JPH0484006A - Liquid fuel burner - Google Patents
Liquid fuel burnerInfo
- Publication number
- JPH0484006A JPH0484006A JP19737290A JP19737290A JPH0484006A JP H0484006 A JPH0484006 A JP H0484006A JP 19737290 A JP19737290 A JP 19737290A JP 19737290 A JP19737290 A JP 19737290A JP H0484006 A JPH0484006 A JP H0484006A
- Authority
- JP
- Japan
- Prior art keywords
- liquid fuel
- fuel
- evaporation chamber
- combustion
- dripping
- 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
Landscapes
- Evaporation-Type Combustion Burners (AREA)
Abstract
Description
【発明の詳細な説明】
〈産業上の利用分野〉
本発明は石油等の液体燃料を加熱された空気により、比
較的低い温度で直接的に蒸発気化させ、燃焼に供するよ
うにした燃料燃焼装置に関する。[Detailed Description of the Invention] <Industrial Application Field> The present invention provides a fuel combustion device in which liquid fuel such as petroleum is directly evaporated and vaporized at a relatively low temperature using heated air, and is then combusted. Regarding.
〈従来の技術〉
加熱された空気中に液体燃料を供給し、比較的低い温度
で直接的に蒸発気化し、燃焼を行う装置として、本出願
人は既に特願平1−302965号等で、無気噴出ノズ
ルを用いた装置を提供した。この装置を第5図(A)、
(B)を用いて説明する。第5図(A)は従来装置の全
体構成図、第5図(B)は第5図(A)のD−D断面図
である。空気がファンlで取り入れられ、供給路2を通
って蒸発室3に送り込まれる。4は電気ヒータで、空気
を途中で加熱するためのものである。一方、石油等の液
体燃料が噴出ノズル5を介して微粒化状態で蒸発室3内
に噴出せられる。そして蒸発室3内で微粒化した液体燃
料が加熱空気によって直接的に接触、蒸発気化され、空
気との混合気となって燃焼部6に送られ、燃焼に供され
る。<Prior Art> The present applicant has already disclosed in Japanese Patent Application No. 1-302965, etc., an apparatus for supplying liquid fuel into heated air, evaporating it directly at a relatively low temperature, and combusting it. A device using an airless jet nozzle was provided. This device is shown in Figure 5 (A).
This will be explained using (B). FIG. 5(A) is an overall configuration diagram of a conventional device, and FIG. 5(B) is a sectional view taken along line DD in FIG. 5(A). Air is taken in by a fan l and sent through a supply path 2 into an evaporation chamber 3. 4 is an electric heater for heating the air midway. On the other hand, liquid fuel such as petroleum is ejected into the evaporation chamber 3 in an atomized state through the ejection nozzle 5 . Then, the liquid fuel atomized in the evaporation chamber 3 is brought into direct contact with the heated air, evaporates and vaporized, becomes a mixture with air, and is sent to the combustion section 6 for combustion.
〈発明が解決しようとする課題〉
ところが上記従来技術では、噴出ノズル5を用い、高圧
を利用して液体燃料を微粒化するため、ノズル5先端の
開口部が非常に小さくなり、ゴミなどの異物による詰ま
り避けるために小流量(17!/時間)のノズルは、実
用には供することができないという欠点があった。<Problems to be Solved by the Invention> However, in the above-mentioned conventional technology, the jet nozzle 5 is used and the liquid fuel is atomized using high pressure, so the opening at the tip of the nozzle 5 becomes very small, and foreign matter such as dust can be removed. A nozzle with a small flow rate (17!/hour) in order to avoid clogging due to this problem had the disadvantage that it could not be put to practical use.
また噴射ノズル5に加わる圧力を変化させて噴霧流量を
変化させようとしても、流量が圧力の二乗に例するため
、大きな絞り比(T、D、R)を取れないという欠点が
あった。Further, even if an attempt is made to change the spray flow rate by changing the pressure applied to the injection nozzle 5, there is a drawback that a large aperture ratio (T, D, R) cannot be achieved because the flow rate is the square of the pressure.
