JPH04324008A - Liquid fuel evaporator - Google Patents
Liquid fuel evaporatorInfo
- Publication number
- JPH04324008A JPH04324008A JP12214791A JP12214791A JPH04324008A JP H04324008 A JPH04324008 A JP H04324008A JP 12214791 A JP12214791 A JP 12214791A JP 12214791 A JP12214791 A JP 12214791A JP H04324008 A JPH04324008 A JP H04324008A
- Authority
- JP
- Japan
- Prior art keywords
- liquid fuel
- temperature air
- nozzle
- 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.)
- Pending
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 49
- 239000007788 liquid Substances 0.000 title claims abstract description 43
- 238000001704 evaporation Methods 0.000 claims abstract description 60
- 230000008020 evaporation Effects 0.000 claims abstract description 59
- 238000007664 blowing Methods 0.000 claims abstract description 5
- 239000007921 spray Substances 0.000 claims description 12
- 238000002347 injection Methods 0.000 claims description 5
- 239000007924 injection Substances 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 4
- 230000035515 penetration Effects 0.000 abstract description 7
- 238000005507 spraying Methods 0.000 abstract description 2
- 239000002245 particle Substances 0.000 description 4
- 238000000889 atomisation Methods 0.000 description 2
- 239000003350 kerosene Substances 0.000 description 2
- 230000007903 penetration ability Effects 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000003014 reinforcing 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 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4
、図5に示す。図4は従来装置の一部断面正面図で、図
5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。液体燃料はタンク4からポンプ5でノズル
3に送られ、さらにカッター等で適当に噴霧量が調整さ
れながら、蒸発室2内へ微粒化状態で導入される。噴霧
カットされた燃料は回収パイプ6を通ってタンク4に戻
る。蒸発容器1には前記ノズル3の噴射口とは反対側の
端壁近くの筒壁に、接線方向に1個の高温空気の導入口
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. 4 shows a conventional example of this type of liquid fuel evaporator.
, shown in FIG. FIG. 4 is a partially sectional front view of a conventional device, and FIG. 5 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 from the tank 4 to the nozzle 3 by a pump 5, and is introduced into the evaporation chamber 2 in an atomized state while the spray amount is appropriately adjusted using a cutter or the like. The sprayed fuel returns to the tank 4 through the recovery pipe 6. The evaporation vessel 1 is provided with one high-temperature air introduction port 7 in the tangential direction on the cylindrical wall near the end wall on the opposite side from the injection port of the nozzle 3. The liquid fuel sprayed into the evaporation chamber 2 is directly vaporized by the hot air 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、ノズル3の噴霧粒子の貫通度(運
動量)が低い場合には、噴霧された液体燃料が十分に蒸
発室2内へ行き渡らない欠点があった。特に、ノズル3
からの噴出量のかなりの部分がカッター等で遮蔽された
場合やノズル3が超音波ノズル等の場合にはノズル3か
ら蒸発容器1内ヘ噴霧された燃料の貫通度(運動量)が
小さいため、高温空気の導入口6から入ってくる多量の
高温空気(運動量が大きい)に押され、蒸発室2内に深
く入って行かなくなる。そのため、実際の蒸発は、ノズ
ル近傍の蒸発室2内でしか起こらず(図5参照)、場合
によっては、未蒸発のまま送り出し口8から送り出され
るという欠点があった。そしてまたこのような状態では
蒸発室2が有効に使われないという欠点があった。一方
、この欠点をなくすため、常温で高速の空気をノズル3
の周囲から噴出するようにしてノズル3による噴霧粒子
の貫通度(運動量)を高くすることも考えられるが、こ
の場合は噴霧された液体燃料への熱伝達が常温の空気を
介して行われるため、蒸発に長時間を要する。However, in the conventional liquid fuel evaporator described above, when the degree of penetration (momentum) of the atomized particles of the nozzle 3 is low, the atomized liquid fuel does not sufficiently spread into the evaporation chamber 2. There were no drawbacks. In particular, nozzle 3
If a considerable part of the amount of fuel ejected from the evaporator is blocked by a cutter or the like, or if the nozzle 3 is an ultrasonic nozzle or the like, the degree of penetration (momentum) of the fuel sprayed from the nozzle 3 into the evaporator container 1 is small. It is pushed by a large amount of high-temperature air (having a large momentum) entering from the high-temperature air inlet 6, and does not go deep into the evaporation chamber 2. Therefore, actual evaporation occurs only in the evaporation chamber 2 near the nozzle (see FIG. 5), and in some cases, there is a drawback that the evaporation is sent out from the delivery port 8 without being evaporated. Another drawback is that the evaporation chamber 2 cannot be used effectively in such a state. On the other hand, in order to eliminate this drawback, air at high speed at room temperature is passed through nozzle 3.
