JPS6363813B2 - - Google Patents
Info
- Publication number
- JPS6363813B2 JPS6363813B2 JP55164711A JP16471180A JPS6363813B2 JP S6363813 B2 JPS6363813 B2 JP S6363813B2 JP 55164711 A JP55164711 A JP 55164711A JP 16471180 A JP16471180 A JP 16471180A JP S6363813 B2 JPS6363813 B2 JP S6363813B2
- Authority
- JP
- Japan
- Prior art keywords
- secondary air
- blades
- combustion
- bevel gear
- swirler
- 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
Landscapes
- Air Supply (AREA)
Description
【発明の詳細な説明】
この発明はバーナ燃焼排ガス中の未燃分を完全
燃焼させるアフターエアポート用二次空気を供給
する装置、特に空気流路内に設けた羽根を、燃焼
用空気流れ方向に対する傾斜角度を可変にした二
次空気供給用スワラ装置の構造に関する。Detailed Description of the Invention The present invention relates to a device for supplying secondary air for an after-air port to completely burn unburned components in burner combustion exhaust gas, and in particular, a device for supplying secondary air for an after-air port to completely burn unburned components in burner combustion exhaust gas, and in particular, a device for supplying secondary air for an after-air port to completely burn unburned components in burner combustion exhaust gas. The present invention relates to a structure of a swirler device for supplying secondary air with variable inclination angle.
大気汚染物質の一つである室素酸化物(以下
NOxと称する)の低減方法としてボイラ等の燃
焼装置において採用されているのは次の如きもの
である。すなわち(1)二段燃焼法、(2)低NOxバー
ナの使用、(3)排ガスの混入等であり、さらに最近
では特定のバーナを不完全燃焼させ、これにより
生ずる中間生成物の還元作用によりNOxを還元
処理する方法を採用されている。しかしこれらの
方法はいずれも燃焼の観点から見た場合には不完
全燃焼を起こさせるものであつて、燃焼効率は低
下する。このため通常低NOx運転に当つては上
記方法を何種か組み合せることにより低NOx化
を図る一方燃焼効率も向上するように努めてい
る。 Chlorine oxide (hereinafter referred to as
The following methods have been adopted in combustion equipment such as boilers to reduce NOx (referred to as NOx). In other words, (1) the two-stage combustion method, (2) the use of low NOx burners, (3) the mixing of exhaust gas, etc., and more recently, the incomplete combustion of certain burners, and the reduction effect of the resulting intermediate products. A method of reducing NOx has been adopted. However, all of these methods cause incomplete combustion when viewed from the viewpoint of combustion, and the combustion efficiency decreases. For this reason, during low NOx operation, efforts are usually made to reduce NOx while also improving combustion efficiency by combining several of the above methods.
例えば二段燃焼法においても、第一段燃焼にお
いて低酸素燃焼を行うのみでなく、排ガスを導入
して火炎温度を低下させる等の方法が併用される
ことが多い。この場合当然のことながら第一段燃
焼においては未燃カーボン等の未燃分が相当量発
生する。このため前記第一段燃焼部の燃焼ガス流
の後流に二次空気を供給する開口を火炉壁面に設
け、この開口からの二次空気を炉内に流入させ燃
焼ガス中の未燃分を燃焼させている。 For example, even in the two-stage combustion method, in addition to performing low-oxygen combustion in the first stage combustion, methods such as introducing exhaust gas to lower the flame temperature are often used in combination. In this case, as a matter of course, a considerable amount of unburned matter such as unburned carbon is generated in the first stage combustion. For this purpose, an opening is provided in the furnace wall to supply secondary air to the wake of the combustion gas flow from the first stage combustion section, and the secondary air from this opening is allowed to flow into the furnace to remove unburned matter in the combustion gas. It's burning.
(この開口をアフターエアポートと称す。)従
来この開口に設ける装置については燃焼負荷に対
応する二次空気の炉内への貫通流入力増強につい
て格別の配慮がされていなかつた。 (This opening is referred to as an after-air port.) Conventionally, no special consideration has been given to the device installed in this opening to enhance the input of secondary air throughflow into the furnace in response to the combustion load.
また近時の低NOx燃焼手段においては、空気
比1以下の主バーナの燃焼ガス後流に更に空気比
0.6等の低空気比のバーナ(副バーナ)を設け、
この副バーナにより発生した還元性中間生成物を
用いて燃焼ガス中のNOxを除去する手段が採用
されている。 In addition, in recent low NOx combustion methods, an air ratio
A burner (auxiliary burner) with a low air ratio of 0.6 etc. is installed,
A method is employed to remove NOx from the combustion gas by using reducing intermediate products generated by the auxiliary burner.
