JP3680002B2 - Fine powder fuel combustion system - Google Patents

Fine powder fuel combustion system Download PDF

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Publication number
JP3680002B2
JP3680002B2 JP2001068444A JP2001068444A JP3680002B2 JP 3680002 B2 JP3680002 B2 JP 3680002B2 JP 2001068444 A JP2001068444 A JP 2001068444A JP 2001068444 A JP2001068444 A JP 2001068444A JP 3680002 B2 JP3680002 B2 JP 3680002B2
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Japan
Prior art keywords
furnace
pulverized fuel
burner nozzle
burner
fuel combustion
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JP2001068444A
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Japanese (ja)
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JP2001272004A (en
Inventor
義 玄後
康一 坂本
正志 菱田
知充 横山
章泰 岡元
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Mitsubishi Heavy Industries Ltd
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Mitsubishi Heavy Industries Ltd
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【0001】
【発明の属する技術分野】
本発明は火力発電用ボイラー火炉や化学工業炉等に適用される微粉状燃料燃焼装置に関する。
【0002】
【従来の技術】
図6は従来の微粉状燃料燃焼装置の一例を示す水平断面図である。図中(1)はバーナーノズル、(2)はバーナーノズル開口面、(3)は微粉状燃料供給管、(4)は燃焼補助空気供給路、(5)は風箱、(6)は火炉壁管、(7)は火炉側面、(11)は火炉側面の延長面をそれぞれ示す。
【0003】
微粉状燃料と搬送空気の混合流は、微粉状燃料供給管(3)を通過してバーナーノズル(1)に導かれ、バーナーノズル開口面(2)から火炉内に向かって噴出する。燃焼補助空気は、燃焼補助空気供給路(4)を通過してバーナーノズル(1)に導かれ、微粉状燃料や搬送空気と同様にバーナーノズル開口面(2)から火炉内に向かって噴出する。
【0004】
それらの噴出方向軸線(8)を通る鉛直面は、火炉側面(7)に直交せず傾斜している。噴出した微粉状燃料と搬送空気ならびに燃焼補助空気は火炉内で拡散・混合しながら火炎を形成する。この際に、火炎が火炉壁管(6)に衝突したり、火炉壁面(6)を舐めるような現象が生じたりすると、火炎が火炉壁管(6)によって冷却され、灰中未燃分の増加等の燃焼性の劣化や、火炉壁管(6)にクリンカが付着する、いわゆるクリンカトラブルが発生する可能性がある。
【0005】
そこで従来は火炎が火炉壁管(6)に衝突するのを防止するために、バーナーノズル(1)の近傍に位置する火炉壁管については、火炉側面の延長面(11)上には配置せず、火炎の広がりを考慮して符号(26)に示すように火炉側面(7)と角度αを付けて風箱(5)側に向かって並ぶように配列していた。
【0006】
燃焼補助空気が火炉内部へ噴出する噴出方向軸線は、微粉状燃料と搬送空気が火炉内部へ噴出する噴出方向軸線(8)と同軸となっている。またバーナーノズル(1)の断面形状はその噴出方向軸線(8)を通る鉛直面を対称面として左右が面対称の形状となっている。
【0007】
図7は上記従来の微粉状燃料燃焼装置の周囲に配置される火炉壁管(6)の構造概念図、いわゆるバーナーパネル構造概念図(平面図)を示す。本図中に示された線素1本1本が火炉壁管(6)1本1本を意味している。
【0008】
【発明が解決しようとする課題】
前記従来の微粉状燃料燃焼装置は、灰中未燃分の増加防止やクリンカトラブルの防止を考慮して、前記符号(26)に示すように、火炉側面(7)と角度αを付けて風箱(5)側に向かって並ぶよう配列しており、性能上は十分に実力が発揮できる構造となっている。しかしながら、このような構造を採用することにより、次のような課題が生じており改善が必要とされていた。即ち、
1) 火炉壁管の一部(26)が、火炉側面(7)や火炉側面の延長面(11)と同一平面内に位置しないので、火炉壁管パネルやバーナーパネルの工作が容易でない。
