JPS5968518A - Combustion chamber for engine with pre-chamber - Google Patents
Combustion chamber for engine with pre-chamberInfo
- Publication number
- JPS5968518A JPS5968518A JP57178268A JP17826882A JPS5968518A JP S5968518 A JPS5968518 A JP S5968518A JP 57178268 A JP57178268 A JP 57178268A JP 17826882 A JP17826882 A JP 17826882A JP S5968518 A JPS5968518 A JP S5968518A
- Authority
- JP
- Japan
- Prior art keywords
- chamber
- sub
- nozzle
- main
- minimum angle
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B19/00—Engines characterised by precombustion chambers
- F02B19/14—Engines characterised by precombustion chambers with compression ignition
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Abstract
Description
【発明の詳細な説明】 本発明は副室式機関の燃焼室に関する。[Detailed description of the invention] The present invention relates to a combustion chamber of a pre-chamber engine.
従来の副室式機関の副燃焼室(以下副室とよぶ)を第1
図に示す。図において、副室1はシリンダヘッド4内に
凹設されていて、その構造は上部が半球型、下部は円錐
台のものあるいは円柱型のもの等があるが、同図では下
部が円錐台のものを示す。副室1には、燃料噴射弁5及
び機関始動時に副室1内を予熱するグロープラグ6を必
要に応じて設ける。副、室1と、ピストン7の頂面、シ
リンダ8.シリンダヘッド4の下面から構成される主燃
焼室(以下主室とよぶ)3とは2口金9の底部の隔壁に
よシ区画され、同隔壁に穿設された副室噴口2により連
通している。同隔壁の副室1側の端面、即ち副室底面9
aと主室3側の端面とは幅室中心線A−Aに直交し、副
室底面9aと副室噴口2の軸心線とのなす最小角度をθ
2とし、主室側端面と副室噴口2の軸心線とのなす最小
角度を01 とするとき、θ1−02である。The auxiliary combustion chamber (hereinafter referred to as the auxiliary chamber) of the conventional auxiliary chamber type engine is the first
As shown in the figure. In the figure, the auxiliary chamber 1 is recessed in the cylinder head 4, and its structure has a hemispherical upper part and a truncated conical or cylindrical lower part. show something The auxiliary chamber 1 is provided with a fuel injection valve 5 and a glow plug 6 for preheating the inside of the auxiliary chamber 1 when the engine is started, as necessary. Secondary, chamber 1 and top surface of piston 7, cylinder 8. A main combustion chamber (hereinafter referred to as the main chamber) 3 formed from the lower surface of the cylinder head 4 is divided by a partition wall at the bottom of the two nozzles 9, and is communicated with the sub-chamber nozzle 2 bored in the partition wall. There is. The end surface of the partition wall on the subchamber 1 side, that is, the subchamber bottom surface 9
a and the end face on the main chamber 3 side are perpendicular to the width chamber center line A-A, and the minimum angle between the sub-chamber bottom surface 9a and the axis of the sub-chamber nozzle 2 is θ.
2 and the minimum angle between the main chamber side end face and the axis of the sub chamber nozzle 2 is 01, then θ1-02.
機関運転時の圧縮行程で、ピストン7により主室3内空
気が圧縮され副室噴口2を経て、副室1内に流入し、渦
流Sを生成する。副室1に流入した空気と燃料噴射弁5
から噴射される燃料との混合はこの渦流によシ促進され
1着火、燃焼する。During the compression stroke during engine operation, air in the main chamber 3 is compressed by the piston 7 and flows into the subchamber 1 through the subchamber nozzle 2 to generate a vortex S. Air flowing into the auxiliary chamber 1 and the fuel injection valve 5
Mixing with the fuel injected from the fuel is promoted by this vortex, and ignition occurs and combustion occurs.
副室1内の既燃、未燃ガスは副室噴口2を通って。Burnt and unburned gas in the pre-chamber 1 passes through the pre-chamber nozzle 2.
