JP2002371851A - Indirect diesel engine - Google Patents

Indirect diesel engine

Info

Publication number
JP2002371851A
JP2002371851A JP2001179735A JP2001179735A JP2002371851A JP 2002371851 A JP2002371851 A JP 2002371851A JP 2001179735 A JP2001179735 A JP 2001179735A JP 2001179735 A JP2001179735 A JP 2001179735A JP 2002371851 A JP2002371851 A JP 2002371851A
Authority
JP
Japan
Prior art keywords
chamber
sub
auxiliary chamber
piston
fuel
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
Application number
JP2001179735A
Other languages
Japanese (ja)
Inventor
Yoji Sasaki
洋士 佐々木
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.)
Isuzu Motors Ltd
Original Assignee
Isuzu Motors 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 Isuzu Motors Ltd filed Critical Isuzu Motors Ltd
Priority to JP2001179735A priority Critical patent/JP2002371851A/en
Publication of JP2002371851A publication Critical patent/JP2002371851A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0675Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space being substantially spherical, hemispherical, ellipsoid or parabolic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0636Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space having a substantially flat and horizontal bottom
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14Direct injection into combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0627Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion having additional bores or grooves machined into the piston for guiding air or charge flow to the piston bowl
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0633Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space being almost completely enclosed in the piston, i.e. having a small inlet in comparison to its volume
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/0669Details related to the fuel injector or the fuel spray having multiple fuel spray jets per injector nozzle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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

Abstract

PROBLEM TO BE SOLVED: To reduce toxic exhaust substance such as smoke and increase high thermal efficiency. SOLUTION: This indirect diesel engine is constituted in such a way that an auxiliary chamber 6 is provided inside a piston 5, a hole 8 in which a fuel injection nozzle 4 mounted on a cylinder head 3 in the vicinity of top dead center is inserted is provided in a top plate 6a in the auxiliary chamber, and a plurality of communication ports 10 communicating the auxiliary chamber 6 with a main combustion chamber 9 facing a top part of the piston are radially arranged around the auxiliary chamber. The communication port 10 is provided in a shoulder part 6b of the auxiliary chamber, its direction is offset close to a side wall from a central line 0 of the auxiliary chamber, and it is obliquely and downward inclined toward a bottom face 12 of the auxiliary chamber crossing the central line 0 of the auxiliary chamber. Moreover, a part around a lower part 16 of the auxiliary chamber is formed into a circular arc smooth shape which is large as much as possible from the bottom face 12 of the auxiliary chamber to the side wall 17. Furthermore, fuel (b) is injected between adjacent communication ports or toward below each communication port from the fuel injection nozzle 4.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】この発明は、ピストンに副室
を有する副室式ディーゼルエンジンに関する。
The present invention relates to a sub-chamber diesel engine having a sub-chamber in a piston.

【0002】[0002]

【従来の技術】従来、ピストンの内部に空洞状の副室を
設けると共に、副室の天板にピストンの上死点付近でシ
リンダヘッドに装着した燃料噴射ノズルが入り込む穴を
設け、更に、副室の周囲に副室とピストン頂部に面する
主燃焼室とを連通する連絡口を放射状に複数配置させた
副室式ディーゼルエンジンが知られている。
2. Description of the Related Art Conventionally, a hollow sub-chamber is provided inside a piston, and a hole is formed in a top plate of the sub-chamber near the top dead center of the piston, through which a fuel injection nozzle mounted on a cylinder head enters. 2. Description of the Related Art A sub-chamber diesel engine is known in which a plurality of communication ports are radially arranged around a chamber to communicate a sub-chamber and a main combustion chamber facing the top of a piston.

【0003】[0003]

【発明が解決しようとする課題】ところが、従来の副室
式ディーゼルエンジンは、ピストンの頂部に対する連絡
口の傾斜角度が比較的小さいために、圧縮行程中に主燃
焼室から副室に流入する空気流によって生成されるスワ
ールが副室の下部に達するまでに不揃いになる欠点があ
る。
However, in the conventional subchamber diesel engine, the air flowing from the main combustion chamber into the subchamber during the compression stroke is relatively small because the angle of inclination of the communication port with respect to the top of the piston is relatively small. The drawback is that the swirl created by the flow is uneven before reaching the lower part of the subchamber.

