JPS5935707A - Combustion device - Google Patents

Combustion device

Info

Publication number
JPS5935707A
JPS5935707A JP57144769A JP14476982A JPS5935707A JP S5935707 A JPS5935707 A JP S5935707A JP 57144769 A JP57144769 A JP 57144769A JP 14476982 A JP14476982 A JP 14476982A JP S5935707 A JPS5935707 A JP S5935707A
Authority
JP
Japan
Prior art keywords
air
air passage
furnace
passage pipe
supply
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.)
Granted
Application number
JP57144769A
Other languages
Japanese (ja)
Other versions
JPH0262767B2 (en
Inventor
Tadahisa Masai
政井 忠久
Hitoshi Migaki
三垣 仁志
Toshio Uemura
俊雄 植村
Shigeki Morita
茂樹 森田
Kiichi Itagaki
喜一 板垣
Shoichi Masuko
益子 庄一
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 Power Ltd
Original Assignee
Babcock Hitachi KK
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 Babcock Hitachi KK filed Critical Babcock Hitachi KK
Priority to JP57144769A priority Critical patent/JPS5935707A/en
Publication of JPS5935707A publication Critical patent/JPS5935707A/en
Publication of JPH0262767B2 publication Critical patent/JPH0262767B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23LSUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L15/00Heating of air supplied for combustion
    • F23L15/02Arrangements of regenerators
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/34Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Abstract

PURPOSE:To reduce NOx without increasing the smoke dust contained in waste gas by dividing an after air port into a primary air passage pipe at the central part and air passages for secondary or more passages provided successively on the outer periphery of the primary air passage and providing a tapered throttle at the tip end on the furnace side of the primary air passage pipe. CONSTITUTION:Air taken from a blast box 18 into a primary air passage pipe 17 through a primary air take-in port 10, is shaped the flow by a distributing plate 11 and thereafter is accelerated by the tapered nozzle 13, thus the air being injected in a high-speed and high-density state from the primary air passage pipe 12 to the central part of a furnace. Accordingly, sufficient supply of air becomes possible with respect to the central part of the furnace to which supply of air has heretofore been difficult, and complete combustion is satisfactorily achieved. On the other hand, air sent from the blast box 18 to a secondary air passage 15 is given with appropriate swirl by a secondary air resister 14 and the injecting port of the secondary air passage 15 is enlarged in the tip. On the above described causes, supply of air to the furnace wall surface becomes satisfactory, whereby a complete combustion becomes possible even on the furnace wall surface to which supply of air has been heretofore difficult.

Description

【発明の詳細な説明】 本発明は燃焼装置に係り、特に排ガス中の窒素酸化物(
以下、NO,と称する)を低減するに好適なボイラ装置
に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a combustion device, and in particular to a combustion device that eliminates nitrogen oxides (
The present invention relates to a boiler device suitable for reducing NO (hereinafter referred to as NO).

NOアは光化学オキシダントの原因物質の1つとされて
いるだめ、近年、その発生を効果的に抑制する燃焼法の
開発が要望されている。このような目的に沿った燃焼法
として、(1)排ガス再循環法、(2)水噴射法、(3
)二段燃焼法および(4)脱硝燃焼法が知られているが
、この内、NO,低減効果および運転性等に優れた二段
燃焼法が特に注目されている。
NOA is considered to be one of the causative substances of photochemical oxidants, and in recent years, there has been a demand for the development of a combustion method that effectively suppresses its generation. Combustion methods that meet these objectives include (1) exhaust gas recirculation method, (2) water injection method, and (3)
) Two-stage combustion method and (4) Denitrification combustion method are known, and among these, the two-stage combustion method is attracting particular attention because of its excellent NO reduction effect and drivability.