主室3内に噴出し、ピストンに仕事をすると同時に主室
3内の空気との混合、燃焼を行わしめる。It is ejected into the main chamber 3, works on the piston, and simultaneously mixes with the air in the main chamber 3 and causes combustion.
しかし上記のものには次の欠点がある。However, the above method has the following drawbacks.
副室式機関の燃費、吐煙を低減するためには。In order to reduce the fuel consumption and smoke emissions of pre-chamber engines.
副室1内の未燃、既燃ガスをすみやかに主室3に流出し
、主室3内の空気との混合、燃焼を促進させねばならな
い。副室1内の未燃、既燃ガスをすみやかに流出するた
めに、副室噴口2の通路断面積を大きくすると、主室3
内へのガスの噴出速度が低下し、主室3内の空気との混
合、従って燃焼が悪化する。また、副室噴口角度θ2
(=θ1 )を大きくすると、副室1内の未燃、既燃ガ
スは主室3に流出しやすくなるが、副室噴口角度θ2(
=θ1)が大きいため主室3内の噴流のペネトレーショ
ンが低下し、空気との混合従って燃焼が悪くなり。The unburnt and burned gases in the auxiliary chamber 1 must quickly flow out into the main chamber 3 to promote mixing with the air in the main chamber 3 and combustion. In order to quickly drain out the unburned and burned gas in the subchamber 1, if the passage cross-sectional area of the subchamber nozzle 2 is increased, the main chamber 3
The injection speed of the gas inward decreases, and the mixing with the air in the main chamber 3 and therefore the combustion deteriorates. Also, the pre-chamber nozzle angle θ2
(=θ1), the unburned and burned gas in the subchamber 1 will more easily flow out to the main chamber 3, but the subchamber nozzle angle θ2(
= θ1) is large, the penetration of the jet flow in the main chamber 3 decreases, and the mixing with air and hence combustion deteriorates.
吐煙、燃費を改善できない。Smoke and fuel efficiency cannot be improved.
本発明の目的は上記の点に着目し2幅室式機関の燃費、
吐煙対策として副室から主室へのガスの流出を容易にす
るために副室噴口角度を大きくした場合に生ずる主室内
の噴流の被ネトレーション悪化、従って空気との混合、
燃焼悪化を防止できる燃焼室を提供することであシ、そ
の特徴とするところは、主室と副室とを区画する隔壁に
穿設され上記主室と副室とを連通ずる副室噴口を有する
副室式内燃機関において、上記副室噴口の軸心線と上記
隔壁の副室側端面とのなす最小角度をθ2で表わし、上
記副室噴口の軸心線と上記隔壁の主室側端面とのなす最
小角度をθ1とするとき、上記隔壁の副室側端面の少な
くとも上記副室噴口の開口部まわりの一部を傾斜させて
θ2〉θ1としたことでちる。The purpose of the present invention is to improve the fuel efficiency of a double-chamber engine by focusing on the above-mentioned points.
When the antechamber nozzle angle in the antechamber is increased to facilitate the outflow of gas from the antechamber to the main chamber as a smoke countermeasure, netting of the jet in the main chamber that occurs is worsened, resulting in mixing with air.
The purpose of the present invention is to provide a combustion chamber capable of preventing deterioration of combustion, and its feature is that a sub-chamber nozzle is provided in a partition wall that partitions the main chamber and the sub-chamber, and communicates the main chamber with the sub-chamber. In the pre-chamber type internal combustion engine, the minimum angle between the axis of the pre-chamber nozzle and the end surface of the partition wall on the sub-chamber side is represented by θ2, and the minimum angle between the axis of the pre-chamber nozzle and the end surface of the partition wall on the main chamber side When the minimum angle formed by the partition wall is θ1, at least a part of the end surface of the partition wall on the sub-chamber side around the opening of the sub-chamber nozzle is inclined so that θ2>θ1.
以下図面を参照して本発明による実施例につき説明する
。Embodiments of the present invention will be described below with reference to the drawings.
