JPS618509A - Flame form adjusting mechanism of burner nozzle - Google Patents

Flame form adjusting mechanism of burner nozzle

Info

Publication number
JPS618509A
JPS618509A JP12816784A JP12816784A JPS618509A JP S618509 A JPS618509 A JP S618509A JP 12816784 A JP12816784 A JP 12816784A JP 12816784 A JP12816784 A JP 12816784A JP S618509 A JPS618509 A JP S618509A
Authority
JP
Japan
Prior art keywords
air
tip
air flow
out opening
burner nozzle
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
JP12816784A
Other languages
Japanese (ja)
Inventor
Akihiko Kishida
岸田 晃彦
Shuji Iida
修司 飯田
Mitsunobu Matsunaga
松永 三信
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor 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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP12816784A priority Critical patent/JPS618509A/en
Publication of JPS618509A publication Critical patent/JPS618509A/en
Pending legal-status Critical Current

Links

Landscapes

  • Nozzles For Spraying Of Liquid Fuel (AREA)

Abstract

PURPOSE:To obtain a flame form adjusting mechanism of a burner nozzle which can retain the flame form in optimum condition by the variation of the size of an air flow out opening which is provided at the axis of a tip blow out opening of the burner nozzle by a turning operation thereof. CONSTITUTION:An air flow passage is provided at the axis of the blow out opening 11 of the tip of this burner nozzle, that is at the inside of an oil nozzle. A shaft 18 is projected to the outside of the tip opening of an air flow passage 13, and a circular collision plate 19 to which the air passed through the air flow passage 13 wound collide is provided. The clearance between the outer periphery or the circular collision plate 19 and the tip opening of the air flow passage 13 is formed as a ring shaped air blow out opening 20. An atomized fuel oil is sprayed from the blow out opening 11. In this case, the size of the clearance of the air flown out opening 20 is varied by the screwy displacement of a connection section 16 with an air supply pipe 15 being revolved, a dispersion of an air being blown out from the blow out opening 20 is changed, the flame is lengthen or shorten from its inside and an optimum flame shape is obtained according to a load.

Description

【発明の詳細な説明】 〔発明の利用分野〕 本発明は、燃料油を空気、蒸気等のアトマイズ媒体によ
り微粒化して燃焼するバーナーノズルの火炎形状調節機
構に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Application of the Invention] The present invention relates to a flame shape adjustment mechanism for a burner nozzle that atomizes and burns fuel oil using an atomizing medium such as air or steam.

〔発明の背景〕[Background of the invention]

先ず第2図に基いて従来技術を説明する。アトマイズ媒
体として空気が流入管1を通ってバーナーノズル2内に
送給され、この送給されたアトマイズ媒体の一部が穴3
を通ってオイルノズル4の燃料噴き出し口5から出る燃
料油をエアーノズル6の内面7に付着させるように旋回
流として供給される。残シのアトマイズ媒体は穴8を通
しバーナーノズル2の本体9の先端と遮蔽板1oとの隙
間として形成されたリング形状の先端噴射口11を通り
外へ吹き出る。12は燃料油の流入管を示し、該流入管
12は前記燃料噴き出し口5を介してエアーノズル6内
と連通されている。また、バーナーノズル2の周囲には
前記微粒化された燃焼油と混合される燃焼用エアーを供
給するエアー噴出口(図示せず)が設けられている。流
入管12を流れてきた燃料油は熾、料噴き出し口5より
ェアーノズル2内に流れ出るが、この燃料油は穴3より
xy−/スル2内に流入するアトマイズ媒体の一部によ
転旋回流として先方に送られ、遮蔽板10に衝当すると
同時に、バーナーノズル2の先端開口面より外方に噴出
するアトマイズ媒体によって吹き飛ばされリング形状の
先端噴射口11よね微粒化されて噴射される。これに点
火すれば火炎となる。
First, the prior art will be explained based on FIG. Air is fed as an atomizing medium into the burner nozzle 2 through the inflow pipe 1, and a part of this fed atomizing medium flows into the hole 3.
The fuel oil that passes through the air nozzle 4 and exits from the fuel outlet 5 of the oil nozzle 4 is supplied as a swirling flow so as to adhere to the inner surface 7 of the air nozzle 6. The remaining atomized medium passes through the hole 8 and is blown out through the ring-shaped tip injection port 11 formed as a gap between the tip of the main body 9 of the burner nozzle 2 and the shielding plate 1o. Reference numeral 12 indicates a fuel oil inflow pipe, and the inflow pipe 12 communicates with the inside of the air nozzle 6 via the fuel jet port 5 . Furthermore, an air jet port (not shown) is provided around the burner nozzle 2 for supplying combustion air to be mixed with the atomized combustion oil. The fuel oil that has flowed through the inflow pipe 12 then flows out into the air nozzle 2 from the fuel jet port 5, but this fuel oil is rotated by a part of the atomized medium that flows into the xy-/through 2 from the hole 3. At the same time as it hits the shielding plate 10, it is blown off by the atomizing medium jetted outward from the tip opening surface of the burner nozzle 2, and is atomized into atomized particles by the ring-shaped tip injection port 11 and is injected. If you ignite it, it will become a flame.

