JP2020008221A - Solid fuel burner - Google Patents

Abstract

To provide a solid fuel burner excellent in ignitability and flame stability at a time of a low load when a fuel concentration is low, and excellent in maintainability.SOLUTION: A solid fuel burner (1) comprises a fuel nozzle (9) that injects a mixed fluid consisting of solid fuel fed to a bent pipe section (5) and of carrier gas therefor into a furnace (13) from an opening of a straight pipe section (2), a swirl unit (21) having a first swirler (23) that gives swirl to the mixed fluid, a second swirler (24) that gives swirl in the reverse direction relative to the first swirler (23) to the mixed fluid, and a shaft (22) that connects the first swirler (23) and the second swirler (24), and a plurality of supports (26) that connect the swirl unit (21) and the inner face of the fuel nozzle (9) to support the swirl unit (21) on the fuel nozzle (9).SELECTED DRAWING: Figure 2

Description

  The present invention relates to a solid fuel burner using coal, biomass, or the like as a fuel.

  In a combustion device using solid fuel, in order to achieve stable ignition and flame holding, a mixed fluid containing a sufficient concentration of fuel (mixed fluid with fuel and its carrier gas) is supplied to the flame holding section at the burner outlet. It is required to supply. As a conventional technique for enriching a solid fuel inside a burner, the following Patent Document 1 is known.

  In Patent Literature 1, a first swirler (6) and a second swirler (7) are provided on an outer periphery of an oil burner (8) penetrating a fuel nozzle, and a mixed fluid is provided by the first swirler (6). A technique is described in which a second swirler (7) imparts a reverse swirl to a mixed fluid while imparting swirl to the fluid. According to the technique described in Patent Document 1, the first swirler (6) imparts swirling to the mixed fluid, and concentrates the fuel by biasing the fuel outward in the radial direction, so that the fuel concentration is low and the load is low. In addition to improving the ignitability at the time, the second swirler (7) reduces the swirling of the mixed fluid, thereby reducing the scattering of fuel and improving the stability of the flame.

JP-A-2017-15305

According to the configuration described in Patent Literature 1, an oil burner penetrating the center of the fuel nozzle at the time of startup is used, and each swirler is supported by the oil burner.
In a configuration without an oil burner, a support member that penetrates the center of the fuel nozzle is required as a support member for supporting each swirler, as with the oil burner.
However, in the case of the center shaft penetrating type support member, since the swirler on the downstream side is installed at a position near the nozzle opening (furnace side), the support member becomes long. Therefore, it is necessary to increase the outer diameter of the support member to some extent in order to provide sufficient strength for supporting the swivel. When the outer diameter of the support member is increased, the flow path on the upstream side of the swirler is narrowed, and there is a problem that the pressure loss increases.
In the vicinity of the elbow (curved pipe), high-speed fuel particles conveyed from below collide from the side surface of the support member, so that there is a problem that a countermeasure against wear is required.

  An object of the present invention is to provide a solid fuel burner which is excellent in ignitability and flame stability even at a low load with low fuel concentration, suppresses an increase in pressure loss, and is excellent in maintainability.

The above object of the present invention can be achieved by employing the following configuration.
The invention according to claim 1 has a straight pipe section having an opening toward the furnace, and a curved pipe section continuing to the straight pipe section, and a solid fuel supplied to the curved pipe section and a carrier gas thereof. A fuel nozzle for injecting the mixed fluid into the furnace from the opening of the straight pipe portion, a first swirler provided on the center axis side in the straight pipe portion to swirl the mixed fluid, and a first swirler A second swirler provided downstream of the mixed fluid in the flow direction of the mixed fluid to give a swirl in the opposite direction to the first swirler, and the first swirler extending along the axial direction of the fuel nozzle A swivel unit having a shaft body connecting the swirl unit and the second swirler; extending in a radial direction of the fuel nozzle, connecting the swirl unit to an inner surface of the fuel nozzle, and connecting the swirl unit to the fuel A solid fuel bar, comprising: a support member supported by the nozzle. It is.

