JPS6335227Y2 - - Google Patents
Info
- Publication number
- JPS6335227Y2 JPS6335227Y2 JP5503284U JP5503284U JPS6335227Y2 JP S6335227 Y2 JPS6335227 Y2 JP S6335227Y2 JP 5503284 U JP5503284 U JP 5503284U JP 5503284 U JP5503284 U JP 5503284U JP S6335227 Y2 JPS6335227 Y2 JP S6335227Y2
- Authority
- JP
- Japan
- Prior art keywords
- tip
- fuel injection
- injection pipe
- burner
- gas
- 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
Links
- 238000002485 combustion reaction Methods 0.000 claims description 35
- 238000002347 injection Methods 0.000 claims description 29
- 239000007924 injection Substances 0.000 claims description 29
- 239000000446 fuel Substances 0.000 claims description 28
- 238000005192 partition Methods 0.000 claims description 6
- 239000007789 gas Substances 0.000 description 41
- 239000002737 fuel gas Substances 0.000 description 5
- 238000009792 diffusion process Methods 0.000 description 4
- 239000000567 combustion gas Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000571 coke Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 229910001882 dioxygen Inorganic materials 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
Landscapes
- Gas Burners (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Description
(産業上の利用分野)
本考案は、高炉ガス等の低カロリーガスを燃焼
室内の温度に関係なく且つ、着火後はパイロツト
バーナを必要とせず安定燃焼させるようにした低
カロリーガス燃焼用バーナに関するものである。
(従来技術とその問題点)
ガスバーナには、一般に燃焼ガスと空気とを
別々に噴出し、拡散混合して燃焼させる拡散燃焼
型ガスバーナと、燃焼ガスと空気或いは酸素ガス
を燃焼前に予め混合して燃焼させる予混合燃焼型
ガスバーナとに大別されるが、工業炉において
は、前者の拡散燃焼型ガスバーナが多用されてい
る。この拡散燃焼型ガスバーナの中でも、燃焼用
空気に強い旋回を与えてその空気と燃料ガスとの
混合性を良好にし、燃焼効率を高めるようにした
高旋回流バーナが脚光を沿びている。
しかし、上記のような従来の高旋回流バーナに
あつては、コークス炉ガス等の高カロリーガス
や、高炉ガスのような低カロリーガスに高カロリ
ーガスを混合したものを燃料ガスとして用いられ
ているのが通常であり、低カロリーガスのみを単
独の燃料ガスとして用いた場合には、その燃料単
位量を燃焼させるに必要な空気量が低下するた
め、旋回流による火炎安定効果が低下し、雰囲気
ガスとの混合により希薄な燃焼となり、火炎温度
が低下し、安定燃焼ができず燃焼可能量の低下を
来たすため、実用不可能なものであつた。
また、上記バーナ以外の低カロリーガス専焼用
バーナとして、熱風発生炉などを対象としたもの
もあるが、これは空気および燃料ガスの流速を遅
くして両者の混合を緩慢にして燃焼させようとす
るものであり、燃焼容量に対してバーナの主要寸
法が大きくなり、且つ加熱炉の炉内温度が低い場
合には、火炎が不安定になるという問題が有り、
可及的に安定した燃焼を行なわせるためには、常
時、パイロツトバーナを用いる以外に対策がなか
つた。
(考案の目的)
本考案は、上記問題点に鑑みてなされたもので
あり、常温の低カロリーガスを単独で2段に投入
して燃焼用空気との混合比が異なる領域をもつた
火炎部を形成させるよう構成することにより、冷
炉においても、着火後はパイロツトバーナを必要
とすることなく安定燃焼させることができるよう
にしたコンパクト設計の低カロリーガス燃焼用バ
ーナを提供することを目的とするものである。
(考案の構成)
すなわち、本考案の低カロリーガス燃焼用バー
ナは、バーナ本体の中心にその先端がバーナタイ
ル内に臨むサイトホールを備えると共に、該サイ
トホールの外周に、通路内に旋回羽根を設けてそ
の先端を前記サイトホールよりも稍突出状に臨ま
せた2次燃料噴射管と、先端に整流板を備えて該
先端を前記バーナタイルより後方に位置させた一
次燃料噴射管と、通路内に旋回羽根を設けてその
先端を前記バーナタイルの後面に位置させた空気
導入管を順次同心円状に配設し、しかも前記2次
燃料噴射管の先端内周と前記サイトホールの先端
外周面には、先端をその2次燃料噴射管の先端よ
り後方に位置させるよう該噴射管の内壁に環状仕
切板を固設し、且つ該仕切板固定位置前方の前記
2次燃料噴射管の所定部位には、その周方向に所
定間隔を存して複数の開孔部を穿設せしめてなる
ものである。
(実施例)
以下本考案の低カロリーガス燃焼用バーナを図
面に示す一実施例に基づき詳細に説明する。
図中1は、本考案の低カロリーガス燃焼用バー
ナを示すものであり、該バーナ1は、高炉ガス等
の低カロリーガスを2段に個別供給することによ
り、燃焼用空気との異なる混合比を有する燃料ガ
スを多層的に噴出して、且つ、これを燃焼させる
ことにより、3領域からなる火炎部を形成させる
ように構成したものである。
而して、2はバーナ1本体の中心に配備された
サイトホールであり、該サイトホール2の先端
は、燃焼領域を構成するバーナタイル3内に稍臨
ませている。
また、4は前記サイトホール2の外周に同心円
状に設けられた低カロリーガス供給用の2次燃料
噴射管であり、該2次燃料噴射管4は、その先端
がバーナタイル3内に前記サイトホール2よりも
稍突出すべく臨ませて、(バーナタイル3長さの
約1/5)且つその噴射管4内の燃料通路には流通
ガスに旋回流を与えてバーナタイル3内に供給す
べく旋回羽根5を設けたものである。
