JPH07225010A - Burner - Google Patents

Burner

Info

Publication number
JPH07225010A
JPH07225010A JP6018132A JP1813294A JPH07225010A JP H07225010 A JPH07225010 A JP H07225010A JP 6018132 A JP6018132 A JP 6018132A JP 1813294 A JP1813294 A JP 1813294A JP H07225010 A JPH07225010 A JP H07225010A
Authority
JP
Japan
Prior art keywords
fuel
heater
air
combustor
tip
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
JP6018132A
Other languages
Japanese (ja)
Other versions
JP3407228B2 (en
Inventor
Tomomitsu Takeuchi
朝光 竹内
Saburo Maruko
三郎 丸子
Kenji Onoe
健志 尾上
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.)
Nippon Chemical Plant Consultant Co Ltd
Eneos Corp
Original Assignee
Nippon Chemical Plant Consultant Co Ltd
Nippon Oil 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 Nippon Chemical Plant Consultant Co Ltd, Nippon Oil Corp filed Critical Nippon Chemical Plant Consultant Co Ltd
Priority to JP01813294A priority Critical patent/JP3407228B2/en
Publication of JPH07225010A publication Critical patent/JPH07225010A/en
Application granted granted Critical
Publication of JP3407228B2 publication Critical patent/JP3407228B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00Combustion technologies with mitigation potential
    • Y02E20/34Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Landscapes

  • Spray-Type Burners (AREA)

Abstract

PURPOSE:To suppress generation of NOx without preheating the air even in a burner for a liquid fuel and to obtain high-temperature combustion gas without unburned matter. CONSTITUTION:A burner has a fuel heating mixer connected to one side of a combustion chamber 1 to heat fuel and mixing it with the air to diffuse to the chamber 1. The mixer has a throat 4 at an intermediate part, a venturi 3, having an air inlet at an upstream side of the throat 4, and a rodlike heater contained in a fuel introducing tube 10 having a nozzlelike end. A fuel supply tube is connected to one annular passage along an outer periphery of the heater, and its end is opened with the throat 4 of the venturi 3 to form a fuel heater.

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、高温の燃焼ガスを得る
ための燃焼器に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combustor for obtaining high temperature combustion gas.

【0002】[0002]

【従来の技術】燃焼器で得られる燃焼ガスは、公害物
質、すなわちNOx 及び未燃焼分が無く、さらに完全燃
焼して残留O2 が少ないことが望ましい。従来のこの種
の燃焼器は、空気と燃料を爆発限界範囲内の濃度で混合
し、これを電気スパーク等の手段にて着火させて火炎を
形成し、その後は上記空気と燃料の混合気を継続して燃
焼させるようにしている。
2. Description of the Related Art It is desirable that the combustion gas obtained in a combustor is free of pollutants, that is, NO x and unburned components, and that it is completely combusted to reduce residual O 2 . This type of conventional combustor mixes air and fuel at a concentration within an explosion limit range, ignites this by means such as electric sparks to form a flame, and thereafter, mixes the air-fuel mixture. I try to burn it continuously.

【0003】[0003]

【発明が解決しようとする課題】しかしながら上記従来
の燃焼器にて液体燃料を燃焼した場合には、燃料が液滴
状となって分散されるので、燃焼時に部分的な高温部が
発生してしまい、NOxがかなりの量で発生していた。
これを防止するためには、混合用の空気を予熱しなけれ
ばならない。
However, when liquid fuel is burned in the above-mentioned conventional combustor, the fuel is dispersed in the form of liquid droplets, so that a partial high temperature portion is generated during burning. However, NO x was generated in a considerable amount.
To prevent this, the mixing air must be preheated.

【0004】本発明は上記のことにかんがみなされたも
ので、液体燃料用の燃焼器でも、空気を予熱することな
く、NOx の発生を抑制でき、未燃物が無い高温の燃焼
ガスを得ることができるようにした燃焼器を提供するこ
とを目的とするものである。
The present invention has been conceived in view of the above, and even in a combustor for liquid fuel, the generation of NO x can be suppressed without preheating the air, and a high-temperature combustion gas containing no unburned matter can be obtained. It is an object of the present invention to provide a combustor capable of being manufactured.

