JPH0835427A - Combustion chamber of auxiliary chamber-type internal combustion engine - Google Patents

Combustion chamber of auxiliary chamber-type internal combustion engine

Info

Publication number
JPH0835427A
JPH0835427A JP6192865A JP19286594A JPH0835427A JP H0835427 A JPH0835427 A JP H0835427A JP 6192865 A JP6192865 A JP 6192865A JP 19286594 A JP19286594 A JP 19286594A JP H0835427 A JPH0835427 A JP H0835427A
Authority
JP
Japan
Prior art keywords
combustion chamber
auxiliary
chamber
sub
gas
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.)
Withdrawn
Application number
JP6192865A
Other languages
Japanese (ja)
Inventor
Koji Imoto
浩二 井元
Tadao Omura
忠雄 大村
Yoichi Kataoka
洋一 片岡
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 JP6192865A priority Critical patent/JPH0835427A/en
Publication of JPH0835427A publication Critical patent/JPH0835427A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

PURPOSE:To decrease the gas flow loss, so as to promote gas outflow into a main combustion chamber, and so as to decrease the fuel consumption and NOx by largely inclining the side wall on the lower part of an auxiliary combustion chamber toward the upper part, in an auxiliary chamber-type internal combustion engine wherein the auxiliary combustion chamber is communicated with the main combustion chamber through a plurality of auxiliary chamber injection ports. CONSTITUTION:In an auxiliary chamber-type internal combustion engine wherein an auxiliary combustion chamber 2 in which a fuel injection valve 5 and a glow plug are installed are communicated with a main combustion chamber 1 through a plurality of auxiliary chamber injection ports 3, the side wall on the lower part 22 of the auxiliary combustion chamber is largely inclined in the direction of the auxiliary combustion chamber upper part 21. When gas in the main combustion chamber 1 is compressed and allowed to flow to the auxiliary combustion chamber lower part 22 from the auxiliary chamber injection port 3, gas is prevented from being rapidly expanded since the opening end side of the auxiliary chamber injection port 3 is contracted, and the gas flow loss is decreased. Since the side wall of the auxiliary combustion chamber lower part 22 is largely inclined, the gas flow velocity and the mixing combustion in the auxiliary combustion chamber 2 are restrained, and NOx can be prevented from being increased.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は副室式内燃機関の燃焼室
に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combustion chamber of an internal combustion engine of a subchamber type.

【0002】[0002]

【従来の技術】従来例の副室式内燃機関の燃焼室を図2
によって説明する。図2は従来例の副室式内燃機関の燃
焼室の断面図である。図において副燃焼室2aはシリン
ダヘッド4a内に設置されている。副燃焼室の形状は円
柱形、球形、円錐台形等を基本とした各種形状のものが
あるが副燃焼室2aは円柱形を基本にしたものである。
副燃焼室2aには燃料噴射弁5を設置し、機関始動の時
に副燃焼室内を予熱するグロープラグ(図示していな
い)を必要に応じて設置する。副燃焼室2aは副室噴口
3aを介してピストン6aの頂面、シリンダ7a、シリ
ンダヘッド4aの下面で構成される主燃焼室1aと連通
している。副燃焼室下部22aの形状は円柱形で先端は
球形である。
2. Description of the Related Art FIG. 2 shows a combustion chamber of a conventional auxiliary chamber type internal combustion engine.
It will be explained by. FIG. 2 is a sectional view of a combustion chamber of a conventional sub-chamber internal combustion engine. In the figure, the auxiliary combustion chamber 2a is installed in the cylinder head 4a. The auxiliary combustion chamber 2a has various shapes based on a cylindrical shape, a spherical shape, a truncated cone shape, etc., but the auxiliary combustion chamber 2a is based on a cylindrical shape.
A fuel injection valve 5 is installed in the auxiliary combustion chamber 2a, and a glow plug (not shown) that preheats the auxiliary combustion chamber when the engine is started is installed as necessary. The sub combustion chamber 2a communicates with the main combustion chamber 1a formed by the top surface of the piston 6a, the cylinder 7a, and the lower surface of the cylinder head 4a through the sub chamber injection port 3a. The shape of the sub-combustion chamber lower portion 22a is cylindrical and the tip is spherical.

