particles. A fine passage through which the premixed gas G is passed with stirring is formed. A space surrounded by the inner water cooling wall 1 above the primary particle layer 6 is a primary combustion chamber 10.
If the diameter of the ceramic particles or metal particles forming the primary particle layer 6 is too small, the holes and meshes of the premixed gas supply unit 5 that supports the primary particle layer 6 become unnecessarily small, which is clogged. In addition, the pressure loss in the primary particle layer 6 increases. On the contrary, if the diameter of the ceramic particles or the metal particles is too large, the pressure loss is reduced, but the combustion of the premixed gas G tends to be unstable on the upper surface of the primary particle layer 6. Moreover, regardless of the diameter of the ceramic particles or the metal particles, if the thickness of the primary particle layer 6 becomes too thick, the pressure loss increases more than necessary, and the required blowing function force becomes excessive. On the other hand, if the thickness of the primary particle layer 6 becomes too thin, the combustion of the premixed gas G may become unstable, and the possibility of causing backfire becomes extremely high. For these reasons, it is preferable that the diameter of the ceramic particles or metal particles and the thickness of the primary particle layer 6 are appropriately set according to the combustion conditions and the like.

The secondary air distributor 7 is formed in a circular plate shape from a porous ceramic material or metal material having heat resistance, and the secondary air A is formed from fine pores of the porous ceramic material or metal material. Is uniformly ejected to the cross section of the secondary combustion chamber 11 and the primary combustion gas G1 in the primary combustion chamber 10 is passed to the secondary combustion chamber 11 through the fine holes.
For example, the secondary air distributor 7 is obtained by molding a ceramic powder such as alumina into a disk shape and firing the molded product at an appropriate temperature. You may make it form with a ceramic sintered compact, or you may make it form with the sintered compact of the long fiber which consists of alloys, such as iron, chromium, silicon, aluminum, and yttrium.
The secondary air distributor 7 is supported in a horizontal posture by an annular support member 17 made of a refractory attached to the inner surface of the intermediate portion of the inner water cooling wall 1, and is surrounded by the inner water cooling wall 1. Is divided into upper and lower.
The porosity and thickness of the secondary air distributor 7 are set so that the secondary air A is uniformly distributed to the transverse section of the secondary combustion chamber 11 and the primary combustion gas G1 is allowed to pass uniformly. Has been.

The secondary air supply pipe 8 is formed in a pipe shape from a heat-resistant ceramic material or metal material, and a plurality of the secondary air supply pipes 8 are arranged in the primary combustion chamber 10, and the downstream end portion thereof is the secondary air distributor 7. Is connected to the lower surface side of the slab , and its upstream end is connected to a secondary air blower (not shown). The plurality of secondary air supply pipes 8 are arranged in the primary combustion chamber 10 at regular intervals. As a result, the secondary air A can be evenly supplied to the secondary air distributor 7, and the secondary air A can be more evenly distributed from the secondary air distributor 7 to the cross section of the secondary combustion chamber 11. Can do.

The secondary particle layer 9 is formed by laminating many ceramic particles or metal particles having heat resistance on the secondary air distributor 7 in a point contact state, and between the ceramic particles or between the metal particles. Is formed with a fine passage through which the primary combustion gas G1 and the secondary air A pass while being stirred and mixed. A space surrounded by the inner water cooling wall 1 above the secondary particle layer 9 is a secondary combustion chamber 11.
Of course, the diameter of the ceramic particles or metal particles of the secondary particle layer 9 and the thickness of the secondary particle layer 9 are set to optimum values according to the combustion conditions and the like.

  In the multitubular once-through boiler, the primary air amount of the premixed gas G is set so that the primary combustion chamber 10 performs combustion at an air ratio (excess air ratio) of 0.7 to 0.8. At the same time, the amount of secondary air A is set in the secondary combustion chamber 11 so as to perform combustion at a total air ratio (excess air ratio) of 1.2 to 1.3. The multi-tube once-through boiler is provided with a pilot burner (not shown). The pilot burner is installed at a position near the upper part of the primary particle layer 6 so that the pilot flame faces the upper surface of the primary particle layer 6.

  According to the multi-tube type once-through boiler configured as described above, the premixed gas G obtained by premixing the gas fuel and the combustion air supplied into the wind box 16 at the bottom of the boiler is a premixed gas supply unit. 5 is uniformly distributed in the cross section of the primary combustion chamber 10 and flows uniformly into the primary particle layer 6, passes through the primary particle layer 6 while being stirred in the primary particle layer 6, and is supplied by a pilot burner (not shown). By being ignited, combustion is started in the primary combustion chamber 10.