更に6は、前記2次燃料噴射管4の外周に同心
円状に設けられた低カロリーガス供給用の1次燃
料噴射管であり、該1次燃料噴射管6は、その先
端が前記バーナタイル3より後方に位置され且つ
噴射管4の先端に第2図に示すような整流板7が
設けられたものである。
更にまた、8は前記1次燃料噴射管6の外周に
同心円状に設けられた燃焼用空気送給用の空気導
入管であり、該空気導入管8は、その先端が前記
バーナタイル3の後面に位置するよう配備され、
且つ該導入管8内の空気流通路には燃焼用空気に
旋回流を与える旋回羽根9を設けて、前記1次燃
料噴射管6から供給される低カロリーガスと燃焼
用空気とを可及的良好に混合させるようにしたも
のである。
また、10は前記2次燃料噴射管4の先端内周
と前記サイトホール2の先端外周間に設けられた
環状仕切板であり、該仕切板10は第3図に示し
たように、その先端が前記2次燃料噴射管4の先
端より後方で且つ前記サイトホール2の先端より
前方に位置するよう、2次燃料噴射管4の内壁に
固設され、2次燃料噴射管4に絞り部を形成させ
るようにしたものである。
尚、11は前記2次燃料噴射管4の先端部近傍
に、周方向に所定間隔を存して複数個を穿設せし
めた開孔部である。
(考案の作用)
本考案の低カロリーガス燃焼用バーナは、以上
の一実施例で示したように構成されたものであ
り、これを使用するにあつては第3図に示すよう
に、2次燃料噴射管4より供給された低カロリー
ガスは単独で燃焼して火炎の炎心部aを形成し、
(Field of Industrial Application) The present invention relates to a burner for burning low-calorie gas such as blast furnace gas, which stably burns low-calorie gas such as blast furnace gas regardless of the temperature inside the combustion chamber and without the need for a pilot burner after ignition. It is something. (Prior art and its problems) Gas burners generally include diffusion combustion type gas burners, which eject combustion gas and air separately and burn them by diffusion mixing, and gas burners, which mix combustion gas and air or oxygen gas in advance before combustion. It is broadly divided into premix combustion type gas burners and premix combustion type gas burners, which perform combustion in different ways.In industrial furnaces, the former diffusion combustion type gas burners are often used. Among these diffusion combustion type gas burners, high swirl flow burners that give strong swirl to combustion air to improve the mixing properties of the air and fuel gas and increase combustion efficiency are attracting attention. However, in the case of the conventional high swirl flow burner described above, a mixture of high calorie gas such as coke oven gas or low calorie gas such as blast furnace gas with high calorie gas is used as fuel gas. Normally, when only low-calorie gas is used as the sole fuel gas, the amount of air required to burn a unit amount of fuel decreases, so the flame stabilizing effect due to swirling flow decreases. Mixing with atmospheric gas results in lean combustion, lowering the flame temperature, making stable combustion impossible and reducing the combustible amount, making it impractical. In addition, there are burners for burning only low-calorie gas other than the burners mentioned above, which are intended for hot air generators, etc., but these burn by slowing down the flow velocity of air and fuel gas to slow the mixing of the two. If the main dimensions of the burner are large relative to the combustion capacity and the temperature inside the heating furnace is low, there is a problem that the flame becomes unstable.
