JP2005133679A - Cylinder injection type spark ignition internal combustion engine - Google Patents

Cylinder injection type spark ignition internal combustion engine Download PDF

Info

Publication number
JP2005133679A
JP2005133679A JP2003372324A JP2003372324A JP2005133679A JP 2005133679 A JP2005133679 A JP 2005133679A JP 2003372324 A JP2003372324 A JP 2003372324A JP 2003372324 A JP2003372324 A JP 2003372324A JP 2005133679 A JP2005133679 A JP 2005133679A
Authority
JP
Japan
Prior art keywords
fuel
fan
cylinder
fuel spray
shaped
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
JP2003372324A
Other languages
Japanese (ja)
Other versions
JP4103775B2 (en
Inventor
Tomojiro Sugimoto
知士郎 杉本
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
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 Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP2003372324A priority Critical patent/JP4103775B2/en
Publication of JP2005133679A publication Critical patent/JP2005133679A/en
Application granted granted Critical
Publication of JP4103775B2 publication Critical patent/JP4103775B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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 generate good homogeneous fuel/air mixture without diluting engine oil, in a cylinder injection type spark ignition internal combustion engine for performing homogeneous combustion. <P>SOLUTION: The cylinder injection type spark ignition internal combustion engine injects fuel with a fuel injection valve 2 arranged around the upper part of the cylinder to generate the homogeneous fuel/air mixture. The fuel injection valve injects fan-like fuel spray spreading mainly in the width direction W into the whole cylinder of last half of an intake process so that the center plane in the thickness direction of the fan-like fuel spray is substantially parallel with the center axis C of the cylinder, and a penetration force in the upper part of the fan-like fuel spray is weakened compared with the lower part of the fan-like fuel spray. <P>COPYRIGHT: (C)2005,JPO&NCIPI

Description

本発明は、筒内噴射式火花点火内燃機関に関する。   The present invention relates to a direct injection spark ignition internal combustion engine.

気筒内へ必要量の燃料を確実に供給するために気筒内へ直接的に燃料を噴射する筒内噴射式火花点火内燃機関が公知である。   2. Description of the Related Art A cylinder injection spark ignition internal combustion engine that directly injects fuel into a cylinder in order to reliably supply a required amount of fuel into the cylinder is known.

このような筒内噴射式火花点火内燃機関において、吸気行程において燃料を噴射して気筒内に均質混合気を形成し、この均質混合気を着火燃焼させる均質燃焼が実施される。良好な均質燃焼を実現するためには十分に均質化された均質混合気を形成することが必要である。   In such an in-cylinder injection spark ignition internal combustion engine, fuel is injected in the intake stroke to form a homogeneous mixture in the cylinder, and homogeneous combustion is performed in which this homogeneous mixture is ignited and combusted. In order to achieve good homogeneous combustion, it is necessary to form a sufficiently homogenized homogeneous mixture.

十分に均質化された均質混合気を形成するには、吸気行程後半の大きな気筒内空間全体に噴射燃料が行き亘るように、気筒上部周囲に配置された燃料噴射弁によって先広がりの燃料噴霧を比較的大きな貫徹力を持たせて噴射することが必要である。円錐状燃料噴霧では貫徹力が弱いために、先広がりの燃料噴霧として、主に幅方向に広がる扇状燃料噴霧を使用することが考えられる。   In order to form a sufficiently homogenized homogeneous air-fuel mixture, fuel spray that spreads out is spread by a fuel injection valve arranged around the upper part of the cylinder so that the injected fuel spreads over the entire large cylinder space in the latter half of the intake stroke. It is necessary to inject with a relatively large penetration force. Since the penetration force is weak in the conical fuel spray, it is conceivable to use a fan-shaped fuel spray that spreads mainly in the width direction as the fuel spray that spreads forward.

扇状燃料噴霧を縦方向に、例えば、扇状燃料噴霧の幅方向が燃料噴射弁の噴孔中心と気筒の中心軸線とを通る平面に対して平行となるように使用する筒内噴射式火花点火内燃機関が提案されている(例えば、特許文献1参照)。   In-cylinder injection spark-ignition internal combustion that uses fan-shaped fuel spray in the vertical direction, for example, so that the width direction of fan-shaped fuel spray is parallel to a plane passing through the center of the injection hole of the fuel injection valve and the center axis of the cylinder An engine has been proposed (see, for example, Patent Document 1).

