JPH0484005A - Liquid fuel burner - Google Patents
Liquid fuel burnerInfo
- Publication number
- JPH0484005A JPH0484005A JP19737190A JP19737190A JPH0484005A JP H0484005 A JPH0484005 A JP H0484005A JP 19737190 A JP19737190 A JP 19737190A JP 19737190 A JP19737190 A JP 19737190A JP H0484005 A JPH0484005 A JP H0484005A
- Authority
- JP
- Japan
- Prior art keywords
- porous body
- liquid fuel
- heated air
- evaporation chamber
- 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.)
- Pending
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 56
- 239000007788 liquid Substances 0.000 title claims abstract description 43
- 238000002485 combustion reaction Methods 0.000 claims abstract description 23
- 238000001704 evaporation Methods 0.000 claims abstract description 21
- 230000008020 evaporation Effects 0.000 claims abstract description 20
- 239000000203 mixture Substances 0.000 claims abstract description 7
- 238000007664 blowing Methods 0.000 claims abstract description 3
- 238000004891 communication Methods 0.000 abstract description 3
- 239000011148 porous material Substances 0.000 abstract description 2
- 239000012528 membrane Substances 0.000 abstract 1
- 239000011800 void material Substances 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 7
- 238000002347 injection Methods 0.000 description 6
- 239000007924 injection Substances 0.000 description 6
- 239000007921 spray Substances 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 2
- 239000003208 petroleum Substances 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
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
ルを用いた装置を捉供した。この装置を第6図(A)、
(B)を用いて説明する。第6図(A)は従来装置の全
体構成図、第6図(B)は第6図(A)のD−D断面図
である。空気がファン1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 used. This device is shown in Figure 6 (A).
This will be explained using (B). FIG. 6(A) is an overall configuration diagram of a conventional device, and FIG. 6(B) is a sectional view taken along line DD in FIG. 6(A). Air is taken in by a fan 1 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(ll/時間、以下)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 (1 liter/hour, or less) to avoid clogging due to this problem has the disadvantage that it cannot be used practically.
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
、液体燃料の供給手段と、加熱空気送風手段とを有し、
蒸発室内で液体燃料を加熱空気で直接的に蒸発気化し、
得られた混合気を燃焼部へ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、前記蒸発室内に多孔質体
を配置し、該多孔質体に対して前記液体燃料を供給する
と共に多孔質体を通過するようにして前記加熱空気を送
風し、前記多孔質体内を降下する液体燃料を多孔質体内
を通過する加熱空気で直接的に蒸発気化することを特徴
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 has a liquid fuel supply means, a heated air blowing means,
Liquid fuel is directly evaporated with heated air in the evaporation chamber,
A liquid fuel combustion device configured to send the obtained air-fuel mixture to a combustion section for combustion, wherein a porous body is disposed within the evaporation chamber, the liquid fuel is supplied to the porous body, and the liquid fuel is supplied to the porous body. The heated air is blown through the porous body, and the liquid fuel falling inside the porous body is directly evaporated and vaporized by the heated air passing through the porous body.
く作用〉
上記本発明の特徴によれば、蒸発室内の多孔質体に供給
された液体燃料は、多孔質体内を空隙に沿って降下する
。また加熱空気は多孔質体内の空隙を吹き抜ける。そし
てその際、膜状になった液体燃料が加熱空気によって比
較的低い温度で直接的に蒸発気化され、加熱空気と共に
多孔質体から出て、混合気となって燃焼部へ送られる。Effect> According to the features of the present invention described above, the liquid fuel supplied to the porous body within the evaporation chamber descends along the voids within the porous body. The heated air also blows through the voids within the porous body. At that time, the liquid fuel in the form of a film is directly evaporated and vaporized by the heated air at a relatively low temperature, exits the porous body together with the heated air, and is sent to the combustion section as an air-fuel mixture.
噴射ノズルの代わりに多孔質体を用いているので、燃料
詰まりの虞れがなくなる。また大流量から小流量まで絞
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。Since a porous body is used instead of the injection nozzle, there is no risk of fuel clogging. Furthermore, the throttle ratio can be varied widely from large flow rates to small flow rates. 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図は多孔質
体部分の拡大発明図、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 an enlarged inventive diagram of a porous body portion, and FIG. 3 is a plan view of the apparatus for implementing the present invention.
蒸発室10に多孔質体11を配置し、送られて(る加熱
空気が必ず前記多孔質体11を通過するようにする。前
記加熱空気はヒータ21と図示しないファンとからなる
加熱空気送風手段によって供給される。すなわち図示し
ない送風ファンによって送られてくる空気がヒータ21
を通る際に加熱され、高温空気となって蒸発室10に送
られる。A porous body 11 is arranged in the evaporation chamber 10 so that the heated air that is sent always passes through the porous body 11. In other words, air sent by a blower fan (not shown) is supplied to the heater 21.
