[go: up one dir, main page]

JP2004019480A - In-cylinder direct injection internal combustion engine - Google Patents

In-cylinder direct injection internal combustion engine Download PDF

Info

Publication number
JP2004019480A
JP2004019480A JP2002172352A JP2002172352A JP2004019480A JP 2004019480 A JP2004019480 A JP 2004019480A JP 2002172352 A JP2002172352 A JP 2002172352A JP 2002172352 A JP2002172352 A JP 2002172352A JP 2004019480 A JP2004019480 A JP 2004019480A
Authority
JP
Japan
Prior art keywords
fuel
cavity
cylinder
fuel injection
combustion engine
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.)
Granted
Application number
JP2002172352A
Other languages
Japanese (ja)
Other versions
JP4096637B2 (en
Inventor
Akihiko Kakuho
角方 章彦
Koji Hiratani
平谷 康治
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co 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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP2002172352A priority Critical patent/JP4096637B2/en
Publication of JP2004019480A publication Critical patent/JP2004019480A/en
Application granted granted Critical
Publication of JP4096637B2 publication Critical patent/JP4096637B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

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)
  • Fuel-Injection Apparatus (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To enlarge a stratified charge combustion region by enlarging a control range in a fuel injection time when stratified air-fuel mixture of a cylinder direct injection type internal combustion engine is produced. <P>SOLUTION: In the cylinder direct injection type internal combustion engine, an ignition plug is disposed near a cylinder axis, and a cavity 11 having a bottom wall and a side wall is recessed in a substantially center of a crown surface of a piston 4. The tip of a fuel injection valve is disposed above the side wall of the cavity 11, and fuel is injected from the fuel injection valve toward the side wall of the cavity 11. Much fuel is advanced downward from the above part of the side wall of the cavity 11 along the cylinder axis, and collided with the side wall of the cavity always keeping the same positional relation even when a piston position (crank angle) at the collision is different. Thus, influence of the fuel injection time to the formation of the stratified air-fuel mixture is reduced, a settable range of the fuel injection time is extended, and stratified charge combustible operation region is enlarged. <P>COPYRIGHT: (C)2004,JPO

