JPH06313513A - Gun type burner - Google Patents

Gun type burner

Info

Publication number
JPH06313513A
JPH06313513A JP12492193A JP12492193A JPH06313513A JP H06313513 A JPH06313513 A JP H06313513A JP 12492193 A JP12492193 A JP 12492193A JP 12492193 A JP12492193 A JP 12492193A JP H06313513 A JPH06313513 A JP H06313513A
Authority
JP
Japan
Prior art keywords
combustion cylinder
introduction hole
swirling
air flow
flame stabilizer
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
JP12492193A
Other languages
Japanese (ja)
Other versions
JP3146760B2 (en
Inventor
Masaru Hiroyasu
勝 廣安
Noboru Tanaka
昇 田中
Norihiro Hori
紀弘 堀
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 JP12492193A priority Critical patent/JP3146760B2/en
Publication of JPH06313513A publication Critical patent/JPH06313513A/en
Application granted granted Critical
Publication of JP3146760B2 publication Critical patent/JP3146760B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Landscapes

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

Abstract

PURPOSE:To provide a gun type burner whose flame stabilizing property is good and which can realize a stable combustion even during a small capacity operation without disturbing a smooth gasstream in a combustion cylinder. CONSTITUTION:In gun type burner, a base end of a combustion cylinder 10 is formed of a flame stabilizer 20 which is provided with an introduction hole 21 of liquid spray fuel in a central part and a swirling vane part 22 around the introduction hole 21, so that the liquid spray fuel from a spraying nozzle 30 is introduced into the combustion cylinder 10 through the introduction hole 21. On the other hand, air sent from a fan 70 is divided into at least two airstreams. A first airstream is introduced into the combustion cylinder 10 together with the liquid spray fuel through the introduction hole 21 and a second airstream is introduced into the combustion cylinder 10 while it is swirled through the swirling vane part 22. At this time, the airstream introduced into the combustion cylinder 10 through the introduction hole 21 is formed in a swirling airstream which swirls in the same direction as the swirling air-stream which is introduced into the combustion cylinder 10 through the swirling vane part 22.

Description

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

【0001】[0001]

【産業上の利用分野】本発明は噴霧ノズルによって液体
燃料を燃焼筒内に噴霧供給して、燃焼筒内で燃焼を行う
ガンタイプバーナに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a gun type burner for spraying liquid fuel into a combustion cylinder by a spray nozzle to burn the liquid fuel in the combustion cylinder.

【0002】[0002]

【従来の技術】図4に従来のガンタイプバーナの断面構
成図を示し、図5に図4に示すガンタイプバーナを燃焼
筒の正面からみた図を示す。燃焼筒10の基端面が保炎器
20で構成されており、該保炎器20は中心部に液体噴霧燃
料の導入穴21を設けると共にその周囲に旋回羽根部22を
設けている。保炎器20の手前側には噴霧ノズル30がその
噴出方向を燃焼筒10の中心軸にあわせた形で保炎器20の
導入穴21の手前に設けられている。前記噴霧ノズル30の
外周空間は第1の仕切り筒40によって仕切られており、
該第1の仕切り筒40の空気流入穴41から仕切り筒40内に
入った第1の空気流は前記保炎器20の導入穴21から噴霧
燃料と共に燃焼筒10内に導入されるようにされている。
また前記第1の仕切り筒40の外側に第2の仕切り筒50が
設けられており、該第2の仕切り筒50の空気流入穴51か
ら仕切り筒50内に入った空気流は前記第1の仕切り筒40
内に更に流入するものを除き、第2の空気流として前記
保炎器20の旋回羽根部22を通って旋回空気流Aとなって
燃焼筒10内に導入される。さらに第2の仕切り筒50の外
側に送風器70から送られてくる空気を受け入れるケース
60が設けられ、該ケース60内に入った空気の一部は第3
の空気流として、前記燃焼筒10の壁面の穴11から燃焼筒
10内に流入されるようになされている。80は点火器であ
る。
2. Description of the Related Art FIG. 4 shows a sectional view of a conventional gun type burner, and FIG. 5 shows the gun type burner shown in FIG. The flame end is the base end face of the combustion tube 10.
The flame stabilizer 20 is provided with a liquid spray fuel introduction hole 21 in the center and a swirl vane portion 22 around the hole 21. On the front side of the flame stabilizer 20, a spray nozzle 30 is provided in front of the introduction hole 21 of the flame stabilizer 20 in such a manner that the ejection direction thereof is aligned with the central axis of the combustion tube 10. The outer peripheral space of the spray nozzle 30 is partitioned by a first partition cylinder 40,
The first air flow entering the partition tube 40 from the air inflow hole 41 of the first partition tube 40 is introduced into the combustion tube 10 together with the atomized fuel from the introduction hole 21 of the flame stabilizer 20. ing.
A second partition cylinder 50 is provided outside the first partition cylinder 40, and the air flow entering the partition cylinder 50 from the air inflow hole 51 of the second partition cylinder 50 is the first partition cylinder 50. Partition tube 40
Except for the one that further flows into the combustion cylinder 10, a second air flow passes through the swirl vane portion 22 of the flame stabilizer 20 to become a swirl air flow A and is introduced into the combustion cylinder 10. Further, a case for receiving the air sent from the blower 70 to the outside of the second partition tube 50.
60 is provided, and a part of the air entering the case 60 is the third
As the air flow of the combustion cylinder from the hole 11 in the wall surface of the combustion cylinder 10.
It is designed to be flown into within 10. 80 is an igniter.

