JP2552578Y2 - Combustion chamber of subchamber internal combustion engine - Google Patents

Combustion chamber of subchamber internal combustion engine

Info

Publication number
JP2552578Y2
JP2552578Y2 JP1991094949U JP9494991U JP2552578Y2 JP 2552578 Y2 JP2552578 Y2 JP 2552578Y2 JP 1991094949 U JP1991094949 U JP 1991094949U JP 9494991 U JP9494991 U JP 9494991U JP 2552578 Y2 JP2552578 Y2 JP 2552578Y2
Authority
JP
Japan
Prior art keywords
combustion chamber
sub
chamber
main combustion
main
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 - Fee Related
Application number
JP1991094949U
Other languages
Japanese (ja)
Other versions
JPH0538327U (en
Inventor
洋一 片岡
浩二 井元
忠雄 大村
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP1991094949U priority Critical patent/JP2552578Y2/en
Publication of JPH0538327U publication Critical patent/JPH0538327U/en
Application granted granted Critical
Publication of JP2552578Y2 publication Critical patent/JP2552578Y2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Combustion Methods Of Internal-Combustion Engines (AREA)

Description

【考案の詳細な説明】[Detailed description of the invention]

【0001】[0001]

【産業上の利用分野】この考案は副室式内燃機関の燃焼
室に関する。
BACKGROUND OF THE INVENTION The present invention relates to a combustion chamber of a sub-chamber internal combustion engine.

【0002】[0002]

【従来の技術】従来の副室式内燃機関の燃焼室を図3〜
4によって説明する。図3は従来の副室式内燃機関の燃
焼室のピストンが上死点にあるときの断面図、図4は図
3におけるIV−IV断面図である。図において7はシリン
ダ、4はシリンダヘッド、6はピストンで何れも内燃機
関の公知の要素である。2は副燃焼室でシリンダヘッド
4内に設けられ略円筒形である。副燃焼室の形状は円筒
形、球形、円錐形を基本とした各種形状があるがこの例
は円筒形を基本としている。1は主燃焼室でピストン6
の頂面、シリンダヘッド4の下面、シリンダ7でかこま
れた空間である。8は副室口金で副燃焼室2の先端部を
形成し、主燃焼室1へ突出し、主燃焼室1と副燃焼室2
を仕切っている。3は副室噴口で副室口金8の先端部に
あけられた穴で8個あり副室口金8の中心線に関して放
射状に等間隔に設けられている。5は燃料噴射弁で副燃
焼室に開口している。
2. Description of the Related Art A combustion chamber of a conventional sub-chamber internal combustion engine is shown in FIGS.
4 will be described. FIG. 3 is a sectional view when a piston of a combustion chamber of a conventional sub-chamber internal combustion engine is at a top dead center, and FIG. 4 is a sectional view taken along line IV-IV in FIG. In the figure, reference numeral 7 denotes a cylinder, 4 denotes a cylinder head, and 6 denotes a piston, all of which are known elements of an internal combustion engine. Reference numeral 2 denotes a sub-combustion chamber provided in the cylinder head 4 and having a substantially cylindrical shape. The auxiliary combustion chamber has various shapes based on a cylindrical shape, a spherical shape, and a conical shape, but this example is based on a cylindrical shape. 1 is a main combustion chamber and a piston 6
, The lower surface of the cylinder head 4, and the space surrounded by the cylinder 7. Reference numeral 8 denotes a sub-chamber base, which forms the tip of the sub-combustion chamber 2 and protrudes into the main combustion chamber 1.
Is divided. Reference numeral 3 denotes a sub-chamber nozzle, which has eight holes formed at the tip of the sub-chamber base 8 and is provided at equal intervals radially with respect to the center line of the sub-chamber base 8. Reference numeral 5 denotes a fuel injection valve which is open to the sub combustion chamber.