【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
に、本発明に係る燃焼器は、燃焼室1の一側部に、燃料
を加熱すると共に、空気と混合して燃焼室1へ吹き込む
燃料加熱混合器を接続した燃焼器において、上記燃料加
熱混合器を、中間部にスロート部4を有し、このスロー
ト部4より上流側に空気流入管6を接続したベンチュリ
ー体3と、先端をノズル状にした燃料投入管10内に棒
状のヒータを内装し、このヒータの外周に沿う環状の通
路の一方に燃料供給管13を接続し、先端を上部ベンチ
ュリー体3のスロート部4に開口してなる燃料加熱器と
にて構成した。
To achieve the above object, a combustor according to the present invention heats fuel on one side of a combustion chamber 1 and mixes it with air and blows it into the combustion chamber 1. In a combustor to which a fuel heating mixer is connected, the fuel heating mixer is provided with a venturi body 3 having a throat portion 4 in an intermediate portion and an air inflow pipe 6 connected to an upstream side of the throat portion 4, and a tip thereof. A rod-shaped heater is provided inside a nozzle-shaped fuel injection pipe 10, a fuel supply pipe 13 is connected to one of the annular passages along the outer circumference of the heater, and the tip is opened to the throat portion 4 of the upper venturi body 3. It consists of a fuel heater.

【0006】そして上記燃料加熱器のヒータの外周に沿
う環状の通路内に螺旋状のバッフル12を設ける。さら
に、上記燃料加熱器の外周側に、先端が燃料加熱器のノ
ズル側に開口し、基端部に空気入口を有する管状通路1
6を設けた。
A spiral baffle 12 is provided in an annular passage along the outer circumference of the heater of the fuel heater. Further, on the outer peripheral side of the fuel heater, a tubular passage 1 having a tip opening toward the nozzle side of the fuel heater and an air inlet at the base end portion 1
6 is provided.

【0007】そしてさらに、上記管状通路16内にスワ
ラー17を設け、またヒータは電熱シースヒータ11あ
るいは燃焼ガスヒータ18が用いられる。そして燃焼ガ
スヒータである場合、これを折り返して2重管構造にす
る。
Further, a swirler 17 is provided in the tubular passage 16, and an electric sheath heater 11 or a combustion gas heater 18 is used as a heater. If it is a combustion gas heater, it is folded back to form a double tube structure.

【0008】[0008]

【作 用】燃料加熱器の燃料投入管10内に流入した
燃料は、この燃料投入管10を通る間にヒータ11,1
8にて加熱されて気体となってベンチュリー体3のスロ
ート部4に噴出され、この気体となった燃料はベンチュ
リー体3内で空気と混合されると共に加速されて燃焼室
1内へ流入され、燃焼室1内で着火燃焼される。
[Operation] The fuel flowing into the fuel input pipe 10 of the fuel heater is heated by the heaters 11, 1 while passing through the fuel input pipe 10.
8 is heated to become a gas and is jetted out to the throat portion 4 of the Venturi body 3, and the gasified fuel is mixed with air in the Venturi body 3 and is accelerated and flowed into the combustion chamber 1. Ignition and combustion are performed in the combustion chamber 1.

【0009】[0009]