【0009】
2) 火炉壁支持構造物が複雑な構造となる。
【0010】
3) 大容量バーナー、大容量ボイラーの場合には、図6中符号(26)で示される火炉壁管列の長さLが火炉幅もしくは火炉奥行内に占める割合が長くなるから、火炉壁周囲へのアクセスが困難になり、このためメインテナンスに不都合を来すことがある。
【0011】
4) バーナーノズル(1)が比較的火炉外部側に配置されているのでメインテナンス性を損ない易い。
【0012】
【課題を解決するための手段】
本発明者は、前記従来の課題を解決するために、立型角筒状の火炉の側面に設けられ、微粉状燃料と空気の混合流を噴出するバーナーノズルと、上記バーナーノズルに連結されて微粉状燃料と空気を供給する微粉状燃料供給管と、上記微粉状燃料供給管の周囲に燃焼補助空気供給路を形成する風箱とを備え、上記混合流の噴出方向軸線を通る鉛直面が上記火炉の側面に直交しない微粉状燃料燃焼装置において、上記バーナーノズルの形状が上記鉛直面に対して左右非対称であり、かつ上記バーナーノズルの先端部開口面が上記火炉の側面と同一な平面内に位置することを特徴とする微粉状燃料燃焼装置を提案するものである。
【0013】
本発明の微粉状燃料燃焼装置は上記構成を有し、バーナーノズルの形状が微粉状燃料と空気の混合流の噴出方向軸線を通る鉛直面に対して左右非対称で、かつ上記バーナーノズルの先端部開口面が火炉の側面と同一な平面内に位置するので、バーナーノズルの開口面から噴出する微粉状燃料と搬送空気ならびに燃焼補助空気の混合流は、火炉側面およびその延長面もしくはこれらの面の近傍よりも火炉内部側で火炎を形成することができる。
したがって、火炎が火炉壁管に衝突したり、または火炉壁管を舐めたりする現象を防止することができる。
【0014】
【発明の実施の形態】
図1は本発明の実施の第1形態に係る微粉状燃料燃焼装置を示す水平断面図である。図中、(1)はバーナーノズル、(2)はバーナーノズル開口面、(3)は微粉状燃料供給管、(4)は燃焼補助空気供給路、(5)は風箱、(6)は火炉壁管、(7)は火炉側面をそれぞれ示す。
【0015】
微粉状燃料と搬送空気が火炉内部へ噴出する噴出方向軸線(8)は、燃焼補助空気が火炉内部へ噴出する噴出方向軸線と同軸を成し、それら軸線を通る鉛直面は、火炉側面(7)に垂直ではなく傾斜している。バーナーノズル(1)の形状は、前記図6中で示された従来のものとは異なり、上記噴出方向軸線(8)を通る鉛直面に対して左右非対称となっている。
【0016】
このような形状を採用することによりバーナーノズル開口面(2)を火炉側面(7)と同一平面内に位置させることができ、従来のように火炉壁管を火炉側面と角度を持たせて風箱側に向けて配置しなくても、火炎が火炉壁管(6)に衝突したり火炉壁管(6)を舐めたりする現象を生じさせずに燃焼させることができる。
【0017】
図2は本実施形態の微粉状燃料燃焼装置の周囲に配置される火炉壁管(6)の構造概念図、いわゆるバーナーパネル構造概念図(平面図)を示す。前記図7に示された従来の場合と比較すれば、本発明によりバーナーパネル構造が格段に簡素化できることが判る。
【0018】
図3は、本実施形態におけるバーナー部近傍の流動状態を模式的に説明した図である。この図において、(15)は微粉状燃料供給管もしくは燃焼補助空気供給路の模式図、(16)はバーナーノズル模式図、矢印(17)は微粉状燃料と搬送空気もしくは燃焼補助空気の火炉内部への噴出軸線方向速度分布、(18)は火炉側面とαの角度で風箱側へ向かって配置された火炉壁管の模式図、矢印(19)は火炉内旋回火炎の模式図それぞれを示す。
【0019】
本実施形態の微粉状燃料燃焼装置は従来のバーナーに比べて、バーナー近傍における基本的な流動特性が異なる。まず図3(a)に示すように、微粉状燃料と搬送空気の火炉内部への噴出方向軸線(8)に垂直な面に対し、バーナーノズル開口面(2)がβの角度を有する本実施形態においては、微粉状燃料と搬送空気もしくは燃焼補助空気の噴流の流路が長くなるバーナーノズル壁面(20)では、逆側の壁面すなわち微粉状燃料と搬送空気もしくは燃焼補助空気の噴流の流路長が短くなるバーナーノズル壁面(21)よりも噴流の圧力損失が大きくなるから、同噴流の噴出方向は実際には軸線(8)から逸れて壁面(21)側に矢印(22)のように偏向する。そしてその偏向の度合は角度βならびに壁面(20)、(21)内面の摩擦抵抗係数によって異なる。
【0020】
また図3(b)に示すように、従来の微粉状燃料燃焼装置では、火炉側面とαの角度で風箱側に向かって配置された火炉壁管(18)の影響によって、噴流が軸線(8)から(23)で示すように偏向する傾向にあったが、本実施形態においては、そのような火炉壁管(18)とは火炉壁管の配置が異なるため、偏向の度合が小さくなり、噴流は(24)で示すようになる。
【0021】
このように従来の微粉状燃料燃焼装置とはバーナー部近傍の流動様式が異なる影響と併せて、火炉内旋回火炎(19)が噴流に与える影響によって、最終的に本実施形態におけるバーナーの噴流(22)の噴出方向は、実際には軸線(8)から最大15度ないし20度偏向すると推定される。
【0022】