【0004】このため、空気流には、部分的に弱い領域
が生じ、その部分に達した燃料と空気との混合が悪化し
てスモークの生成、あるいは燃焼ガスの主燃焼室への流
出に遅れを生じ易いという問題があった。
For this reason, the air flow partially has a weak region, and the mixing of the fuel and the air that has reached that portion deteriorates, delaying the generation of smoke or the outflow of the combustion gas into the main combustion chamber. There is a problem that is easily generated.

【0005】また、空気流の縦方向の流れが弱いため
に、副室の底面に達した燃料、あるいは燃焼ガスが副室
の底面に滞留し、スモークの生成、あるいは燃焼ガスの
主燃焼室への流出遅れに起因する性能悪化を招くことが
あった。特に、燃料噴霧が副室の側壁部に多量に衝突す
る燃料噴射方向の場合には、衝突後、噴射燃料が側壁に
沿って副室の底部に達し、上記の影響が多く出る傾向に
あった。
[0005] Further, because the vertical flow of the air flow is weak, the fuel or the combustion gas that has reached the bottom of the sub-chamber stays at the bottom of the sub-chamber to generate smoke or to move the combustion gas to the main combustion chamber. In some cases, the performance was deteriorated due to the outflow delay. In particular, in the case of the fuel injection direction in which a large amount of fuel spray collides with the side wall of the sub-chamber, after the collision, the injected fuel tends to reach the bottom of the sub-chamber along the side wall, and the above-mentioned effects tend to appear more. .

【0006】この発明は、係る問題に鑑みてなされたも
のであり、その目的とするところは、ピストンに副室を
有する副室式ディーゼルエンジンにおいて、スモークな
どの有害排出物が少なく、且つ、高熱効率の副室式ディ
ーゼルエンジンを提供することにある。
The present invention has been made in view of the above-mentioned problems, and an object of the present invention is to provide a sub-chamber diesel engine having a sub-chamber in a piston, which has less harmful emissions such as smoke and high heat. An object of the present invention is to provide an efficient sub-chamber diesel engine.

【0007】[0007]

【課題を解決するための手段】上記課題を解決するた
め、この発明は、次のように構成されている。
Means for Solving the Problems To solve the above problems, the present invention is configured as follows.

【0008】すなわち、 (1) ピストンの内部に空洞状の副室を設けると共
に、副室の天板にピストンの上死点付近でシリンダヘッ
ドに装着した燃料噴射ノズルが入り込む穴を設け、更
に、副室の周囲に副室とピストン頂部に面する主燃焼室
とを連通する連絡口を放射状に複数配置させた副室式デ
ィーゼルエンジンにおいて、前記連絡口を、副室の肩部
に設けると共に、その向きを副室の中心線から側壁寄り
にオフセットさせ、更に、副室の中心線を越えた副室の
底面に向けて斜め下向きに傾斜させ、更に、副室の下部
周辺を副室の底面から側壁にかけて可及的に大きな円弧
状の滑らかな形状に形成し、且つ、隣接する連絡口間又
は各連絡口の下方に向けて燃料噴射ノズルから燃料を噴
射することを特徴とする副室式ディーゼルエンジンであ
る。
That is, (1) a hollow sub-chamber is provided inside the piston, and a hole is formed in the top plate of the sub-chamber near the top dead center of the piston, into which the fuel injection nozzle mounted on the cylinder head enters. In a sub-chamber diesel engine in which a plurality of communication ports communicating the sub-chamber and the main combustion chamber facing the top of the piston are arranged radially around the sub-chamber, the communication ports are provided on shoulders of the sub-chamber. The direction is offset toward the side wall from the center line of the sub-chamber, and further tilted obliquely downward toward the bottom surface of the sub-chamber beyond the center line of the sub-chamber. A sub-chamber type characterized in that it is formed in an arc-shaped smooth shape as large as possible from the front to the side wall, and that fuel is injected from a fuel injection nozzle between adjacent communication ports or downward of each communication port. With a diesel engine That.

