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JPS6011290B2 - combustion device - Google Patents
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JPS6011290B2 - combustion device - Google Patents

combustion device

Info

Publication number
JPS6011290B2
JPS6011290B2 JP52060505A JP6050577A JPS6011290B2 JP S6011290 B2 JPS6011290 B2 JP S6011290B2 JP 52060505 A JP52060505 A JP 52060505A JP 6050577 A JP6050577 A JP 6050577A JP S6011290 B2 JPS6011290 B2 JP S6011290B2
Authority
JP
Japan
Prior art keywords
diameter
heavy oil
small
flow
primary 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
JP52060505A
Other languages
Japanese (ja)
Other versions
JPS53146332A (en
Inventor
仁 永井
久司 宮嶋
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.)
NIPPON FUAANESU KOGYO KK
SEMENTO KYOKAI
Original Assignee
NIPPON FUAANESU KOGYO KK
SEMENTO KYOKAI
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 NIPPON FUAANESU KOGYO KK, SEMENTO KYOKAI filed Critical NIPPON FUAANESU KOGYO KK
Priority to JP52060505A priority Critical patent/JPS6011290B2/en
Publication of JPS53146332A publication Critical patent/JPS53146332A/en
Publication of JPS6011290B2 publication Critical patent/JPS6011290B2/en
Expired legal-status Critical Current

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  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Muffle Furnaces And Rotary Kilns (AREA)

Description

【発明の詳細な説明】 たとえば、セメント焼成用のロータリーキルンにおいて
は、長大なロータリーキルン内に供孫台される原料を1
550qoの高温に加熱して焼成するため、燃焼用空気
の大部分量である約90%の2次空気はあらかじめクリ
ンカーボツクス内を通して約800℃に予熱して談ロー
タリーキルンに製品の排出に逆流させて供給し、大量の
重油は多数束ねられた高圧噴霧型バ−ナから約10%量
の高圧1次空気と倶に該ロータリーキルン内に供給され
、高負荷燃焼が行なわれる。
DETAILED DESCRIPTION OF THE INVENTION For example, in a rotary kiln for firing cement, raw materials fed into a large rotary kiln are
In order to perform firing by heating to a high temperature of 550 qo, the majority of the combustion air, about 90% of the secondary air, is passed through a clinker box, preheated to about 800°C, and then flowed back into the rotary kiln to discharge the product. A large amount of heavy oil is supplied into the rotary kiln together with about 10% of the amount of high-pressure primary air from a large number of bundled high-pressure spray burners, and high-load combustion is performed.

かかる大規模な高温燃焼においては、当然N○×が大量
に発生し、その排煙中にN0×が40Q剛なし、し10
0の岬と極めて高濃度に含まれるから公害上の問題であ
り従来からN○×発生量の少ない燃焼装置の開発が要望
されていた。本発明者らは、低N0×燃焼装置の研究、
実験を重ねた結果、はじめに第3図、第4図に示す燃焼
装置を開発した。
In such large-scale high-temperature combustion, a large amount of N○× is naturally generated, and the exhaust gas contains NOx of 40Q and 10%.
Since it is contained in extremely high concentrations, it is a pollution problem, and there has been a demand for the development of combustion equipment that generates a small amount of N○x. The present inventors conducted research on low N0x combustion equipment,
As a result of repeated experiments, we first developed the combustion device shown in Figures 3 and 4.