特開2000−220460号公報JP 2000-220460 A 特開平11−200866号公報Japanese Patent Application Laid-Open No. 11-200086

扇状燃料噴霧を前述のように縦方向に使用し、吸気行程後半のピストン位置において、扇状燃料噴霧の上部が気筒内空間のシリンダヘッド近傍を、また、扇状燃料噴霧の下部がピストン近傍を向くように、扇状燃料噴霧の扇夾角を適当に選択することにより、吸気行程後半の大きな気筒内空間全体に噴射燃料を行き亘らせるようにすることができる。それにより、その後の圧縮行程において良好な均質混合気を形成することが可能となる。しかしながら、貫徹力が比較的大きな扇状燃料噴霧をこのように噴射すると、シリンダヘッド近傍においては、燃料噴射弁の噴孔からシリンダボアまでの距離が比較的短いために、扇状燃料噴霧の上部はシリンダボアに衝突し、その際にシリンダボアに付着する燃料がエンジンオイルを希釈させてしまう。   Using fan-shaped fuel spray in the vertical direction as described above, at the piston position in the latter half of the intake stroke, the upper part of the fan-shaped fuel spray faces the cylinder head in the cylinder space, and the lower part of the fan-shaped fuel spray faces the piston. In addition, by appropriately selecting the fan angle of the fan fuel spray, the injected fuel can be spread over the entire large cylinder space in the latter half of the intake stroke. This makes it possible to form a good homogeneous mixture in the subsequent compression stroke. However, when a fan-shaped fuel spray having a relatively high penetrating force is injected in this manner, the distance from the nozzle hole of the fuel injection valve to the cylinder bore is relatively short in the vicinity of the cylinder head. The fuel that collides and adheres to the cylinder bore at that time dilutes the engine oil.

従って、本発明の目的は、均質燃焼を実施する筒内噴射式火花点火内燃機関において、エンジンオイルを希釈させることなく良好な均質混合気の形成を可能とすることである。   Accordingly, an object of the present invention is to enable the formation of a good homogeneous air-fuel mixture without diluting engine oil in an in-cylinder injection spark ignition internal combustion engine that performs homogeneous combustion.

本発明による請求項1に記載の筒内噴射式火花点火内燃機関は、気筒上部周囲に配置された燃料噴射弁により燃料を噴射して均質混合気を形成する筒内噴射式火花点火内燃機関において、前記燃料噴射弁は、主には幅方向に広がる扇状燃料噴霧を、前記扇状燃料噴霧の厚さ方向中心平面が気筒中心軸線と略平行となるように吸気行程後半の気筒内全体に噴射し、前記扇状燃料噴霧の上部は、前記扇状燃料噴霧の下部に比較して貫徹力が弱められることを特徴とする。   A direct injection spark ignition internal combustion engine according to claim 1 of the present invention is a direct injection spark ignition internal combustion engine in which fuel is injected by a fuel injection valve disposed around the upper part of the cylinder to form a homogeneous mixture. The fuel injection valve mainly injects fan-shaped fuel spray spreading in the width direction into the entire cylinder in the latter half of the intake stroke so that the center plane in the thickness direction of the fan-shaped fuel spray is substantially parallel to the cylinder center axis. The upper part of the fan-shaped fuel spray has a penetrating force weaker than that of the lower part of the fan-shaped fuel spray.

また、本発明による請求項2に記載の筒内噴射式火花点火内燃機関は、請求項1に記載の筒内噴射式火花点火内燃機関において、前記燃料噴射弁は、前記扇状燃料噴霧を噴射するために互いに所定扇夾角で対向する上壁及び下壁を有するスリット状の噴孔を具備し、前記噴孔は前記燃料噴射弁内の燃料溜と連通し、前記噴孔の厚さ方向に垂直な各断面において、前記燃料溜と前記噴孔との間の境界は円弧形状であり、前記各断面において、前記上壁及び前記下壁の延長線の交点は、前記各断面における前記円弧形状の中心に対して偏倚し、前記交点までの前記上壁の延長線は前記交点までの前記下壁の延長線より長くされることを特徴とする。   According to a second aspect of the present invention, the direct injection spark ignition internal combustion engine according to the second aspect is the direct injection spark ignition internal combustion engine according to the first aspect, wherein the fuel injection valve injects the fan-shaped fuel spray. Therefore, a nozzle hole having an upper wall and a lower wall facing each other at a predetermined fan angle is provided. The nozzle hole communicates with a fuel reservoir in the fuel injection valve and is perpendicular to the thickness direction of the nozzle hole. In each cross section, the boundary between the fuel reservoir and the nozzle hole has an arc shape, and in each cross section, the intersection of the extension lines of the upper wall and the lower wall is the arc shape in each cross section. It is biased with respect to the center, and the extension line of the upper wall to the intersection point is longer than the extension line of the lower wall to the intersection point.

また、本発明による請求項3に記載の筒内噴射式火花点火内燃機関は、請求項1に記載の筒内噴射式火花点火内燃機関において、前記燃料噴射弁は、前記扇状燃料噴霧を噴射するために上下方向に配列された多数の小径噴孔を具備し、上側の小径噴孔群の孔径が下側の小径噴孔群の孔径より小さいか、又は、上側の小径噴孔群の孔数が下側の小径噴孔群の孔数より少ないことを特徴とする。   According to a third aspect of the present invention, the direct injection spark ignition internal combustion engine according to the third aspect is the direct injection spark ignition internal combustion engine according to the first aspect, wherein the fuel injection valve injects the fan-shaped fuel spray. Therefore, it has a large number of small diameter nozzle holes arranged in the vertical direction, and the hole diameter of the upper small diameter hole group is smaller than the hole diameter of the lower small diameter hole group or the number of holes of the upper small diameter hole group Is smaller than the number of holes in the lower small-diameter nozzle hole group.