【0003】前記従来例の作用を説明する。機関運転時
の圧縮行程でピストン6aにより主燃焼室1a内の空気
が圧縮され副室噴口3aを経て副燃焼室2a内に流入す
る。燃料噴射弁5aから副燃焼室2a内に燃料を噴射す
ると、燃料と空気が混合し着火燃焼する。副燃焼室2a
から噴出される未燃、燃料の主燃焼室1a内への空気と
の混合は副燃焼室2aからのガス噴出による。
The operation of the conventional example will be described. Air in the main combustion chamber 1a is compressed by the piston 6a during the compression stroke during engine operation and flows into the sub combustion chamber 2a through the sub chamber injection port 3a. When fuel is injected from the fuel injection valve 5a into the auxiliary combustion chamber 2a, the fuel and air are mixed and ignited and burned. Sub combustion chamber 2a
Mixing of unburned fuel and fuel ejected from the main combustion chamber 1a with air is caused by gas ejection from the auxiliary combustion chamber 2a.

【0004】[0004]

【発明が解決しようとする課題】副室式機関の燃費、N
X を改善するためには副燃焼室内の燃料と空気の混合
気形成燃焼制御が重要である。副燃焼室下部22aの直
径を大きくすると副燃焼室2a内のガス流速が抑制さ
れ、燃料と空気との混合および燃焼がゆるやかに行われ
低NOX 化に有利である。しかし圧縮行程時主燃焼室内
のガスが副室噴口から副燃焼室下部22aに流入する際
ガスが急膨張するため、ガス流動損失が大きくなりガス
流速は低下し、副燃焼室内の燃料と空気の混合および燃
焼が不十分となる。
Fuel consumption of a subchamber engine, N
To improve the O X is mixture formation combustion control of the auxiliary combustion chamber fuel and air are important. When the diameter of the auxiliary combustion chamber bottom 22a to increase the gas flow velocity of the auxiliary combustion chamber 2a is suppressed, mixing and combustion of fuel and air takes place slowly is advantageous in low NO X reduction. However, when the gas in the main combustion chamber during the compression stroke flows into the lower portion 22a of the auxiliary combustion chamber from the outlet of the auxiliary chamber, the gas expands rapidly, resulting in a large gas flow loss and a decrease in the gas flow velocity, and the fuel and air in the auxiliary combustion chamber are reduced. Inadequate mixing and combustion.

【0005】また膨張行程時副燃焼室内の既燃、未燃ガ
スは副燃焼室下部22aから副室噴口3aに流れる際、
急縮小となるため流出し難くなり燃費が悪化する。逆に
副燃焼室下部22aの直径を小さくすると、副燃焼室内
の燃料と空気との混合及び燃焼が活発化しNOX が増大
する。また副燃焼室内のガスは小さい副燃焼室下部を通
り難く副室噴口から流出し難くなり燃費が悪化する。
When the burnt and unburned gases in the auxiliary combustion chamber during the expansion stroke flow from the lower portion 22a of the auxiliary combustion chamber to the auxiliary chamber injection port 3a,
Since it shrinks abruptly, it will be difficult for it to flow out and fuel consumption will deteriorate. Reducing the diameter of the auxiliary combustion chamber bottom 22a Conversely, mixing and combustion of the auxiliary combustion chamber fuel and air are activated NO X increases. Further, the gas in the sub-combustion chamber does not easily pass through the lower part of the sub-combustion chamber and is difficult to flow out from the sub-combustion nozzle, and the fuel efficiency deteriorates.

【0006】本発明の目的は、副室式内燃機関の燃費、
NOX 低減のために副燃焼室内の燃料と空気との混合気
形成燃焼を改善すると共に、ガス流動損失の低減、主燃
焼室へのガス流出を促進できる燃焼室を提供するにあ
る。
An object of the present invention is to improve the fuel economy of a sub-chamber internal combustion engine,
(EN) A combustion chamber capable of improving mixture-forming combustion of fuel and air in the auxiliary combustion chamber to reduce NO X, reducing gas flow loss, and promoting gas outflow to the main combustion chamber.

【0007】[0007]

【課題を解決するための手段】本発明は副燃焼室が複数
個の副室噴口を介して主燃焼室と連通している副室式内
燃機関において、副燃焼室下部の側壁を副燃焼室上部方
向に拡大傾斜させて成ることを特徴としている。
According to the present invention, in a sub-chamber internal combustion engine in which the sub-combustion chamber communicates with the main combustion chamber through a plurality of sub-chamber injection holes, the side wall of the lower portion of the sub-combustion chamber is the sub-combustion chamber. It is characterized by being enlarged and inclined in the upper direction.