これは中心に1基の大口径バーナ21を設け、該大口径
バーナはその先端に大口径の油噴出孔22を有し、それ
を囲んで1次空気中心流が高速で噴出する1次空気中心
流噴出孔23を有し、上記大口径バーナを囲んでその周
囲に4基ないし1を基の小口径バーナ24,24′…を
設けこれら小口径バーナはそれぞれその先端に小口径の
油噴出孔25,25′・・・を有し、これら4・口径油
噴出孔を囲んで1次空気周囲流が高速で噴出する環状の
1次空気周囲流噴出孔26,26′・・・を有し、大量
の高温の2次空気は該燃焼装置のこれらバーナ群の外周
部から供給されるようにした構造であった。このような
構造にすれば周囲部の小口径バーナ24,24′の各重
油噴出孔25,52′・・・からは比較的細かい粒子で
重油が噴出せられ従って高温の2次空気の供給によって
比較的短かし、炎を作って急速に燃焼されるが、中央の
大口径バーナ2iの重油噴出孔22からは比較的大粒の
粒子で重油が噴出せられ、かつ2次空気は周囲の短火炎
を通りぬけた後でなければこの大口蓬バーナの重油噴流
に至らず、その間に周囲の小口径バーナによって発生す
る燃焼ガスも、重油噴流に吸引せられ、従って全体とし
て比較的長い火炎で燃焼が行なわれる。
This is provided with one large-diameter burner 21 in the center, and the large-diameter burner has a large-diameter oil jet hole 22 at its tip, and surrounding it, a primary air central flow is spouted out at high speed. It has a central flow jet hole 23, and surrounding the large diameter burner are four or one small diameter burners 24, 24', etc., each of which has a small diameter oil jet at its tip. It has holes 25, 25'..., and has annular primary air ambient flow ejection holes 26, 26'... surrounding these 4 diameter oil ejection holes and from which the primary air ambient flow is ejected at high speed. However, the structure was such that a large amount of high-temperature secondary air was supplied from the outer periphery of these burner groups of the combustion apparatus. With this structure, heavy oil is ejected in relatively fine particles from the respective heavy oil injection holes 25, 52' of the small-diameter burners 24, 24' in the surrounding area, and therefore, by supplying high-temperature secondary air. Although it is relatively short, a flame is created and the fuel is rapidly combusted, relatively large particles of heavy oil are ejected from the heavy oil jet hole 22 of the central large-diameter burner 2i, and the secondary air is The heavy oil jet of the large-mouth burner does not reach the heavy oil jet until it passes through the flame, and during this time the combustion gas generated by the surrounding small-diameter burners is also sucked into the heavy oil jet, resulting in combustion as a whole with a relatively long flame. will be carried out.

このような燃焼によって従来より大中にNO戊発生量を
低減せしめることができた。しかしながら、従来の単に
重油バーナ多数を束ねた燃焼装置および上述の燃焼装置
において、各油圧噴霧型バーナから噴出される重油噴流
が隣同志お互に交叉し合った場合そこに重油の濃密な固
まりが生じやすく、この重油濃密部の燃焼は円滑に行な
われず、このことは高負荷燃焼において問題となるので
、この問題点を解決すべく、次に第5図、第6図に示す
燃焼装置を開発した。これは中心に1次空気中心流供給
路31を設け、従って該燃焼装置の先端中央部に1次空
気中心流噴出孔32を有し該1次空気中心流供給路を囲
んでその周囲に4基ないし12基の小口径バーナ33,
33′を設け、これら小口径バーナはそれぞれの先端に
小口径の油噴出孔34,34′・・・を有し、これら4
・口径油噴出孔を囲んで少量の1次空気周囲流が高速で
噴出する環状の1次空気周囲流噴出孔35,35′を有
し、大量の高温の2次空気は該燃焼装置のこれらバーナ
群の外周部から供給されるようにした構造であった。こ
のような構造にすれば、各小口蚤バーナ33,33′の
重油噴出孔34,34′から噴出される重油噴流は1次
空気中心流の作用によって中心藤から遠ざかる方向に、
すなわち放射状に拡げられて、各重油噴流はその隣同志
が交叉して重油の濃密部を作ることはなくなり、かつ高
温の2次空気により接しやすくなり、従って燃焼が良好
になると共に燃焼効率を高めることできる。
By such combustion, it was possible to reduce the amount of NO gas generated in the large medium compared to the conventional method. However, in the conventional combustion device that simply bundles a large number of heavy oil burners and the above-mentioned combustion device, when the heavy oil jets ejected from each hydraulic spray burner intersect with each other, dense lumps of heavy oil are formed there. This is a problem that occurs in high-load combustion.In order to solve this problem, we developed the combustion equipment shown in Figures 5 and 6. did. This has a primary air central flow supply path 31 in the center, and therefore has a primary air central flow jetting hole 32 in the center of the tip of the combustion device, and has four central air flow injection holes surrounding the primary air central flow supply path. one to twelve small diameter burners 33;
33', and these small-diameter burners have small-diameter oil spout holes 34, 34'... at their tips, and these four
- It has annular primary air ambient flow jetting holes 35, 35' surrounding the diameter oil jetting hole and from which a small amount of primary air peripheral flow is jetted out at high speed, and a large amount of high temperature secondary air flows through these of the combustion device. The structure was such that the fuel was supplied from the outer periphery of the burner group. With this structure, the heavy oil jets ejected from the heavy oil jet holes 34, 34' of the respective small-mouth flea burners 33, 33' are directed away from the central pipe by the action of the primary air central flow.
That is, by being spread out radially, each heavy oil jet no longer intersects with its neighbors to create a dense area of heavy oil, and is more likely to come into contact with the high-temperature secondary air, thus improving combustion and increasing combustion efficiency. I can do that.