また噴射ノズル5で噴霧する場合には、噴霧がある角度
を持って広がり、蒸発室3の内壁面に当たり易く、壁面
で凝縮しやすい欠点があった。Furthermore, when spraying with the injection nozzle 5, the spray spreads at a certain angle, tends to hit the inner wall surface of the evaporation chamber 3, and has the disadvantage that it tends to condense on the wall surface.
そこで本発明は上記従来装置の欠点を解消することがで
き、しかも比較的低い温度で液体燃料を直接的に蒸発気
化して、燃焼に供することができる液体燃料燃焼装置の
提供を目的とする。SUMMARY OF THE INVENTION Therefore, an object of the present invention is to provide a liquid fuel combustion device that can eliminate the drawbacks of the conventional devices described above, and that can directly evaporate liquid fuel at a relatively low temperature and use it for combustion.
〈課題を解決するための手段〉
上記目的を達成するため、本発明の液体燃料燃焼装置は
、粒化された液体燃料を蒸発室内で加熱空気により直接
的に接触暴発させ、得られた混合気を燃焼部に送って燃
焼に供するようにした液体燃料燃焼装置であって、前記
蒸発室の上部に液体燃料を細粒化して滴下させる液体燃
料滴下手段を設け、該手段から滴下してくる液体燃料を
加熱空気による上昇気流で直接的に蒸発させるよう構成
し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 combustion device of the present invention causes granulated liquid fuel to contact and explode directly with heated air in an evaporation chamber, and the resulting mixture A liquid fuel combustion device is provided in which liquid fuel is sent to a combustion section for combustion, and a liquid fuel dripping means is provided above the evaporation chamber to finely drop the liquid fuel, and the liquid that drips from the means is provided. It is characterized by a structure in which the fuel is directly evaporated by the upward current of heated air.
〈作用〉
蒸発室の上方から落下してくる液体燃料の細粒が下方か
ら吹き上げてくる加熱空気によって直接的に接触せられ
、比較的低温で蒸発せられる。そして燃料と空気の混合
気となって燃焼部へ送られ、燃焼に供される。滴下され
る細粒は、従来の噴射ノズルによる場合に比べて、直径
が太き(なるので、蒸発しきれないものも生じるが、蒸
発室の下方で回収して、再利用できる。噴射ノズルの代
わりに液体燃料滴下手段を用いることにより、小流量(
11/時間、以下)でもノズル詰まりが生じない。また
滴下流量の絞り比の幅を大きくとることができる。また
噴射ノズルの如く液体が一定の角度をもって噴霧される
ことがないので、蒸発室の内壁で蒸発燃料が凝縮される
ことも減少される。<Operation> Fine particles of liquid fuel falling from above the evaporation chamber are brought into direct contact with heated air blowing up from below, and are evaporated at a relatively low temperature. A mixture of fuel and air is then sent to the combustion section where it is combusted. The fine particles that are dropped have a larger diameter than when using a conventional injection nozzle, so some particles may not be completely evaporated, but they can be collected below the evaporation chamber and reused. By using liquid fuel dripping means instead, small flow rates (
11/hour or less), no nozzle clogging occurs. Further, the range of the aperture ratio of the dripping flow rate can be increased. Further, since the liquid is not sprayed at a fixed angle as in the case of an injection nozzle, condensation of the evaporated fuel on the inner wall of the evaporation chamber is also reduced.
〈実施例〉
第1図は本発明実施装置の全体構成図、第2図は実施装
置の部分詳細図、第3図は実施装置の平面図である。<Example> FIG. 1 is an overall configuration diagram of an apparatus for implementing the present invention, FIG. 2 is a partial detailed view of the apparatus for implementing the invention, and FIG. 3 is a plan view of the apparatus for implementing the invention.
縦長の筒状容器10内に蒸発室11が設けられている。An evaporation chamber 11 is provided within a vertically long cylindrical container 10.