請求項1に記載の筒内噴射式火花点火内燃機関によれば、扇状燃料噴霧の上部は、扇状燃料噴霧の下部に比較して貫徹力が弱められるために、吸気行程後半において、扇状燃料噴霧の下部は、強い貫徹力によって長い距離の飛行が可能であるために、ピストン近傍へ確実に到達し、また、扇状燃料噴霧の上部は、弱くされた貫徹力によって短い距離の飛行しか可能とならず、シリンダボア近傍には達するが、シリンダボアに衝突することは抑制される。こうして、エンジンオイルを希釈させることなく、吸気行程後半の大きな気筒内空間全体に噴射燃料を行き亘らせるようにすることができ、良好な均質混合気の形成が可能となる。   According to the cylinder-injection spark ignition internal combustion engine according to claim 1, since the penetrating force is weakened in the upper part of the fan-shaped fuel spray as compared with the lower part of the fan-shaped fuel spray, the fan-shaped fuel spray in the latter half of the intake stroke. The lower part of the fan can fly long distances with a strong penetrating force, so that it can reach the vicinity of the piston reliably, and the upper part of the fan fuel spray can only fly a short distance with weak penetrating forces. However, although it reaches the vicinity of the cylinder bore, collision with the cylinder bore is suppressed. Thus, the injected fuel can be spread over the entire large cylinder space in the latter half of the intake stroke without diluting the engine oil, and a good homogeneous mixture can be formed.

図1は本発明による筒内噴射式火花点火内燃機関の吸気行程後半における概略縦断面図であり、図2は図1の気筒内平面図である。これらの図において、1は気筒上部略中心に配置された点火プラグであり、2は気筒上部周囲から気筒内へ直接的に燃料を噴射するための燃料噴射弁である。また、3はピストンである。4は気筒上部に接続された吸気ポートであり、5は吸気ポート4の気筒内開口を開閉する吸気弁である。6は気筒上部に接続された排気ポートであり。7は排気ポート6の気筒内開口を開閉する排気弁である。燃料噴射弁2は、燃料のベーパを防止するために、気筒内において吸気流により比較的低温度となる吸気ポート側に配置されている。   FIG. 1 is a schematic longitudinal sectional view in the latter half of an intake stroke of a cylinder injection type spark ignition internal combustion engine according to the present invention, and FIG. 2 is a plan view of the cylinder in FIG. In these drawings, reference numeral 1 denotes an ignition plug disposed substantially at the center of the upper part of the cylinder, and 2 denotes a fuel injection valve for injecting fuel directly from the periphery of the upper part of the cylinder into the cylinder. Reference numeral 3 denotes a piston. 4 is an intake port connected to the upper part of the cylinder, and 5 is an intake valve that opens and closes the opening of the intake port 4 in the cylinder. 6 is an exhaust port connected to the upper part of the cylinder. Reference numeral 7 denotes an exhaust valve that opens and closes the cylinder opening of the exhaust port 6. The fuel injection valve 2 is disposed on the intake port side where the temperature becomes relatively low due to the intake air flow in the cylinder in order to prevent fuel vapor.

また、燃料噴射弁2は、スリット状の噴孔を有し、主には幅方向Wに広がる扇状燃料噴霧を、扇状燃料噴霧の厚さ方向Tの中心平面Pが気筒中心軸線Cと略平行となるように噴射するものである。図2に示すように、扇状燃料噴霧は、厚さ方向Tにも僅かに広がるようにしても良い。また、燃料噴射弁2は、図3に示すように、複数(例えば、二つ)の扇状燃料噴霧を、それぞれの厚さ方向の中心平面(P1及びP2)が気筒中心軸線Cと略平行となるように噴射するようにしても良い。   The fuel injection valve 2 has a slit-shaped injection hole, and mainly serves as a fan-shaped fuel spray extending in the width direction W. The center plane P in the thickness direction T of the fan-shaped fuel spray is substantially parallel to the cylinder center axis C. It is injected so that As shown in FIG. 2, the fan-shaped fuel spray may spread slightly in the thickness direction T. Further, as shown in FIG. 3, the fuel injection valve 2 is configured such that a plurality of (for example, two) fan-shaped fuel sprays have center planes (P1 and P2) in the thickness direction substantially parallel to the cylinder center axis C. You may make it inject so that it may become.