【0009】(2) 副室の底面を、円錐状に突出させ
ることを特徴とする(1)記載の副室式ディーゼルエン
ジンである。
(2) The sub-chamber diesel engine according to (1), wherein a bottom surface of the sub-chamber is projected in a conical shape.

【0010】[0010]

【発明の実施の形態】以下、この発明の実施の形態を図
面を用いて説明する。
Embodiments of the present invention will be described below with reference to the drawings.

【0011】図1は、この発明に係る副室式ディーゼル
エンジンの縦断面図、図2は、図1のA−A′断面図で
ある。
FIG. 1 is a longitudinal sectional view of a sub-chamber type diesel engine according to the present invention, and FIG. 2 is a sectional view taken along line AA 'of FIG.

【0012】図1に示すように、この副室式ディーゼル
エンジンは、シリンダ1を備えたシリンダブロック2
と、シリンダブロック2に固定したシリンダヘッド3
と、シリンダヘッド3に装着させた燃料噴射ノズル4及
びシリンダ1内を往復運動するピストン5から構成され
ている。
As shown in FIG. 1, this sub-chamber diesel engine has a cylinder block 2 having a cylinder 1.
And a cylinder head 3 fixed to the cylinder block 2
A fuel injection nozzle 4 mounted on the cylinder head 3 and a piston 5 reciprocating in the cylinder 1.

【0013】副室式ディーゼルエンジンは、更に、ピス
トン5の内部に空洞状の副室6を有すると共に、副室6
の天板6aにピストン5の上死点付近でシリンダヘッド
3に装着した燃料噴射ノズル4が入り込む穴8を有し、
更に、副室6の周囲に副室6とピストン頂部7に面する
主燃焼室9とを連通する連絡口10を放射状に複数有し
ている。
The sub-chamber diesel engine further has a hollow sub-chamber 6 inside the piston 5 and a sub-chamber 6.
Near the top dead center of the piston 5 has a hole 8 into which the fuel injection nozzle 4 attached to the cylinder head 3 enters,
Further, a plurality of communication ports 10 are provided radially around the sub-chamber 6 to communicate the sub-chamber 6 with the main combustion chamber 9 facing the piston top 7.

【0014】ところで、この発明では、図1に示すよう
に、連絡口10を、副室6の上部周辺、即ち、肩部6b
に設けると共に、圧縮工程中に主燃焼室9から副室6に
流入する空気aが、副室6の中心線Oで互いに衝突しな
いように連絡口10の向きを副室6の中心軸Oから横側
にオフセットさせている(図2参照)。即ち、図2に示
すように、連絡口10を、副室6の半径方向の直線11
から真横にLだけ平行移動させている。しかし、この例
に限るものではない。要は、圧縮工程中に主燃焼室9か
ら副室6に流入する空気aが、副室6の中心軸Oで互い
に衝突しないようにすればよい。
According to the present invention, as shown in FIG. 1, the communication port 10 is formed around the upper part of the sub-chamber 6, ie, the shoulder 6b.
And the direction of the communication port 10 from the center axis O of the sub-chamber 6 so that the air a flowing from the main combustion chamber 9 to the sub-chamber 6 during the compression process does not collide with each other at the center line O of the sub-chamber 6. It is offset laterally (see FIG. 2). That is, as shown in FIG.
Is translated by L just beside L. However, it is not limited to this example. The point is that air a flowing from the main combustion chamber 9 into the sub-chamber 6 during the compression process should not collide with each other at the central axis O of the sub-chamber 6.

【0015】更に、連絡口10は、図1に示すように、
副室6のほぼ水平な底面12に向けて斜め下向きに傾斜
されている。例えば、連絡口10aは、その中心線13
と副室の底面12との交点14が、連絡口の中心線13
と直交する副室の半径方向の直線11a(図2参照)を
越える側に位置するように傾斜されている。その傾斜角
度θは、連絡口10から副室6内に流入した空気aの流
速が副室の底面12との衝突により大幅に減衰しないよ
うに、水平面15、即ち副室の底面12に対して概ね4
5度以下に設定される。
Further, as shown in FIG.
The sub chamber 6 is inclined obliquely downward toward a substantially horizontal bottom surface 12. For example, the communication port 10a has its center line 13
The intersection 14 between the sub-chamber and the bottom surface 12 of the sub-chamber
The sub chamber is inclined so as to be located on the side beyond the radial straight line 11a (see FIG. 2) of the sub-chamber which is orthogonal to. The inclination angle θ is set with respect to the horizontal surface 15, that is, the bottom surface 12 of the sub-chamber so that the flow velocity of the air a flowing into the sub-chamber 6 from the communication port 10 is not greatly attenuated by the collision with the bottom surface 12 of the sub-chamber. About 4
Set to 5 degrees or less.

