JPH0861609A - Marine liquid fuel burner - Google Patents
Marine liquid fuel burnerInfo
- Publication number
- JPH0861609A JPH0861609A JP19410094A JP19410094A JPH0861609A JP H0861609 A JPH0861609 A JP H0861609A JP 19410094 A JP19410094 A JP 19410094A JP 19410094 A JP19410094 A JP 19410094A JP H0861609 A JPH0861609 A JP H0861609A
- Authority
- JP
- Japan
- Prior art keywords
- oil
- air
- fuel
- flame
- combustion
- 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.)
- Withdrawn
Links
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は舶用液体燃料バーナー、
特に窒素酸化物の発生を抑制するバーナーに関するもの
であるが、一般の産業用ボイラ等のバーナーにも適用で
きる。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a marine liquid fuel burner,
In particular, the present invention relates to a burner that suppresses the generation of nitrogen oxides, but it can also be applied to burners for general industrial boilers and the like.
【0002】[0002]
【従来の技術】図3は従来の典型的な舶用ボイラの液体
燃料バーナーの一例を示す縦断側面図である。図中(0
1)は油噴霧器、(02)はこの油噴霧器(01)の先
端部に設けられ、同一径の油噴射孔を有するオイルアト
マイザー、(03)はハウジングチューブ、(05)は
ハウジングチューブ(03)先端部の外面オイルアトマ
イザー(02)近傍に設けられたスワラー、(06)は
ハウジングチューブ(03)の周囲に設けられたバーナ
ースロートである。2. Description of the Related Art FIG. 3 is a vertical sectional side view showing an example of a conventional typical liquid fuel burner for a marine boiler. In the figure (0
1) is an oil atomizer, (02) is an oil atomizer provided at the tip of this oil atomizer (01) and having oil injection holes of the same diameter, (03) is a housing tube, (05) is a housing tube (03) A swirler provided in the vicinity of the outer surface oil atomizer (02) at the tip portion, and (06) is a burner throat provided around the housing tube (03).
【0003】[0003]
【発明が解決しようとする課題】従来のバーナーは、燃
料油と空気との混合が均一に行なわれるため、燃え切り
時間が短く火炎温度も高い。したがって窒素酸化物(以
下NOx と記す)の発生率が非常に高かった。In the conventional burner, the fuel oil and the air are uniformly mixed, so that the burnout time is short and the flame temperature is high. Therefore, the generation rate of nitrogen oxides (hereinafter referred to as NO x ) was extremely high.
【0004】[0004]
【課題を解決するための手段】本発明者は、前記従来の
課題を解決するために、複数の油噴射孔の寸法が大小2
種類あるアトマイザーを先端に装備する油噴霧器と、上
記油噴霧器を間隔をへだてて取囲み、複数の空気取入孔
が明けられた筒状のハウジングチューブと、上記ハウジ
ングチューブの先端部外面に取付けられたスワラーと、
上記ハウジングチューブおよび上記スワラーを間隔をへ
だてて取囲み、内部に二次燃焼空気通路を形成する筒状
のバーナースロートと、上記バーナースロートの外周に
形成され、可変式空気ダンパおよびダンパ開度調節手段
を有する三次燃焼空気通路とを具えたことを特徴とする
舶用液体燃料バーナーを提案するものである。In order to solve the above-mentioned conventional problems, the inventor of the present invention has a plurality of oil injection holes of different sizes.
It is attached to the oil sprayer equipped with atomizers of various types, a cylindrical housing tube that surrounds the above oil sprayer at intervals and has multiple air intake holes, and the outer surface of the end of the housing tube. Swirler,
A cylindrical burner throat which surrounds the housing tube and the swirler with a space therebetween to form a secondary combustion air passage therein, and a variable air damper and damper opening adjusting means formed on the outer periphery of the burner throat. A liquid fuel burner for a marine vessel is proposed, which is provided with a tertiary combustion air passage having a.