ところが、上記従来のバーナーノズルでは、先端噴射口
110面積が可変ではないため、該噴射口J1の隙間の
大きさをバーナー高負荷時に最適な火炎形状となるよう
に設定すると、バーナー低負荷時には火炎が短くなって
しまい加熱効率が低下する。逆に前記隙間の大きさをバ
ーナー低負荷時に最適な火炎形状となるように設定する
と、バーナー高負荷時には火炎が長くなり過ぎ同じく加
熱効率が低下する。
However, in the above-described conventional burner nozzle, the area of the tip injection port 110 is not variable, so if the size of the gap between the injection port J1 is set to provide an optimal flame shape when the burner is under high load, the flame shape will not be as large when the burner is under low load. becomes shorter and heating efficiency decreases. Conversely, if the size of the gap is set so as to provide an optimal flame shape when the burner is under low load, the flame becomes too long when the burner is under high load, and the heating efficiency also decreases.

〔考案の目的〕 一 本考案は上記事情に鑑みなされたもので、バーナーの負
荷状態の違いにかかわらず、火炎形状を最適状態に保つ
ことができ、これにより加熱効率を向上させることので
きるバーナーノズルの火炎形状調節機構を提供するのが
目的である。
[Purpose of the invention] The present invention was developed in view of the above circumstances, and is a burner that can maintain an optimal flame shape regardless of the burner load condition, thereby improving heating efficiency. The purpose is to provide a nozzle flame shape adjustment mechanism.

〔考案の概要〕[Summary of the idea]

本考案の特徴は、バーナーノズルの先端噴射口の軸芯位
置に空気流路を設け、該空気流路の基端側にエアー供給
管との連結部を軸芯方向に螺進移動可能に螺合し、該連
結部より空気流路の先端開口面の外方までシャフトを延
出形成すると共に該シャフト先端に空気が衝当する円形
衝当部を設け、該円形衝当部と前記空気流路の先端開口
面との隙間を空気噴射口として形成することにより、前
記エアー供給管を回転させて前記連結部を螺進移動させ
、これにより先端の空気噴射口の隙間の大きさを変えて
該空気噴射口から噴射される空気の拡がりを変え、バー
ナーの負荷状態に合わせて火炎、を長炎化あるいは短炎
化して最適な火炎形状に保つようにした点におる。
The feature of the present invention is that an air flow path is provided at the axial position of the tip injection port of the burner nozzle, and a connecting part with the air supply pipe is screwed on the base end side of the air flow path so that it can be moved in the axial direction. A shaft is formed to extend from the connecting portion to the outside of the opening surface at the tip of the air flow path, and a circular abutting portion against which air hits is provided at the tip of the shaft, and the circular abutting portion and the air flow By forming a gap with the opening surface at the tip of the channel as an air injection port, the air supply pipe is rotated to move the connecting portion in a spiral manner, thereby changing the size of the gap between the air injection port at the tip. The advantage is that the spread of the air injected from the air injection port is changed to make the flame longer or shorter depending on the load condition of the burner, thereby maintaining an optimal flame shape.

〔考案の実施例〕[Example of idea]

−以下、本考案を図面の実施例に基いて詳細に説明する
。第1図は本考案に係るバーナーノズルの断面図を示す
。先端の噴射口11の軸芯位置すなわちオイルノス゛ル
4内に空気流路13が設けられている。該空気流路13
は円筒形状の空洞とじて形成され、基端側に雌ねじ14
が刻設されている。
-Hereinafter, the present invention will be explained in detail based on the embodiments shown in the drawings. FIG. 1 shows a sectional view of a burner nozzle according to the present invention. An air flow path 13 is provided at the axial center of the injection port 11 at the tip, that is, within the oil nozzle 4 . The air flow path 13
is formed as a cylindrical cavity, and has a female thread 14 on the proximal end.
is engraved.