【0008】[0008]

【作用】本発明は前記のとおり構成されているので、機
関の圧縮行程時主燃焼室内のガスが副室噴口から副燃焼
室下部へ流入する際前記副燃焼室下部の副室噴口開口端
が縮小されているのでガスの急膨張を防止できガス流動
損失を小さくできる。また前記副燃焼室下部の側壁は副
燃焼室上部方向に拡大傾斜しているのでガス流速は抑制
され副燃焼室内燃料と空気との混合、燃焼が抑制されN
X の増大を防止できる。
Since the present invention is constructed as described above, when the gas in the main combustion chamber during the compression stroke of the engine flows from the sub chamber injection port to the sub combustion chamber lower part, the sub chamber injection port opening end of the sub combustion chamber lower part is Since the size is reduced, rapid expansion of gas can be prevented and gas flow loss can be reduced. Further, since the side wall of the lower portion of the auxiliary combustion chamber is enlarged and inclined toward the upper portion of the auxiliary combustion chamber, the gas flow velocity is suppressed and the mixing and combustion of the fuel and air in the auxiliary combustion chamber are suppressed.
An increase in the O X can be prevented.

【0009】また副燃焼室下部の上端部は拡大している
と共に下端部は縮小しているので副燃焼室内の未燃既燃
ガスは主燃焼室内へ流出しやすくなるとともにこの際ガ
ス流動損失も小さくなる。
Further, since the upper end of the lower part of the auxiliary combustion chamber is expanded and the lower end thereof is contracted, unburned burnt gas in the auxiliary combustion chamber is likely to flow into the main combustion chamber and at the same time, gas flow loss is also caused. Get smaller.

【0010】[0010]

【実施例】本発明に係る第1実施例を図1によって説明
する。図1は本発明に係る第1実施例の燃焼室の断面図
である。副燃焼室2はシリンダヘッド4内に設置されて
いる。副燃焼室の形状には円柱形、球形、円錐台形等を
基本にした各種形状のものがあるが副燃焼室2は円柱形
を基本にしたものの一例である。副燃焼室2には燃料噴
射弁5が設置され、さらに機関始動時に副燃焼室2内を
予熱するグロープラグが必要に応じ設置されるが該グロ
ープラグは図示していない。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A first embodiment according to the present invention will be described with reference to FIG. FIG. 1 is a sectional view of a combustion chamber of a first embodiment according to the present invention. The sub combustion chamber 2 is installed in the cylinder head 4. The auxiliary combustion chamber 2 has various shapes based on a cylindrical shape, a spherical shape, a truncated cone shape, and the like, but the auxiliary combustion chamber 2 is an example based on the cylindrical shape. A fuel injection valve 5 is installed in the sub-combustion chamber 2, and a glow plug for preheating the inside of the sub-combustion chamber 2 when the engine is started is also installed if necessary, but the glow plug is not shown.

【0011】副燃焼室2は複数個の副室噴口3を介して
ピストン6の頂面、シリンダ7、シリンダヘッド4の下
面で構成される主燃焼室1と連通されている。副燃焼室
下部22の側壁は副燃焼室上部21方向に拡大傾斜して
構成されている。
The sub-combustion chamber 2 is connected to the main combustion chamber 1 composed of the top surface of the piston 6, the cylinder 7 and the bottom surface of the cylinder head 4 through a plurality of sub-chamber injection holes 3. The side wall of the sub-combustion chamber lower part 22 is configured to be enlarged and inclined toward the sub-combustion chamber upper part 21.

【0012】前記第1実施例の作用を説明する。機関運
転時の圧縮行程でピストン6により主燃焼室1内のガス
が圧縮され、副室噴口3から副燃焼室下部22へ流入す
る際副燃焼室下部22の副室噴口開口端が縮小されてい
るので、ガスの急膨張を防止できガス流動損失を小さく
できる。また副燃焼室下部22の側壁は副燃焼室上部2
1方向に拡大傾斜しているので、ガス流速は抑制され副
燃焼室2内の燃料と空気の混合燃焼が抑制されNOX
大を防止できる。
The operation of the first embodiment will be described. When the gas in the main combustion chamber 1 is compressed by the piston 6 in the compression stroke during engine operation and flows into the sub combustion chamber lower part 22 from the sub chamber injection port 3, the opening end of the sub chamber injection port of the sub combustion chamber lower part 22 is reduced. Therefore, the rapid expansion of the gas can be prevented and the gas flow loss can be reduced. The side wall of the sub combustion chamber lower part 22 is the upper side of the sub combustion chamber 2
Since expanding inclined in one direction, the gas flow rate can prevent mixing combustion is inhibited NO X increasing of fuel and air in the auxiliary combustion chamber 2 is suppressed.