【0005】[0005]
【作用】本発明は前記の構成を有し、アトマイザーに設
けられた複数の油噴射孔の寸法が大小2種類あるので、
アトマイザーから噴出する燃料は、その流量に大小の差
が生じ、ハウジングチューブに明けられた空気取入孔を
通って来た空気およびスワラーによって旋回しながら供
給される空気と混合しつつ、空気過剰の火炎域と燃料過
剰の火炎域を形成する。したがってNOx のピーク生成
領域を避けることができ、また火炎温度を低く抑えるこ
とができる。The present invention has the above-mentioned structure, and since the plurality of oil injection holes provided in the atomizer have two sizes, large and small,
The fuel ejected from the atomizer has large and small flow rates, and is mixed with the air coming through the air intake hole opened in the housing tube and the air supplied while being swirled by the swirler, while the excess air is mixed. Form a flame zone and a flame zone with excess fuel. Therefore, the NO x peak generation region can be avoided, and the flame temperature can be kept low.
【0006】更に燃料過剰の火炎域から逸脱した未燃分
は、スワラーとバーナースロートとのすきまを通過して
くる二次燃焼空気およびバーナースロートの外側から供
給される三次燃焼空気と混合しつつ、主火炎下流部に安
定した空気過剰の火炎域を形成する。Further, the unburned portion deviating from the flame region of excess fuel is mixed with the secondary combustion air passing through the clearance between the swirler and the burner throat and the tertiary combustion air supplied from the outside of the burner throat, A stable excess-air flame region is formed downstream of the main flame.
【0007】[0007]
【実施例】図1は本発明の一実施例を示す縦断側面図で
ある。また図2は図1中のオイルアトマイザーを示す詳
細図であって、図2(a)は縦断側面図、図2(b)は
正面図である。DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is a vertical sectional side view showing an embodiment of the present invention. 2 is a detailed view showing the oil atomizer in FIG. 1, FIG. 2 (a) is a vertical side view, and FIG. 2 (b) is a front view.
【0008】図中の符号(1)は油噴霧器であって、こ
の油噴霧器(1)の先端部には、蒸気等の圧力により斜
め前方へ燃料油を噴出する複数の大径の噴出孔(9A)
および小径の噴出孔(9B)を有するオイルアトマイザ
ー(2)を設ける。また油噴霧器(1)の外周には、空
気取り入れ孔(4)を有するハウジングチューブ(3)
を設け、その先端部外面、前記オイルアトマイザー
(2)の近傍に、一次燃焼空気(21)を供給かつ旋回
させるためのスワラー(5)を設ける。前記ハウジング
チューブ(3)およびスワラー(5)の周囲は、二次燃
焼空気(22)の通路を形成するため筒状のバーナース
ロート(6)で覆い、その外周に三次燃焼空気(23)
を供給するための空気通路を設けて、その空気通路内に
可変式空気ダンパ(7)を装備する。Reference numeral (1) in the drawing denotes an oil sprayer, and a plurality of large-diameter jet holes (for jetting fuel oil obliquely forward due to the pressure of steam or the like are provided at the tip of the oil sprayer (1) ( 9A)
And an oil atomizer (2) having a small diameter ejection hole (9B). Moreover, a housing tube (3) having an air intake hole (4) on the outer periphery of the oil sprayer (1).
A swirler (5) for supplying and swirling the primary combustion air (21) is provided near the oil atomizer (2) on the outer surface of the tip end thereof. The housing tube (3) and the swirler (5) are covered with a cylindrical burner throat (6) to form a passage for the secondary combustion air (22), and the tertiary combustion air (23) is provided on the outer periphery thereof.
An air passage for supplying air is provided, and a variable air damper (7) is provided in the air passage.
【0009】このような構成において、燃料油と噴霧用
蒸気は油噴霧器(1)の内部を通って先端部のオイルア
トマイザ−(2)に至り、大小複数の噴出孔(9A),
(9B)から斜め前方に噴出する。このとき、噴出孔
(9A),(9B)の寸法は大小2種類あるので、燃料
流量に大小の差が生じ、ハウジングチューブ(3)内を
通ってくる空気およびスワラー(5)によって旋回しな
がら供給される一次燃焼空気(21)と混合しつつ、空
気過剰の火炎域と燃料過剰の火炎域を形成する。したが
って、NOx のピーク生成領域が避けられ、また火炎温
度も低く抑えられる。In such a structure, the fuel oil and the spraying vapor pass through the inside of the oil sprayer (1) to reach the oil atomizer (2) at the tip end, and a plurality of large and small ejection holes (9A),
(9B) spouts diagonally forward. At this time, since the injection holes (9A) and (9B) have two sizes, large and small, a difference in fuel flow rate occurs, and the swirler (5) is swirled by the air and swirler (5) passing through the housing tube (3). While mixing with the supplied primary combustion air (21), an excess air flame region and an excess fuel flame region are formed. Therefore, the peak generation region of NO x can be avoided, and the flame temperature can be kept low.
