JPH04224231A - Inner cylinder injection type internal combustion engine - Google Patents

Inner cylinder injection type internal combustion engine

Info

Publication number
JPH04224231A
JPH04224231A JP40681790A JP40681790A JPH04224231A JP H04224231 A JPH04224231 A JP H04224231A JP 40681790 A JP40681790 A JP 40681790A JP 40681790 A JP40681790 A JP 40681790A JP H04224231 A JPH04224231 A JP H04224231A
Authority
JP
Japan
Prior art keywords
groove
air
fuel
valve
fuel spray
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
JP40681790A
Other languages
Japanese (ja)
Inventor
Hiroshi Nomura
啓 野村
Norihiko Nakamura
徳彦 中村
Kenichi Nomura
野村 憲一
Tatsuo Kobayashi
辰夫 小林
Hiroaki Nihei
裕昭 仁平
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 JP40681790A priority Critical patent/JPH04224231A/en
Priority to US07/736,692 priority patent/US5115774A/en
Priority to DE91112766T priority patent/DE69100803T2/en
Priority to EP91112766A priority patent/EP0496029B1/en
Publication of JPH04224231A publication Critical patent/JPH04224231A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/24Cylinder heads
    • F02F1/42Shape or arrangement of intake or exhaust channels in cylinder heads
    • F02F1/4214Shape or arrangement of intake or exhaust channels in cylinder heads specially adapted for four or more valves per 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
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • 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
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • F02F3/26Pistons  having combustion chamber in piston head

Landscapes

  • 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)

Abstract

PURPOSE:To collect air-fuel mixture around an ignition plug in a two-cycle engine adopting an air blast valve. CONSTITUTION:A groove 20 is formed on a top face of a piston 2. Fuel is injected together with compressed air from an air blast valve 14 into the groove 20 in a latter half period of a compression process. A horizontal width of the groove 20 in a direction perpendicular to the fuel injection direction is narrower than the vertical width of the groove 20. Both side wall surfaces 20b of the groove 20 which determine the horizontal width thereof are arranged a little outer than an outer periphery of atomized fuel F. The atomized fuel F is prevented from diffusing in a transverse direction by means of the both side wall surfaces 20b of the groove. Air-fuel mixture is thus collected in the engine groove 20 and below an ignition plug 10.

Description

【発明の詳細な説明】[Detailed description of the invention]

【0001】0001

【産業上の利用分野】本発明は筒内噴射式内燃機関に関
する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a direct injection internal combustion engine.

【0002】0002

【従来の技術】ピストン頂面上に凹溝を形成すると共に
燃料噴射弁から凹溝内に向けて燃料を噴射し、燃焼室内
にシリンダ軸線回りの旋回流を発生させてこの旋回流に
より点火栓の周りに着火可能な混合気を形成するように
した筒内噴射式内燃機関が公知である(実開平1−12
4042号公報参照)。
[Prior Art] A concave groove is formed on the top surface of the piston, and fuel is injected from the fuel injection valve into the concave groove to generate a swirling flow around the cylinder axis within the combustion chamber. A direct-injection internal combustion engine is known in which an ignitable air-fuel mixture is formed around the
(See Publication No. 4042).

【0003】0003

【発明が解決しようとする課題】しかしながらこの筒内
噴射式内燃機関ではシリンダ軸線周りの旋回流を発生さ
せることが必須の要件であるのでシリンダ軸線回りの旋
回流を発生させない場合にはもはやこの噴射方法を採用
することができない。また、旋回流の強さは機関の運転
状態により変化するので点火栓周りの混合気の形成を全
面的に旋回流に依存しているとあらゆる機関の運転状態
に対して最適な混合気を点火栓の周りに形成するのは困
難であるという問題がある。
However, in this direct injection internal combustion engine, it is essential to generate a swirling flow around the cylinder axis, so if the swirling flow around the cylinder axis is not generated, this injection method cannot be adopted. In addition, the strength of the swirling flow changes depending on the operating condition of the engine, so if the formation of the mixture around the spark plug is completely dependent on the swirling flow, the optimum mixture will be ignited for every operating condition of the engine. The problem is that it is difficult to form around the stopper.

【0004】0004

【課題を解決するための手段】上記問題点を解決するた
めに本発明によればシリンダヘッド内壁面の中心部に点
火栓を配置し、圧縮空気によって燃料を噴射するエアブ
ラスト弁をシリンダヘッド内壁面の周縁部に配置し、点
火栓の下方からエアブラスト弁の下方まで延びる凹溝を
ピストン頂面上に形成してエアブラスト弁から噴射され
た燃料噴霧が凹溝の底壁面に沿いつつ点火栓下方の凹溝
内に向かうようにエアブラスト弁から凹溝内に向けて燃
料噴霧を噴射し、燃料噴霧軸線に対して直角方向の凹溝
の横巾を燃料噴霧軸線方向の凹溝の縦巾よりも狹くする
と共にこの横巾を画定する凹溝の両側壁面を燃料噴霧の
外側面よりもわずかばかり外側に位置せしめている。
[Means for Solving the Problems] In order to solve the above problems, according to the present invention, an ignition plug is disposed at the center of the inner wall surface of the cylinder head, and an air blast valve for injecting fuel with compressed air is installed in the cylinder head. A concave groove is formed on the top surface of the piston, which is placed on the peripheral edge of the wall and extends from below the ignition plug to below the air blast valve, so that the fuel spray injected from the air blast valve ignites while following the bottom wall of the concave groove. Fuel spray is injected from the air blast valve into the groove below the plug, and the width of the groove in the direction perpendicular to the fuel spray axis is the vertical width of the groove in the direction of the fuel spray axis. It is made narrower than the width, and both side wall surfaces of the groove defining the width are positioned slightly outside the outer surface of the fuel spray.