図4は本発明の実施の第2形態に関わる微粉状燃料燃焼装置を示す水平断面図である。本実施形態は、微粉状燃料供給管(3)がバーナーノズル(1)に連結される屈曲部(12)もしくは屈曲部(12)のバーナーノズル(1)側にスワラ式分散器(13)を設置するとともにバーナーノズル(1)近傍に中子式濃淡分離器(14)を設置した微粉状燃料供給管(3)である微粉状燃料燃焼装置の例である。
【0023】
この図において、屈曲部(12)に矢印の方向から流入してきた微粉状燃料と搬送空気の混合流は、屈曲部(12)における遠心力によって濃淡分布を生じ、微粉状燃料の濃度が屈曲部(12)の外周側において濃くなり、逆に内周側において薄くなる。
【0024】
この濃淡分布はスワラ式分散器(13)の作用によって、分布が均一になるように分散される。しかる後、濃度が均一化した混合流は中子式濃淡分離器(14)によって最適な燃焼状態が得られるように濃淡分離が行なわれ、バーナーノズル(1)を通じて火炉内部に噴出される。
【0025】
図5は本発明の実施の第3形態に関わる微粉状燃料燃焼装置を火炉内部から見た正面図である。
本実施形態においては、風箱が2本の微粉状燃料供給管(3)と5つの燃焼補助空気供給路(4)とからなる単位風箱を複数組(図示例では2組)互いに隔離して形成されている。本図においてバーナーノズル開口面(2)は三角形、矩形、ならびに半円と直線の組合わせによる形状など複数種類の形状を有している。
【0026】
【発明の効果】
本発明により次の効果を得ることができる。
1)火炉壁管ならびにバーナーパネルの工作が容易になる。
2)低コストで簡素な構造の火炉壁支持構造物が採用できる。
3)大容量バーナー、大容量ボイラーの場合にも、火炉壁周囲へのアクセスを容易にすることができ、メインテナンス性を良好にすることができる。
4)バーナーノズルの位置を従来以上に火炉内部側に配置することができ、メインテナンス性を良好にすることができる。
【図面の簡単な説明】
【図1】図1は本発明の実施の第1形態に関わる微粉状燃料燃焼装置を示す水平断面図である。
【図2】図2は上記実施形態に関わる火炉壁管の構造概念図である。
【図3】図3は上記実施形態におけるバーナー部近傍の流動状態を模式的に説明する図である。
【図4】図4は本発明の実施の第2形態に関わる微粉状燃料燃焼装置を示す水平断面図である。
【図5】図5は本発明の実施の第3形態に関わる微粉状燃料燃焼装置を示す正面図である。
【図6】図6は従来の微粉状燃料燃焼装置の一例を示す水平断面図である。
【図7】図7は上記従来の微粉状燃料燃焼装置に関わる火炉壁管の構造概念図である。
【符号の説明】
(1) バーナーノズル
(2) バーナーノズル開口面
(3) 微粉状燃料供給管
(4) 燃焼補助空気供給路
(5) 風箱
(6) 火炉壁管
(7) 火炉側面
(8) 微粉状燃料と搬送空気の噴出方向軸線
(11) 火炉側面の延長面
(12) 微粉状燃料供給管屈曲部
(13) スワラ式分散器
(14) 中子式濃淡分離器
(15) 微粉状燃料または燃焼補助空気の供給管路模式図
(16) バーナーノズル模式図
(17) 噴出方向速度分布
(18) 火炉側面よりも風箱側に配置された火炉壁管の模式図
(19) 火炉内旋回火炎の模式図
(20) 噴流の流路長が長い側のバーナーノズル壁面
(21) 噴流の流路長が短い側のバーナーノズル壁面
(22) 偏向した噴流の噴出方向
(23) 従来のバーナーにおける偏向噴流
(24) 本発明のバーナーにおける偏向噴流
(26) 火炉側面とαの角度で風箱側に配置された火炉壁管
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a pulverized fuel combustion apparatus applied to a boiler furnace for thermal power generation, a chemical industrial furnace, or the like.
[0002]
[Prior art]
FIG. 6 is a horizontal sectional view showing an example of a conventional pulverized fuel combustion apparatus. In the figure, (1) is a burner nozzle, (2) is a burner nozzle opening surface, (3) is a pulverized fuel supply pipe, (4) is a combustion auxiliary air supply path, (5) is a wind box, and (6) is a furnace A wall pipe, (7) is a furnace side surface, and (11) is an extended surface of the furnace side surface.
[0003]
