JPH0454848B2 - - Google Patents

Info

Publication number
JPH0454848B2
JPH0454848B2 JP60217549A JP21754985A JPH0454848B2 JP H0454848 B2 JPH0454848 B2 JP H0454848B2 JP 60217549 A JP60217549 A JP 60217549A JP 21754985 A JP21754985 A JP 21754985A JP H0454848 B2 JPH0454848 B2 JP H0454848B2
Authority
JP
Japan
Prior art keywords
combustion
swirling
diameter
combustion tube
chamber
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.)
Expired - Lifetime
Application number
JP60217549A
Other languages
Japanese (ja)
Other versions
JPS6277522A (en
Inventor
Yoichiro Ookubo
Yoshinori Idota
Yasushi Tanazawa
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Central R&D Labs Inc
Original Assignee
Toyota Central R&D Labs Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Toyota Central R&D Labs Inc filed Critical Toyota Central R&D Labs Inc
Priority to JP21754985A priority Critical patent/JPS6277522A/en
Priority to CA000519274A priority patent/CA1285207C/en
Priority to US06/913,378 priority patent/US4850195A/en
Publication of JPS6277522A publication Critical patent/JPS6277522A/en
Publication of JPH0454848B2 publication Critical patent/JPH0454848B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Combustion Of Fluid Fuel (AREA)

Description

【発明の詳細な説明】 本発明は、家庭用又は工業用の噴霧式燃焼装
置、特に車載用の小型の噴霧式燃焼装置に関す
る。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a spray combustion device for domestic or industrial use, and particularly to a small spray combustion device for vehicle use.

従来の車載用の噴霧式燃焼装置は、特開昭59−
147921号公報に開示されているように、旋回空気
流発生装置の中心部の旋回室に、その閉鎖端側か
ら開放端側へ液体燃料を噴霧する燃料噴射弁を同
芯状に設け、旋回室の旋回空気流の中心部に液体
燃料を噴霧する構成にしている。
The conventional in-vehicle spray combustion device was developed in Japanese Patent Application Laid-open No.
As disclosed in Japanese Patent No. 147921, a fuel injection valve that sprays liquid fuel from the closed end side to the open end side is provided concentrically in the swirling chamber at the center of the swirling airflow generating device. The structure is such that liquid fuel is sprayed into the center of the swirling airflow.

旋回室の開放端には、旋回室より大径の第1燃
焼筒を同芯状に連結し、第1燃焼筒の出口に第1
絞りを介して第2燃焼筒を同芯状に連結し、第2
燃焼筒を第1燃焼筒より大径に形成し、第2燃焼
筒の出口に第2絞りを設けている。
A first combustion tube having a larger diameter than the swirl chamber is concentrically connected to the open end of the swirl chamber, and a first combustion tube is connected to the outlet of the first combustion tube.
The second combustion cylinders are concentrically connected through the throttle, and the second
The combustion tube is formed to have a larger diameter than the first combustion tube, and a second throttle is provided at the outlet of the second combustion tube.

この噴霧式燃焼装置においては、液体燃料が中
心部に噴霧された旋回空気流即ち混合気流は、旋
回室から大径の第1燃焼筒に流入すると、その旋
回力によつて径が拡大し、混合が促進され、第1
燃焼筒から第1絞りを介して大径の第2燃焼筒に
流入すると、径が縮小した後にその旋回力によつ
て拡大し、混合が促進される。
In this spray type combustion device, when the swirling air flow, that is, the mixture flow, in which liquid fuel is sprayed in the center, flows from the swirling chamber into the large-diameter first combustion cylinder, its diameter expands due to the swirling force. Mixing is promoted and the first
When it flows from the combustion tube through the first throttle into the second combustion tube, which has a large diameter, the diameter decreases and then expands due to its swirling force, promoting mixing.

また、混合気流は、旋回しているので、旋回し
ていない場合に比較して、混合気流の安定性が良
く、従つて、火炎の安定性が良い。
Furthermore, since the air mixture is swirling, the stability of the air mixture is better than in the case where the air mixture is not swirling, and therefore, the stability of the flame is better.

ところが、この噴霧式燃焼装置は、第2燃焼筒
が第1燃焼筒より太く、燃焼筒が先太の拡管構造
をしていて、火炎が先太になるので、燃料の流量
が微小になると、火炎の安定性が悪くなり、火炎
のゆらぎや排ガスの逆流等に起因して燃焼が悪化
する。また、排ガスの逆流を防止するため、第2
燃焼筒の出口に第2絞りを必要とする。
However, in this spray type combustion device, the second combustion tube is thicker than the first combustion tube, and the combustion tube has an expanded tube structure with a thicker tip, so the flame becomes thicker at the tip, so when the fuel flow rate becomes small, Flame stability deteriorates, and combustion deteriorates due to flame fluctuations, backflow of exhaust gas, etc. In addition, in order to prevent backflow of exhaust gas, a second
A second restriction is required at the exit of the combustion tube.

即ち、燃料流量の微小領域で、火炎の安定性が
悪くなつて燃焼が悪化する。
That is, in a region where the fuel flow rate is very small, flame stability deteriorates and combustion deteriorates.

また、この噴霧式燃焼装置は、燃焼筒が先太の
拡管構造をしていで、胴体が太いので、胴体に熱
交換器を被せてカーヒータを構成する、カーヒー
タが大型になる。
Further, in this spray type combustion device, the combustion cylinder has an expanded tube structure with a thicker end, and the body is thick, so the car heater, which is constructed by covering the body with a heat exchanger, becomes large.

即ち、小型のカーヒータを構成することが困難
である。
That is, it is difficult to construct a small car heater.

本発明の目的は、上記のような従来の課題を解
決することである。
An object of the present invention is to solve the conventional problems as described above.

