JPH0674421A - Atomizer burner - Google Patents

Atomizer burner

Info

Publication number
JPH0674421A
JPH0674421A JP25392492A JP25392492A JPH0674421A JP H0674421 A JPH0674421 A JP H0674421A JP 25392492 A JP25392492 A JP 25392492A JP 25392492 A JP25392492 A JP 25392492A JP H0674421 A JPH0674421 A JP H0674421A
Authority
JP
Japan
Prior art keywords
fuel spray
swirl vane
spray nozzle
air
combustion chamber
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.)
Pending
Application number
JP25392492A
Other languages
Japanese (ja)
Inventor
Noboru Tanaka
昇 田中
Tetsuya Azuma
哲也 東
Masaru Hiroyasu
勝 廣安
Akinobu Koufu
昭宣 河府
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.)
Noritz Corp
Original Assignee
Noritz Corp
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 Noritz Corp filed Critical Noritz Corp
Priority to JP25392492A priority Critical patent/JPH0674421A/en
Publication of JPH0674421A publication Critical patent/JPH0674421A/en
Pending legal-status Critical Current

Links

Landscapes

  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

PURPOSE:To make it hard for backfire to occur in the case of low load combustion and enable enhancing a revolving force of a swirl vane with the result that a good combustion performance resulted from a good flame holding capacity is provided. CONSTITUTION:An atomizer burner is constructed such that fuel sprayed and supplied from a fuel spray nozzle is introduced into a combustion cylinder 5 through a central hole 3a of a forwardly positioned swirl vane 3 for supply of air, and at least a part of air supplied is divided by a primary air partition cylinder 7 into a primary air which is to be introduced into a combustion chamber 5 through the central hole 3a of the swirl vane 3 from around the fuel spray nozzle 1 and a secondary air which is to be introduced into the combustion chamber 5 through a vane portion 3b of the swirl vane 3 and secondary air blowout holes 10 provided around the vane portion 3b. About the central hole 3a of the swirl vane 3 is provided a backfire screening ring 20 which converges toward the fuel spray nozzle located inside.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は燃料を燃焼室内に噴霧供
給して燃焼を行う燃料噴霧式のバーナに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fuel spray type burner which sprays fuel into a combustion chamber for combustion.

【0002】[0002]

【従来の技術】図3に従来のこの種、燃料噴霧式バーナ
の断面構成図を示す。1はオイル燃料の燃料噴霧ノズル
で、該ノズル1の直前位置に噴霧カット板2を配置し、
ノズル1から一定の拡がり角度で噴霧された燃料が噴霧
カット板2で一部カットされ、所定の噴霧供給量になっ
て、更に前方に配置された旋回羽根3の中心穴3aを通っ
て、燃焼室5に導入される。4は点火器である。旋回羽
根3は燃焼室5を燃料噴霧ノズル側から仕切るコーン状
仕切り壁6に取り付けられている。このコーン状仕切り
壁6で仕切られた燃料噴霧ノズル側には、前記燃料噴霧
ノズル1の周囲に1次空気仕切り筒7が配置され、その
先端が前記旋回羽根3の中心穴3aの縁に、また後端が固
定壁8に到達している。矢符Aに沿って供給されてきた
空気はその一部が前記1次空気仕切り筒7に設けられた
分配穴9から1次空気仕切り筒7内に入り、一次空気と
して、燃料噴霧ノズル1の周囲から前記旋回羽根3の中
心穴3aを通って燃焼室5に導入される。また矢符Aに沿
って供給されてきた空気の残りは、2次空気として、前
記旋回羽根3の羽根部3b及びコーン状仕切り壁6の2次
空気吹き出し孔10を通って燃焼室5に導入される。燃焼
筒11の外周は3次空気室12にされており、矢符Bに沿っ
て供給された3次空気が3次空気吹き出し口13から燃焼
室5内に導入される。
2. Description of the Related Art FIG. 3 shows a sectional view of a conventional fuel spray burner of this type. Reference numeral 1 is a fuel spray nozzle for oil fuel, and a spray cut plate 2 is arranged immediately in front of the nozzle 1.
The fuel sprayed from the nozzle 1 at a constant spread angle is partially cut by the spray cut plate 2, reaches a predetermined spray supply amount, passes through the central hole 3a of the swirl vane 3 arranged further forward, and burns. Introduced into chamber 5. Reference numeral 4 is an igniter. The swirl vane 3 is attached to a cone-shaped partition wall 6 that partitions the combustion chamber 5 from the fuel spray nozzle side. On the side of the fuel spray nozzle partitioned by the cone-shaped partition wall 6, a primary air partition cylinder 7 is arranged around the fuel spray nozzle 1, the tip of which is at the edge of the center hole 3a of the swirl vane 3. Further, the rear end reaches the fixed wall 8. A part of the air supplied along the arrow A enters the primary air partition tube 7 through the distribution holes 9 provided in the primary air partition tube 7, and is supplied as primary air to the fuel spray nozzle 1 from the fuel spray nozzle 1. It is introduced into the combustion chamber 5 from the surroundings through the central hole 3a of the swirl vane 3. The rest of the air supplied along arrow A is introduced into the combustion chamber 5 as secondary air through the blade portion 3b of the swirl blade 3 and the secondary air blowing hole 10 of the cone-shaped partition wall 6. To be done. The outer periphery of the combustion cylinder 11 is a tertiary air chamber 12, and the tertiary air supplied along the arrow B is introduced into the combustion chamber 5 from the tertiary air outlet 13.