  At this time, since the premixed gas G is burned at an air ratio of 0.7 to 0.8 in the primary combustion chamber 10, a combustion region of a reducing atmosphere is formed in the primary combustion chamber 10. . Further, the primary flame formed on the upper surface of the primary particle layer 6 becomes a large number of micro flames and emits combustion heat to the inner water-cooled wall 1 forming the primary combustion chamber 10 for comparison between 1200 ° C. and 1300 ° C. At a low temperature. As a result, the generation of NOx in the primary combustion chamber 10 is suppressed. Further, in the primary combustion chamber 10, in addition to the radiation of the primary flame, the ceramic particles or metal particles forming the primary particle layer 6, the solid air radiation of the secondary air supply pipe 8 and the secondary air distributor 7 cause the inside. Heat absorption to the water cooling wall 1 is promoted. In addition, the primary particle layer 6 is formed by laminating ceramic particles or metal particles in a point contact state where they do not adhere to each other, and since the premixed gas G is surface-combusted on the upper surface thereof, the primary particle layer 6 is There is no risk of clogging.

  The primary combustion gas G <b> 1 generated in the primary combustion chamber 10 continues to flow uniformly into the secondary particle layer 9 through the fine holes of the secondary air distributor 7 and distributes the secondary air in the secondary particle layer 9. Passing through the secondary particle layer 9 while being agitated and mixed with the secondary air A that is uniformly distributed and discharged from the vessel 7 to the cross section of the secondary combustion chamber 11, and in the secondary combustion chamber 11 above the secondary particle layer 9. Secondary combustion is performed.

  At this time, in the secondary combustion chamber 11, since the primary combustion gas G1 is subjected to secondary combustion with the secondary air A under the condition of the total air ratio of 1.2 to 1.3, the primary combustion gas G1 is completely discharged. Burned. However, in the secondary combustion chamber 11, the primary combustion gas G1 and the secondary air A are agitated and mixed in the secondary particle layer 9 and burned with no mixing unevenness. As a result, the generation of CO is suppressed. Further, in the secondary combustion chamber 11, in addition to the radiation of the secondary flame formed on the upper surface of the secondary particle layer 9, the inside of the secondary combustion chamber 11 is caused by solid radiation of ceramic particles or metal particles forming the secondary particle layer 9. Heat absorption to the water cooling wall 1 is promoted.

  The secondary combustion gas G2 generated in the secondary combustion chamber 11 flows into the gas passage 12 from the inner gas outlet 13 formed in the inner water cooling wall 1 and descends in the gas passage 12, while the inner water cooling wall. After heat is applied to the first and outer water cooling walls 2, the heat is discharged from the outer gas outlet 14 formed in the outer water cooling wall 2 to the outside through a flue (not shown).

Thus, in the multi-tube recirculation boiler described above, a large number of micro flames are formed in the primary combustion chamber 10 and the flame temperature is maintained at 1200 ° C. to 1300 ° C. However, the premixed gas G Is burned at an air ratio of 1 or less to form a reducing atmosphere combustion region in the primary combustion chamber 10, so that a significant reduction in NOx can be achieved.
In this multi-tube recirculation boiler, the primary combustion gas G1 and the secondary air A are agitated and mixed in the secondary particle layer 9 and supplied to the secondary combustion chamber 11 without mixing unevenness. Thus, the combustion with the total air ratio of 1.2 to 1.3 is performed, so that the primary combustion gas G1 is completely combusted and the CO can be significantly reduced.
Furthermore, according to this multi-tube type once-through boiler, the heat absorption into the boiler water is performed by the radiation heat transfer by the primary flame and the secondary flame in the primary combustion chamber 10 and the secondary combustion chamber 11, the primary particle layer 6 and This is performed by ceramic particles or metal particles forming the secondary particle layer 9, the solid air radiation of the secondary air distributor 7 and the secondary air supply pipe 8. As a result, the heat absorption amount per unit area of the water-cooled wall 1 is increased, and the boiler itself can be reduced in size.

  FIG. 2 is a schematic longitudinal sectional view of a multitubular once-through boiler according to another embodiment of the present invention. The multitubular once-through boiler is a multitubular once-through boiler having the above-described structure (shown in FIG. 1). The partition 18 is provided below the secondary air distributor 7 to form an inlet space 19 to the secondary combustion chamber 11 between the secondary air distributor 7 and the partition 18. In addition, an annular gas passage 12 through which the primary combustion gas G1 passes is formed between the portion forming the primary combustion chamber 10 of the inner water cooling wall 1 and the outer water cooling wall 2, and the gas passage 12 A particle layer 20 through which the primary combustion gas G1 passes is formed, and further, the primary combustion gas G1 in the primary combustion chamber 10 is caused to flow horizontally in a part of the water cooling wall 1 on the inner side to uniformly form the annular gas passage 12. The gas outlet 21 that flows into the gas passage and the particle layer 20 in the gas passage 12 And a gas inlet 22 for uniformly flowing the combustion gas G1 into the inlet space 19 and the secondary air distributor 7 is obtained by respectively formed.

