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
JP2569845B2 - Liquid fuel evaporator - Google Patents
[go: Go Back, main page]

JP2569845B2 - Liquid fuel evaporator - Google Patents

Liquid fuel evaporator

Info

Publication number
JP2569845B2
JP2569845B2 JP1302964A JP30296489A JP2569845B2 JP 2569845 B2 JP2569845 B2 JP 2569845B2 JP 1302964 A JP1302964 A JP 1302964A JP 30296489 A JP30296489 A JP 30296489A JP 2569845 B2 JP2569845 B2 JP 2569845B2
Authority
JP
Japan
Prior art keywords
liquid fuel
evaporating
air
burner
temperature 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 - Lifetime
Application number
JP1302964A
Other languages
Japanese (ja)
Other versions
JPH03164616A (en
Inventor
浩作 城出
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.)
Noritz Corp
Original Assignee
Noritz 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 Noritz Corp filed Critical Noritz Corp
Priority to JP1302964A priority Critical patent/JP2569845B2/en
Publication of JPH03164616A publication Critical patent/JPH03164616A/en
Application granted granted Critical
Publication of JP2569845B2 publication Critical patent/JP2569845B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Spray-Type Burners (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Control Of Combustion (AREA)

Description

【発明の詳細な説明】 〈産業上の利用分野〉 本発明は噴霧液体燃料を高温空気で蒸発させ、バーナ
での燃焼に供するための液体燃料蒸発装置に関する。
DETAILED DESCRIPTION OF THE INVENTION <Industrial Application Field> The present invention relates to a liquid fuel evaporator for evaporating atomized liquid fuel with high-temperature air and subjecting it to combustion in a burner.

〈従来技術とその課題〉 従来、灯油等の液体燃料を蒸発する方法として、液体
燃料の液滴を加熱した蒸発容器の内壁面等に衝突させて
蒸発を行う装置が提供されているが、これらの装置では
タール状物質が発生しやすい問題があった。このため本
出願人は本書と同日提出の出願にて、高温空気によって
微粒化した噴霧液体燃料を直接的に蒸発する装置を提供
した。この装置では液体燃料を比較的低い温度(120℃
〜250℃程度)で蒸発させることができるので、タール
状物質の発生を抑制することができる効果がある。
<Prior art and its problems> Conventionally, as a method for evaporating a liquid fuel such as kerosene, apparatuses for evaporating liquid fuel by impinging droplets of the liquid fuel on an inner wall surface or the like of a heated evaporation container are provided. However, there is a problem that tar-like substances are easily generated in the above-mentioned apparatus. To this end, the applicant has provided, in an application filed on the same date as the present specification, a device for directly evaporating atomized liquid fuel atomized by hot air. In this system, liquid fuel is heated to a relatively low temperature (120 ° C).
(About 250 ° C.), which has the effect of suppressing the generation of tar-like substances.

ところがこの高温空気による直接蒸発式の装置では、
高温空気が導入される蒸発容器は、その内部の雰囲気温
度は液体燃料の蒸発に十分な温度に簡単に達するが、蒸
発容器そのものの温度(壁温)は比較的上昇し難く、こ
のため蒸発開始初期において、一旦蒸発した燃料が壁面
に当たって凝縮する問題があった。又このためバーナで
の点火、消火が短時間内に頻発すると白煙や臭いが発生
しやすい問題があった。
However, in this device of direct evaporation type using hot air,
In the evaporating vessel into which the high-temperature air is introduced, the atmospheric temperature in the inside easily reaches a temperature sufficient for evaporating the liquid fuel, but the temperature (wall temperature) of the evaporating vessel itself is relatively hard to rise, so that the evaporation starts. In the early stage, there was a problem that the evaporated fuel hits the wall surface and condenses. Further, if ignition and extinguishing by the burner occur frequently within a short time, there is a problem that white smoke and odor are likely to be generated.

そこで本発明は上記問題点を解消し、液体燃料を高温
空気で蒸発させるものにおいて、蒸発燃料の凝縮が抑制
され、よってバーナの点火、消火が短時間に頻発しても
白煙や臭いを発生しない、過渡特性の優れた液体燃料蒸
発装置の提供を目的とする。
Therefore, the present invention solves the above problems, and in the case of evaporating liquid fuel with high-temperature air, the condensation of the evaporated fuel is suppressed, so that even if ignition and extinguishing of the burner occur frequently in a short time, white smoke or odor is generated. It is an object of the present invention to provide a liquid fuel evaporator having excellent transient characteristics.

