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JPS6257685B2 - - Google Patents
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JPS6257685B2 - - Google Patents

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Publication number
JPS6257685B2
JPS6257685B2 JP9822785A JP9822785A JPS6257685B2 JP S6257685 B2 JPS6257685 B2 JP S6257685B2 JP 9822785 A JP9822785 A JP 9822785A JP 9822785 A JP9822785 A JP 9822785A JP S6257685 B2 JPS6257685 B2 JP S6257685B2
Authority
JP
Japan
Prior art keywords
combustion
axis
fuel
radiant tube
air
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
Application number
JP9822785A
Other languages
Japanese (ja)
Other versions
JPS61264126A (en
Inventor
Ryuichi Odawara
Isamu Hirose
Fumio Tomimatsu
Hideo Tatemichi
Akira Yamamoto
Hiroshi Wakushima
Toshihiro Nagamachi
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.)
Kobe Steel Ltd
Original Assignee
Kobe Steel 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 Kobe Steel Ltd filed Critical Kobe Steel Ltd
Priority to JP9822785A priority Critical patent/JPS61264126A/en
Publication of JPS61264126A publication Critical patent/JPS61264126A/en
Publication of JPS6257685B2 publication Critical patent/JPS6257685B2/ja
Granted legal-status Critical Current

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Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、特にNOxと黒煙(スモーク)の排
出量(濃度)の少ないラジアントチユーブの燃焼
方法および装置に関する。
DETAILED DESCRIPTION OF THE INVENTION (Industrial Application Field) The present invention particularly relates to a radiant tube combustion method and apparatus with low emissions (concentrations) of NOx and black smoke.

(従来技術) 従来、第5図a及び第5図bに示すように、熱
処理炉の炉壁1を挿通するラジアントチユーブ2
の端部にバーナ本体3が連絡され、先端に保炎板
4を有する燃料噴出管5をラジアントチユーブ2
のチユーブ軸心Tに一致(同軸心)させて設け、
燃料Gを燃料噴出管5から噴出すると同時に、該
燃料噴出管5の外周に形成された燃焼空気噴出通
路6から燃焼空気Aを噴出するようにした燃焼装
置が提案されている。
(Prior Art) Conventionally, as shown in FIGS. 5a and 5b, a radiant tube 2 inserted through a furnace wall 1 of a heat treatment furnace has been used.
A burner main body 3 is connected to the end of the radiant tube 2, and a fuel injection pipe 5 having a flame stabilizing plate 4 at the tip
Provided so as to coincide with (coaxial center) the tube axis T of
A combustion device has been proposed in which fuel G is ejected from a fuel ejection pipe 5 and, at the same time, combustion air A is ejected from a combustion air ejection passage 6 formed on the outer periphery of the fuel ejection pipe 5.

しかしながら、該燃焼装置では、低負荷燃焼率
時は未燃分、特に黒煙(スモーク)が発生しやす
くなる。
However, in this combustion device, unburned matter, especially black smoke, is likely to be generated when the combustion rate is low.

即ち、高温の燃焼空気A(500℃以上)といえ
ども、火炎(900〜1200℃)よりも温度が低いの
で、密度の小さい火炎は浮力でラジアントチユー
ブ2の上層流へ、密度の大きい燃焼空気Aは下層
流へと流れる力が働く。特に低負荷燃焼率時は、
燃料Gや燃焼空気Aの噴出流速及びラジアントチ
ユーブ2内のガス流速が遅くなるので、火炎の浮
力が支配的となる。したがつて、燃料Gは燃焼が
始まると、燃焼空気Aと交差混合し、空気不足の
燃焼状態で上層流へ移り、また、燃料流より真下
の燃焼空気Aはもとより、燃料流の横の燃焼空気
流も下層流へと流れが移る。そして、ラジアント
チユーブ2内の流れは、マクロ的に未燃分を多く
含んだ上層流の火炎と下層流の燃焼空気流の二相
流になり、層流混合しながら下流へと流れて行
く。しかし、下流へ行くと燃焼熱よりもチユーブ
2の抜熱量が大きくなるので、ガス温度が下が
り、未燃分は燃焼しにくくなり、黒煙(スモー
ク)が発生しやすくなるのである。
In other words, even though the combustion air A is at a high temperature (500°C or higher), its temperature is lower than that of the flame (900-1200°C), so the low-density flame flows into the upper flow of the radiant tube 2 due to buoyancy, and the high-density combustion air The force that flows to the lower flow acts on A. Especially at low load combustion rates,
Since the ejection flow velocity of the fuel G and combustion air A and the gas flow velocity within the radiant tube 2 are reduced, the buoyancy of the flame becomes dominant. Therefore, when combustion begins, fuel G cross-mixes with combustion air A and moves to the upper flow in an air-starved combustion state. The airflow also shifts to the lower flow. Then, the flow inside the radiant tube 2 becomes a two-phase flow consisting of an upper flow of flame containing a large amount of unburned matter macroscopically and a lower flow of combustion air, and flows downstream while being laminarly mixed. However, when going downstream, the amount of heat removed from the tube 2 becomes larger than the combustion heat, so the gas temperature decreases, making it difficult to burn unburned components, and making it easier to generate black smoke.

