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JP3388951B2 - Pulverized fuel combustion device - Google Patents
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JP3388951B2 - Pulverized fuel combustion device - Google Patents

Pulverized fuel combustion device

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Publication number
JP3388951B2
JP3388951B2 JP20324995A JP20324995A JP3388951B2 JP 3388951 B2 JP3388951 B2 JP 3388951B2 JP 20324995 A JP20324995 A JP 20324995A JP 20324995 A JP20324995 A JP 20324995A JP 3388951 B2 JP3388951 B2 JP 3388951B2
Authority
JP
Japan
Prior art keywords
furnace
pulverized fuel
burner nozzle
burner
supply pipe
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP20324995A
Other languages
Japanese (ja)
Other versions
JPH0949613A (en
Inventor
義 玄後
康一 坂本
正志 菱田
知充 横山
章泰 岡元
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP20324995A priority Critical patent/JP3388951B2/en
Publication of JPH0949613A publication Critical patent/JPH0949613A/en
Application granted granted Critical
Publication of JP3388951B2 publication Critical patent/JP3388951B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Description

【発明の詳細な説明】 【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。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(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。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。 【0004】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
る鉛直面に対し左右面対称となっている。 【0005】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。 【0006】 【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。 【0007】2) 火炉壁支持構造物が複雑な構造とな
る。 【0008】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。 【0009】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。 【0010】 【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
バーナーノズルの先端部開口面を上記微粉状燃料供給管
及び燃焼補助空気供給路の先端部を含めて上記鉛直面に
対して左右非対称に形成し、同バーナーノズルの先端部
開口面を上記火炉の側面と同一な平面内に位置させたこ
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。 【0011】本発明の微粉状燃料燃焼装置は上記構成を
有し、バーナーノズルの先端開口面を上記微粉状燃料供
給管及び燃焼補助空気供給路の先端部を含めて上記鉛直
面に対して左右非対称に形成し、かつ、同バーナーノズ
ルの先端部開口面を上記火炉の側面と同一な平面内に位
置させているので、バーナーノズルの先端開口面から噴
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。 【0012】 【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。 【0013】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。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。 【0014】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
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。 【0015】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。 【0016】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。 【0017】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。 【0018】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。 【0019】 【0020】 【0021】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。 【0022】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。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。 【0023】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。 【0024】 【発明の効果】本発明により次の効果を得ることができ
る。 【0025】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。 【0026】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。 【0027】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。 【0028】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。
Description: BACKGROUND OF THE INVENTION 1. Field 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, and the like. 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 fine powder fuel supply pipe, (4) is a combustion auxiliary air supply path, (5) is a wind box, and (6) is a furnace. The wall tube, (7) shows the furnace side, and (11) shows the extension of the furnace side. [0003] The mixed flow of the pulverulent fuel and the carrier air passes through the pulverulent fuel supply pipe (3), is led to the burner nozzle (1), and is ejected from the burner nozzle opening surface (2) into the furnace. . The combustion auxiliary air passes through the combustion auxiliary air supply passage (4) and is guided to the burner nozzle (1), and the burner nozzle opening surface (2) like the pulverized fuel and the carrier air.
Spouts out of the furnace. The vertical plane passing through the ejection direction axis (8) is not perpendicular to the furnace side surface (7) but is inclined. The jetted pulverized fuel, carrier air and combustion auxiliary air form a flame while diffusing and mixing in the furnace. At this time, if the flame collides with the furnace wall tube (6) or a phenomenon such as licking the furnace wall tube (6) occurs, the flame is cooled by the furnace wall tube (6) and unburned ash in the ash is removed. Therefore, there is a possibility that deterioration of flammability such as an increase in the amount of clinker and so-called clinker trouble that the clinker adheres to the furnace wall tube (6) may occur. Therefore, conventionally, in order to prevent the flame from colliding with the furnace wall tube (6), the furnace wall tube located near the burner nozzle (1) is arranged on the extension surface (11) of the furnace side surface. In consideration of the spread of the flame, the wind box (5) is formed at an angle α with the furnace side (7) as shown by reference numeral (26).
They were arranged side by side. [0004] The axis of the ejection direction in which the auxiliary combustion air is ejected into the furnace is coaxial with the axis (8) of the ejection direction in which the pulverized fuel and the carrier air are ejected into the furnace. The cross-sectional shape of the burner nozzle (1) is symmetrical with respect to the vertical plane passing through the ejection direction axis (8). FIG . 7 is a conceptual view (plan view) of a structure of a furnace wall tube (6) disposed around the above-mentioned conventional pulverized fuel combustion apparatus, that is, a so-called burner panel structure. Each wire element shown in the figure means one furnace wall tube (6). The above-mentioned conventional pulverized fuel combustion device is designed to prevent unburned ash in ash from increasing and clinker trouble as shown in the above-mentioned reference numeral (26). The furnace side (7) is arranged at an angle α so as to line up toward the wind box (5), and has a structure capable of fully exhibiting its performance. However, adopting such a structure has caused the following problems, and improvements have been required. 1) Since a part (26) of the furnace wall tube is not located on the same plane as the furnace side surface (7) or the extension surface (11) of the furnace side surface, it is not easy to work the furnace wall tube panel and the burner panel. . 2) The furnace wall support structure has a complicated structure. 3) In the case of a large-capacity burner or a large-capacity boiler, the length L of the furnace wall tube row indicated by reference numeral (26) in FIG. 6 increases in the furnace width or the furnace depth. Access to the surroundings of the furnace wall becomes difficult, which may cause inconvenience to maintenance. 