JPH04324006A - Liquid fuel evaporator - Google Patents
Liquid fuel evaporatorInfo
- Publication number
- JPH04324006A JPH04324006A JP12214591A JP12214591A JPH04324006A JP H04324006 A JPH04324006 A JP H04324006A JP 12214591 A JP12214591 A JP 12214591A JP 12214591 A JP12214591 A JP 12214591A JP H04324006 A JPH04324006 A JP H04324006A
- Authority
- JP
- Japan
- Prior art keywords
- liquid fuel
- temperature air
- evaporation
- nozzle
- 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.)
- Pending
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 43
- 239000007788 liquid Substances 0.000 title claims abstract description 36
- 230000008020 evaporation Effects 0.000 claims abstract description 43
- 238000001704 evaporation Methods 0.000 claims abstract description 43
- 239000000203 mixture Substances 0.000 claims description 12
- 238000002347 injection Methods 0.000 claims description 8
- 239000007924 injection Substances 0.000 claims description 8
- 239000007921 spray Substances 0.000 claims description 6
- 238000005507 spraying Methods 0.000 abstract description 3
- 206010037660 Pyrexia Diseases 0.000 abstract 1
- 239000002245 particle Substances 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 2
- 239000003350 kerosene Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
Landscapes
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Spray-Type 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 evaporator that directly vaporizes the fuel at a relatively low temperature using heated air and sends the resulting mixture to the combustor side.
【0002】0002
【従来の技術】この種液体燃料蒸発装置の従来例を図3
、図4に示す。図3は従来装置の一部断面正面図で、図
4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側に送られ、燃焼に供さ
れる。[Prior Art] Fig. 3 shows a conventional example of this type of liquid fuel evaporator.
, shown in Figure 4. FIG. 3 is a partially sectional front view of a conventional device, and FIG. 4 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 the combustor 9 side 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外筒の導入口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の送り出し口8に対して接
線方向に接続して構成しているので、前記混合気の送り
出し口8に向かう高温空気の流れが強いため、蒸発室に
噴霧された液体燃料は高温空気に押し流される形で、短
絡的に前記送り出し口8に送り込まれる。そのため、実
際の蒸発は、噴霧された液体燃料が送り出し口8に到達
するまでの空間でしか起こらず、蒸発室2が有効に使わ
れない問題があった。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. facing on the central axis of the outer cylinder from the end wall, the high-temperature air feeding means is located on the side opposite to the nozzle 3 position, and its feeding pipe is connected tangentially to the inlet 7 of the outer cylinder, In addition, since the air-fuel mixture sending pipe from the evaporation chamber 2 to the combustor 9 side is connected tangentially to the sending port 8 of the outer cylinder, the high-temperature air flowing toward the air-fuel mixture sending port 8 is connected. Since the flow is strong, the liquid fuel sprayed into the evaporation chamber is swept away by the high-temperature air and sent into the delivery port 8 in a short-circuit manner. Therefore, actual evaporation occurs only in the space until the sprayed liquid fuel reaches the delivery port 8, resulting in the problem 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、送り出し口に行くまでに高温空気との十
分な混合接触の機会があり、よって効率的で安定した蒸
発ができ、且つコンパクトな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 ensures that the liquid fuel sprayed into the evaporation chamber sufficiently enters the evaporation chamber and has sufficient mixing contact with high-temperature air before reaching the outlet. The purpose of the present invention is to provide a compact liquid fuel evaporation device that allows efficient and stable evaporation.
【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、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、前記ノズルの噴射
口から離れた位置に前記混合気の送り出し口を設けたこ
とを特徴としている。[Means for Solving the Problems] In order to achieve the above object, a liquid fuel evaporation device of the present invention includes a cylindrical evaporation container,
The atomized liquid sprayed into the evaporation container includes at least a nozzle for spraying atomized liquid fuel into the container from one side end wall of the evaporation container, and a high-temperature air sending means for sending high-temperature air into the evaporation container. A liquid fuel evaporation device that directly evaporates fuel by contact with the high-temperature air and sends the mixture to the combustor side, wherein the mixture is disposed at a position away from the injection port of the nozzle. It is characterized by having a delivery port.
【0006】[0006]
【作用】ノズルの噴射口から離れた位置に混合気の送り
出し口が設けられるので、これにより、ノズル近傍での
高温空気の流れに偏りがなくなり、噴霧がある程度広が
った後、高温空気と接触することができる。よって液体
燃料粒子は容器内で十分に高温空気と接触することがで
き、コンパクトな容器内で効率よく且つ安定して蒸発を
行うことができる。[Operation] Since the air-fuel mixture outlet is provided at a position away from the nozzle injection port, this eliminates the bias in the flow of high-temperature air near the nozzle, and after the spray spreads to a certain extent, it comes into contact with the high-temperature air. be able to. Therefore, the liquid fuel particles can sufficiently come into contact with high-temperature air within the container, and can be efficiently and stably evaporated within the compact container.
【0007】[0007]
【実施例】図1は本発明実施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 for implementing 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10の外
筒11には、ノズル構造体23から遠い方に、高温空気
導入口15が接線方向に設けられている。26は導入口
15から接線方向に配設された導入パイプである。該導
入パイプ26と前記高温空気導入口15と高温空気発生
器27で高温空気送り込み手段を構成する。The evaporation container 10 is composed of a cylindrical outer tube 11 and a disc-shaped end wall 12, and has 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. Further, in the outer cylinder 11 of the evaporation container 10, a high temperature air inlet 15 is provided in a tangential direction on the side far from the nozzle structure 23. Reference numeral 26 denotes an introduction pipe arranged tangentially from the introduction port 15. The introduction pipe 26, the high temperature air introduction port 15, and the high temperature air generator 27 constitute a high temperature air feeding means.