第2図は本発明による第1実施例の副室を示す断面図で
ある。FIG. 2 is a sectional view showing the subchamber of the first embodiment of the present invention.
図において、1、は副室、2は副室噴口、3は主室、4
はシリングヘッド、5は燃料噴射弁、6はグロープラグ
、7はピストン、8はシリンダである。In the figure, 1 is the subchamber, 2 is the subchamber nozzle, 3 is the main chamber, and 4
is a cylinder head, 5 is a fuel injection valve, 6 is a glow plug, 7 is a piston, and 8 is a cylinder.
副室噴口2は副室1と主室3との間の隔壁を貫通して両
室1,3を連通している。The auxiliary chamber nozzle 2 penetrates the partition wall between the auxiliary chamber 1 and the main chamber 3 to communicate the two chambers 1 and 3.
副室1は上部構造が半球型で、上記隔壁の副室側端面で
ある副室底面1aは、全体を図示のように、隔壁の内方
側を厚くして、傾斜させている。The auxiliary chamber 1 has a hemispherical upper structure, and the auxiliary chamber bottom surface 1a, which is the end surface of the partition wall on the side of the auxiliary chamber, is made thicker on the inner side of the partition wall and inclined as a whole, as shown in the figure.
即ち、副室噴口2の軸心線と副室底面1aとのなす最小
角度をθ2とし、副室噴口2の軸心線と上記隔壁の主室
側端面とのなす最小角度をθ1とすると、上記の傾斜に
よシθ2〉θ1に形成されている。That is, if the minimum angle between the axis of the sub-chamber nozzle 2 and the sub-chamber bottom surface 1a is θ2, and the minimum angle between the axis of the sub-chamber nozzle 2 and the end surface of the partition wall on the main chamber side is θ1, Due to the above-mentioned inclination, the angle θ2>θ1 is formed.
上記構成の場合の作用、効果について述べる。The functions and effects of the above configuration will be described.
副室底面1aを図示のように傾斜させると、副室1から
主室3へのガス流出が容易になるため。If the sub-chamber bottom 1a is inclined as shown, gas can easily flow out from the sub-chamber 1 to the main chamber 3.
副室噴口2の絞り損失が低減すると同時に、高負荷時に
副室1内に多量の燃料を噴射しても空気不足にはならな
い。The throttling loss of the sub-chamber nozzle 2 is reduced, and at the same time, even if a large amount of fuel is injected into the sub-chamber 1 under high load, no air shortage occurs.
また、主室3内の噴流のペネトレーションを確保でき、
未燃ガスと空気との混合が促進され燃焼が改善される。In addition, the penetration of the jet flow inside the main chamber 3 can be ensured,
Mixing of unburned gas and air is promoted and combustion is improved.
以上の理由によシ機関の燃費、吐煙低減が実現できる。For the above reasons, the engine's fuel efficiency and smoke reduction can be achieved.
第3図は本発明による第2実施例の副室を示す断面図で
ある。FIG. 3 is a sectional view showing the subchamber of the second embodiment of the present invention.
副室1の底面の一部、即ち副室噴口2の開口部まわシの
部分1bを傾斜させて、θ2〉θlとした場合であり、
その作用、効果は前記した実施例の場合と同じである。This is a case where a part of the bottom surface of the subchamber 1, that is, a portion 1b around the opening of the subchamber nozzle 2 is inclined so that θ2>θl,
Its action and effect are the same as in the embodiment described above.
本発明による第3実施例としては次のものがある。A third embodiment of the present invention is as follows.
第1実施例の副室1の中心線A−Aをθ2−θl傾斜さ
せることによシ、副室1を上記中心線A−Aに対し軸対
称としたものである。この場合は副室の加工が容易とな
り1作用、効果は第1実施例の場合と同じである。By tilting the center line A-A of the sub-chamber 1 of the first embodiment by θ2-θ1, the sub-chamber 1 is made axially symmetrical with respect to the center line A-A. In this case, the subchamber can be easily processed, and the effects and effects are the same as in the first embodiment.
