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JP3689974B2 - In-cylinder direct fuel injection internal combustion engine - Google Patents
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JP3689974B2 - In-cylinder direct fuel injection internal combustion engine - Google Patents

In-cylinder direct fuel injection internal combustion engine Download PDF

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Publication number
JP3689974B2
JP3689974B2 JP13158796A JP13158796A JP3689974B2 JP 3689974 B2 JP3689974 B2 JP 3689974B2 JP 13158796 A JP13158796 A JP 13158796A JP 13158796 A JP13158796 A JP 13158796A JP 3689974 B2 JP3689974 B2 JP 3689974B2
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Japan
Prior art keywords
cylinder
intake
combustion chamber
opening
fuel injection
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 - Lifetime
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JP13158796A
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Japanese (ja)
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JPH09317475A (en
Inventor
章彦 角方
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Nissan Motor Co Ltd
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Nissan Motor Co Ltd
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    • 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
    • F02B23/08Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • F02B23/10Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder
    • F02B23/104Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder the injector being placed on a side position of the cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/12Other methods of operation
    • F02B2075/125Direct injection in the combustion chamber for spark ignition engines, i.e. not in pre-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
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/48Tumble motion in gas movement in cylinder
    • 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は、筒内直接燃料噴射内燃機関に関する。
【0002】
【従来の技術】
従来の筒内直接燃料噴射内燃機関としては、例えば図5に示すような、特開平6−81651号公報に開示されている。この従来例では図5において、4aは吸気ポート、2はピストン、20は着火手段、18は燃料噴射弁であり、Cが燃料噴霧、Vfが筒内のガス流動である。
【0003】
【発明が解決しようとする課題】
しかしながら、このような従来の筒内直接燃料噴射内燃機関にあっては、吸気ポートを燃焼室に対して垂直に近い角度でレイアウトし、圧縮行程後半に燃料噴射弁から着火手段へと向かいピストン上面を這うガス流動を形成し、ピストン凹部に直接燃料を衝突させ、前記ガス流動により燃料を着火手段に輸送する構造となっていたため、ピストン上面にて反射した霧化していない燃料噴霧が直接点火栓に輸送され、点火栓がくすぶるという問題点があった。
【0004】
本発明は、このような従来の問題点に着目してなされたもので、ピストン上面に吸気ポートからの空気流からの進入方向に対し、反時計方向に0度以上90度以下の角度をなし吸気弁側に寄った位置に稜線を有する凸部と排気弁側に寄った位置に凹部を設けることで吸気ポートからの空気流の方向を筒内にて偏向し、シリンダ中心軸に対して、斜めの旋回流を形成し、ピストン上面の凹部に燃料噴射することにより、安定した燃焼を行うことができる、筒内直接燃料噴射内燃機関を提供することを目的としている。
【0005】
【課題を解決するための手段】
本発明は上述の課題を解決するために、シリンダブロックのシリンダ内壁面と該シリンダ内に嵌装されるピストンの上面とシリンダヘッド下面とで定められた燃焼室と、燃焼室の上壁となるシリンダヘッド下面のほぼ中心に設けられた着火手段、シリンダヘッド部燃焼室の一方側に配設された吸気開口部を有する吸気ポートと、吸気開口部を開閉する吸気弁と吸気開口部と相対するシリンダヘッド部燃焼室の他の一方側に配設された排気開口部を有する排気ポートと、排気開口部を開閉する排気弁と前記吸気弁は各々2個である4弁式弁配置の燃焼室構造であり、2つの吸気開口部のほぼ中心付近に排気開口側に向けて配設された筒内直接燃料噴射弁と、ピストン上面にシリンダ中心軸線を含み燃焼室の吸気開口部から排気開口部へ向かう軸線に垂直な平面をシリンダ中心軸線回りに0度より大きく90度より小さい角度だけ回転させた平面と平行で、かつ燃焼室中心より吸気開口部側へ寄った稜線を有する凸部と、その稜線から排気開口側に至るピストン冠面部分に設けられた凹部と、を有し、吸気行程中にシリンダ内に形成したタンブル流を前記凹部および凸部によって斜めスワール流に変換する
【0006】
【発明の実施の形態】
以下、本発明を図面に基づいて詳細に説明する。
【0007】
図1及び図2は、本発明の一実施の形態を示す図である。
【0008】
まず構成を説明すると、図1に示すように燃焼室4のほぼ中心に点火栓2が設けられており、吸気ポート6は2つの吸気弁5を介して燃焼室4に開口している。燃焼室4の吸気ポート6と相対する位置に排気ポート15が排気弁14を介して燃焼室4に開口している。燃焼室内の吸気ポート下部の2つの吸気ポートの中間に排気弁14方向に向けて燃料噴射弁1が配設されている。
【0009】
シリンダブロック9内に嵌装され、上下動するピストン3の上面にシリンダ中心軸12を含有し吸気弁5から排気弁14へ向かう軸線に垂直な平面pに対し、エンジン上面から見て反時計方向に90度以下の角度θ回転させた仮想平面fに平行で燃焼室中心より吸気弁側へ寄った稜線mを有する凸部10とその稜線から排気弁側に至るピストン上面部分に凹部13を設けている。
【0010】
次に本発明の実施の形態の作用を説明する。
【0011】
図3に示すように、吸気弁より流入する空気は排気弁14方向に向かうがピストン上面の凹凸により、シリンダ内の仮想平面fに垂直な方向に偏向され、シリンダ内を斜めに旋回する。ピストン3が上動する圧縮行程後半に噴射弁1より排気弁14側に向けて燃料を噴射する。噴射された燃料16は、排気弁14側のピストン凹部13に集中しシリンダ室11内及び燃焼室4内に形成された斜めスワール流18によりピストン上面凹部13からピストン上面凸部10に斜めに添って燃焼室上部に輸送される。この時、燃料噴射弁1から噴射された燃料16は排気弁14側のピストン上面凹部13にて十分気化した後に、点火栓周辺まで輸送され、濃混合気17が点火栓2の周辺に配されることになる。これによって低負荷時に良好な希薄燃焼が可能となる。
【0012】
一方、図4に示すように、高負荷時は、ピストン3が下動する吸気行程中に燃料を噴射する。燃料噴射弁1より噴射された燃料は、貫徹力によりピストン上面凸部10に衝突し、シリンダ内に燃料を広く拡散することが出来、かつタンブル流19がピストンにより斜めスワール流18に変換されるため、半径方向のガス流動によって、さらに燃料が拡散する。その結果、ガス流動を強化する手段を特別に設けなくても燃料の拡散が容易になされ、混合気の均質化によりサイクル変動に影響されない安定した燃焼を行うことが出来る。
【0013】
【発明の効果】
以上説明してきたように、本発明によれば、その構成を、ピストン上面に、シリンダ中心軸線を含み吸気開口から排気開口へ向かう軸線に垂直な平面をシリンダ中心軸線回りに0度より大きく90度より小さい角度だけ回転させた平面と平行で、かつ燃焼室中心より吸気開口部側へ寄った稜線を有する凸部と、その稜線から排気開口側に至るピストン冠面部分に設けられた凹部と、を設け、吸気行程中にシリンダ内に形成したタンブル流を凹部および凸部によって斜めスワール流に変換するようにしたため、低負荷時に点火栓をくすぶらせることなく、混合気の成層化を成立させ、高負荷時には混合器の均質化を促進できるという効果が得られる。
【図面の簡単な説明】
【図1】本発明の一実施の形態を示す模式図である。
【図2】本発明の一実施の形態を示す模式図である。
【図3】本発明の実施の形態における低負荷時の燃料及び混合気の動きを表す模式図である。
【図4】本発明の実施の形態における高負荷時の燃料及び混合気の動きを表す模式図である。