4) Since the burner nozzle (1) is relatively arranged outside the furnace, the maintainability is easily impaired. [0010] In order to solve the above-mentioned conventional problems, the present inventor is provided on a side surface of a vertical prismatic furnace, and ejects a mixed flow of pulverized fuel and air. A burner nozzle, a pulverized fuel supply pipe connected to the burner nozzle to supply pulverized fuel and air, and a wind box forming a combustion auxiliary air supply path around the pulverized fuel supply pipe, In a pulverized fuel combustion device in which a vertical plane passing through an axis of a jet direction of the mixed flow is not orthogonal to a side surface of the furnace, a tip end opening surface of the burner nozzle is connected to a tip end of the pulverized fuel supply pipe and a combustion auxiliary air supply passage. the included formed asymmetrically with respect to the vertical plane, it proposes a pulverized fuel combustion apparatus, characterized in that the end opening surface of the burner nozzle was positioned in the side surface and the same plane of the furnace Is what you do. The pulverized fuel combustion device according to the present invention has the above-described structure, and the opening face of the tip of the burner nozzle is left and right with respect to the vertical plane including the tip of the pulverized fuel supply pipe and the tip of the combustion auxiliary air supply path. formed asymmetrically, and, since the end opening surface of the burner nozzle is positioned within the side surface and the same plane of said furnace, conveying air and combustion with pulverized fuel ejected from the distal end opening face of the burner nozzle The mixed flow of auxiliary air can form a flame on the furnace interior side relative to the furnace side surfaces and extensions or near these surfaces. Therefore, it is possible to prevent the flame from colliding with the furnace wall tube or licking the furnace wall tube. 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 fine powder fuel supply pipe, (4) is a combustion auxiliary air supply path, (5) is a wind box, and (6) is Furnace wall tube, (7)
Indicates the sides of the furnace, respectively. The ejection direction axis (8) from which the pulverized fuel and the carrier air are ejected into the furnace is coaxial with the ejection direction axis from which the auxiliary combustion air is ejected into the furnace, and the vertical plane passing through these axes corresponds to the furnace. The side (7) is not perpendicular but inclined.
The shape of the burner nozzle (1) is different from the conventional one shown in FIG. 6 and is asymmetrical with respect to a vertical plane passing through the ejection direction axis (8). By adopting such a shape, the burner nozzle opening surface (2) can be located in the same plane as the furnace side surface (7),
The flame collides with the furnace wall tube (6) or licks the furnace wall tube (6) without having to arrange the furnace wall tube at an angle to the furnace side surface and facing the wind box side as in the related art. It can be burned without causing a phenomenon. FIG. 2 is a conceptual diagram (plan view) of a structure of a furnace wall tube (6) disposed around the pulverized fuel combustion device of the present embodiment, that is, a so-called burner panel structure. The figure above
7 , it can be seen that the present invention can significantly simplify the burner panel structure. FIG. 3 is a diagram schematically illustrating a flow state in the vicinity of the burner portion in the present embodiment. In this figure, (15) is a schematic view of a pulverized fuel supply pipe or a combustion auxiliary air supply path, (16) is a schematic view of a burner nozzle,
The arrow (17) indicates the axial velocity distribution of the pulverized fuel and carrier air or combustion auxiliary air into the furnace, and (18) indicates the furnace wall tube arranged toward the wind box side at an angle α with the furnace side surface. The schematic diagram and arrow (19) show schematic diagrams of the swirling flame in the furnace, respectively. The pulverized fuel combustion device of the present embodiment differs from the conventional burner in the basic flow characteristics near the burner. First, as shown in FIG. 3A, the burner nozzle opening surface (2) has an angle of β with respect to a plane perpendicular to the axis (8) of the direction in which the pulverized fuel and the carrier air are injected into the furnace. In the embodiment, in the burner nozzle wall surface (20) where the flow path of the jet of the pulverized fuel and the carrier air or the combustion auxiliary air is long, the opposite wall surface, that is, the flow path of the jet of the pulverized fuel and the carrier air or the combustion auxiliary air Since the pressure loss of the jet is larger than that of the burner nozzle wall (21) having a shorter length, the jet direction of the jet is actually deviated from the axis (8) toward the wall (21) as shown by an arrow (22). Deflect. The degree of the deflection depends on the angle β and the coefficient of frictional resistance of the inner surfaces of the wall surfaces (20) and (21). Further, as shown in FIG. 3 (b), in the conventional pulverized fuel combustion apparatus, the jet flow is influenced by the furnace wall tube (18) arranged toward the wind box side at an angle α with respect to the furnace side. Tended to deflect as shown by the axes (8) to (23), but in the present embodiment, the degree of deflection is different because the arrangement of the furnace wall tube is different from that of the furnace wall tube (18). Becomes smaller, and the jet becomes as shown by (24). As described above, in addition to the influence of the different flow pattern in the vicinity of the burner portion from the conventional pulverized fuel combustion device, the burner in the furnace finally influences the jet by the effect of the swirling flame (19) in the furnace. The jet direction of the jet (22) is actually at most 15 degrees to 20 degrees from the axis (8).
It is estimated to be deviated by degrees. FIG . 4 is a horizontal sectional view showing a pulverized fuel combustion device according to a second embodiment of the present invention. In the present embodiment, a swirler-type disperser (13) is provided on the bent portion (12) where the pulverized fuel supply pipe (3) is connected to the burner nozzle (1) or on the burner nozzle (1) side of the bent portion (12). This is an example of a pulverized fuel combustion device which is a pulverized fuel supply pipe (3) in which a core type concentration separator (14) is installed near a burner nozzle (1). In this figure, the mixed flow of the pulverized fuel and the carrier air flowing into the bent portion (12) from the direction of the arrow produces a density distribution due to the centrifugal force at the bent portion (12), and the concentration of the fine powder fuel Becomes thicker on the outer peripheral side of the bent portion (12) and conversely becomes thinner on the inner peripheral side. The density distribution is dispersed by the operation of the swirler type disperser (13) so that the distribution becomes uniform. Thereafter, the mixed stream having a uniform concentration is subjected to density separation by a core type density separator (14) so as to obtain an optimal combustion state, and is discharged into the furnace through the burner nozzle (1). FIG . 5 is a front view of a pulverized fuel combustion apparatus according to a third embodiment of the present invention as viewed from the inside of a furnace. In the present embodiment, the windbox are two pulverized fuel supply pipe (3) and five combustion auxiliary air supply passage (4) and a plurality of sets of units wind box consisting (two pairs in the illustrated example) and isolated from one another It 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 shape obtained by combining a semicircle and a straight line. According to the present invention, the following effects can be obtained. 1) The furnace wall tube and burner panel can be easily manufactured. 2) A furnace wall supporting structure having a simple structure at a low cost can be adopted. 3) Even in the case of a large-capacity burner or a large-capacity boiler, access to the periphery of the furnace wall can be facilitated, and maintenance performance can be improved. [0028] 4) the position of Bananozu Le can be placed in the furnace interior side than ever, it is possible to improve the maintainability.