【0016】なお、副室6の高さが高い場合には、図3
に示すように、副室6の底面12′を円錐状に突出さ
せ、円錐状の底面12′に対する連絡口10の傾斜角度
θが設定範囲内に納まるようにしている。図中、αは、
円錐状底面12′の開脚角度を示している。
When the height of the sub-chamber 6 is high, FIG.
As shown in FIG. 5, the bottom surface 12 'of the sub chamber 6 is made to protrude in a conical shape so that the inclination angle θ of the communication port 10 with respect to the conical bottom surface 12' falls within a set range. In the figure, α is
It shows the leg opening angle of the conical bottom surface 12 '.

【0017】また、図1に戻って説明すると、副室6の
下部周辺16は、副室の底面12から副室の側壁17に
かけて可及的に大きな円弧状の滑らかな形状に形成され
る。
Returning to FIG. 1, the lower periphery 16 of the sub-chamber 6 is formed as large as possible in the shape of a circular arc from the bottom surface 12 of the sub-chamber to the side wall 17 of the sub-chamber.

【0018】更に、燃料噴射ノズル4からは、隣接する
連絡口10の間に向けて燃料bが噴射されるようになっ
ている。しかし、所望により、各連絡口10の下方に向
けて燃料噴射ノズル4から燃料bを噴射させてもよい。
要は、燃料噴射ノズル4から噴射された燃料4が副室6
の側壁17に沿って下流できればよい。
Further, the fuel b is injected from the fuel injection nozzle 4 toward a space between the adjacent communication ports 10. However, if desired, the fuel b may be injected from the fuel injection nozzle 4 downwardly of each communication port 10.
In short, the fuel 4 injected from the fuel injection nozzle 4 is
Downstream along the side wall 17.

【0019】次に、この副室式ディーゼルエンジンの作
動状況について説明する。
Next, the operation of the sub-chamber diesel engine will be described.

【0020】図4(a)及び(b)に示すように、圧縮
行程中に主燃焼室9から副室6に流入する空気aは、連
絡口10が副室6の中心軸Oからオフセットされている
ために、隣り合う連絡口10から流入する空気aと干渉
することなく、副室6の底面12に達する。
As shown in FIGS. 4A and 4B, the air a flowing from the main combustion chamber 9 to the sub-chamber 6 during the compression stroke is such that the communication port 10 is offset from the central axis O of the sub-chamber 6. Therefore, the air reaches the bottom surface 12 of the sub-chamber 6 without interfering with the air a flowing from the adjacent communication port 10.

【0021】副室6の底面12に達した空気aは、連絡
口10の傾斜角度θが比較的小さいため、その流速を殆
ど減衰することなく、副室6の底面12から側壁17に
沿って流れ、副室6の側壁17では、図4(a)に示す
ように、上方に向かう縦方向の流れcが形成される。
The air a reaching the bottom surface 12 of the sub-chamber 6 flows along the side wall 17 from the bottom surface 12 of the sub-chamber 6 without substantially attenuating the flow velocity because the inclination angle θ of the communication port 10 is relatively small. On the side wall 17 of the sub-chamber 6, as shown in FIG. 4A, an upward vertical flow c is formed.

【0022】また、連絡口10は、既に説明したよう
に、副室6の中心軸Oからオフセットされているので、
図4(b)に示すように、スワールdも生成され、副室
6内に3次元的な揃った空気の流れが形成される。
Further, since the communication port 10 is offset from the central axis O of the sub chamber 6 as described above,
As shown in FIG. 4B, a swirl d is also generated, and a three-dimensional uniform air flow is formed in the sub-chamber 6.