該雌ねじ14の部分にエアー供給管15との連結部16
が螺合されて込る。すなわち、該連結部16の外周面に
は雄ねじ17が刻設され、エアー供給管15を回転する
ことにより当該連結部16が軸芯方向に螺進移動可能に
形成されている。該連結部16からシャフト18が先方
に向って延出形成されている。該シャフト18はその先
端が空気流路13の先端開口面より外方にまで突出され
ており、該先端に空気流路13内を通過してきた空気が
衝当する円形衝当部19が設けられている。該円形衝当
部19の外周と前記空気流路13の先端開口面との隙間
がり/グ形状の空気噴射口20として形成されている。
A connecting portion 16 with the air supply pipe 15 is provided at the female thread 14.
are screwed together. That is, a male thread 17 is formed on the outer circumferential surface of the connecting portion 16, and the connecting portion 16 is configured to be able to move in the axial direction by rotating the air supply pipe 15. A shaft 18 is formed to extend forward from the connecting portion 16. The tip of the shaft 18 protrudes outward from the opening surface of the tip of the air flow path 13, and the tip is provided with a circular impact portion 19 against which the air passing through the air flow path 13 hits. ing. An air injection port 20 is formed in the shape of a gap between the outer periphery of the circular abutting portion 19 and the opening surface at the tip of the air flow path 13 .

21は連通孔を示す。また22はスペーサを示シ、該ス
ペーサ22はシャフト18を軸芯線上に保持するための
もので、通孔23が穿設されている。その他の構成は上
記従来例と同様なので同一部分に同一符号を付して説明
は省略する。
21 indicates a communicating hole. Further, 22 indicates a spacer, and the spacer 22 is for holding the shaft 18 on the axial center line, and has a through hole 23 formed therein. The rest of the configuration is similar to that of the conventional example, so the same parts are given the same reference numerals and the explanation will be omitted.

次に作用を説明する。前述の如く、先端の噴射口11よ
りアトマイト媒体により微粒化された燃料油が先方に向
って噴射される。この点は従来例と同様である。エアー
供給管15を回転して連結部16を螺進移動させて空気
噴射口20の隙間の大きさを変化させ、該空気噴射口2
0より噴射される空気の拡がりを変えて火炎の内側より
該火炎を長炎化あるいは短炎化する。すなわち、バーナ
ー高負荷時には空気噴射口20の隙間の大きさを小さく
して該空気噴射口20より噴射される空気の拡がりを大
きくすることによって火炎を短炎化して最適な火炎形状
傾する。逆にバーナー低負荷時には前記隙間の大きさを
大きくして噴射される空気の拡がりを小さくすることに
よって火炎を長炎化して最適な火炎形状にする。
Next, the effect will be explained. As described above, fuel oil atomized by the atomite medium is injected forward from the injection port 11 at the tip. This point is similar to the conventional example. The air supply pipe 15 is rotated to spirally move the connecting portion 16 to change the size of the gap between the air injection ports 20.
By changing the spread of air injected from zero, the flame is made longer or shorter from inside the flame. That is, when the burner is under high load, the size of the gap between the air injection ports 20 is reduced to increase the spread of the air injected from the air injection ports 20, thereby shortening the flame and tilting the optimal flame shape. Conversely, when the burner is under low load, the size of the gap is increased to reduce the spread of the injected air, thereby making the flame longer and giving it an optimal flame shape.

〔考案の効果〕[Effect of idea]

本考案によれば、バーナーノズルの先端噴射口の軸芯位
置に空気噴射口を設け、該空気噴射口の大きさをエアー
供給管の回転操作により変えて該空気噴射口から噴射さ
れる空気の拡がりを変え、バーナーの負荷状態に合わせ
て火炎の形状を長炎化あるいは短炎化することができる
ようにしたので、バーナーの負荷状態の違いにかかわら
ず、火炎形状を最適状態に保つことができる。従って加
熱効率を向上させることができる。
According to the present invention, an air injection port is provided at the axial center position of the tip injection port of the burner nozzle, and the size of the air injection port is changed by rotating the air supply pipe, so that the amount of air injected from the air injection port is changed. By changing the spread, the flame shape can be made longer or shorter depending on the burner load condition, so the flame shape can be maintained in the optimal state regardless of the burner load condition. can. Therefore, heating efficiency can be improved.

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

第1図は本考案に係るバーナーノズルの断面図、第2図
は従来のバーナーノズルの断面図を示す。 2・・・バーナーノズル、  11・・・先端噴射口。 13・・・空気流路、  15・・・エアー供給管。 16・・・連結部、1B・・・シャフト、  19・・
・円形衝当部、  20・・・空気噴射口。
FIG. 1 is a sectional view of a burner nozzle according to the present invention, and FIG. 2 is a sectional view of a conventional burner nozzle. 2... Burner nozzle, 11... Tip injection port. 13... Air flow path, 15... Air supply pipe. 16...Connection part, 1B...Shaft, 19...
- Circular impact part, 20... air injection port.