The air is heated as it passes through the air, becomes high-temperature air, and is sent to the evaporation chamber 10.
前記多孔質体11に対しては、定油面器31と送油管3
2と送油ポンプ33とからなる液体燃料供給手段によっ
て、多孔質体11の上端面部に液体燃料が供給される。For the porous body 11, an oil level regulator 31 and an oil pipe 3 are connected.
Liquid fuel is supplied to the upper end surface portion of the porous body 11 by a liquid fuel supply means consisting of a fuel pump 2 and an oil feed pump 33.
液体燃料りは多孔質体11を空隙に沿って重力で下方へ
降下してゆく。多孔質体11の途中で蒸発気化されなか
った分は多孔質体11下端の未蒸発燃料費は部41まで
達し、回収管42によって前記定油面器31に戻される
。The liquid fuel falls downward through the porous body 11 by gravity along the voids. The unevaporated fuel at the lower end of the porous body 11 that is not evaporated midway through the porous body 11 reaches a portion 41 and is returned to the oil level regulator 31 through the recovery pipe 42 .
前記蒸発室lOの下流側に連通して燃焼部50が設けら
れている。A combustion section 50 is provided in communication with the downstream side of the evaporation chamber IO.
前記多孔質体11の空隙率を比較的高くし、且つ表面と
内部の空隙との連通性のよいものを用いることによって
、前記供給された加熱空気Aは多孔質体11内をスムー
ズに流れる。一方、液体燃料りが多孔質体11を上から
下へ空隙に沿って降下する。そしてその時、膜状になっ
た液体燃料が加熱空気で直接的に加熱され、比較的低い
温度で蒸発気化し、混合気となって多孔質体11外へ出
、燃焼部50へ送られ、燃焼せられる。By making the porous body 11 relatively high in porosity and having good communication between the surface and the internal voids, the supplied heated air A flows smoothly inside the porous body 11. On the other hand, the liquid fuel descends from the top to the bottom of the porous body 11 along the voids. At that time, the liquid fuel in the form of a film is directly heated by the heated air, evaporates and vaporizes at a relatively low temperature, becomes an air-fuel mixture, exits the porous body 11, is sent to the combustion section 50, and is combusted. be given
燃焼部50への混合気供給量は送油ポンプ33流量を変
更し、また加熱空気の供給手段であるヒータ21及び図
示しない送風ファンの強弱を調整することにより行うこ
とができる。そして多孔質体11を従来の噴射ノズルの
代わりに用いることにより、小流量(11!/時間、以
下)でもノズル詰まりのない、且つ絞り比の大きな液体
燃料の供給が可能となった。The amount of air-fuel mixture supplied to the combustion section 50 can be controlled by changing the flow rate of the oil pump 33 and by adjusting the strength of the heater 21 and the blower fan (not shown), which are means for supplying heated air. By using the porous body 11 in place of a conventional injection nozzle, it has become possible to supply liquid fuel with a large throttle ratio without clogging the nozzle even at a small flow rate (11!/hour or less).
また、多孔質体11そのものを加熱するのではなく、加
熱空気で液体燃料を加熱、蒸発させるので、比較的低温
で液体燃料が蒸発し、タール状物質の発生及びタール状
物質の多孔質体11への付着、閉塞の虞れが回避できる
。In addition, since the liquid fuel is heated and evaporated with heated air instead of heating the porous body 11 itself, the liquid fuel evaporates at a relatively low temperature, and tar-like substances are generated and the porous body 11 is made of tar-like substances. This avoids the risk of adhesion and blockage.
また噴射ノズルを用いる場合は、噴霧がある角度を持っ
て広がり、蒸発室の内壁等に衝突し易くなるのに対し、
多孔質体11を用いる場合には、燃料が液体のままで多
孔質体11以外に触れることはない。よって多孔質体1
1配置部以外は自由に部材をレイアウトすることができ
る。In addition, when using an injection nozzle, the spray spreads at a certain angle, making it easier to collide with the inner wall of the evaporation chamber.
When the porous body 11 is used, the fuel remains in liquid form and does not touch anything other than the porous body 11. Therefore, porous body 1
Members can be freely laid out except for one arrangement section.
第3図、第4図はそれぞれ第1図とはレイアウトを変更
した他の実施例を示す。同一機能、作用をなす部材、要
素には第1図で説明した部材、要素の符号と同一の符号
を付して説明を省くが、作用、効果も第1図の場合と同
様である。3 and 4 respectively show other embodiments in which the layout is changed from that in FIG. 1. Members and elements having the same functions and actions are designated by the same reference numerals as those explained in FIG. 1, and their explanations are omitted, but the actions and effects are also the same as in FIG. 1.