また、燃料噴射弁2から噴射される扇状燃料噴霧は、図1に示すように、吸気行程後半のピストン位置において、扇状燃料噴霧の上部が気筒内空間のシリンダヘッド近傍を、また、扇状燃料噴霧の下部がピストン近傍を向くようにされている。   Further, as shown in FIG. 1, the fan-shaped fuel spray injected from the fuel injection valve 2 has an upper portion of the fan-shaped fuel spray near the cylinder head in the cylinder space and a fan-shaped fuel spray at the piston position in the latter half of the intake stroke. The lower part of is directed to the vicinity of the piston.

扇状燃料噴霧は円錐状燃料噴霧に比較して大きな貫徹力を有し、扇状燃料噴霧の各部は比較的長い距離を飛行可能である。それにより、吸気行程後半において、扇状燃料噴霧の下部(ピストン側)はピストン近傍まで確実に到達し、吸気行程後半の大きな気筒内空間全体に噴射燃料を行き亘らせるようにすることができ、その後の圧縮行程において十分に均質化された均質混合気の形成が可能となる。しかしながら、通常の扇状燃料噴霧を使用すると、シリンダヘッド近傍においては、燃料噴射弁の噴孔からシリンダボアまでの距離が比較的短いために、扇状燃料噴霧の上部(シリンダヘッド側)は大きな貫徹力が災いしてシリンダボアに衝突してしまう。その際にシリンダボアに燃料が付着するとエンジンオイルの希釈の問題が発生する。   The fan-shaped fuel spray has a greater penetration force than the conical fuel spray, and each part of the fan-shaped fuel spray can fly over a relatively long distance. Thereby, in the latter half of the intake stroke, the lower part (piston side) of the fan-shaped fuel spray reliably reaches the vicinity of the piston, and the injected fuel can be spread over the entire large cylinder space in the latter half of the intake stroke. In the subsequent compression stroke, it is possible to form a homogeneous mixture that is sufficiently homogenized. However, when a normal fan fuel spray is used, the distance from the nozzle hole of the fuel injection valve to the cylinder bore is relatively short in the vicinity of the cylinder head. A disaster strikes the cylinder bore. At this time, if fuel adheres to the cylinder bore, a problem of dilution of engine oil occurs.

本実施形態においては、この問題を解決するために、燃料噴射弁2から噴射する扇状燃料噴霧の上部における貫徹力を下部に比較して弱めるようにしている。それにより、扇状燃料噴霧の上部は、シリンダボア近傍へ到達しても、シリンダボアへ衝突することは抑制される。それにより、エンジンオイルを希釈させることなく良好な均質混合気の形成が可能となる。   In this embodiment, in order to solve this problem, the penetration force at the upper part of the fan-shaped fuel spray injected from the fuel injection valve 2 is weakened as compared with the lower part. Thereby, even if the upper part of the fan-shaped fuel spray reaches the vicinity of the cylinder bore, the collision with the cylinder bore is suppressed. Thereby, it is possible to form a good homogeneous mixture without diluting the engine oil.

このように扇状燃料噴霧の上部の貫徹力を弱めるために、本実施形態において、燃料噴射弁2のスリット状の噴孔21は図4に示すように形成されている。図4は、燃料噴射弁2の噴孔近傍における噴孔21の厚さ方向に垂直な拡大断面図である。同図において、22は燃料噴射弁内の燃料溜であり、噴孔21は燃料溜22に連通している。それにより、弁体(図示せず)が開弁して燃料溜22へ高圧燃料が供給されれば、燃料溜22内の高圧燃料が噴孔21を介して噴射される。一方、弁体が閉弁して燃料溜22への高圧燃料の供給が停止されれば、燃料溜22内の燃料圧力が低下し、噴孔21を介しての燃料噴射は停止される。   Thus, in order to weaken the penetration force of the upper part of fan-shaped fuel spray, in this embodiment, the slit-shaped injection hole 21 of the fuel injection valve 2 is formed as shown in FIG. FIG. 4 is an enlarged cross-sectional view perpendicular to the thickness direction of the injection hole 21 in the vicinity of the injection hole of the fuel injection valve 2. In the figure, reference numeral 22 denotes a fuel reservoir in the fuel injection valve, and the nozzle hole 21 communicates with the fuel reservoir 22. As a result, when the valve body (not shown) is opened and high pressure fuel is supplied to the fuel reservoir 22, the high pressure fuel in the fuel reservoir 22 is injected through the injection hole 21. On the other hand, when the valve body is closed and the supply of the high-pressure fuel to the fuel reservoir 22 is stopped, the fuel pressure in the fuel reservoir 22 decreases, and the fuel injection through the nozzle hole 21 is stopped.