従来の二段燃焼法に適用される装置は、第1図および第
2図に示す通り、火炉1の前側壁において下方から上方
へ向けて順次設けられた下段バーナ3、中段バーナ4お
よび上段バーナ5と、上段バーナ5の上方に設けられた
前側アフタエアポート6と、火炉1の後側壁に設けられ
た後側アフタエアポート7と、火炉1の下部に設けられ
た排ガス調整用のホッパ口2とから主として構成されて
いる。
As shown in FIGS. 1 and 2, the device applied to the conventional two-stage combustion method includes a lower burner 3, a middle burner 4, and an upper burner, which are sequentially provided from the bottom to the top on the front side wall of the furnace 1. 5, a front after-air port 6 provided above the upper burner 5, a rear after-air port 7 provided on the rear wall of the furnace 1, and a hopper port 2 for exhaust gas adjustment provided at the bottom of the furnace 1. It is mainly composed of.

上記構成において、バーナ部では空気比(実際に供給す
る空気酸/理論的に必要な空気喰)が通常、下段バー力
3では0.8〜1,0、中段バーナ4では0.6〜0.
8、上段バーナ5でハ0.4〜0.6に設定され、この
ような条件下で燃焼が行われる。
In the above configuration, the air ratio (actually supplied air acid/theoretically required air intake) in the burner section is usually 0.8 to 1.0 for the lower bar force 3 and 0.6 to 0 for the middle burner 4. ..
8. The upper stage burner 5 is set to 0.4 to 0.6, and combustion is performed under such conditions.

この場合、相対的に空気の多い下段バーナ3および中段
バーナ4の燃焼領域で発生したNO,は、燃料が過剰下
にある上段バーナ5の燃焼領域で発生する・CN、・N
H2および・N )I等の還元ラジカルと接触してN2
に還元されることとなる。
In this case, NO, generated in the combustion region of the lower stage burner 3 and middle stage burner 4, where there is a relatively large amount of air, is generated in the combustion region of the upper stage burner 5, where there is an excess of fuel.
H2 and N2 in contact with reducing radicals such as I
will be returned to.

二段燃焼法は、このような利点がある反面、上記燃焼ガ
ス中には未燃物が多量に含まれており、これをそのまま
排出することは煤じんの防止上および熱効率上好ましく
ないので、アフタエアポート6および7がら空気を供給
することにより、未燃物の完全燃焼化が計られている。
Although the two-stage combustion method has these advantages, the combustion gas contains a large amount of unburned matter, and it is not desirable to discharge it as it is from the viewpoint of preventing soot and dust and from the standpoint of thermal efficiency. By supplying air through the after air ports 6 and 7, complete combustion of unburned materials is achieved.

なお、上記燃焼部ともない発生する熱は、例えばボイラ
給水の蒸発用熱源として利用され、一方、高温排ガスは
火炉1上部の煙道を通り、必要により設けられる熱交換
器(図示省略)で熱回収されたのち大気中へ排出される
The heat generated by the above-mentioned combustion section is used, for example, as a heat source for evaporating boiler feed water, while the high-temperature exhaust gas passes through the flue at the top of the furnace 1 and is recovered by a heat exchanger (not shown) provided as necessary. It is then released into the atmosphere.

しかしながら、上記従来の燃焼装置におけるアフタエア
ポートからの空気供給は、空気通路管から空気を単にま
たは旋回流で噴出させるといった簡単な方法によって行
われていただめ、以下の欠点があった。すなわ°ち、空
気を単に噴出させる場合には、火炉壁面部への空気供給
が不充分となり、そこでの完全燃焼が困難となる。他方
、空気を旋回流で噴出させる場合には、上記とは逆に火
炉中心部への空気供給が不充分となり、該火炉中心部で
の完全燃焼が困難になるという不利がある。このような
不完全燃焼部分を生ずると結果的に煤じんが発生し易く
なるが、これを避けるためにはバーナ部での燃焼を強化
する必要があり、NO,抑制上好ましくない結果となる
However, the air supply from the after-air port in the above-mentioned conventional combustion apparatus was carried out by a simple method such as simply blowing out air from an air passage pipe or in a swirling flow, and this had the following drawbacks. That is, if air is simply blown out, the air supply to the furnace wall becomes insufficient and complete combustion there becomes difficult. On the other hand, when air is ejected in a swirling flow, there is a disadvantage in that, contrary to the above, the air supply to the center of the furnace becomes insufficient, making complete combustion in the center of the furnace difficult. If such an incomplete combustion part occurs, soot and dust are likely to be generated as a result, but in order to avoid this, it is necessary to strengthen the combustion in the burner part, which results in an unfavorable result in terms of suppressing NO.