また、高温燃焼空気(500℃以上)の高負荷燃
焼率時はNOxが多量に発生しやすくなる。
Additionally, large amounts of NOx are likely to be generated during high-load combustion rates of high-temperature combustion air (500°C or higher).

即ち、ラジアントチユーブ2の燃焼は、燃料G
の燃料量に対して燃焼室が狭いため、燃焼室負荷
率が大きくて、10×106kcal/m3h以上である。
したがつて、従来では燃焼効率を良くするため
に、燃料Gと燃焼空気Aとを早期に均一混合さ
せ、急速な燃焼に主眼がおかれていたため、燃焼
初期の酸素分圧の高い所で火炎温度が高くなり、
NOxが発生しやすくなるのである。
That is, the combustion of the radiant tube 2 causes the fuel G
Since the combustion chamber is narrow for the amount of fuel, the combustion chamber load factor is large, exceeding 10×10 6 kcal/m 3 h.
Therefore, in the past, in order to improve combustion efficiency, the main focus was on uniformly mixing fuel G and combustion air A at an early stage to achieve rapid combustion. The temperature increases,
This makes it easier for NOx to be generated.

このため、燃焼設備のNOx,黒煙(スモー
ク)等の環境が悪くなるばかりでなく、黒煙が
レキユペレータの伝熱管に付着し、熱交換能力を
低下させると共に圧損の増大をきたす。ま
た、ラジアントチユーブ2の下層に未燃炭素が堆
積し、ラジアントチユーブ2の炉内での伝熱能力
が低下する。そして、排ガス温度が高くなりレ
キユペレータの耐久性が悪くなる等の問題があ
る。
For this reason, not only does the environment of the combustion equipment deteriorate with NOx, black smoke, etc., but the black smoke also adheres to the heat exchanger tubes of the recuperator, reducing heat exchange ability and increasing pressure loss. Further, unburned carbon is deposited in the lower layer of the radiant tube 2, and the heat transfer ability of the radiant tube 2 in the furnace is reduced. Further, there are problems such as the exhaust gas temperature becoming high and the durability of the recuperator becoming poor.

また、第6図a及び第6図bに示すように燃料
噴出管5をラジアントチユーブ2のチユーブ軸心
Tの上側に偏位された燃料軸心に沿つて設けられ
た燃料噴出管5′から燃料Gを噴出すると同時
に、該チユーブ軸心Tの下側に偏位された空気軸
心に沿つて形成された燃焼空気噴出通路6′から
燃焼空気Aを噴出するようにした燃焼装置が提案
されている。
Further, as shown in FIGS. 6a and 6b, the fuel injection pipe 5 is connected to the fuel injection pipe 5' provided along the fuel axis which is offset above the tube axis T of the radiant tube 2. A combustion device has been proposed in which, at the same time as fuel G is injected, combustion air A is ejected from a combustion air ejection passage 6' formed along an air axis offset below the tube axis T. ing.

しかしながら、該燃焼装置では、高負荷燃焼率
時のNOxは少量になるが、低負荷燃焼率時にな
ると火炎の浮力が支配的となり、黒煙(スモー
ク)の発生量が非常に多くなるという問題があ
る。
However, with this combustion device, the amount of NOx is small at high load combustion rates, but at low load combustion rates, the buoyancy of the flame becomes dominant, resulting in an extremely large amount of black smoke. be.

