JPH01155111A - Burner - Google Patents

Burner

Info

Publication number
JPH01155111A
JPH01155111A JP31279087A JP31279087A JPH01155111A JP H01155111 A JPH01155111 A JP H01155111A JP 31279087 A JP31279087 A JP 31279087A JP 31279087 A JP31279087 A JP 31279087A JP H01155111 A JPH01155111 A JP H01155111A
Authority
JP
Japan
Prior art keywords
gas
fuel gas
pipe
air
ejection
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
JP31279087A
Other languages
Japanese (ja)
Inventor
Jiro Nakamaru
中丸 治郎
Katsuhisa Yamada
勝久 山田
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.)
SANREE REINETSU KK
Tokyo Gas Co Ltd
Sunray Reinetsu Co Ltd
Original Assignee
SANREE REINETSU KK
Tokyo Gas Co Ltd
Sunray Reinetsu Co Ltd
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 SANREE REINETSU KK, Tokyo Gas Co Ltd, Sunray Reinetsu Co Ltd filed Critical SANREE REINETSU KK
Priority to JP31279087A priority Critical patent/JPH01155111A/en
Publication of JPH01155111A publication Critical patent/JPH01155111A/en
Pending legal-status Critical Current

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  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Abstract

PURPOSE:To curtail operation cost, eliminate restrictions on installation sites, and reduce production cost as well, by forming an ejection section in a gas ejection member so that fuel gas may be ejected in a peripheral direction so as to obtain a rotary force, providing air discharge impellers made in one piece with said gas ejection member, and flame maintenance section on the lower stream side of the gas ejection member. CONSTITUTION:As ejection sections 5 are designed so that fuel gas may be ejected in a peripheral direction of a fuel gas pipe 3, a gas ejection member 4 obtains a rotary force in a peripheral direction of the fuel gas pipe 3 from the ejection energy of fuel gas ejected from the ejection section 5, and starts rotary motion. Since the gas ejection member 4 and air discharge impellers 6 are made in one piece construction, the air discharge impellers 6 carry out rotary motion as well. This construction makes it possible to feed combustion air smoothly into an air blow pipe 2 from an opening 7a on the upper stream side of the air blow pipe 2, and mix the fuel gas and the combustion air to a satisfactory extent in a flame maintenance section 10, then start combustion. More specifically, high temperature combustion gas is generated in the air discharge pipe 2. The generated combustion gas is ejected as a hot air from an opening 7b on the lower stream side of said blow pipe 2, which makes it possible to use the hot air for drying and heating service as well.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、例えば乾燥や暖房に使用するバーナ装置に関
するものである。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a burner device used, for example, for drying or heating.

(従来の技術およびその問題点) 従来の大容量バーナとしては、例えば第5図に示すもの
がある。かかる従来の大容量バーナaは、送風管す内に
燃料ガスパイプCと炎口部dとを設けると共に、モータ
駆動のブロワeにより、強制的に空気を送風管す内に送
り込み、炎口部dにおいて燃料ガスを燃焼させ、この際
発生する高温の燃焼ガスを送風管すより外部へ噴出して
使用するものである。
(Prior art and its problems) As a conventional large capacity burner, there is one shown in FIG. 5, for example. Such a conventional large-capacity burner a is provided with a fuel gas pipe C and a flame port d in the blast pipe, and uses a motor-driven blower e to forcibly send air into the blast pipe to open the flame port d. The fuel gas is combusted in the combustion chamber, and the high-temperature combustion gas generated at this time is blown out through the blast pipe and used.

このように、従来の大容量バーナaは、ブロワeを用い
て燃焼用空気の供給を行なっており、ブロワeは不可欠
の構成要素になっている。このため、ブロワeの運転に
多くの電力を必要とし、運転コストがかかるうえ、電気
配線等の面で設置場所に制限があり、製造コストも高い
という問題点がある。
In this way, the conventional large-capacity burner a uses the blower e to supply combustion air, and the blower e has become an essential component. Therefore, there are problems in that a large amount of electric power is required to operate the blower e, which increases operating costs, and there are restrictions on installation locations due to electrical wiring, etc., and manufacturing costs are also high.

