Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPH0718549B2 - Direct ignition burner device for boiler - Google Patents
[go: Go Back, main page]

JPH0718549B2 - Direct ignition burner device for boiler - Google Patents

Direct ignition burner device for boiler

Info

Publication number
JPH0718549B2
JPH0718549B2 JP59240575A JP24057584A JPH0718549B2 JP H0718549 B2 JPH0718549 B2 JP H0718549B2 JP 59240575 A JP59240575 A JP 59240575A JP 24057584 A JP24057584 A JP 24057584A JP H0718549 B2 JPH0718549 B2 JP H0718549B2
Authority
JP
Japan
Prior art keywords
fuel
ignition
burner
hole
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 - Fee Related
Application number
JP59240575A
Other languages
Japanese (ja)
Other versions
JPS61119918A (en
Inventor
俊一 津村
Original Assignee
バブコツク日立株式会社
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 バブコツク日立株式会社 filed Critical バブコツク日立株式会社
Priority to JP59240575A priority Critical patent/JPH0718549B2/en
Publication of JPS61119918A publication Critical patent/JPS61119918A/en
Publication of JPH0718549B2 publication Critical patent/JPH0718549B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23QIGNITION; EXTINGUISHING-DEVICES
    • F23Q3/00Igniters using electrically-produced sparks
    • F23Q3/008Structurally associated with fluid-fuel burners

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Description

【発明の詳細な説明】 <産業上の利用分野> 本発明はバーナ装置に係り、特に点火ミスを防止し得る
ボイラ用バーナ装置に関する。
Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a burner device, and more particularly to a burner device for a boiler that can prevent misfire.

<従来の技術及びその問題点> バーナの着火法には直接点火方式と点火バーナを用いる
方式があるが、直接点火方式は通常スパークを用いるた
め、着火領域が狭くても点火可能な家庭用等の小型バー
ナにのみ適用され一般の工業用バーナでは点火位置設定
が困難で点火に失敗すると一度に多量のガスが流出爆発
の危険性があるためスパーク式を用いず点火バーナ方式
が採用されている。
<Prior art and its problems> There are two types of ignition methods for a burner, a direct ignition method and a method using an ignition burner. However, since the direct ignition method usually uses a spark, it can be ignited even in a narrow ignition area for household use. It is applied only to small burners of general type and it is difficult to set the ignition position in a general industrial burner, and if ignition fails, a large amount of gas may flow out at one time and there is a risk of explosion, so the ignition burner method is used instead of the spark type. .

第1図にボイラ用ガスバーナの点火バーナと主バーナの
配置の一例を示す。バーナを点火する際には先ず点火バ
ーナ2の燃料パイプに燃料を流し、この燃料にパルスイ
グナイタ等の点火装置で点火し、点火用の火炎を形成す
る。次に主バーナ用燃料弁を開いて主バーナ用燃料ノズ
ル3から燃料を噴射させると、まず点火用火災に近い部
分の燃料ノズルから噴射した燃料が着火し、この火災が
次々に他のノズルからの噴射燃料に移り、全バーナの点
火が完了する。第2図に点火バーナの先端部の一例を示
す。点火用の燃料は点火バーナ燃料パイプ6によつて点
火バーナの先端部に導かれる。点火装置のパルスイグナ
イタ7の点火プラグ8は点火時には図に示す様に先端が
燃料流中に突出される様になつているが、点火時以外は
パルスイグナイタ7の外筒の中に収納されている。燃料
流が点火バーナの先端部に達する時期に合せて、パルス
イグナイタ7により点火プラグ8の先端にパルスアーク
(6〜7パルス/秒)を発生させ、燃料と空気の混合流
に着火させる。ところでパルスアークは点火プラグ8の
先端部とアースの間に発生するわけであるが、その発生
位置が局在化するため、燃料流に確実に着火させるには
点火プラグ8の先端位置を微調整する必要がある。更に
燃料流の圧力変化等によりアーク発生位置と燃料流の通
過位置にずれが生じると着火しないことがある。又、点
火プラグ先端の焼損を防止するため、点火プラグは点火
時のみ突出させ、点火時以外は引抜く事が必要であるた
め、これらの駆動装置を必要とするが、駆動装置の故障
は直ちに点火不能につながる可能性がある。一方点火プ
ラグ8の寿命は金属の劣化等の問題から、200〜300時間
程度と非常に短かいのが現状である。さらに点火プラグ
8の放電により、火災検出器が誤作動する場合もある。
FIG. 1 shows an example of the arrangement of the ignition burner and the main burner of the boiler gas burner. When igniting the burner, first, fuel is flown through the fuel pipe of the ignition burner 2, and this fuel is ignited by an ignition device such as a pulse igniter to form a flame for ignition. Next, when the fuel valve for the main burner is opened to inject fuel from the fuel nozzle 3 for the main burner, the fuel injected from the fuel nozzle near the ignition fire is ignited first, and this fire is successively emitted from other nozzles. Then, the injection fuel is changed to the injection fuel, and the ignition of all burners is completed. FIG. 2 shows an example of the tip of the ignition burner. The fuel for ignition is guided to the tip of the ignition burner by the ignition burner fuel pipe 6. The ignition plug 8 of the pulse igniter 7 of the ignition device has a tip projecting into the fuel flow as shown in the figure at the time of ignition, but is housed in the outer cylinder of the pulse igniter 7 except at the time of ignition. There is. A pulse arc (6 to 7 pulses / sec) is generated at the tip of the spark plug 8 by the pulse igniter 7 at the timing when the fuel flow reaches the tip of the ignition burner, and the mixed flow of fuel and air is ignited. By the way, the pulse arc is generated between the tip of the spark plug 8 and the ground, but since the position is localized, the tip position of the spark plug 8 is finely adjusted in order to reliably ignite the fuel flow. There is a need to. Further, if the arc generation position and the fuel flow passage position deviate from each other due to the pressure change of the fuel flow, ignition may not occur. Also, in order to prevent the tip of the spark plug from burning out, it is necessary to project the spark plug only during ignition and to pull it out except during ignition. It may lead to ignition failure. On the other hand, the life of the spark plug 8 is currently as short as about 200 to 300 hours due to problems such as metal deterioration. Further, the fire detector may malfunction due to the discharge of the spark plug 8.

