JPH0245614Y2 - - Google Patents

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Publication number
JPH0245614Y2
JPH0245614Y2 JP16447685U JP16447685U JPH0245614Y2 JP H0245614 Y2 JPH0245614 Y2 JP H0245614Y2 JP 16447685 U JP16447685 U JP 16447685U JP 16447685 U JP16447685 U JP 16447685U JP H0245614 Y2 JPH0245614 Y2 JP H0245614Y2
Authority
JP
Japan
Prior art keywords
combustion
inner cylinder
swirler
air
primary air
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
Application number
JP16447685U
Other languages
Japanese (ja)
Other versions
JPS6275319U (en
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 filed Critical
Priority to JP16447685U priority Critical patent/JPH0245614Y2/ja
Publication of JPS6275319U publication Critical patent/JPS6275319U/ja
Application granted granted Critical
Publication of JPH0245614Y2 publication Critical patent/JPH0245614Y2/ja
Expired legal-status Critical Current

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

Description

【考案の詳細な説明】 (産業上の利用分野) 本考案は家庭用の給湯機などに使用される灯油
を燃料とする圧力噴霧式のバーナに関する。
[Detailed Description of the Invention] (Industrial Application Field) The present invention relates to a pressure spray type burner that uses kerosene as fuel and is used in household water heaters and the like.

(従来の技術) 従来、この種の石油バーナは第3図、第4図に
示すように、ノズル口1を先端に備えたノズル2
を筒状の内筒3内にのぞませ、ノズル2の後方側
に1次空気導入口4を開口し、1次空気を内筒3
内に導入し、旋回羽根5を有する旋回器6により
1次空気に旋回を与え1次燃焼を行い、さらに内
筒3の外周に外筒7を設け、内筒3と外筒7との
間に2次空気通路8を形成し、内筒3に設けた2
次空気口9より2次空気を供給し、2次燃焼を行
うものがあるが、この旋回器6は中心に丸穴10
を有し、丸穴10に連通するように旋回羽根5が
配置されている。
(Prior Art) Conventionally, this type of oil burner has a nozzle 2 equipped with a nozzle opening 1 at the tip, as shown in FIGS. 3 and 4.
into the cylindrical inner cylinder 3, the primary air inlet 4 is opened on the rear side of the nozzle 2, and the primary air is introduced into the inner cylinder 3.
A swirler 6 having swirling vanes 5 swirls the primary air to perform primary combustion, and an outer barrel 7 is provided on the outer periphery of the inner barrel 3 so that the air between the inner barrel 3 and the outer barrel 7 A secondary air passage 8 is formed in the inner cylinder 3, and a secondary air passage 8 is formed in the inner cylinder 3.
There is a device that supplies secondary air from the secondary air port 9 to perform secondary combustion, but this swirler 6 has a circular hole 10 in the center.
The rotating blade 5 is arranged so as to communicate with the round hole 10.

(考案が解決しようとする問題点) 従来構造の旋回器では中心の丸穴10に接する
ように旋回羽根5が傾斜をもつて切起されて配置
されているため、旋回器6周辺の旋回流領域とこ
の旋回流により2次的に生じる再循環領域とが互
いに干渉しやすいために灯油と空気との混合が不
均一となる領域があり、火災が安定せず燃焼騒音
も高いものであつた。そのため安定燃焼させるに
は燃焼用の1次空気と2次空気の配合を厳密に行
う必要があつた。即ち1次空気が過多となると旋
回器6での保炎性が悪くなり着火性、燃焼性が不
安定となり易かつた。旋回器6での保炎性を良く
し、安定燃焼させるには1次空気を少なくする必
要があり、このため1次空気導入口4の開口面積
を小さくする必要があつた。従つて2次燃焼主体
の燃焼となり、短火炎となるが燃焼騒音が高く、
バーナ部での圧力損失も大きく、大形のフアンを
使用する必要があつた。
(Problem to be solved by the invention) In the conventional structure of the swirler, the swirling blades 5 are cut and raised at an angle so as to be in contact with the central circular hole 10, so the swirling flow around the swirler 6 is reduced. Because the recirculation area and the recirculation area secondary to this swirling flow tend to interfere with each other, there are areas where kerosene and air mix unevenly, resulting in unstable fires and high combustion noise. . Therefore, in order to achieve stable combustion, it was necessary to strictly mix the primary air and secondary air for combustion. That is, when there is too much primary air, the flame stability in the swirler 6 deteriorates, and the ignitability and combustibility tend to become unstable. In order to improve flame stability in the swirler 6 and achieve stable combustion, it is necessary to reduce the amount of primary air, and therefore it is necessary to reduce the opening area of the primary air inlet 4. Therefore, the combustion is mainly secondary combustion, resulting in a short flame, but the combustion noise is high.
The pressure loss in the burner was also large, necessitating the use of a large fan.