〈課題を解決するための手段〉 上記目的を達成するため、本発明の液体燃料蒸発装置
は、内部を蒸発室20とした蒸発容器10と、害蒸発容器10
内に液体燃料を微粒化して噴霧する噴出ノズル30と、前
記蒸発容器10内に高温空気を送り込む高温空気送り込み
手段40とを備え、前記蒸発容器10内で前記噴霧された液
体燃料を前記送り込まれた高温空気で直接的に蒸発、混
合して、バーナ60側へ送り出すようにした液体燃料蒸発
装置であって、前記高温空気送り込み手段40として、前
記バーナ60とは別経路で燃料を燃焼させて燃焼排ガスを
発生させる今1つのバーナ41と、発生した燃焼排ガスに
空気を混合する手段とを設け、且つ、装置の運転開始
後、高温空気及び液体燃料の前記蒸発容器10内への導入
開始前の一定時間を準備期間として、該準備期間中に前
記高温空気送り込み手段40のバーナ41で発生させた燃焼
排ガスをそのまま蒸発容器10内へ導くようにした制御部
70を設けたことを特徴としている。
<Means for Solving the Problems> In order to achieve the above object, the liquid fuel evaporating apparatus of the present invention comprises an evaporating container 10 having an evaporating chamber 20 inside, and a harmful evaporating container 10
A spray nozzle 30 for atomizing and spraying the liquid fuel therein, and a high-temperature air feeding means 40 for feeding high-temperature air into the evaporation container 10, and the liquid fuel sprayed in the evaporation container 10 is fed therein. Liquid fuel evaporator directly evaporating and mixing with the high-temperature air, and sending the mixture to the burner 60 side, wherein the high-temperature air feeding means 40 burns fuel in a separate path from the burner 60. A single burner 41 for generating combustion exhaust gas and a means for mixing air with the generated combustion exhaust gas are provided, and after starting operation of the apparatus, before starting introduction of high-temperature air and liquid fuel into the evaporation container 10. The control unit is such that the combustion exhaust gas generated by the burner 41 of the high-temperature air feeding means 40 during the preparation period is directly introduced into the evaporating vessel 10 during the preparation period.
The feature is that 70 is provided.

〈作用〉 上記本発明の特徴によれば、装置の運転開始後、まず
高温の燃焼排ガス(後から導入される高温空気よりもか
なり高い温度を有する)が蒸発容器内に導入される。こ
れにより蒸発容器が燃料の凝縮を起こさない温度まで加
熱される。そしてその後、燃焼排ガスに空気が混入され
た高温空気が蒸発容器に送り込まれ、また液体燃料が噴
霧される。よって液体燃料が蒸発される時には蒸発容器
が十分な温度となっており、凝縮が生じない。
<Operation> According to the above-mentioned feature of the present invention, after the operation of the apparatus is started, first, a high-temperature flue gas (having a considerably higher temperature than hot air to be introduced later) is first introduced into the evaporation vessel. As a result, the evaporating vessel is heated to a temperature at which fuel does not condense. Then, high-temperature air in which air is mixed into the combustion exhaust gas is sent to the evaporating container, and the liquid fuel is sprayed. Therefore, when the liquid fuel is evaporated, the evaporating container has a sufficient temperature, and no condensation occurs.

〈実施例〉 第1図は本発明実施装置を示し、第1図(A)は縦断
面図、第1図(B)は一部断面左側面図である。
<Embodiment> Fig. 1 shows a device according to the present invention. Fig. 1 (A) is a longitudinal sectional view, and Fig. 1 (B) is a partial sectional left side view.

蒸発容器10内に蒸発室20が構成され、蒸発室20に対し
て液体燃料、例えば灯油を微粒化状態で噴出させるため
の噴出ノズル30が臨んでいる。また蒸発室20に対して高
温空気を送り込む高温空気送り込み手段40が設けられて
いる。
An evaporation chamber 20 is formed in the evaporation container 10, and an ejection nozzle 30 for ejecting a liquid fuel, for example, kerosene, in an atomized state faces the evaporation chamber 20. Further, high-temperature air feeding means 40 for feeding high-temperature air to the evaporation chamber 20 is provided.