またこの場合においても低空気比バーナを使用
することから排ガス中の未燃成分は多いものであ
り、前記したアフターエアポートを設け、二次空
気供給により未燃成分を充分に燃焼させることが
必要である。 Also in this case, since a low air ratio burner is used, there are many unburned components in the exhaust gas, so it is necessary to provide the above-mentioned after-air port and supply secondary air to sufficiently burn the unburned components. be.
一方通常のバーナや低空気比バーナにおいて
は、バーナと一体構造でバーナ周りからバーナ火
炎を囲むように二次空気を供給して燃料との混合
をよくし燃焼負荷が変つても良好な燃焼をするよ
うな固定羽根付きのバーナ構造を採用している。
(例えば特開昭53−145130号の発明、特開昭54−
13017号公報の発明)。 On the other hand, ordinary burners and low air ratio burners are built integrally with the burner and supply secondary air from around the burner to surround the burner flame to improve mixing with the fuel and ensure good combustion even when the combustion load changes. A burner structure with fixed blades is adopted.
(For example, the invention of JP-A-53-145130, JP-A-54-
Invention of Publication No. 13017).
しかしこれらは何れも二次空気の旋回力付与手
段としては固定の旋回用羽根を使用しているため
ボイラの負荷変化に対応する燃料量に対し適当し
た燃焼状態を形成する、二次空気には十分な噴出
エネルギー、旋回エネルギーが与えられないこと
になり、供給される空気量に比較して未燃分の燃
焼率が低下し煤塵や未燃分が増加する。 However, since all of these use fixed swirling vanes as means for imparting swirling force to the secondary air, they create a combustion state appropriate for the amount of fuel that corresponds to changes in the boiler load. Sufficient ejection energy and swirling energy will not be given, and the combustion rate of unburned matter will decrease compared to the amount of air supplied, and soot and dust and unburned matter will increase.
この発明の目的は上述した問題点を除去し、二
次空気供給量の多少にかかわらず空気に十分な噴
射エネルギー、旋回エネルギーを与えることがで
きるアフターエアポート用二次空気供給用スワラ
装置を提供することにある。 An object of the present invention is to eliminate the above-mentioned problems and provide a swirler device for supplying secondary air for an after-airport, which can give sufficient injection energy and swirling energy to the air regardless of the amount of secondary air supplied. There is a particular thing.
要するにこの発明はアフターエアポートに設け
る二次空気供給用スロート部にスワラ(旋回器)
を配置し、かつこのスワラの羽根(ブレード)が
回動しその取り付け角即ち燃焼用空気流れ方向に
対するブレード面の傾斜角度を可変とするよう構
成したものである。 In short, this invention uses a swirler (swirler) in the throat section for secondary air supply provided at the after air port.
The swirler blades are arranged so that the blades of the swirler can be rotated to vary the mounting angle, that is, the inclination angle of the blade surface with respect to the direction of combustion air flow.
以下この発明の実施例を図面を用いて説明す
る。 Embodiments of the present invention will be described below with reference to the drawings.
第1図および第2図はこの発明に係る回動ブレ
ード付きスワラ装置の構造を示す。図中1はスワ
ラ本体を支える支持軸で、支持軸1の内部にはこ
の支持軸1の中心軸線上に位置するよう回転軸2
が配置してある。回転軸2の火炉側端部(図中右
側)には親傘歯車3が設けてある。一方支持軸1
の火炉側端部には支柱4により支持軸1に取り付
けたダクト5が配置してあり、このダクト5内に
は支持軸1を中心として複数枚の羽根6が放射状
に配置してある。この羽根6の構成を第1図に示
した羽根6aによつて説明すると、羽根6aのダ
クト側端部はダクト5に取り付けたボルト7と羽
根6a側に形成したボス8の係合により羽根6a
がダクト5に対して自由回転するよう形成してあ
る。一方羽根6aの支持軸側端部には調節軸9が
固設してあり、この調節軸9は支持軸1を挿通
し、その先端には前記親傘歯車3に係合する子傘
歯車10が取り付けてある。他の羽根6も以上に
説明した羽根6aと同一構造となつており、回転
軸2の回転が親傘歯車3、各子傘歯車10および
各調節軸9経て羽根6に伝わり、各羽根の支持軸
1の軸心に平行する空気流れに対する傾斜、つま
り回転軸2の中心軸線に対する羽根面の傾斜角度
を調節する。 1 and 2 show the structure of a swirler device with rotating blades according to the present invention. In the figure, 1 is a support shaft that supports the swirler body, and inside the support shaft 1 there is a rotating shaft 2 located on the center axis of this support shaft 1.