In order to achieve as stable combustion as possible, there was no other option than to use a pilot burner at all times. (Purpose of the invention) The present invention was made in view of the above-mentioned problems, and consists of a flame section in which low-calorie gas at room temperature is separately introduced into two stages and has regions with different mixing ratios with combustion air. The purpose of the present invention is to provide a low-calorie gas combustion burner with a compact design that enables stable combustion even in a cold furnace without requiring a pilot burner after ignition. It is something to do. (Structure of the invention) In other words, the low-calorie gas combustion burner of the invention is provided with a sight hole in the center of the burner body, the tip of which faces into the burner tile, and a swirl vane in the passage around the outer periphery of the sight hole. a secondary fuel injection pipe whose tip is slightly protruding from the sight hole; a primary fuel injection pipe whose tip is provided with a baffle plate and whose tip is positioned rearward from the burner tile; and a passageway. Air introduction pipes each having a swirl vane therein and having a tip thereof located on the rear surface of the burner tile are successively arranged concentrically, and furthermore, the inner circumference of the tip of the secondary fuel injection pipe and the outer circumference of the tip of the sight hole are arranged concentrically. An annular partition plate is fixed to the inner wall of the injection pipe so that the tip thereof is located behind the tip of the secondary fuel injection pipe, and a predetermined portion of the secondary fuel injection pipe is located in front of the position where the partition plate is fixed. A plurality of openings are formed at predetermined intervals in the circumferential direction. (Example) The low calorie gas combustion burner of the present invention will be described in detail below based on an example shown in the drawings. Reference numeral 1 in the figure shows a burner for burning low-calorie gas according to the present invention, and the burner 1 is configured to supply low-calorie gas such as blast furnace gas to two stages individually, so that it can be mixed at different mixing ratios with combustion air. The fuel gas is ejected in multiple layers and is combusted to form a flame section consisting of three regions. Reference numeral 2 denotes a sight hole located at the center of the main body of the burner 1, and the tip of the sight hole 2 slightly faces into the burner tile 3 constituting the combustion area. Further, reference numeral 4 denotes a secondary fuel injection pipe for supplying low-calorie gas that is provided concentrically around the outer periphery of the sight hole 2, and the tip of the secondary fuel injection pipe 4 is located inside the burner tile 3 at the site. It is arranged so as to protrude slightly from the hole 2 (approximately 1/5 of the length of the burner tile 3), and the fuel passage in the injection pipe 4 provides a swirling flow to the circulating gas and supplies it into the burner tile 3. A swirling vane 5 is provided to suit the purpose. Furthermore, 6 is a primary fuel injection pipe for supplying low-calorie gas that is provided concentrically around the outer periphery of the secondary fuel injection