本実施形態において、燃料溜22は半球形状の先端部を有し、この先端部に連通して、扇状燃料噴霧を噴射するために所定扇夾角で対向する上壁21a及び下壁21bを有する噴孔21が形成されている。それにより、噴孔21の厚さ方向に垂直な各断面において、燃料溜22と噴孔21との境界は円弧形状となっている。   In the present embodiment, the fuel reservoir 22 has a hemispherical tip, and is an injection having an upper wall 21a and a lower wall 21b that communicate with the tip and face each other at a predetermined fan angle in order to inject a fan-shaped fuel spray. A hole 21 is formed. Thereby, in each cross section perpendicular | vertical to the thickness direction of the nozzle hole 21, the boundary of the fuel reservoir 22 and the nozzle hole 21 becomes circular arc shape.

これら各断面において、本実施形態とは異なり、噴孔21の上壁21aの延長線と下壁21bの延長線との交点Rが、もし、境界の円弧形状の中心Q(厚さ方向における中央断面においては、円弧形状中心Qと燃料溜22の先端部の半球形状中心とは一致する)に一致していると、燃料溜22から噴孔21の内側開口へ流入した燃料を放射状に分割して考えた場合において、燃料各部は、燃料溜22内の燃料圧力が円弧形状中心Qを中心として放射状に作用するために、噴孔21内で等しく幅方向に広がって噴孔21の外側開口から噴射される。こうして、扇状燃料噴霧を形成する燃料各部は、比較的高い貫徹力を有し、扇状燃料噴霧の上部はシリンダボアへ衝突してしまう。   In each of these cross sections, unlike the present embodiment, the intersection R of the extension line of the upper wall 21a and the extension line of the lower wall 21b of the nozzle hole 21 is the center Q of the boundary arc shape (the center in the thickness direction). In the cross section, if the arc-shaped center Q coincides with the hemispherical center of the tip of the fuel reservoir 22, the fuel flowing from the fuel reservoir 22 into the inner opening of the injection hole 21 is radially divided. In this case, since the fuel pressure in the fuel reservoir 22 acts radially around the arc-shaped center Q, each fuel part spreads in the width direction equally in the nozzle hole 21 and from the outer opening of the nozzle hole 21. Be injected. Thus, each fuel part forming the fan-shaped fuel spray has a relatively high penetration force, and the upper part of the fan-shaped fuel spray collides with the cylinder bore.

本実施形態では、前述の各断面において、噴孔21の上壁21aの延長線と下壁21bの延長線との交点Rが、境界の円弧形状中心Qから偏倚するようにし、交点までの上壁21aの延長線が、交点までの下壁21bの延長線より長くされている。こうすることにより、交点Rは円弧形状中心Qと噴孔21の外側開口の幅方向中心とを通る直線より下側となる。   In the present embodiment, in each cross section described above, the intersection R of the extension line of the upper wall 21a and the extension line of the lower wall 21b of the nozzle hole 21 is deviated from the arcuate center Q of the boundary. The extension line of the wall 21a is made longer than the extension line of the lower wall 21b to the intersection. By doing so, the intersection R is below the straight line passing through the arcuate center Q and the center in the width direction of the outer opening of the nozzle hole 21.

それにより、前述同様に考えた場合において、燃料溜22から噴孔21の内側開口へ流入した燃料各部は、噴孔21内において円弧形状中心Qを中心として放射状に作用する燃料圧力によって幅方向に広がることとなるが、前述の交点Rの偏倚によって、図4に示すように、下壁21bに近いほど幅方向にあまり広がることなく、また、噴孔21の上壁21aに近いほど幅方向に大きく広がって、噴孔21の外側開口から噴射されることとなる。こうして、扇状燃料噴霧の上部を形成する燃料部分の貫徹力は弱められ、短い距離の飛行しか可能とならず、シリンダボアへの衝突が抑制される。一方、扇状燃料噴霧の下部を形成する燃料部分の貫徹力は強められ、長い距離の飛行が可能となって吸気行程後半においてピストン近傍まで確実に到達することができる。   As a result, in the same way as described above, each part of the fuel that has flowed from the fuel reservoir 22 into the inner opening of the injection hole 21 is expanded in the width direction by the fuel pressure acting radially around the arc-shaped center Q in the injection hole 21. As shown in FIG. 4, due to the deviation of the intersection point R described above, the closer to the lower wall 21b, the less it spreads in the width direction, and the closer to the upper wall 21a of the nozzle hole 21, the more in the width direction. It spreads greatly and will be injected from the outer side opening of the nozzle hole 21. Thus, the penetration force of the fuel portion forming the upper part of the fan-shaped fuel spray is weakened, and only a short distance flight is possible, and the collision with the cylinder bore is suppressed. On the other hand, the penetrating force of the fuel portion forming the lower part of the fan-shaped fuel spray is strengthened, and it is possible to fly over a long distance and reliably reach the vicinity of the piston in the latter half of the intake stroke.