【実 施 例】本発明の実施例を図面に基づいて説明す
る。図中1は燃焼室であり、この燃焼室1の一側部に燃
焼加熱混合器2が接続してあると共に点火棒1aが設け
てある。この燃料加熱混合器2は、一端を燃焼室1に開
口して接続したベンチュリー体3と、このベンチュリー
体3のスロート部4に空気と混合した燃料を上記燃焼室
1の方向へ向けて供給する燃料加熱器5,5a,5bと
からなっている。ベンチュリー体3のスロート部4より
上流側に一次空気が流入する空気流入管6が接続されて
いる。また上記燃焼室1の一側部には上記燃料加熱混合
器2のベンチュリー体3を囲繞して二次空気室7が設け
てあり、この二次空気室7は二次空気出口孔8を介して
燃焼室1に連通されている。9は二次空気流入管であ
る。
EXAMPLES Examples of the present invention will be described with reference to the drawings. In the figure, reference numeral 1 denotes a combustion chamber. A combustion heating mixer 2 is connected to one side of the combustion chamber 1 and an ignition rod 1a is provided. The fuel heating mixer 2 supplies a fuel mixed with air to a venturi body 3 having one end opened and connected to the combustion chamber 1 and a throat portion 4 of the venturi body 3 toward the combustion chamber 1. It is composed of fuel heaters 5, 5a and 5b. An air inflow pipe 6 through which the primary air flows is connected to the upstream side of the throat portion 4 of the venturi body 3. A secondary air chamber 7 is provided at one side of the combustion chamber 1 so as to surround the venturi body 3 of the fuel heating mixer 2. The secondary air chamber 7 is provided with a secondary air outlet hole 8 through the secondary air outlet hole 8. Is communicated with the combustion chamber 1. 9 is a secondary air inflow pipe.

【0010】次に上記燃料加熱器5,5a,5bを図
1、図2、図3にて示したそれぞれ異なる実施例におい
て説明する。図1にて示される燃料加熱器5は、先端を
ノズル状にした燃料投入管10の軸心部に棒状の電熱シ
ースヒータ11に同心状に配置した構成となっている。
そして電熱シースヒータ11と燃料投入管10とで構成
される環状の空間にはバッフル12が螺旋状に設けてあ
り、上記燃料投入管10の先端は上記したように、ベン
チュリー体3のスロート部に、燃焼室1の方向に向けて
開口しており、またこれの基端部に燃料供給管13が接
続されている。
Next, the fuel heaters 5, 5a and 5b will be described with reference to different embodiments shown in FIGS. 1, 2 and 3. The fuel heater 5 shown in FIG. 1 has a configuration in which a rod-shaped electrothermal sheath heater 11 is concentrically arranged at the axial center of a fuel injection pipe 10 having a nozzle-shaped tip.
A baffle 12 is spirally provided in an annular space formed by the electric heat sheath heater 11 and the fuel injection pipe 10, and the tip of the fuel injection pipe 10 is, as described above, in the throat portion of the venturi body 3. It opens toward the combustion chamber 1, and a fuel supply pipe 13 is connected to the base end portion of the opening.

【0011】この構成では、電熱ヒースヒータ11を加
熱した状態で燃料供給管13より液体燃料を供給するこ
とにより、この液体燃料はバッフル12に案内されて電
熱シースヒータ11の外周に沿って螺旋状に流れる。こ
の間にこの液体燃料は電熱シースヒータ11にて加熱さ
れて気化されると共に、この気化に伴う体積膨脹により
流速が早くなる。そしてこのときの燃料投入管10の投
入経路長さを、燃料供給量、電熱シースヒータ11から
受ける熱量を勘案した所定の長さにしておくことによ
り、液体燃料は燃料投入管10より完全に気体状になっ
て噴出される。
In this structure, liquid fuel is supplied from the fuel supply pipe 13 while the electrothermal heat heater 11 is heated, and the liquid fuel is guided by the baffle 12 and spirally flows along the outer periphery of the electrothermal sheath heater 11. . During this period, the liquid fuel is heated by the electrothermal sheath heater 11 and vaporized, and the flow velocity is increased due to the volume expansion accompanying the vaporization. Then, the length of the charging path of the fuel charging pipe 10 at this time is set to a predetermined length in consideration of the fuel supply amount and the amount of heat received from the electrothermal sheath heater 11, so that the liquid fuel is completely gaseous from the fuel charging pipe 10. It is spouted.