【0010】一方、スワラー(5)とバーナースロート
(6)のすきまを通過してくる二次燃焼空気(22)お
よびバーナースロート(6)外側より供給される三次燃
焼空気(23)は、前記燃料過剰火炎域より逸脱した未
燃分と混合しつつ、主火炎下流部に安定した空気過剰の
火炎域を形成する。このとき、火炎の状態と、後部煙道
に設けられたNOx 計およびO2 計によって計測された
排ガス中のNOx ,O 2 濃度とに応じて、可変式空気ダ
ンパ(7)をダンパ開度調節ハンドル(8)で操作し、
三次燃焼空気(23)の供給量を調節する。On the other hand, the swirler (5) and the burner throat
Secondary combustion air (22) passing through the clearance (6)
And tertiary combustion supplied from outside the burner throat (6)
The burnt air (23) has not deviated from the excess fuel flame region.
While mixing with the fuel, a stable excess of air is provided downstream of the main flame.
Form a flame zone. At this time, the state of the flame and the rear flue
NO provided inxTotal and O2Measured by a meter
NO in exhaust gasx, O 2Depending on the concentration and variable air
Operate the damper (7) with the damper opening adjustment handle (8),
The supply amount of the tertiary combustion air (23) is adjusted.
【0011】このように、大小2種類の噴出孔(9
A),(9B)を有するオイルアトマイザー(2)によ
る濃淡燃焼と、3段階に及ぶ燃焼空気供給による多段燃
焼との組み合わせによって、火炎中に局所的な高温部が
形成されず、NOx の生成を抑制することができる。As described above, the large and small types of ejection holes (9
Due to the combination of the rich / lean combustion by the oil atomizer (2) having (A) and (9B) and the multi-stage combustion by the supply of combustion air in three stages, a local high temperature part is not formed in the flame and NO x is generated. Can be suppressed.
【0012】[0012]
【発明の効果】本発明においては、複数の油噴射孔の寸
法が大小2種類あるアトマイザーを用いる濃淡燃焼と、
3段階にわたって燃焼用空気を供給する多段燃焼とを組
み合わせることによって、局所的高温部を形成させず、
燃焼領域全域でNOx の発生を抑えることができる。ま
た、燃料と空気との混合が非常に効率よく行なわれるた
め、O2 濃度が低い状態でも燃焼が可能、油噴霧用蒸気
が少なくてすむ、といった利点もある。更に加えて、多
段燃焼構造をバーナー本体に組み込んでいるので、ボイ
ラ本体を大きく変更することなく実施できる。EFFECTS OF THE INVENTION In the present invention, dark and light combustion using an atomizer having a plurality of oil injection holes of different sizes,
By combining with multi-stage combustion in which combustion air is supplied over three stages, a local high temperature part is not formed,
Generation of NO x can be suppressed in the entire combustion region. Further, since the fuel and the air are mixed very efficiently, there are advantages that combustion can be performed even in a low O 2 concentration and the amount of oil spraying vapor is small. In addition, since the multi-stage combustion structure is incorporated in the burner body, it can be carried out without significantly changing the boiler body.
【図1】図1は本発明の一実施例を示す縦断側面図であ
る。FIG. 1 is a vertical sectional side view showing an embodiment of the present invention.
【図2】図2は図1中のオイルアトマイザーを示す詳細
図であって、図2(a)は縦断側面図、図2(b)は正
面図である。FIG. 2 is a detailed view showing the oil atomizer in FIG. 1, FIG. 2 (a) is a vertical side view, and FIG. 2 (b) is a front view.
【図3】図3は従来の舶用液体燃料バーナーの一例を示
す縦断側面図である。FIG. 3 is a vertical side view showing an example of a conventional marine liquid fuel burner.