従来のように一様にされた扇状燃料噴霧の各部の貫徹力に対して、扇状燃料噴霧の上部の貫徹力を弱めると共に、扇状燃料噴霧の下部の貫徹力を強める場合には、噴孔21の上壁の延長線が円弧形状中心Qと噴孔21の外側開口の幅方向中心とを通る直線に対して、円弧形状中心Qより噴孔側で交差するように、また、噴孔21の下壁の延長線が円弧形状中心Qと噴孔21の外側開口の幅方向中心とを通る直線に対して、円弧形状中心Qより反噴孔側(弁体側)で交差するようにすれば良い。もちろん、この場合においても、互いの交点までの上壁21aの延長線は、互いの交点までの下壁21bの延長線より長くなる。   In order to weaken the penetration force of the upper part of the fan-shaped fuel spray and to increase the penetration force of the lower part of the fan-shaped fuel spray with respect to the penetration force of each part of the fan-shaped fuel spray made uniform as in the prior art, the injection hole 21 An extension line of the upper wall intersects the straight line passing through the arc-shaped center Q and the center in the width direction of the outer opening of the nozzle hole 21 on the nozzle hole side with respect to the arc-shaped center Q. The extension line of the lower wall may intersect the straight line passing through the arc-shaped center Q and the center in the width direction of the outer opening of the injection hole 21 on the side opposite to the injection hole (valve element side) from the arc-shaped center Q. . Of course, also in this case, the extension line of the upper wall 21a to the mutual intersection becomes longer than the extension line of the lower wall 21b to the mutual intersection.

ところで、スリット状噴孔ではなく、図5及び図6に示すように上下方向に配列された多数の小径噴孔により前述の扇状燃料噴霧を形成することが可能である。図5及び図6において、多数の小径噴孔は、好ましくは、それぞれ燃料溜の半球形状先端部の中心から放射状に形成される。この場合においても、扇状燃料噴霧の上部における貫徹力を弱めることが必要である。   By the way, it is possible to form the above-mentioned fan-shaped fuel spray not by the slit-shaped nozzle holes but by a large number of small-diameter nozzle holes arranged in the vertical direction as shown in FIGS. 5 and 6, the large number of small-diameter injection holes are preferably formed radially from the center of the hemispherical tip of the fuel reservoir. Even in this case, it is necessary to weaken the penetrating force in the upper part of the fan-shaped fuel spray.

図5に示す燃料噴射弁2’では、扇状燃料噴霧の上部を形成する上側の第一小径噴孔群Aの孔径を扇状燃料噴霧の下部を形成する下側の第二小径噴孔群Bの孔径より小さくしている。それにより、第一小径噴孔群A全体から噴射される燃料の流量は第二小径噴孔群B全体から噴射される燃料の流量より少なくなり、扇状燃料噴霧の上部における貫徹力を弱めることができる。   In the fuel injection valve 2 'shown in FIG. 5, the hole diameter of the upper first small-diameter nozzle hole group A forming the upper part of the fan-shaped fuel spray is set to the lower second small-diameter nozzle hole group B forming the lower part of the fan-shaped fuel spray. It is smaller than the hole diameter. Thereby, the flow rate of the fuel injected from the entire first small-diameter nozzle hole group A becomes smaller than the flow rate of the fuel injected from the entire second small-diameter nozzle hole group B, and the penetration force in the upper part of the fan-shaped fuel spray can be weakened. it can.

また、図6に示す燃料噴射弁2”では、扇状燃料噴霧の上部を形成する上側の第一小径噴孔群Cの孔数を扇状燃料噴霧の下部を形成する下側の第二小径噴孔群Dの孔数より少なくしている。それにより、第一小径噴孔群C全体から噴射される燃料の流量は第二小径噴孔群D全体から噴射される燃料の流量より少なくなり、扇状燃料噴霧の上部における貫徹力を弱めることができる。また、第二小径噴孔群Dの各噴孔は第一小径噴孔群Cの各噴孔に比較して密に形成されるために、第二小径噴孔群Dの各噴孔から噴射される各燃料噴霧は、互いに干渉して一塊となり易く、一塊となれば貫徹力が高まるために、扇状燃料噴霧の下部は吸気行程後半においてピストン近傍まで確実に到達することができる。   In addition, in the fuel injection valve 2 ″ shown in FIG. 6, the number of holes in the upper first small-diameter nozzle hole group C forming the upper part of the fan-shaped fuel spray is set to the lower second small-diameter nozzle hole forming the lower part of the fan-shaped fuel spray. The number of holes is smaller than that of the group D. Thereby, the flow rate of the fuel injected from the entire first small-diameter nozzle hole group C is smaller than the flow rate of the fuel injected from the entire second small-diameter nozzle hole group D. The penetration force in the upper part of the fuel spray can be weakened, and the injection holes of the second small diameter injection hole group D are formed more densely than the injection holes of the first small diameter injection hole group C. Each fuel spray injected from each nozzle hole of the second small-diameter nozzle hole group D is likely to interfere with each other and easily form a lump. When the lump becomes a lump, the penetration force increases. It is possible to reliably reach the vicinity.