【0012】燃料投入管10より気体状になって噴出さ
れた燃料はベンチュリー体3のスロート部4にて加速さ
れると共に、ベンチュリー体3の空気入口管6より供給
された一次空気と混合されて燃焼室1に流入し、ここで
点火棒1aにて点火されて燃焼される。このとき、燃焼
室1の上流側端部には二次空気室7に連通した二次空気
出口孔8より二次空気が供給されて、この燃焼室1内で
の上記燃焼が良好に行なわれ、所定温度の燃焼ガスが得
られる。
The fuel jetted in a gaseous state from the fuel injection pipe 10 is accelerated in the throat portion 4 of the venturi body 3 and mixed with the primary air supplied from the air inlet pipe 6 of the venturi body 3. It flows into the combustion chamber 1, where it is ignited by the ignition rod 1a and burned. At this time, secondary air is supplied to the upstream end of the combustion chamber 1 from the secondary air outlet hole 8 communicating with the secondary air chamber 7, and the above combustion in the combustion chamber 1 is favorably performed. A combustion gas having a predetermined temperature can be obtained.

【0013】この場合、理論燃焼温度は1700〜17
50℃位、すなわち、空気過剰率(燃焼用空気量/理論
燃焼空気量=1.4位で、火炎は継続して燃焼可能であ
る。そしてこの温度での燃焼の場合、NOx は酸素ゼロ
%換算で25ppm位となる。なお上記実施例におい
て、燃料投入管10と電熱シースヒータ11との間の環
状の空間には、必ずしもバッフル12を介装することな
く、環状の空間のままであってもよい。
In this case, the theoretical combustion temperature is 1700 to 17
At about 50 ° C, that is, the excess air ratio (combustion air amount / theoretical combustion air amount = 1.4), the flame can continue to burn. And in the case of combustion at this temperature, NO x is zero oxygen. In the above embodiment, the baffle 12 is not necessarily provided in the annular space between the fuel injection pipe 10 and the electrothermal sheath heater 11, and the annular space remains as it is. Good.

【0014】図2にて示される燃料加熱混合器5aは、
上記図1にて示した燃料加熱混合器5に、これの燃料投
入管10の外側を囲繞する空気案内管14を設けた構成
となっている。そしてこの空気案内管14の先端は燃料
投入管10の先端よりわずかに突出させて開口し、基端
部には空気流入管15が接続してあり、さらに、空気案
内管14の内側に構成される管状流路16の出口側にス
ワラー17が設けてある。
The fuel heating mixer 5a shown in FIG.
The fuel heating mixer 5 shown in FIG. 1 is provided with an air guide tube 14 surrounding the outside of the fuel injection tube 10. The tip of the air guide tube 14 is slightly protruded from the tip of the fuel injection tube 10 to open, the air inflow tube 15 is connected to the base end, and the inside of the air guide tube 14 is formed. A swirler 17 is provided on the outlet side of the tubular flow channel 16 that is formed.

【0015】この構成では、空気案内管14の先端か
ら、他の一次空気が燃料投入管10の先端側を包み込む
ようにして渦巻き状に供給される。従って、燃料投入管
10より気体状になって噴出される燃料は、上記空気案
内管14より噴出される他の一次空気にて充分に分散、
攪拌されて燃焼室1へ流入される。
In this structure, the other primary air is spirally supplied from the tip of the air guide tube 14 so as to wrap around the tip side of the fuel injection tube 10. Therefore, the fuel jetted in a gaseous state from the fuel injection pipe 10 is sufficiently dispersed in the other primary air jetted from the air guide pipe 14,
It is stirred and flowed into the combustion chamber 1.