It is also possible to increase the degree of penetration (momentum) of the atomized particles by the nozzle 3 by ejecting them from the surrounding area, but in this case, heat transfer to the atomized liquid fuel is performed through air at room temperature. , it takes a long time to evaporate.
【0004】そこで、本発明は上記従来技術の欠点を解
消し、ノズルから噴霧された液体燃料の貫通度が低い場
合でも、噴霧燃料が蒸発室内へ十分入って行くことがで
き、効率的で安定した蒸発をコンパクトな蒸発室ででき
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 even when the penetration degree of the liquid fuel sprayed from the nozzle is low, the sprayed fuel can sufficiently enter the evaporation chamber, making it efficient and stable. The purpose of the present invention is to provide a liquid fuel evaporation device that can perform evaporation using a compact evaporation chamber.
【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、該ノズルのある側とは反対側の筒壁若
しくは端壁に設けられた導入口から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、前記導入口の
他に前記ノズルの噴射口の周囲から高温空気を蒸発容器
内に吹き出す高温空気補助吹き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,
A nozzle that sprays atomized liquid fuel into the container from one side end wall of the evaporation container, and high-temperature air that sends high-temperature air through an inlet provided in the cylindrical wall or end wall on the opposite side to the side where the nozzle is located. A liquid fuel evaporator having at least a feeding means, directly evaporating the atomized liquid fuel sprayed into the evaporation container by contact with the high temperature air, and sending the mixture to the combustor side. The present invention is characterized in that, in addition to the inlet, a high-temperature air auxiliary outlet is provided for blowing high-temperature air into the evaporation container from around the injection port of the nozzle.
【0006】[0006]
【作用】高温空気がノズルの周囲にある高温空気補助吹
き出し口から噴出される。ノズルから噴霧された液体燃
料粒子はこの高温空気によって貫通度を補強され、蒸発
室に深く侵入する。そしてまた、ノズルから噴霧された
液体燃料粒子は噴出直後から高温空気と積極的に接触す
るので蒸発が促進される。以上によって蒸発室内に噴霧
された液体燃料は高温空気と十分に混合し、効率よく且
つ安定して蒸発を行うことができ、装置もコンパクトに
できる。[Operation] High-temperature air is blown out from the high-temperature air auxiliary outlet around the nozzle. The liquid fuel particles sprayed from the nozzle are reinforced by the high temperature air and penetrate deeply into the evaporation chamber. Further, the liquid fuel particles sprayed from the nozzle actively contact the high temperature air immediately after being ejected, so that evaporation is promoted. As described above, the liquid fuel sprayed into the evaporation chamber is sufficiently mixed with high-temperature air, and evaporation can be performed efficiently and stably, and the apparatus can also be made compact.
【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23を容器10内へ臨ましてなるノズル構
造体20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20に近い方に、蒸発気化さ
れた液体燃料を燃焼器30側へ送り出す送り出し口14
が設けられ、ノズル構造体20から遠い方に、高温空気
導入口15が設けられている。31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。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 20 having a nozzle 23 facing into the container 10 on the central axis is attached to one end wall 12 of the evaporation container 10. Further, in the outer cylinder 11 of the evaporation container 10, a delivery port 14 is provided near the nozzle structure 20 to send out the evaporated liquid fuel to the combustor 30 side.
is provided, and a high-temperature air inlet 15 is provided on the side farther from the nozzle structure 20. 31 is a delivery pipe arranged tangentially from the delivery port 14.