以上のように従来の点火バーナを用いる方式には、種々
の技術的問題点があり点火ミスは実際にしばしば経験さ
れている。
As described above, the conventional system using the ignition burner has various technical problems, and the misfire is often actually experienced.

点火ミスが生じた場合には、装置の爆発や火災あるいは
人的災害につながる虞れがあり、燃焼装置用の点火バー
ナの信頼性向上は、特にボイラを坦う工業において非常
に重要な課題とされている。
If a misfire occurs, it may lead to an explosion or fire of the equipment or a human disaster. Improving the reliability of the ignition burner for the combustion equipment is a very important issue especially in the boiler industry. Has been done.

<本発明の目的> 本発明の目的は、上記した従来技術の欠点をなくし、点
火ミスがなく、且つ構造が大巾に簡略化されたガスバー
ナ装置を提供するにある。
<Object of the Present Invention> An object of the present invention is to provide a gas burner device which eliminates the above-mentioned drawbacks of the prior art, has no ignition error, and has a greatly simplified structure.

<問題点を解決するための手段> 要するにこの発明は、主バーナの周囲より与えられる空
気と燃料とを混合する予混合着火室からの混合気体に発
熱ヒータで着火させ燃料用孔が設けられた燃料ノズルを
有する主バーナに着火させるバーナ用直接点火型バーナ
装置において、該発熱ヒータをセラミツクスヒータと
し、火炉側に開口し底面に空気孔をもつ茶筒蓋状フレー
ムコンテイナに燃料用主バーナノズルを挿通接続して予
混合着火室を形成し、前記コンテイナの火炉側開口は前
記燃料用孔直前に位置し、この予混合着火室に気体燃料
を供給する点火用燃料孔を燃料用主バーナノズル壁に設
けたことを特徴とするボイラ用直接点火型バーナ装置で
ある。
<Means for Solving Problems> In short, according to the present invention, the gas mixture from the premixing ignition chamber for mixing the air and the fuel supplied from the periphery of the main burner is ignited by the heat generating heater and the fuel hole is provided. In a direct ignition burner device for a burner that ignites a main burner having a fuel nozzle, the heating heater is a ceramics heater, and the main burner nozzle for fuel is inserted into a tea-cup-shaped frame container having an air hole on the bottom side and an air hole on the bottom side. The premixed ignition chamber is connected to form a premixed ignition chamber, the furnace side opening of the container is located immediately before the fuel hole, and an ignition fuel hole for supplying gaseous fuel to the premixed ignition chamber is provided in the fuel main burner nozzle wall. It is a direct ignition type burner device for a boiler characterized by the above.