定油面器50からポンプ51により送られ、噴出ノズル30
から噴霧された微粒化状態の液体燃料は、高温空気送り
込み手段40からの高温空気に接触せられ、蒸発せられ
て、高温空気と混合した状態で送り出しパイプ61を通っ
てバーナ60に導かれる。前記噴出される液体燃料の粒径
は例えば数ミクロンから数十ミクロンとする。また蒸発
室20に送り込まれる高温空気は例えば200℃〜400℃とす
る。このようにすることで噴霧液体燃料は120℃〜250℃
程度の低い温度で蒸発する。
It is sent from the constant oil level unit 50 by the pump 51, and the jet nozzle 30
The atomized liquid fuel sprayed from is brought into contact with the high-temperature air from the high-temperature air feeding means 40, evaporates, and is guided to the burner 60 through the delivery pipe 61 in a state of being mixed with the high-temperature air. The particle size of the ejected liquid fuel is, for example, several microns to several tens microns. The high-temperature air sent into the evaporation chamber 20 is set at, for example, 200 ° C. to 400 ° C. In this way, the sprayed liquid fuel is 120 ℃ ~ 250 ℃
Evaporates at moderate temperatures.

前記高温空気送り込み手段40は、前記バーナ60とは別
に設けられる小バーナ41と、該小バーナ41への燃料供給
器42と、前記小バーナ41上に構成される燃焼室43と、該
燃焼室43を取り巻く空気導入室44と、送り込みパイプ45
と、前記小バーナ41と空気導入室44に対する空気供給器
46とを有する。該空気供給器46からの空気通路は小バー
ナ用空気通路46aと空気導入室用空気通路46bに分かれ、
空気導入室用の空気通路46bには空気制御弁47が設けら
れている。前記空気導入室44、空気供給器46、空気導入
室用空気通路46b、空気制御弁47で前記小バーナ41で発
生した燃焼排ガスに空気を混合する手段を構成してい
る。48は点火器、49は炎検出器である。
The high-temperature air feeding means 40 includes a small burner 41 provided separately from the burner 60, a fuel supply unit 42 for the small burner 41, a combustion chamber 43 formed on the small burner 41, and a combustion chamber 43. Air introduction chamber 44 surrounding 43 and feed pipe 45
And an air supply device for the small burner 41 and the air introduction chamber 44
46 and The air passage from the air supply 46 is divided into a small burner air passage 46a and an air introduction chamber air passage 46b.
An air control valve 47 is provided in the air passage 46b for the air introduction chamber. The air introduction chamber 44, the air supply device 46, the air passage 46b for the air introduction chamber, and the air control valve 47 constitute means for mixing air with the combustion exhaust gas generated by the small burner 41. 48 is an igniter and 49 is a flame detector.

70は装置全体の動作タイミングを制御する制御部で、
燃料供給器42、空気供給器46、空気制御弁47、点火器4
8、炎検出器49、ポンプ51等の運転タイミングを制御す
る。
70 is a control unit that controls the operation timing of the entire device,
Fuel supply 42, air supply 46, air control valve 47, igniter 4
8. Control the operation timing of the flame detector 49, the pump 51, and the like.

本発明では、運転開始後、高温空気及び噴霧燃料を蒸
発容器10内に導入する前に、前記小バーナ41で発生した
燃焼排ガスをそのまま蒸発容器10内へ導入する一定時間
の準備期間を設ける。この準備期間中に導入された高温
の燃焼排ガスによって蒸発容器10内壁が加熱され、蒸発
燃料が凝縮を起こさない温度まで上昇せられる。前記燃
焼排ガスの温度は1200℃〜2000℃となるので、凝縮を起
こさない温度、例えば110℃近辺まで蒸発容器10の内壁
温度を上昇させるのに必要な準備期間は短時間でよい。
勿論この準備期間は蒸発容器10の大きさや燃料排ガスの
量によって適当な一定時間を予め選んでおくことにな
る。
In the present invention, after the operation is started, before the high-temperature air and the spray fuel are introduced into the evaporating container 10, a preparation period for a certain period of time for introducing the combustion exhaust gas generated by the small burner 41 as it is into the evaporating container 10 is provided. The inner wall of the evaporating vessel 10 is heated by the high-temperature flue gas introduced during the preparation period, and the temperature is raised to a temperature at which the evaporated fuel does not condense. Since the temperature of the combustion exhaust gas is 1200 ° C. to 2000 ° C., the preparation period required for raising the inner wall temperature of the evaporation container 10 to a temperature at which condensation does not occur, for example, to around 110 ° C., may be short.
Needless to say, an appropriate fixed time is selected in advance for the preparation period depending on the size of the evaporation container 10 and the amount of fuel exhaust gas.