Description

【0001】
【発明の属する技術分野】
本発明は、燃焼室内に直接燃料噴射する筒内直噴式内燃機関に関する。
【0002】
【従来の技術】
従来の筒内直噴式内燃機関として、特開平11−82028号公報に示すものでは、燃焼室上部に設けた燃料噴射弁から中空円錐状の燃料を、ピストン冠面に設けたキャビティに向けて噴射する構成としている。キャビティは円筒状の周壁面と底壁面と円錐状隆起部からなり、上方より噴射された略中空円錐状の燃料噴霧はキャビティの周壁面に鋭角に衝突し、該周壁面に衝突した燃料が底壁面および円錐隆起部を経て、円錐状隆起部の上方に設けた点火プラグに向けて上昇することで、点火プラグ周辺に成層混合気を形成することを意図している。
【0003】
【発明が解決しようとする課題】
しかしながら、上記従来の筒内直噴式内燃機関においては、燃料噴霧が広がりながら進行すると共に、ピストン摺動方向と燃料進行方向ないしは燃料の広がり方向が大きく異なり、その結果、機関回転速度ならびに機関負荷に応じて燃料噴射時期が変わった場合に、ピストンに衝突する際の燃料噴霧の広がり程度や、ピストンヘの衝突位置などが大きく異なってくるため、必ずしも意図したような良好な成層混合気を形成できない。
【0004】
すなわち、ある限られた期間のみ燃料噴射が可能であるため、成層燃焼を行える運転領域が制限され、燃料消費率の向上、排気エミッション低減が十分に行えない。
【0005】
【課題を解決するための手段】
このため、本発明は、シリンダ軸線付近に点火プラグを配置し、ピストン冠面の略中央に底壁面と側壁面とを有するキャビティを凹設する一方、このキャビティ側壁面の上方に燃料噴射弁の先端部を配置し、この燃料噴射弁から前記キャビティ側壁面へ向けて燃料を噴射する構成とした。
【0006】
このようにすれば、燃料噴射弁から噴射された燃料の噴霧は、キャビティ側壁面の上方から下方へ向かいシリンダ軸線に沿って進行する燃料の割合が多くなり、この方向に進行する燃料は、衝突時のピストン位置(クランク角度)が異なっていても常に同じ位置関係を保ってキャビティ側壁面に衝突するので、成層混合気の形成に対する燃料噴射時期の影響が小さくなり、設定可能な燃料噴射時期の範囲を広げることができる。その結果、成層燃焼可能な運転領域が拡大して燃料消費率の向上、排気エミッション低減を十分に行うことができる。
【0007】
【発明の実施の形態】
図1及び図2に、本発明の第1実施形態の構成を示す。燃焼室1はシリンダヘッド2と、シリンダブロック3と、ピストン4によって画成され、吸気ポート5と排気ポート6と、それぞれ吸気弁7、排気弁8を介して連通している。燃焼室1上部には、前記吸気弁7、排気弁8とともに、燃料噴射弁9と点火プラグ10が配されており、点火プラグ10が燃焼室1の略中心に設置されている。ピストン4冠面には燃料噴霧を受け止めるためのキャビティ11が設けられている。該キャビティ11は図2に示すように、平面図において略円形をなし、側壁面から底壁面に向けて緩やかな勾配を有している。
【0008】
図3は、第1実施形態の燃料噴霧の形態を示す。前記キャビティ11側壁面の上方に燃料噴射弁9の先端すなわち噴孔9aが位置し、この燃料噴射弁9から前記キャビティ11側壁面11へ向けて噴射した燃料の噴霧円錐の中心軸線とシリンダ軸線とのなす角度βが噴霧円錐角αの略1/2となるように、燃料噴射弁9をシリンダヘッド2に取り付ける。
【0009】
また、前記燃料噴霧は、噴孔9a形状等により、前記中空円錐形からシリンダ中心側の半分を切り欠いた半円錐状に形成される。
ここで、燃料噴射は各サイクル中に燃料噴射弁を所定期間開弁することで行われ、燃料噴射量は一般的な燃料噴射弁では噴射率が一定であるため、燃料噴射期間を変えることで調整され、その場合、噴射開始時期または終了時期を変更することになる。機関回転速度が変わった場合は、要求負荷に基づいて所定期間の燃料噴射が行われるが、噴射期間が同一でも、噴射開始時期が固定の場合、回転速度が高い場合は、クランク角度換算では噴射終了時期が遅くなる。反対に、噴射終了時期が固定の場合は、噴射開始が相対的に早まることになる。また、機関負荷が変わる場合も、当然のことながら、噴射期間の変化に伴い、噴射終了時期または噴射開始時期が変動することになる。この結果、既述したように、従来の噴霧形態では、機関の負荷や回転速度の変化に応じて噴射終了時期または噴射開始時期が変動すると、ピストン冠面に燃料噴霧が衝突する際のピストン位置が大きく変化し、良好な成層混合気を安定して得ることが困難であった。
【0010】
これに対し、本実施形態では、前記キャビティ11側壁面の上方に燃料噴射弁9の先端を配置するとともに、この燃料噴射弁9から前記キャビティ11側壁面へ向けて燃料を噴射する構成としたため、燃料噴霧の多くがキャビティ11側壁面の上方から下方へ向かいシリンダ軸線に沿って進行し、衝突時のピストン位置(クランク角度)が異なっていても常に同じ位置関係を保ってキャビティ側壁面に衝突するので、成層混合気の形成に対する燃料噴射時期の影響が小さくなり、設定可能な燃料噴射時期の範囲を広げられ、成層燃焼可能な運転領域が拡大して燃料消費率の向上、排気エミッション低減が促進される。
【0011】
上記本実施形態の効果を、図4を用いてより詳細に説明する。図4は、成層燃焼を行うために圧縮行程噴射を行った場合の、筒内の燃料の運動を示す。燃料噴射弁9から噴射される燃料は、シリンダ軸線方向、すなわちピストン摺動方向に噴射されるため、燃料噴射時期によらずキャビティ11のおおむね同一位置で受け止められる。
【0012】
燃料噴射弁9の中心部とキャビティ11周壁のスロープ部11aとが、シリンダ軸線投影方向に同じ個所に配されているため、燃料噴霧はキャビティ11周壁の対向するスロープ部11aに衝突する。燃料噴霧は10Mpa以上の高圧で噴射されるため、該スロープ部11aに一旦衝突した後、その貫徹力で該スロープ部11aの勾配により方向を変え、キャビティ11底面を点火プラグ10下方に設けたシリンダ軸線を挟んで反対側のスロープ部に向けて進む。
【0013】
この際、高圧噴射により微粒化された燃料噴霧がスロープと鈍角をなして衝突するため、冠面上に厚い液膜を生じることがなく、キャビティ11底面を這うように移動する噴霧および液膜は順次気化・混合がなされる。しかる後に、点火プラグ10下方のキャビティ11周壁のスロープ部により燃料噴霧は燃焼室1上側へ跳ね上げられ、点火プラグ10付近に良好な混合気を形成する。上記ような混合気運動は、ピストン4摺動方向に燃料噴霧が噴射されるため、機関負荷、回転速度によって、燃料噴射時期、燃料噴射期間が変わってもおおよそ同様となり、幅広い運転領域で良好な混合気を点火プラグ10周辺に形成することが可能となる。
【0014】
また本実施形態では、前記燃料噴射弁を、噴霧円錐の中心軸線とシリンダ軸線とのなす角度が噴霧円錐角の略1/2となるようシリンダヘッドに取り付け、かつ、中空円錐形からシリンダ中心側の一部分を切り欠いた半円錐状の噴霧を形成するように構成したため、以下のような効果が得られる。
すなわち、従来一般的なように燃料噴霧を切れ目のない中空円錐状とし、成層燃焼のために圧縮行程後半に燃料噴射を行った場合、円錐内部が圧縮行程後半の高い雰囲気圧力に対して低圧となるために、噴霧が内側に寄せられ、結果的に噴霧角が小さくなる。ところが、本実施形態のように、噴霧を半円錐状に広げることにより、噴霧内外に差圧を生じることがないため、噴霧角が筒内圧力つまりは噴射時期によって大きく変化することがない。したがって、キャビティ11の一部に集中して燃料が衝突することを防ぐことが可能となり、スモークや燃焼室デポジットの生成を抑制することができる。
【0015】
図5は、第2実施形態のキャビティ形状を示す。第2実施形態ではキャビティ11の側壁面から底壁面に向けて緩やかな傾斜を有しているが、燃料噴射弁9側に相当する方向から点火プラグ10側に相当するキャビティ11位置に向けて、扇状に開口部が狭くなるように設定されている。これにより、一旦受け止めた燃料をより集中させて点火プラグ10方向へ導くことが可能となる。
【0016】
図6は、第3実施形態の燃料噴霧形状の模式図を示す。ここでは燃料噴射弁9は多噴孔のホールノズルであり、噴霧の重心がシリンダ軸線方向と略一致するように、各噴孔の指向方向がおおむねシリンダ中心軸方向を向いており、燃料噴霧形状は各噴孔から噴射される燃料噴霧が半円形をなすよう配置されている。
このように、本実施形態では、前記燃料噴射弁9から噴射される燃料噴霧が、燃料噴射弁9中心軸に対して非対称であり、燃料噴霧の重心方向がシリンダ軸線方向と略平行である構成としたため、燃料噴射時期によらずキャビティ11で確実に燃料を受け止めることが可能となり、広い運転領域で良好な性状の混合気を点火プラグ10に配することにより成層燃焼が可能となる。
【0017】
図7は、第4実施形態の燃料噴霧形状の模式図を示す。第3実施形態と同様、燃料噴射弁9は多噴孔のホールノズルであり、燃料噴霧形状は各噴孔から噴射される燃料噴霧が半円形をなすよう配置される点も同様であるが、半円形の中心部分がシリンダ軸線と平行に指向するように配される。
本実施形態では、前記燃料噴射弁から噴射される燃料噴霧の最もシリンダ周壁に近い側の稜線が、シリンダ軸線と略平行であるように構成したことにより、ピストン摺動方向と異なる方向へ飛翔する燃料噴霧を少なくすることができ、第3実施形態と同様、広い運転領域で良好な混合気を点火プラグ10に配することが可能となる。
【0018】