このため、排熱回収率を向上させた高温レキユ
ペレータを採用する場合、その燃焼空気温度の上
限が、NOxの規制濃度や、黒煙(スモーク)濃
度で制約されるため、排熱回収率の高いレキユ
ペレータの採用が困難である。高温燃焼空気用
の蒸発添加等による低NOx対策はランニングコ
ストが高くなるため、高効率排熱回収の投資メリ
ツトが少なくなる等の問題がある。
Therefore, when adopting a high-temperature recuperator with improved exhaust heat recovery rate, the upper limit of the combustion air temperature is restricted by the NOx regulatory concentration and black smoke concentration. It is difficult to employ a requioperator. Measures to reduce NOx by adding evaporation to high-temperature combustion air increase running costs, which reduces the investment benefits of high-efficiency waste heat recovery.

(発明の目的) 本発明は上記従来の諸問題に鑑みてなされたも
ので、低NOxと低黒煙のターンダウン特性の良
いラジアントチユーブの燃焼方法および装置を提
供することを目的とするものである。
(Object of the Invention) The present invention has been made in view of the above-mentioned conventional problems, and an object of the present invention is to provide a radiant tube combustion method and apparatus with good turndown characteristics of low NOx and black smoke. be.

(発明の構成) このため本発明に係る燃焼方法は、ラジアント
チユーブのチユーブ軸心の上側に偏位された空気
軸心に沿つて燃焼空気が噴出されると同時に、該
チユーブ軸心の下側に偏位された燃料軸心に沿つ
て燃料が噴出されるように構成したものである。
(Structure of the Invention) Therefore, in the combustion method according to the present invention, combustion air is ejected along the air axis of the radiant tube, which is offset above the tube axis, and at the same time The structure is such that the fuel is injected along the fuel axis which is deviated from the center.

また、本発明に係る燃焼装置は、ラジアントチ
ユーブのチユーブ軸心の上側に偏位された空気軸
心に沿つて燃焼空気噴出通路が形成され、該チユ
ーブ軸心の下側に偏位された燃料軸心に沿つて燃
料噴出管が設けられて構成されたものである。
Further, in the combustion device according to the present invention, the combustion air jet passage is formed along the air axis of the radiant tube, which is offset to the upper side of the tube axis, and the combustion air jet passage is formed along the air axis of the radiant tube, which is displaced to the lower side of the tube axis. A fuel injection pipe is provided along the axis.

(発明の効果) 本発明によれば、ラジアントチユーブのチユー
ブ軸心に対して、上部側に燃焼空気の噴出軸心を
偏位させ、下部側に燃料の噴出軸心を偏位させる
ようにしたものであるから、高負荷燃焼率時の急
速な燃料と燃焼空気の混合がさけられ、緩慢な燃
焼になるためにNOxが抑制されるようになる。
(Effects of the Invention) According to the present invention, the combustion air ejection axis is offset toward the upper side and the fuel ejection axis is offset toward the lower side with respect to the tube axis of the radiant tube. As a result, rapid mixing of fuel and combustion air at high load combustion rates is avoided, resulting in slow combustion, which suppresses NOx.

また、低負荷燃焼率時は、下部側火炎が浮力に
より上部側へ浮き上がる過程で上部側から吹き込
まれた燃焼空気と混合燃焼するために、未燃黒煙
(スモーク)の排出が抑制されるようになる。
In addition, at low load combustion rates, the flame on the lower side rises to the upper side due to buoyancy and mixes with the combustion air blown from the upper side, which suppresses the emission of unburned black smoke. become.

したがつて、排熱回収率の高い高温用レキユ
ペレータが採用でき、蒸気添加による低NOx
ランニングコストが不要となり、燃焼設備の環
境が良くなり、レキユペレータの熱交能力の低
下がなくなり、レキユペレータの圧損増加がな
くなり、ラジアントチユーブ内のカーボン堆積
による炉内伝熱能力低下がなくなり、レキユペ
レータの耐久性が向上するようになる。
Therefore, a high-temperature recuperator with a high waste heat recovery rate can be used, and low NOx can be achieved by adding steam.
Running costs are no longer required, the environment of the combustion equipment is improved, there is no reduction in the heat exchange capacity of the recuperator, there is no increase in pressure drop in the recuperator, there is no decrease in the heat transfer capacity in the furnace due to carbon accumulation in the radiant tube, and the durability of the recuperator is improved. Sexuality will improve.

(実施例) 以下、本発明の実施例を添付図面について詳細
に説明する。
(Embodiments) Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings.