【0003】次に従来例の作用を説明する。機関運転時
圧縮行程でシリンダ内の圧縮された空気が主燃焼室1か
ら副室噴口3を通って副燃焼室2内へ流入する。ピスト
ンの上死点少し手前で燃料噴射弁5から副燃焼室2内へ
燃料が噴射される。この噴射された燃料は着火点以上の
高温空気と混合し、その一部が自己着火燃焼し副燃焼室
2内の圧力が上昇し、前記副燃焼室2内の未燃燃料は空
気もろとも副室噴口3から主燃焼室1へ噴出され、主燃
焼室内の空気と混合し燃焼する。この間にピストンは上
死点をすぎ膨張行程になる。
Next, the operation of the conventional example will be described. During the compression stroke during engine operation, compressed air in the cylinder flows from the main combustion chamber 1 through the sub chamber injection port 3 into the sub combustion chamber 2. The fuel is injected from the fuel injection valve 5 into the sub-combustion chamber 2 slightly before the top dead center of the piston. The injected fuel is mixed with high-temperature air having a temperature equal to or higher than the ignition point, and a part of the fuel is self-ignited and the pressure in the sub-combustion chamber 2 is increased. The fuel is ejected from the injection port 3 into the main combustion chamber 1 and mixed with air in the main combustion chamber to burn. During this time, the piston passes the top dead center and enters the expansion stroke.

【0004】[0004]

【考案が解決しようとする課題】従来の副室式内燃機関
の燃焼室には次の不具合がある。副室式内燃機関の燃
費、吐煙を改善するためには、主燃焼室内における燃料
と空気の混合気形成、従って燃焼促進が重要である。従
来の技術では複数の副室噴口が等間隔に設けられている
ので、副室噴口の総面積を一定とし副室噴口数を減少す
ると各副室噴口径は大きくなるため噴流ペネトレーショ
ンは向上するが噴流分散性が悪化し噴流と噴流の間の空
気利用率が悪化し燃焼は不良となる。逆に副室噴口数を
増すと副燃焼室から主燃焼室へ流入する噴流の分散性は
増すが、各噴口径が小さくなるため噴流ペネトレーショ
ンが低下し、燃料と空気の混合気形成、燃焼が悪化す
る。本考案の目的は前記不具合を解消し、燃費、吐煙を
低減するために主燃焼室内の燃料と空気の混合気形成従
って燃焼を促進するための燃焼室を提供するにある。
The combustion chamber of the conventional sub-chamber internal combustion engine has the following disadvantages. In order to improve the fuel efficiency and smoke emission of the sub-chamber internal combustion engine, it is important to form a mixture of fuel and air in the main combustion chamber, and therefore to promote combustion. In the prior art, a plurality of sub-chamber nozzles are provided at equal intervals, so if the total area of the sub-chamber nozzles is constant and the number of sub-chamber nozzles is reduced, the diameter of each sub-chamber nozzle increases, so that the jet penetration improves. The jet dispersibility deteriorates, the air utilization rate between the jets deteriorates, and the combustion becomes poor. Conversely, increasing the number of sub-chamber injection ports increases the dispersibility of the jet flowing from the sub-combustion chamber to the main combustion chamber, but reduces the diameter of each injection port, lowering the jet penetration, resulting in the formation of a fuel-air mixture and combustion. Getting worse. SUMMARY OF THE INVENTION An object of the present invention is to provide a combustion chamber for promoting the formation of a mixture of fuel and air in the main combustion chamber and thus the combustion in order to solve the above problems and reduce fuel consumption and smoke emission.