図8は、第5実施形態のピストン形状を示す。本実施形態では、燃料噴射弁9下方のピストンキャビティ形状が平面図において略直線状をなしている。該第5実施形態における燃料噴霧は、概略を図9に示すように、平板状の燃料噴霧を噴孔がスリット状に開口した燃料噴射弁を用いて噴射する構成となっている。図8に示すピストン冠面に対して、図9に示す平板状の燃料噴霧がシリンダ軸線方向に噴射され、直線状のスロープで一旦噴霧を受け止めた後、燃料噴射時期、燃料噴射期間が変わっても、キャビティを経由して点火プラグ付近に良好な混合気を形成し、幅広い運転領域で良好な混合気を点火プラグ周辺に形成することが可能となる。
【0019】
本実施形態では、前記燃料噴射弁9から噴射される燃料噴霧が平板状であり、燃料噴霧の噴射方向がシリンダ軸線方向と略平行であるように構成したため、噴霧の進行方向のベクトルが揃うことになり、キャビティ11で受け止めやすい上に、一旦受け止められた燃料噴霧がキャビティ11内で進む方向を制御しやすくなり、より確実に成層混合気を形成できる。
【0020】
また、各実施形態に共通して、前記燃料噴射弁9から噴射された燃料噴霧の少なくとも半分が、前記キャビティ11のシリンダ軸線側の壁面に対して鈍角をなして衝突するよう設定されている構成としたため、衝突した燃料噴霧はキャビティ11で進行方向を変え、点火プラグ10方向に向かうため、キャビティ11内に厚い液膜を形成することない。一旦薄く付着した燃料液膜は速やかに気化・混合がなされるため、スモーク、燃焼室デポジットを生成することがなく、成層燃焼を行うことができる。
【0021】
同じく、各実施形態に共通して、前記キャビティ11が、側壁面から底壁面に向かって緩やかな勾配を有するように構成したため、ピストン4冠面のキャビティ11で受け止められた燃料が気化しながら、勾配を這い上がり、点火プラグ10方向へと舞い上がることにより、確実に点火プラグ10周辺に成層混合気を配置することが可能となる。
【図面の簡単な説明】
【図1】本発明の第1実施形態を示す縦断面図。
【図2】同上実施形態のピストンを示す平面図及び縦断面図。
【図3】同上実施形態の燃料噴霧の形態を示す図。
【図4】同上実施形態の筒内の燃料の運動を示す図。
【図5】第2同上実施形態のピストンを示す平面図及び縦断面図。
【図6】第3実施形態の燃料噴霧の形態を示す図。
【図7】第4実施形態の燃料噴霧の形態を示す図。
【図8】第5同上実施形態のピストンを示す平面図及び縦断面図。
【図9】第5実施例の燃料噴霧の形態を示す図。
【符号の説明】
1…燃焼室  4…ピストン  9…燃料噴射弁  9a…噴孔  10…点火プラグ  11…キャビティ
[0001]
TECHNICAL FIELD OF THE INVENTION
The present invention relates to an in-cylinder direct injection internal combustion engine that directly injects fuel into a combustion chamber.
[0002]
[Prior art]
As a conventional in-cylinder direct injection internal combustion engine disclosed in Japanese Patent Application Laid-Open No. H11-82028, a hollow conical fuel is injected from a fuel injection valve provided in an upper portion of a combustion chamber toward a cavity provided in a piston crown surface. Configuration. The cavity is composed of a cylindrical peripheral wall, a bottom wall, and a conical ridge, and the substantially hollow conical fuel spray injected from above collides with the peripheral wall of the cavity at an acute angle, and the fuel that has collided with the peripheral wall has a bottom. It is intended to form a stratified mixture around the spark plug by ascending via the wall surface and the conical ridge toward the spark plug provided above the conical ridge.
[0003]
[Problems to be solved by the invention]
However, in the above-described conventional in-cylinder direct injection type internal combustion engine, the fuel spray advances while spreading, and the piston sliding direction and the fuel advancing direction or the fuel spreading direction are greatly different. As a result, the engine rotation speed and the engine load are reduced. If the fuel injection timing changes accordingly, the degree of spread of the fuel spray when colliding with the piston, the position of collision with the piston, and the like greatly differ, so that a desired stratified mixture cannot always be formed as intended.
[0004]
That is, since fuel injection can be performed only for a certain limited period, the operation range in which stratified combustion can be performed is limited, and the fuel consumption rate cannot be improved and the exhaust emission cannot be sufficiently reduced.
[0005]
[Means for Solving the Problems]
Therefore, according to the present invention, an ignition plug is disposed near the cylinder axis and a cavity having a bottom wall surface and a side wall surface is formed substantially at the center of the piston crown surface, while a fuel injection valve is provided above the cavity side wall surface. A tip is disposed, and fuel is injected from the fuel injection valve toward the side wall surface of the cavity.
[0006]
In this way, the spray of the fuel injected from the fuel injection valve increases the proportion of the fuel traveling along the cylinder axis from above to below the cavity side wall surface, and the fuel traveling in this direction impinges. Even if the piston position (crank angle) at the time is different, it always collides with the cavity side wall surface while maintaining the same positional relationship, so that the influence of the fuel injection timing on the formation of the stratified mixture becomes small, and the settable fuel injection timing The range can be expanded. As a result, the operating region in which stratified combustion can be performed is expanded, so that the fuel consumption rate can be improved and the exhaust emission can be sufficiently reduced.
[0007]