第1図aおよび第1図bに示すように、熱処理
炉の炉壁11を挿通するラジアントチユーブ12
の端部にバーナ本体13が連結され、先部に保炎
板14を有する燃料噴出管15を、ラジアントチ
ユーブ12のチユーブ軸心Tの下側に偏位された
燃料軸心に沿つて設けるとともに、チユーブ軸心
Tの上側に偏位された空気軸心に沿つて燃焼空気
噴出通路16を形成している。
As shown in FIGS. 1a and 1b, a radiant tube 12 inserted through the furnace wall 11 of the heat treatment furnace
The burner main body 13 is connected to the end of the radiant tube 12, and a fuel injection pipe 15 having a flame stabilizing plate 14 at the tip is provided along the fuel axis offset below the tube axis T of the radiant tube 12. , a combustion air jetting passage 16 is formed along the air axis shifted upward from the tube axis T.

したがつて、燃焼空気噴出通路16から噴出さ
れた燃焼空気Aは、燃料空気噴出管15から噴出
された燃料Gと混合燃焼するが、燃焼初期は燃料
Gに近い空気A1,A2と空気不足の状態(保炎板
14とラジアントチユーブ12の接点17から空
気が供給されない)で燃焼するので、高負荷燃焼
率時はNOxが低くなる。
Therefore, the combustion air A jetted out from the combustion air jetting passage 16 is mixed and combusted with the fuel G jetted out from the fuel air jetting pipe 15, but in the early stage of combustion, the air A 1 , A 2 close to the fuel G and the air are mixed. Since combustion occurs in a insufficient state (air is not supplied from the contact point 17 between the flame holding plate 14 and the radiant tube 12), NOx becomes low at high load combustion rates.

そして、燃料流は火炎の浮力で上層流へ、残り
の燃焼空気流A3,A4,A5は下層流へと移行して
ゆき、この過程で燃料Gや未燃分は完全燃焼する
ので、低負荷燃焼率時は黒煙(スモーク)の排出
が少なくなる。
Then, the fuel flow moves to the upper flow due to the buoyancy of the flame, and the remaining combustion air flows A 3 , A 4 , A 5 shift to the lower flow, and in this process, the fuel G and unburned components are completely combusted. , less black smoke is emitted at low load combustion rates.

なお、燃焼空気流の下部域から出る燃焼空気流
A1は、温度の高い排ガス循環流G1と共に保炎板
14とラジアントチユーブ12の接点17近辺に
生成するカーボンを燃焼し、カーボンの堆積防止
の機能をもつている。
In addition, the combustion air flow exiting from the lower region of the combustion air flow
A 1 has the function of burning carbon generated in the vicinity of the contact point 17 between the flame stabilizing plate 14 and the radiant tube 12 together with the high temperature exhaust gas circulation flow G 1 and preventing carbon accumulation.

第2図aおよび第2図bは、他の実施例で、燃
料噴出管15の基部をチユーブ軸心Tと一致さ
せ、保炎板14を有する先部を、ラジアントチユ
ーブ12のチユーブ軸心Tの下側に偏位させて斜
めに設けたものである。
2a and 2b show another embodiment in which the base of the fuel injection pipe 15 is aligned with the tube axis T, and the tip portion having the flame stabilizing plate 14 is aligned with the tube axis T of the radiant tube 12. It is installed diagonally and offset to the lower side.

この装置でも、第1図aおよび第1図bの装置
と同様の作用・効果を奏することができる。
This device can also provide the same functions and effects as the devices shown in FIGS. 1a and 1b.

第3図及び第4図は、本発明に係る燃焼装置
(□は第2図aの装置を示す)と従来の燃焼装置
(〇は第5図aの装置、△は第6図aの装置をそ
れぞれ示す)の燃焼負荷率とNOx、黒煙(スモ
ーク)との関係を測定したデータである。
FIGS. 3 and 4 show a combustion device according to the present invention (□ indicates the device in FIG. 2 a) and a conventional combustion device (○ indicates the device in FIG. 5 a, and △ indicates the device in FIG. 6 a). This is data measuring the relationship between the combustion load factor, NOx, and black smoke (respectively).