蒸発室11の下部側壁に加熱空気の導入バイブ12が接
続され、蒸発室11の上部側壁に混合気を燃焼部14へ
導く送出パイプ13が接続されている。加熱空気は図示
しない送風ファンによって送られ、途中でヒータ15に
より加熱された後、導入パイプ12を通って蒸発室11
に入り、上昇気流となる。A heating air introduction vibe 12 is connected to the lower side wall of the evaporation chamber 11, and a delivery pipe 13 for guiding the air-fuel mixture to the combustion section 14 is connected to the upper side wall of the evaporation chamber 11. The heated air is sent by a blower fan (not shown), heated by a heater 15 on the way, and then passed through an introduction pipe 12 to the evaporation chamber 11.
and becomes an updraft.
前記蒸発室11の上部天井部には液体燃料滴下手段とし
て油タンク21と複数の中空ニードル22が設けられて
いる。前記油タンク21には、定油面器23から液体燃
料を供給する送油ポンプ24と連通した送油管25と、
油タンク21が溢れるのを防ぐ戻し管26とが接続され
ている。また前記蒸発室11の最下端に未蒸発燃料費は
部16が設けられ、蒸発室11で蒸発されなかった液体
燃料を受は取って、回収管17で定油面器23へ戻すよ
うになされている。An oil tank 21 and a plurality of hollow needles 22 are provided on the upper ceiling of the evaporation chamber 11 as liquid fuel dripping means. The oil tank 21 includes an oil feed pipe 25 that communicates with an oil feed pump 24 that supplies liquid fuel from an oil level regulator 23;
A return pipe 26 is connected to prevent the oil tank 21 from overflowing. Further, an unevaporated fuel collecting section 16 is provided at the lowermost end of the evaporation chamber 11 to receive liquid fuel that has not been evaporated in the evaporation chamber 11 and return it to the oil level regulator 23 through a collection pipe 17. ing.
前記中空ニードル22は液体燃料を油タンク21から蒸
発室11に滴下するためのもので、油タンク21の底か
ら蒸発室11側へ突出しており、また油タンク21内へ
も高さHだけ突出している。油タンク21内の液体燃料
は中空ニードル22の細い穴を通って蒸発室11に滴下
される。The hollow needle 22 is for dropping liquid fuel from the oil tank 21 into the evaporation chamber 11, and protrudes from the bottom of the oil tank 21 toward the evaporation chamber 11, and also protrudes into the oil tank 21 by a height H. ing. The liquid fuel in the oil tank 21 is dripped into the evaporation chamber 11 through a narrow hole in the hollow needle 22.
ヒータ15で加熱された空気は、導入バイブ12から蒸
発室11内に導かれ、上昇気流として上向きに流れる。The air heated by the heater 15 is guided into the evaporation chamber 11 from the introduction vibe 12 and flows upward as an upward air current.
一方、油タンク21には中空ニードル22の上端部まで
の高さHだけ予め液体燃料が供給されており、送油ポン
プ24から送られてくる新たな液体燃料は、中空ニード
ル22の上端部から高さhの所に液面を形成する。高さ
hが中空ニードル22通路抵抗に打ち勝つまで高くなる
と、液体燃料が中空ニードル22の下端より液滴となっ
て落下し始める。もし中空ニードル22を油タンク21
内に突き出さず、油タンク21の底に取り付ける場合に
は、送油管25の油タンク21への入口と各中空ニード
ル22との距離が一定でないため、燃料供給の初期段階
や終了段階で滴下している中空ニードル22と滴下して
いない中空ニードル22とが存在し、燃料供給に過渡特
性が生じる。中空ニードル22が油タンク21内に突き
出すことにより、蒸発室11への燃料供給は油タンク2
1液面の上下動に変換され、各二ドル22が一斉に滴下
を開始し、また停止する。On the other hand, liquid fuel is previously supplied to the oil tank 21 by a height H up to the upper end of the hollow needle 22, and new liquid fuel sent from the oil pump 24 is fed from the upper end of the hollow needle 22. A liquid level is formed at a height h. When the height h becomes high enough to overcome the passage resistance of the hollow needle 22, the liquid fuel starts to fall from the lower end of the hollow needle 22 in the form of droplets. If the hollow needle 22 is attached to the oil tank 21
If it is attached to the bottom of the oil tank 21 instead of protruding inward, the distance between the entrance of the oil pipe 25 to the oil tank 21 and each hollow needle 22 is not constant, so that dripping occurs at the initial stage or end stage of fuel supply. There are hollow needles 22 that are dripping and hollow needles 22 that are not dripping, causing transient characteristics in the fuel supply. Since the hollow needle 22 protrudes into the oil tank 21, fuel is supplied to the evaporation chamber 11 from the oil tank 2.