BEST MODE FOR CARRYING OUT THE INVENTION
1 and 2 show the configuration of the first embodiment of the present invention. The combustion chamber 1 is defined by a cylinder head 2, a cylinder block 3, and a piston 4, and communicates with an intake port 5 and an exhaust port 6 via an intake valve 7 and an exhaust valve 8, respectively. A fuel injection valve 9 and a spark plug 10 are arranged in the upper part of the combustion chamber 1 together with the intake valve 7 and the exhaust valve 8, and the spark plug 10 is installed substantially at the center of the combustion chamber 1. A cavity 11 for receiving fuel spray is provided on the crown surface of the piston 4. As shown in FIG. 2, the cavity 11 has a substantially circular shape in a plan view, and has a gentle gradient from the side wall surface to the bottom wall surface.
[0008]
FIG. 3 shows a form of fuel spray of the first embodiment. The tip of the fuel injection valve 9, that is, the injection hole 9 a, is located above the side wall surface of the cavity 11, and the center axis and the cylinder axis of the spray cone of the fuel injected from the fuel injection valve 9 toward the side wall surface 11 of the cavity 11. The fuel injection valve 9 is attached to the cylinder head 2 so that the angle β is approximately の of the spray cone angle α.
[0009]
Further, the fuel spray is formed in a semi-conical shape in which a half on the cylinder center side is cut off from the hollow conical shape due to the shape of the injection hole 9a or the like.
Here, the fuel injection is performed by opening the fuel injection valve for a predetermined period during each cycle, and the fuel injection amount is changed by changing the fuel injection period because the injection rate of a general fuel injection valve is constant. It is adjusted, and in that case, the injection start timing or the end timing will be changed. When the engine rotation speed changes, fuel injection is performed for a predetermined period based on the required load.However, even if the injection period is the same, if the injection start timing is fixed, or if the rotation speed is high, the injection is calculated in terms of crank angle. The end time is delayed. Conversely, when the injection end timing is fixed, the injection start is relatively early. Also, when the engine load changes, the injection end timing or the injection start timing naturally changes with the change of the injection period. As a result, as described above, in the conventional spray mode, when the injection end timing or the injection start timing fluctuates according to the change in the load or the rotation speed of the engine, the piston position when the fuel spray collides with the piston crown surface. Greatly changed, and it was difficult to stably obtain a good stratified mixture.
[0010]
On the other hand, in the present embodiment, the tip of the fuel injection valve 9 is arranged above the side wall surface of the cavity 11 and the fuel is injected from the fuel injection valve 9 toward the side wall surface of the cavity 11. Most of the fuel spray proceeds along the cylinder axis from above to below the side wall surface of the cavity 11 and collides with the side wall surface of the cavity 11 while always maintaining the same positional relationship even when the piston position (crank angle) at the time of collision is different. Therefore, the influence of the fuel injection timing on the formation of the stratified mixture is reduced, the range of the fuel injection timing that can be set is expanded, the operation region where stratified combustion can be performed is expanded, and the fuel consumption rate is improved and the exhaust emission is reduced. Is done.
[0011]
The effect of the present embodiment will be described in more detail with reference to FIG. FIG. 4 shows the movement of fuel in the cylinder when the compression stroke injection is performed to perform stratified combustion. Since the fuel injected from the fuel injection valve 9 is injected in the cylinder axis direction, that is, in the sliding direction of the piston, the fuel is received at substantially the same position in the cavity 11 regardless of the fuel injection timing.
[0012]