本発明の目的は、上記した従来技術の欠点をなくシ、排
ガス中の煤じんを増加させることなくNO。
The object of the present invention is to eliminate the above-mentioned drawbacks of the prior art, and to eliminate NO without increasing soot and dust in exhaust gas.

を低減できる燃焼装置を提供することにある。The objective is to provide a combustion device that can reduce the

上記目的を達成するため、本発明は、複数個のバーナを
多段に設け、かつそれらの上方にアフタエアポートを設
けた燃焼装置において、上記アフタエアポートを、中心
部の一次空気通路管とその外周に順次設けられる二次以
上の空気通路とに分割し、かつ該−次空気通路管の火炉
側先端部に先細状絞りを設けたことを特徴とする。
In order to achieve the above object, the present invention provides a combustion apparatus in which a plurality of burners are provided in multiple stages and an after air port is provided above the burners, in which the after air port is provided between the primary air passage pipe in the center and its outer periphery. The present invention is characterized in that it is divided into secondary and higher air passages which are sequentially provided, and that a tapered throttle is provided at the front end of the secondary air passage pipe on the furnace side.

本発明においては、アフタエアポートを中心部の一次空
気通路管とその外周に順次設けられる二次以上の空気通
路に分割することにより、−次空気通路管により火炉中
心部への空気供給が良好に行なわれ、また二次以上の空
気通路により火炉壁面部への空気供給も好適に行なわれ
るので、火炉内部での空気不足個所の発生が解消し、均
一かつ完全な燃焼を達成することができる。また−次空
気通路管の火炉側先端部に先細状絞りを設けることによ
り、−次空気通路管内を送られてくる空気が加速される
とともに、噴出方向における空気密度が向上し、火炉中
心部への空気供給が好適に行なわれる。
In the present invention, by dividing the after-air port into a primary air passage pipe in the center and secondary and higher air passages sequentially provided on the outer periphery of the after-air port, the air supply to the center of the furnace is improved by the secondary air passage pipes. Furthermore, since air is suitably supplied to the furnace wall through the secondary and higher air passages, the occurrence of air-deficient areas within the furnace is eliminated, and uniform and complete combustion can be achieved. In addition, by providing a tapered throttle at the tip of the secondary air passage tube on the furnace side, the air sent through the secondary air passage tube is accelerated, and the air density in the jetting direction is improved, allowing it to reach the center of the furnace. air supply is carried out suitably.

上記噴出方向における空気密度をさらに向上させるだめ
には、−次空気通路管内に整流板を設けることが望まし
い、先細状絞りは通常、−次空気通路管の軸心方向に設
置されるが、該軸心に対し傾斜(偏向)して設けてもよ
い。その際、−次空気通路管を外部駆動手段と連結させ
て回転自在とすることにより、空気の噴出方向を所望方
向に設定することが可能となる。また燃焼状態の変化に
対応するだめ、各空気通路にはそれぞれに対応して空気
流量調節機構を設けることが望ましい。該空気流量調節
機構の内、二次以上の空気通路に設けるものは、噴出空
気を火炉壁面部に導く必要上、空気に適度な旋回流を与
え得るもの、例えばエアレジスタ等が好ましい。
In order to further improve the air density in the above-mentioned jetting direction, it is desirable to provide a rectifying plate in the secondary air passage pipe.A tapered throttle is usually installed in the axial direction of the secondary air passage pipe. It may be provided inclined (deflected) with respect to the axis. At this time, by connecting the secondary air passage pipe to an external drive means and making it rotatable, it is possible to set the direction of air ejection to a desired direction. In addition, in order to respond to changes in combustion conditions, it is desirable to provide an air flow rate adjustment mechanism for each air passage. Among the air flow rate regulating mechanisms, those provided in the secondary and higher air passages are preferably those capable of imparting an appropriate swirling flow to the air, such as an air register, since it is necessary to guide the ejected air to the furnace wall surface.