発明の構成 軸芯の回りに旋回する空気流が導入される円筒
状の旋回室に、その閉鎖端側から開放端側へ液体
燃料を噴霧する燃料噴射弁を同芯状に設け、旋回
室に導入された旋回空気流の中心部に液体燃料を
噴霧する構成にし、 旋回空気流に液体燃料が噴霧された混合気流の
中心部に点火する点火栓を設け、 旋回室の開放端に第1絞りを介して第1燃焼筒
を同芯状に連結し、第1燃焼筒を旋回室に対して
大径又は同径に形成し、 第1燃焼筒の出口に第2絞りを介して第2燃焼
筒を同芯状に連結し、第2燃焼筒を第1燃焼筒に
対して小径又は同径に形成したことを特徴とする
噴霧式燃焼装置。
Structure of the Invention A fuel injection valve that sprays liquid fuel from a closed end side to an open end side is provided concentrically in a cylindrical swirling chamber into which an air flow swirling around an axis is introduced. The structure is such that liquid fuel is sprayed at the center of the swirling airflow that has been introduced, an ignition plug is provided to ignite the mixture at the center of the mixed airflow in which the liquid fuel is sprayed into the swirling airflow, and a first throttle is installed at the open end of the swirling chamber. The first combustion tube is connected concentrically through the swirl chamber, the first combustion tube is formed to have a larger diameter or the same diameter as the swirl chamber, and the second combustion tube is connected to the outlet of the first combustion tube through a second throttle. A spray combustion device characterized in that the cylinders are concentrically connected and the second combustion cylinder is formed to have a smaller diameter or the same diameter as the first combustion cylinder.

発明の作用 混合気流は、旋回室から第1絞りを介して大径
又は同径の第1燃焼筒に流入すると、径が縮小し
た後にその旋回力によつて拡大し、混合が促進さ
れ、第1燃焼筒から第2絞りを介して小径又は同
径の第2燃焼筒に流入すると、径が縮小した後に
その旋回力によつて拡大し、混合が促進される。
Effect of the Invention When the air mixture flows from the swirling chamber through the first throttle into the first combustion cylinder having a large diameter or the same diameter, the diameter decreases and then expands due to the swirling force, promoting mixing and increasing the first combustion tube. When it flows from one combustion tube to a second combustion tube with a smaller diameter or the same diameter through a second throttle, the diameter decreases and then expands due to its swirling force, promoting mixing.

第2燃焼筒が第1燃焼筒より小径である場合、
混合気流は、第1燃焼筒から第2燃焼筒に流入す
ると、増速し、増速によつても混合が促進され
る。
When the second combustion tube has a smaller diameter than the first combustion tube,
When the mixture flow flows from the first combustion tube to the second combustion tube, the speed increases, and the speed increase also promotes mixing.

混合気流は、旋回しているので、混合気流の安
定性が良く、従つて、火炎の安定性が良い。
Since the air mixture is swirling, the stability of the air mixture is good, and therefore the stability of the flame is good.

第2燃焼筒が第1燃焼筒より小径である場合、
火炎が先細になり、火炎の安定性が良い。従つ
て、燃料の流量を減少しても、火炎の長さが短く
なるだけであり、火炎が不安定にならない。ま
た、火炎の安定性が良いので、第2燃焼筒の出口
に絞りがなくても、排ガスが第2燃焼筒に逆流す
ることが少ない。
When the second combustion tube has a smaller diameter than the first combustion tube,
The flame becomes tapered and the flame stability is good. Therefore, reducing the fuel flow rate only shortens the length of the flame and does not cause the flame to become unstable. Furthermore, since the flame stability is good, even if there is no restriction at the outlet of the second combustion tube, the exhaust gas is less likely to flow back into the second combustion tube.

第2燃焼筒が第1燃焼筒と同径である場合は、
小径である上記の場合におけるより混合気流の流
量が多いときに、上記の場合とほぼ同様な作用を
奏する。
If the second combustion tube has the same diameter as the first combustion tube,
When the flow rate of the air mixture is larger than in the above case where the diameter is small, substantially the same effect as in the above case is achieved.

発明の効果 燃料流量の微小領域でも、火炎の不安定になら
ず、火炎のゆらぎや排ガスの逆流等に起因する燃
焼の悪化が少ない。
Effects of the Invention Even in a small fuel flow rate range, the flame does not become unstable, and there is little deterioration of combustion due to flame fluctuations, backflow of exhaust gas, etc.

第2燃焼筒の出口には、排ガスの逆流を防止す
る絞りを必要としない。
The outlet of the second combustion tube does not require a restriction to prevent backflow of exhaust gas.

また、第2燃焼筒が第1燃焼筒に対して小径又
は同径であつて、胴体が太くならないので、胴体
に熱交換器を被せてカーヒータを構成する場合、
小型のカーヒータを構成することが容易である。
In addition, since the second combustion cylinder has a smaller diameter or the same diameter as the first combustion cylinder, and the body does not become thicker, when constructing a car heater by covering the body with a heat exchanger,
It is easy to construct a small car heater.

次に、本発明の実施例について説明する。 Next, examples of the present invention will be described.

第1実施例 (第1図乃至第7図参照) 本例の噴霧式燃焼装置は、第1図に示すよう
に、旋回空気流発生装置1即ち旋回器1の中心部
に形成された円筒形状の旋回室2に、その閉鎖端
側から開放端側へ燃料を噴霧する燃料噴射弁11
を同芯状に設け、旋回室2の開放端に第1絞り1
5を介して円筒形状の第1燃焼筒16を同芯状に
連設し、第1燃焼筒16の軸芯位置に点火栓17
の先端の点火部を突出し、第1燃焼筒16の出口
に第2絞り19を介して円筒形状の第2燃焼筒2
0を同芯状に連設している。
First Example (See Figures 1 to 7) As shown in Figure 1, the spray combustion device of this example has a cylindrical shape formed in the center of a swirling airflow generating device 1, that is, a swirler 1. A fuel injection valve 11 sprays fuel into the swirling chamber 2 from the closed end side to the open end side thereof.
are provided concentrically, and a first aperture 1 is provided at the open end of the swirling chamber 2.
5, a cylindrical first combustion tube 16 is concentrically arranged, and an ignition plug 17 is provided at the axial position of the first combustion tube 16.
A cylindrical second combustion tube 2 is inserted into the outlet of the first combustion tube 16 through a second throttle 19.
0 are arranged concentrically.