本発明者らが今回開発した燃焼装置はN○×発生量を低
減せしめ、かつ重油の濃密部を作ることはなく燃焼が円
滑に効率よく行なわれる燃焼装置である。
The combustion device that the present inventors have developed this time is a combustion device that reduces the amount of N○× generated and that burns smoothly and efficiently without creating heavy oil-dense areas.

本発明の燃焼装置をその実施例を示す第1図、第2図に
よって説明する。
The combustion apparatus of the present invention will be explained with reference to FIGS. 1 and 2 showing embodiments thereof.

吹込管1の中心に1次空気中央流供給路2を設けその周
囲にそれぞれ1次空気周囲流供給路で囲まれた大口軽重
油バーナ5,5′・・・と小口径重油バーナ6,6′・
・・とを、お互に隣同志に配設し従って該吹込管先端部
7においては中央に1次空気中央流の噴出口8を有し、
その周囲にそれぞれ1次空気周囲流の環状噴出孔9,9
′・・・に囲まれた大口径バーナの重油噴出孔11,1
1′・・・と、1次空気周囲流の環状噴出孔10,10
′・・・に囲まれた小口径のバーナの重油噴出孔12,
12′・・・を有する構造のものである。
A primary air central flow supply passage 2 is provided at the center of the blowing pipe 1, and is surrounded by a primary air peripheral flow supply passage, respectively. ′・
... are arranged next to each other, so that the blowing pipe tip 7 has a primary air central flow outlet 8 in the center,
At its periphery are annular orifices 9, 9 for primary air ambient flow, respectively.
Heavy oil spout holes 11, 1 of the large-diameter burner surrounded by '...
1'... and the annular ejection holes 10, 10 for the primary air ambient flow.
' The heavy oil outlet hole 12 of the small-diameter burner surrounded by...
12'...

なお13は1次空気中央流のダンパ−付取入口14は1
次空気周囲流のダンパー付取入口である。15は吹込管
の外殻である。
Note that 13 is the primary air central flow intake port 14 with a damper.
Next is the intake with a damper for the ambient air flow. 15 is the outer shell of the blowing pipe.

本発明の燃焼装置においては、重油供給量に対する理論
空気量の約10%量が1次空気として該燃焼装置内に供
給せられるが、1次空気は中央流と周囲流とに分けて供
給せられ、中央流の方が周囲流に比し多量でその比は8
:2ないし6:4であり、それぞれの取入口からいずれ
も水柱1000肋及至250仇吻の高圧で供給せられ、
周囲流は各バーナの重油噴出量にほぼ比例するように各
バーナに配分されて各重油噴出孔の周囲から噴出される
In the combustion apparatus of the present invention, approximately 10% of the theoretical air amount relative to the amount of heavy oil supplied is supplied as primary air into the combustion apparatus, but the primary air is supplied separately into a central flow and a peripheral flow. The central flow is larger than the surrounding flow, and the ratio is 8.
:2 to 6:4, and is supplied from each intake at a high pressure of 1000 m2 to 250 m2 water column.
The ambient flow is distributed to each burner so as to be approximately proportional to the amount of heavy oil ejected from each burner, and is ejected from around each heavy oil ejection hole.

重油は40k9/従ないし70k9/鮒の高圧でこれら
各油圧燈霧式バーナに供給されるが、大口径バーナの重
油噴出量と小口蓬バーナとの重油噴出量の比は9:1な
いし7:3である。燃焼用空気の約90%大量の2次空
気はクリンカーボックスを通り製品の搬出に逆流して該
ロータリーキルン内に入り、約800℃の高温に子熱さ
れて各バーナの外周部から供給される。
Heavy oil is supplied to each of these hydraulic light mist burners at a high pressure of 40k9/min to 70k9/carp, and the ratio of the amount of heavy oil ejected from the large diameter burner to the amount of heavy oil ejected from the small diameter burner is 9:1 to 7: It is 3. The secondary air, which is about 90% of the combustion air, passes through the clinker box, flows back to the product discharge, enters the rotary kiln, is heated to a high temperature of about 800° C., and is supplied from the outer periphery of each burner.