【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 (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
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a horizontal sectional view showing a pulverized fuel combustion device according to a first embodiment of the present invention. FIG. 2 is a structural conceptual view of a furnace wall tube according to the embodiment. FIG. 3 is a diagram schematically illustrating a flow state near a burner portion in the embodiment. FIG. 4 is a horizontal sectional view showing a pulverized fuel combustion device according to a second embodiment of the present invention. FIG. 5 is a front view showing a pulverized fuel combustion device according to a third embodiment of the present invention. FIG. 6 shows an example of a conventional pulverized fuel combustion device.
It is a horizontal sectional view . FIG. 7 relates to the above-mentioned conventional pulverized fuel combustion device .
It is a structure conceptual diagram of a furnace wall tube . [Description of Signs] (1) Burner nozzle (2) Burner nozzle opening surface (3) Fine powder fuel supply pipe (4) Auxiliary combustion air supply path (5) Wind box (6) Furnace wall pipe (7) Furnace side ( 8) pulverized fuel and injection direction axis of the conveying air (11) extending surface of the furnace side (12) pulverized fuel supply pipe bending portion (13) swirler type disperser (14) inner support ring shades separator (15) Schematic diagram of supply pipe for pulverized fuel or combustion auxiliary air (16) Schematic diagram of burner nozzle (17) Velocity distribution in jet direction (18) Schematic diagram of furnace wall tube arranged closer to wind box than furnace side surface (19) Schematic diagram of the swirling flame in the furnace (20) Burner nozzle wall surface on the side where the flow path length of the jet is long (21) Burner nozzle wall surface on the side where the flow path length of the jet is short (22) Jet direction of the deflected jet (23) Conventional Jet in the burner (24) Furnace wall tubes disposed in the windbox side at an angle of deflection jets (26) and furnace side α in the burner

