JPH04324009A - Liquid fuel evaporator - Google Patents
Liquid fuel evaporatorInfo
- Publication number
- JPH04324009A JPH04324009A JP12214891A JP12214891A JPH04324009A JP H04324009 A JPH04324009 A JP H04324009A JP 12214891 A JP12214891 A JP 12214891A JP 12214891 A JP12214891 A JP 12214891A JP H04324009 A JPH04324009 A JP H04324009A
- Authority
- JP
- Japan
- Prior art keywords
- liquid fuel
- temperature air
- evaporation
- container
- evaporation container
- 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
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 46
- 239000007788 liquid Substances 0.000 title claims abstract description 36
- 230000008020 evaporation Effects 0.000 claims abstract description 68
- 238000001704 evaporation Methods 0.000 claims abstract description 68
- 238000005507 spraying Methods 0.000 claims abstract description 4
- 239000000203 mixture Substances 0.000 claims description 7
- 230000002093 peripheral effect Effects 0.000 abstract description 2
- 239000007921 spray Substances 0.000 description 7
- 239000002245 particle Substances 0.000 description 4
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 230000003197 catalytic effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Landscapes
- Spray-Type Burners (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
Description
【0001】0001
【産業上の利用分野】本発明は、灯油等の液体燃料を、
加熱した空気により比較的低い温度で直接的に蒸発気化
させ、得られた混合気を燃焼器側へ送り出すようにした
液体燃料蒸発装置に関する。[Industrial Application Field] The present invention provides a method for using liquid fuel such as kerosene,
The present invention relates to a liquid fuel evaporation device that directly evaporates and vaporizes air at a relatively low temperature using heated air and sends the resulting mixture to a combustor.
【0002】0002
【従来の技術】この種液体燃料蒸発装置の従来例を図6
、図7に示す。図6は従来装置の一部断面正面図で、図
7は同一部断面側面図である。円筒状の蒸発容器1内に
蒸発室2が構成されており、液体燃料噴霧用のノズル3
が円筒状蒸発容器1の中心軸上を内部の蒸発室2へ臨ま
されている。液体燃料はノズル3に送られ、蒸発室2内
へ微粒化状態で導入される。蒸発容器1には前記ノズル
3の噴射口と対向する端壁近くの円筒壁面に、接線方向
に1個の高温空気導入口7が設けられており、該導入口
7から導入された高温空気によって、蒸発室2内に噴霧
された液体燃料が比較的低い温度で直接的に気化される
。得られた混合気は前記噴射口近くの円筒壁面に設けら
れた送り出し口8から燃焼器9に送られ、燃焼に供され
る。[Prior Art] Fig. 6 shows a conventional example of this type of liquid fuel evaporation device.
, shown in FIG. FIG. 6 is a partially sectional front view of a conventional device, and FIG. 7 is a partially sectional side view of the same. An evaporation chamber 2 is configured in a cylindrical evaporation container 1, and a nozzle 3 for spraying liquid fuel is provided.
is placed on the central axis of the cylindrical evaporation container 1 and faces into the evaporation chamber 2 inside. The liquid fuel is sent to the nozzle 3 and introduced into the evaporation chamber 2 in an atomized state. The evaporation vessel 1 is provided with one high-temperature air inlet 7 in the tangential direction on the cylindrical wall surface near the end wall facing the injection port of the nozzle 3, and the high-temperature air introduced from the inlet 7 , the liquid fuel sprayed into the evaporation chamber 2 is directly vaporized at a relatively low temperature. The obtained air-fuel mixture is sent to a combustor 9 from a delivery port 8 provided on the cylindrical wall near the injection port, and is subjected to combustion.