  The invention according to claim 2 is the solid fuel burner according to claim 1, wherein the first swirler, the second swirler, and the shaft are integrally formed.

  According to a third aspect of the present invention, there is provided the solid fuel burner according to the first or second aspect, further comprising the support connecting the shaft and the inner surface of the fuel nozzle.

  According to a fourth aspect of the present invention, the first swirler constituted by the first swirler which is inclined with respect to the axial direction of the straight pipe portion, and the first swirler are inclined in the opposite direction. The solid fuel burner according to any one of claims 1 to 3, further comprising: a second swirler configured by a second swirler vane.

  According to a fifth aspect of the present invention, there is provided the solid fuel burner according to the fourth aspect, further comprising the support that connects an outer edge of the swirl blade and an inner surface of the fuel nozzle.

  According to a sixth aspect of the present invention, when viewed from the opening side of the straight pipe portion, the mixed fluid flows in the axial direction within an outer diameter of the first swirling blade and the second swirling blade. The solid fuel burner according to claim 4 or 5, further comprising: the first swirling vanes and the second swirling vanes that are arranged so as to be out of phase with each other so as not to penetrate.

According to the first aspect of the present invention, the swivel unit is supported on the inner surface of the fuel nozzle by the support, and is excellent in ignitability and flame stability even at a low fuel concentration and a low load, and increases pressure loss. It is possible to provide a solid fuel burner that is suppressed and has excellent maintainability.
According to the second aspect of the present invention, the manufacturing cost can be reduced as compared with the case where the first swirler, the second swivel, and the shaft are not integrally formed.

According to the third aspect of the invention, the turning unit can be fixed by the support that connects the shaft and the inner surface of the fuel nozzle.
According to the fourth aspect of the invention, it is possible to increase the fuel concentration in the vicinity of the inner surface of the fuel nozzle with the first swirling blade and to weaken the swirling component of the mixed fluid with the second swirling blade.
According to the fifth aspect of the present invention, the length of the support can be reduced as compared with the case where the support is not provided on the outer edge of the swirling blade.
According to the sixth aspect of the present invention, it is possible to easily increase the fuel concentration near the inner surface of the fuel nozzle as compared with the case where the configuration of the present invention is not provided.

It is a side view showing a partial section of a solid fuel burner which is one example of the present invention. FIG. 2A is a perspective view, FIG. 2B is a cross-sectional view, and FIG. 2C is a view as viewed from an opening side. FIG. 3A is a perspective view, FIG. 3B is a cross-sectional view, and FIG. 3C is a view as viewed from the opening side. FIG. 4A is a perspective view, FIG. 4B is a cross-sectional view, and FIG. 4C is a view from the opening side. FIG. 5A is a perspective view, FIG. 5B is a cross-sectional view, and FIG. 5C is a view seen from an opening side.

  Hereinafter, embodiments of the present invention will be described.

FIG. 1 is a side view (schematic diagram) showing a partial cross section of a solid fuel burner according to one embodiment of the present invention.
The solid fuel burner 1 according to the embodiment of the present invention is provided on a wall throat 13 a of a furnace 13. The solid fuel burner 1 has a fuel nozzle 9 having a circular cross section through which a mixed fluid (solid-gas two-phase flow) of fine powder fuel and carrier gas flows. The fuel nozzle 9 has a curved pipe part 5 having a 90 ° bend and a straight pipe part 2 continuous with the curved pipe part 5.

  The solid fuel may be coal, biomass, or a mixture thereof. As the carrier gas for the solid fuel, air is usually used, but a mixed gas of combustion exhaust gas and air can also be used, and the type of fuel and carrier gas are not limited. In the present embodiment, an example is shown in which pulverized coal is used as the solid fuel and air is used as the carrier gas. In the following description, the fuel nozzle 9 may also be referred to as a primary air nozzle 9.