【0003】[0003]

【発明が解決しようとする課題】ところが上記従来のガ
ンタイプバーナにおいては、旋回羽根部22を通って燃焼
筒10内に旋回空気流Aとして流入し、さらに燃焼筒10内
で再循環流Bとなって燃焼筒10の中心付近を戻ってくる
空気流と、前記保炎器20の中心部の導入穴21を通って流
入される空気流Cとが対向するため、これによって前記
再循環流Bの流れが阻害され、燃焼筒10内での保炎性が
悪くなり、特に小能力運転における燃焼が安定して行え
なくなるという欠点があった。
However, in the above-mentioned conventional gun type burner, the swirl vane portion 22 is introduced into the combustion cylinder 10 as the swirling air flow A, and the recirculation flow B is further generated in the combustion cylinder 10. As a result, the air flow returning near the center of the combustion tube 10 and the air flow C flowing in through the introduction hole 21 at the center of the flame stabilizer 20 face each other, whereby the recirculation flow B However, there is a drawback in that the flame holding property in the combustion cylinder 10 is deteriorated and the combustion cannot be stably performed especially in a small capacity operation.

【0004】そこで本発明は、上記従来の欠点を解消
し、燃焼筒内での円滑なガスの流れを阻害することな
く、よって保炎性がよく、小能力運転においても安定し
た燃焼を行うことができるガンタイプバーナの提供を目
的とする。
In view of the above, the present invention solves the above-mentioned drawbacks of the prior art, does not impede the smooth flow of gas in the combustion cylinder, and therefore has good flame holding properties and stable combustion even in small capacity operation. The purpose is to provide a gun type burner that can

【0005】[0005]

【課題を解決するための手段】上記目的を達成する本発
明のガンタイプバーナは、中心部に液体噴霧燃料の導入
穴を設けると共にその周囲に旋回羽根部を設けた保炎器
で燃焼筒の基端面を構成し、噴霧ノズルからの液体噴霧
燃料を前記保炎器中心部の導入穴から燃焼筒内に導入す
ると共に、送風器から送られてくる空気を少なくとも2
つの空気流に分けて、その第1の空気流を前記保炎器中
心部の導入穴から液体噴霧燃料と一緒に燃焼筒内に導入
し、第2の空気流を前記保炎器の旋回羽根部を通して旋
回させながら燃焼筒内に導入するようにし、燃焼筒内で
燃焼させるようにしたガンタイプバーナであって、前記
保炎器中心部の導入穴から液体噴霧燃料と一緒に燃焼筒
内に導入される空気流を、保炎器の旋回羽根部を通して
燃焼筒内に導入される旋回空気流と同じ方向に旋回する
旋回空気流としたことを特徴としている。
The gun-type burner of the present invention which achieves the above-mentioned object is a flame stabilizer which has an inlet for introducing liquid atomized fuel in the center and a swirl vane around the inlet. A liquid atomized fuel from the atomizing nozzle is introduced into the combustion cylinder through the introduction hole in the central part of the flame stabilizer, and at least 2 air blown from the blower is formed.
The air stream is divided into two air streams, and the first air stream is introduced into the combustion cylinder together with the liquid atomized fuel through the introduction hole in the central portion of the flame stabilizer, and the second air stream is swirl vanes of the flame stabilizer. It is a gun type burner that is introduced into the combustion cylinder while swirling through the portion, and is burned in the combustion cylinder, and is introduced into the combustion cylinder together with the liquid atomized fuel from the introduction hole of the flame stabilizer center portion. It is characterized in that the introduced air flow is a swirling air flow swirling in the same direction as the swirling air flow introduced into the combustion cylinder through the swirl vane portion of the flame stabilizer.