第1燃焼筒16は、旋回室2より大径に形成し
ている。第2燃焼筒20は、第1燃焼筒16と同
径に形成している。なお、第2燃焼筒20の出口
には、絞りを設けていない。
The first combustion cylinder 16 is formed to have a larger diameter than the swirl chamber 2. The second combustion tube 20 is formed to have the same diameter as the first combustion tube 16. Note that no throttle is provided at the outlet of the second combustion cylinder 20.

旋回器1は、第1図と第2図に示すように、旋
回室2の周壁を形成している内周壁3とその外回
り位置に同芯状に配置した円筒形状の外周壁4の
前後端に前端板5と後端板6を設けて、円環状の
空気旋回路7を形成し、外周壁4の一個所にその
個所の接線方向に沿つて空気導入管8を接続し
て、空気旋回路7に接続した空気導入路8を形成
し、空気導入路8に空気供給源9を接続し、内周
壁3の4個所にそれぞれその個所の内周面の接続
方向に沿つて空気導入孔10を貫設して、空気旋
回路7を旋回室2に接続し、旋回室2にその軸芯
の回りに旋回する空気流を導入する構成にしてい
る。
As shown in FIGS. 1 and 2, the swirler 1 includes an inner circumferential wall 3 forming the circumferential wall of a swirling chamber 2, and the front and rear ends of a cylindrical outer circumferential wall 4 arranged concentrically around the outer circumferential position of the inner circumferential wall 3. A front end plate 5 and a rear end plate 6 are provided to form an annular air swirl path 7, and an air introduction pipe 8 is connected to one location on the outer peripheral wall 4 along the tangential direction of that location to form an air swirl path 7. An air introduction passage 8 connected to the passage 7 is formed, an air supply source 9 is connected to the air introduction passage 8, and air introduction holes 10 are formed at four locations on the inner circumferential wall 3 along the connecting direction of the inner circumferential surface of the respective locations. is installed through the shaft to connect the air swirling path 7 to the swirling chamber 2, so that an air flow swirling around the axis of the swirling chamber 2 is introduced into the swirling chamber 2.

燃料噴射弁11は、第1図に示すように、噴射
端を旋回室の後端板6の中心に貫着しており、燃
料供給路12からの液体燃料を空気供給路14か
らの空気流によつて微粒化する二流体噴霧形であ
り、燃料供給路12に燃料供給源13を、空気供
給路14に空気供給源9をそれぞれ接続してい
る。
As shown in FIG. 1, the fuel injection valve 11 has an injection end penetrated into the center of the rear end plate 6 of the swirling chamber, and the liquid fuel from the fuel supply passage 12 is injected into the air flow from the air supply passage 14. It is a two-fluid spray type that is atomized by atomization, and a fuel supply source 13 is connected to the fuel supply path 12, and an air supply source 9 is connected to the air supply path 14.

点火栓17は、先端の点火部を燃料噴射弁11
の燃料噴霧領域に配置し、基端の端子に点火源1
8を接続している。
The ignition plug 17 connects the ignition part at the tip to the fuel injection valve 11.
ignition source 1 at the proximal terminal.
8 is connected.

更に、本発明の噴霧式燃焼装置は、燃焼筒1
6,20に熱交換器21を被嵌してカーヒータを
構成している。
Furthermore, the spray combustion device of the present invention has a combustion tube 1.
6 and 20 are fitted with a heat exchanger 21 to form a car heater.

熱交換器21は、第1図、第3図と第4図に示
すように、第1燃焼筒16と第2燃焼筒20に円
筒容器形状の器体22を被嵌し、器体22と第
1、第2燃焼筒16,20の間に、第2燃焼筒2
0の出口に連通したガス通路23を形成し、器体
22内周面の第2燃焼筒20外回り位置に多数枚
の熱交換用フイン24を等間隔に軸芯方向に沿つ
て設け、器体22の第1燃焼筒16側部分にガス
通路23の出口25を設けている。器体22の第
2燃焼筒20側部分は、二重容器形状に形成し
て、流体通路26を形成し、流体通路26の内周
面に螺旋状の熱交換用フイン27を設け、流体通
路26の一部と他端に入口28と出口29を設け
ている。なお、流体通路の入口28には流体供給
源を、流体通路の出口29には放熱器をそれぞれ
接続する。
As shown in FIGS. 1, 3, and 4, the heat exchanger 21 has a cylindrical container-shaped vessel body 22 fitted into the first combustion tube 16 and the second combustion tube 20, and the vessel body 22 and Between the first and second combustion tubes 16 and 20, the second combustion tube 2
A large number of heat exchange fins 24 are provided at equal intervals along the axial direction of the second combustion cylinder 20 on the inner circumferential surface of the vessel body 22. An outlet 25 of the gas passage 23 is provided in the first combustion cylinder 16 side portion of the gas passage 22 . The second combustion cylinder 20 side portion of the vessel body 22 is formed into a double container shape to form a fluid passage 26, and a spiral heat exchange fin 27 is provided on the inner circumferential surface of the fluid passage 26 to form a fluid passage 26. An inlet 28 and an outlet 29 are provided at one end of 26 and the other end. Note that a fluid supply source is connected to the inlet 28 of the fluid passage, and a radiator is connected to the outlet 29 of the fluid passage.