本考案は上記欠点を鑑みてなされたものであ
り、バーナ部での圧力損失を小さく、燃焼騒音も
低くできる旋回器を提供することを目的とする。
The present invention was made in view of the above-mentioned drawbacks, and an object of the present invention is to provide a swirler that can reduce pressure loss in the burner section and reduce combustion noise.

(問題点を解決するための手段) 第1図、第2図に基づき、実施例と合せて説明
する。
(Means for Solving the Problems) Description will be made based on FIGS. 1 and 2 together with examples.

ノズル口1を先端に備えたノズル2を筒状の内
筒3内にのぞませ、ノズル2の後方側に1次空気
導入口4を開口し、1次空気を内筒3内に導入
し、旋回羽根5を有する旋回器6により1次空気
に旋回を与え1次燃焼を行い、さらに内筒3の外
周に外筒7を設け、内筒3と外筒7との間に2次
空気通路8を形成し、内筒3に設けた2次空気口
9より2次空気を供給し2次燃焼を行うものにお
いて、旋回器6の中心に丸穴10を設け、この丸
穴10の周りに旋回羽根5のない部分、即ちリン
グ状の安定板12を設けその周りに複数の旋回羽
根5を設けたものである。
A nozzle 2 equipped with a nozzle port 1 at the tip is inserted into a cylindrical inner cylinder 3, a primary air introduction port 4 is opened at the rear side of the nozzle 2, and primary air is introduced into the inner cylinder 3. , a swirler 6 having swirling vanes 5 swirls the primary air to perform primary combustion, and an outer cylinder 7 is provided around the outer circumference of the inner cylinder 3, and secondary air is circulated between the inner cylinder 3 and the outer cylinder 7. In a device that forms a passage 8 and performs secondary combustion by supplying secondary air from a secondary air port 9 provided in the inner cylinder 3, a round hole 10 is provided at the center of the swirler 6, and the air around this round hole 10 is A ring-shaped stabilizing plate 12 is provided at the portion without the swirling vanes 5, and a plurality of swirling vanes 5 are provided around the ring-shaped stabilizing plate 12.