Claims (1)

【特許請求の範囲】[Claims] 微粒化された燃料をノズル先端のリング形状の噴射口よ
り噴霧するバーナーノズルにおいて、該噴射口の軸芯位
置に空気流路を設け、該空気流路の基端側にエアー供給
管との連結部を軸芯方向に螺進移動可能に螺合し、該連
結部より空気流路の先端開口面の外方までシャフトを延
出形成すると共に該シャフト先端に空気が衝当する円形
衝当部を設け、該円形衝当部と前記空気流路の先端開口
面との隙間を空気噴射口として形成したことを特徴とす
るバーナーノズルの火炎形状調節機構。
In a burner nozzle that sprays atomized fuel from a ring-shaped injection port at the tip of the nozzle, an air flow path is provided at the axial position of the injection port, and the base end of the air flow path is connected to an air supply pipe. a circular abutting part in which the shaft is screwed together so as to be able to move in the axial direction, and a shaft is formed to extend from the connecting part to the outside of the opening surface at the tip of the air flow path, and air hits the tip of the shaft; A flame shape adjustment mechanism for a burner nozzle, characterized in that the gap between the circular abutting portion and the opening surface at the tip of the air flow path is formed as an air injection port.
JP12816784A 1984-06-21 1984-06-21 Flame form adjusting mechanism of burner nozzle Pending JPS618509A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12816784A JPS618509A (en) 1984-06-21 1984-06-21 Flame form adjusting mechanism of burner nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12816784A JPS618509A (en) 1984-06-21 1984-06-21 Flame form adjusting mechanism of burner nozzle

Publications (1)

Publication Number Publication Date
JPS618509A true JPS618509A (en) 1986-01-16

Family

ID=14978049

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12816784A Pending JPS618509A (en) 1984-06-21 1984-06-21 Flame form adjusting mechanism of burner nozzle

Country Status (1)

Country Link
JP (1) JPS618509A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5048681A (en) * 1989-04-27 1991-09-17 Henkel Walter R Envelope storage for compact discs
US6164956A (en) * 1997-02-11 2000-12-26 Ge Energy & Environmental Research Corporation System and method for removing ash deposits in a combustion device
CN114673987A (en) * 2022-03-08 2022-06-28 湘潭大学 Adjustable heavy oil atomizing nozzle and adjusting method

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5048681A (en) * 1989-04-27 1991-09-17 Henkel Walter R Envelope storage for compact discs
US6164956A (en) * 1997-02-11 2000-12-26 Ge Energy & Environmental Research Corporation System and method for removing ash deposits in a combustion device
CN114673987A (en) * 2022-03-08 2022-06-28 湘潭大学 Adjustable heavy oil atomizing nozzle and adjusting method

Similar Documents

Publication Publication Date Title
US3310240A (en) Air atomizing nozzle
CN106996561B (en) Fuel atomizer
JP2005351614A (en) Fuel atomizer, conical swirler for combustor dome, and manufacturing method thereof
US4003692A (en) High velocity burner
US4815664A (en) Airblast fuel atomizer
US4728285A (en) Device for the combustion of fluid combustible materials
US5176324A (en) Fuel spraying method in liquid fuel combustion burner, and liquid fuel combustion burner
US4014639A (en) Recirculating vortex burner
US4201538A (en) Large burners, particularly for liquid fuels
CN106016364A (en) Unit two-cyclone premixed combustion nozzle for dry-type low-pollution combustion chamber of gas turbine
JPH0849816A (en) Method and equipment for distributing fuel in burner also proper to liquid fuel and also proper to gas fuel
US20030110776A1 (en) Atomizer for a combustor and associated method for atomizing fuel
US1587249A (en) Method of and apparatus for burning oil
JPS618509A (en) Flame form adjusting mechanism of burner nozzle
JPH0550646B2 (en)
JP3889079B2 (en) Burner
WO1987002756A1 (en) Radiant tube burner
US1144719A (en) Oil-burner.
US4194874A (en) Variable flame shape oil burner
JPH1182941A (en) Oxygen burner
JPS59145405A (en) Burner device
JPH0120323B2 (en)
KR910001837B1 (en) Radiant tube burner
JPH0424254Y2 (en)
US3446439A (en) Liquid fuel burners