  The end of the straight pipe portion 2 opens toward the furnace 13, and the mixed fluid of pulverized coal and primary air supplied to the primary air nozzle 9 from the direction of arrow A (below) passes through the curved pipe portion 5. The direction changes by approximately 90 °, flows from the straight pipe portion 2 toward the furnace 13, and is ejected from the opening (the outlet of the primary air nozzle 9). The curved tube section 5 may have an L-shaped or U-shaped vertical cross section. Further, the angle of the bent portion of the curved tube portion 5 is not limited to 90 °, and may be larger or smaller. An elbow tube, a bend tube, or the like is used as the curved tube portion 5.

  Further, the secondary air nozzle 3 and the tertiary air nozzle 4 are arranged concentrically around the primary air nozzle 9, and the secondary air and the tertiary air are supplied toward the furnace 13. These air flows are ejected so as to spread in the outer peripheral direction. Further, a flame stabilizer (flame holding ring) 10 is supported around the outlet of the primary air nozzle 9 and between the primary air nozzle 9 and the secondary air nozzle 3. The flame stabilizer 10 is formed in a divergent shape (conical shape) toward the furnace 13 side. Note that a burner in which the flame stabilizer 10 is not installed is also included in the present embodiment.

A circulating flow is formed downstream of the flame stabilizer 10 (furnace 13 side), and a mixture of fuel and air ejected from the primary air nozzle 9, secondary air, high-temperature combustion gas, and the like flow into the circulating flow. And stay. In addition, the temperature of the fuel particles increases due to the radiation heat from the furnace 13. Due to these effects, the solid fuel is ignited downstream of the flame stabilizer 10 and the flame is kept flame.
The air supplied to the secondary air nozzle 3 and the tertiary air nozzle 4 can adjust and control the flow rate and flow rate of air by using a flow rate adjusting member (not shown) such as a damper or an air register.

(Description of swivel unit)
2A and 2B are explanatory diagrams of the turning unit according to the first embodiment. FIG. 2A is a perspective view, FIG. 2B is a cross-sectional view, and FIG. 2C is a view from the opening side.
In FIGS. 1 and 2, a turning unit 21 is disposed downstream of the straight pipe section 2. The turning unit 21 has a spindle unit 22 as an example of a shaft body. The spindle portion 22 is formed in a spindle shape extending along the axial direction of the fuel nozzle 9. Note that the spindle portion 22 is desirably formed in a hollow rod shape for weight reduction and cost reduction, and may be a solid rod shape.
A first swirler 23 as an example of a first swirler is supported on the outer surface of the spindle portion 22 on the upstream side in the flow direction of the mixed fluid. The first turning blade 23 of the first embodiment is configured by four plate-shaped members. The first swirl vanes 23 are supported by the spindle unit 22 in a state of being inclined with respect to the axial direction of the fuel nozzle 9 so that swirl such that the passing mixed fluid is sent to the outside in the radial direction is imparted. I have.

A second swirling blade 24 as an example of a second swirler is supported on the outer surface of the downstream side of the spindle unit 22 with respect to the flow direction of the mixed fluid. The second swirling blade 24 of the first embodiment is configured by four plate-shaped members. The second swirling blade 24 is supported by the spindle unit 22 in a state where the second swirling blade 24 is inclined in a direction opposite to the axial direction of the fuel nozzle 9 with respect to the first swirling blade 23.
In the first embodiment, the angle of inclination of each of the swirling blades 23 and 24 with respect to the axial direction is set to the same angle of inclination. It is also possible to have different inclination angles.