【0003】[0003]

【発明が解決しようとする課題】上記従来の燃料噴霧式
バーナにおいて、低負荷での燃焼を良好に行わせるため
には、旋回羽根3の羽根部3b及び2次空気吹き出し孔10
からの吹き出し圧を上げ、燃料噴霧ノズル1の周囲から
前記旋回羽根3の中心穴3aを通って燃焼室5に導入され
る1次空気の量を減らすのが良いのであるが、中心穴3a
を通って燃焼室5に導入される1次空気の量を減らす
と、燃焼室5内の火炎が旋回羽根3の中心穴3aからノズ
ル1側に逆火し易くなる問題があった。これに対しては
前記旋回羽根3の中心穴3aの径を小さくすればよいので
あるが、該中心穴3aは供給されてくる噴霧燃料の通過を
確保することから縮径には限度があった。この為、中心
穴3aを通る一次空気量を極端に減らすことが出来ず、そ
の結果、旋回羽根3の旋回力を上げることが出来ず、火
炎の保炎力及び燃焼性能の向上を図れなかった。
In the above conventional fuel spray type burner, in order to favorably perform combustion under a low load, the vane portion 3b of the swirl vane 3 and the secondary air blowing hole 10 are provided.
The amount of primary air introduced into the combustion chamber 5 from the periphery of the fuel spray nozzle 1 through the center hole 3a of the swirl vane 3 is preferably reduced by increasing the blowout pressure from the center hole 3a.
If the amount of primary air introduced into the combustion chamber 5 through the same is reduced, there is a problem that the flame in the combustion chamber 5 tends to flash back from the central hole 3a of the swirl vane 3 to the nozzle 1 side. For this purpose, the diameter of the central hole 3a of the swirl vane 3 may be reduced, but the central hole 3a has a limit to the diameter reduction because it secures the passage of the supplied spray fuel. . Therefore, the amount of primary air passing through the central hole 3a cannot be extremely reduced, and as a result, the swirl force of the swirl vane 3 cannot be increased, and the flame holding power and combustion performance cannot be improved. .

【0004】そこで、本発明は上記従来技術の欠点を解
消し、低負荷燃焼を行う場合においても、逆火が生じ難
く、しかも旋回羽根の旋回力を向上させることができ、
結果として良好な保炎力による良好な燃焼性能を有する
燃料噴霧式バーナの提供を目的とする。
Therefore, the present invention solves the above-mentioned drawbacks of the prior art, makes it difficult for flashback to occur even when performing low-load combustion, and can improve the turning force of the turning blades.
As a result, an object of the present invention is to provide a fuel spray burner having good combustion performance with good flame holding power.