The mixed flow of the pulverized fuel and the carrier air passes through the pulverized fuel supply pipe (3), is guided to the burner nozzle (1), and is ejected from the burner nozzle opening surface (2) toward the furnace. The combustion auxiliary air passes through the combustion auxiliary air supply passage (4), is guided to the burner nozzle (1), and is ejected from the burner nozzle opening surface (2) into the furnace in the same manner as the pulverized fuel and the carrier air. .
[0004]
The vertical planes passing through these ejection direction axes (8) are not orthogonal to the furnace side surface (7) but are inclined. The finely pulverized fuel, the carrier air, and the combustion auxiliary air that are ejected form a flame while being diffused and mixed in the furnace. At this time, if a flame collides with the furnace wall tube (6) or a phenomenon such as licking the furnace wall surface (6) occurs, the flame is cooled by the furnace wall tube (6), and the unburned ash content is reduced. There is a possibility that a combustible deterioration such as an increase or a so-called clinker trouble that the clinker adheres to the furnace wall pipe (6) may occur.
[0005]
Therefore, conventionally, in order to prevent the flame from colliding with the furnace wall pipe (6), the furnace wall pipe located in the vicinity of the burner nozzle (1) is disposed on the extension surface (11) of the furnace side surface. In consideration of the spread of the flame, as shown by reference numeral (26), it was arranged so as to be aligned with the furnace side surface (7) and an angle α toward the wind box (5) side.
[0006]
The jetting direction axis line in which the combustion auxiliary air is jetted into the furnace is coaxial with the jetting direction axis (8) in which the pulverized fuel and the carrier air are jetted into the furnace. The cross-sectional shape of the burner nozzle (1) is symmetrical with respect to a vertical plane passing through the ejection direction axis (8) as a symmetry plane.
[0007]
FIG. 7 shows a structural conceptual diagram of a furnace wall tube (6) arranged around the conventional pulverized fuel combustion apparatus, a so-called burner panel structural conceptual diagram (plan view). Each line element shown in the figure means one furnace wall pipe (6).