【0003】0003
【発明が解決しようとする課題】ところが上記従来の液
体燃料蒸発装置では、蒸発室2は円筒状の外筒と円盤状
の両端壁からなる蒸発容器1内に構成され、ノズル3は
何れか一方の端壁から前記外筒の中心軸上に臨み、高温
空気送り込み手段はノズル3位置とは対向する側にあっ
てその送り込みパイプを前記一個の高温空気導入口7に
対して接線方向に接続し、且つ蒸発室2から燃焼器9側
への混合気送り出しパイプも前記外筒に対して接線方向
に接続して構成しているので、導入された高温空気の流
れが蒸発容器内で偏心的な螺旋状となりやすく、そのた
めに、蒸発室2に噴霧された液体燃料は特定の方向に曲
げられ(噴霧コーンが偏心し)、蒸発室2外筒に衝突す
る。特に、噴霧された液体燃料の貫通度(運動量)が低
い場合は、この現象は顕著になる。そのため、実際の蒸
発は噴霧された液体燃料が蒸発室2外筒に衝突するまで
の空間でしか起こらず、蒸発室2が有効に使われないと
いう欠点があった。また噴霧が充分に広がらずに高温空
気と接触するので、噴霧粒子と高温空気との混合が充分
に行なわれない欠点があった。However, in the above-mentioned conventional liquid fuel evaporation device, the evaporation chamber 2 is constructed within the evaporation container 1 consisting of a cylindrical outer tube and disk-shaped both end walls, and the nozzle 3 is located at either end. The high-temperature air feeding means is located on the side opposite to the nozzle 3 position, and its feeding pipe is tangentially connected to the one high-temperature air inlet 7. In addition, since the air-fuel mixture sending pipe from the evaporation chamber 2 to the combustor 9 side is connected tangentially to the outer cylinder, the flow of the introduced high-temperature air is prevented from being eccentric within the evaporation container. The liquid fuel tends to form a spiral shape, so that the liquid fuel sprayed into the evaporation chamber 2 is bent in a specific direction (the spray cone is eccentric) and collides with the outer cylinder of the evaporation chamber 2. This phenomenon becomes particularly noticeable when the degree of penetration (momentum) of the sprayed liquid fuel is low. Therefore, actual evaporation occurs only in the space until the sprayed liquid fuel collides with the outer cylinder of the evaporation chamber 2, which has the disadvantage that the evaporation chamber 2 is not used effectively. Furthermore, since the spray does not spread sufficiently and comes into contact with the high temperature air, there is a drawback that the spray particles and the high temperature air are not sufficiently mixed.
【0004】そこで、本発明は上記従来技術の欠点を解
消し、蒸発室内に噴霧された液体燃料が蒸発室内に十分
に入って行き、コンパクトな蒸発室内で効率よく且つ安
定して蒸発ができる液体燃料蒸発装置の提供を目的とす
る。Therefore, the present invention solves the above-mentioned drawbacks of the prior art, and the liquid fuel sprayed into the evaporation chamber sufficiently enters the evaporation chamber, and the liquid fuel can be efficiently and stably evaporated in the compact evaporation chamber. The purpose is to provide fuel evaporation equipment.
【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
、本発明の液体燃料蒸発装置は、外筒と両端壁からなる
円筒型の蒸発容器と、該蒸発容器の1側端壁から容器内
に微粒化液体燃料を噴霧するノズルと、蒸発容器内に高
温空気を送り込む高温空気送り込み手段を少なくとも有
し、前記蒸発容器内に噴霧された微粒化液体燃料を前記
高温空気との接触で直接的に蒸発させて、その混合気を
燃焼器側へ送り出すようにした液体燃料蒸発装置であっ
て、前記蒸発容器外筒の円周領域に複数個の高温空気導
入口を均等に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 evaporation device of the present invention includes a cylindrical evaporation container consisting of an outer cylinder and both end walls, and an interior of the evaporation container from one side end wall of the evaporation container. the atomized liquid fuel sprayed into the evaporation container, the atomized liquid fuel sprayed into the evaporation container is directly contacted with the high temperature air; This liquid fuel evaporator is configured to evaporate the air-fuel mixture and send the mixture to the combustor side, characterized in that a plurality of high-temperature air inlets are evenly provided in the circumferential area of the outer cylinder of the evaporator container. It is said that
【0006】[0006]
【作用】蒸発容器外筒の円周領域に均等に設けた複数個
の高温空気導入口から高温空気が導入されるので、1ヵ
所から高温空気を導入する場合に比べて、高温空気流の
分布が均一となり、噴霧を特定方向等に曲げる力が働か
ない。よってノズルから噴霧された液体燃料粒子は容器
内に深く侵入し易くなり、広い範囲で且つ適当な接触時
間をもって高温空気と接触することができる。その結果
、効率よく且つ安定して蒸発を行うことができる。また
空間利用率がよいので蒸発室を小さくすることができ、
装置をコンパクトにできる。[Operation] Since high-temperature air is introduced from multiple high-temperature air inlets evenly provided in the circumferential area of the outer cylinder of the evaporation container, the distribution of high-temperature air flow is better than when high-temperature air is introduced from one place. is uniform, and there is no force that bends the spray in a specific direction. Therefore, the liquid fuel particles sprayed from the nozzle can easily penetrate deeply into the container and come into contact with the high temperature air over a wide range and for a suitable contact time. As a result, efficient and stable evaporation can be performed. In addition, the space utilization rate is good, so the evaporation chamber can be made smaller.