この2次空気の供給によって、周囲に交互に配議された
大口径バーナと小口径バーナのうち小口径のバーナから
噴出された重油はその油滴が微細であるから容易に比較
的短い火炎で燃焼され、大口径のバーナから噴出される
重油噴流は運動量大なる1次空気周囲流に包まれており
、該大口径バーナの1次空気周囲流は小口蓬バーナの燃
焼によって生じる高温燃焼ガスを吸引して大口蓬バーナ
の重油噴流中に巻き込むから大口径バーナによる噴出重
油は先づ高温燃焼ガスによって吸熱ガス化反応をし、該
反応によって生じる還元舷や還元COを主成分とした噴
流が2次空気によって燃焼せられる。
By supplying this secondary air, the heavy oil ejected from the small-diameter burner among the large-diameter burners and small-diameter burners arranged alternately around it can be easily created into a relatively short flame because the oil droplets are fine. The jet of heavy oil that is combusted and ejected from the large-diameter burner is surrounded by a primary air surrounding flow with a large momentum, and the primary air surrounding flow of the large-diameter burner absorbs the high-temperature combustion gas generated by the combustion of the small-mouth burner. Since it is sucked into the heavy oil jet of the large-mouth burner, the heavy oil jetted out by the large-diameter burner first undergoes an endothermic gasification reaction with the high-temperature combustion gas. It is then combusted by air.

かように大部分の重油は大口径バーナから噴出されて部
分燃焼された後高温2次空気の供給による完全燃焼が行
なわれ、それによって生ずる火炎は極端な高温部を作る
ことがなく円滑に燃焼が行なわれ、従ってNO広発生量
は大中に低減する。
In this way, most of the heavy oil is ejected from a large-diameter burner, partially combusted, and then completely combusted by supplying high-temperature secondary air, and the resulting flame burns smoothly without creating an extremely high-temperature area. Therefore, the amount of NO produced is greatly reduced.

また1次空気中央流によって各バーナの重油噴流は中心
軸から遠ざかる方向に噴射されるが特に小口径バーナの
重油噴流が先づ中心軸から遠ざかる方向に放射状に拡げ
られて2次空気との接触が容易となり短炎で早急な燃焼
が助成される。次に大口径バーナの噴流も若干放射状に
中心軸から、ご・かる方向に拡げられて、隣同志の重油
噴流の叉による重油の濃密部の生成は全くなくなり、階
な燃焼が行なわれる。本発明の燃焼装置によるN○k発
生量の低減」果は第7図に示すごとくである。
In addition, the primary air central flow causes the heavy oil jets of each burner to be injected in a direction away from the central axis, and in particular, the heavy oil jets of small diameter burners are first spread radially in the direction away from the central axis and come into contact with the secondary air. This facilitates quick combustion with a short flame. Next, the jets of the large-diameter burner are also slightly radially expanded in the direction from the central axis, and the formation of dense areas of heavy oil due to the intersection of adjacent heavy oil jets is completely eliminated, resulting in efficient combustion. The reduction in the amount of N○k generated by the combustion apparatus of the present invention is as shown in FIG.