<実施例> 第4図は本発明の実施例を示し、主バーナ用燃料ノズル
3の先端部近傍に対しては、中心軸線をこのノズル3と
ほぼ等しくするようにフレームコンテイナ17が形成して
ある。10はこのフレームコンテイナ17に取り付けた点火
装置であり、後述する如くセラミツクスヒータとしてお
く。21はこの点火装置10を覆うように形成した予混合着
火室、19はこの予混合着火室21に空気を供給する空気
孔、18は点火装置支持部、20は予混合着火室21に燃料を
供給する燃料孔、14は主孔、15は副孔、16はフレームコ
ンテイナ17に形成した空気孔である。
<Embodiment> FIG. 4 shows an embodiment of the present invention. A frame container 17 is formed near the tip of the main burner fuel nozzle 3 so that the central axis of the fuel nozzle 3 is substantially the same as that of the nozzle 3. There is. Reference numeral 10 denotes an ignition device attached to the frame container 17, which is a ceramic heater as described later. 21 is a premix ignition chamber formed to cover the ignition device 10, 19 is an air hole for supplying air to the premix ignition chamber 21, 18 is an igniter support portion, 20 is fuel for the premix ignition chamber 21 Fuel holes to be supplied, 14 is a main hole, 15 is a sub hole, and 16 is an air hole formed in the frame container 17.

この装置の作動につき第3図も含めて説明する。The operation of this device will be described with reference to FIG.

例えば、上述のバーナを燃料量300Nm3/hのガス燃焼装置
とした場合、バーナ元弁11及びバーナ入口弁26を介して
送られた燃料ガス(以下ブタンガスを例として説明す
る。)は主バーナ用燃料ノズル3より主孔14及び副孔15
を通つて炉内に噴射され、同時に点火用燃焼孔20を通つ
て予混合着火室21に燃料が噴射される。
For example, when the above burner is a gas combustion device with a fuel amount of 300 Nm 3 / h, the fuel gas sent through the burner source valve 11 and the burner inlet valve 26 (hereinafter, butane gas will be described as an example) is the main burner. From fuel nozzle 3 for main hole 14 and sub hole 15
The fuel is injected into the furnace through the combustion hole for ignition 20 and at the same time, the fuel is injected into the premix ignition chamber 21 through the combustion hole 20 for ignition.

また燃焼用空気はエアレジスタ1からインペラ4及びバ
ーナスロート5部へ供給され(第1図参照)、同時に点
火用空気孔19を経由して予混合着火室21に供給される。
Combustion air is supplied from the air register 1 to the impeller 4 and the burner throat 5 (see FIG. 1), and at the same time, supplied to the premix ignition chamber 21 via the ignition air hole 19.

なお、予混合着火室21における空気比は、着火燃焼を確
実に行せるため空気比1〜1.5に設定するのが望ましい
が、空気比1.1に設定した場合点火燃料用として消費す
る燃料量は0.01〜0.1Nm3/h程度で十分である。
The air ratio in the premixing ignition chamber 21 is preferably set to an air ratio of 1 to 1.5 in order to ensure ignition combustion, but when the air ratio is set to 1.1, the amount of fuel consumed for ignition fuel is 0.01. Approximately 0.1 Nm 3 / h is sufficient.

次にこの装置において、燃料ガス圧が7000mmHg、燃焼用
空気の軸方向速度10m/秒、点火用燃料量0.1Nm3/hとし
て、予混合着火室21内の空気比を1.1と設定するために
必要な空気孔19及び燃料孔20の孔径寸法を以下に記述す
る。
Next, in this device, the fuel gas pressure is 7000 mmHg, the axial velocity of combustion air is 10 m / sec, the ignition fuel amount is 0.1 Nm 3 / h, and the air ratio in the premix ignition chamber 21 is set to 1.1. The required hole diameter dimensions of the air hole 19 and the fuel hole 20 are described below.

まずガス圧7,000mmHgで、0.1Nm3/hの燃料量を流すのに
必要な燃料供給孔面積はブタンガスの場合約0.1mmとな
る。またこの時のガス流速は110m/秒となる。さて空気
比1.1にするには、ブタンガスの場合約24倍の空気量が
必要であるが、空気孔19を通過する空気流速を10m/秒と
すると、空気孔19の空気通過面積は約0.7cm2である。
First, at a gas pressure of 7,000 mmHg, the fuel supply hole area required to flow a fuel amount of 0.1 Nm 3 / h is about 0.1 mm for butane gas. The gas flow velocity at this time is 110 m / sec. In the case of butane gas, about 24 times the amount of air is required to achieve an air ratio of 1.1, but if the air flow rate through the air holes 19 is 10 m / sec, the air passage area of the air holes 19 is about 0.7 cm. Is 2 .