  Each of the swirling blades 23 and 24 of the first embodiment is supported at an interval of 90 °. In the first embodiment, the first swirling blades 23 are arranged at positions of 45 °, 135 °, 225 °, and 315 ° when the phase above the vertical direction is 0 °. In addition, the second swirling vanes 24 are installed at positions of 0 °, 90 °, 180 °, and 270 ° when the phase above the vertical is 0 °. Therefore, as shown in FIG. 2C, the first swirl blade 23 and the second swirl blade 24 of the first embodiment are in the Within the range of the radius of the second swirling vane 24, they are arranged with a phase shift in the circumferential direction so that the mixed fluid does not penetrate in the axial direction. That is, when viewed from the axial direction, the phase and the rotation blade 23 are set so that either the first rotation blade 23 or the second rotation blade 24 exists in a range of 360 ° around the spindle portion 22. , 24 in the circumferential direction are set.

2A and 2B, a support rod 26 as an example of a support member is provided at an outer edge of the second swirling blade 24 (24a) installed at a position of 180 ° in phase. In the first turning blade 23, a support rod 26 as an example of a supporting member is also provided on an outer edge of the first turning blade (23a, 23b) installed at a position of 135 ° and 225 ° in phase. I have. The support rod 26 of the first embodiment is installed at a central position with respect to the longitudinal direction (almost the flow direction) of the swirling blades 23a, 23b, 24a.
Each support rod 26 is formed in a rod shape extending outward in the radial direction. The outer end of the support rod 26 is fixed to the inner wall 9a of the fuel nozzle 9 by welding or the like. Therefore, the turning unit 21 of the first embodiment is fixed to the fuel nozzle 9 at three positions.

Note that the support rod 26 of the first embodiment is integrally formed with each of the turning blades 23a, 23b, and 24a by casting.
Further, in the fuel nozzle 9 of the first embodiment, a portion 2a downstream of the position where the swirling unit 21 is installed is made of a wear-resistant material. That is, although the fuel is not biased toward the inner surface side of the fuel nozzle 9 in the upstream portion 2b than the swirl unit 21, the fuel is biased in the downstream portion 2a than the swirl unit 21 and the inner surface of the fuel nozzle 9 is easily worn. Therefore, it is made of a wear-resistant material.
A member that forms a hollow portion where no structure is installed in the fuel nozzle 9 on the upstream side of the turning unit 21 and penetrates a collision plate provided on the outer peripheral side of the curved tube portion 5 through a flange portion. Is not desirably provided.

(Operation of First Embodiment)
In the solid fuel burner 1 according to the first embodiment having the above-described configuration, the mixed fluid containing the fuel supplied to the fuel nozzle 9 is swirled when passing through the first swirling blade 23. Therefore, the fuel moves radially outward due to the centrifugal effect of the swirl, and the fuel concentration near the inner surface of the fuel nozzle 9 increases. Then, when the swirled fluid passes through the second swirling blade 24, a reverse swirl is applied. Therefore, the swirling component of the fluid is canceled and the swirling is weakened. At the burner outlet, the swirl component has a weak flow in a state where the fuel concentration in the vicinity of the flame stabilizer 10 has increased.

Therefore, the ignitability of the fuel (pulverized coal) at the burner outlet is improved. In particular, since the pulverized coal concentration needs to be equal to or higher than a certain value for ignition of pulverized coal, the fuel concentration in the vicinity of the flame stabilizer 10 is increased even at a low load when the average concentration of pulverized coal is low. The ignitability is secured.
If the mixed fluid is strongly swirled at the outlet of the primary air nozzle 9, the pulverized coal particles scatter in the furnace 13 toward the outer periphery of the solid fuel burner 1, thereby decreasing the stability of the flame and reducing the NOx emission. To increase. On the other hand, in the first embodiment, the swirling strength is reduced by the second swirling blade 24 before the mixed fluid is jetted into the furnace 13. Therefore, the stability of the flame is improved, and an increase in NOx emission is also suppressed.