本発明はかかる問題点を解決することを目的とするもの
である。
The present invention aims to solve such problems.

(問題点を解決するための手段) 本発明の構成を実施例に対応する第1図〜第4図に基づ
いて説明する。
(Means for Solving the Problems) The configuration of the present invention will be explained based on FIGS. 1 to 4, which correspond to embodiments.

本発明の第一のバーナ装置lは、第1図に示す通り、上
下流側を開口した送風管2内に燃料ガスパイプ3を設置
し、この燃料ガスパイプ3の先端にガス噴出部材4を旋
回自在に設けると共に、該ガス噴出部材4には燃料ガス
を周方向に噴射して、回転力を得るように噴出部5を構
成し、前記ガス噴出部材にはそれと一体に空気流送用羽
根6を設け、前記ガス噴出部材の下流側には保炎部10
を設けた構成とする。第二の発明のバーナ装置1′は、
第2図に示す通り、第一の発明に加えて、燃料ガスパイ
プ2を回転自在に構成すると共に前記燃料ガスパイプ2
の外周には空気流送用羽根6′を設ける構成である。
As shown in FIG. 1, the first burner device 1 of the present invention has a fuel gas pipe 3 installed in a blast pipe 2 that is open on the upstream and downstream sides, and a gas jetting member 4 that can be freely rotated at the tip of the fuel gas pipe 3. The gas jetting member 4 is provided with a jetting portion 5 to inject fuel gas in the circumferential direction to obtain rotational force, and the gas jetting member is integrally provided with an air flow blade 6. A flame stabilizing section 10 is provided on the downstream side of the gas ejecting member.
The configuration includes the following. The burner device 1' of the second invention is
As shown in FIG. 2, in addition to the first invention, the fuel gas pipe 2 is configured to be rotatable, and the fuel gas pipe 2
Air-flowing vanes 6' are provided on the outer periphery of the blade.

(作 用) 本発明の作用を実施例と共に説明する。(for production) The operation of the present invention will be explained with reference to examples.

第1図に示すように、燃料ガスパイプ3内に矢印Aの方
向に燃料ガスを供給すると、燃料ガスは燃料ガスパイプ
3の先端に設けたガス噴出部材4に到達して噴出部5よ
り噴出する。
As shown in FIG. 1, when fuel gas is supplied into the fuel gas pipe 3 in the direction of arrow A, the fuel gas reaches the gas ejection member 4 provided at the tip of the fuel gas pipe 3 and is ejected from the ejection part 5.

かかる噴出に於いて、ガス噴出部材4は燃料ガスパイプ
3の先端に燃料ガスパイプ3の周方向に旋回自在に設け
てあり、しかも噴出部5は燃料ガスを燃料ガスパイプ3
の周方向に噴射するように構成したので、噴出部5から
の燃料ガスの噴射エネルギーにより、ガス噴出部材4は
燃料ガスパイプ3の周方向に回転力を得て、回転運動を
始める。
In such jetting, the gas jetting member 4 is provided at the tip of the fuel gas pipe 3 so as to be able to freely rotate in the circumferential direction of the fuel gas pipe 3, and the jetting portion 5 is configured to supply the fuel gas to the fuel gas pipe 3.
Since the fuel gas is configured to be injected in the circumferential direction of the fuel gas pipe 3, the gas ejection member 4 obtains rotational force in the circumferential direction of the fuel gas pipe 3 due to the injection energy of the fuel gas from the ejection part 5, and starts rotating.