フロントページの続き (72)発明者 菱田 正志 東京都千代田区丸の内二丁目5番1号 三菱重工業株式会社内 (72)発明者 横山 知充 東京都千代田区丸の内二丁目5番1号 三菱重工業株式会社内 (72)発明者 岡元 章泰 長崎市深堀町5丁目717番1号 三菱重 工業株式会社長崎研究所内 (56)参考文献 特開 昭57−164207(JP,A) 特開 平6−341761(JP,A) 特開 昭57−157913(JP,A) 実開 昭59−71005(JP,U) 特公 平3−10841(JP,B2) (58)調査した分野(Int.Cl.7,DB名) F23C 5/08 - 5/32 F23D 1/00 - 1/06 F27D 17/00 - 23/04 C23C 11/00 F22B 31/00 Continued on the front page (72) Inventor Masashi Hishida 2-5-1 Marunouchi, Chiyoda-ku, Tokyo Inside Mitsubishi Heavy Industries, Ltd. (72) Inventor Tomitsu Yokoyama 2-5-1 Marunouchi, Chiyoda-ku, Tokyo Mitsubishi Heavy Industries, Ltd. (72) Inventor Akiyasu Okamoto 5-717-1 Fukahori-cho, Nagasaki-shi, Nagasaki Laboratory, Mitsubishi Heavy Industries, Ltd. (56) References JP-A-57-164207 (JP, A) JP-A-6-341176 ( JP, A) JP-A-57-157913 (JP, A) JP-A-59-71005 (JP, U) JP-B 3-10841 (JP, B2) (58) Fields investigated (Int. Cl. 7 , DB name) F23C 5/08-5/32 F23D 1/00-1/06 F27D 17/00-23/04 C23C 11/00 F22B 31/00

Claims (1)

(57)【特許請求の範囲】 【請求項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
ノズルの先端部開口面を上記微粉状燃料供給管及び燃焼
補助空気供給路の先端部を含めて上記鉛直面に対して左
右非対称に形成し、同バーナーノズルの先端部開口面を
上記火炉の側面と同一な平面内に位置させたことを特徴
とする微粉状燃料燃焼装置。
(57) [Claims 1] A burner nozzle provided on a side surface of a vertical prismatic furnace, and for ejecting a mixed flow of pulverized fuel and air;
A pulverized fuel supply pipe connected to the burner nozzle for supplying pulverized fuel and air; and a wind box forming a combustion auxiliary air supply path around the pulverized fuel supply pipe, and ejecting the mixed flow. In a pulverized fuel combustion device, a vertical plane passing through a direction axis is not orthogonal to the side surface of the furnace, the opening face of the tip of the burner nozzle is vertically extended including the tip of the pulverized fuel supply pipe and the tip of a combustion auxiliary air supply path. formed asymmetrically with respect to the plane, pulverized fuel combustion apparatus, characterized in that the end opening surface of the burner nozzle was positioned in the side surface and the same plane of the furnace.
JP20324995A 1995-08-09 1995-08-09 Pulverized fuel combustion device Expired - Lifetime JP3388951B2 (en)

Priority Applications (1)

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

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

Related Child Applications (1)

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

Publications (2)

Publication Number Publication Date
JPH0949613A JPH0949613A (en) 1997-02-18
JP3388951B2 true JP3388951B2 (en) 2003-03-24

Family

ID=16470905

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Link
JP (1) JP3388951B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004092644A1 (en) * 1998-02-16 2004-10-28 Tadashi Gengo Pulverized fuel combustion apparatus

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JPH0949613A (en) 1997-02-18

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