  In the turning unit 21 of the first embodiment, the spindle unit 22, the first turning blade 23, and the second turning blade 24 are unitized. Therefore, as compared with the case where the first swirl blade 23 and the second swirl blade 24 are individually installed on the fuel nozzle 9, the assembly is completed only by attaching the swirl unit 21, and the first swirl blade 23 and the second swirl blade There is no need to adjust the positional relationship such as the spacing and phase of the two swirling vanes 24, and they can be replaced as a unit when they are replaced. Therefore, assemblability and maintainability are improved.

Further, the swivel unit 21 of the first embodiment is integrally formed by casting, so that the manufacture is easy and the cost can be reduced. In particular, in the first embodiment, the support rod 26 is also integrally formed, so that the cost can be further reduced as compared with the case where the support rod 26 is formed separately.
Further, in the swirling unit 21 of the first embodiment, when viewed from the axial direction of the fuel nozzle 9, the mixed fluid penetrates in the axial direction within the radius of the first swirling blade 23 and the second swirling blade 24. The first swirl blade 23 and the second swirl blade 24 are arranged so as not to be disturbed. Therefore, it is reduced that a part of the mixed fluid passes without touching the swirling blades 23 and 24. Therefore, as compared with the case where the mixed fluid can penetrate in the axial direction, the fuel is more likely to be biased toward the inner surface of the fuel nozzle 9, and the fuel enrichment effect is enhanced.

Further, in the swivel unit 21 of the first embodiment, the support rod 26 is supported on the inner surface of the fuel nozzle 9. Therefore, as compared with the case of using a support member (oil burner) of a central shaft penetration type as described in Patent Document 1, the flow path on the upstream side of the swivel unit 21 is not narrowed, and the pressure loss increases. Is suppressed. Therefore, in order to ensure the same flow path cross-sectional area, the inner diameter of the fuel nozzle needs to be increased in the configuration of Patent Document 1, but in the first embodiment, the fuel nozzle is larger than the configuration described in Patent Document 1. The inner diameter of the nozzle 9 can be reduced.
Further, in the configuration using the center shaft penetrating type support member described in Patent Document 1, it is necessary to take measures against abrasion of the support member (oil burner) in the curved tube portion 5, but in the first embodiment, this measure is taken. unnecessary. Therefore, there is no need to replace parts due to wear, and it can be expected that the frequency of maintenance can be reduced, resulting in excellent maintainability.

Further, in the turning unit 21 of the first embodiment, the support rod 26 is supported on the outer edges of the turning blades 23a, 23b, 24a. Therefore, the length of the support rod 26 can be reduced as compared with the case where the support rod 26 is supported by the spindle unit 22.
Therefore, it is possible to narrow the range of the portion (the support rod 26) requiring a measure against abrasion, and it is possible to reduce the material cost. In particular, when the support rod 26 is made of another material such as an expensive wear-resistant material, the cost reduction effect is high. Further, when the support rod 26 is short, the flow of the mixed fluid is less likely to be hindered than when the support rod 26 is long. Therefore, ignitability and flame stability are also improved.

  In the solid fuel burner 1 according to the first embodiment, the downstream portion 2a of the straight pipe portion 2 is made of a wear-resistant material, and the life of the straight pipe portion 2 is extended. Therefore, the frequency of component replacement is reduced, and the maintainability is improved.

3A and 3B are explanatory views of the turning unit according to the second embodiment. FIG. 3A is a perspective view, FIG. 3B is a cross-sectional view, and FIG. 3C is a view from the opening side.
Next, a description will be given of a second embodiment of the present invention. In the description of the second embodiment, the same reference numerals are given to components corresponding to the components of the first embodiment, and a detailed description thereof will be omitted. I do.
The second embodiment differs from the first embodiment in the following points, but has the same configuration as the first embodiment in other points.
In FIG. 3, in the turning unit 21 of the second embodiment, unlike the first embodiment in which the support rod 26 is disposed at the center in the longitudinal direction of the turning blades 23a, 23b, and 24a, the support rod 31 is different from the second turning blade. 24 are disposed at both ends (upstream and downstream) in the longitudinal direction. The support rod 31 according to the second embodiment is, as it were, formed so that the outer end of the second swirling blade 24 extends in the radial direction.