Since the center portion of the fuel injection valve 9 and the slope portion 11a of the peripheral wall of the cavity 11 are arranged at the same position in the cylinder axis projection direction, the fuel spray collides with the slope portion 11a facing the peripheral wall of the cavity 11. Since the fuel spray is injected at a high pressure of 10 Mpa or more, after once colliding with the slope portion 11a, the direction of the fuel spray is changed by the slope of the slope portion 11a by the penetrating force, and the bottom of the cavity 11 is provided below the ignition plug 10 in the cylinder. Proceed toward the opposite slope section across the axis.
[0013]
At this time, since the fuel spray atomized by the high-pressure injection collides with the slope at an obtuse angle, a thick liquid film is not formed on the crown surface, and the spray and the liquid film moving along the bottom surface of the cavity 11 are Vaporization and mixing are performed sequentially. Thereafter, the fuel spray is jumped up to the upper side of the combustion chamber 1 by the slope portion of the peripheral wall of the cavity 11 below the ignition plug 10, and a good mixture is formed near the ignition plug 10. Since the fuel mixture is sprayed in the sliding direction of the piston 4 as described above, the fuel mixture is substantially the same even if the fuel injection timing and the fuel injection period are changed depending on the engine load and the rotational speed. An air-fuel mixture can be formed around the spark plug 10.
[0014]
Further, in the present embodiment, the fuel injection valve is attached to the cylinder head so that the angle formed by the central axis of the spray cone and the cylinder axis is approximately の of the spray cone angle, and the hollow cone is used to move the fuel injection valve from the cylinder center to the cylinder center. Is formed so as to form a semi-conical spray in which a part is cut out, the following effects can be obtained.
That is, as in the conventional general case, when the fuel spray is formed into a continuous hollow conical shape and fuel injection is performed in the latter half of the compression stroke for stratified combustion, the inside of the cone has a low pressure with respect to the high atmospheric pressure in the latter half of the compression stroke. As a result, the spray is moved inward, resulting in a smaller spray angle. However, as in the present embodiment, by spreading the spray in a semi-conical shape, no differential pressure is generated inside and outside the spray, so that the spray angle does not greatly change depending on the in-cylinder pressure, that is, the injection timing. Therefore, it is possible to prevent the fuel from colliding with a part of the cavity 11 and to suppress generation of smoke and combustion chamber deposit.
[0015]
FIG. 5 shows a cavity shape according to the second embodiment. In the second embodiment, the cavity 11 has a gentle inclination from the side wall surface to the bottom wall surface, but from the direction corresponding to the fuel injection valve 9 toward the position of the cavity 11 corresponding to the ignition plug 10, The opening is set to be narrow in a fan shape. As a result, the once received fuel can be more concentrated and guided toward the spark plug 10.
[0016]
FIG. 6 is a schematic diagram of a fuel spray shape according to the third embodiment. Here, the fuel injection valve 9 is a multi-injection hole nozzle, and the directing direction of each injection hole is substantially directed to the cylinder center axis direction so that the center of gravity of the spray substantially matches the cylinder axis direction. Are arranged so that the fuel spray injected from each injection hole forms a semicircle.
As described above, in the present embodiment, the fuel spray injected from the fuel injection valve 9 is asymmetric with respect to the center axis of the fuel injection valve 9, and the center of gravity of the fuel spray is substantially parallel to the cylinder axis direction. Therefore, the fuel can be reliably received in the cavity 11 irrespective of the fuel injection timing, and the stratified combustion can be performed by arranging the air-fuel mixture having good properties in the ignition plug 10 in a wide operating region.