予混合着火室21内の燃料及び空気を適切に予混合するた
めに、第4図(a)では空気孔19に対する燃料孔20の噴
射角θを90゜としたが、燃料孔20の噴射角θは下記の範
囲であればよい。
In order to properly premix the fuel and air in the premix ignition chamber 21, the injection angle θ of the fuel hole 20 with respect to the air hole 19 is 90 ° in FIG. 4 (a). θ may be in the following range.

ここでt:予混合着火室の半径方向高さ、 l:予混合着火室の軸方向高さ、 通常燃料ガスの流速は80〜150m/秒と極めて高いが、予
混合着火室21に噴射された燃料は、該着火室21の側壁等
に衝突することにより減速し、その過程で空気と適切に
予混合して流速1〜5m/秒程度の着火しやすい流速にな
る。
Where t: radial height of the premixed ignition chamber, l: axial height of the premixed ignition chamber, the flow velocity of the fuel gas is usually as high as 80 to 150 m / sec, but injected into the premixed ignition chamber 21. The fuel is decelerated by colliding with the side wall of the ignition chamber 21 and the like, and is appropriately premixed with air in the process to have a flow velocity of about 1 to 5 m / sec, which facilitates ignition.

一方、制御装置12によりバーナ元弁11及びバーナ入口弁
26を開にした後、一定時間の遅れを経て燃料ガスと空気
とが良好に混合した時点で制御装置12より電源装置13に
通電開始信号を送る。この信号により電源装置13により
予混合着火室21に設置された着火装置10(以下「セラミ
ツクスヒータ」で説明する)に電流を印加する。ここで
予混合着火室21は、燃料と燃焼用空気が理論空気比以上
に予混合された低流速領域であるので、ガス燃料の場合
2ジュール程度のエネルギーで着火可能であり、セラミ
ツクスヒータ10の発熱量を2〜100Wとすれば確実に着火
する。従つてヒータに一定量以上の電流印加をすること
により予混合着火室21の出口部に火炎が形成され、次に
これが副孔及び主孔から噴射される燃料に着火し、この
火炎が次々に他のノズルからの噴射燃料に着火し、バー
ナ装置全体の点火が完了する。
On the other hand, the controller 12 controls the burner source valve 11 and the burner inlet valve.
After opening 26, the control device 12 sends an energization start signal to the power supply device 13 when the fuel gas and the air are mixed well after a certain time delay. By this signal, a current is applied by the power supply device 13 to the ignition device 10 (hereinafter described as "ceramic heater") installed in the premix ignition chamber 21. Here, since the premix ignition chamber 21 is a low flow velocity region in which the fuel and the combustion air are premixed at a ratio equal to or higher than the theoretical air ratio, in the case of gas fuel, it is possible to ignite with energy of about 2 Joules, and the ceramic heater 10 If the amount of heat generation is set to 2 to 100 W, it will ignite reliably. Accordingly, by applying a current of a certain amount or more to the heater, a flame is formed at the exit portion of the premix ignition chamber 21, which then ignites the fuel injected from the auxiliary hole and the main hole, and this flame is successively generated. The fuel injected from the other nozzles is ignited, and the ignition of the entire burner device is completed.

第5図にセラミツクスヒータの構造を示す。導電部22は
両側壁と、ヒータ中央部の長手方向に形成した絶縁部23
で分離されており、ヒータ先端の厚さを薄くして電気抵
抗を高くした赤熱部24でこの導電部22は合体している。
従つて電極部25に電圧を印加すると、電流は導電部を流
れ、先端の厚さを薄くした赤熱部24で赤熱することにな
る。印加電圧は直流でも交流でも良く又先端を赤熱(約
900℃以上)させるに必要な印加電圧値は、赤熱部24の
抵抗値長さ及び断面積により設定できる。
FIG. 5 shows the structure of the ceramic heater. The conductive portion 22 is formed on both side walls and the insulating portion 23 formed in the longitudinal direction of the central portion of the heater.
The conductive portion 22 is united by the red heating portion 24 in which the thickness of the heater tip is reduced to increase the electric resistance.
Therefore, when a voltage is applied to the electrode portion 25, a current flows through the conductive portion, and the red heating portion 24 having the thinned tip end glows red. The applied voltage may be DC or AC, and the tip may glow red (approx.
The applied voltage value required to make it 900 ° C. or higher) can be set by the resistance value length and cross-sectional area of the red heating part 24.