本例の噴霧式燃焼装置を作動すると、旋回室2
にその軸芯の回りに旋回する空気流が導入され、
燃料噴射弁11から旋回室2の旋回空気流の中心
部に軽油や灯油又はガソリンのような燃料が噴霧
され、噴霧燃料と旋回空気の混合気流が旋回室2
から第1絞り15を経て第1燃焼筒16に流入
し、点火栓17によつて点火されて燃焼し、燃焼
の火炎が第1燃焼筒16から第2絞り19を経て
第2燃焼筒20に流入し、燃焼の排ガスが第2燃
焼筒20からガス通路23に流入し、ガス通路の
熱交換用フイン24や器体22を加熱して、出口
25から排出される。一方、流体通路の入口28
に供給された水や空気のような流体は、流体通路
26に流入し、流体通路の熱交換用フイン27と
器体22によつて加熱され、高温になつて、出口
29から流出する。
When the spray combustion device of this example is operated, the swirling chamber 2
An airflow is introduced that swirls around its axis,
Fuel such as light oil, kerosene, or gasoline is sprayed from the fuel injection valve 11 into the center of the swirling airflow in the swirling chamber 2, and the mixture flow of the sprayed fuel and swirling air flows into the swirling chamber 2.
flows into the first combustion tube 16 through the first throttle 15, is ignited by the spark plug 17 and burns, and the combustion flame flows from the first combustion tube 16 through the second throttle 19 to the second combustion tube 20. The combustion exhaust gas flows into the gas passage 23 from the second combustion cylinder 20, heats the heat exchange fins 24 and the vessel body 22 of the gas passage, and is discharged from the outlet 25. On the other hand, the inlet 28 of the fluid passage
Fluid such as water or air flows into the fluid passage 26, is heated by the heat exchange fins 27 of the fluid passage and the container body 22, reaches a high temperature, and flows out from the outlet 29.

本例の噴霧式燃焼装置は、旋回室2と第1燃焼
筒16の間に第1絞り15を設け、第1燃焼筒1
6を旋回室2より大径に形成しているので、混合
気の燃焼火炎は、旋回室2から第1絞り15を経
て第1燃焼筒16に流入すると、径が縮小した後
にその旋回力によつて急拡大して、第1燃焼筒1
6の周壁付近まで広がり、第1燃焼筒16の全体
に均一に分布する。従つて、高負荷の燃焼が可能
になる。
The spray type combustion device of this example has a first throttle 15 provided between the swirl chamber 2 and the first combustion tube 16, and
6 is formed to have a larger diameter than the swirling chamber 2, so when the combustion flame of the air-fuel mixture flows from the swirling chamber 2 through the first throttle 15 and into the first combustion tube 16, its diameter is reduced and then due to the swirling force. Then, it suddenly expanded and the first combustion tube 1
6 and is uniformly distributed throughout the first combustion cylinder 16. Therefore, high load combustion becomes possible.

また、火炎の急拡大によつて第1燃焼筒16に
安定な循環領域が形成されて、火炎の保持が良好
に行なわれる。従つて、最大負荷の1/3程度の負
荷であつても、火炎が安定する。
Further, due to the rapid expansion of the flame, a stable circulation region is formed in the first combustion tube 16, and the flame is well maintained. Therefore, the flame is stable even under a load of about 1/3 of the maximum load.

また、第1燃焼筒16を旋回室2と同径に形成
した場合は、大径に形成した上記の場合における
より混合気の流量が多いときに、第1絞り15の
径を適当に選定することにより、上記の場合とほ
ぼ同様な効果を奏する。
In addition, when the first combustion tube 16 is formed to have the same diameter as the swirling chamber 2, the diameter of the first throttle 15 is appropriately selected when the flow rate of the air-fuel mixture is larger than in the above case where the first combustion tube 16 is formed to have a large diameter. This produces almost the same effect as the above case.

本例の噴霧式燃焼装置においては、第5図に示
すように、 D1:旋回室2の径 D2:第1絞り15の径 D3:第1燃焼筒16の径 D4:第2絞り19の径 D5:第2燃焼筒20の径 L1:旋回室2の長さ としたときに、それらの比率は、次のように設定
するのが好ましい。
In the spray type combustion apparatus of this example , as shown in FIG . When the diameter D5 of the throttle 19: the diameter L1 of the second combustion cylinder 20: the length of the swirling chamber 2, it is preferable to set the ratio as follows.

(1) 0.6≦D2/D1≦1 D2/D1<0.6の場合は、噴霧燃料が第1絞り
15に付着して流下する。また、火炎の保持が
良好ではない。
(1) When 0.6≦D 2 /D 1 ≦1 D 2 /D 1 <0.6, the sprayed fuel adheres to the first throttle 15 and flows down. Also, flame retention is not good.

(2) 0.5≦D4/D3≦0.8 D4/D3<0.5の場合は、第1燃焼筒16から
第2燃焼筒20への通路抵抗が大きくなつて火
炎の流れが円滑でなくなる。D4/D3>0.8の場
合は、第2絞り19の絞り効果が少ない。
(2) 0.5≦D 4 /D 3 ≦0.8 When D 4 /D 3 <0.5, the passage resistance from the first combustion tube 16 to the second combustion tube 20 becomes large, and the flame flow becomes unstable. When D 4 /D 3 >0.8, the aperture effect of the second diaphragm 19 is small.

(3) 0.6≦D5/D3≦1 D5/D3<0.6の場合は、火炎が第2燃焼筒2
0の周壁に接近し過ぎ、また、第2燃焼筒20
の通路抵抗が増加し、燃焼が悪化する。
(3) If 0.6≦D 5 /D 3 ≦1 D 5 /D 3 <0.6, the flame is in the second combustion tube 2.
0 too close to the peripheral wall of the second combustion tube 20.
passage resistance increases and combustion worsens.