[0017]
FIG. 7 is a schematic diagram of a fuel spray shape according to the fourth embodiment. As in the third embodiment, the fuel injection valve 9 is a multi-injection hole nozzle, and the fuel spray shape is the same in that the fuel spray injected from each of the injection holes is arranged to form a semicircle. The semicircular center portion is arranged so as to be directed parallel to the cylinder axis.
In this embodiment, the fuel spray injected from the fuel injection valve is configured so that the ridge line closest to the cylinder peripheral wall is substantially parallel to the cylinder axis, so that the fuel spray flies in a direction different from the piston sliding direction. The amount of fuel spray can be reduced, and a good air-fuel mixture can be distributed to the ignition plug 10 in a wide operating range as in the third embodiment.
[0018]
FIG. 8 shows a piston shape according to the fifth embodiment. In the present embodiment, the shape of the piston cavity below the fuel injection valve 9 is substantially straight in a plan view. As schematically shown in FIG. 9, the fuel spray in the fifth embodiment has a configuration in which a flat fuel spray is injected using a fuel injection valve having an injection hole opened in a slit shape. The flat fuel spray shown in FIG. 9 is injected in the cylinder axial direction with respect to the piston crown surface shown in FIG. 8, and once the spray is received by a linear slope, the fuel injection timing and the fuel injection period change. Also, a good air-fuel mixture is formed near the ignition plug via the cavity, and a good air-fuel mixture can be formed around the ignition plug in a wide operating range.
[0019]
In the present embodiment, the fuel spray injected from the fuel injection valve 9 has a flat plate shape, and the injection direction of the fuel spray is configured to be substantially parallel to the cylinder axis direction. In addition to the fact that the fuel spray is easily received in the cavity 11, the direction in which the fuel spray once received advances in the cavity 11 can be easily controlled, and a stratified mixture can be formed more reliably.
[0020]
In addition, a configuration in which at least half of the fuel spray injected from the fuel injection valve 9 collides with the wall surface of the cavity 11 on the cylinder axis side at an obtuse angle is common to each embodiment. Therefore, the colliding fuel spray changes its traveling direction in the cavity 11 and moves toward the spark plug 10, so that a thick liquid film is not formed in the cavity 11. Once thinly deposited, the fuel liquid film is quickly vaporized and mixed, so that stratified combustion can be performed without generating smoke and combustion chamber deposits.
[0021]
Similarly, since the cavity 11 is configured so as to have a gentle gradient from the side wall surface to the bottom wall surface in common to each embodiment, while the fuel received by the cavity 11 on the piston 4 crown surface is vaporized, By climbing up the gradient and soaring toward the spark plug 10, it is possible to reliably arrange the stratified mixture around the spark plug 10.
[Brief description of the drawings]
FIG. 1 is a longitudinal sectional view showing a first embodiment of the present invention.
FIG. 2 is a plan view and a longitudinal sectional view showing the piston of the embodiment.
FIG. 3 is a view showing a form of fuel spray according to the embodiment.
FIG. 4 is a view showing movement of fuel in a cylinder according to the embodiment.
FIG. 5 is a plan view and a longitudinal sectional view showing a piston according to the second embodiment.
FIG. 6 is a diagram showing a form of fuel spray according to a third embodiment.
FIG. 7 is a view showing a form of fuel spray according to a fourth embodiment.
FIG. 8 is a plan view and a longitudinal sectional view showing a piston according to the fifth embodiment.
FIG. 9 is a view showing a form of fuel spray according to a fifth embodiment.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 ... Combustion chamber 4 ... Piston 9 ... Fuel injection valve 9a ... Injection hole 10 ... Spark plug 11 ... Cavity