【図5】従来の筒内直接燃料噴射装置を示す図である。
【符号の説明】
1 燃料噴射弁
2 着火手段
3 ピストン
4 燃焼室
5 吸気弁
6 吸気ポート
9 シリンダブロック
10 ピストン上面凸部
11 シリンダ室
12 シリンダ中心軸
13 ピストン上面凹部
14 排気弁
15 排気ポート
16 燃料噴霧
17 濃混合気
18 スワール流
19 タンブル流
f 仮想平面
m 凸部稜線
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to an in-cylinder direct fuel injection internal combustion engine.
[0002]
[Prior art]
A conventional in-cylinder direct fuel injection internal combustion engine is disclosed, for example, in Japanese Patent Laid-Open No. 6-81651 as shown in FIG. In this conventional example, in FIG. 5, 4a is an intake port, 2 is a piston, 20 is an ignition means, 18 is a fuel injection valve, C is fuel spray, and Vf is gas flow in the cylinder.
[0003]
[Problems to be solved by the invention]
However, in such a conventional in-cylinder direct fuel injection internal combustion engine, the intake port is laid out at an angle close to perpendicular to the combustion chamber, and the upper surface of the piston is directed from the fuel injection valve to the ignition means in the latter half of the compression stroke. Since the gas flow is formed so that the fuel directly collides with the piston recess and the fuel is transported to the ignition means by the gas flow, the non-atomized fuel spray reflected from the upper surface of the piston is directly connected to the spark plug. There was a problem that the spark plug smoldered.
[0004]
The present invention has been made paying attention to such a conventional problem, and forms an angle of 0 degree or more and 90 degrees or less counterclockwise with respect to the approach direction from the air flow from the intake port on the upper surface of the piston. By providing a convex portion having a ridge line at a position close to the intake valve side and a concave portion at a position close to the exhaust valve side, the direction of the air flow from the intake port is deflected in the cylinder, An object of the present invention is to provide an in-cylinder direct fuel injection internal combustion engine capable of performing stable combustion by forming an oblique swirl flow and injecting fuel into a recess on the upper surface of a piston.
[0005]
[Means for Solving the Problems]
In order to solve the above-mentioned problems, the present invention provides a combustion chamber defined by the cylinder inner wall surface of the cylinder block, the upper surface of the piston fitted in the cylinder, and the lower surface of the cylinder head, and the upper wall of the combustion chamber. almost a ignition means provided at the center, and an intake port having an intake opening disposed on one side of the cylinder head combustion chamber, the intake valve and the intake opening and the relative opening and closing the intake opening portion of the lower surface the cylinder head Combustion with a four-valve valve arrangement in which there are two exhaust ports each having an exhaust opening disposed on the other side of the cylinder head combustion chamber, two exhaust valves for opening and closing the exhaust opening, and two intake valves. This is a chamber structure, and includes an in-cylinder direct fuel injection valve disposed near the center of two intake openings toward the exhaust opening, and a cylinder center axis on the upper surface of the piston, and the exhaust opening from the intake opening of the combustion chamber Head to the club A convex portion having a plane perpendicular in the parallel to the plane which is rotated by an angle smaller than than 90 degrees above 0 degrees to the cylinder central axis, and edge line closer than the combustion chamber center to the intake opening side line, ridge line thereof And a concave portion provided in the piston crown surface portion extending from the exhaust opening to the exhaust opening side, and the tumble flow formed in the cylinder during the intake stroke is converted into an oblique swirl flow by the concave portion and the convex portion .
[0006]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, the present invention will be described in detail with reference to the drawings.
[0007]
1 and 2 are diagrams showing an embodiment of the present invention.
[0008]
First, the structure will be described. As shown in FIG. 1, the ignition plug 2 is provided substantially at the center of the combustion chamber 4, and the intake port 6 is opened to the combustion chamber 4 through two intake valves 5. An exhaust port 15 opens to the combustion chamber 4 via an exhaust valve 14 at a position facing the intake port 6 of the combustion chamber 4. The fuel injection valve 1 is disposed in the middle of the two intake ports below the intake port in the combustion chamber toward the exhaust valve 14.