制御部70による運転の動作タイミングを第2図も参照
して更に説明する。
The operation timing of the operation by the control unit 70 will be further described with reference to FIG.

今、装置の運転が開始されると、まず制御部70を介し
て空気供給器46から小バーナ41へ空気が供給され、また
点火器48が作動する。この時空気制御弁47は閉止状態と
される。そして短時間後に制御部70を介して燃料供給器
42が作動せられ、燃料が小バーナ41に送られる。燃料供
給器42からは気体燃料を送ってもよいし、また液体燃料
を蒸発させたものを送るようにしてもよい。炎検出器49
により小バーナ41の着火が確認されると、制御部70内の
タイマーが働き、一定時間の準備期間となる。この準備
期間中は、小バーナ41の燃焼で燃焼室43内に発生した高
温排ガスがそのまま送り込みパイプ45を通って蒸発容器
10内に入り、該蒸発容器10内壁を加熱する。排ガスその
ものはかなり高温(1200℃〜2000℃)であるので、短時
間で蒸発容器10の内壁を凝縮を起こさない温度(110℃
近辺)まで加温することができる。前記準備期間が終了
すると、制御部70を介して空気制御弁47が開放され、空
気供給器46からの空気が空気導入室44に供給される。こ
れにより空気導入室44から新鮮な空気が燃焼室43の燃焼
排ガスに混入せられ、高温空気とせられる。この高温空
気は200℃〜400℃に調整せられて、蒸発容器10内に送り
込まれる。一方前記ポンプ51は、制御部70によって、前
記準備期間が終了した後少し遅れて運転を開始するよ
う、着火からのプリパージ期間が予め定められており、
プリパージ期間終了と同時に液体燃料を送り始める。こ
れにより高温空気の導入に若干遅れて噴出ノズルによる
液体燃料の噴霧が開始され、蒸発が開始される。
Now, when the operation of the apparatus is started, first, air is supplied from the air supply unit 46 to the small burner 41 via the control unit 70, and the igniter 48 is operated. At this time, the air control valve 47 is closed. After a short time, the fuel supply via the control unit 70
42 is activated and fuel is sent to the small burner 41. A gaseous fuel may be sent from the fuel supply unit 42, or a liquid fuel vaporized may be sent from the fuel supply unit 42. Flame detector 49
When the ignition of the small burner 41 is confirmed, the timer in the control unit 70 is activated, and a preparation period for a fixed time is started. During this preparation period, the high-temperature exhaust gas generated in the combustion chamber 43 by the combustion of the small burner 41 passes through the feed pipe 45 as it is and the evaporating vessel.
10 and heats the inner wall of the evaporation container 10. Since the exhaust gas itself is at a very high temperature (1200 ° C. to 2000 ° C.), the temperature (110 ° C.) at which the inner wall of the evaporation vessel 10 does not condense in a short time
(Near). When the preparation period ends, the air control valve 47 is opened via the control unit 70, and the air from the air supply unit 46 is supplied to the air introduction chamber 44. As a result, fresh air from the air introduction chamber 44 is mixed into the combustion exhaust gas of the combustion chamber 43 and is turned into high-temperature air. This high-temperature air is adjusted to 200 ° C. to 400 ° C. and sent into the evaporation container 10. On the other hand, the pump 51 has a pre-purge period from ignition set in advance by the control unit 70 so as to start operation with a slight delay after the preparation period ends,
The liquid fuel starts to be sent at the same time as the end of the pre-purge period. As a result, the spraying of the liquid fuel by the ejection nozzle is started slightly after the introduction of the high-temperature air, and the evaporation is started.

もし燃焼排ガスをそのまま導入する準備期間がない
と、前記液体燃料の噴霧が開始されるまでのプリパージ
期間は、200℃〜400℃程度の高温空気が蒸発容器10内に
導入されることになるため、蒸発容器10の短時間の温度
上昇は望めず、一旦蒸発した液体燃料の凝縮の虞れが生
じる。
If there is no preparation period for directly introducing the combustion exhaust gas, the pre-purge period until the spraying of the liquid fuel is started, because high-temperature air of about 200 ° C. to 400 ° C. will be introduced into the evaporation container 10. However, a short rise in temperature of the evaporation container 10 cannot be expected, and there is a risk of condensation of the liquid fuel once evaporated.