【0009】前記噴出ノズル構造体23から距離Lだけ
離れた位置に、蒸発気化された液体燃料を燃焼器25側
へ送り出す送り出し口14を設ける。この送り出し口1
4の位置は少なくともノズル22の噴射口の近傍には設
けない。比較的離れた距離Lをおくようにする。この距
離Lは外筒11の長さ、高温空気導入口15の位置、高
温空気の導入圧、ノズル22の噴出力等に応じて多少調
整される。24は送り出し口14から接線方向に配設さ
れた送り出しパイプである。A delivery port 14 is provided at a distance L from the injection nozzle structure 23 to send the evaporated liquid fuel to the combustor 25 side. This outlet 1
Position 4 is not provided at least near the injection port of the nozzle 22. They should be placed at a relatively distant distance L. This distance L is adjusted somewhat depending on the length of the outer cylinder 11, the position of the high temperature air inlet 15, the high temperature air introduction pressure, the jetting force of the nozzle 22, etc. 24 is a delivery pipe arranged tangentially from the delivery port 14.
【0010】運転が開始されると、高温空気導入口15
から高温空気が導入され、ノズル22から液体燃料が噴
霧される。そしてこのとき送り出し口14がノズル22
の近傍にないため、ノズル22近傍での高温空気の流れ
に偏りや乱れが生じにくく、よって噴霧燃料は噴出直後
から高温空気によって偏った方向に強制されてしまうと
いったことがなく、燃焼室13内に十分侵入して広がる
ことができる。[0010] When the operation is started, the high temperature air inlet 15
High temperature air is introduced from the nozzle 22, and liquid fuel is sprayed from the nozzle 22. At this time, the delivery port 14 is connected to the nozzle 22.
Because it is not near the nozzle 22, the flow of high-temperature air in the vicinity of the nozzle 22 is less likely to be biased or turbulent.Therefore, the atomized fuel is not forced in a biased direction by the high-temperature air immediately after it is ejected, and the flow inside the combustion chamber 13 is less likely to occur. can fully invade and spread.
【0011】なお上記実施例では、送り出し口14から
送り出しパイプ24を接線方向に設けているが、半径方
向やその他の方向でもよい。また高温空気導入口15を
外筒11の接線方向に設けているが、ノズル22とは反
対側の端壁12の中心軸上に対向して設けてもよい。In the above embodiment, the delivery pipe 24 is provided in the tangential direction from the delivery port 14, but it may be provided in the radial direction or in any other direction. Further, although the high temperature air inlet 15 is provided in the tangential direction of the outer cylinder 11, it may also be provided on the central axis of the end wall 12 on the opposite side to the nozzle 22.
【0012】0012
【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、ノズルの噴
射口から離れた位置に前記混合気の送り出し口を設けた
ので、ノズル近傍での高温空気の流れに偏りがなく、噴
霧がある程度広がった後、高温空気と接触する。これに
より液体燃料粒子は容器内で十分滞留、分散した後、高
温空気と接触することになり、よって液体燃料の噴霧貫
通度自体が低い場合でも、蒸発室内で十分に高温空気と
接触させることができ、液体燃料の蒸発を安定して効率
よく行うことができる。そのため蒸発容器の小型化も図
ることができる。According to the liquid fuel evaporator according to the first aspect of the present invention, the air-fuel mixture delivery port is provided at a position away from the injection port of the nozzle. The flow of high-temperature air near the nozzle is unbalanced, and the spray spreads to a certain extent before coming into contact with the high-temperature air. As a result, the liquid fuel particles will come into contact with the high-temperature air after being sufficiently retained and dispersed within the container. Therefore, even if the spray penetration of the liquid fuel itself is low, it is possible to sufficiently contact the high-temperature air within the evaporation chamber. This allows stable and efficient evaporation of liquid fuel. Therefore, it is possible to downsize the evaporation container.
【図1】本発明実施装置の一部断面正面図である。FIG. 1 is a partially sectional front view of an apparatus implementing the present invention.
【図2】同実施装置の一部断面側面図である。FIG. 2 is a partially sectional side view of the same implementation device.
【図3】従来装置の一部断面正面図である。FIG. 3 is a partially sectional front view of a conventional device.
【図4】同従来装置の一部断面側面図である。FIG. 4 is a partially sectional side view of the conventional device.
10 蒸発容器 12 端壁 14 混合気の送り出し口 15 高温空気送り込み口 25 燃焼器 10 Evaporation container 12 End wall 14 Mixture outlet 15 High temperature air inlet 25 Combustor
Claims (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、前記ノズルの噴射口から離れた位
置に前記混合気の送り出し口を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 and one of the evaporation containers.
It has at least a nozzle that sprays atomized liquid fuel into the container from a side end wall, and a high-temperature air sending means that sends high-temperature air into the evaporation container, and the atomized liquid fuel sprayed into the evaporation container is transferred to the high-temperature air. A liquid fuel evaporator that evaporates the mixture directly by contact with the liquid fuel and sends the mixture to the combustor side, the mixture having a delivery port located away from the injection port of the nozzle. A liquid fuel evaporation device characterized by:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12214591A JPH04324006A (en) | 1991-04-23 | 1991-04-23 | Liquid fuel evaporator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12214591A JPH04324006A (en) | 1991-04-23 | 1991-04-23 | Liquid fuel evaporator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH04324006A true JPH04324006A (en) | 1992-11-13 |
Family
ID=14828725
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12214591A Pending JPH04324006A (en) | 1991-04-23 | 1991-04-23 | Liquid fuel evaporator |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH04324006A (en) |
-
1991
- 1991-04-23 JP JP12214591A patent/JPH04324006A/en active Pending
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