Claims (9)

シリンダ軸線付近に点火プラグを配置し、ピストン冠面の略中央に底壁面と側壁面とを有するキャビティを凹設した筒内直噴式内燃機関であって、
前記キャビティ側壁面の上方に燃料噴射弁の先端部を配置するとともに、この燃料噴射弁から前記キャビティ側壁面へ向けて燃料を噴射することを特徴とする筒内直噴式内燃機関。
An in-cylinder direct injection internal combustion engine in which a spark plug is disposed near the cylinder axis and a cavity having a bottom wall surface and a side wall surface is provided substantially at the center of the piston crown surface,
An in-cylinder direct injection internal combustion engine, wherein a tip of a fuel injection valve is arranged above the cavity side wall surface, and fuel is injected from the fuel injection valve toward the cavity side wall surface.
前記燃料噴射弁を、該燃料噴射弁から噴射される燃料の噴霧円錐の中心軸線とシリンダ軸線とのなす角度が噴霧円錐角の略1/2となるようシリンダヘッドに取り付けたことを特徴とする請求項1に記載の筒内直噴式内燃機関。The fuel injection valve is attached to a cylinder head such that an angle formed between a central axis of a spray cone of fuel injected from the fuel injection valve and a cylinder axis is approximately の of a spray cone angle. An in-cylinder direct injection internal combustion engine according to claim 1. 前記燃料噴射弁は、中空円錐形からシリンダ中心側の一部分を切り欠いた半円錐状の噴霧を形成することを特徴とする請求項2に記載の筒内直噴式内燃機関。The in-cylinder direct injection internal combustion engine according to claim 2, wherein the fuel injection valve forms a semi-conical spray in which a part on the cylinder center side is cut away from the hollow conical shape. 前記燃料噴射弁から噴射される燃料噴霧が、燃料噴射弁中心軸に対して非対称であり、燃料噴霧の重心方向がシリンダ軸線方向と略平行であることを特徴とする請求項1に記載の筒内直噴式内燃機関。The cylinder according to claim 1, wherein the fuel spray injected from the fuel injection valve is asymmetric with respect to the center axis of the fuel injection valve, and the center of gravity of the fuel spray is substantially parallel to the cylinder axis direction. Internal direct injection type internal combustion engine. 前記燃料噴射弁から噴射される燃料噴霧の最もシリンダ周壁に近い側の稜線が、シリンダ軸線と略平行であることを特徴とする請求項1に記載の筒内直噴式内燃機関。2. The direct injection internal combustion engine according to claim 1, wherein a ridge line of the fuel spray injected from the fuel injection valve closest to the cylinder peripheral wall is substantially parallel to the cylinder axis. 3. 前記燃料噴射弁から噴射される燃料噴霧が平板状であり、燃料噴霧の噴射方向がシリンダ軸線方向と略平行であることを特徴とする請求項1に記載の筒内直噴式内燃機関。2. The direct injection type internal combustion engine according to claim 1, wherein the fuel spray injected from the fuel injection valve has a flat plate shape, and an injection direction of the fuel spray is substantially parallel to a cylinder axis direction. 前記燃料噴射弁から噴射された燃料噴霧の少なくとも半分が、前記キャビティのシリンダ中心側の壁面に対して鈍角をなして衝突するよう設定されていることを特徴とする請求項1〜請求項6のいずれか1つに記載の筒内直噴式内燃機関。7. The fuel injection valve according to claim 1, wherein at least half of the fuel spray injected from the fuel injection valve collides at an obtuse angle with the cylinder center side wall surface of the cavity. An in-cylinder direct injection internal combustion engine according to any one of the preceding claims. 前記キャビティは、側壁面から底壁面に向かって緩やかな勾配を有することを特徴とする請求項1〜請求項7のいずれか1つに記載の筒内直噴式内燃機関。The direct injection internal combustion engine according to any one of claims 1 to 7, wherein the cavity has a gentle gradient from a side wall surface to a bottom wall surface. 前記キャビティの点火プラグ下方位置に、キャビティ底壁面から上部に向かう緩やかな勾配を有することを特徴とする請求項1〜請求項8のいずれか1つに記載の筒内直噴式内燃機関。The direct injection type internal combustion engine according to any one of claims 1 to 8, wherein the cavity has a gentle gradient from a bottom wall surface toward an upper portion of the cavity below the spark plug.
JP2002172352A 2002-06-13 2002-06-13 In-cylinder direct injection internal combustion engine Expired - Fee Related JP4096637B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2002172352A JP4096637B2 (en) 2002-06-13 2002-06-13 In-cylinder direct injection internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2002172352A JP4096637B2 (en) 2002-06-13 2002-06-13 In-cylinder direct injection internal combustion engine