【0005】[0005]

【課題を解決するための手段】上記目的を達成するた
め、本発明の燃料噴霧式バーナは、燃料噴霧ノズル側か
ら噴霧供給されてくる燃料を前方に配置された空気供給
用の旋回羽根の中心穴を通して燃焼室に導入すると共
に、供給されてきた空気の少なくとも一部を1次空気仕
切り筒によって、前記燃料噴霧ノズルの周囲から前記旋
回羽根の中心穴を通って燃焼室に導入される1次空気と
前記旋回羽根の羽根部及びその周囲に設けられる2次空
気吹き出し孔を通って燃焼室に導入される2次空気とに
分配するようにした燃料噴霧式バーナであって、前記旋
回羽根の中心穴に、内側の燃料噴霧ノズル側に向けて先
窄まりとされた逆火遮蔽リングを設けたことを特徴とし
ている。
In order to achieve the above object, the fuel spray burner of the present invention has a center of a swirl vane for supplying the fuel spray-supplied from the fuel spray nozzle side to the front. The air is introduced into the combustion chamber through the holes, and at least a part of the supplied air is introduced into the combustion chamber from the periphery of the fuel spray nozzle through the center hole of the swirl vane by the primary air partition tube. What is claimed is: 1. A fuel spray burner for distributing air and secondary air introduced into a combustion chamber through a secondary air blowing hole provided in the swirl vane and its surroundings, It is characterized in that the central hole is provided with a flashback shield ring which is tapered toward the inner side of the fuel spray nozzle.

【0006】[0006]

【作用】上記特徴によれば、旋回羽根の中心穴に、内側
の燃料噴霧ノズル側に向けて先窄まりとされた逆火遮蔽
リングを設けたので、噴霧燃料の通過を妨げることな
く、しかも燃料噴霧ノズル側と燃焼室側とが連通する穴
を小さくすることができ、逆火を発生し難くすることが
できる。即ち、燃料噴霧の断面積は燃料噴霧ノズル側に
近づくにつれて小さくなるので、燃料噴霧ノズル側に向
けて先窄まりとされた逆火遮蔽リングを旋回羽根の中心
穴に設けることで、燃料噴霧を妨げることなく燃料噴霧
ノズル側と燃焼室側との連通する穴を小さくすることが
できる。よって、1次空気を絞って旋回羽根の羽根部を
通る2次空気の分配率を増やすことができ、保炎性がよ
く逆火の生じない低負荷燃焼性能の良い燃料噴霧式バー
ナが提供できる。
According to the above feature, since the flashback shield ring, which is tapered toward the inner side of the fuel spray nozzle, is provided in the center hole of the swirl vane, it does not hinder the passage of the sprayed fuel. The hole through which the fuel spray nozzle side and the combustion chamber side communicate with each other can be made small, and flashback can be made difficult to occur. That is, since the cross-sectional area of the fuel spray becomes smaller as it approaches the fuel spray nozzle side, by providing a flashback shield ring that is tapered toward the fuel spray nozzle side in the center hole of the swirl vane, It is possible to make the hole communicating between the fuel spray nozzle side and the combustion chamber side small without hindering. Therefore, the primary air can be throttled to increase the distribution ratio of the secondary air passing through the blade portion of the swirl blade, and a fuel spray burner having good flame holding property and low back load combustion performance without backfire can be provided. .

【0007】[0007]

【実施例】図1は本発明の実施例を示す燃料噴霧式バー
ナの断面構成図、図2は要部の断面構成図である。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is a sectional view of a fuel spray burner showing an embodiment of the present invention, and FIG.

【0008】燃料噴霧ノズル1、噴霧カット板2、旋回
羽根3、燃焼室5、1次空気仕切り筒7、固定壁8等の
構成は既述した従来例と同様であるので、同様の機能を
果たす部材、要素には同じ番号を付して説明を省略す
る。
The structure of the fuel spray nozzle 1, the spray cut plate 2, the swirl vane 3, the combustion chamber 5, the primary air partition cylinder 7, the fixed wall 8 and the like is the same as that of the conventional example described above, and therefore has the same function. The same members and elements are given the same numbers, and the description thereof will be omitted.