(作用) 燃焼用の1次空気は1次空気導入口4から内筒
3内に入り、旋回器6により旋回流が与えられ、
ポンプ15で加圧された灯油は送油管14により
ノズル2に送られ、ノズル口1より噴霧され1次
空気と混合し旋回しながら旋回器6により保炎さ
れ1次燃焼し、2次空気口9より供給される2次
空気により2次燃焼する。本考案によれば1次空
気が旋回する際に旋回器6周辺の旋回流領域とこ
の旋回流により2次的に生じる再循環領域との間
に明確な境界領域を形成するために旋回器6の中
心の丸穴10の周りに旋回羽根のない部分、即ち
リング状の安定板12を設けたので旋回流領域と
再循環領域とが互いに干渉せず灯油と空気との混
合拡散が均一となり安定した燃焼が得られる。上
記理由により旋回器6での保炎性が良くなるため
1次空気量を多くすることができ、1次空気導入
口4の開口面積を大きくすることができる。また
旋回羽根5の一部を安定板12と平行にすると、
1次燃焼した旋回火炎の内筒3内での滞留時間が
長くなり、1次燃焼を有効に行つてから2次燃焼
へ移行することができ、従来のように2次燃焼主
体の燃焼となりにくく、より良好な安定した燃焼
が得られる。
(Function) Primary air for combustion enters the inner cylinder 3 from the primary air inlet 4, is given a swirling flow by the swirler 6,
The kerosene pressurized by the pump 15 is sent to the nozzle 2 through the oil pipe 14, sprayed from the nozzle port 1, mixed with primary air, and swirled while being held flame-stabilized by the swirler 6 for primary combustion. The secondary air supplied from 9 causes secondary combustion. According to the present invention, when the primary air swirls, the swirler 6 is used to form a clear boundary region between the swirling flow region around the swirler 6 and the recirculation region secondarily generated by this swirling flow. Since a part without swirling vanes, that is, a ring-shaped stabilizing plate 12 is provided around the circular hole 10 at the center of the kerosene, the swirling flow area and the recirculation area do not interfere with each other, and the mixing and diffusion of kerosene and air becomes uniform and stable. The result is a combustion with a high degree of combustion. For the above reasons, the flame stability in the swirler 6 is improved, so the amount of primary air can be increased, and the opening area of the primary air inlet 4 can be increased. Also, if a part of the swirling blade 5 is made parallel to the stabilizer plate 12,
The residence time of the swirling flame that has undergone primary combustion in the inner cylinder 3 becomes longer, and it is possible to effectively perform primary combustion before proceeding to secondary combustion, making it less likely that combustion will be dominated by secondary combustion as in the past. , better and more stable combustion can be obtained.

なお、旋回羽根5の一部を安定板12と平行に
した場合には、旋回羽根5の平行部と旋回器6本
体との隙間が小さ過ぎると旋回流が強過ぎ、圧力
損失も大きくなり、逆に隙間が大き過ぎると旋回
流が弱まり、灯油と空気の混合が悪くなるので、
隙間は3〜5mmが望ましい。さらに、旋回羽根5
がリング状の安定板12と旋回器6本体とで連結
されているため旋回羽根5の位置精度が確保され
る。
In addition, when a part of the swirling vane 5 is made parallel to the stabilizer plate 12, if the gap between the parallel part of the swirling vane 5 and the body of the swirler 6 is too small, the swirling flow will be too strong and the pressure loss will increase. On the other hand, if the gap is too large, the swirling flow will be weakened and the mixing of kerosene and air will be poor.
The gap is preferably 3 to 5 mm. Furthermore, the swirl vane 5
is connected by the ring-shaped stabilizing plate 12 and the main body of the swirler 6, so that the positional accuracy of the swirler blade 5 is ensured.