1 燃焼条件 (1) 空気温度:550℃(バーナ本体内) (2) ラジアントチユーブ温度:850℃ (3) 排ガス酸素濃度:2.0% (4) 100%燃焼:120×103kcal/H (5) 燃料:コークス炉ガス 2 燃焼装置 (1) ラジアントチユーブ 内径:145mm 長さ:6000mm 形状:U字形 3 実験炉 幅:760cm 高さ:950cm 長さ:3120cm 同図からも明らかなように、本燃焼装置によれ
ば、高負荷燃焼率時には低NOxで黒煙(スモー
ク)も低く、低負荷燃焼率時には黒煙(スモー
ク)が低いことがわかる。
1 Combustion conditions (1) Air temperature: 550℃ (inside the burner body) (2) Radiant tube temperature: 850℃ (3) Exhaust gas oxygen concentration: 2.0% (4) 100% combustion: 120×10 3 kcal/H (5 ) Fuel: Coke oven gas 2 Combustion device (1) Radiant tube inner diameter: 145 mm Length: 6000 mm Shape: U-shaped 3 Experimental furnace width: 760 cm Height: 950 cm Length: 3120 cm As is clear from the figure, main combustion According to the device, it can be seen that when the combustion rate is high, NOx is low and the amount of black smoke is low, and when the combustion rate is low, the amount of black smoke is low.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図aは本発明に係る第1実施例の燃焼装置
の側面断面図、第1図bは第1図aの―断面
図、第2図aは第2実施例の燃焼装置の側面断面
図、第2図bは第2図aの―断面図、第3図
は燃焼負荷率とNOxとの関係を示すグラフ、第
4図は燃焼負荷率と黒煙(スモーク)との関係を
示すグラフ、第5図aは従来の燃焼装置の側面断
面図、第5図bは第5図aの―断面図、第6
図aは従来の燃焼装置の側面断面図、第6図bは
第6図aの―断面図である。 12……ラジアントチユーブ、13……バーナ
本体、15……燃料噴出管、16……燃焼空気噴
出通路、T……チユーブ軸心。
FIG. 1a is a side sectional view of a combustion device according to a first embodiment of the present invention, FIG. 1b is a cross-sectional view taken from FIG. 1a, and FIG. Figure 2b is a cross-sectional view of Figure 2a, Figure 3 is a graph showing the relationship between combustion load factor and NOx, and Figure 4 is a graph showing the relationship between combustion load rate and black smoke. Graph, FIG. 5a is a side cross-sectional view of a conventional combustion device, FIG. 5b is a cross-sectional view of FIG. 5a, and FIG.
FIG. 6a is a side sectional view of a conventional combustion device, and FIG. 6b is a cross-sectional view taken from FIG. 6a. 12...Radiant tube, 13...Burner body, 15...Fuel injection pipe, 16...Combustion air injection passage, T...Tube axis center.

Claims (1)

【特許請求の範囲】 1 ラジアントチユーブのチユーブ軸心の上側に
偏位された空気軸心に沿つて燃焼空気が噴出され
ると同時に、該チユーブ軸心の下側に偏位された
燃料軸心に沿つて燃料が噴出されるようにしたこ
とを特徴とするラジアントチユーブの燃焼方法。 2 ラジアントチユーブのチユーブ軸心の上側に
偏位された空気軸心に沿つて燃焼空気噴出通路が
形成され、該チユーブ軸心の下側に偏位された燃
料軸心に沿つて燃料噴出管が設けられていること
を特徴とするラジアントチユーブの燃焼装置。
[Claims] 1. Combustion air is ejected along the air axis of the radiant tube, which is offset above the tube axis, and at the same time, the fuel axis is offset below the tube axis. A radiant tube combustion method characterized in that fuel is ejected along the radiant tube. 2. A combustion air injection passage is formed along the air axis of the radiant tube that is offset above the tube axis, and a fuel injection pipe is formed along the fuel axis that is offset below the tube axis. A radiant tube combustion device characterized in that:
JP9822785A 1985-05-08 1985-05-08 Method and apparatus for combustion of radiant tube Granted JPS61264126A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9822785A JPS61264126A (en) 1985-05-08 1985-05-08 Method and apparatus for combustion of radiant tube

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9822785A JPS61264126A (en) 1985-05-08 1985-05-08 Method and apparatus for combustion of radiant tube

Publications (2)

Publication Number Publication Date
JPS61264126A JPS61264126A (en) 1986-11-22
JPS6257685B2 true JPS6257685B2 (en) 1987-12-02

Family

ID=14214070

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9822785A Granted JPS61264126A (en) 1985-05-08 1985-05-08 Method and apparatus for combustion of radiant tube

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JPS61264126A (en) 1986-11-22

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