The device can be made more compact.
【0007】[0007]
【実施例】図1は本発明の第1実施例に係る装置の一部
断面正面図、図2は同一部断面側面図である。DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is a partially sectional front view of an apparatus according to a first embodiment of the present invention, and FIG. 2 is a partially sectional side view of the same.
【0008】蒸発容器10は円筒状の外筒11と円盤状
の端壁12、28とからなり、内部に蒸発室13を構成
している。そして前記蒸発容器10の一方の端壁12に
は中心軸上にノズル22を容器10内へ臨ましてなるノ
ズル構造体23が取り付けられている。また蒸発容器1
0の外筒11には、ノズル構造体23に近い方に蒸発気
化された液体燃料を燃焼器25に送り出す送り出し口1
4が設けられている。一方、ノズル構造体23から遠い
方の外筒10の円周領域には一定の幅をもって高温空気
室20が設けられている。そして高温空気室20の内周
壁17に複数の高温空気導入口15が円周方向に均等に
設けられている。また前記高温空気室20の外周壁18
には高温空気生成装置である空気加熱手段27からのパ
イプ26が接続されている。空気加熱手段27、パイプ
26、高温空気室20、高温空気導入口15で高温空気
送り込み手段を構成する。The evaporation container 10 consists of a cylindrical outer tube 11 and disk-shaped end walls 12 and 28, and defines an evaporation chamber 13 inside. A nozzle structure 23 having a nozzle 22 facing into the container 10 is attached to one end wall 12 of the evaporation container 10 on the central axis. Also, evaporation container 1
0 outer cylinder 11 has a delivery port 1 closer to the nozzle structure 23 that sends the evaporated liquid fuel to the combustor 25.
4 is provided. On the other hand, a high-temperature air chamber 20 having a constant width is provided in a circumferential region of the outer cylinder 10 farther from the nozzle structure 23. A plurality of high temperature air inlets 15 are provided evenly in the circumferential direction on the inner circumferential wall 17 of the high temperature air chamber 20. Further, the outer peripheral wall 18 of the high temperature air chamber 20
A pipe 26 from an air heating means 27, which is a high-temperature air generating device, is connected to. The air heating means 27, the pipe 26, the high temperature air chamber 20, and the high temperature air inlet 15 constitute a high temperature air feeding means.
【0009】本実施例では、前記高温空気室20から蒸
発室13への複数の高温空気導入口15を、蒸発室13
に対して接線方向に空気が導入されるように設けている
。本実施例では蒸発容器外筒11の円周領域に設けた高
温空気室20の複数個の高温空気導入口15から均等に
高温空気が導入されるので、1ヵ所から高温空気を導入
する場合に比べて、高温空気流の分布が均一となり、噴
霧を特定方向等に曲げる力が働かない。よってノズル2
2から噴霧された液体燃料粒子は容器10内に深く侵入
し易くなり、広い範囲で且つ適当な接触時間をもって高
温空気と接触することができる。また本実施例では、高
温空気導入口15から接線方向に高温空気が導入される
ことで、蒸発室13の内壁面に沿った高温空気の流れが
生じさせることができ、その結果、噴霧燃料が噴霧後す
ぐに内壁面に接触するのが防止でき、特に運転初期等に
おいて蒸発燃料が未だ低温の壁面に接触して再液化する
といったことが防止される。In this embodiment, a plurality of high temperature air inlets 15 from the high temperature air chamber 20 to the evaporation chamber 13 are connected to the evaporation chamber 13.