(Operation of the Second Embodiment)
In the revolving unit 21 of the second embodiment having the above-described configuration, similar to the first embodiment, it is possible to improve the maintainability while securing the ignitability and the stability of the flame.
Further, in the second embodiment, the support rod 31 is provided on the second turning blade 24, but it is also possible to provide the support rod 31 on the first turning blade 23. A support rod 31 is provided on the first swirl vane 23 on the upstream side before the fuel is deflected radially outward, and is supported by the second swirl vane 24 on the downstream side after the fuel is deflected radially outward. When the rod 31 is not provided, wear of the support rod 31 is suppressed, and a longer life can be expected.

4A and 4B are explanatory views of the turning unit according to the third embodiment. FIG. 4A is a perspective view, FIG. 4B is a cross-sectional view, and FIG. 4C is a view from the opening side.
Next, a third embodiment of the present invention will be described. In the description of the third embodiment, the same reference numerals are given to components corresponding to the components of the first and second embodiments, and a detailed description thereof will be given. Is omitted.
The third embodiment differs from the first and second embodiments in the following points, but has the same configuration as the first and second embodiments in other points.
In FIG. 4, in the swivel unit 21 of the third embodiment, unlike the first embodiment in which the support rod 26 is disposed on the swirling blades 23 a, 23 b, and 24 a, the support rod 32 is formed in a rod shape penetrating the spindle unit 22. I have. The support rod 32 of the third embodiment is formed in a shape in which two rods penetrate the spindle part 22 in a cross shape.

(Operation of Embodiment 3)
Also in the swivel unit 21 of the third embodiment having the above-described configuration, similar to the first and second embodiments, the ignitability and the stability of the flame can be secured, and the maintainability can be improved.
Since the fuel concentration of the support rod 32 becomes higher toward the outer end, the wear becomes severe. Therefore, it is desirable to improve the wear resistance by attaching the wear-resistant ceramic ring 33 to the outer end.

5A and 5B are explanatory views of the turning unit according to the fourth embodiment. FIG. 5A is a perspective view, FIG. 5B is a cross-sectional view, and FIG. 5C is a view as viewed from the opening side.
Next, a fourth embodiment of the present invention will be described. In the description of the fourth embodiment, components corresponding to the components of the first to third embodiments are denoted by the same reference numerals, and a detailed description thereof will be given. Is omitted.
The fourth embodiment differs from the first to third embodiments in the following points, but has the same configuration as the first to third embodiments in other points.

In FIG. 5, in the turning unit 21 according to the fourth embodiment, the spindle unit 22 is configured by joining three parts of an upstream part 22a, a middle part 22b, and a downstream part 22c. The first turning blade 23 is formed integrally with the upstream portion 22a, and the second turning blade 24 is formed integrally with the downstream portion 22c.
The middle part 22b is made of a wear-resistant material, and a support rod 36 also made of a wear-resistant material penetrates the middle part 22b in a cross-like manner as in the third embodiment.

(Operation of Fourth Embodiment)
Also in the swivel unit 21 of the fourth embodiment having the above-described configuration, similar to the first to third embodiments, the ignitability and the stability of the flame can be secured, and the maintainability can be improved.
Further, in the swivel unit 21 of the fourth embodiment, since the support rod 36 and the midstream portion 22b are made of a wear-resistant material, wear due to passage of the mixed fluid including fuel is less likely to occur.

(Example of change)
As described above, the embodiments of the present invention have been described in detail. However, the present invention is not limited to the above embodiments, and various changes may be made within the scope of the present invention described in the appended claims. Is possible. Modifications (H01) to (H07) of the present invention are exemplified below.
(H01) In the above embodiment, it is desirable that only the downstream portion 2a of the straight pipe portion 2 be made of a wear-resistant material. However, the entire straight pipe portion 2 may be made of a wear-resistant material. Further, it is also possible to make the whole of a material which is not a wear-resistant material for reasons such as cost reduction and sufficient life.