That is, the partition wall 18 is formed in a circular plate shape with a refractory material, and is attached in a horizontal posture at a position below the secondary air distributor 7 and on the inner surface of the inner water cooling wall 1. As a result, an inlet space 19 to the secondary combustion chamber 11 is formed between the secondary air distributor 7 and the partition wall 18.
The gas passage 12 is provided with a refractory 23 in an annular space formed between the inner water cooling wall 1 and the outer water cooling wall 2 and at substantially the same height as the secondary air distributor 7. Thus, a portion forming the primary combustion chamber 10 of the inner water cooling wall 1 and the outer water cooling wall 2 are formed.
Further, the particle layer 20 is formed by laminating a large number of heat-resistant ceramic particles or metal particles in a point contact state on the refractory 23 provided in the gas passage 12 and below the gas passage 12. A fine passage through which the primary combustion gas G1 passes is formed between the ceramic particles or between the metal particles.
And the gas outlet 21 is formed by notching the lower end part of the fin 1b of the water cooling wall 1 inside appropriately, and the primary combustion gas G1 in the primary combustion chamber 10 flows out from the primary combustion chamber 10 in the horizontal direction. Thus, the gas is uniformly introduced into the gas passage 12. Further, the gas inlet 22 is formed by appropriately notching a fin 1b at a portion facing the inlet space 19 of the inner water cooling wall 1, and the primary combustion gas G1 that has passed through the particle layer 20 in the gas passage 12 is formed. Are uniformly introduced into the inlet space 19.
This multitubular once-through boiler has the same structure as the multitubular once-through boiler shown in FIG. 1 except that a partition wall 18, an inlet space 19, a particle layer 20, a gas outlet 21 and a gas inlet 22 are provided. The same reference numerals are assigned to the same parts and members as those in the multi-tube once-through boiler of FIG. 1, and detailed description thereof is omitted.

  According to the multi-tube type once-through boiler configured as described above, the premixed gas G supplied into the wind box 16 at the bottom of the boiler is uniformly distributed in the cross section of the primary combustion chamber 10 by the premixed gas supply unit 5. It is distributed and flows uniformly into the primary particle layer 6, passes through the primary particle layer 6 while being stirred in the primary particle layer 6, and is ignited by a pilot burner (not shown). Start burning.

The primary combustion gas G1 generated in the primary combustion chamber 10 uniformly flows out in the horizontal direction from the gas outlet 21 and flows into the gas passage 12 uniformly, and moves the particle layer 20 in the gas passage 12 upward from below. Flow to the gas inlet 22.
At this time, the primary combustion gas G1 passing through the particle layer 20 gives heat to the ceramic particles or metal particles forming the inner water cooling wall 1 and the outer water cooling wall 2 and the particle layer 20, respectively. The ceramic particles or metal particles forming the particle layer 20 give heat to the inner water cooling wall 1 and the outer water cooling wall 2 by contact heat conduction by solid radiation and flow.

  The primary combustion gas G1 that has passed through the particle layer 20 uniformly flows into the inlet space 19 from the gas inlet 22 and also flows uniformly into the secondary particle layer 9 through the fine holes of the secondary air distributor 7. In the secondary particle layer 9, it passes through the secondary particle layer 9 while being stirred and mixed with the secondary air A that is uniformly distributed and discharged from the secondary air distributor 7 to the cross section of the secondary combustion chamber 11 in the secondary particle layer 9. Secondary combustion is performed in the secondary combustion chamber 11 above the particle layer 9.

  The secondary combustion gas G2 generated in the secondary combustion chamber 11 flows into the space between the inner water cooling wall 1 and the outer water cooling wall 2 from the inner gas outlet 13 formed in the inner water cooling wall 1, and is cooled by water. After heat is applied to the walls 1 and 2, the heat is discharged from the space through a flue (not shown) to the outside.