ガス噴出部材4が回転すると、ガス噴出部材4には空気
流送用羽根6を一体に設けであるので、空気流送用羽根
6も回転を行う。空気流送用羽根6は図に示すように、
噴出部5からの燃料ガスの噴射方向とは反対の方向に回
転した場合、送風管2の空気を、送風管2の下流側聞ロ
アb方向にし、上流側聞ロアaから下流側聞ロアbに向
かう空気流を形成する。したがって、空気流送用羽根6
が回転することによって、送風管2の上流側聞ロアaか
ら送風管2内へ、円滑に燃焼用空気を送り込むことがで
き、保炎部10に於いて、燃料ガスと燃焼用空気が良好
に混合して燃焼を開始する。
When the gas ejection member 4 rotates, since the air flow blade 6 is integrally provided with the gas ejection member 4, the air flow blade 6 also rotates. As shown in the figure, the air flow vane 6 is
When the rotation is in the opposite direction to the injection direction of the fuel gas from the jetting part 5, the air in the blast pipe 2 is directed toward the downstream lower part b of the blast pipe 2, and from the upstream lower part a to the downstream lower part b. Forms an airflow towards. Therefore, the air flow blade 6
By rotating, combustion air can be smoothly sent into the blast pipe 2 from the upstream side lower part a of the blast pipe 2, and the fuel gas and combustion air can be well exchanged in the flame stabilizing section 10. Mix and start combustion.

しかして、送風管2内において、高温の燃焼ガスが発生
して、送風管2の下流側聞ロアbから熱風として噴出し
、これを乾燥あるいは暖房等に用いることができる。
As a result, high-temperature combustion gas is generated within the blast pipe 2 and is blown out as hot air from the downstream lower part b of the blast pipe 2, which can be used for drying, heating, or the like.

さらに本発明のバーナ装置1においては、空気流送用羽
根6の回転により、送風管2の上流側聞ロアaから送風
管2内へ流入する空気量は、空気流送用羽根6の回転速
度に依存し、回転を早めれば多くなり、遅くすれば少な
くなる。そして、空気流送用羽根6の回転速度は、ガス
噴出部材4における燃料ガスの噴出圧に依存し、燃料ガ
スの噴出圧を大きくすれば早くなり、反対に小さくする
と遅くなる。したがって、ガス噴出部材4の噴出圧に対
応して、望ましい空気量を自動的に実現することができ
る。第2図に示すバーナ装置1′は以上に加えて、回転
自在とした燃料ガスパイプ2の外周に羽根6′を設けた
ので、羽根6′による圧縮力が加わって、その分だけ空
気量が増加し、保炎部10に於いて、高負荷燃焼が達成
できる。
Furthermore, in the burner device 1 of the present invention, the amount of air flowing into the blast pipe 2 from the upstream lower lower a of the blast pipe 2 due to the rotation of the airflow vanes 6 is determined by the rotational speed of the airflow vanes 6. It depends on the speed, the faster the rotation, the more it will be, and the slower the rotation, the less it will be. The rotational speed of the air flow vane 6 depends on the fuel gas ejection pressure in the gas ejection member 4, and increases as the fuel gas ejection pressure increases, and decreases as the fuel gas ejection pressure decreases. Therefore, a desired amount of air can be automatically achieved in accordance with the ejection pressure of the gas ejection member 4. In addition to the above, the burner device 1' shown in Fig. 2 is equipped with blades 6' around the outer periphery of the freely rotatable fuel gas pipe 2, so the compressive force from the blades 6' is applied, increasing the amount of air accordingly. However, high load combustion can be achieved in the flame stabilizing section 10.

以上の構成において、ガス噴出部材4は、例えば燃料ガ
スパイプ3の先端内側に、気密性軸受8を介して、一端
開放で他端閉塞の中空パイプ9の開放端側を嵌合し、中
空パイプ9を燃料ガスパイプ3の周方向に旋回自在に設
け、さらに中空パイプ9の外側に適数のガス噴出部材4
を突設する等適宜に構成して良い。第2図に於いて、符
号11はロータリージヨイントを示す。
In the above configuration, the gas ejection member 4 fits the open end side of the hollow pipe 9 with one end open and the other end closed, for example, inside the tip of the fuel gas pipe 3 via the airtight bearing 8. are provided so as to be able to turn freely in the circumferential direction of the fuel gas pipe 3, and furthermore, an appropriate number of gas ejection members 4 are provided on the outside of the hollow pipe 9.
It may be configured as appropriate, such as by protruding. In FIG. 2, reference numeral 11 indicates a rotary joint.