従来のパルスイグナイタの印加電圧値は1KV以上の高電
圧であるのに対し該セラミツクスヒータでは高々20V程
度でよく、且つ交流電源でもよいため防爆構造が不要で
あり、電源装置が極めて簡易化される。
The applied voltage value of the conventional pulse igniter is a high voltage of 1 KV or more, whereas the ceramic heater may have a maximum of about 20 V, and since it may be an AC power supply, an explosion-proof structure is not required, and the power supply device is extremely simplified. .

尚ヒータ設置部はエアレジスタ1からの空気流で100〜2
00℃に冷却されるため、耐熱構造にする必要はない。さ
らにセラミツクスヒータは本来耐熱温度1200〜1300℃と
耐熱性に優れており、点火後も噴射口周辺に配置したま
まで良く、パルスイグナイタの点火プラグに相当するセ
ラミツクスヒータ部を突出させたり、引き抜いたりする
などの駆動機構を必要とせずまた寿命も長い。
In addition, the heater installation part is 100 to 2 by the air flow from the air register 1.
Since it is cooled to 00 ℃, it is not necessary to have a heat resistant structure. Furthermore, the ceramic heater has excellent heat resistance of 1200 to 1300 ° C originally, and it can be left around the injection port even after ignition, and the ceramic heater part corresponding to the ignition plug of the pulse igniter can be projected or pulled out. It does not require a driving mechanism such as a screw and has a long life.

<効果> 本発明を実施することにより、点火ミスを起こすことな
くバーナ装置の直接点火が可能となり、専用の点火バー
ナが不用となつて構造が大幅に簡素化でき、装置の軽量
化、低コスト化を達成することができる。
<Effects> By implementing the present invention, it is possible to directly ignite the burner device without causing an ignition error, the dedicated ignition burner is not required, and the structure can be greatly simplified, the weight of the device can be reduced, and the cost can be reduced. Can be achieved.

また点火用の電源の電圧を大幅に低下させることがで
き、かつ点火部の冷却が良好でしかも点火部自体が耐熱
性を有しているため、点火部の出し入れ構造が不用とな
つて装置の信頼性を高めることができる。
In addition, the voltage of the ignition power source can be greatly reduced, the ignition part is cooled well, and the ignition part itself has heat resistance. The reliability can be increased.

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

第1図(a)は従来のバーナ装置の縦断面図、同(b)
は正面図、第2図は点火バーナ先端部縦断面図、第3図
は本発明のバーナ装置の燃料供給系統図、第4図(a)
は本発明の実施例を示すバーナノズルの断面図、(b)
はノズル正面図、第5図はセラミツクスヒータの拡大し
た斜視図である。 10……セラミツクスヒータ 20……点火用燃料孔 21……予混合着火室
FIG. 1 (a) is a longitudinal sectional view of a conventional burner device, and FIG. 1 (b).
Is a front view, FIG. 2 is a vertical sectional view of the tip of the ignition burner, FIG. 3 is a fuel supply system diagram of the burner device of the present invention, and FIG. 4 (a).
Is a sectional view of a burner nozzle showing an embodiment of the present invention, (b)
Is a nozzle front view, and FIG. 5 is an enlarged perspective view of a ceramic heater. 10 …… Ceramic heater 20 …… Ignition fuel hole 21 …… Premix ignition chamber

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】主バーナの周囲より与えられる空気と燃料
とを混合する予混合着火室からの混合気体に発熱ヒータ
で着火させ燃料用孔が設けられた燃料ノズルを有する主
バーナに着火させるバーナ用直接点火型バーナ装置にお
いて、該発熱ヒータをセラミツクスヒータとし、火炉側
に開口し底面に空気孔をもつ茶筒蓋状フレームコンテイ
ナに燃料用主バーナノズルを挿通接続して予混合着火室
を形成し、前記コンテイナの火炉側開口は前記燃料用孔
直前に位置し、この予混合着火室に気体燃料を供給する
点火用燃料孔を燃料用主バーナノズル壁に設けたことを
特徴とするボイラ用直接点火型バーナ装置。
1. A burner for igniting a mixed gas from a premixing ignition chamber, which mixes air and fuel provided around the main burner, with a heating heater to ignite a main burner having a fuel nozzle provided with a fuel hole. In the direct ignition type burner device for a vehicle, the heating heater is used as a ceramics heater, and the main burner nozzle for fuel is inserted and connected to the tea container lid-shaped frame container that has an air hole on the bottom side and opens on the furnace side to form a premix ignition chamber. A direct ignition for a boiler characterized in that a furnace side opening of the container is located immediately before the fuel hole, and an ignition fuel hole for supplying gaseous fuel to the premixing ignition chamber is provided in a fuel main burner nozzle wall. Type burner device.
JP59240575A 1984-11-16 1984-11-16 Direct ignition burner device for boiler Expired - Fee Related JPH0718549B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59240575A JPH0718549B2 (en) 1984-11-16 1984-11-16 Direct ignition burner device for boiler