is placed. A parent bevel gear 3 is provided at the furnace side end of the rotating shaft 2 (on the right side in the figure). One side support shaft 1
A duct 5 attached to a support shaft 1 by a strut 4 is arranged at the end of the furnace side, and within this duct 5 a plurality of blades 6 are arranged radially around the support shaft 1. The configuration of this blade 6 will be explained using the blade 6a shown in FIG.
is formed to rotate freely relative to the duct 5. On the other hand, an adjustment shaft 9 is fixed to the end of the blade 6a on the support shaft side.The adjustment shaft 9 passes through the support shaft 1, and at its tip there is a child bevel gear 10 that engages with the parent bevel gear 3. is installed. The other blades 6 have the same structure as the blade 6a described above, and the rotation of the rotating shaft 2 is transmitted to the blade 6 via the parent bevel gear 3, each child bevel gear 10, and each adjustment shaft 9, and supports each blade. The inclination with respect to the air flow parallel to the axis of the shaft 1, that is, the inclination angle of the blade surface with respect to the central axis of the rotating shaft 2 is adjusted.
次に回転軸2および支持軸1は風箱11の壁面
11aを挿通して外部に突出配置してあり、この
うち回転軸2は角度調節器20に接続している。
回転軸2の端部は約90゜曲折して調節器接続部2
aとなつておりこの調節器接続部2aの端部はピ
ン21に回転可能に嵌挿してある。22はピン2
1に形成したフランジ21aを介してピン先端部
を係合穴23に挿入するバネである。作業者は羽
根(ブレード)6の支持軸軸心に対する傾斜角度
を変更したい場合には先ずハンドル24をX方向
に引いてピン21と係合穴23の係合状態を解除
ししかる後ハンドル24をX′もしくはY′方向に
移動させて別の係合穴とピンを係合させ羽根6の
バーナ軸心に対する傾斜角度αを変更する(第3
図参照)。なお係合穴23とピン21の係合が完
了すればハンドル24はバネ22によりY方向に
戻る。 Next, the rotating shaft 2 and the supporting shaft 1 are inserted through the wall surface 11a of the wind box 11 and protruded to the outside, and the rotating shaft 2 is connected to the angle adjuster 20.
The end of the rotating shaft 2 is bent approximately 90 degrees and connected to the regulator connection part 2.
The end of the regulator connecting portion 2a is rotatably fitted into the pin 21. 22 is pin 2
This spring inserts the tip end of the pin into the engagement hole 23 via the flange 21a formed in 1. When the operator wants to change the inclination angle of the blade 6 with respect to the support shaft axis, the operator first pulls the handle 24 in the X direction to release the engagement between the pin 21 and the engagement hole 23, and then pulls the handle 24. The blade 6 is moved in the X' or Y' direction to engage another engagement hole and the pin to change the inclination angle α of the blade 6 with respect to the burner axis (third
(see figure). Note that when the engagement between the engagement hole 23 and the pin 21 is completed, the handle 24 is returned to the Y direction by the spring 22.
第4図は以上説明した回動ブレード付きスワラ
装置をボイラの二次空気供給部を配置した状態を
示す。ボイラの炉壁15に形成した二段燃焼用空
気スロート14の最大直径Dはこのスロート14
から噴射される二次空気Aの最大流量を基準とし
て定めてある。前述した回動ブレード付きスワラ
はこのスロートの中央部に配置され、二段燃焼用
の二次空気Aは通常その大部分がスロート14を
通過し、かつスワラの羽根6により旋回力を与え
られて火炉16に噴射される。なお二次空気の一
部はダクト5とスロート14の壁面の間をスワラ
による旋回空気流れを囲み流れ、この旋回力を低
減させることはない。この場合ボイラ負荷が低下
したり、二段燃焼比率が変更されて二次空気量が
低下した場合には羽根6の傾斜角度αを大きくし
い二次空気の旋回エネルギーが低下するのを防止
する。さらにこの傾斜角度調節によつても十分な
エネルギーが得られないほどに二次空気供給量が
低下した場合には角度αをほぼ90゜に近づけスワ
ラを全閉とする。これにより二次空気はスワラ装
置のダクト5とスロート14との間の狭い環状空
間を経て噴射されるので高い噴射エネルギーを得
ることができる。 FIG. 4 shows a state in which the above-described swirler device with rotating blades is arranged in a secondary air supply section of a boiler. The maximum diameter D of the air throat 14 for two-stage combustion formed in the furnace wall 15 of the boiler is
It is determined based on the maximum flow rate of secondary air A injected from. The aforementioned swirler with rotating blades is placed in the center of this throat, and most of the secondary air A for two-stage combustion normally passes through the throat 14 and is given a swirling force by the blades 6 of the swirler. It is injected into the furnace 16. Note that a part of the secondary air flows between the wall surface of the duct 5 and the throat 14 surrounding the swirling air flow due to the swirler, and this swirling force is not reduced. In this case, when the boiler load decreases or the secondary air amount decreases due to a change in the two-stage combustion ratio, the inclination angle α of the blade 6 is increased to prevent the swirling energy of the secondary air from decreasing. Furthermore, if the amount of secondary air supply decreases to the extent that sufficient energy cannot be obtained even with this tilt angle adjustment, the angle α is brought to approximately 90° and the swirler is fully closed. As a result, the secondary air is injected through the narrow annular space between the duct 5 and the throat 14 of the swirler device, so that high injection energy can be obtained.