[0008]
[Problems to be solved by the invention]
The conventional pulverized fuel combustion apparatus has an angle α with respect to the furnace side surface (7) as shown in the reference (26) in consideration of prevention of an increase in unburned ash content and prevention of clinker trouble. It is arranged so as to be lined up toward the box (5) side, and has a structure that can fully demonstrate its performance. However, by adopting such a structure, the following problems have arisen and improvement has been required. That is,
1) Since a part (26) of the furnace wall tube is not located in the same plane as the furnace side surface (7) or the extended surface (11) of the furnace side surface, it is not easy to work on the furnace wall tube panel or the burner panel.
[0009]
2) The furnace wall support structure has a complicated structure.
[0010]
3) In the case of a large-capacity burner and a large-capacity boiler, the length L of the furnace wall tube row indicated by reference numeral (26) in FIG. May be difficult to access, which may cause inconvenience to maintenance.
[0011]
4) Since the burner nozzle (1) is relatively disposed on the outside of the furnace, maintenance is easily impaired.
[0012]
[Means for Solving the Problems]
In order to solve the above-described conventional problems, the present inventor is provided on a side surface of a vertical prismatic furnace and is connected to the burner nozzle that ejects a mixed flow of pulverized fuel and air. A fine powder fuel supply pipe that supplies fine powder fuel and air; and a wind box that forms a combustion auxiliary air supply passage around the fine powder fuel supply pipe, and a vertical plane passing through the jet direction axis of the mixed flow in pulverized fuel combustion apparatus that is not orthogonal to the side of the furnace, the shape of the burner nozzle is asymmetrical with respect to the vertical plane, and the end opening surface side and the same plane of the furnace of the burner nozzle The present invention proposes a pulverized fuel combustion device that is located inside.
[0013]
The pulverized fuel combustion apparatus of the present invention has the above-described configuration, and the shape of the burner nozzle is asymmetrical with respect to the vertical plane passing through the jet direction axis of the mixed flow of pulverized fuel and air, and the tip of the burner nozzle the opening surface is positioned within the side and the same plane of the furnace, pulverized fuel and the carrier air, as well as mixed flow of the combustion auxiliary air ejected from the opening of the burner nozzles, furnace side and the extension surface or these surfaces thereof A flame can be formed on the inner side of the furnace than in the vicinity of.
Therefore, it is possible to prevent a phenomenon in which the flame collides with the furnace wall tube or licks the furnace wall tube.
[0014]
DETAILED DESCRIPTION OF THE INVENTION
FIG. 1 is a horizontal sectional view showing a pulverized fuel combustion apparatus according to a first embodiment of the present invention. In the figure, (1) is a burner nozzle, (2) is a burner nozzle opening surface, (3) is a pulverized fuel supply pipe, (4) is a combustion auxiliary air supply path, (5) is an air box, and (6) is A furnace wall pipe, (7) shows a furnace side surface.
[0015]
A jetting direction axis (8) through which finely pulverized fuel and carrier air are jetted into the furnace is coaxial with a jetting direction axis through which combustion auxiliary air is jetted into the furnace, and the vertical plane passing through these axes is the side surface of the furnace (7 ) Is not vertical but inclined. The shape of the burner nozzle (1) is asymmetrical with respect to the vertical plane passing through the ejection direction axis (8), unlike the conventional one shown in FIG.
[0016]
By adopting such a shape, the burner nozzle opening surface (2) can be located in the same plane as the furnace side surface (7), and the furnace wall tube is angled with respect to the furnace side surface as in the prior art. Even if it does not arrange | position toward a box side, it can be made to burn without producing the phenomenon that a flame collides with a furnace wall pipe (6) or licks a furnace wall pipe (6).
[0017]
FIG. 2 is a structural conceptual diagram of a furnace wall pipe (6) disposed around the pulverized fuel combustion apparatus of the present embodiment, that is, a so-called burner panel structural conceptual diagram (plan view). As compared with the conventional case shown in FIG. 7, it can be seen that the burner panel structure can be greatly simplified by the present invention.