以下、図面に示す実施例により本発明をさらに詳しく説
明する。
Hereinafter, the present invention will be explained in more detail with reference to embodiments shown in the drawings.

第3図および第4図は、第1図および第2図に示す装置
のアフタエアポート6および7に代えて適用される本発
明のアフタエアポート部を拡大して示すものであり、こ
のものは、管内に格子状の整流板11と火炉側先端部に
先細状絞り13とを有し、かつ中心部に設けられた一次
空気通路管17と、該−次空気通路管17の外周に設け
られた二次空気通路15とから主として構成される。な
お、18は風箱、9は風箱18から送られる空気を一次
空気取入口10を経て一次空気通路管17へ導くに当り
、−天空気取入口10の開度を調節して取入空気量を制
御するための一次空気ダンパ、14は風箱18から送ら
れる空気の二次空気通路15への取入量を調節するとと
もに、取入空気に対し適度の旋回流を賦与することので
きる二次空気レジスタ、12は先細状絞り13の先端部
に形成される一次空気噴出口、8は火炉内壁である。
3 and 4 are enlarged views of the after air port portion of the present invention applied in place of the after air ports 6 and 7 of the device shown in FIGS. 1 and 2, which The primary air passage pipe 17 has a grid-like rectifier plate 11 in the pipe and a tapered throttle 13 at the tip end on the furnace side, and is provided in the center, and a primary air passage pipe 17 provided on the outer periphery of the secondary air passage pipe 17. It mainly consists of a secondary air passage 15. In addition, 18 is a wind box, and 9 is a wind box 18. When guiding the air sent from the wind box 18 to the primary air passage pipe 17 via the primary air intake 10, the opening degree of the sky air intake 10 is adjusted to control the intake air. The primary air damper 14 for controlling the amount of air can adjust the amount of air sent from the wind box 18 taken into the secondary air passage 15, and can also impart an appropriate swirling flow to the intake air. A secondary air register, 12 is a primary air outlet formed at the tip of a tapered throttle 13, and 8 is an inner wall of the furnace.

上記の構成とすることにより、風箱18から一次空気取
入口10を経て一次空気通路管17内へ取入られた空気
は、整流板11で整流後先細状絞り13で加速され、−
次空気噴出口12から高速高密度状態で火炉中心部へ噴
出される。これにより、従来空気供給が困難であった火
炉中心部に対しても充分に空気供給が可能となり、完全
燃焼が良好に達成される。
With the above configuration, the air taken from the wind box 18 through the primary air intake port 10 into the primary air passage pipe 17 is rectified by the rectifying plate 11, then accelerated by the tapered throttle 13, and -
The secondary air is ejected from the air outlet 12 at high speed and high density into the center of the furnace. As a result, sufficient air can be supplied to the center of the furnace, where it has been difficult to supply air in the past, and complete combustion can be achieved satisfactorily.

一方、風箱18から二次空気通路15へ送られる空気は
、二次空気レジスタ14で適度な旋回を与えられること
および二次空気通路15の噴出口部は先開状となってい
ること等が原因して、火炉壁面部への供給が良好となる
。これにより、従来空気供給が困難であった火炉壁面部
でも完全燃焼が可能となる。
On the other hand, the air sent from the wind box 18 to the secondary air passage 15 is given an appropriate swirl by the secondary air register 14, and the ejection port of the secondary air passage 15 is shaped like a tip. As a result, the supply to the furnace wall is improved. This makes it possible to achieve complete combustion even on the furnace wall, where it has been difficult to supply air in the past.

以上、木実施例によれば、火炉内への空気供給が均一に
達成されるので、不完全燃焼部の形成により煤じんが増
加することなく、そのため、バーナ部での燃焼をNO,
低減化に有利な燃料過剰の条件へさらに傾斜させること
が可能となり、一段と優れた低NOx化を達成すること
ができる。
As described above, according to the wood embodiment, air is uniformly supplied into the furnace, so there is no increase in soot and dust due to the formation of incomplete combustion parts, and therefore, the combustion in the burner part is reduced to NO.
It becomes possible to further incline to excessive fuel conditions that are advantageous for reduction, and it is possible to achieve even more excellent reduction in NOx.