Air is introduced in the tangential direction. In this embodiment, high-temperature air is uniformly introduced from the plurality of high-temperature air inlets 15 of the high-temperature air chamber 20 provided in the circumferential area of the outer cylinder 11 of the evaporation container. In comparison, the distribution of the high-temperature air flow is uniform, and no force acts to bend the spray in a particular direction. Therefore, nozzle 2
The liquid fuel particles sprayed from 2 can easily penetrate deeply into the container 10, and can come into contact with the high temperature air over a wide range and with a suitable contact time. Furthermore, in this embodiment, by introducing high temperature air in the tangential direction from the high temperature air inlet 15, it is possible to generate a flow of high temperature air along the inner wall surface of the evaporation chamber 13, and as a result, the atomized fuel is It is possible to prevent the evaporated fuel from coming into contact with the inner wall surface immediately after spraying, and to prevent the evaporated fuel from coming into contact with the still-low-temperature wall surface and re-liquefying the fuel, especially at the beginning of operation.
【0010】図3は本発明の第2実施例に係る装置の一
部断面正面図である。第2実施例の場合は、高温空気室
20の内壁17に複数個、均等に設けられる高温空気導
入口15を、蒸発室13に対して接線方向(第1実施例
の場合)よりも小さい角度a、例えば半径方向に対して
45度にして設けている。他の点は第1実施例と同様の
構成である。FIG. 3 is a partially sectional front view of an apparatus according to a second embodiment of the present invention. In the case of the second embodiment, a plurality of high-temperature air inlets 15 evenly provided on the inner wall 17 of the high-temperature air chamber 20 are arranged at an angle smaller than the tangential direction (in the case of the first embodiment) with respect to the evaporation chamber 13. a, for example, at 45 degrees with respect to the radial direction. The other points are the same configuration as the first embodiment.
【0011】第1実施例の場合には、蒸発室13に対し
て接線方向に高温空気導入口15を設けたため、導入さ
れた高温空気が蒸発室13内壁面に沿った旋回空気流と
なり、このため高温空気の壁面への放熱が大きい欠点、
及び高温空気と噴霧燃料との混合が遅く、蒸発に長時間
かかる問題があった。本第2実施例では高温空気による
旋回空気流が蒸発室13内壁面から離れて形成される(
旋回空気流の半径が小さくなる)ため壁面への放熱が少
なく、省エネである。また高温空気と噴霧燃料との混合
が第1実施例の場合に比べて早くなり、一層蒸発効率が
よくなる。勿論、高温空気導入室15を容器外筒11の
円周領域に複数個、均等に設けた点による作用効果は上
記第1の実施例の場合と同様である。In the case of the first embodiment, since the high-temperature air inlet 15 is provided in the tangential direction to the evaporation chamber 13, the high-temperature air introduced becomes a swirling air flow along the inner wall surface of the evaporation chamber 13. Therefore, the disadvantage is that there is a large amount of heat dissipated from high-temperature air to the wall.
Also, there was a problem that the mixing of the high temperature air and the sprayed fuel was slow, and it took a long time for evaporation. In the second embodiment, a swirling airflow of high-temperature air is formed away from the inner wall surface of the evaporation chamber 13 (
(The radius of the swirling airflow becomes smaller), so less heat is radiated to the wall, resulting in energy savings. Furthermore, the high temperature air and the sprayed fuel are mixed more quickly than in the first embodiment, and the evaporation efficiency is further improved. Of course, the effect obtained by providing a plurality of high-temperature air introduction chambers 15 evenly around the circumferential area of the container outer cylinder 11 is the same as that of the first embodiment.