(考案の効果) 本考案によれば旋回器6での保炎性が良くなる
ので燃焼用の1次空気を大量に供給することが可
能となり、1次空気導入口4の開口面積を大きく
してバーナ部の圧力損失を小さくでき、小形のフ
アンが使用できる。さらに灯油と空気との均一な
混合拡散ができるので1次燃焼を有効に行つてか
ら2次燃焼へ移行することができ、短火炎でかつ
低騒音で良好な安定した燃焼性能を発揮すること
ができる。すなわち本考案により短火炎、低騒音
で性能の安定した液体燃料燃焼装置を得ることが
できる。
(Effects of the invention) According to the invention, flame stability in the swirler 6 is improved, making it possible to supply a large amount of primary air for combustion, and increasing the opening area of the primary air inlet 4. The pressure loss in the burner section can be reduced, and a small fan can be used. Furthermore, since kerosene and air can be mixed and diffused evenly, primary combustion can be carried out effectively before moving on to secondary combustion, resulting in good and stable combustion performance with short flame and low noise. can. That is, according to the present invention, a liquid fuel combustion device with short flame, low noise, and stable performance can be obtained.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本考案の一実施例を示す断面図、第2
図は第1図のP矢視図、第3図は従来例を示す断
面図、第4図は第3図のQ矢視図である。 符号の説明、1……ノズル口、2……ノズル、
3……内筒、4……1次空気導入口、5……旋回
羽根、6……旋回器、7……外筒、8……2次空
気通路、9……2次空気口、10……丸穴、12
……安定板、13……送風機、14……送油管、
15……ポンプ。
Fig. 1 is a sectional view showing one embodiment of the present invention;
The figures are a view in the direction of arrow P in FIG. 1, FIG. 3 is a sectional view showing a conventional example, and FIG. 4 is a view in direction of arrow Q in FIG. Explanation of symbols, 1... Nozzle mouth, 2... Nozzle,
3...Inner cylinder, 4...Primary air inlet, 5...Swirl vane, 6...Swirler, 7...Outer cylinder, 8...Secondary air passage, 9...Secondary air port, 10 ...Round hole, 12
... Stabilizer plate, 13 ... Air blower, 14 ... Oil pipe,
15...Pump.

Claims (1)

【実用新案登録請求の範囲】 1 液体燃料燃焼装置において、内筒と、より大
径の外筒との間に送風機により通風される通気
路を形成し、内筒内側に設けられた液体燃料噴
霧用ノズルのノズル口より前方側に2次空気口
を、後方側に1次空気導入口を開口して燃焼用
空気を内筒内側に供給し、ノズル口の前方に、
中心に丸穴を有し、その周りに複数の旋回羽根
を有する旋回器を設け、1次空気に旋回を与え
るものにおいて、旋回器の中心の丸穴の周りに
旋回羽根のない部分、即ちリング状の安定板を
設け、その周りに複数の旋回羽根を設けたこと
を特徴とする液体燃料燃焼装置。 2 旋回羽根の一部がリング状の安定板と平行で
あることを特徴とする実用新案登録請求の範囲
第1項記載の液体燃料燃焼装置。
[Claims for Utility Model Registration] 1. In a liquid fuel combustion device, an air passage is formed between an inner cylinder and an outer cylinder having a larger diameter to be ventilated by a blower, and liquid fuel spray provided inside the inner cylinder. A secondary air inlet is opened in front of the nozzle opening of the nozzle for combustion, and a primary air inlet is opened in the rear side to supply combustion air to the inside of the inner cylinder, and in front of the nozzle opening,
A swirler having a round hole in the center and a plurality of swirling vanes around it is provided to give swirl to the primary air. A liquid fuel combustion device characterized in that a stabilizer plate having a shape of the shape is provided and a plurality of swirl vanes are provided around the stabilizer plate. 2. The liquid fuel combustion device according to claim 1, wherein a part of the swirling vane is parallel to the ring-shaped stabilizing plate.
JP16447685U 1985-10-25 1985-10-25 Expired JPH0245614Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16447685U JPH0245614Y2 (en) 1985-10-25 1985-10-25

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16447685U JPH0245614Y2 (en) 1985-10-25 1985-10-25

Publications (2)

Publication Number Publication Date
JPS6275319U JPS6275319U (en) 1987-05-14
JPH0245614Y2 true JPH0245614Y2 (en) 1990-12-03

Family

ID=31093630

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16447685U Expired JPH0245614Y2 (en) 1985-10-25 1985-10-25

Country Status (1)

Country Link
JP (1) JPH0245614Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2523012B2 (en) * 1989-03-20 1996-08-07 三洋電機株式会社 Liquid fuel combustion device

Also Published As

Publication number Publication date
JPS6275319U (en) 1987-05-14

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