[0009]
A counterclockwise direction when viewed from the engine upper surface with respect to a plane p perpendicular to the axis extending from the intake valve 5 to the exhaust valve 14 and including the cylinder central shaft 12 on the upper surface of the piston 3 which is fitted in the cylinder block 9 and moves up and down. Is provided with a convex portion 10 having a ridge line m parallel to a virtual plane f rotated 90 degrees or less and close to the intake valve side from the center of the combustion chamber, and a concave portion 13 on the piston upper surface portion extending from the ridge line to the exhaust valve side. ing.
[0010]
Next, the operation of the embodiment of the present invention will be described.
[0011]
As shown in FIG. 3, the air flowing in from the intake valve is directed toward the exhaust valve 14, but is deflected in a direction perpendicular to the virtual plane f in the cylinder due to the unevenness of the upper surface of the piston, and turns obliquely in the cylinder. In the latter half of the compression stroke in which the piston 3 moves upward, fuel is injected from the injection valve 1 toward the exhaust valve 14. The injected fuel 16 is concentrated in the piston recess 13 on the exhaust valve 14 side and obliquely follows the piston upper surface recess 13 from the piston upper surface recess 13 to the piston upper surface protrusion 10 by the oblique swirl flow 18 formed in the cylinder chamber 11 and the combustion chamber 4. And transported to the upper part of the combustion chamber. At this time, the fuel 16 injected from the fuel injection valve 1 is sufficiently vaporized in the piston upper surface recess 13 on the exhaust valve 14 side, and then transported to the vicinity of the spark plug, and the rich mixture 17 is arranged around the spark plug 2. It will be. This enables good lean combustion at low loads.
[0012]
On the other hand, as shown in FIG. 4, during a high load, fuel is injected during the intake stroke in which the piston 3 moves downward. The fuel injected from the fuel injection valve 1 collides with the piston upper surface convex portion 10 by a penetrating force, can diffuse the fuel widely in the cylinder, and the tumble flow 19 is converted into an oblique swirl flow 18 by the piston. Therefore, the fuel is further diffused by the gas flow in the radial direction. As a result, the fuel can be easily diffused without specially providing a means for enhancing the gas flow, and stable combustion can be performed without being affected by cycle fluctuations by homogenizing the air-fuel mixture.
[0013]
【The invention's effect】
As described above, according to the present invention, the configuration is such that the plane on the upper surface of the piston is perpendicular to the axis that includes the cylinder center axis and extends from the intake opening to the exhaust opening, and is greater than 0 degree and about 90 degrees around the cylinder center axis. A convex portion having a ridge line parallel to a plane rotated by a smaller angle and approaching the intake opening side from the center of the combustion chamber, and a concave portion provided in a piston crown surface portion extending from the ridge line to the exhaust opening side ; The tumble flow formed in the cylinder during the intake stroke is converted into an oblique swirl flow by the concave and convex portions, so that stratification of the air-fuel mixture can be established without smoldering the spark plug at low load. The effect that the homogenization of the mixer can be promoted at a high load is obtained.
[Brief description of the drawings]
FIG. 1 is a schematic diagram showing an embodiment of the present invention.
FIG. 2 is a schematic diagram showing an embodiment of the present invention.
FIG. 3 is a schematic diagram showing the movement of fuel and air-fuel mixture at low load in the embodiment of the present invention.
FIG. 4 is a schematic diagram showing the movement of fuel and air-fuel mixture at high load in the embodiment of the present invention.
FIG. 5 is a view showing a conventional in-cylinder direct fuel injection device.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 Fuel injection valve 2 Ignition means 3 Piston 4 Combustion chamber 5 Intake valve 6 Intake port 9 Cylinder block 10 Piston upper surface convex part 11 Cylinder chamber 12 Cylinder central axis 13 Piston upper surface recessed part 14 Exhaust valve 15 Exhaust port 16 Fuel spray 17 Concentrated mixture 18 Swirl flow 19 Tumble flow f Virtual plane m Convex ridgeline