【0012】図4は本発明の第3実施例に係る装置の一
部断面正面図である。第3実施例の場合は、高温空気室
20の内壁17に複数個、均等に設けられる高温空気導
入口15を、蒸発室13に対して半径方向に設けている
。他の点は第1、第2の実施例の場合と同様である。
本第3実施例の場合は、高温空気が周囲から蒸発室13
内にその中心に向けて吹き込まれる。従って壁面に沿っ
た旋回流は構成されず、噴霧されてきた液体燃料に対し
て側方から吹き込まれた高温空気が直接的に接触し、効
率よく蒸発がなされる。また噴霧された液体燃料の侵入
に対する抵抗も少なく、噴霧貫通力の小さい噴霧器を用
いても、良好な接触蒸発ができる。FIG. 4 is a partially sectional front view of an apparatus according to a third embodiment of the present invention. In the case of the third embodiment, a plurality of high-temperature air inlets 15 are provided evenly on the inner wall 17 of the high-temperature air chamber 20 in a radial direction with respect to the evaporation chamber 13. Other points are the same as in the first and second embodiments. In the case of the third embodiment, high temperature air is supplied from the surroundings to the evaporation chamber 13.
It is blown inward towards its center. Therefore, a swirling flow along the wall surface is not formed, and the high temperature air blown from the side comes into direct contact with the sprayed liquid fuel, resulting in efficient evaporation. Furthermore, there is little resistance to the intrusion of the atomized liquid fuel, and good catalytic evaporation can be achieved even if a sprayer with a small spray penetration force is used.
【0013】図5は本発明の上記各実施例における変形
例を示す一部断面側面図である。この変形例は、ノズル
22を高温空気導入口15がある側の端壁28に設けて
いる。即ち、上記1〜3の実施例において、ノズル22
に対する高温空気導入口15と高温空気の送り出し口1
4の位置関係を逆にしてもよい。その他、送り出し口1
4はノズル22側とは反対側の端壁の中心軸上に設けて
もよい。FIG. 5 is a partially sectional side view showing a modification of each of the above embodiments of the present invention. In this modification, the nozzle 22 is provided on the end wall 28 on the side where the high temperature air inlet 15 is located. That is, in the above embodiments 1 to 3, the nozzle 22
High temperature air inlet 15 and high temperature air outlet 1 for
4 may be reversed. Others, outlet 1
4 may be provided on the central axis of the end wall on the opposite side to the nozzle 22 side.
【0014】[0014]
【発明の効果】本発明は以上の構成、作用よりなり、請
求項1に記載の液体燃料蒸発装置によれば、蒸発容器外
筒の円周領域に均等に設けた複数個の高温空気導入口か
ら高温空気が導入されるので、1ヵ所から高温空気を導
入する場合に比べて、高温空気流の分布が均一となり、
噴霧を特定方向等に曲げる力が働かない。よってノズル
から噴霧された液体燃料粒子は容器内に深く侵入し易く
なり、広い範囲で且つ適当な接触時間をもって高温空気
と接触することができる。その結果、効率よく且つ安定
して蒸発を行うことができる。また空間利用率がよいの
で蒸発室を小さくすることができ、装置をコンパクトに
できる。According to the liquid fuel evaporator according to claim 1, the present invention has the above-described structure and operation. Since high-temperature air is introduced from one place, the distribution of high-temperature air flow is more uniform than when high-temperature air is introduced from one place.
The force that bends the spray in a specific direction does not work. Therefore, the liquid fuel particles sprayed from the nozzle can easily penetrate deeply into the container and come into contact with the high temperature air over a wide range and for a suitable contact time. As a result, efficient and stable evaporation can be performed. Moreover, since the space utilization efficiency is good, the evaporation chamber can be made small, and the apparatus can be made compact.
【図1】本発明の第1実施例に係る装置の一部断面正面
図である。FIG. 1 is a partially sectional front view of an apparatus according to a first embodiment of the present invention.
【図2】同第1実施例に係る装置の一部断面側面図であ
る。FIG. 2 is a partially sectional side view of the device according to the first embodiment.