【0006】[0006]

【作用】保炎器中心部の導入穴から液体噴霧燃料と一緒
に燃焼筒内に導入される空気流を、保炎器の旋回羽根部
を通して燃焼筒内に導入される旋回空気流と同じ方向に
旋回する旋回空気流とすることで、導入穴から流入する
空気流と旋回羽根部から流入する旋回空気流とが全体で
1つの流れからなる旋回空気流となり、空気同士の正面
衝突的な錯乱がなくなり、小能力運転においても保炎性
のよい安定した燃焼が確保される。
The air flow introduced into the combustion cylinder together with the liquid atomized fuel through the introduction hole in the central portion of the flame stabilizer is in the same direction as the swirling air flow introduced into the combustion cylinder through the swirl vane portion of the flame stabilizer. By making the swirling air flow swirl into the swirling air flow, the swirling air flow that flows in from the introduction hole and the swirling air flow that flows in from the swirling vane part become a swirling air flow that is a single flow as a whole, and the air is a frontal collision-like confusion. As a result, stable combustion with good flame retention is secured even in small capacity operation.

【0007】[0007]

【実施例】図1は本発明の実施例を示すガンタイプバー
ナの縦断面構成図、図2は第1の仕切り筒の要部の横断
面図、図3は図2を上からみた図である。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is a vertical cross sectional view of a gun type burner showing an embodiment of the present invention, FIG. 2 is a cross sectional view of an essential part of a first partition cylinder, and FIG. 3 is a view of FIG. 2 from above. is there.

【0008】燃焼筒10の基端面が保炎器20で構成され、
該保炎器20は中心部に液体噴霧燃料の導入穴21が設けら
れ、周囲に旋回羽根部22が設けられている点、保炎器20
の手前側には噴霧ノズル30がその噴出方向を燃焼筒10の
中心軸にあわせた形で保炎器20の導入穴21の手前に設け
られ、噴霧ノズル30の外周空間は第1の仕切り筒40によ
って仕切られ、該第1の仕切り筒40の空気流入穴43から
仕切り筒40内に入った第1の空気流は前記保炎器20の導
入穴21から噴霧燃料と共に燃焼筒10内に導入される点、
また前記第1の仕切り筒40の外側に第2の仕切り筒50が
設けられており、該第2の仕切り筒50の空気流入穴51か
ら仕切り筒50内に入った空気流は前記第1の仕切り筒40
内に更に流入するものを除き、第2の空気流として前記
保炎器20の旋回羽根部22を通って旋回空気流Aとなって
燃焼筒10内に導入される点、第2の仕切り筒50の外側に
送風器70から送られてくる空気を受け入れるケース60が
設けられ、該ケース60内に入った空気の一部は第3の空
気流として、前記燃焼筒10の壁面の穴11から燃焼筒10内
に流入されるようになされている点等については既述し
た構成と同じである。
The base end surface of the combustion cylinder 10 is composed of a flame stabilizer 20,
The flame stabilizer 20 is provided with a liquid spray fuel introduction hole 21 at the center and a swirl vane portion 22 at the periphery.
In front of the spray nozzle 30, a spray nozzle 30 is provided in front of the introduction hole 21 of the flame stabilizer 20 with its jet direction aligned with the central axis of the combustion cylinder 10, and the outer peripheral space of the spray nozzle 30 is the first partition cylinder. The first air flow that is partitioned by 40 and enters the partition tube 40 from the air inflow hole 43 of the first partition tube 40 is introduced into the combustion tube 10 through the introduction hole 21 of the flame stabilizer 20 together with the atomized fuel. Point to be
A second partition cylinder 50 is provided outside the first partition cylinder 40, and the air flow entering the partition cylinder 50 from the air inflow hole 51 of the second partition cylinder 50 is the first partition cylinder 50. Partition tube 40
The second partition cylinder except the one that further flows into the combustion chamber 10 as a second air flow through the swirl vane portion 22 of the flame stabilizer 20 to become the swirling air flow A. A case 60 for receiving the air sent from the blower 70 is provided outside the air blower 50, and a part of the air that has entered the case 60 is a third air flow from the hole 11 on the wall surface of the combustion tube 10. The configuration in which the gas is introduced into the combustion cylinder 10 is the same as the configuration described above.