【0023】一方、図4(a)に示すように、燃料噴射
ノズル4から隣り合う連絡口10の間の側壁17に向け
て燃料bが噴射されるので、副室6の側壁17に衝突し
た燃料b及び燃焼ガスは、矢印eのように、側壁17に
沿って副室6の下方に向かって流れる。
On the other hand, as shown in FIG. 4A, the fuel b is injected from the fuel injection nozzle 4 toward the side wall 17 between the adjacent communication ports 10, so that the fuel b collides with the side wall 17 of the sub chamber 6. The fuel b and the combustion gas flow along the side wall 17 toward the lower part of the sub-chamber 6 as shown by the arrow e.

【0024】既に説明したように、空気aは、副室6の
側壁17に沿って上方に向かう流れを形成しているの
で、副室6の側壁17に衝突した後の燃料b及び燃焼ガ
スと衝突し、副室6の下方に向かう燃料b及び燃焼ガス
の流れを阻止する。その結果、燃料b及び燃焼ガスは、
副室6の底面12に達せず、副室6の底部には、空気a
のみが存在する。
As described above, since the air a forms a flow flowing upward along the side wall 17 of the sub-chamber 6, the air a and the fuel b and the combustion gas after colliding with the side wall 17 of the sub-chamber 6 It collides and blocks the flow of the fuel b and the combustion gas toward the lower part of the sub-chamber 6. As a result, the fuel b and the combustion gas are
The air a does not reach the bottom surface 12 of the sub-chamber 6, and the air a
Only exists.

【0025】連絡口10は、副室6の肩部6bに設置さ
れているので、上方に向かう空気aと、下方の向かう燃
料b及び燃焼ガスとが副室6の上部で衝突した後、混合
燃焼しながら、直ちに主燃焼室4に矢印gのように噴出
し、主燃焼室9では、主燃焼室9の空気と2次混合し、
完全燃焼する。副室底部の空気aは、燃焼後期に穴8及
び連絡口10から主燃焼室9に噴出し、主燃焼室9での
2次燃焼を促進し、燃え切りの良い燃焼が実現される。
図4(a)中、fは、混合燃焼部を示している。
Since the communication port 10 is provided at the shoulder 6b of the sub-chamber 6, after the upward air a, the downward fuel b and the combustion gas collide with each other at the upper part of the sub-chamber 6, they are mixed. While burning, the fuel is immediately jetted into the main combustion chamber 4 as shown by an arrow g.
Completely burn. The air a at the bottom of the sub-chamber is blown out into the main combustion chamber 9 from the hole 8 and the communication port 10 at the latter stage of the combustion, and promotes the secondary combustion in the main combustion chamber 9, thereby realizing good combustion.
In FIG. 4A, f indicates a mixed combustion section.

【0026】上記のように、この発明は、燃料及び燃料
ガスが副室6の底面12まで達しないので、低スモーク
が実現できる。また、副室6では、燃料及び燃焼ガスが
副室6内に大きく拡散することなく、連絡口10付近で
過濃燃焼し、主燃焼室9で再燃焼するので、低NOx及
び低スモークが実現できる。
As described above, according to the present invention, since the fuel and the fuel gas do not reach the bottom surface 12 of the sub chamber 6, low smoke can be realized. Further, in the sub-chamber 6, the fuel and the combustion gas do not greatly diffuse into the sub-chamber 6 but richly burn near the communication port 10 and recombust in the main combustion chamber 9, so that low NOx and low smoke are realized. it can.

【0027】また、副室6から燃焼ガスが速やかに噴出
するので、急速燃焼し、高熱効率が計れる。また、3次
元的空気流動による混合促進により、低い空気過剰率で
の運転が可能となり、出力が向上する。
Further, since the combustion gas is quickly spouted from the sub-chamber 6, it burns rapidly and high heat efficiency can be obtained. Further, by promoting the mixing by the three-dimensional air flow, the operation at a low excess air ratio becomes possible, and the output is improved.