本実施形態の筒内噴射式火花点火内燃機関は、吸気行程燃料噴射により均質燃焼を実施するものであるが、燃料噴射量が少ない機関低負荷時等において、圧縮行程後半で燃料を噴射して点火プラグ近傍だけに可燃混合気を形成する成層燃焼も実施可能である。   The in-cylinder injection spark ignition internal combustion engine of the present embodiment performs homogeneous combustion by intake stroke fuel injection, but injects fuel in the latter half of the compression stroke when the engine has a low fuel injection amount and a low load. Stratified combustion in which a combustible air-fuel mixture is formed only near the spark plug is also possible.

本発明による筒内噴射式火花点火内燃機関の実施形態を示す吸気行程後半における概略縦断面図である。It is a schematic longitudinal cross-sectional view in the second half of the intake stroke showing an embodiment of a direct injection spark ignition internal combustion engine according to the present invention. 図1の筒内噴射式火花点火内燃機関の気筒内平面図である。FIG. 2 is a plan view in a cylinder of the cylinder injection type spark ignition internal combustion engine of FIG. 1. 図1の筒内噴射式火花点火内燃機関のもう一つの気筒内平面図である。FIG. 2 is another in-cylinder plan view of the in-cylinder injection spark ignition internal combustion engine of FIG. 1. 燃料噴射弁の噴孔近傍における噴孔の厚さ方向に垂直な拡大断面図である。It is an expanded sectional view perpendicular to the thickness direction of the nozzle hole in the vicinity of the nozzle hole of the fuel injection valve. もう一つの燃料噴射弁の正面図である。It is a front view of another fuel injection valve. さらにもう一つの燃料噴射弁の正面図である。It is a front view of another fuel injection valve.

符号の説明Explanation of symbols

1…点火プラグ
2,2’,2”…燃料噴射弁
3…ピストン
21…噴孔
22…燃料溜
DESCRIPTION OF SYMBOLS 1 ... Spark plug 2, 2 ', 2 "... Fuel injection valve 3 ... Piston 21 ... Injection hole 22 ... Fuel reservoir

Claims (3)

気筒上部周囲に配置された燃料噴射弁により燃料を噴射して均質混合気を形成する筒内噴射式火花点火内燃機関において、前記燃料噴射弁は、主には幅方向に広がる扇状燃料噴霧を、前記扇状燃料噴霧の厚さ方向中心平面が気筒中心軸線と略平行となるように吸気行程後半の気筒内全体に噴射し、前記扇状燃料噴霧の上部は、前記扇状燃料噴霧の下部に比較して貫徹力が弱められることを特徴とする筒内噴射式火花点火内燃機関。   In a cylinder injection spark ignition internal combustion engine in which fuel is injected by a fuel injection valve arranged around the upper part of the cylinder to form a homogeneous mixture, the fuel injection valve mainly produces a fan-shaped fuel spray spreading in the width direction. The fan-shaped fuel spray is injected into the entire cylinder in the latter half of the intake stroke so that the thickness-direction center plane is substantially parallel to the cylinder center axis, and the upper portion of the fan-shaped fuel spray is lower than the lower portion of the fan-shaped fuel spray. An in-cylinder injection spark ignition internal combustion engine characterized in that the penetration force is weakened. 前記燃料噴射弁は、前記扇状燃料噴霧を噴射するために互いに所定扇夾角で対向する上壁及び下壁を有するスリット状の噴孔を具備し、前記噴孔は前記燃料噴射弁内の燃料溜と連通し、前記噴孔の厚さ方向に垂直な各断面において、前記燃料溜と前記噴孔との間の境界は円弧形状であり、前記各断面において、前記上壁及び前記下壁の延長線の交点は、前記各断面における前記円弧形状の中心に対して偏倚し、前記交点までの前記上壁の延長線は前記交点までの前記下壁の延長線より長くされることを特徴とする請求項1に記載の筒内噴射式火花点火内燃機関。   The fuel injection valve includes a slit-shaped injection hole having an upper wall and a lower wall facing each other at a predetermined fan angle for injecting the fan-shaped fuel spray, and the injection hole is a fuel reservoir in the fuel injection valve. In each cross section perpendicular to the thickness direction of the nozzle hole, the boundary between the fuel reservoir and the nozzle hole has an arc shape, and the upper wall and the lower wall are extended in each cross section. The intersection of the lines is biased with respect to the center of the arc shape in each cross section, and the extension line of the upper wall to the intersection is longer than the extension line of the lower wall to the intersection. The in-cylinder injection spark ignition internal combustion engine according to claim 1. 前記燃料噴射弁は、前記扇状燃料噴霧を噴射するために上下方向に配列された多数の小径噴孔を具備し、上側の小径噴孔群の孔径が下側の小径噴孔群の孔径より小さいか、又は、上側の小径噴孔群の孔数が下側の小径噴孔群の孔数より少ないことを特徴とする請求項1に記載の筒内噴射式火花点火内燃機関。   The fuel injection valve includes a large number of small diameter nozzle holes arranged in the vertical direction to inject the fan-shaped fuel spray, and the hole diameter of the upper small diameter nozzle hole group is smaller than the hole diameter of the lower small diameter nozzle hole group. The in-cylinder injection spark ignition internal combustion engine according to claim 1, wherein the number of holes in the upper small-diameter hole group is smaller than the number of holes in the lower small-diameter hole group.
JP2003372324A 2003-10-31 2003-10-31 In-cylinder injection spark ignition internal combustion engine Expired - Lifetime JP4103775B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2003372324A JP4103775B2 (en) 2003-10-31 2003-10-31 In-cylinder injection spark ignition internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2003372324A JP4103775B2 (en) 2003-10-31 2003-10-31 In-cylinder injection spark ignition internal combustion engine