(01),(1) 油噴霧器 (01),(2) オイルアトマイザー (03),(3) ハウジングチューブ (4) 空気取り入れ孔 (05),(5) スワラー (06),(6) バーナースロート (7) 可変式空気ダンパ (8) ダンパ開度調節ハンドル (9A),(9B) 油噴射口 (10) 油流路 (11) 蒸気流路 (21) 一次燃焼空気 (22) 二次燃焼空気 (23) 三次燃焼空気 (01), (1) Oil atomizer (01), (2) Oil atomizer (03), (3) Housing tube (4) Air intake hole (05), (5) Swirler (06), (6) Burner throat (7) Variable air damper (8) Damper opening adjustment handle (9A), (9B) Oil injection port (10) Oil flow path (11) Steam flow path (21) Primary combustion air (22) Secondary combustion air (23) Tertiary combustion air
Claims (1)
アトマイザーを先端に装備する油噴霧器と、上記油噴霧
器を間隔をへだてて取囲み、複数の空気取入孔が明けら
れた筒状のハウジングチューブと、上記ハウジングチュ
ーブの先端部外面に取付けられたスワラーと、上記ハウ
ジングチューブおよび上記スワラーを間隔をへだてて取
囲み、内部に二次燃焼空気通路を形成する筒状のバーナ
ースロートと、上記バーナースロートの外周に形成さ
れ、可変式空気ダンパおよびダンパ開度調節手段を有す
る三次燃焼空気通路とを具えたことを特徴とする舶用液
体燃料バーナー。1. An oil sprayer equipped with an atomizer having a plurality of oil injection holes of two sizes, large and small, and a cylindrical shape in which the oil sprayer is surrounded at intervals and a plurality of air intake holes are formed. A housing tube, a swirler attached to the outer surface of the front end of the housing tube, and a cylindrical burner throat that surrounds the housing tube and the swirler with a gap and forms a secondary combustion air passage therein. A liquid fuel burner for marine use, comprising a variable combustion air damper and a tertiary combustion air passage having a damper opening adjusting means formed on the outer periphery of the burner throat.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19410094A JPH0861609A (en) | 1994-08-18 | 1994-08-18 | Marine liquid fuel burner |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19410094A JPH0861609A (en) | 1994-08-18 | 1994-08-18 | Marine liquid fuel burner |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH0861609A true JPH0861609A (en) | 1996-03-08 |
Family
ID=16318951
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP19410094A Withdrawn JPH0861609A (en) | 1994-08-18 | 1994-08-18 | Marine liquid fuel burner |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0861609A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009115388A (en) * | 2007-11-07 | 2009-05-28 | Mitsubishi Heavy Ind Ltd | Burner for liquid fuel and marine boiler |
KR101065594B1 (en) * | 2011-06-13 | 2011-09-19 | 한국기계연구원 | Low nox combustor with air staging |
WO2015136609A1 (en) * | 2014-03-11 | 2015-09-17 | 三菱日立パワーシステムズ株式会社 | Combustion burner for boiler |
CN112484021A (en) * | 2020-10-23 | 2021-03-12 | 西安交通大学 | Ultralow-load stable-combustion pre-pyrolysis combustion system and ultralow-load operation method |
-
1994
- 1994-08-18 JP JP19410094A patent/JPH0861609A/en not_active Withdrawn
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009115388A (en) * | 2007-11-07 | 2009-05-28 | Mitsubishi Heavy Ind Ltd | Burner for liquid fuel and marine boiler |
KR101065594B1 (en) * | 2011-06-13 | 2011-09-19 | 한국기계연구원 | Low nox combustor with air staging |
WO2015136609A1 (en) * | 2014-03-11 | 2015-09-17 | 三菱日立パワーシステムズ株式会社 | Combustion burner for boiler |
KR20160064155A (en) | 2014-03-11 | 2016-06-07 | 미츠비시 히타치 파워 시스템즈 가부시키가이샤 | Combustion burner for boiler |
CN105683656A (en) * | 2014-03-11 | 2016-06-15 | 三菱日立电力系统株式会社 | Combustion burner for boiler |
CN105683656B (en) * | 2014-03-11 | 2018-05-29 | 三菱日立电力系统株式会社 | Boiler burning pulverizing jet |
US10197270B2 (en) | 2014-03-11 | 2019-02-05 | Mitsubishi Hitachi Power Systems, Ltd. | Combustion burner for boiler |
CN112484021A (en) * | 2020-10-23 | 2021-03-12 | 西安交通大学 | Ultralow-load stable-combustion pre-pyrolysis combustion system and ultralow-load operation method |
CN112484021B (en) * | 2020-10-23 | 2021-11-19 | 西安交通大学 | Ultralow-load stable-combustion pre-pyrolysis combustion system and ultralow-load operation method |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
A300 | Withdrawal of application because of no request for examination |
Free format text: JAPANESE INTERMEDIATE CODE: A300 Effective date: 20011106 |