次に、第5図は、本発明の他の実施例に係る装置を示す
もので、第3図に示す先細状絞り13に代え、空気噴出
方向が一次空気通路管17の軸に対し下方に傾斜した先
細状絞り16を設けたものである。
Next, FIG. 5 shows a device according to another embodiment of the present invention, in which instead of the tapered throttle 13 shown in FIG. A tapered slanted aperture 16 is provided.

上記構成とすることにより、火炉内での火炎上昇の影響
を少くできるので、−次空気の噴出到達距離が向上し、
これにともない燃焼性がより良好となる。なお、上記先
細状絞り16の空気噴出方向は下向に限る必要はない。
By adopting the above configuration, the influence of flame rise in the furnace can be reduced, so the ejection reach distance of secondary air is improved,
Accordingly, combustibility becomes better. Note that the air jetting direction of the tapered aperture 16 is not necessarily limited to the downward direction.

下向以外の方向忙適用するためには、−次空気通路管1
7を外部駆動手段(図示省略)により回転自在とすit
ばよ℃・。
In order to apply a direction other than downward, the -next air passage pipe 1
7 can be freely rotated by an external drive means (not shown).
Bye ℃・.

以上の説明は本発明の典型的プZ実施例につ℃・て行っ
たものであるが、本発明は勿論これらに19嗅定される
ものではなく、他に種々の態様や変形力(存在すること
はいうまでもない。1列えば、木精n月をi各バーナを
火炉の後側にも設けた対向設置方式の燃焼装置に対して
も同様に適用可能である。また、アフタエアポートは火
炉の前後壁に対向して二段以上設けることもでき、同様
な効果が得らiする。
Although the above explanation has been made with reference to typical embodiments of the present invention, the present invention is of course not intended to be limited to these embodiments, and may include various other aspects and deformation forces (existence). Needless to say, it can be applied in the same way to a combustion device with facing installation type in which each burner is installed on the rear side of the furnace. It is also possible to provide two or more stages facing the front and rear walls of the furnace, and the same effect can be obtained.

以上、本発明によれば、アフタエアポートを一次空気通
路管とその外周に順次設けられる二次以上の空気通路と
に分割することと、−次空気通路管の火炉側先端部に先
細状絞りを設けたことにより、−次空気通路管からは火
炉中心部への空気供給をまた、二次以上の空気通路から
(1火炉壁面@じへの空気供給をそれぞれ向上せしめる
ことカニできる。また、これにより、〕く−ナ部で発生
した未燃物を含む燃焼ガスの完全燃焼化が可能となり、
その結果、バーナ部ではNO!低減化に有利な燃料過剰
の燃焼条件を一段と進めることができる上に、アフタエ
アポート部では空気の供給量を極力抑ff1lJした所
謂紙02燃焼が可能となるので、ボイラ効率も改善され
る。
As described above, according to the present invention, the after-air port is divided into a primary air passage pipe and secondary and higher air passages sequentially provided on the outer periphery of the after-air port, and a tapered throttle is provided at the front end of the secondary air passage pipe on the furnace side. By providing this, it is possible to improve the air supply from the secondary air passage pipe to the center of the furnace, and from the secondary and higher air passages to the furnace wall surface. This makes it possible to completely burn the combustion gas containing unburned materials generated in the burner section.
As a result, NO! in the burner section! Not only can the combustion conditions for excess fuel, which are advantageous for reduction, be further advanced, but also so-called paper 02 combustion can be performed in which the amount of air supplied is suppressed as much as possible in the after-air port section, so the boiler efficiency is also improved.