Claims (2)

シリンダブロックのシリンダ内壁面と該シリンダ内に嵌装されるピストンの上面とシリンダヘッド下面とで定められた燃焼室と、該燃焼室の上壁となるシリンダヘッド下面のほぼ中心に設けられた着火手段、該シリンダヘッド部燃焼室の一方側に配設された吸気開口部を有する吸気ポートと、前記吸気開口部を開閉する吸気弁と前記吸気開口部と相対するシリンダヘッド部燃焼室の他の一方側に配設された排気開口部を有する排気ポートと、前記排気開口部を開閉する排気弁と前記吸気弁は各々2個である4弁式弁配置の燃焼室構造であり、前記2つの吸気開口部のほぼ中心付近に排気開口側に向けて配設された筒内直接燃料噴射弁と、前記ピストン上面にシリンダ中心軸線を含み燃焼室の吸気開口部から排気開口部へ向かう軸線に垂直な平面を前記シリンダ中心軸線回りに0度より大きく90度より小さい角度だけ回転させた平面と平行で、かつ燃焼室中心より吸気開口部側へ寄った稜線を有する凸部と、その稜線から排気開口側に至るピストン冠面部分に設けられた凹部と、を有し、吸気行程中にシリンダ内に形成したタンブル流を前記凹部および凸部によって斜めスワール流に変換することを特徴とした筒内直接燃料噴射内燃機関。A combustion chamber defined by the cylinder inner wall surface of the cylinder block, the upper surface of the piston fitted in the cylinder, and the lower surface of the cylinder head, and the ignition provided substantially at the center of the lower surface of the cylinder head serving as the upper wall of the combustion chamber means and the other of said intake port having an intake opening disposed on one side of the cylinder head combustion chamber, an intake valve for opening and closing the intake opening and the intake opening opposite the cylinder head combustion chamber An exhaust port having an exhaust opening disposed on one side of the combustion chamber, a four-valve valve arrangement combustion chamber structure in which two exhaust valves and two intake valves each for opening and closing the exhaust opening are provided. An in-cylinder direct fuel injection valve disposed near the center of one intake opening toward the exhaust opening, and an axis extending from the intake opening of the combustion chamber to the exhaust opening including the cylinder central axis on the upper surface of the piston. Vertical Plane at a parallel to the plane obtained by rotating by the angle the less than greater 90 degrees above 0 degrees to the cylinder central axis, and a convex portion having a ridge line closer than the combustion chamber center to the intake opening side, the exhaust opening from the ridge And a concave portion provided in a piston crown surface portion to the side, and a tumble flow formed in the cylinder during the intake stroke is converted into an oblique swirl flow by the concave portion and the convex portion, and directly in the cylinder Fuel injection internal combustion engine. 前記燃料噴射弁より燃料を噴射する時期を、低負荷時は圧縮行程とし、高負荷時は吸気行程とすることを特徴とする上記請求項1に記載の筒内直接燃料噴射内燃機関。  2. The direct injection fuel injection internal combustion engine according to claim 1, wherein the fuel is injected from the fuel injection valve at a compression stroke when the load is low and an intake stroke when the load is high.
JP13158796A 1996-05-27 1996-05-27 In-cylinder direct fuel injection internal combustion engine Expired - Lifetime JP3689974B2 (en)