第5図にさらに他の実施例を示す。この実施例では蒸発
室10内に多孔質体11を環状に形成して配置し、加熱
空気を多孔質体11の外周側から内周側へ通過させて、
液体燃料を蒸発気化させるようにしている。他の点は既
に説明した実施例と同様である。既述した実施例の部材
と同一の部材、要素には同一の符号を付している。FIG. 5 shows yet another embodiment. In this embodiment, a porous body 11 is arranged in an annular shape in an evaporation chamber 10, and heated air is passed from the outer circumferential side of the porous body 11 to the inner circumferential side.
The liquid fuel is evaporated. Other points are similar to the embodiments already described. The same members and elements as those in the previously described embodiments are given the same reference numerals.
く効果〉
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、多孔質体を用いて液体燃料と加熱
空気の接触面積を増すようにしているので、液体燃料を
微粒化して供給する場合と同様に、比較的低い温度で燃
料を直接的に蒸発気化することができる。よってタール
分等の発生が少なく、また省エネである。また特に多孔
質体を用いることにより、大流量から小流量まで目詰ま
りすることなく、しかも絞り比の大きな液体燃料の供給
が可能となり、燃焼力の調節が容易となった。Effects> The present invention has the above configuration, and according to the liquid fuel combustion apparatus according to claim 1, since the porous body is used to increase the contact area between the liquid fuel and the heated air, the liquid fuel Similar to the case where fuel is atomized and supplied, it is possible to directly evaporate the fuel at a relatively low temperature. Therefore, less tar is generated and energy is saved. Furthermore, by using a porous material in particular, it has become possible to supply liquid fuel from large flow rates to small flow rates without clogging and with a large throttle ratio, making it easy to adjust the combustion power.
また多孔質体を用いることにより、噴°射ノズルを用い
る場合に比べて、装置各部のレイアウトの自由度を増す
ことができた。Furthermore, by using a porous body, it was possible to increase the degree of freedom in the layout of each part of the device compared to the case where a spray nozzle was used.
第1図は本発明実施装置の全体構成図、第2図は多孔質
体部分の拡大説明図、第3図と第4図はそれぞれ他の実
施装置の全体構成図、第5図はさらに他の実施装置の全
体構成図、第6図(A)は従来装置の全体構成図、第6
図(B)は第6図(八)のD−D断面図である。
10:蒸発室
11:多孔質体
21:ヒータ
31:定油面器
32:送油管
33:送油ポンプ
41:未蒸発燃料費は部
42:回収管
50:燃焼部FIG. 1 is an overall configuration diagram of an apparatus for implementing the present invention, FIG. 2 is an enlarged explanatory diagram of a porous body portion, FIGS. 3 and 4 are overall configuration diagrams of other implementation apparatuses, and FIG. Figure 6 (A) is an overall configuration diagram of a conventional device;
Figure (B) is a sectional view taken along line DD in Figure 6 (8). 10: Evaporation chamber 11: Porous body 21: Heater 31: Oil level regulator 32: Oil feed pipe 33: Oil feed pump 41: Unevaporated fuel cost part 42: Recovery pipe 50: Combustion part
Claims (1)
し、蒸発室内で液体燃料を加熱空気で直接的に蒸発気化
し、得られた混合気を燃焼部へ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、前記蒸発室内に多孔
質体を配置し、該多孔質体に対して前記液体燃料を供給
すると共に多孔質体を通過するようにして前記加熱空気
を送風し、前記多孔質体内を降下する液体燃料を多孔質
体内を通過する加熱空気で直接的に蒸発気化することを
特徴とする液体燃料燃焼装置。(1) It has a liquid fuel supply means and a heated air blowing means, and is configured to directly evaporate and vaporize the liquid fuel with heated air in the evaporation chamber and send the obtained air-fuel mixture to the combustion section for combustion. In the liquid fuel combustion device, a porous body is arranged in the evaporation chamber, and the liquid fuel is supplied to the porous body and the heated air is blown so as to pass through the porous body. . A liquid fuel combustion device, characterized in that the liquid fuel descending within the porous body is directly vaporized by heated air passing through the porous body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19737190A JPH0484005A (en) | 1990-07-25 | 1990-07-25 | Liquid fuel burner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19737190A JPH0484005A (en) | 1990-07-25 | 1990-07-25 | Liquid fuel burner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0484005A true JPH0484005A (en) | 1992-03-17 |
Family
ID=16373389
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19737190A Pending JPH0484005A (en) | 1990-07-25 | 1990-07-25 | Liquid fuel burner |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0484005A (en) |
-
1990
- 1990-07-25 JP JP19737190A patent/JPH0484005A/en active Pending
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