(4) 1≦D3/D1≦2 D3/D1>2の場合は、火炎が第1燃焼筒1
6の全体に拡がらず、余分の空間が生じ、小型
にならない。
(4) If 1≦D 3 /D 1 ≦2 D 3 /D 1 >2, the flame is in the first combustion tube 1.
6, and an extra space is created, which prevents it from being compact.

(5) 0.5≦L1/D1≦1.5 L1/D1<0.5の場合は、旋回室2において旋
回空気流と噴霧燃料が混合するのに必要な距離
が不足し、燃焼が悪化する。L1/D1>1.5の場
合は、噴霧燃料が旋回室2の周壁に付着し、末
燃の炭化水素の排出が多くなる。
(5) 0.5≦L 1 /D 1 ≦1.5 When L 1 /D 1 <0.5, the distance required for the swirling airflow and the sprayed fuel to mix in the swirling chamber 2 is insufficient, and combustion deteriorates. When L 1 /D 1 >1.5, the sprayed fuel adheres to the peripheral wall of the swirling chamber 2, and more end-burning hydrocarbons are discharged.

(6) 旋回室2の空気導入孔10の総断面積をS0
旋回室2の周壁の面積をS1=π・D1・L1とす
ると、 2≦S1/S0≦100 S1/S0>100の場合は、旋回室2に旋回空気
流を導入するために、高圧発生装置が必要とな
り、大掛りになつて、小型の燃焼装置に適さな
い。また、旋回空気流の速度が高くなり過ぎ、
かえつて旋回空気流と噴霧燃料の混合が妨げら
れる。S1/S0<2の場合は、旋回空気流の速度
が不足する。
(6) The total cross-sectional area of the air introduction holes 10 of the swirling chamber 2 is S 0 ,
If the area of the peripheral wall of the swirling chamber 2 is S 1 = π・D 1・L 1 , then 2≦S 1 /S 0 ≦100 If S 1 /S 0 >100, a swirling air flow is introduced into the swirling chamber 2. In order to do so, a high-pressure generator is required, which is large-scale and unsuitable for small-sized combustion devices. Also, the speed of the swirling airflow becomes too high,
On the contrary, mixing of the swirling air flow and the atomized fuel is hindered. When S 1 /S 0 <2, the speed of the swirling airflow is insufficient.

(7) また、燃料噴射弁11の旋回室2内への突出
長さをlとすると、 O≦l≦L1/2 燃料噴射弁11が流体燃料を気流によつて微
粒化する二流体噴霧形の場合は、噴射速度が高
いため、噴霧燃料と旋回空気流が十分に混合す
るのには、旋回室2においてL1/2以上の距
離を必要とする。
(7) Furthermore, if the protrusion length of the fuel injection valve 11 into the swirling chamber 2 is l, then O≦l≦L 1 /2 Two-fluid spray in which the fuel injection valve 11 atomizes the fluid fuel by airflow In the case of this type, since the injection speed is high, a distance of L 1 /2 or more is required in the swirling chamber 2 for sufficient mixing of the atomized fuel and the swirling air flow.

次に、本例の噴霧式燃料装置において、 D2/D1=1、D3/D1=1.5、 D4/D3=0.56、D5/D3=1、 L1/D1=1、S1/S0=47、l=0 と設定した場合の性能を示す。 Next, in the spray fuel system of this example, D 2 /D 1 = 1, D 3 /D 1 = 1.5, D 4 /D 3 = 0.56, D 5 /D 3 = 1, L 1 /D 1 = 1. The performance is shown when S 1 /S 0 =47 and l=0.

第6図と第7図は、それぞれ、縦軸に、旋回器
の空気導入路8と燃料噴射弁の空気供給路14に
供給する空気の流量を採り、横軸に、燃料噴射弁
の燃料供給路12に供給する燃料の軽油の流量を
採つている。両図中において、λは、空気過剰率
即ち燃焼に必要な理論空気流量に対する供給空気
流量の比を示す。λ=3の線と交差したハツチン
グ付の縦線の左側は、火炎が不安定になる領域を
示している。
6 and 7, the vertical axis shows the flow rate of air supplied to the swirler's air introduction path 8 and the fuel injection valve's air supply path 14, and the horizontal axis shows the fuel supply to the fuel injection valve. The flow rate of light oil, which is the fuel supplied to the road 12, is measured. In both figures, λ indicates the excess air ratio, ie the ratio of the supplied air flow rate to the theoretical air flow rate required for combustion. The left side of the hatched vertical line intersecting the λ=3 line indicates the region where the flame becomes unstable.

第6図中において、COは、ガス通路の出口2
5から排出される排ガス中の一酸化炭素の濃度を
示す。従つて、第6図から明らかなように、排ガ
ス中の一酸化炭素の濃度は、1.1≦λ≦2.2の範囲
において、約300ppm以下であり、非常に低い。
In Figure 6, CO is at the outlet 2 of the gas passage.
It shows the concentration of carbon monoxide in the exhaust gas discharged from No. 5. Therefore, as is clear from FIG. 6, the concentration of carbon monoxide in the exhaust gas is approximately 300 ppm or less in the range of 1.1≦λ≦2.2, which is very low.

また、第7図中において、TEは、カーヒータ
の熱効率即ち供給燃料の発熱量に対する流体通路
26通過水の受熱量の100分率を示す。従つて、
第7図から明らかなように、カーヒータの熱効率
は、85〜95%であり、非常に高い。
Further, in FIG. 7, TE indicates the thermal efficiency of the car heater, that is, the 100% ratio of the amount of heat received by the water passing through the fluid passage 26 to the amount of heat generated by the supplied fuel. Therefore,
As is clear from FIG. 7, the thermal efficiency of the car heater is 85 to 95%, which is very high.

結局、1.2〜6c.c./minという微小流量の燃料
が良好に燃焼する。即ち、燃焼範囲が燃料流量の
微少領域でありかつ広い。なお、発熱量は、600
〜3.000Kcal/hである。
In the end, fuel with a minute flow rate of 1.2 to 6 c.c./min burns well. That is, the combustion range is a small range of fuel flow rate and is wide. In addition, the calorific value is 600
~3.000Kcal/h.