  This multi-pipe once-through boiler can achieve the same effects as the multi-pipe once-through boiler shown in FIG. However, in this multitubular once-through boiler, the primary combustion gas G1 passing through the particle layer 20 gives heat to the ceramic particles or the metal particles forming the inner water cooling wall 1 and the outer water cooling wall 2 and the particle layer 20, respectively. At the same time, heat is applied to the water cooling walls 1 and 2 because heat is applied to the inner water cooling wall 1 and the outer water cooling wall 2 by contact heat conduction caused by solid radiation and flow of ceramic particles or metal particles forming the particle layer 20. It is further promoted. Further, when the primary combustion gas G1 passes through the particle layer 20, it is possible to earn a reduction convection time until the secondary combustion is started.

  In each of the above embodiments, the present invention has the structure of a multi-tube once-through boiler. However, if the boiler has a combustion chamber formed of a water-cooled wall, it may be a boiler having another structure. good. For example, the present invention may have a structure such as a natural circulation boiler or a forced circulation boiler.

  In each of the above embodiments, the cross-sectional shapes of the water cooling walls 1 and 2 and the combustion chambers 10 and 11 of the multitubular once-through boiler are formed in a circular shape, and the upper header 3 and the lower header 4 are annularly formed. In other embodiments, the water cooling walls 1 and 2, the combustion chambers 10 and 11, the upper header 3 and the lower header 4 of the multitubular once-through boiler are formed in a rectangular shape. Anyway.

1 is a schematic longitudinal sectional view of a multitubular once-through boiler according to an embodiment of the present invention. It is a schematic longitudinal cross-sectional view of the multi-tube type once-through boiler which concerns on other embodiment of this invention.

Explanation of symbols

  1 is an inner water cooling wall, 1a is a water pipe, 1b is a fin, 2 is an outer water cooling wall, 2a is a water pipe, 2b is a fin, 3 is an upper header, 4 is a lower header, 5 is a premixed gas supply unit, and 6 is Primary particle layer, 7 secondary air distributor, 8 secondary air supply pipe, 9 secondary particle layer, 10 primary combustion chamber, 11 secondary combustion chamber, 12 gas passage, 18 partition wall, 19 Is an inlet space, 20 is a particle layer, 21 is a gas inlet, 22 is a gas outlet, A is secondary air, G is a premixed gas, G1 is a primary combustion gas, and G2 is a secondary combustion gas.

Claims (2)

A water cooling wall having a circular cross-sectional shape composed of a plurality of water tubes and fins forms a combustion chamber, and an outer water-cooling wall having a circular cross-sectional shape composed of a plurality of water tubes and fins at the outer peripheral position of the inner water-cooling wall. Are arranged concentrically to form an annular gas passage between the inner water cooling wall and the outer water cooling wall, and the upper and lower ends of the water pipes of the two water cooling walls communicate with the upper header and the lower header, respectively. In a multi-pipe once-through boiler that is connected, a premixed gas supply section is provided at the bottom of the combustion chamber to uniformly distribute the premixed gas, which is a mixture of gaseous fuel and combustion air, across the cross section of the combustion chamber. Forming a primary particle layer formed by laminating a large number of ceramic particles or metal particles passing through the premixed gas with stirring on the premixed gas supply unit, and forming a primary particle layer above the primary particle layer . Primary space surrounded by water cooling wall And baked chamber, also perforated to uniformly distribute the cross-section of the combustion chamber secondary air supplied by a plurality of secondary air supply pipe which is arranged in equal intervals in the primary combustion chamber to an intermediate portion of the combustion chamber A plate-like secondary air distributor made of a qualitative ceramic material or metal material is provided, and the primary combustion gas from the primary combustion chamber and the secondary air from the secondary air distributor are placed on the secondary air distributor. A secondary particle layer is formed by laminating a number of ceramic particles or metal particles that are passed while stirring and mixing in a point contact state, and secondary combustion is performed in the space surrounded by the water cooling wall inside the secondary particle layer. A multi-tube type once-through boiler characterized in that an inner gas outlet for uniformly flowing out the secondary combustion gas in the secondary combustion chamber into the annular gas passage is formed at the upper end of the inner water cooling wall . The multi-tube once-through boiler according to claim 1, wherein a partition wall is provided below the secondary air distributor to form an inlet space to the secondary combustion chamber between the secondary air distributor and the partition wall. also to form a annular gas passage primary combustion gas passes through between the inner side of the water-cooled wall of the primary combustion chamber forming part and the outer water wall, passing through the primary combustion gas into the gas passage A gas outlet for forming a particle layer formed by laminating a large number of ceramic particles or metal particles to be contacted in a point contact state, and further uniformly discharging the primary combustion gas into the gas passage at the lower end of the inner water cooling wall And a gas inlet for uniformly flowing the primary combustion gas that has passed through the particle layer in the gas passage into the inlet space and the secondary air distributor is formed in a portion facing the inlet space of the inner water cooling wall. Features a multi-tube once-through boiler.

Images