【0009】本実施例においては、前記第1の仕切り筒
40の長手方向の1箇所に一定の幅を有するリング体90を
外嵌するように取り付け、このリング体90に円周方向に
複数個の空気流入穴91を設け、且つ前記第1の仕切り筒
40の前記空気流入穴91が重なる部分に、前記保炎器20の
旋回羽根部22と同じ切り起こし方向にして、円周方向へ
空気を導くための切り起こし片42と、該片42によって開
けられた空気流入穴43を設けている。前記切り起こし片
42によって、第1の仕切り筒40内に入る空気流が、前記
保炎器20の旋回羽根部22を通って燃焼筒10内に流入する
旋回空気流Aと同じ方向に旋回する旋回空気流Dとな
る。また前記リング体90の空気流入穴91によって第1の
仕切り筒40内に流入する空気量を調節している。このよ
うにして第1の仕切り筒40内に入った空気流は旋回流か
らなる第1の空気流として、前記保炎器20の導入穴21か
ら旋回空気流Dとして燃焼筒10内に流入する。勿論、第
2の仕切り筒50内を流れる第2の空気流は保炎器20の旋
回羽根部22を通って旋回空気流Aとなり、前記導入穴21
からの旋回空気流Dと1つの流れになって、燃焼筒10内
を流れ、再循環流Bとなる。この再循環流Bと前記旋回
空気流Dとは正面衝突することなく、互いに互いの流れ
を阻害することがなくなる。よって再循環流Bが安定
し、燃焼筒内での保炎状態が良くなって、小能力運転に
至るまで良好な燃焼を行うことが可能となる。
In this embodiment, the first partition cylinder
A ring body 90 having a constant width is attached to one location in the longitudinal direction of 40 so as to be fitted onto the ring body 90, and a plurality of air inflow holes 91 are provided in the ring body 90 in the circumferential direction, and the first partition cylinder is provided.
In a portion where 40 of the air inflow hole 91 overlaps, a cut-and-raised piece 42 for guiding air in the circumferential direction in the same cut-and-raised direction as the swirl vane portion 22 of the flame stabilizer 20, and the cut-and-raised piece 42 is opened. The air inlet hole 43 is provided. The cut and raised piece
By 42, the air flow entering the first partition cylinder 40 swirls in the same direction as the swirling air flow A flowing into the combustion cylinder 10 through the swirl vane portion 22 of the flame stabilizer 20. Becomes Further, the amount of air flowing into the first partition cylinder 40 is adjusted by the air inlet hole 91 of the ring body 90. The air flow thus entering the first partition tube 40 flows into the combustion tube 10 as the swirling air flow D as the first air flow consisting of the swirling flow from the introduction hole 21 of the flame stabilizer 20. . Of course, the second air flow flowing in the second partition cylinder 50 becomes the swirling air flow A through the swirl vane portion 22 of the flame stabilizer 20, and the introduction hole 21
And the swirling air flow D from the above, and flows into the combustion cylinder 10 to become a recirculation flow B. The recirculation flow B and the swirling air flow D do not directly collide with each other and do not interfere with each other. Therefore, the recirculation flow B is stabilized, the flame holding state in the combustion cylinder is improved, and good combustion can be performed up to low capacity operation.

【0010】[0010]

【発明の効果】本発明は以上の構成、作用よりなり、請
求項1に記載のガンタイプバーナによれば、保炎器の中
心部の導入穴から液体噴霧燃料と一緒に燃焼筒内に導入
される空気流を、保炎器の旋回羽根部を通して燃焼筒内
に導入される旋回空気流と同じ方向に旋回する旋回空気
流としたので、導入穴から流入する空気流と旋回羽根部
から流入する旋回空気流とを全体で1つの流れからなる
旋回空気流とすることができ、また再循環流と導入穴か
ら流入する空気流との正面衝突的な空気流の相互の阻害
をなくすことができる。よって、再循環流が安定した、
保炎性の良い、小能力運転に至るまで良好な燃焼を行う
ことが可能となる。
According to the gun type burner according to the first aspect of the present invention, the present invention is introduced into the combustion cylinder together with the liquid atomized fuel from the introduction hole in the center of the flame stabilizer. Since the generated air flow is a swirling air flow that swirls in the same direction as the swirling air flow introduced into the combustion cylinder through the swirling blade part of the flame stabilizer, the air flow that flows in from the introduction hole and the swirling blade part that flows in The swirling air flow that forms a swirling air flow can be a single swirling air flow as a whole, and it is possible to eliminate mutual obstruction of the recirculating flow and the air flow entering from the introduction hole from the frontally colliding air flows. it can. Therefore, the recirculation flow is stable,
It is possible to perform good combustion up to low capacity operation with good flame retention.