第2実施例 (第8図乃至第11図参照) 本例の噴霧式燃焼装置は、第8図に示すよう
に、旋回空気流発生装置31即ち旋回器31の中
心部に形成された円筒形状の旋回室32に、その
閉鎖端側から開放端側へ燃料を噴霧する燃料噴射
射弁39を同芯状に設け、旋回室32の開放端に
第1絞り43を介して円筒形状の第1燃焼筒44
を同芯状に連設し、第1燃焼筒44内に点火栓4
5の先端の点火部を突出し、第1燃焼筒44の出
口に第2絞り46を介して円筒形状の第2燃焼筒
47を同芯状に連設している。
Second Embodiment (See FIGS. 8 to 11) As shown in FIG. A fuel injection valve 39 that sprays fuel from the closed end side to the open end side is provided concentrically in the swirling chamber 32, and a cylindrical first Combustion tube 44
The spark plugs 4 are arranged concentrically in a row, and the ignition plug 4 is installed in the first combustion cylinder 44.
A cylindrical second combustion tube 47 is concentrically connected to the outlet of the first combustion tube 44 via a second throttle 46.

第1燃焼筒44は、旋回室32より大径に形成
している。第2燃焼筒47は、第1燃焼筒44よ
り小径に形成している。
The first combustion cylinder 44 is formed to have a larger diameter than the swirl chamber 32. The second combustion tube 47 is formed to have a smaller diameter than the first combustion tube 44.

旋回器31は、第8図と第9図に示すように、
旋回室32の外回り位置に同芯状に配置した円筒
形状の外周壁33の前後端に前端板34と後端板
35を設けて、円環状の空気旋回路36を形成
し、外周壁33の一個所にその個所の接続方向に
沿つて空気導入管37を接続して、空気旋回路3
6に接続した空気導入路37を形成し、空気旋回
路36に多数枚の案内羽根38を旋回室32の回
りに等間隔に放射状に設け、各案内羽根38をそ
れぞれその内端が近接した位置の旋回室32周面
の接続方向に沿つて配置し、空気旋回路36を案
内羽根38間の透間を経て旋回室32に連通し、
旋回室32にその軸芯の回りに旋回する空気流を
導入する構成にしている。
As shown in FIGS. 8 and 9, the swirler 31 is
A front end plate 34 and a rear end plate 35 are provided at the front and rear ends of a cylindrical outer peripheral wall 33 arranged concentrically at the outer circumferential position of the swirling chamber 32 to form an annular air swirling path 36 . An air introduction pipe 37 is connected to one location along the connection direction of that location, and the air swirl circuit 3
6, a large number of guide vanes 38 are provided radially in the air swirling circuit 36 at equal intervals around the swirling chamber 32, and each guide vane 38 is located at a position where the inner ends thereof are close to each other. The air swirling path 36 is arranged along the connection direction of the circumferential surface of the swirling chamber 32, and the air swirling path 36 is communicated with the swirling chamber 32 through a gap between the guide vanes 38.
The structure is such that an air flow that swirls around the axis of the swirling chamber 32 is introduced into the swirling chamber 32.

燃料噴射弁39は、第8図に示すように、噴射
端を旋回室32内に旋回室長さの半分以上突出し
て、旋回室の後端板35の中心に貫着しており、
燃料供給路40からの液体燃料を、電極41を挾
持した2枚の電歪素子42により発生する超音波
振動によつて微粒化する超音波振動形である。
As shown in FIG. 8, the fuel injection valve 39 has an injection end protruding into the swirling chamber 32 by more than half the length of the swirling chamber, and is attached to the center of the rear end plate 35 of the swirling chamber.
This is an ultrasonic vibration type in which the liquid fuel from the fuel supply path 40 is atomized by ultrasonic vibrations generated by two electrostrictive elements 42 holding an electrode 41 between them.

点火栓45は、先端の点火部を燃料噴射弁39
の燃料噴霧領域に配置している。
The ignition plug 45 connects the ignition part at the tip to the fuel injection valve 39.
located in the fuel spray area.

更に、本例の噴霧式燃焼装置は、燃焼筒44,
47に熱交換器48を被嵌してカーヒータを構成
している。
Furthermore, the spray combustion device of this example has a combustion tube 44,
47 is fitted with a heat exchanger 48 to form a car heater.

熱交換器48は、第8図、第10図と第11図
に示すように、第1、第2燃焼筒44,47に円
筒容器形状の器体49を被嵌し、器体49と第
1、第2燃焼筒44,47の間に、第2燃焼筒4
7の出口に連通したガス通路50を形成し、器体
49内周面の第2燃焼筒47外回り位置に多数枚
の熱交換用フイン51を等間隔に軸芯方向に沿つ
て設け、器体49の第1燃焼筒44側部分にガス
通路50の出口52を設けている。器体49は、
二重容器形状に形成して、流体通路53を形成
し、流体通路53の内周面に螺旋状の熱交換用フ
イン54を設け、流体通路53の一端と他端に入
口55と出口56を設けている。
As shown in FIG. 8, FIG. 10, and FIG. 1, between the second combustion cylinders 44 and 47, the second combustion cylinder 4
A large number of heat exchange fins 51 are provided at equal intervals along the axial direction of the second combustion cylinder 47 on the inner peripheral surface of the vessel body 49, and a gas passage 50 is formed in communication with the outlet of the vessel body 49. An outlet 52 of a gas passage 50 is provided in the first combustion cylinder 44 side portion of the combustion chamber 49 . The vessel body 49 is
It is formed into a double container shape to form a fluid passage 53, a spiral heat exchange fin 54 is provided on the inner peripheral surface of the fluid passage 53, and an inlet 55 and an outlet 56 are provided at one end and the other end of the fluid passage 53. It is set up.