[0018]
FIG. 3 is a diagram schematically illustrating the flow state in the vicinity of the burner portion in the present embodiment. In this figure, (15) is a schematic diagram of a pulverized fuel supply pipe or combustion auxiliary air supply path, (16) is a schematic diagram of a burner nozzle, and (17) is an interior of a furnace of pulverized fuel and carrier air or combustion auxiliary air. (18) is a schematic diagram of a furnace wall tube arranged toward the wind box at an angle α with respect to the side surface of the furnace, and an arrow (19) is a schematic diagram of a swirling flame in the furnace. .
[0019]
The pulverized fuel combustion apparatus according to the present embodiment differs from the conventional burner in basic flow characteristics in the vicinity of the burner. First, as shown in FIG. 3 (a), the burner nozzle opening surface (2) has an angle of β with respect to a surface perpendicular to the axis (8) of the pulverized fuel and carrier air into the furnace. In the form, in the burner nozzle wall surface (20) in which the flow path of the pulverized fuel and the jet flow of the carrier air or the combustion auxiliary air becomes long, the opposite wall surface, that is, the flow path of the jet flow of the pulverized fuel and the carrier air or combustion auxiliary air Since the pressure loss of the jet becomes larger than that of the burner nozzle wall surface (21) whose length becomes shorter, the jet direction of the jet is actually deviated from the axis (8) as indicated by the arrow (22) on the wall surface (21) side. To deflect. The degree of deflection varies depending on the angle β and the frictional resistance coefficient of the inner surfaces of the wall surfaces (20) and (21).
[0020]
Further, as shown in FIG. 3B, in the conventional pulverized fuel combustion apparatus, the jet flows along the axis line (18) due to the influence of the furnace wall pipe (18) arranged toward the wind box side at an angle α with the furnace side surface. 8) to (23) tend to be deflected. However, in this embodiment, since the arrangement of the furnace wall tube is different from that of the furnace wall tube (18), the degree of deflection is reduced. The jet is as shown in (24).
[0021]
Thus, the burner jet in the present embodiment (finally) due to the influence of the swirling flame in the furnace (19) on the jet, together with the influence of the difference in the flow mode in the vicinity of the burner part from the conventional pulverized fuel combustion apparatus. 22) It is estimated that the jetting direction of 22) is actually deflected by a maximum of 15 to 20 degrees from the axis (8).
[0022]
FIG. 4 is a horizontal sectional view showing a pulverized fuel combustion apparatus according to the second embodiment of the present invention. In this embodiment, the swirl type dispersion device (13) is provided on the bent nozzle (1) side of the bent portion (12) or the bent portion (12) where the pulverized fuel supply pipe (3) is connected to the burner nozzle (1). It is an example of the pulverized fuel combustion apparatus which is a pulverized fuel supply pipe (3) which is installed and a core type density separator (14) is installed in the vicinity of the burner nozzle (1).
[0023]
In this figure, the mixed flow of the pulverized fuel and the carrier air that has flowed into the bent portion (12) from the direction of the arrow produces a density distribution due to the centrifugal force in the bent portion (12), and the concentration of the pulverized fuel becomes the bent portion. It becomes darker on the outer peripheral side of (12) and conversely thinner on the inner peripheral side.
[0024]
This density distribution is dispersed so that the distribution is uniform by the action of the swirler type disperser (13). Thereafter, the mixed stream having a uniform concentration is subjected to concentration separation so as to obtain an optimum combustion state by a core-type concentration separator (14), and is jetted into the furnace through a burner nozzle (1).
[0025]
FIG. 5 is a front view of the pulverized fuel combustion apparatus according to the third embodiment of the present invention as seen from inside the furnace.
In the present embodiment, the wind box is separated from each other by a plurality of unit wind boxes (two sets in the illustrated example) composed of two pulverized fuel supply pipes (3) and five combustion auxiliary air supply paths (4). Is formed. In this figure, the burner nozzle opening surface (2) has a plurality of types of shapes such as a triangle, a rectangle, and a combination of a semicircle and a straight line.
[0026]
【The invention's effect】
The following effects can be obtained by the present invention.
1) The furnace wall tube and burner panel can be easily constructed.
2) A furnace wall support structure having a simple structure with low cost can be adopted.