【0028】[0028]

【発明の効果】上記のように、この発明によれば、燃料
及び燃料ガスが副室の底面まで達しないので、低スモー
クが実現できる。また、副室では、燃料及び燃焼ガスが
副室内に大きく拡散することなく、連絡口付近で過濃燃
焼し、主燃焼室で再燃焼するので、低NOx及び低スモ
ークが実現できる。
As described above, according to the present invention, since the fuel and the fuel gas do not reach the bottom of the sub chamber, low smoke can be realized. Further, in the sub-chamber, fuel and combustion gas do not greatly diffuse into the sub-chamber, but perform rich combustion near the communication port and re-combust in the main combustion chamber, so that low NOx and low smoke can be realized.

【0029】また、副室から燃焼ガスが速やかに噴出す
るので、急速燃焼し、高熱効率が計れる。また、3次元
的空気流動による混合促進により、低い空気過剰率での
運転が可能となり、出力が向上する。
Further, since the combustion gas is quickly spouted from the sub-chamber, it burns rapidly and high heat efficiency can be obtained. Further, by promoting the mixing by the three-dimensional air flow, the operation at a low excess air ratio becomes possible, and the output is improved.

【0030】また、連絡口面積比を大きくしても(例、
1.5%→2.3%)、副室内の空気流動が揃ったもの
となるので、絞り損失が減少して出力が向上する。ま
た、過給圧を高くすることが困難な低速回転での低空気
過剰率運転が可能となり、低速トルクの向上が計れる。
Further, even if the area ratio of the communication port is increased (for example,
(1.5% to 2.3%), the air flow in the sub-chamber becomes uniform, so that the throttle loss is reduced and the output is improved. Further, low excess air ratio operation can be performed at low speed rotation where it is difficult to increase the supercharging pressure, and low speed torque can be improved.

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

【図1】この発明に係る副室式ディーゼルエンジンの縦
断面図である。
FIG. 1 is a longitudinal sectional view of a sub-chamber diesel engine according to the present invention.

【図2】図1のA−A′断面図である。FIG. 2 is a sectional view taken along the line AA 'of FIG.

【図3】副室の底面形状の他の例を示す縦断面である。FIG. 3 is a longitudinal section showing another example of the bottom shape of the sub chamber.

【図4】(a),(b)はこの発明に係る副室式ディー
ゼルエンジンの作動説明図である。
FIGS. 4 (a) and 4 (b) are explanatory diagrams of the operation of the sub-chamber diesel engine according to the present invention.

【符号の説明】[Explanation of symbols]

3 シリンダヘッド 4 燃料噴射ノズル 5 ピストン 6 副室 6a 副室の天板 6b 副室の肩部 7 ピストン頂部 8 穴 9 主燃焼室 10 連絡口 12 副室の底面 16 副室の下部周辺 17 副室の側壁 b 燃料 O 副室の中心線 Reference Signs List 3 cylinder head 4 fuel injection nozzle 5 piston 6 sub-chamber 6a sub-chamber top plate 6b sub-chamber shoulder 7 piston top 8 hole 9 main combustion chamber 10 communication port 12 sub-chamber bottom surface 16 sub-chamber lower periphery 17 sub-chamber Side wall of b Fuel O Center line of sub chamber