(H02) In the first and second embodiments, the support rods 26 and 31 are formed separately from the revolving blades 23 and 24, or made of a different material such as a wear-resistant member, and fixed by welding or the like. A configuration is also possible.
(H03) In the above embodiment, it is preferable that the number of the support rods 26, 31, 32, and 36 is smaller because the number of flow path resistance and abraded portions is reduced. Is also possible. Further, the positions at which the support rods 26, 31, 32, and 36 are provided are not limited to the illustrated positions, and can be changed.

(H04) In the above-described embodiment, the number of the rotating blades 23 and 24 is four, but is not limited thereto. The number of sheets can be increased or decreased according to required performance (specifications), design, and the like. Also, the positions and intervals at which the swirling blades 23 and 24 are installed are not limited to the configuration illustrated in the embodiment, and can be arbitrarily changed.
(H05) In the above-described embodiment, the configuration in which the swirling blades 23 and 24 are not rotatable has been exemplified, but the configuration is not limited to this. It is also possible to adopt a configuration that is rotatable around the spindle unit 22. In this case, the support is provided on the spindle unit 22.

(H06) In the above-described embodiment, the plate-like swirling blades 23 and 24 are exemplified as the swirler, but the swirler is not limited to this. Any form to which turning can be applied can be adopted.
(H07) In the above-described embodiment, the configuration in which the turning unit 21 is installed on the downstream side of the straight pipe section 2 is exemplified, but the configuration is not limited to this. It can be installed upstream.

  It can be used as a burner device using solid fuel.

1 ... Solid fuel burner,
2. Straight pipe section
5 ... curved tube part,
9 ... fuel nozzle,
13 ... Furnace,
21 ... Swirl unit,
22 ... shaft,
23 ... First swivel,
24 ... second swirler,
26, 31, 32, 36 ... support.

Claims (6)

A straight pipe section having an opening toward the furnace; and a curved pipe section continuing to the straight pipe section, wherein a mixed fluid of a solid fuel and a carrier gas supplied to the curved pipe section is supplied to the straight pipe section. A fuel nozzle squirting into the furnace from the opening of the
A first swirler provided on the central shaft side in the straight pipe portion to provide swirling to the mixed fluid; and a first swirler provided downstream of the first swirler in a flow direction of the mixed fluid to provide a mixed fluid. A swirler having a second swirler for providing a swirl in a direction opposite to the direction of rotation of the fuel nozzle, and a shaft body extending along the axial direction of the fuel nozzle and connecting the first swirler and the second swirler. When,
A support that extends in the radial direction of the fuel nozzle, connects the swirling unit to the inner surface of the fuel nozzle, and supports the swirling unit on the fuel nozzle;
A solid fuel burner comprising: The solid fuel burner according to claim 1, wherein the first swirler, the second swirler, and the shaft are integrally formed. The support for connecting the shaft and the inner surface of the fuel nozzle,
The solid fuel burner according to claim 1 or 2, further comprising: The first swirler configured by first swirlers inclined with respect to the axial direction of the straight pipe portion;
The second swirler constituted by a second swirl blade inclined in a direction opposite to the first swirl blade;
The solid fuel burner according to any one of claims 1 to 3, further comprising: The support body that connects an outer edge of the swirling blade and an inner surface of the fuel nozzle,
The solid fuel burner according to claim 4, comprising: When viewed from the opening side of the straight pipe portion, the phase in the circumferential direction is set so that the mixed fluid does not penetrate in the axial direction within the range of the outer diameter of the first swirling blade and the second swirling blade. The first swirl vanes and the second swirl vanes, which are shifted from each other;
The solid fuel burner according to claim 4, further comprising:

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