この発明を実施することにより、空気流量の多
少にかかわらず、炉内に供給する空気に対し常に
十分な旋回力もしくは噴射力を与えることがで
き、低NOx燃焼における未燃成分の完全燃焼の
効果をあげることができる。 By implementing this invention, it is possible to always provide sufficient swirling force or injection force to the air supplied into the furnace regardless of the air flow rate, and the effect of complete combustion of unburned components in low NOx combustion. can be given.
第1図はこの発明に係る回動ブレード付きスワ
ラ装置の断面図、第2図は第1図の斜視図、第3
図は傾斜角度調節器の斜視図、第4図は二次空気
供給用スワラ装置のスロートを含む縦断面図であ
る。
1……支持軸、2……回転軸、3……親傘歯
車、5……ダクト、6……羽根、9……調節軸、
10……子傘歯車、α……傾斜角度。
FIG. 1 is a sectional view of a swirler device with rotating blades according to the present invention, FIG. 2 is a perspective view of FIG. 1, and FIG.
The figure is a perspective view of the inclination angle adjuster, and FIG. 4 is a longitudinal sectional view including the throat of the swirler device for supplying secondary air. 1... Support shaft, 2... Rotating shaft, 3... Main bevel gear, 5... Duct, 6... Vane, 9... Adjustment shaft,
10... Child bevel gear, α... Inclination angle.
Claims (1)
るアフターエアポート用二次空気を供給するもの
において、 二次空気流路のスロート内に複数枚の羽根をス
ロート中心線から放射状に展出配置して燃焼空気
に旋回力を与えるものに、該複数枚の羽根の面の
空気流れ方向に対する傾斜角度を変更する駆動装
置を設け、かつ前記複数枚の羽根の外端部を囲む
ダクトを設けたことを特徴とする二次空気供給用
スワラ装置。 2 支持軸内にこの支持軸と同一軸心線上に位置
するよう回転軸を配置し、この回転軸の火炉側端
部には親傘歯車を設け、かつ前記複数枚の羽根は
一方の端部をダクトに対して回転自由に取り付
け、他方の端部には調節軸を介して親傘歯車と係
合する子傘歯車をそれぞれ取りつけて回転軸の回
転により各羽根のガス流れ方向に対する傾斜角度
を変更するよう構成したことを特徴とする特許請
求の範囲第1項記載の二次空気供給用スワラ装
置。[Scope of Claims] 1. In a device that supplies secondary air for an after-air port to completely burn unburned content in burner combustion exhaust gas, a plurality of blades are installed in the throat of the secondary air flow path radially from the throat center line. a driving device for changing the angle of inclination of the surfaces of the plurality of blades with respect to the air flow direction, and surrounding the outer ends of the plurality of blades; A swirler device for supplying secondary air characterized by being provided with a duct. 2. A rotating shaft is arranged within the supporting shaft so as to be located on the same axis as the supporting shaft, and a parent bevel gear is provided at the furnace side end of the rotating shaft, and the plurality of blades are arranged at one end. is attached to the duct so that it can rotate freely, and a child bevel gear that engages with the master bevel gear via an adjustment shaft is attached to the other end, so that the inclination angle of each blade with respect to the gas flow direction can be adjusted by rotating the rotating shaft. A swirler device for supplying secondary air according to claim 1, characterized in that it is configured to be modified.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16471180A JPS5790517A (en) | 1980-11-25 | 1980-11-25 | Swirler with adjustable blade |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16471180A JPS5790517A (en) | 1980-11-25 | 1980-11-25 | Swirler with adjustable blade |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5790517A JPS5790517A (en) | 1982-06-05 |
| JPS6363813B2 true JPS6363813B2 (en) | 1988-12-08 |
Family
ID=15798426
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16471180A Granted JPS5790517A (en) | 1980-11-25 | 1980-11-25 | Swirler with adjustable blade |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5790517A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1984002033A1 (en) * | 1982-11-10 | 1984-05-24 | Mitsubishi Electric Corp | Switch |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4106890A (en) * | 1977-03-07 | 1978-08-15 | The Babcock & Wilcox Company | Air deflector |
-
1980
- 1980-11-25 JP JP16471180A patent/JPS5790517A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5790517A (en) | 1982-06-05 |
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