Publications (2)

Publication Number Publication Date
JP2005133679A true JP2005133679A (en) 2005-05-26
JP4103775B2 JP4103775B2 (en) 2008-06-18

Family

ID=34648739

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003372324A Expired - Lifetime JP4103775B2 (en) 2003-10-31 2003-10-31 In-cylinder injection spark ignition internal combustion engine

Country Status (1)

Country Link
JP (1) JP4103775B2 (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08177499A (en) * 1994-12-20 1996-07-09 Nissan Motor Co Ltd Direct injection and spark-ignition type internal combustion engine
JPH11200865A (en) * 1998-01-05 1999-07-27 Kawasaki Heavy Ind Ltd Fuel supply method of gasoline engine
JPH11280611A (en) * 1998-03-26 1999-10-15 Toyota Motor Corp Fuel injection valve for interal combustion engine
JP2000314358A (en) * 1999-04-30 2000-11-14 Nissan Motor Co Ltd Fuel injection valve in direct injection spark ignition internal combustion engine
JP2001027170A (en) * 1999-07-12 2001-01-30 Nissan Motor Co Ltd Direct injection type gasoline engine, and fuel injection valve

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08177499A (en) * 1994-12-20 1996-07-09 Nissan Motor Co Ltd Direct injection and spark-ignition type internal combustion engine
JPH11200865A (en) * 1998-01-05 1999-07-27 Kawasaki Heavy Ind Ltd Fuel supply method of gasoline engine
JPH11280611A (en) * 1998-03-26 1999-10-15 Toyota Motor Corp Fuel injection valve for interal combustion engine
JP2000314358A (en) * 1999-04-30 2000-11-14 Nissan Motor Co Ltd Fuel injection valve in direct injection spark ignition internal combustion engine
JP2001027170A (en) * 1999-07-12 2001-01-30 Nissan Motor Co Ltd Direct injection type gasoline engine, and fuel injection valve

Also Published As

Publication number Publication date
JP4103775B2 (en) 2008-06-18

Similar Documents

Publication Publication Date Title
JP4342481B2 (en) In-cylinder injection spark ignition internal combustion engine
JP4722129B2 (en) In-cylinder injection spark ignition internal combustion engine
JP4888330B2 (en) Direct injection internal combustion engine
US7740002B2 (en) Fuel injector
JP2007315276A (en) Multi-hole type injector
JP2007231852A (en) Fuel injection device
US9970350B2 (en) Opposed piston engine with pistons having conical recesses therein
JP2007291934A (en) Multi-hole injector
JP4306710B2 (en) Fuel injection nozzle
JP7226639B2 (en) Pre-chamber spark ignition engine
JP2007327464A (en) Direct injection type spark ignition internal combustion engine
JP5115267B2 (en) In-cylinder direct injection spark ignition internal combustion engine
US6877477B2 (en) Fuel injection system
JP2007315279A (en) Multi-hole type injector
JP4103775B2 (en) In-cylinder injection spark ignition internal combustion engine
JP2005155624A (en) Fuel injection system
JP2009121251A (en) Cylinder injection type spark ignition internal combustion engine
JP2008267155A (en) Fuel injector for diesel engine
JP6213285B2 (en) Fuel injection valve
JP5071090B2 (en) Diesel engine fuel injection method and diesel engine
JP2007321619A (en) Cylinder injection type spark ignition internal combustion engine
JP4582049B2 (en) In-cylinder injection spark ignition internal combustion engine
JP5217402B2 (en) Fuel injection valve
JP2007285205A (en) Cylinder injection type spark ignition internal combustion engine
JP2007146680A (en) Cylinder injection type spark ignition internal combustion engine

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20060310

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20071213

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20071218

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20080205

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: 20080304

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20080317

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

Free format text: PAYMENT UNTIL: 20110404

Year of fee payment: 3

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

Free format text: PAYMENT UNTIL: 20120404

Year of fee payment: 4

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

Free format text: PAYMENT UNTIL: 20130404

Year of fee payment: 5

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

Free format text: PAYMENT UNTIL: 20140404

Year of fee payment: 6