【0005】[0005]

【課題を解決するための手段】本考案の要旨は、先端部
がシリンダヘッドから主燃焼室内に突出された副室口金
の内部に設けられた副燃焼室と前記主燃焼室とを複数個
の副室噴口により連通されてなる内燃機関の燃焼室にお
いて、前記複数個の副室噴口は、隣り合う2個づつの中
心線(C−C)が前記主燃焼室の中心近傍に配置された
前記副燃焼室から前記主燃焼室内の外周側へ向けて延
び、前記中心線(C−C)の延長線が水平方向の投影に
おいて、主燃焼室の外周寄りの部位で交叉するように構
成されたことを特徴ととする副室式内燃機関の燃焼室に
ある。
SUMMARY OF THE INVENTION The gist of the present invention is that a main combustion chamber and a sub-combustion chamber provided inside a sub-chamber base whose tip projects from the cylinder head into the main combustion chamber are provided. In the combustion chamber of the internal combustion engine which is communicated with the sub-chamber injection port, the plurality of sub-chamber injection ports have two adjacent center lines (C-C) arranged near the center of the main combustion chamber. The main combustion chamber extends from the sub-combustion chamber toward the outer periphery, and the extension of the center line (C-C) intersects at a position near the outer periphery of the main combustion chamber in horizontal projection. A combustion chamber of a sub-chamber internal combustion engine.

【0006】[0006]

【作用】副燃焼室内に噴射された燃料の一部が燃焼して
副燃焼室の圧力が上り副燃焼室から、主燃焼室中心に近
傍に設けられた前記副燃焼室から主燃焼室の外周へ向け
て延びる副室噴口を通って主燃焼室へ既燃未燃ガスや燃
料が流出する際、隣り合う2つずつの副室噴口の軸線の
延長が主燃焼室内の外周寄りの部位で交叉するため、噴
流が前記交叉部で衝突し合い、ベクトルが合成され、噴
流ペネトレーションを向上できる。更に衝突噴流により
噴流(既燃ガス,燃料,空気で構成)中に大きな乱れを
生じるため、主燃燃室内の未燃燃料と空気の混合気形
成、燃焼を促進できる。
A part of the fuel injected into the sub-combustion chamber burns and the pressure in the sub-combustion chamber rises, and from the sub-combustion chamber to the outer periphery of the main combustion chamber from the sub-combustion chamber provided near the center of the main combustion chamber When burned unburned gas or fuel flows out to the main combustion chamber through the sub chamber injection port extending toward the main chamber, the extension of the axis of two adjacent sub chamber injection ports intersects at a position near the outer periphery in the main combustion chamber Therefore, the jets collide with each other at the intersection, the vectors are synthesized, and the jet penetration can be improved. Further, since the impinging jet causes large turbulence in the jet (composed of burned gas, fuel, and air), the formation and combustion of a mixture of unburned fuel and air in the main combustion chamber can be promoted.

【0007】[0007]

【実施例】本考案の実施例を図1〜2によって説明す
る。図1は実施例のビストンが上死点にあるときの燃焼
室の断面図、図2は図1におけるII−II断面図であ
る。図において1は主燃焼室でピストン6の頂面、シリ
ンダヘッド4、シリンダヘッド7によってかこまれた空
間である。2は副燃焼室でシリンダヘッド4に固定され
た副室口金8内に設けられ略円筒形である。副燃焼室2
は円筒形、球形、円盤形を基本とした各種形状があるが
この実施例は円筒形を基本としている。6は燃料噴射弁
で副燃焼室2に開口している。副燃焼室2には機関始動
時に副燃焼室内を予熱するグロープラグを必要に応じ設
置するが、図示していない。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described with reference to FIGS. FIG. 1 is a cross-sectional view of the combustion chamber when the piston according to the embodiment is at the top dead center, and FIG. 2 is a cross-sectional view along II-II in FIG. In the figure, reference numeral 1 denotes a main combustion chamber, which is a space surrounded by the top surface of the piston 6, the cylinder head 4, and the cylinder head 7. Reference numeral 2 denotes a sub-combustion chamber which is provided in a sub-chamber base 8 fixed to the cylinder head 4 and has a substantially cylindrical shape. Secondary combustion chamber 2
There are various shapes based on a cylindrical shape, a spherical shape, and a disk shape, but this embodiment is based on a cylindrical shape. Reference numeral 6 denotes a fuel injection valve which is open to the sub-combustion chamber 2. A glow plug for preheating the sub-combustion chamber when the engine is started is installed in the sub-combustion chamber 2 as necessary, but is not shown.