本例の噴霧式燃焼装置は、第2燃焼筒47が第
1燃焼筒44より小径であるので、混合気の燃焼
火炎は、第1燃焼筒44から第2絞り46を経て
第2燃焼筒47に流入すると、旋回速度と前進速
度を回復して増速し、増速によつて燃料と空気の
混合が促進される。また、火炎は、先細になり、
安定性が良くなる。従つて、燃焼が良好に行なわ
れる。
In the spray type combustion device of this example, since the second combustion tube 47 has a smaller diameter than the first combustion tube 44, the combustion flame of the air-fuel mixture passes from the first combustion tube 44 through the second throttle 46 to the second combustion tube 47. When the fuel flows into the air, the turning speed and forward speed are restored and increased, and the increased speed promotes the mixing of fuel and air. Also, the flame becomes tapered,
Improves stability. Therefore, combustion is performed well.

また、燃料噴射弁39は、超音波振動形である
ので、噴霧燃料の粒径は小さくなり、微粒化が良
好に行なわれる。また、噴霧燃料の粒子は、霧化
時の運動量が非常に小さいので、旋回空気流に流
され易く、旋回空気流との混合が迅速に行なわれ
る。
Further, since the fuel injection valve 39 is of the ultrasonic vibration type, the particle size of the sprayed fuel is small, and atomization is performed well. Furthermore, since the particles of the atomized fuel have a very small momentum during atomization, they are easily swept away by the swirling airflow, and are quickly mixed with the swirling airflow.

また、燃料噴射弁39の旋回室32内への突出
長さが旋回室長さの半分以上であるので、安定し
た旋回空気流中に燃料が噴射され、燃料と空気の
混合気流の変動が少なく、火炎が安定する。ま
た、燃料噴射弁39は、その回りの旋回空気流に
よつて温度上昇が防止され、振動源の電歪素子4
2の耐久性が向上する。
In addition, since the length of the fuel injection valve 39 protruding into the swirling chamber 32 is more than half the length of the swirling chamber, the fuel is injected into a stable swirling air flow, and there is little variation in the fuel-air mixture flow. The flame becomes stable. Further, the temperature of the fuel injection valve 39 is prevented from rising due to the swirling air flow around it, and the electrostrictive element 4, which is a source of vibration, is prevented from increasing in temperature.
2. Durability is improved.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は、本発明の第1実施例の噴霧式燃焼装
置の縦断側面図である。第2図は、第1図の−
線断面図である。第3図は、第1図の−線
断面図である。第4図は、第1図の−線断面
図である。第5図は、同噴霧式燃焼装置の部分縦
断側面図である。第6図と第7図は、同噴霧式燃
焼装置の性能を示す線図である。第8図は、第2
実施例の噴霧式燃焼装置の縦断側面図である。第
9図は、第8図の−線断面図である。第10
図は、第8図の−線断面図である。第11図
は、第8図のXI−XI線断面図である。 2:旋回室、11:二流体噴霧形燃料噴射弁、
15:第1絞り、16:第1燃焼筒、17:点火
栓、19:第2絞り、20:第2燃焼筒、32:
旋回室、39:超音波振動形燃料噴射弁、43:
第1絞り、44:第1燃焼筒、45:点火栓、4
6:第2絞り、47:第2燃焼筒。
FIG. 1 is a longitudinal sectional side view of a spray combustion apparatus according to a first embodiment of the present invention. Figure 2 is the − of Figure 1.
FIG. FIG. 3 is a sectional view taken along the line -- in FIG. 1. FIG. 4 is a sectional view taken along the - line in FIG. 1. FIG. 5 is a partial longitudinal sectional side view of the same spray combustion device. FIG. 6 and FIG. 7 are diagrams showing the performance of the spray combustion device. Figure 8 shows the second
FIG. 2 is a longitudinal cross-sectional side view of the spray combustion device according to the embodiment. FIG. 9 is a sectional view taken along the - line in FIG. 8. 10th
The figure is a sectional view taken along the line -- in FIG. FIG. 11 is a sectional view taken along the line XI-XI in FIG. 8. 2: swirling chamber, 11: two-fluid spray type fuel injection valve,
15: First throttle, 16: First combustion tube, 17: Spark plug, 19: Second throttle, 20: Second combustion tube, 32:
Turning chamber, 39: Ultrasonic vibration type fuel injection valve, 43:
1st throttle, 44: 1st combustion tube, 45: Spark plug, 4
6: Second throttle, 47: Second combustion tube.

Claims (1)