【0009】前記ノズル構造体20は、風向きガイド2
1を介して蒸発容器10の端壁12に取り付けられたノ
ズル取り付け筒22と、該ノズル取り付け筒22内に固
定されたノズル23と、該ノズル23の周囲に進退自在
に取り付けられた可動ガイド24を有する。ノズル23
の噴出口23aは蒸発容器10の中心軸状にあって蒸発
室13内に臨まされている。またノズル23へは、タン
ク70からポンプ71により、灯油等の液体燃料が送油
管72を通って、接続金具73を介して送られる。前記
可動ガイド24には、その先端部に噴霧カッター25が
設けられている。そして可動ガイド24は、前記ノズル
取り付け筒22に取り付け板26を介して支えられたス
テッピングモータ27により、押し棒28及びバネ29
を介して進退自在とされる。The nozzle structure 20 includes a wind direction guide 2
1, a nozzle mounting tube 22 attached to the end wall 12 of the evaporation container 10, a nozzle 23 fixed within the nozzle attaching tube 22, and a movable guide 24 attached around the nozzle 23 so as to be able to move forward and backward. has. Nozzle 23
The spout 23 a is located along the central axis of the evaporation container 10 and faces into the evaporation chamber 13 . Further, liquid fuel such as kerosene is sent from a tank 70 to the nozzle 23 by a pump 71 through an oil feed pipe 72 and via a connecting fitting 73 . The movable guide 24 is provided with a spray cutter 25 at its tip. The movable guide 24 is moved by a push rod 28 and a spring 29 by a stepping motor 27 supported by the nozzle mounting tube 22 via a mounting plate 26.
It is said that it can move forward and backward freely through.
【0010】前記ノズル取り付け筒22と可動ガイド2
4との間が高温空気通路Aとされ、高温空気送り込み手
段40から送風パイプ62を通じて送られてきた高温空
気が高温空気通路Aに入る。そしてこの高温空気通路A
から風向きガイド21を有する高温空気補助吹き出し口
Bを介して高温空気が前記ノズル23の噴出口23a周
囲から蒸発室13内へ噴出される。噴出方向は、風向き
ガイド21により、液体燃料が噴出される噴出口23a
の周囲から蒸発容器10の中心軸方向に向けて斜め内向
きとされる。ノズル23から蒸発室13内へ噴霧された
液体燃料は、高温空気補助吹き出し口Bから吹き出され
た高温空気に乗って蒸発室13の奥深くまで到達する。[0010] The nozzle mounting tube 22 and the movable guide 2
4 is defined as a high-temperature air passage A, and high-temperature air sent from the high-temperature air sending means 40 through the blowing pipe 62 enters the high-temperature air passage A. And this high temperature air passage A
From there, high-temperature air is ejected into the evaporation chamber 13 from around the ejection port 23a of the nozzle 23 via a high-temperature air auxiliary outlet B having a wind direction guide 21. The ejection direction is determined by the wind direction guide 21 from the ejection port 23a through which the liquid fuel is ejected.
It is directed diagonally inward from the periphery toward the central axis direction of the evaporation container 10. The liquid fuel sprayed into the evaporation chamber 13 from the nozzle 23 reaches deep into the evaporation chamber 13 on the high temperature air blown out from the high temperature air auxiliary outlet B.
【0011】なお、前記ノズル23から噴出された液体
燃料の一部は噴霧カッター25でカットされ、可動ガイ
ド部24部分を通って回収パイプ73からタンク70に
戻される。また前記高温空気送り込み手段40からは導
入パイプ43が高温空気導入口15に接線方向に接続さ
ている。A portion of the liquid fuel ejected from the nozzle 23 is cut by the spray cutter 25 and returned to the tank 70 from the recovery pipe 73 through the movable guide section 24. Further, an introduction pipe 43 from the high temperature air feeding means 40 is connected to the high temperature air introduction port 15 in a tangential direction.