第7図は、横に空気比をとり、縦軸に燃焼排ガス中のN
○×字度(脚)をとり各空気比における本発明の燃焼装
置によるN0×発生量を実線で示し各空気比における従
来の単にバーナ多数基を束ねた構造の燃焼装置によるN
○k発生量を点線で示している。実験の結果本発明の燃
焼装置は従来構造の燃焼装置に比し半量以下のNOk側
となっていることが確認され、また、重油の濃密部を作
らないから円滑な燃焼が行なわれ良好な形状の火炎が得
られ熱効率を向上せしめることができる。本発明の燃焼
装置はセメント燃焼用のロータリーキルンに好適なもの
であるが、一般のロータリーキルンに対しても適用する
ことができ、そのN0k発生量を低減せしめ、かつ良好
な形状の火炎を作って円滑に燃焼するから燃料の効率を
高めることができる。
Figure 7 shows the air ratio on the horizontal axis and the N in the combustion exhaust gas on the vertical axis.
The solid line indicates the amount of NOx generated by the combustion device of the present invention at each air ratio, and the N0x amount generated by the conventional combustion device with a structure of simply bundling a large number of burners at each air ratio.
The dotted line indicates the amount of ○k generated. As a result of experiments, it was confirmed that the combustion device of the present invention has less than half the amount of NOk compared to a combustion device with a conventional structure, and since it does not create a dense area of heavy oil, smooth combustion occurs and the combustion device has a good shape. flame can be obtained and thermal efficiency can be improved. Although the combustion device of the present invention is suitable for rotary kilns for burning cement, it can also be applied to general rotary kilns, reducing the amount of N0k generated, and creating a flame with a good shape for smooth combustion. The efficiency of the fuel can be increased because it is combusted.

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

第1図、第2図は本発明に係る燃焼装置のそれぞれ第2
図における1‐1断面側断面図と燃焼室側から見た正面
図である。 第3図、第4図は本発明者らが最初に開発した低N0k
燃焼装置のそれぞれ側断面図と燃焼室側から見た正面図
である。第5,第6図は本発明者らが燃焼の円滑化のた
め次に開発した燃焼装置のそれぞれ側断面図と燃焼室側
から見た正面図である。第7図は本発明の燃焼装置と従
来の燃焼装置との各空気比におけるN0k発生量を比較
して示したグラフである。1は吹込管2は1次空気中央
流供給路3は大口径バーナの1次空気周囲流供給路4は
小口蓬バーナの1次空気周囲流供給路5は大口径重油バ
ーナ6は小口径重油バーナ7は吹込管先端面8は1次空
気中央流の噴出孔9は大口径バーナの1次空気周囲流の
噴出孔10は4・口径バーナの1次空気周囲流の噴出孔
11は大口径バーナの重油噴出孔12は小口径バーナの
重油噴出孔。 第7図 第2図 弊3図 界4図 第5図 兼6図 粥7図
FIG. 1 and FIG. 2 show the second part of the combustion apparatus according to the present invention, respectively.
They are a 1-1 section side sectional view and a front view seen from the combustion chamber side in the figure. Figures 3 and 4 show the low N0k first developed by the inventors.
They are a side sectional view and a front view of the combustion device as seen from the combustion chamber side, respectively. 5 and 6 are a side sectional view and a front view, respectively, of a combustion device developed by the present inventors for smooth combustion, as seen from the combustion chamber side. FIG. 7 is a graph showing a comparison of the amount of NOk generated at various air ratios between the combustion apparatus of the present invention and the conventional combustion apparatus. 1 is a blow pipe 2 is a primary air central flow supply passage 3 is a primary air ambient flow supply passage for a large-diameter burner 4 is a primary air ambient flow supply passage for a small-mouth burner 5 is a large-diameter heavy oil burner 6 is a small-diameter heavy oil In the burner 7, the blowing pipe tip face 8 has a primary air central flow jet hole 9. The primary air peripheral flow jet hole 10 of the large diameter burner has a large diameter.The primary air peripheral flow jet hole 11 of the diameter burner has a large diameter. The heavy oil spout hole 12 of the burner is a heavy oil spout hole of a small diameter burner. Figure 7 Figure 2 Figure 3 Figure 4 Figure 5 and 6 Figure 7 Figure 7

Claims (1)