This is converted into an up and down movement of the liquid level, and each droplet 22 starts and stops dropping at the same time.
前記中空ニードル22から細粒となって滴下した液体燃
料は上昇してくる加熱空気と接触し、蒸発気化される。The liquid fuel dripping from the hollow needle 22 in the form of fine particles comes into contact with the rising heated air and is evaporated.
そして混合気となって送出バイブ13を通って燃焼部1
4へ送られ、燃焼せられる。Then, it becomes an air-fuel mixture and passes through the sending vibe 13 to the combustion section 1.
4 and burned.
前記中空ニードル22の内径や本数は装置の規模等に応
じて任意に設計することができる。The inner diameter and number of the hollow needles 22 can be arbitrarily designed depending on the scale of the apparatus and the like.
なお、中空ニードル22から滴下される液滴は、従来の
噴射ノズルのそれに比べて、直径が大きめになる。その
ため、液滴は、蒸発室11の高さにもよるが、完全には
蒸発しきれず、下部の未蒸発燃料費は部16まで到達す
ることがあるが、該未蒸発燃料費は部16は前記加熱空
気の導入パイプ12接続口より低く、壁面温度があまり
高くならないようにされているので、蒸発はせず、回収
管14によって定油面器23に戻され、再利用される。Note that the droplet dropped from the hollow needle 22 has a larger diameter than that of a conventional injection nozzle. Therefore, depending on the height of the evaporation chamber 11, the droplets may not be completely evaporated and the unevaporated fuel cost in the lower part may reach part 16; Since it is lower than the connection port of the heated air introduction pipe 12 and the wall surface temperature is not too high, it does not evaporate and is returned to the oil level regulator 23 through the recovery pipe 14 and reused.
また、従来の噴射ノズルを用いる場合には、噴霧がある
角度を持って広がり、蒸発室の側面に衝突し易くなるの
に対して、本発明では中空ニードル22から液滴が重力
によって真下に滴下するので、蒸発室側面に液滴が衝突
する可能性が少なくなり、側面で蒸気が凝縮する欠点が
減少する。よってまた各部材のレイアウトの自由度が増
す。In addition, when using a conventional injection nozzle, the spray spreads at a certain angle and tends to collide with the side of the evaporation chamber, whereas in the present invention, the droplets drop directly downward from the hollow needle 22 due to gravity. Therefore, the possibility of droplets colliding with the sides of the evaporation chamber is reduced, and the disadvantage of vapor condensation on the sides is reduced. This also increases the degree of freedom in the layout of each member.
前記筒状容器10は円筒状とする他、正方形断面、その
他矩形断面とすることができるが、本実施例の如く、円
筒状の筒状容器10を用いる場合には、第3図に示す如
(、加熱空気を筒状容器10に接線方向に導入するよう
にすることで、筒状容器10や全体を小型化することが
できる。The cylindrical container 10 may have a cylindrical shape, a square cross section, or a rectangular cross section. However, when a cylindrical container 10 is used as in this embodiment, a shape as shown in FIG. 3 is used. (By introducing the heated air tangentially into the cylindrical container 10, the cylindrical container 10 and the whole can be downsized.
第4図(A)、(B)は本発明の他の実施装置の全体構
成図と平面図である。この実施装置は矩形断面の筒状容
器10を用いた場合の各部のレイアウト例を示す。各部
を図のようなレイアウトにすることで、筒状容器lOや
全体を小型化することができる。装置の作用、効果は既
述の実施例と同様である。同一の機能を有する部材には
同一の符号を付して、説明を省く。FIGS. 4(A) and 4(B) are an overall configuration diagram and a plan view of another implementation device of the present invention. This implementation device shows an example of the layout of each part when a cylindrical container 10 with a rectangular cross section is used. By arranging each part as shown in the figure, the cylindrical container IO and the entire container can be downsized. The functions and effects of the device are similar to those of the previously described embodiments. The same reference numerals are given to members having the same functions, and the description thereof will be omitted.