第1図は従来の副室式機関の副室を示す断面図2第2図
は本発明による第1実施例の副室を示す断。
面図、第3図は本発明による第2実施例の副室を示す断
面図である。
1・・・副室、2・・・副室噴口、3・・・主室、1a
。
9a・・・副室底面、1b・・・副室底面の一部。
牙1 図
/〆一一
つ
□□仝赤
ゝ−8
太2図
)
/
〜8
コ
105−
5
f
2
5
−ブFIG. 1 is a cross-sectional view showing the sub-chamber of a conventional sub-chamber type engine; FIG. 2 is a cross-sectional view showing the sub-chamber of a first embodiment of the present invention. The plan view and FIG. 3 are cross-sectional views showing the subchamber of the second embodiment of the present invention. 1... Sub-chamber, 2... Sub-chamber nozzle, 3... Main chamber, 1a
. 9a... Bottom of the sub-chamber, 1b... Part of the bottom of the sub-chamber. Fang 1 Figure / 〆One one□□Red ゝ-8 Thick 2) / ~8 Ko105- 5 f 2 5 -B
Claims (1)
副室とを連通ずる副室噴口を有する副室式内燃機関にお
いて、上記副室噴口の軸心線と上記隔壁の副室側端面と
のなす最小角度を02で表わし、上記副室噴口の軸心線
と上記隔壁の主室側端面とのなす最小角度をθ1とする
とき、上記隔壁の副室側端面の少なくとも上記副室噴口
の開口部まわシの一部を傾斜させてθ2〉θ1としたこ
とを特徴とする副室式機関の燃焼室。1. In a sub-chamber type internal combustion engine having a sub-chamber nozzle that is bored in a partition wall that partitions a main chamber and a sub-chamber and communicates the main chamber and sub-chamber, the axial line of the sub-chamber nozzle and the line of the partition wall communicate with each other. When the minimum angle between the sub-chamber side end surface and the sub-chamber side end surface is represented by 02, and the minimum angle between the axial line of the sub-chamber nozzle and the main chamber-side end surface of the partition wall is θ1, at least the sub-chamber side end surface of the partition wall A combustion chamber for a pre-chamber type engine, characterized in that a part of the opening circumference of the pre-chamber nozzle is inclined so that θ2>θ1.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57178268A JPS5968518A (en) | 1982-10-13 | 1982-10-13 | Combustion chamber for engine with pre-chamber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57178268A JPS5968518A (en) | 1982-10-13 | 1982-10-13 | Combustion chamber for engine with pre-chamber |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5968518A true JPS5968518A (en) | 1984-04-18 |
Family
ID=16045508
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57178268A Pending JPS5968518A (en) | 1982-10-13 | 1982-10-13 | Combustion chamber for engine with pre-chamber |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5968518A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59139518U (en) * | 1983-03-09 | 1984-09-18 | いすゞ自動車株式会社 | Swirl chamber diesel engine |
JPS59168524U (en) * | 1983-04-27 | 1984-11-12 | マツダ株式会社 | Diesel engine pre-chamber structure |
EP0150050A2 (en) * | 1984-01-21 | 1985-07-31 | Mitsubishi Jukogyo Kabushiki Kaisha | Structure for combustion chamber of auxiliary chamber type internal combustion engine |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS526907B1 (en) * | 1971-03-31 | 1977-02-25 |
-
1982
- 1982-10-13 JP JP57178268A patent/JPS5968518A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS526907B1 (en) * | 1971-03-31 | 1977-02-25 |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59139518U (en) * | 1983-03-09 | 1984-09-18 | いすゞ自動車株式会社 | Swirl chamber diesel engine |
JPS59168524U (en) * | 1983-04-27 | 1984-11-12 | マツダ株式会社 | Diesel engine pre-chamber structure |
EP0150050A2 (en) * | 1984-01-21 | 1985-07-31 | Mitsubishi Jukogyo Kabushiki Kaisha | Structure for combustion chamber of auxiliary chamber type internal combustion engine |
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