【0016】図3にして示される燃料加熱混合器5bは
燃料の加熱手段の構成を変えたもので、燃料投入管10
aの内側に、2重管構成にした燃焼ガスヒータ18が配
置されている。この燃焼ガスヒータ18は、燃焼ガス流
入口に接続した内管19と、この内管19の先端部から
折り返し環状に形成した外管20とからなっていて、内
管19に流入した燃焼ガスはこれの先端部が折り返され
て外管20を流れ、これの終端部に設けられた出口21
より排出されるようになっている。この燃焼ガスヒータ
18と上記燃料投入管10aとの間に構成される環状の
空間には螺旋状のバッフル12aが設けてある。
The fuel heating mixer 5b shown in FIG. 3 has a different structure of the fuel heating means.
A combustion gas heater 18 having a double tube structure is arranged inside a. The combustion gas heater 18 is composed of an inner pipe 19 connected to the combustion gas inlet and an outer pipe 20 formed in a loop shape from the tip of the inner pipe 19. The combustion gas flowing into the inner pipe 19 is The tip of the tube is folded back and flows through the outer tube 20, and the outlet 21 provided at the terminal end of the tube
It is being discharged more. A spiral baffle 12a is provided in an annular space formed between the combustion gas heater 18 and the fuel injection pipe 10a.

【0017】[0017]

【発明の効果】本発明によれば、液体燃料用の燃焼器で
も、空気を予熱することなく、NOxの発生を抑制で
き、未燃焼物が無い高温の燃焼ガスを得ることができ
る。
According to the present invention, even in a combustor for liquid fuel, generation of NO x can be suppressed without preheating air, and high-temperature combustion gas free of unburned substances can be obtained.

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

【図1】本発明の実施例を示す断面図である。FIG. 1 is a sectional view showing an embodiment of the present invention.

【図2】本発明の他の実施例を示す断面図である。FIG. 2 is a sectional view showing another embodiment of the present invention.

【図3】本発明の他の実施例を示す断面図である。FIG. 3 is a sectional view showing another embodiment of the present invention.

【符号の説明】[Explanation of symbols]

1…燃焼室、1a…着火棒、2…燃料加熱混合器、3…
ベンチュリー体、4…スロート部、5,5a,5b…燃
料混合器、6,15…空気流入管、7…二次空気室、8
…二次空気出口孔、9…二次空気流入管、10,10a
…燃料投入管、11…電熱シースヒータ、12,12a
…バッフル、13…燃料供給管、14…空気案内管、1
6…管状流路、17…スワラー、18…燃焼ガスヒー
タ、19…内管、20…外管、21…出口。
1 ... Combustion chamber, 1a ... Ignition rod, 2 ... Fuel heating mixer, 3 ...
Venturi body, 4 ... Throat part, 5, 5a, 5b ... Fuel mixer, 6, 15 ... Air inflow pipe, 7 ... Secondary air chamber, 8
... Secondary air outlet hole, 9 ... Secondary air inflow pipe 10,10a
... Fuel injection pipe, 11 ... Electrothermal sheath heater, 12, 12a
... baffle, 13 ... fuel supply pipe, 14 ... air guide pipe, 1
6 ... Tubular flow path, 17 ... Swirler, 18 ... Combustion gas heater, 19 ... Inner tube, 20 ... Outer tube, 21 ... Exit.

Claims (7)