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JP2004224402A Division JP4059234B2 (en) 2004-07-30 2004-07-30 In-cylinder direct fuel injection internal combustion engine

Publications (2)

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JPH09317475A JPH09317475A (en) 1997-12-09
JP3689974B2 true JP3689974B2 (en) 2005-08-31

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JP3692749B2 (en) * 1997-12-22 2005-09-07 日産自動車株式会社 Piston for in-cylinder internal combustion engine
JP3726503B2 (en) * 1998-01-06 2005-12-14 日産自動車株式会社 Direct-injection spark ignition internal combustion engine
AT2538U1 (en) * 1998-01-13 1998-12-28 Avl List Gmbh INTERNAL COMBUSTION ENGINE WITH AT LEAST ONE INJECTION DEVICE PER CYLINDER
JP4026365B2 (en) 1999-06-11 2007-12-26 株式会社日立製作所 In-cylinder injection engine
JP2001241329A (en) 2000-02-28 2001-09-07 Hitachi Ltd In-cylinder injection type internal combustion engine
KR20030021307A (en) * 2001-09-05 2003-03-15 현대자동차주식회사 Engine structure to improve combustion efficiency
JP5262991B2 (en) * 2009-05-22 2013-08-14 マツダ株式会社 Intake control system for spark ignition direct injection engine

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