【特許請求の範囲】 1 軸芯の回りに旋回する空気流が導入される円
筒状の旋回室に、その閉鎖端側から開放端側へ液
体燃料を噴霧する燃料噴射弁を同芯状に設け、旋
回室に導入された旋回空気流の中心部に液体燃料
を噴霧する構成にし、 旋回空気流に液体燃料が噴霧された混合気流の
中心部に点火する点火栓を設け、 旋回室の開放端に第1絞りを介して第1燃焼筒
を同芯状に連結し、第1燃焼筒を旋回室に対して
大径又は同径に形成し、 第1燃焼筒の出口に第2絞りを介して第2燃焼
筒を同芯状に連結し、第2燃焼筒を第1燃焼筒に
対して小径又は同径に形成したことを特徴とする
噴霧式燃焼装置。 2 第1絞りの径が旋回室の径の0.6倍以上であ
り、第1燃焼筒の径が旋回室の径の2倍以下であ
ることを特徴とする特許請求の範囲第1項記載の
噴霧式燃焼装置。 3 旋回室の長さが旋回室の径の0.5倍以上で1.5
倍以下であることを特徴とする特許請求の範囲第
1項又は第2項記載の噴霧式燃焼装置。 4 第2絞りの径が第1燃焼筒の径0.5倍以上で
0.8倍以下であることを特徴とする特許請求の範
囲第1項乃至第3項のいずれかに記載の噴霧式燃
焼装置。 5 第2燃焼筒の径が第1燃焼筒の径の0.6倍以
上であることを特徴とする特許請求の範囲第1項
乃至第4項のいずれかに記載の噴霧式燃焼装置。 6 燃料噴射弁が液体燃料を気流によつて微粒化
する二液体噴霧形であり、燃料噴射弁の旋回室内
への突出長さが旋回室の長さの0.5倍以下である
ことを特徴とする特許請求の範囲第1項乃至第5
項のいずれかに記載の噴霧式燃焼装置。 7 燃料噴射弁が液体燃料を超音波振動によつて
微粒化する超音波振動形であり、燃料噴射弁の旋
回室内への突出長さが旋回室の長さの0.5倍以下
であることを特徴とする特許請求の範囲第1項乃
至第5項のいずれかに記載の噴霧式燃焼装置。
[Claims] 1. A fuel injection valve that sprays liquid fuel from a closed end to an open end is provided concentrically in a cylindrical swirling chamber into which an air flow swirling around an axis is introduced. The structure is such that liquid fuel is sprayed at the center of the swirling air flow introduced into the swirling chamber, and an ignition plug is provided to ignite the center of the mixed air flow in which the liquid fuel is sprayed into the swirling air flow, and the open end of the swirling chamber is The first combustion tube is concentrically connected through a first throttle, the first combustion tube is formed to have a larger diameter or the same diameter as the swirl chamber, and the second combustion tube is connected to the outlet of the first combustion tube through a second throttle. A spray type combustion device characterized in that a second combustion tube is concentrically connected to each other, and the second combustion tube is formed to have a smaller diameter or the same diameter as that of the first combustion tube. 2. The spray according to claim 1, wherein the diameter of the first throttle is 0.6 times or more the diameter of the swirling chamber, and the diameter of the first combustion cylinder is not more than twice the diameter of the swirling chamber. type combustion device. 3 1.5 if the length of the turning chamber is 0.5 times or more the diameter of the turning chamber
The spray type combustion device according to claim 1 or 2, characterized in that the amount is less than or equal to twice as much. 4 The diameter of the second orifice is 0.5 times or more the diameter of the first combustion cylinder.
The spray combustion device according to any one of claims 1 to 3, characterized in that it is 0.8 times or less. 5. The spray combustion device according to any one of claims 1 to 4, wherein the diameter of the second combustion tube is 0.6 times or more the diameter of the first combustion tube. 6 The fuel injection valve is a two-liquid spray type that atomizes liquid fuel by airflow, and the length of the fuel injection valve protruding into the swirling chamber is 0.5 times or less the length of the swirling chamber. Claims 1 to 5
The spray-type combustion device according to any one of paragraphs. 7. The fuel injection valve is of an ultrasonic vibration type that atomizes liquid fuel by ultrasonic vibration, and the length of the fuel injection valve protruding into the swirling chamber is 0.5 times or less the length of the swirling chamber. A spray combustion device according to any one of claims 1 to 5.
JP21754985A 1985-09-30 1985-09-30 Spray combustion device Granted JPS6277522A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP21754985A JPS6277522A (en) 1985-09-30 1985-09-30 Spray combustion device
CA000519274A CA1285207C (en) 1985-09-30 1986-09-29 Fuel spray combustion device
US06/913,378 US4850195A (en) 1985-09-30 1986-09-30 Fuel spray combustion device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21754985A JPS6277522A (en) 1985-09-30 1985-09-30 Spray combustion device

Publications (2)

Publication Number Publication Date
JPS6277522A JPS6277522A (en) 1987-04-09
JPH0454848B2 true JPH0454848B2 (en) 1992-09-01

Family

ID=16705997

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21754985A Granted JPS6277522A (en) 1985-09-30 1985-09-30 Spray combustion device

Country Status (1)

Country Link
JP (1) JPS6277522A (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5790524A (en) * 1980-11-27 1982-06-05 Nissan Motor Co Ltd Combustion device of gas turbine
JPS5858231U (en) * 1981-10-08 1983-04-20 株式会社高田製作所 high speed burner
JPS5960127A (en) * 1982-09-29 1984-04-06 Toshiba Corp Combustor for gas turbine

Also Published As

Publication number Publication date
JPS6277522A (en) 1987-04-09

Similar Documents

Publication Publication Date Title
JP5508879B2 (en) Premixed direct injection injector
US6863522B2 (en) Method for introducing fuel and/or thermal energy into a gas stream
KR100866327B1 (en) Plasma Burner &amp; Soot Filter
JPS6410727B2 (en)
US3915619A (en) Gas turbine combustors and method of operation
US3914096A (en) Device for vaporizing fuel oil
RU2040731C1 (en) Fuel gasification burner
US4850195A (en) Fuel spray combustion device
WO2008018431A1 (en) Burner
JPH0454848B2 (en)
JPS6179864A (en) Engine warming up device
JP3407228B2 (en) Combustor
JP2604933Y2 (en) Gas turbine combustor
JP3616093B2 (en) Fuel gas generator
KR100866331B1 (en) Plasma Burner &amp; Soot Filter
KR100866328B1 (en) Plasma Burner &amp; Soot Filter
JPS6341711A (en) Burner
JPS6329135Y2 (en)
JP3539256B2 (en) Burner
JPS58158412A (en) Gas burner
RU2361107C2 (en) Nozzle for heating device with improved fuel supply
KR100866330B1 (en) Plasma Burner &amp; Soot Filter
JP2605322B2 (en) Combustor structure
US5090894A (en) Enhanced air/fuel mixing for automotive stirling engine turbulator-type combustors
JPS6021607Y2 (en) Premix combustion burner

Legal Events

Date Code Title Description
LAPS Cancellation because of no payment of annual fees