〈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
料燃焼装置によれば、蒸発室の上部に液体燃料を細粒化
して滴下させる液体燃料滴下手段を設け、該手段から滴
下してくる液体燃料を加熱空気による上昇気流で直接的
に蒸発させるよう構成しているので、液体燃料を比較的
低い温度で直接的に蒸発気化することができる。よって
タール分等が少なく、また省エネである。また噴射ノズ
ルを用いる代わりに液体燃料滴下手段を用いることによ
り、燃料詰まりの少ない、且つ絞り比の大きな液体燃料
の供給が可能となる。さらに蒸発燃料の蒸発室の壁面で
の凝縮が少なくなり、また装置各部のレイアウトの自由
度が増す。<Effects> The present invention has the above configuration, and according to the liquid fuel combustion apparatus according to claim 1, a liquid fuel dripping means for finely dropping liquid fuel is provided in the upper part of the evaporation chamber, and the liquid fuel is dripped from the means. Since the liquid fuel that is dripped is directly evaporated by the rising airflow of heated air, the liquid fuel can be directly evaporated and vaporized at a relatively low temperature. Therefore, there is less tar, etc., and energy is saved. Furthermore, by using a liquid fuel dripping means instead of using an injection nozzle, it is possible to supply liquid fuel with less fuel clogging and a large aperture ratio. Furthermore, condensation of evaporated fuel on the wall surface of the evaporation chamber is reduced, and the degree of freedom in layout of various parts of the apparatus is increased.
第1図は本発明実施装置の全体構成図、第2図は実施装
置の部分詳細図、第3図は実施装置の平面図、第4図(
A)、(B)は他の実施例を示し、(A)は全体構成図
、(B)は平面図、第5図(A)、(B)は従来例を示
し、(A)は全体構成図、(B)は(A)図のD−D断
面図である。
11:蒸発室
12:
14:
15:
21:
22:
25:
加熱空気の導入パイプ
燃焼部
ヒータ
油タンク
中空ニードル
送油管Fig. 1 is an overall configuration diagram of an apparatus for implementing the present invention, Fig. 2 is a partial detailed view of the apparatus for implementing the invention, Fig. 3 is a plan view of the apparatus for implementing the invention, and Fig. 4 (
A) and (B) show other embodiments, (A) is an overall configuration diagram, (B) is a plan view, and FIGS. 5 (A) and (B) are conventional examples, and (A) is an overall The configuration diagram, (B) is a cross-sectional view taken along line DD in the diagram (A). 11: Evaporation chamber 12: 14: 15: 21: 22: 25: Heated air introduction pipe Combustion section Heater oil tank Hollow needle oil supply pipe
Claims (1)
直接的に接触蒸発させ、得られた混合気を燃焼部に送っ
て燃焼に供するようにした液体燃料燃焼装置であって、
前記蒸発室の上部に液体燃料を細粒化して滴下させる液
体燃料滴下手段を設け、該手段から滴下してくる液体燃
料を加熱空気による上昇気流で直接的に蒸発させるよう
構成したことを特徴とする液体燃料燃焼装置。(1) A liquid fuel combustion device in which granulated liquid fuel is directly catalytically evaporated with heated air in an evaporation chamber, and the resulting mixture is sent to a combustion section for combustion,
A liquid fuel dripping means is provided in the upper part of the evaporation chamber to drop the liquid fuel into fine particles, and the liquid fuel dripping from the means is directly evaporated by an upward current of heated air. liquid fuel combustion equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19737290A JPH0484006A (en) | 1990-07-25 | 1990-07-25 | Liquid fuel burner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19737290A JPH0484006A (en) | 1990-07-25 | 1990-07-25 | Liquid fuel burner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0484006A true JPH0484006A (en) | 1992-03-17 |
Family
ID=16373408
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19737290A Pending JPH0484006A (en) | 1990-07-25 | 1990-07-25 | Liquid fuel burner |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0484006A (en) |
-
1990
- 1990-07-25 JP JP19737290A patent/JPH0484006A/en active Pending
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