【0008】前記副室口金8は、前記副燃焼室2の先端
部をその内部に形成し主燃焼室内へ突出している。そし
て、該副燃焼室2は図1に示すように、主燃焼室1のほ
ぼ中心に配置されている。3は副室噴口で、前記副室口
金8の主燃焼室1へ突き出た部分に設けられ副燃焼室2
と主燃焼室1を連通する偶数の穴であり、図2に示すよ
うに隣り合う2個ずつの中心線(C−C)の延長が水平
方向の投影において主燃焼室1内の外周部位で交叉して
いる。
The sub-chamber base 8 has the tip of the sub-combustion chamber 2 formed therein and protrudes into the main combustion chamber. The sub-combustion chamber 2 is arranged substantially at the center of the main combustion chamber 1 as shown in FIG. Reference numeral 3 denotes a sub-chamber nozzle, which is provided at a portion of the sub-chamber mouthpiece 8 projecting into the main combustion chamber 1.
And an even number of holes communicating the main combustion chamber 1 with each other. As shown in FIG. 2, the extension of two adjacent center lines (C-C) at the outer peripheral portion in the main combustion chamber 1 in horizontal projection. Crossed.

【0009】次に実施例の作用を説明する。機関運転時
圧縮行程でシリンダ内の空気が圧縮され副室噴口3を通
って副燃焼室2内へ流入する。前記圧縮行程の終り近く
で燃料噴射弁5から副燃焼室2内へ燃料が噴射され、噴
射された燃料の一部が副燃焼室2内で燃焼し、副燃焼室
2内の圧力が上昇し副燃焼室内の未燃物は既燃物もろと
も副室噴口3から主燃焼室1へ噴出する。この間にピス
トン6は上死点をすぎ膨張行程になる。前記主燃焼室1
へ噴出した未燃物は主燃焼室1の空気と混合し燃焼す
る。
Next, the operation of the embodiment will be described. In the compression stroke during engine operation, air in the cylinder is compressed and flows into the sub-combustion chamber 2 through the sub-chamber injection port 3. Near the end of the compression stroke, fuel is injected from the fuel injection valve 5 into the sub-combustion chamber 2, a part of the injected fuel burns in the sub-combustion chamber 2, and the pressure in the sub-combustion chamber 2 increases. The unburned matter in the sub-combustion chamber is ejected from the sub chamber injection port 3 to the main combustion chamber 1 together with the burned matter. During this time, the piston 6 passes the top dead center and enters an expansion stroke. The main combustion chamber 1
The unburned matter ejected to the air mixes with the air in the main combustion chamber 1 and burns.

【0010】任意の一つの副室噴口3から主燃焼室1へ
噴出した噴流は何れかの隣の同様の噴流と主燃焼室1内
で衝突する。その様子を模型的に図2に示す。この噴流
の衝突によりそれぞれの噴流のベクトルが合成され噴流
ペネトレーションを向上できる。更に衝突噴流により噴
流(既燃ガス、燃料、空気で構成)中に大きな乱れを生
じるため主燃焼室1内の未燃燃料と空気の混合気形成、
燃焼を促進し燃費、吐煙を改善できる。
A jet jet from any one sub chamber injection port 3 into the main combustion chamber 1 collides with any adjacent similar jet in the main combustion chamber 1. FIG. 2 schematically shows the state. By the collision of the jets, the vectors of the respective jets are synthesized, and the jet penetration can be improved. Furthermore, since the impinging jet causes large turbulence in the jet (composed of burned gas, fuel, and air), a mixture of unburned fuel and air in the main combustion chamber 1 is formed.
It promotes combustion and improves fuel efficiency and smoke emission.