pipe 4, and the tip of the primary fuel injection pipe 6 is connected to the burner tile 3. A rectifier plate 7 as shown in FIG. 2 is provided at the tip of the injection pipe 4 and is located further rearward. Furthermore, 8 is an air introduction pipe for supplying combustion air that is provided concentrically around the outer periphery of the primary fuel injection pipe 6, and the tip of the air introduction pipe 8 is connected to the rear surface of the burner tile 3. located at
In addition, a swirling vane 9 that gives a swirling flow to the combustion air is provided in the air flow path in the introduction pipe 8, so that the low calorie gas supplied from the primary fuel injection pipe 6 and the combustion air are mixed as much as possible. This ensures good mixing. Further, 10 is an annular partition plate provided between the inner periphery of the tip of the secondary fuel injection pipe 4 and the outer periphery of the tip of the sight hole 2, and the partition plate 10 is, as shown in FIG. is fixed to the inner wall of the secondary fuel injection pipe 4 so that it is located behind the tip of the secondary fuel injection pipe 4 and in front of the tip of the sight hole 2, and a constriction part is provided in the secondary fuel injection pipe 4. It is designed to allow the formation of Incidentally, reference numeral 11 denotes a plurality of openings formed near the tip of the secondary fuel injection pipe 4 at predetermined intervals in the circumferential direction. (Function of the invention) The low-calorie gas combustion burner of the invention is constructed as shown in the above embodiment, and when using it, as shown in FIG. The low calorie gas supplied from the next fuel injection pipe 4 burns independently to form the flame core a of the flame,
【表】
また、第2表に本考案と従来の低カロリーガス
燃焼用バーナを用いて、下記の燃焼条件で低カロ
リーガスを燃焼した場合の排ガス中のCO及びO2
濃度を示す。
〈燃焼条件〉
(1) バーナを点火し、炉内温度が800℃以上にな
るまで燃焼させる。(燃焼量は80%)
(2) 低カロリーガス燃料流通量を一定にして、燃
焼用空気量を減少させてゆき、各段階での排ガ
ス濃度を炉尻にて測定する。[Table] Table 2 shows the amount of CO and O2 in the exhaust gas when low-calorie gas is burned under the following combustion conditions using a burner for burning low-calorie gas in this invention and a conventional burner for burning low-calorie gas.
The concentration is shown. <Combustion conditions> (1) Ignite the burner and burn until the temperature inside the furnace reaches 800°C or higher. (Combustion amount is 80%) (2) Keep the flow rate of low-calorie gas fuel constant and reduce the amount of combustion air, measuring the exhaust gas concentration at each stage at the end of the furnace.
【表】
第2表から明らかなように、本考案のバーナに
よれば、従来のものに比べて燃焼用空気を少なく
して安定燃焼が可能であり、またCO発生量も、
従来に比べて遥かに少なことがわかる。
(考案の効果)
以上のように、本考案の低カロリーガス燃焼用
バーナは、常温の低カロリーガスを2段に分離供
給して空気混合比の異なる3領域をもつた火炎部
を形成させるようにしたものであるから、バーナ
における圧損の低減が図られると共に、着火後は
パイロツトバーナを必要とすることなく安定燃焼
させることができ、しかもコンパクトに設計でき
るものであり、従来の問題を一掃し得る有益なも
のである。[Table] As is clear from Table 2, the burner of the present invention enables stable combustion with less combustion air than conventional burners, and also reduces the amount of CO generated.