【0012】今、運転が開始されると、設定される蒸発
量に応じて可動ガイド24の進退位置が調節され、これ
により噴霧カッター25による遮蔽量が調節されて、必
要量の液体燃料が蒸発室13へ噴霧供給される。と同時
にノズル23の周囲の高温空気補助吹き出し手段Bから
高温空気が噴出されて、その気流に前記噴霧燃料が乗せ
られる。一方、高温空気導入口15から多量の高温空気
が蒸発室13内へ送り込まれる。そしてこの多量の高温
空気に対して前記補助吹き出し口Bからの高温空気によ
って蒸発室13内に十分奥深くまで運ばれた液体燃料が
蒸発室13内全域で十分に接触し、効果的に蒸発せられ
る。なお噴霧の貫通度を補強するための補助吹き出し口
Bからの高温空気と高温空気導入口15からの高温空気
との比率は蒸発容器10の大きさ及びノズル23の種類
、能力等に応じて任意に選ぶことができる。[0012] When the operation is started now, the advance and retreat positions of the movable guide 24 are adjusted according to the set amount of evaporation, and thereby the amount of shielding by the spray cutter 25 is adjusted, so that the required amount of liquid fuel is evaporated. A spray is supplied to the chamber 13. At the same time, high temperature air is ejected from the high temperature air auxiliary blowing means B around the nozzle 23, and the atomized fuel is carried on the airflow. On the other hand, a large amount of high-temperature air is sent into the evaporation chamber 13 from the high-temperature air inlet 15 . The liquid fuel, which has been carried sufficiently deep into the evaporation chamber 13 by the high-temperature air from the auxiliary outlet B, sufficiently contacts this large amount of high-temperature air throughout the evaporation chamber 13 and is effectively evaporated. . Note that the ratio of the high temperature air from the auxiliary outlet B to the high temperature air from the high temperature air inlet 15 for reinforcing the penetration of the spray is arbitrary depending on the size of the evaporation container 10 and the type and capacity of the nozzle 23. You can choose to.
【0013】図3は本発明の他の実施例を示す一部断面
正面図である。この例はノズルとして超音波ノズル83
を設けている。この超音波ノズル83の場合はそれ自体
に噴霧量調節機能を有する。高温空気通路Aや補助吹き
出し口Bが設けられる点は既述の実施例の場合と同様で
ある。同様の部材、要素には同一の符号を付して示して
いる。FIG. 3 is a partially sectional front view showing another embodiment of the present invention. In this example, an ultrasonic nozzle 83 is used as the nozzle.
has been established. The ultrasonic nozzle 83 itself has a spray amount adjustment function. The provision of a high temperature air passage A and an auxiliary outlet B is the same as in the previously described embodiments. Similar members and elements are designated by the same reference numerals.
【0014】なお、以上の実施例においては、高温空気
導入口15からの高温空気を外筒11の接線方向に導入
しているが、高温空気導入口15をノズル23、83と
は反対側の端壁12の中心軸上に設けてもよい。また補
助吹き出し口Bから蒸発室13内へ吹き出される高温空
気は蒸発室10の中心軸線方向に向けて斜め内向きとす
る他、ノズル23、83の貫通能力に応じてその方向を
中心軸方向あるいは任意の角度としてもよい。また上記
実施例において噴霧装置としてのノズルの形状、種類は
特に限定されるものではない。例えば、空気ノズルの場
合、微粒化に用いる空気を加熱してもよい。また極めて
噴霧貫通能力の低い微粒化装置を用いる場合、高温空気
の導入は噴出口の後方からのみ行ってもよい。In the above embodiment, the high temperature air from the high temperature air inlet 15 is introduced in the tangential direction of the outer cylinder 11, but the high temperature air inlet 15 is connected to the opposite side from the nozzles 23 and It may be provided on the central axis of the end wall 12. In addition, the high temperature air blown into the evaporation chamber 13 from the auxiliary outlet B is directed diagonally inward toward the central axis of the evaporation chamber 10, and the direction is directed toward the central axis depending on the penetration ability of the nozzles 23, 83. Alternatively, it may be set at an arbitrary angle. Further, in the above embodiments, the shape and type of the nozzle used as the spray device are not particularly limited. For example, in the case of an air nozzle, the air used for atomization may be heated. Furthermore, when using an atomization device with extremely low spray penetration ability, high-temperature air may be introduced only from the rear of the jet nozzle.