また、流送用羽根6は、噴出部5からの燃料ガスの噴射
方向とは反対の方向に回転した場合に、送風管2内の空
気を下流側に流送できるならば形状、数等は適宜である
In addition, the shape, number, etc. of the flow blades 6 can be changed as long as they can flow the air in the blast pipe 2 to the downstream side when rotated in the opposite direction to the injection direction of the fuel gas from the jetting part 5. It is appropriate.

(発明の効果) 本発明は以上のように、電力を多品に消費するブロワを
用いなくても、燃焼用空気の供給を円滑に行えるので、
運転コストを削減することができると共に電気配線の必
要がないので、設置場所の制限も解消することができる
(Effects of the Invention) As described above, the present invention can smoothly supply combustion air without using a blower that consumes a large amount of electricity.
Operating costs can be reduced, and since there is no need for electrical wiring, restrictions on installation locations can also be eliminated.

その上、燃焼計に応じた望ましい空気量を自動的に実現
できるため、空気量制御のための特別な手段を設ける必
要がないので設計が簡単で、バーナ自体を小型で簡素に
構成することができ、製造コストも低減し得るという効
果がある。
Furthermore, since the desired air volume according to the combustion meter can be automatically achieved, there is no need to provide special means for controlling the air volume, which simplifies the design and allows the burner itself to be small and simple. This has the effect of reducing manufacturing costs.

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

第1図及び第2図は本発明の詳細な説明図、第3図及び
第4図は要部拡大図、第5図は従来例の模式的縦断面図
である。 符号1.1′・・・バーナ装置、2・・・送風管、3・
・・燃料ガスパイプ、4・・・ガス噴出部材、5・・・
噴出部、6.6′・・・空気流送用羽根、7a・・・送
風管2の上流側開口、7b・・・送風管2の下流側開口
、8・・・気密性軸受、9・・・中空パイプ、10・・
・保炎部、11・・・ロータリーバルブ、A・・・燃料
ガスの供給方向。 第1図 手続補正書 28発明の名称 バーナ装置 3、補正をする者 事件との関係   特許出願人 住所 東京都港区海岸−丁目5番20号代表者 渡辺 
宏 4、代理人 〒101  m (294) 7341−
2j”’−−−’7T: 氏名 (7110)弁理士 三 背 晃1司 ・、1! 5、補正命令の日付           し°−−−
一、1自発補正 6、補正の対象 7、補正の内容 (1)図面の全部を本書に添付のものに補正します。 (2)明細書簡3頁18行目、19行目及び第6頁1行
目に夫々記載の「燃料ガスパイプ2」を「燃料ガスパイ
プ3」と補正します。 (3)明m書第6頁13行目に記載の「流送用羽根6」
を「流送用羽根6,6’Jと補正します。 (4)明細書簡7頁9〜10行目に記載の「第3図及び
第4図」を[第3図は第1図の側面説明図及び第4図」
と補正します。 (5)明細書第7頁17行目に記載の「ロータリーバル
ブJを「ロータリージヨイント」と補正します。 8、添付書類の目録
1 and 2 are detailed explanatory views of the present invention, FIGS. 3 and 4 are enlarged views of essential parts, and FIG. 5 is a schematic vertical sectional view of a conventional example. Code 1.1'...Burner device, 2...Blow pipe, 3.
...Fuel gas pipe, 4...Gas ejection member, 5...
Ejection part, 6.6'... Air flow blade, 7a... Upstream opening of blast pipe 2, 7b... Downstream opening of blast pipe 2, 8... Airtight bearing, 9.・Hollow pipe, 10...
・Flame holding part, 11... Rotary valve, A... Fuel gas supply direction. Figure 1 Procedural amendment 28 Name of the invention Burner device 3, person making the amendment Relationship to the case Patent applicant address 5-20 Kaigan-chome, Minato-ku, Tokyo Representative Watanabe
Hiroshi 4, Agent 101 m (294) 7341-
2j"'----'7T: Name (7110) Patent attorney Sanse Akira 1ji ・、1! 5. Date of amendment order shi°----
1.1 Voluntary amendment 6. Subject of amendment 7. Details of amendment (1) All drawings will be amended to those attached to this document. (2) "Fuel gas pipe 2" written on page 3, lines 18 and 19 of the specification letter, and page 6, line 1, respectively, will be corrected to "fuel gas pipe 3." (3) “Flowing vane 6” described on page 6, line 13 of the Meiji M.
(4) "Figures 3 and 4" written on page 7, lines 9-10 of the specification letter [Figure 3 is the same as Figure 1] Side view and Figure 4
I will correct it. (5) "Rotary valve J" written on page 7, line 17 of the specification is corrected to "rotary joint." 8. List of attached documents