【0011】[0011]

【考案の効果】本考案は前記のとおり構成されているの
で主燃焼室内の外周部位での2つずつの噴流の衝突によ
り噴流のペネトレーションが向上し、且噴流の中に大き
な乱れを生じるため主燃焼室内の混合気形成、燃焼が促
進され、燃費,吐煙を低減できる。
[Effect of the Invention] The present invention is configured as described above, so that the collision of two jets at the outer peripheral portion in the main combustion chamber improves the penetration of the jet, and also causes a large turbulence in the jet. Formation of air-fuel mixture and combustion in the combustion chamber are promoted, and fuel consumption and smoke emission can be reduced.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本考案に係る実施例の燃焼室のピストンが上死
点にあるときの断面図。
FIG. 1 is a sectional view of a combustion chamber according to an embodiment of the present invention when a piston is at a top dead center.

【図2】図1におけるII−II断面図。FIG. 2 is a sectional view taken along the line II-II in FIG.

【図3】従来例の燃焼室のピストンが上死点にあるとき
の断面図。
FIG. 3 is a cross-sectional view when a piston of a conventional combustion chamber is at a top dead center.

【図4】図3におけるIV−IV断面図。FIG. 4 is a sectional view taken along line IV-IV in FIG. 3;

【符号の説明】[Explanation of symbols]

1…主燃焼室、2…副燃焼室、3…副室噴口、4…シリ
ンダヘッド、8…副室口金、c−c…副室噴口の中心
線。
DESCRIPTION OF SYMBOLS 1 ... Main combustion chamber, 2 ... Subcombustion chamber, 3 ... Subchamber nozzle, 4 ... Cylinder head, 8 ... Subchamber base, cc ... Center line of subchamber injection port.

Claims (1)

(57)【実用新案登録請求の範囲】(57) [Scope of request for utility model registration] 【請求項1】 先端部がシリンダヘッドから主燃焼室内
に突出された副室口金の内部に設けられた副燃焼室と前
記主燃焼室とを複数個の副室噴口により連通されてなる
内燃機関の燃焼室において、前記複数個の副室噴口は、
隣り合う2個づつの中心線(C−C)が前記主燃焼室の
中心近傍に配置された前記副燃焼室から前記主燃焼室内
の外周側へ向けて延び、前記中心線(C−C)の延長線
が水平方向の投影において、主燃焼室の外周寄りの部位
で交叉するように構成されたことを特徴とする副室式内
燃機関の燃焼室。
An internal combustion engine in which a sub combustion chamber provided inside a sub chamber base whose tip projects from a cylinder head into a main combustion chamber and the main combustion chamber are communicated by a plurality of sub chamber injection holes. In the combustion chamber, the plurality of sub-chamber injection ports are:
Two adjacent center lines (CC) extend from the sub-combustion chamber disposed near the center of the main combustion chamber toward the outer peripheral side of the main combustion chamber, and the center line (CC) is provided. A combustion chamber of a sub-chamber internal combustion engine, characterized in that, in a horizontal projection, an extension line of the crosses at a portion near the outer periphery of the main combustion chamber.
JP1991094949U 1991-10-24 1991-10-24 Combustion chamber of subchamber internal combustion engine Expired - Fee Related JP2552578Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1991094949U JP2552578Y2 (en) 1991-10-24 1991-10-24 Combustion chamber of subchamber internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1991094949U JP2552578Y2 (en) 1991-10-24 1991-10-24 Combustion chamber of subchamber internal combustion engine

Publications (2)

Publication Number Publication Date
JPH0538327U JPH0538327U (en) 1993-05-25
JP2552578Y2 true JP2552578Y2 (en) 1997-10-29

Family

ID=14124197

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1991094949U Expired - Fee Related JP2552578Y2 (en) 1991-10-24 1991-10-24 Combustion chamber of subchamber internal combustion engine

Country Status (1)

Country Link
JP (1) JP2552578Y2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS51104203U (en) * 1976-01-27 1976-08-20

Also Published As

Publication number Publication date
JPH0538327U (en) 1993-05-25

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A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 19970610

LAPS Cancellation because of no payment of annual fees