It can be seen that this is much less than before. (Effects of the invention) As described above, the low-calorie gas combustion burner of the present invention separates and supplies low-calorie gas at room temperature in two stages to form a flame section having three regions with different air mixing ratios. This reduces the pressure drop in the burner, and after ignition, it is possible to achieve stable combustion without the need for a pilot burner. Moreover, it can be designed compactly, eliminating the problems of the conventional method. It is a useful thing to gain.
第1図は、本考案の一実施例を示す縦断面図、
第2図は、第1図のA−A断面図、第3図は、本
考案の一実施例を示す一部拡大断面図。
1は低カロリーガス燃焼用バーナ、2はサイト
ホール、3はバーナタイル、4は2次燃料噴射
管、5,9は旋回羽根、6は1次燃料噴射管、7
は整流板、8は空気導入管、10は環状仕切板、
11は開孔部。
FIG. 1 is a longitudinal sectional view showing an embodiment of the present invention;
FIG. 2 is a sectional view taken along the line AA in FIG. 1, and FIG. 3 is a partially enlarged sectional view showing an embodiment of the present invention. 1 is a low-calorie gas combustion burner, 2 is a sight hole, 3 is a burner tile, 4 is a secondary fuel injection pipe, 5 and 9 are swirl vanes, 6 is a primary fuel injection pipe, 7
is a rectifying plate, 8 is an air introduction pipe, 10 is an annular partition plate,
11 is an opening.
Claims (1)
臨むサイトホールを備えると共に、該サイトホー
ルの外周に、通路内に旋回羽根を設けてその先端
を前記サイトホールよりも稍突出状に臨ませた2
次燃料噴射管と、先端に整流板を備えて、該先端
を前記バーナタイルより後方に位置させた一次燃
料噴射管と、通路内に旋回羽根を設けてその先端
を前記バーナタイルの後面に位置させた空気導入
管を、順次同心円状に配設し、しかも前記2次燃
料噴射管の先端内周と前記サイトホールの先端外
周間には、先端を2次燃料噴射管先端より後方に
位置させた環状仕切板を、該噴射管内壁に固設
し、且つ前記2次燃料噴射管の先端近傍には、そ
の周方向に所定間隔を存して、複数の開孔部を穿
設してなることを特徴とする低カロリーガス燃焼
用バーナ。 At the center of the burner body, there is provided a sight hole whose tip faces into the burner tile, and at the outer periphery of the sight hole, a swirl vane is provided in the passage so that its tip faces out in a slightly protruding shape from the sight hole.
a secondary fuel injection pipe, a primary fuel injection pipe having a rectifying plate at the tip and having the tip located behind the burner tile; and a swirl vane provided in the passage and having the tip positioned at the rear of the burner tile. The air introduction pipes are sequentially arranged concentrically, and the tips are positioned rearward from the tips of the secondary fuel injection pipes between the inner periphery of the tips of the secondary fuel injection pipes and the outer periphery of the tips of the sight holes. An annular partition plate is fixed to the inner wall of the injection pipe, and a plurality of openings are bored at predetermined intervals in the circumferential direction near the tip of the secondary fuel injection pipe. A low calorie gas combustion burner characterized by:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5503284U JPS60170522U (en) | 1984-04-13 | 1984-04-13 | Low calorie gas combustion burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5503284U JPS60170522U (en) | 1984-04-13 | 1984-04-13 | Low calorie gas combustion burner |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS60170522U JPS60170522U (en) | 1985-11-12 |
JPS6335227Y2 true JPS6335227Y2 (en) | 1988-09-19 |
Family
ID=30577325
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP5503284U Granted JPS60170522U (en) | 1984-04-13 | 1984-04-13 | Low calorie gas combustion burner |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS60170522U (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6124596B2 (en) * | 2013-01-09 | 2017-05-10 | 大阪瓦斯株式会社 | Burner nozzle and flame detection structure |
-
1984
- 1984-04-13 JP JP5503284U patent/JPS60170522U/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS60170522U (en) | 1985-11-12 |
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