Claims (2)

【特許請求の範囲】[Claims] (1)上下流側を開口した送風管内に燃料ガスパイプを
設置し、この燃料ガスパイプの先端にガス噴出部材を旋
回自在に設けると共に、該ガス噴出部材には燃料ガスを
周方向に噴射して、回転力を得るように噴出部を構成し
、前記ガス噴出部材にはそれと一体に空気流送用羽根を
設け、前記ガス噴出部材の下流側には、保炎部を設けた
ことを特徴とするバーナ装置。
(1) A fuel gas pipe is installed in a blast pipe with openings on the upstream and downstream sides, a gas jetting member is rotatably provided at the tip of the fuel gas pipe, and fuel gas is injected into the gas jetting member in the circumferential direction, The ejection part is configured to obtain rotational force, the gas ejection member is provided with an air flow blade integrally therewith, and a flame stabilizing part is provided on the downstream side of the gas ejection member. Burner device.
(2)上下流側を開口した送風管内に、燃料ガスパイプ
を設置し、この燃料ガスパイプは回転自在とし、且つそ
の外周には空気流送用羽を設けると共に、前記燃料ガス
パイプの先端にはガス噴出部材を旋回自在に設け、該ガ
ス噴出部材には燃料ガスを周方向に噴出して、回転力を
得るように噴出部を構成し、前記ガス噴出部材には、そ
れと一体に空気流送用羽根を設け、前記ガス噴出部材の
下流側には、保炎部を設けたことを特徴とするバーナ装
置。
(2) A fuel gas pipe is installed in the blast pipe that opens on the upstream and downstream sides, and this fuel gas pipe is rotatable, and air flow blades are provided on the outer periphery, and a gas jet is provided at the tip of the fuel gas pipe. The member is rotatably provided, and the gas ejecting member has an ejecting portion configured to eject fuel gas in the circumferential direction to obtain rotational force, and the gas ejecting member is integrally provided with air flow blades. A burner device comprising: a flame stabilizing section provided downstream of the gas ejecting member.
JP31279087A 1987-12-10 1987-12-10 Burner Pending JPH01155111A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP31279087A JPH01155111A (en) 1987-12-10 1987-12-10 Burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP31279087A JPH01155111A (en) 1987-12-10 1987-12-10 Burner

Publications (1)

Publication Number Publication Date
JPH01155111A true JPH01155111A (en) 1989-06-19

Family

ID=18033437

Family Applications (1)

Application Number Title Priority Date Filing Date
JP31279087A Pending JPH01155111A (en) 1987-12-10 1987-12-10 Burner

Country Status (1)

Country Link
JP (1) JPH01155111A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114060808A (en) * 2021-11-17 2022-02-18 徐州燃烧控制研究院有限公司 Spiral pulse low-nitrogen combustion method and combustor thereof

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5028414U (en) * 1973-07-12 1975-04-01
JPS5677610A (en) * 1979-11-28 1981-06-26 Hitachi Ltd Combustor

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5028414U (en) * 1973-07-12 1975-04-01
JPS5677610A (en) * 1979-11-28 1981-06-26 Hitachi Ltd Combustor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114060808A (en) * 2021-11-17 2022-02-18 徐州燃烧控制研究院有限公司 Spiral pulse low-nitrogen combustion method and combustor thereof
CN114060808B (en) * 2021-11-17 2024-01-05 徐州燃烧控制研究院有限公司 Spiral pulse low-nitrogen combustion method and burner thereof

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