なお、前記蒸発容器10は円筒状の外筒と円板状の両端
壁12、13からなり、噴出ノズル30は一方の端壁13に前記
外筒11の中心軸上に臨むよう取り付けられている。また
前記送り込みパイプ45と送り出しパイプ61は外筒11に対
して接線方向に接続されており、送り込みパイプ45から
蒸発容器10(蒸発室20)に入った高温空気は螺旋状に流
れて送り出しパイプ61に流出する。そしてその間に噴霧
された液体燃料と接触し、これを蒸発させる。
The evaporating vessel 10 is composed of a cylindrical outer cylinder and disk-shaped end walls 12 and 13, and a jet nozzle 30 is attached to one end wall 13 so as to face the center axis of the outer cylinder 11. . The feed pipe 45 and the feed pipe 61 are tangentially connected to the outer cylinder 11, and the high-temperature air that has entered the evaporating vessel 10 (evaporation chamber 20) from the feed pipe 45 flows spirally into the feed pipe 61. Leaked to Then, it comes into contact with the liquid fuel sprayed in the meantime and evaporates it.

〈効果〉 本発明は以上の構成よりなり、請求項1に記載の液体
燃料蒸発装置によれば、高温空気送り込み手段40とし
て、バーナ60とは別経路で燃料を燃焼させて燃焼排ガス
を発生させる今1つのバーナ41と、発生した燃焼排ガス
に空気を混合する手段とを設け、且つ、装置の運転開始
後、高温空気及び液体燃料の前記蒸発容器10内への導入
開始前の一定時間を準備期間として、該準備期間中に前
記高温空気送り込み手段40のバーナ41で発生させた燃焼
排ガスをそのまま蒸発容器10内へ導くようにした制御部
70を設けたので、蒸発容器10内において液体燃料の蒸発
が開始される前に、高温空気送り込み手段40のバーナ41
で発生した燃焼排ガスによって蒸発容器10を十分に加熱
することができる。よって蒸発された液体燃料の凝縮を
確実に防止することができ、また本装置を用いた燃焼器
を短時間に頻繁に点火、消火しても白煙や臭いの発生を
抑制することができる。
<Effect> According to the liquid fuel evaporator according to the first aspect of the present invention, the present invention has the above-described configuration. As the high-temperature air feeding means 40, the fuel is burned in a different path from the burner 60 to generate combustion exhaust gas. One burner 41 and a means for mixing air with the generated flue gas are provided, and a certain period of time before starting the introduction of high-temperature air and liquid fuel into the evaporation vessel 10 after the operation of the apparatus is prepared. As a period, a control unit which guides the combustion exhaust gas generated by the burner 41 of the high-temperature air feeding means 40 during the preparation period directly into the evaporation container 10
Since the fuel tank 70 is provided, the burner 41 of the high-temperature air feeding means 40 is provided before the evaporation of the liquid fuel in the evaporation container 10 is started.
The evaporating container 10 can be sufficiently heated by the combustion exhaust gas generated in the above. Therefore, condensation of the evaporated liquid fuel can be reliably prevented, and the generation of white smoke and odor can be suppressed even if the combustor using the present device is frequently ignited and extinguished in a short time.

勿論、液体燃料は微粒化状態から高温空気により直接
的に蒸発されるので、蒸発温度が低くなり、蒸発容器内
にタール状物質が生成されるのが抑制される。
Of course, since the liquid fuel is directly evaporated from the atomized state by the high-temperature air, the evaporation temperature is lowered, and the generation of tar-like substances in the evaporation container is suppressed.

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

第1図は本発明実施装置を示し、第1図(A)は縦断面
図、第1図(B)は一部断面左側面図、第2図は実施装
置各部の動作タイミングチャートである。 10:蒸発容器 20:蒸発室 30:噴出ノズル 40:高温空気送り込み手段 41:小バーナ 42:燃料供給器 43:燃焼室 44:空気導入室 46:空気供給器 47:空気制御弁 50:定油面器 60:バーナ 70:制御部
FIG. 1 shows an apparatus according to the present invention, FIG. 1 (A) is a longitudinal sectional view, FIG. 1 (B) is a partially sectional left side view, and FIG. 10: Evaporation vessel 20: Evaporation chamber 30: Jet nozzle 40: Hot air sending means 41: Small burner 42: Fuel supply 43: Combustion chamber 44: Air introduction chamber 46: Air supply 47: Air control valve 50: Constant oil Faceplate 60: Burner 70: Control unit