Publications (2)

Publication Number Publication Date
JP2004019480A true JP2004019480A (en) 2004-01-22
JP4096637B2 JP4096637B2 (en) 2008-06-04

Family

ID=31171945

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002172352A Expired - Fee Related JP4096637B2 (en) 2002-06-13 2002-06-13 In-cylinder direct injection internal combustion engine

Country Status (1)

Country Link
JP (1) JP4096637B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007061020A1 (en) * 2005-11-24 2007-05-31 Toyota Jidosha Kabushiki Kaisha Cylinder-injection spark-ignition internal combustion engine
JP2007231924A (en) * 2005-05-24 2007-09-13 Denso Corp Fuel injection valve for internal combustion engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007231924A (en) * 2005-05-24 2007-09-13 Denso Corp Fuel injection valve for internal combustion engine
WO2007061020A1 (en) * 2005-11-24 2007-05-31 Toyota Jidosha Kabushiki Kaisha Cylinder-injection spark-ignition internal combustion engine
US7597085B2 (en) 2005-11-24 2009-10-06 Toyota Jidosha Kabushiki Kaisha Direct fuel injection-type spark ignition internal combustion engine

Also Published As

Publication number Publication date
JP4096637B2 (en) 2008-06-04

Similar Documents

Publication Publication Date Title
JP4280928B2 (en) Direct injection spark ignition internal combustion engine
US6543408B1 (en) Internal combustion engine with direct fuel injection
RU116905U1 (en) Piston with shallow bowl and nozzle for gasoline engine with direct injection (OPTIONS)
GB2328976A (en) Forming a stratified charge in a direct-injection spark-ignition i.c. engine
JP2009513855A (en) Compression ignition internal combustion engine
JP3295975B2 (en) gasoline engine
US6386175B2 (en) Fuel injection
JP3997781B2 (en) In-cylinder direct injection engine
WO2000077359A1 (en) Cylinder injection engine and method of combusting the engine
CN107407223B (en) Fuel injection control device for direct injection engine
JPH07102976A (en) In-cylinder injection spark ignition engine
JP3633392B2 (en) In-cylinder injection spark ignition internal combustion engine
JP2004019480A (en) In-cylinder direct injection internal combustion engine
EP2192287B1 (en) Direct injection internal combustion engine
JP5006905B2 (en) In-cylinder injection spark ignition internal combustion engine
KR20130136917A (en) Injection system for compression ingnition diesel engine
JP2000282873A (en) In-cylinder injection spark ignition internal combustion engine
JP2007138780A (en) Sub-chamber internal combustion engine
JP2002013417A (en) Method for obtaining fuel-air mixture in an internal combustion engine by direct gasoline injection and internal combustion engine with direct gasoline injection
JP2008088920A (en) In-cylinder injection spark ignition internal combustion engine
JP4026406B2 (en) Direct-injection spark ignition internal combustion engine
JP3976153B2 (en) Direct injection spark ignition engine
JPH0712668Y2 (en) Spark ignition direct injection engine
JP3838346B2 (en) In-cylinder injection spark ignition internal combustion engine
JP2010024920A (en) Spark-ignition direct-injection engine

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20050223

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20070530

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20070605

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20070803

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20070918

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20071116

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20080219

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20080303

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20110321

Year of fee payment: 3

LAPS Cancellation because of no payment of annual fees