【特許請求の範囲】[Claims] 1 本燃焼装置に供給される重油量に対する理論空気量
の約10%量である高圧にした1次空気を中央流と周囲
流とに分け、その過半量である中央流を1次空気中央流
供給路2に他の半量に満たない量である周囲流を数個の
大口径周囲流供給路3,3′…と数個の小口径周囲流供
給路4,4′…とに分けて供給し、本燃焼装置吹込管1
の中軸部に1次空気中央流供給路2を設け、該1次空気
中央流供給路2の先端に1次空気中央流噴出孔8を設け
、該1次空気中央流供給路2の周囲に数基の大口径重油
バーナ5,5′…と数基の小口径重油バーナ6,6′と
を交互にして配設し、これら大口径重油バーナ5,5′
…はいづれもその中心に大口径重油供給路を設け、該大
口径重油供給路の先端にそれぞれ大口径重油噴出用チツ
プ11を設け、該大口径重油供給路の周囲にそれぞれ大
口径周囲流供給路3を設け、該大口径周囲流供給路3の
先端にそれぞれ大口径周囲流噴出孔9を設け、これら小
口径重油バーナ6はいづれもその中心に小口径重油供給
路を設け、該小口径重油供給路の先端にそれぞれ小口径
重油噴出用チツプ12を設け、該小口径重油供給路の周
囲にそれぞれ小口径周囲流供給路4を設け、該小口径周
囲流供給路4先端にそれぞれ小口径周囲流噴出孔10を
設けた構造となし、これら大口径バーナ5,5′…と小
口径バーナ6,6′…の外周部から大量の2次空気をク
リンカーボツクスを通した後供給する構造のロータリー
キルン用燃焼装置。
1 The high-pressure primary air, which is about 10% of the theoretical air amount for the amount of heavy oil supplied to this combustion device, is divided into a central flow and a peripheral flow, and the central flow, which is the majority of the amount, is divided into the primary air central flow. The ambient flow, which is less than half of the other amount, is supplied to the supply channel 2 by dividing it into several large-diameter ambient flow supply channels 3, 3'... and several small-diameter ambient flow supply channels 4, 4'... This combustion device blow pipe 1
A primary air central flow supply passage 2 is provided in the central shaft portion, a primary air central flow jetting hole 8 is provided at the tip of the primary air central flow supply passage 2, and a primary air central flow jetting hole 8 is provided around the primary air central flow supply passage 2. Several large-diameter heavy oil burners 5, 5'... and several small-diameter heavy oil burners 6, 6' are arranged alternately, and these large-diameter heavy oil burners 5, 5'...
...A large-diameter heavy oil supply path is provided in the center of each of them, a large-diameter heavy oil jetting chip 11 is provided at the tip of each of the large-diameter heavy oil supply paths, and a large-diameter ambient flow is supplied around each of the large-diameter heavy oil supply paths. A passage 3 is provided, and a large diameter ambient flow jetting hole 9 is provided at the tip of each of the large diameter ambient flow supply passages 3, and each of these small diameter heavy oil burners 6 is provided with a small diameter heavy oil supply passage at the center thereof, and a small diameter heavy oil supply passage is provided at the center thereof. A small-diameter heavy oil jetting tip 12 is provided at each tip of the heavy oil supply path, a small-diameter ambient flow supply path 4 is provided around each of the small-diameter heavy oil supply paths, and a small-diameter fuel oil jetting tip 12 is provided at each tip of the small-diameter ambient flow supply path 4. It has a structure in which a peripheral flow jetting hole 10 is provided, and a large amount of secondary air is supplied from the outer periphery of these large diameter burners 5, 5'... and small diameter burners 6, 6'... after passing through a clinker box. Combustion device for rotary kiln.
JP52060505A 1977-05-26 1977-05-26 combustion device Expired JPS6011290B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP52060505A JPS6011290B2 (en) 1977-05-26 1977-05-26 combustion device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP52060505A JPS6011290B2 (en) 1977-05-26 1977-05-26 combustion device

Publications (2)

Publication Number Publication Date
JPS53146332A JPS53146332A (en) 1978-12-20
JPS6011290B2 true JPS6011290B2 (en) 1985-03-25

Family

ID=13144227

Family Applications (1)

Application Number Title Priority Date Filing Date
JP52060505A Expired JPS6011290B2 (en) 1977-05-26 1977-05-26 combustion device

Country Status (1)

Country Link
JP (1) JPS6011290B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6123720B2 (en) * 2014-03-26 2017-05-10 Jfeスチール株式会社 Multi-tube tubular flame burner

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4988320U (en) * 1972-11-14 1974-07-31
JPS5413610B2 (en) * 1973-12-05 1979-06-01
JPS5228248B2 (en) * 1973-12-27 1977-07-26
JPS5124936A (en) * 1974-08-27 1976-02-28 Mitsubishi Heavy Ind Ltd NENRYONEN SHOSOCHI
JPS5250032Y2 (en) * 1974-10-23 1977-11-14
JPS5320745Y2 (en) * 1974-11-06 1978-05-31

Also Published As

Publication number Publication date
JPS53146332A (en) 1978-12-20

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