【0009】本発明では、前記旋回羽根3の中心穴3a
に、内側の燃料噴霧ノズル側に向けて先窄まりとされた
逆火遮蔽リング20を設けている。この逆火遮蔽リング20
は、実施例では旋回羽根3の中心穴3aの縁に当接する前
記1次空気仕切り筒7の先端部を更に内側に折り曲げる
形で延設して一体に構成している。そしてこの逆火遮蔽
リング20の先窄まり角度は、旋回羽根3の中心穴3aを通
過する燃料噴霧の拡がり角度と同程度にすることで、燃
料噴霧の妨げとならずに、しかも開口を効率よく小さく
することができる。逆火遮蔽リング20の先端は前記噴霧
カット板2の周縁近くまで延ばし、1次空気の通る隙間
を比較的狭くしている。また逆火遮蔽リング20の一部は
前記点火器4による火花の妨げにならないように切り欠
いている。
In the present invention, the central hole 3a of the swirl vane 3
Further, a flashback shield ring 20 is provided which is tapered toward the inner side of the fuel spray nozzle. This flashback shield ring 20
In the embodiment, the tip portion of the primary air partition cylinder 7 that abuts on the edge of the center hole 3a of the swirl vane 3 is extended and bent inward to be integrally formed. The converging angle of the flashback shield ring 20 is set to be approximately the same as the spread angle of the fuel spray passing through the center hole 3a of the swirl vane 3, so that the fuel spray is not hindered and the opening efficiency is improved. It can be made small. The tip of the flashback shield ring 20 extends close to the periphery of the spray cut plate 2 to make the gap through which the primary air passes relatively narrow. Further, a part of the flashback shield ring 20 is cut out so as not to interfere with the spark generated by the igniter 4.

【0010】前記逆火遮蔽リング20は旋回羽根3の中心
穴3aの縁に対して固着して一体に設けるようにしてもよ
し、前記コーン状仕切り壁6の中心穴の縁に一体に設け
てもよい。
The flashback shield ring 20 may be fixed to the edge of the central hole 3a of the swirl vane 3 so as to be provided integrally therewith, or it may be provided integrally with the edge of the central hole of the cone-shaped partition wall 6. Good.

【0011】[0011]

【発明の効果】本発明は以上の構成、作用よりなり、請
求項1に記載の燃料噴霧式バーナによれば、旋回羽根の
中心穴に、内側の燃料噴霧ノズル側に向けて先窄まりと
された逆火遮蔽リングを設けたので、燃料噴霧を妨げる
ことなく、燃焼室側からの逆火を抑制することができ
る。よってまた燃料噴霧ノズルの周囲から前記旋回羽根
の中心穴を通って燃焼室に導入される1次空気の分配量
を減らして2次空気の分配量を増やすことができるの
で、旋回羽根の羽根部を通る空気量を増やして燃焼の保
炎力を増大し、低負荷燃焼を安定して行わせることがで
きる。更に、逆火遮蔽リングを設けることで、該リング
と燃料噴霧ノズル側との間隙がそれだけ狭くなり、旋回
羽根の中心穴を通る1次空気の流速が速くなって、これ
によっても逆火を防止効果を向上させることができる。
また前記1次空気の流速が速くなることで、逆火遮蔽リ
ングの存在によるも、噴霧が逆火遮蔽リングに付着する
ことが抑制される。
According to the fuel spray burner of the present invention, the central hole of the swirl vane is tapered toward the inner side of the fuel spray nozzle. Since the flashback shield ring is provided, the flashback from the combustion chamber side can be suppressed without hindering the fuel spray. Therefore, the distribution amount of the primary air introduced into the combustion chamber from the periphery of the fuel spray nozzle through the central hole of the swirl vane can be reduced to increase the distribution amount of the secondary air. It is possible to increase the amount of air passing through and increase the flame holding power of combustion, and to stably perform low load combustion. Further, by providing the flashback shield ring, the gap between the ring and the fuel spray nozzle side becomes narrower by that amount, and the flow velocity of the primary air passing through the central hole of the swirl vane becomes faster, which also prevents flashback. The effect can be improved.
In addition, since the flow velocity of the primary air is increased, the spray is suppressed from adhering to the flashback shield ring due to the presence of the flashback shield ring.