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

【図1】本発明の実施例を示すガンタイプバーナの縦断
面構成図である。
FIG. 1 is a vertical cross-sectional configuration diagram of a gun type burner showing an embodiment of the present invention.

【図2】第1の仕切り筒の要部の横断面図である。FIG. 2 is a transverse cross-sectional view of a main part of a first partition cylinder.

【図3】図2を上からみた図である。FIG. 3 is a view of FIG. 2 seen from above.

【図4】従来のガンタイプバーナの断面構成図である。FIG. 4 is a cross-sectional configuration diagram of a conventional gun type burner.

【図5】図4に示すガンタイプバーナを燃焼筒の正面か
らみた図である。
5 is a view of the gun-type burner shown in FIG. 4 as seen from the front of a combustion cylinder.

【符号の説明】[Explanation of symbols]

10 燃焼筒 20 保炎器 21 導入穴 22 旋回羽根部 30 噴霧ノズル 40 第1の仕切り筒 42 切り起こし片 43 空気流入穴 50 第2の仕切り筒 60 ケース 70 送風器 80 点火器 90 リング体 91 空気流入穴 10 Combustion tube 20 Flame stabilizer 21 Introductory hole 22 Swirl vane section 30 Spray nozzle 40 First partition tube 42 Cut-and-raised piece 43 Air inlet hole 50 Second partition tube 60 Case 70 Blower 80 Igniter 90 Ring body 91 Air Inflow hole

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 中心部に液体噴霧燃料の導入穴を設ける
と共にその周囲に旋回羽根部を設けた保炎器で燃焼筒の
基端面を構成し、噴霧ノズルからの液体噴霧燃料を前記
保炎器中心部の導入穴から燃焼筒内に導入すると共に、
送風器から送られてくる空気を少なくとも2つの空気流
に分けて、その第1の空気流を前記保炎器中心部の導入
穴から液体噴霧燃料と一緒に燃焼筒内に導入し、第2の
空気流を前記保炎器の旋回羽根部を通して旋回させなが
ら燃焼筒内に導入するようにし、燃焼筒内で燃焼させる
ようにしたガンタイプバーナであって、前記保炎器中心
部の導入穴から液体噴霧燃料と一緒に燃焼筒内に導入さ
れる空気流を、保炎器の旋回羽根部を通して燃焼筒内に
導入される旋回空気流と同じ方向に旋回する旋回空気流
としたことを特徴とするガンタイプバーナ。
1. A base end face of a combustion cylinder is constituted by a flame stabilizer having an introduction hole for a liquid spray fuel in the center and a swirl vane portion provided around the introduction hole, and the liquid spray fuel from a spray nozzle is held by the flame stabilizer. While introducing into the combustion cylinder from the introduction hole in the center of the vessel,
The air sent from the blower is divided into at least two air streams, and the first air stream is introduced into the combustion cylinder together with the liquid atomized fuel from the introduction hole in the central part of the flame stabilizer, Is a gun-type burner adapted to be introduced into the combustion cylinder while being swirled through the swirl vane portion of the flame stabilizer, and to be burned in the combustion cylinder. The air flow introduced into the combustion cylinder together with the liquid atomized fuel from the air is a swirling air flow that swirls in the same direction as the swirling air flow introduced into the combustion cylinder through the swirl vanes of the flame stabilizer. Gun type burner.
JP12492193A 1993-04-27 1993-04-27 Gun type burner Expired - Fee Related JP3146760B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12492193A JP3146760B2 (en) 1993-04-27 1993-04-27 Gun type burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12492193A JP3146760B2 (en) 1993-04-27 1993-04-27 Gun type burner

Publications (2)

Publication Number Publication Date
JPH06313513A true JPH06313513A (en) 1994-11-08
JP3146760B2 JP3146760B2 (en) 2001-03-19

Family

ID=14897442

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12492193A Expired - Fee Related JP3146760B2 (en) 1993-04-27 1993-04-27 Gun type burner

Country Status (1)

Country Link
JP (1) JP3146760B2 (en)

Also Published As

Publication number Publication date
JP3146760B2 (en) 2001-03-19

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