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

第1図は、従来の燃焼装置を示す側断面図、第2図は、
第1図のA方向視図、第31図G主、本発明実施例に係
るアフタエアポート部の側断面図、第4図は、第3図の
C−C線に沿った矢視方向の断面図、第5図は、本発明
の他の実施例に係るアフタエアポート部の内、第3図の
Bに対応する部分の側断面図である。 3・・・下段バーナ、4・・・中段ノ(−す、5・・・
上段)(−す、6・・・前側アフタエアポート、7・・
・後側アフタエアポート、9・・・−次空気ダンノ(,
10・・・−天空気取入口、11・・・整流板、12・
・・−次空気噴出口、13・・・屍細状絞り、14・・
・二次空気レジスタ、15・・・二次空気通路、16・
・・偏向先細状絞り、17・・・−次空気通路管、18
・・・風箱。 代理人 弁理士  川 北 武 長 第1図 第3図 第2図 第4図 第5図 一^8 き゛
Figure 1 is a side sectional view showing a conventional combustion device, and Figure 2 is a
FIG. 31 is a side sectional view of the after air port section according to the embodiment of the present invention; FIG. 4 is a cross section taken along line C-C in FIG. 3 in the direction of arrows. 5 are side sectional views of a portion corresponding to B in FIG. 3 of an after air port portion according to another embodiment of the present invention. 3...lower burner, 4...middle burner (-su, 5...
Upper row) (-su, 6...Front side after air port, 7...
・Rear afterair port, 9...-Next air dunnno (,
10...-sky air intake, 11... rectifier plate, 12...
...-Next air outlet, 13... Corpse narrow aperture, 14...
・Secondary air register, 15...Secondary air passage, 16・
・・Deflection tapered aperture, 17 ・・Next air passage pipe, 18
...Wind box. Agent Patent Attorney Takenaga KawakitaFigure 1Figure 3Figure 2Figure 4Figure 5Figure 1^8 Ki゛

Claims (1)

【特許請求の範囲】 (1)複数個のバーナを多段に設け、かつそれらの上方
にアフタエアポートを設けた燃焼装置において、上記ア
フタエアポートを、中心部の一次空気通路とその外周に
順次設けられる二次以上の空気通路とに分割し、かつ該
−次空気通路の火炉側先端部に先細状絞りを設けたこと
を特徴とする燃焼装置。 (2、特許請求の範囲第1項において、各空気通路には
それぞれに対応して空気流肴調節機構を設けたことを特
徴とする燃焼装置。 (3)特許請求の範囲第1項において、−次空気通路に
整流板を設けたことを特徴とする燃焼装置。 (4) 4?許請求の範囲第1項において、先細状絞り
を偏向形状とし、かつ−次空気通路を回転自在としたこ
とを特徴とする燃焼装置。
[Claims] (1) In a combustion device in which a plurality of burners are provided in multiple stages and after air ports are provided above them, the after air ports are sequentially provided in the primary air passage in the center and the outer periphery thereof. A combustion device characterized in that the secondary air passage is divided into secondary or higher air passages, and a tapered throttle is provided at the front end of the secondary air passage on the furnace side. (2. In claim 1, the combustion device is characterized in that each air passage is provided with an air flow adjustment mechanism corresponding to each air passage. (3) In claim 1, - A combustion device characterized in that a rectifying plate is provided in the secondary air passage. (4) 4? In claim 1, the tapered throttle has a deflection shape, and the secondary air passage is rotatable. A combustion device characterized by:
JP57144769A 1982-08-23 1982-08-23 Combustion device Granted JPS5935707A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57144769A JPS5935707A (en) 1982-08-23 1982-08-23 Combustion device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57144769A JPS5935707A (en) 1982-08-23 1982-08-23 Combustion device

Publications (2)

Publication Number Publication Date
JPS5935707A true JPS5935707A (en) 1984-02-27
JPH0262767B2 JPH0262767B2 (en) 1990-12-26

Family

ID=15369985

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57144769A Granted JPS5935707A (en) 1982-08-23 1982-08-23 Combustion device

Country Status (1)

Country Link
JP (1) JPS5935707A (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4835426A (en) * 1971-09-13 1973-05-24

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4835426A (en) * 1971-09-13 1973-05-24

Also Published As

Publication number Publication date
JPH0262767B2 (en) 1990-12-26

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