【0013】膨張行程時、副燃焼室2内の未燃既燃ガス
は副燃焼室下部22の上端部が拡大しているとともに副
燃焼室下部22の下端部(副室噴口開口端近傍)は縮小
しているので主燃焼室1内へ流出しやすくなるととも
に、この際のガス流動損失も小さくなる。従って主燃焼
室1内の未燃燃料と空気との混合気形成燃焼を促進でき
る。
During the expansion stroke, the unburned burned gas in the sub-combustion chamber 2 expands at the upper end of the sub-combustion chamber lower part 22 and at the lower end of the sub-combustion chamber lower part 22 (near the opening end of the sub-combustion nozzle). Since the size is reduced, it easily flows into the main combustion chamber 1, and the gas flow loss at this time is also reduced. Therefore, the mixture forming combustion of the unburned fuel and the air in the main combustion chamber 1 can be promoted.

【0014】[0014]

【発明の効果】本発明は副燃焼室内の燃料と空気との混
合気形成燃焼を改善できると共に、副燃焼室下部でのガ
ス流動損失低減主燃焼室内へのガス流出促進、従って未
燃燃料と空気との混合気形成燃焼を促進できる。前記に
より本発明は燃費、NOX 、吐煙を改善できる。
The present invention can improve the mixture forming combustion of the fuel and air in the sub-combustion chamber, reduce the gas flow loss in the lower part of the sub-combustion chamber, promote the outflow of gas into the main combustion chamber, and thus the unburned fuel. It is possible to promote the mixture forming combustion with air. The present invention by can improve fuel economy, NO X, the吐煙.

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

【図1】本発明に係る第1実施例の燃焼室の断面図。FIG. 1 is a sectional view of a combustion chamber of a first embodiment according to the present invention.

【図2】従来の副室式内燃機関の燃焼室の断面図。FIG. 2 is a cross-sectional view of a combustion chamber of a conventional sub-chamber internal combustion engine.

【符号の説明】[Explanation of symbols]

1…主燃焼室、2…副燃焼室、21…副燃焼室上部、2
2…副燃焼室下部、3…副室噴口、4…シリンダヘッ
ド、6…ピストン、7…シリンダ。
1 ... Main combustion chamber, 2 ... Sub combustion chamber, 21 ... Upper part of sub combustion chamber, 2
2 ... Lower part of auxiliary combustion chamber, 3 ... Injection port of auxiliary chamber, 4 ... Cylinder head, 6 ... Piston, 7 ... Cylinder.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 副燃焼室が複数個の副室噴口を介して主
燃焼室と連通している副室式内燃機関において、副燃焼
室下部(22)の側壁を副燃焼室上部(21)方向に拡
大傾斜させて成ることを特徴とする副室式内燃機関の燃
焼室。
1. In a sub-chamber internal combustion engine in which the sub-combustion chamber communicates with the main combustion chamber through a plurality of sub-chamber nozzles, the side wall of the sub-combustion chamber lower part (22) is connected to the sub-combustion chamber upper part (21). A combustion chamber of a sub-chamber type internal combustion engine, characterized in that it is enlarged and inclined in a direction.
JP6192865A 1994-07-25 1994-07-25 Combustion chamber of auxiliary chamber-type internal combustion engine Withdrawn JPH0835427A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6192865A JPH0835427A (en) 1994-07-25 1994-07-25 Combustion chamber of auxiliary chamber-type internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6192865A JPH0835427A (en) 1994-07-25 1994-07-25 Combustion chamber of auxiliary chamber-type internal combustion engine

Publications (1)

Publication Number Publication Date
JPH0835427A true JPH0835427A (en) 1996-02-06

Family

ID=16298264

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6192865A Withdrawn JPH0835427A (en) 1994-07-25 1994-07-25 Combustion chamber of auxiliary chamber-type internal combustion engine

Country Status (1)

Country Link
JP (1) JPH0835427A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2019120170A (en) * 2017-12-28 2019-07-22 本田技研工業株式会社 Internal combustion engine
US10837355B2 (en) 2017-12-28 2020-11-17 Honda Motor Co., Ltd. Internal combustion engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2019120170A (en) * 2017-12-28 2019-07-22 本田技研工業株式会社 Internal combustion engine
US10837355B2 (en) 2017-12-28 2020-11-17 Honda Motor Co., Ltd. Internal combustion engine

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Effective date: 20011002