【特許請求の範囲】[Claims] 【請求項1】 燃焼室1の一側部に、燃料を加熱すると
共に、空気と混合して燃焼室1へ吹き込む燃料加熱混合
器を接続した燃焼器において、上記燃料加熱混合器を、
中間部にスロート部4を有し、このスロート部4より上
流側に空気流入管6を接続したベンチュリー体3と、先
端をノズル状にした燃料投入管10内に棒状のヒータを
内装し、このヒータの外周に沿う環状の通路の一方に燃
料供給管13を接続し、先端を上記ベンチュリー体3の
スロート部4に開口してなる燃料加熱器とにて構成した
ことを特徴とする燃焼器。
1. A combustor in which a fuel heating mixer that heats fuel and mixes with air and blows into the combustion chamber 1 is connected to one side of the combustion chamber 1, wherein the fuel heating mixer is
A venturi body 3 having a throat portion 4 in an intermediate portion and an air inflow pipe 6 connected upstream of the throat portion 4 and a fuel injection pipe 10 having a nozzle-like tip are internally provided with a rod-shaped heater. A combustor characterized in that a fuel supply pipe (13) is connected to one of the annular passages along the outer circumference of the heater, and a fuel heater is formed by opening the tip to the throat portion (4) of the venturi body (3).
【請求項2】 燃料加熱器のヒータの外周に沿う環状の
通路内に螺旋状のバッフル12を設けたことを特徴とす
る請求項1記載の燃焼器。
2. The combustor according to claim 1, wherein a spiral baffle 12 is provided in an annular passage along the outer periphery of the heater of the fuel heater.
【請求項3】 請求項1記載の燃焼器の燃料加熱器の外
周側に、先端が燃料加熱器のノズル側に開口し、基端部
に空気流入管を接続した管状通路16を設けたことを特
徴とする燃焼器。
3. A tubular passage 16 is provided on the outer peripheral side of the fuel heater of the combustor according to claim 1, the tip of which is open to the nozzle side of the fuel heater, and the base end portion of which is connected to an air inflow pipe. Combustor characterized by.
【請求項4】 管状通路16内にスワラー17を設けた
ことを特徴とする請求項3記載の燃焼器。
4. The combustor according to claim 3, wherein a swirler 17 is provided in the tubular passage 16.
【請求項5】 ヒータが電熱シースヒータ11であるこ
とを特徴とする請求項1,2,3または4記載の燃焼
器。
5. The combustor according to claim 1, 2, 3 or 4, wherein the heater is an electrothermal sheath heater 11.
【請求項6】 ヒータが燃焼ガスヒータ18であること
を特徴とする請求項1,2,3または4記載の燃焼器。
6. The combustor according to claim 1, 2, 3 or 4, wherein the heater is a combustion gas heater 18.
【請求項7】 燃焼ガスヒータを折り返えし2重管構造
としたことを特徴とする請求項6記載の燃焼器。
7. The combustor according to claim 6, wherein the combustion gas heater is folded back to have a double tube structure.
JP01813294A 1994-02-15 1994-02-15 Combustor Expired - Fee Related JP3407228B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP01813294A JP3407228B2 (en) 1994-02-15 1994-02-15 Combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP01813294A JP3407228B2 (en) 1994-02-15 1994-02-15 Combustor

Publications (2)

Publication Number Publication Date
JPH07225010A true JPH07225010A (en) 1995-08-22
JP3407228B2 JP3407228B2 (en) 2003-05-19

Family

ID=11963085

Family Applications (1)

Application Number Title Priority Date Filing Date
JP01813294A Expired - Fee Related JP3407228B2 (en) 1994-02-15 1994-02-15 Combustor

Country Status (1)

Country Link
JP (1) JP3407228B2 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103438572A (en) * 2013-09-06 2013-12-11 洛阳沃达机械技术开发有限公司 Combustion-type gas preheater
JP5623676B1 (en) * 2014-02-12 2014-11-12 カンケンテクノ株式会社 Exhaust gas treatment burner and exhaust gas treatment apparatus using the burner
CN105983243A (en) * 2015-07-10 2016-10-05 李保春 Liquid oxygen and fuel oil mixing device
WO2017183510A1 (en) * 2016-04-22 2017-10-26 住友精化株式会社 Liquefied natural gas vaporizer, natural gas fuel supply system provided with same, and method for operating natural gas fuel supply system

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103438572A (en) * 2013-09-06 2013-12-11 洛阳沃达机械技术开发有限公司 Combustion-type gas preheater
JP5623676B1 (en) * 2014-02-12 2014-11-12 カンケンテクノ株式会社 Exhaust gas treatment burner and exhaust gas treatment apparatus using the burner
WO2015121890A1 (en) * 2014-02-12 2015-08-20 カンケンテクノ株式会社 Exhaust gas treatment burner and exhaust gas treatment device using same
TWI607184B (en) * 2014-02-12 2017-12-01 Kanken Techno Co Ltd Burner for exhaust gas treatment, and exhaust gas treatment device using the burner
CN105983243A (en) * 2015-07-10 2016-10-05 李保春 Liquid oxygen and fuel oil mixing device
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