【0015】[0015]
【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、高温空気導
入口の他に前記ノズルの噴射口の周囲から高温空気を蒸
発容器内に吹き出す高温空気補助吹き出し口を設けたの
で、ノズルからの噴霧液体燃料を補助吹き出し口からの
高温空気によって蒸発室内に十分深く送り込むことがで
きる。しかも噴霧液体燃料は噴出直後から高温空気と積
極的に接触するので蒸発が促進される。よって液体燃料
の噴霧の貫通度自体が低い場合でも、蒸発室内全域で十
分に全ての高温空気と接触することができ、液体燃料の
蒸発を安定して効率よく行うことができる。またそのた
め蒸発容器の小型化も図ることができる。Effects of the Invention According to the liquid fuel evaporator according to claim 1, the present invention has the above-described structure and operation.In addition to the high-temperature air inlet, high-temperature air is supplied to the evaporator vessel from around the injection port of the nozzle. Since the auxiliary hot air outlet is provided, the atomized liquid fuel from the nozzle can be sent sufficiently deep into the evaporation chamber by the hot air from the auxiliary outlet. Moreover, since the sprayed liquid fuel comes into active contact with high-temperature air immediately after being ejected, evaporation is promoted. Therefore, even if the degree of penetration of the liquid fuel spray itself is low, it can sufficiently contact all the high temperature air throughout the evaporation chamber, and the liquid fuel can be evaporated stably and efficiently. Moreover, the evaporation container can therefore be made smaller.
【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】本発明の他の実施装置の一部断面正面図である
。FIG. 3 is a partially sectional front view of another implementation device of the present invention.
【図4】従来装置の一部断面側面図である。FIG. 4 is a partially sectional side view of a conventional device.
【図5】同従来装置の一部断面側面図である。FIG. 5 is a partially sectional side view of the conventional device.
10 蒸発容器 12 端壁 15 高温空気導入口 23、83 ノズル 30 燃焼器 40 高温空気送り込み手段 B 高温空気補助吹き出し口 10 Evaporation container 12 End wall 15 High temperature air inlet 23, 83 nozzle 30 Combustor 40 High temperature air feeding means B High temperature air auxiliary outlet
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
、該ノズルのある側とは反対側の筒壁若しくは端壁に設
けられた導入口から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、前記導入口の他に前記ノズル
の噴射口の周囲から高温空気を蒸発容器内に吹き出す高
温空気補助吹き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 from an inlet provided in the cylinder wall or end wall on the opposite side to the side where the nozzle is located. The liquid fuel evaporator is configured to directly evaporate the atomized liquid fuel sprayed into the evaporation container through contact with the high-temperature air and send the mixture to the combustor side, A liquid fuel evaporator characterized in that, in addition to the inlet, a high-temperature air auxiliary outlet is provided for blowing high-temperature air into the evaporator container from around the injection port of the nozzle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12214791A JPH04324008A (en) | 1991-04-23 | 1991-04-23 | Liquid fuel evaporator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12214791A JPH04324008A (en) | 1991-04-23 | 1991-04-23 | Liquid fuel evaporator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH04324008A true JPH04324008A (en) | 1992-11-13 |
Family
ID=14828772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12214791A Pending JPH04324008A (en) | 1991-04-23 | 1991-04-23 | Liquid fuel evaporator |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH04324008A (en) |
-
1991
- 1991-04-23 JP JP12214791A patent/JPH04324008A/en active Pending
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