3) Even in the case of a large-capacity burner and a large-capacity boiler, it is possible to easily access the periphery of the furnace wall and to improve the maintainability.
4) The position of the burner nozzle can be arranged on the inner side of the furnace more than before, and the maintenance property can be improved.
[Brief description of the drawings]
FIG. 1 is a horizontal sectional view showing a pulverized fuel combustion apparatus according to a first embodiment of the present invention.
FIG. 2 is a structural conceptual diagram of a furnace wall tube according to the embodiment.
FIG. 3 is a diagram schematically illustrating a flow state in the vicinity of a burner portion in the embodiment.
FIG. 4 is a horizontal sectional view showing a pulverized fuel combustion apparatus according to a second embodiment of the present invention.
FIG. 5 is a front view showing a pulverized fuel combustion apparatus according to a third embodiment of the present invention.
FIG. 6 is a horizontal sectional view showing an example of a conventional pulverized fuel combustion apparatus.
FIG. 7 is a structural conceptual diagram of a furnace wall tube related to the conventional pulverized fuel combustion apparatus.
[Explanation of symbols]
(1) Burner nozzle (2) Burner nozzle opening surface (3) Fine powder fuel supply pipe (4) Combustion auxiliary air supply path (5) Wind box (6) Furnace wall pipe (7) Furnace side face (8) Fine powder fuel And the jet direction axis of the carrier air (11) Extension surface of the furnace side surface (12) Bending part of fine powder fuel supply pipe (13) Swirler type distributor (14) Core type density separator (15) Fine powder fuel or combustion auxiliary Air supply pipe schematic diagram (16) Burner nozzle schematic diagram (17) Ejection direction velocity distribution (18) Schematic diagram of furnace wall tube arranged on the windbox side from the furnace side surface (19) Schematic of swirling flame in the furnace Figure (20) Burner nozzle wall surface (21) with longer jet flow path length Burner nozzle wall surface (22) with shorter jet flow path length Deflection jet flow direction (23) Deflection jet in conventional burner ( 24) In the burner of the present invention Deflection jet (26) Furnace wall tube placed on the wind box side at an angle α with the furnace side

Claims (1)

立型角筒状の火炉の側面に設けられ、微粉状燃料と空気の混合流を噴出するバーナーノズルと、上記バーナーノズルに連結されて微粉状燃料と空気を供給する微粉状燃料供給管と、上記微粉状燃料供給管の周囲に燃焼補助空気供給路を形成する風箱とを備え、上記混合流の噴出方向軸線を通る鉛直面が上記火炉の側面に直交しない微粉状燃料燃焼装置において、上記バーナーノズルの形状が上記鉛直面に対して左右非対称であり、かつ上記バーナーノズルの先端部開口面が上記火炉の側面と同一な平面内に位置することを特徴とする微粉状燃料燃焼装置。A burner nozzle that is provided on a side surface of a vertical rectangular cylindrical furnace and ejects a mixed flow of pulverized fuel and air; a pulverized fuel supply pipe that is connected to the burner nozzle and supplies pulverized fuel and air; A pulverized fuel combustion apparatus comprising a wind box forming a combustion auxiliary air supply passage around the pulverized fuel supply pipe, wherein a vertical plane passing through the jet direction axis of the mixed flow is not orthogonal to a side surface of the furnace, the shape of the burner nozzle is asymmetrical with respect to the vertical plane, and pulverized fuel combustion apparatus end opening face of the burner nozzle, characterized in that located in the side surface and the same plane of the furnace.
JP2001068444A 2001-03-12 2001-03-12 Fine powder fuel combustion system Expired - Lifetime JP3680002B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2001068444A JP3680002B2 (en) 2001-03-12 2001-03-12 Fine powder fuel combustion system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2001068444A JP3680002B2 (en) 2001-03-12 2001-03-12 Fine powder fuel combustion system

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
JP20324995A Division JP3388951B2 (en) 1995-08-09 1995-08-09 Pulverized fuel combustion device

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JP2001272004A JP2001272004A (en) 2001-10-05
JP3680002B2 true JP3680002B2 (en) 2005-08-10

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