【図3】本発明の第2実施例に係る装置の一部断面正面
図である。FIG. 3 is a partially sectional front view of an apparatus according to a second embodiment of the present invention.
【図4】本発明の第3実施例に係る装置の一部断面正面
図である。FIG. 4 is a partially sectional front view of an apparatus according to a third embodiment of the present invention.
【図5】本発明の上記各実施例における変形例を示す一
部断面側面図である。FIG. 5 is a partially sectional side view showing a modification of each of the above embodiments of the present invention.
【図6】従来装置の一部断面正面図である。FIG. 6 is a partially sectional front view of a conventional device.
【図7】従来装置の一部断面側面図である。FIG. 7 is a partially sectional side view of a conventional device.
10 蒸発容器 11 外筒 12、28 端壁 13 蒸発室 14 混合気の送り出し口 15 高温空気導入口 20 高温空気室 22 ノズル 25 燃焼器 10 Evaporation container 11 Outer cylinder 12, 28 End wall 13 Evaporation chamber 14 Mixture outlet 15 High temperature air inlet 20 High temperature air chamber 22 Nozzle 25 Combustor
Claims (1)
器と、該蒸発容器の1側端壁から容器内に微粒化液体燃
料を噴霧するノズルと、蒸発容器内に高温空気を送り込
む高温空気送り込み手段を少なくとも有し、前記蒸発容
器内に噴霧された微粒化液体燃料を前記高温空気との接
触で直接的に蒸発させて、その混合気を燃焼器側へ送り
出すようにした液体燃料蒸発装置であって、前記蒸発容
器外筒の円周領域に複数個の高温空気導入口を均等に設
けたことを特徴とする液体燃料蒸発装置。Claim 1: A cylindrical evaporation container consisting of an outer cylinder and both end walls, a nozzle for spraying atomized liquid fuel into the container from one end wall of the evaporation container, and a high-temperature nozzle for sending high-temperature air into the evaporation container A liquid fuel evaporator comprising at least an air feeding means, the atomized liquid fuel sprayed into the evaporator container is directly evaporated by contact with the high temperature air, and the mixture is sent to the combustor side. 1. A liquid fuel evaporation device, characterized in that a plurality of high-temperature air inlets are evenly provided in a circumferential region of the outer cylinder of the evaporation container.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3122148A JP2624018B2 (en) | 1991-04-23 | 1991-04-23 | Liquid fuel evaporator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3122148A JP2624018B2 (en) | 1991-04-23 | 1991-04-23 | Liquid fuel evaporator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH04324009A true JPH04324009A (en) | 1992-11-13 |
| JP2624018B2 JP2624018B2 (en) | 1997-06-25 |
Family
ID=14828797
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3122148A Expired - Lifetime JP2624018B2 (en) | 1991-04-23 | 1991-04-23 | Liquid fuel evaporator |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2624018B2 (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5672167A (en) * | 1979-11-19 | 1981-06-16 | Hitachi Ltd | Heat resisting alloy |
| JPS61252414A (en) * | 1985-05-02 | 1986-11-10 | Matsushita Electric Ind Co Ltd | Petroleum combustion device |
| JPS6380058A (en) * | 1986-09-22 | 1988-04-11 | Kazuo Ueshima | Liquid fuel gasifying device |
| JPH02298704A (en) * | 1989-05-11 | 1990-12-11 | Hitachi Home Tec Ltd | Gasification gas bunsen burner |
-
1991
- 1991-04-23 JP JP3122148A patent/JP2624018B2/en not_active Expired - Lifetime
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5672167A (en) * | 1979-11-19 | 1981-06-16 | Hitachi Ltd | Heat resisting alloy |
| JPS61252414A (en) * | 1985-05-02 | 1986-11-10 | Matsushita Electric Ind Co Ltd | Petroleum combustion device |
| JPS6380058A (en) * | 1986-09-22 | 1988-04-11 | Kazuo Ueshima | Liquid fuel gasifying device |
| JPH02298704A (en) * | 1989-05-11 | 1990-12-11 | Hitachi Home Tec Ltd | Gasification gas bunsen burner |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2624018B2 (en) | 1997-06-25 |
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