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59240575A JPH0718549B2 (en) 1984-11-16 1984-11-16 Direct ignition burner device for boiler

Publications (2)

Publication Number Publication Date
JPS61119918A JPS61119918A (en) 1986-06-07
JPH0718549B2 true JPH0718549B2 (en) 1995-03-06

Family

ID=17061559

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59240575A Expired - Fee Related JPH0718549B2 (en) 1984-11-16 1984-11-16 Direct ignition burner device for boiler

Country Status (1)

Country Link
JP (1) JPH0718549B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7958721B2 (en) 2007-06-29 2011-06-14 Caterpillar Inc. Regeneration system having integral purge and ignition device
US8484947B2 (en) 2007-03-02 2013-07-16 Caterpillar Inc. Fluid injector having purge heater

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2581208B2 (en) * 1989-03-23 1997-02-12 三菱電機株式会社 Combustion device of fuel reformer for fuel cell power generator
JPH0330059U (en) * 1989-07-31 1991-03-25
DE4138433C2 (en) * 1991-11-22 1996-03-28 Aichelin Gmbh Burners for industrial furnaces
US5513981A (en) * 1991-11-22 1996-05-07 Aichelin Gmbh Burner with variable volume combination chamber
JP2717923B2 (en) * 1993-09-29 1998-02-25 株式会社ココロ An ignition device using an ignition heater
US8499739B2 (en) 2006-08-31 2013-08-06 Caterpillar Inc. Injector having tangentially oriented purge line
US8215100B2 (en) 2007-03-02 2012-07-10 Caterpillar Inc. Regeneration device having external check valve
US8006482B2 (en) 2007-03-02 2011-08-30 Caterpillar Inc. Method of purging fluid injector by heating

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS516665Y2 (en) * 1971-02-27 1976-02-24
JPS5234433U (en) * 1975-09-03 1977-03-11
JPS58206090A (en) * 1982-05-25 1983-12-01 株式会社デンソー Ceramic heater

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8484947B2 (en) 2007-03-02 2013-07-16 Caterpillar Inc. Fluid injector having purge heater
US7958721B2 (en) 2007-06-29 2011-06-14 Caterpillar Inc. Regeneration system having integral purge and ignition device

Also Published As

Publication number Publication date
JPS61119918A (en) 1986-06-07

Similar Documents

Publication Publication Date Title
US20090165436A1 (en) Premixed, preswirled plasma-assisted pilot
CA1183075A (en) Ignition system for post-mixed burner
EP0303522B1 (en) Pulverised fuel burner
JPH01212819A (en) Fuel nozzle
JPH0718549B2 (en) Direct ignition burner device for boiler
JPH02192515A (en) Ignition system and method for post mixing burner
US6079976A (en) Structure for supply of fuel and pilot air
WO1996014540A1 (en) Pilot burner and pilot burner gas nozzle utilizing the same
JPH1068510A (en) Fuel injection gun
KR870004270A (en) Igniters for radiators
US5314329A (en) Pulse combustor ignitor system
GB2062824A (en) Method of igniting solid fuel and apparatus for use in the method
RU2169885C1 (en) Igniter
JPH08233226A (en) Premixing gas burner and its igniting method
JPS6222741Y2 (en)
JPH0740849Y2 (en) Premix burner
SU991110A1 (en) Igniter
US1349877A (en) Liquid-fuel-ignition mechanism
RU1777640C (en) Igniter
CN109162854B (en) A kind of control method of double discharge mode plasma igniter
CN114459026A (en) Electronic pulse combustion method
JPS584022Y2 (en) gas burner
SU850987A1 (en) Gas burner
JPS599012B2 (en) Ignition method and device
JP2748675B2 (en) Combustion equipment

Legal Events

Date Code Title Description
LAPS Cancellation because of no payment of annual fees