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】内部を蒸発室20とした蒸発容器10と、該蒸
発容器10内に液体燃料を微粒化して噴霧する噴出ノズル
30と、前記蒸発容器10内に高温空気を送り込む高温空気
送り込み手段40とを備え、前記蒸発容器10内で前記噴霧
された液体燃料を前記送り込まれた高温空気で直接的に
蒸発、混合して、バーナ60側へ送り出すようにした液体
燃料蒸発装置であって、前記高温空気送り込み手段40と
して、前記バーナ60とは別経路で燃料を燃焼させて燃焼
排ガスを発生させる今1つのバーナ41と、発生した燃焼
排ガスに空気を混合する手段とを設け、且つ、装置の運
転開始後、高温空気及び液体燃料の前記蒸発容器10内へ
の導入開始前の一定時間を準備期間として、該準備期間
中に前記高温空気送り込み手段40のバーナ41で発生させ
た燃焼排ガスをそのまま蒸発容器10内へ導くようにした
制御部70を設けたことを特徴とする液体燃料蒸発装置。
An evaporating container having an evaporating chamber therein, and a jet nozzle for atomizing and spraying liquid fuel into the evaporating container.
30 and a high-temperature air feeding means 40 for feeding high-temperature air into the evaporating container 10, and the liquid fuel sprayed in the evaporating container 10 is directly evaporated and mixed with the sent high-temperature air in the evaporating container 10. A liquid fuel evaporating device configured to feed the fuel to the burner 60 side, wherein the high-temperature air feeding means 40 includes a single burner 41 that burns fuel in a different path from the burner 60 to generate combustion exhaust gas; Means for mixing air with the generated combustion exhaust gas, and a certain period of time after the start of operation of the apparatus and before the start of introduction of high-temperature air and liquid fuel into the evaporation container 10 as a preparation period, and during the preparation period, A liquid fuel evaporating apparatus, further comprising a control unit 70 for guiding the combustion exhaust gas generated by the burner 41 of the high-temperature air feeding means 40 into the evaporation container 10 as it is.
JP1302964A 1989-11-20 1989-11-20 Liquid fuel evaporator Expired - Lifetime JP2569845B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1302964A JP2569845B2 (en) 1989-11-20 1989-11-20 Liquid fuel evaporator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1302964A JP2569845B2 (en) 1989-11-20 1989-11-20 Liquid fuel evaporator

Publications (2)

Publication Number Publication Date
JPH03164616A JPH03164616A (en) 1991-07-16
JP2569845B2 true JP2569845B2 (en) 1997-01-08

Family

ID=17915276

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1302964A Expired - Lifetime JP2569845B2 (en) 1989-11-20 1989-11-20 Liquid fuel evaporator

Country Status (1)

Country Link
JP (1) JP2569845B2 (en)

Also Published As

Publication number Publication date
JPH03164616A (en) 1991-07-16

Similar Documents

Publication Publication Date Title
US20040058290A1 (en) Self-sustaining premixed pilot burner for liquid fuels
JP2569845B2 (en) Liquid fuel evaporator
JPS56149522A (en) Vaporizing type liquid combustor
JPS589070Y2 (en) flame detection device
JPS584018Y2 (en) liquid fuel combustion equipment
JPH0875121A (en) Fan heater combustion device
JPH0229389Y2 (en)
JP3854342B2 (en) Mixed firing device
JPH0113264Y2 (en)
JPH0547932Y2 (en)
JPS60253731A (en) Vaporizing combustion device
JPH0942615A (en) Burner device
JPS563812A (en) Liquid fuel combustion device
JPH0335942Y2 (en)
JP2748675B2 (en) Combustion equipment
JP2002005429A (en) Liquid fuel combustor
JPS6152553A (en) hot water boiler
JPS563811A (en) Combustion device for liquid fuel
JPS563813A (en) Liquid fuel combustion device
JPS576230A (en) Liquid fuel burner
KR100249225B1 (en) Device for activating flame of oil burner
JPH0127328B2 (en)
JPS6362652B2 (en)
JPS5741508A (en) Liquid fuel gasifying burner
JPS62106210A (en) Supersonic combustion apparatus