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

【図1】本発明の実施例を示す燃料噴霧式バーナの断面
構成図である。
FIG. 1 is a cross-sectional configuration diagram of a fuel spray type burner showing an embodiment of the present invention.

【図2】要部の断面構成図である。FIG. 2 is a cross-sectional configuration diagram of a main part.

【図3】従来の燃料噴霧式バーナの断面構成図である。FIG. 3 is a cross-sectional configuration diagram of a conventional fuel spray burner.

【符号の説明】[Explanation of symbols]

1 燃料噴霧ノズル 2 噴霧カット板 3 旋回羽根 3a 中心穴 3b 羽根部 5 燃焼室 7 1次空気仕切り筒 10 2次空気吹き出し孔 20 逆火遮蔽リング 1 Fuel Spray Nozzle 2 Spray Cut Plate 3 Swirling Blade 3a Center Hole 3b Blade 5 Combustion Chamber 7 Primary Air Partition Tube 10 Secondary Air Blowing Hole 20 Flashback Shield Ring

───────────────────────────────────────────────────── フロントページの続き (72)発明者 河府 昭宣 兵庫県神戸市中央区明石町32番地 株式会 社ノーリツ内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Akinobu Kawafu 32 No. Akashi-cho, Chuo-ku, Kobe-shi, Hyogo In stock company Noritsu

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 燃料噴霧ノズル側から噴霧供給されてく
る燃料を前方に配置された空気供給用の旋回羽根の中心
穴を通して燃焼室に導入すると共に、供給されてきた空
気の少なくとも一部を1次空気仕切り筒によって、前記
燃料噴霧ノズルの周囲から前記旋回羽根の中心穴を通っ
て燃焼室に導入される1次空気と前記旋回羽根の羽根部
及びその周囲に設けられる2次空気吹き出し孔を通って
燃焼室に導入される2次空気とに分配するようにした燃
料噴霧式バーナであって、前記旋回羽根の中心穴に、内
側の燃料噴霧ノズル側に向けて先窄まりとされた逆火遮
蔽リングを設けたことを特徴とする燃料噴霧式バーナ。
1. A fuel spray-supplied from a fuel spray nozzle side is introduced into a combustion chamber through a center hole of a swirl vane for air supply arranged in the front, and at least a part of the supplied air is 1 The primary air introduced into the combustion chamber from the periphery of the fuel spray nozzle through the central hole of the swirl vane and the vane portion of the swirl vane and the secondary air blowout holes provided in the periphery thereof are provided by the secondary air partition tube. A fuel spray burner adapted to be distributed to the secondary air that is introduced into the combustion chamber through a reverse hole that is tapered in the center hole of the swirl vane toward the inner fuel spray nozzle side. A fuel spray burner characterized by having a fire shield ring.
JP25392492A 1992-08-27 1992-08-27 Atomizer burner Pending JPH0674421A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25392492A JPH0674421A (en) 1992-08-27 1992-08-27 Atomizer burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25392492A JPH0674421A (en) 1992-08-27 1992-08-27 Atomizer burner

Publications (1)

Publication Number Publication Date
JPH0674421A true JPH0674421A (en) 1994-03-15

Family

ID=17257922

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25392492A Pending JPH0674421A (en) 1992-08-27 1992-08-27 Atomizer burner

Country Status (1)

Country Link
JP (1) JPH0674421A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014214919A (en) * 2013-04-24 2014-11-17 日野自動車株式会社 Burner
CN107228362A (en) * 2017-06-10 2017-10-03 北京航空航天大学 A kind of oil-poor direct-injection low pollution combustor of multiple spot with precombustion chamber

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014214919A (en) * 2013-04-24 2014-11-17 日野自動車株式会社 Burner
CN107228362A (en) * 2017-06-10 2017-10-03 北京航空航天大学 A kind of oil-poor direct-injection low pollution combustor of multiple spot with precombustion chamber
CN107228362B (en) * 2017-06-10 2019-05-21 北京航空航天大学 A kind of oil-poor direct-injection low pollution combustor of multiple spot with precombustion chamber

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