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 ピストンの内部に空洞状の副室を設ける
と共に、副室の天板にピストンの上死点付近でシリンダ
ヘッドに装着した燃料噴射ノズルが入り込む穴を設け、
更に、副室の周囲に副室とピストン頂部に面する主燃焼
室とを連通する連絡口を放射状に複数配置させた副室式
ディーゼルエンジンにおいて、前記連絡口を、副室の肩
部に設けると共に、その向きを副室の中心線から側壁寄
りにオフセットさせ、更に、副室の中心線を越えた副室
の底面に向けて斜め下向きに傾斜させ、更に、副室の下
部周辺を副室の底面から側壁にかけて可及的に大きな円
弧状の滑らかな形状に形成し、且つ、隣接する連絡口間
又は各連絡口の下方に向けて燃料噴射ノズルから燃料を
噴射することを特徴とする副室式ディーゼルエンジン。
1. A hollow sub-chamber is provided inside a piston, and a hole is formed in a top plate of the sub-chamber near a top dead center of the piston, into which a fuel injection nozzle mounted on a cylinder head enters.
Further, in a sub-chamber diesel engine in which a plurality of communication ports for communicating the sub-chamber and the main combustion chamber facing the top of the piston are arranged radially around the sub-chamber, the communication ports are provided on shoulders of the sub-chamber. At the same time, the direction is offset from the center line of the sub-chamber toward the side wall, and further inclined obliquely downward toward the bottom surface of the sub-chamber beyond the center line of the sub-chamber. Characterized in that the fuel injection nozzle is formed into a shape as large as possible from the bottom surface to the side wall and is as smooth as possible, and the fuel is injected from a fuel injection nozzle between adjacent communication ports or downward of each communication port. Room type diesel engine.
【請求項2】 副室の底面を、円錐状に突出させること
を特徴とする請求項1記載の副室式ディーゼルエンジ
ン。
2. The sub-chamber diesel engine according to claim 1, wherein a bottom surface of the sub-chamber protrudes in a conical shape.
JP2001179735A 2001-06-14 2001-06-14 Indirect diesel engine Pending JP2002371851A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2001179735A JP2002371851A (en) 2001-06-14 2001-06-14 Indirect diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2001179735A JP2002371851A (en) 2001-06-14 2001-06-14 Indirect diesel engine

Publications (1)

Publication Number Publication Date
JP2002371851A true JP2002371851A (en) 2002-12-26

Family

ID=19020261

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001179735A Pending JP2002371851A (en) 2001-06-14 2001-06-14 Indirect diesel engine

Country Status (1)

Country Link
JP (1) JP2002371851A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2918114A1 (en) * 2007-06-26 2009-01-02 Peugeot Citroen Automobiles Sa Internal combustion engine i.e. diesel engine, for motor vehicle, has cavity communicating with chamber through feed tube formed by throat of cavity for permitting removal of fuel by gas passing between chamber and cavity
WO2013030115A3 (en) * 2011-08-26 2015-11-26 Federal-Mogul Nürnberg GmbH Shape-optimized combustion chamber bowl of a piston

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2918114A1 (en) * 2007-06-26 2009-01-02 Peugeot Citroen Automobiles Sa Internal combustion engine i.e. diesel engine, for motor vehicle, has cavity communicating with chamber through feed tube formed by throat of cavity for permitting removal of fuel by gas passing between chamber and cavity
WO2013030115A3 (en) * 2011-08-26 2015-11-26 Federal-Mogul Nürnberg GmbH Shape-optimized combustion chamber bowl of a piston

Similar Documents

Publication Publication Date Title
JP3953430B2 (en) In-cylinder internal combustion engine
JP6508240B2 (en) Spark-ignition type internal combustion engine
JP2008513659A (en) Internal combustion engine
JP2002522704A (en) Piston with active guide head and combustion chamber associated therewith
US10774782B2 (en) Piston design for flow re-direction
JP6508238B2 (en) Spark-ignition type internal combustion engine
JP6515941B2 (en) Spark-ignition type internal combustion engine
JP2002371851A (en) Indirect diesel engine
JP6515942B2 (en) Spark-ignition type internal combustion engine
JP6508239B2 (en) Spark-ignition type internal combustion engine
JPH1082323A (en) Combustion chamber of diesel engine
JP2819054B2 (en) Secondary combustion chamber insulated engine
JP4075471B2 (en) In-cylinder direct injection internal combustion engine
JP6515943B2 (en) Spark-ignition type internal combustion engine
CN110446835B (en) Spark ignition type internal combustion engine
JP2526324Y2 (en) Torch ignition device for torch ignition type gas engine
KR920007246B1 (en) Combustion chamber in piesel engine
JPH0143467Y2 (en)
JP2005155395A (en) Cylinder direct injection type internal combustion engine
JPH06317156A (en) Auxiliary chamber type engine
JP2006063862A (en) Internal combustion engine
JPH06173687A (en) Combustion chamber having subchamber of internal combustion engine
JP2542738Y2 (en) Combustion chamber of subchamber internal combustion engine
JPS63179123A (en) Internal combustion engine
JP2008297990A (en) Method and structure for generating squish flow in internal combustion engine