【0005】[0005]

【作用】エアブラスト弁を用いることによって着火可能
な燃料噴霧が凹溝内に形成される。凹溝の横巾を画定す
る凹溝の両側壁面が燃料噴霧の外側面よりもわずかばか
り外側に位置せしめられているので燃料噴霧は横方向に
広がることなく点火栓下方の凹溝内に導びかれ、この燃
料噴霧が点火栓によって着火せしめられる。
Operation: By using the air blast valve, an ignitable fuel spray is formed in the groove. Since both side wall surfaces of the groove that define the width of the groove are positioned slightly outside the outer surface of the fuel spray, the fuel spray is guided into the groove below the ignition plug without spreading laterally. This fuel spray is then ignited by a spark plug.

【0006】[0006]

【実施例】図1および図2を参照すると、1はシリンダ
ブロック、2はシリンダブロック1内で往復動するピス
トン、3はシリンダブロック1上に固定されたシリンダ
ヘッド、4はシリンダヘッド3の内壁面3aとピストン
2の頂面間に形成された燃焼室を夫々示す。シリンダヘ
ッド内壁面3a上には凹溝5が形成され、この凹溝5の
底壁面をなすシリンダヘッド内壁面部分3b上に一対の
給気弁6が配置される。一方、凹溝5を除くシリンダヘ
ッド内壁面部分3cは傾斜したほぼ平坦をなし、このシ
リンダヘッド内壁面部分3c上に一対の排気弁7が配置
される。シリンダヘッド内壁面部分3bとシリンダヘッ
ド内壁面部分3cは凹溝5の周壁8を介して互いに接続
されている。この凹溝周壁8は給気弁6の周縁部に極め
て近接配置されかつ給気弁6の周縁部に沿って円弧状に
延びる一対のマスク壁8aと、給気弁6間に位置する新
気ガイド壁8bと、シリンダヘッド内壁面3aの周壁と
給気弁6間に位置する一対の新気ガイド壁8cとにより
構成される。各マスク壁8aは最大リフト位置にある給
気弁6よりも下方まで燃焼室4に向けて延びており、従
って排気弁7側に位置する給気弁6周縁部と弁座9間の
開口は給気弁6の開弁期間全体に亙ってマスク壁8aに
より閉鎖されることになる。また、各新気ガイド壁8b
,8cはほぼ同一平面内に位置しており、更にこれらの
新気ガイド壁8b,8cは両給気弁6の中心を結ぶ線に
対してほぼ平行に延びている。点火栓10はシリンダヘ
ッド内壁面3aの中心に位置するようにシリンダヘッド
内壁面部分3c上に配置されている。一方、排気弁7に
対しては排気弁7と弁座11間の開口を覆うマスク壁が
設けられておらず、従って排気弁7が開弁すると排気弁
7と弁座11間に形成される開口はその全体が燃焼室4
内に開口することになる。
[Embodiment] Referring to FIGS. 1 and 2, 1 is a cylinder block, 2 is a piston that reciprocates within the cylinder block 1, 3 is a cylinder head fixed on the cylinder block 1, and 4 is an inner part of the cylinder head 3. The combustion chambers formed between the wall surface 3a and the top surface of the piston 2 are shown. A recessed groove 5 is formed on the cylinder head inner wall surface 3a, and a pair of air supply valves 6 are arranged on the cylinder head inner wall surface portion 3b forming the bottom wall surface of the recessed groove 5. On the other hand, the cylinder head inner wall surface portion 3c excluding the groove 5 is inclined and substantially flat, and a pair of exhaust valves 7 are arranged on this cylinder head inner wall surface portion 3c. The cylinder head inner wall surface portion 3b and the cylinder head inner wall surface portion 3c are connected to each other via the peripheral wall 8 of the groove 5. This concave groove peripheral wall 8 is arranged very close to the peripheral edge of the air supply valve 6 and extends in an arc shape along the peripheral edge of the air supply valve 6. It is constituted by a guide wall 8b and a pair of fresh air guide walls 8c located between the peripheral wall of the cylinder head inner wall surface 3a and the air supply valve 6. Each mask wall 8a extends toward the combustion chamber 4 below the intake valve 6 at the maximum lift position, and therefore the opening between the peripheral edge of the intake valve 6 and the valve seat 9 located on the exhaust valve 7 side is The air supply valve 6 is closed by the mask wall 8a throughout its opening period. In addition, each fresh air guide wall 8b
, 8c are located substantially in the same plane, and furthermore, these fresh air guide walls 8b, 8c extend substantially parallel to a line connecting the centers of both air supply valves 6. The ignition plug 10 is arranged on the cylinder head inner wall surface portion 3c so as to be located at the center of the cylinder head inner wall surface 3a. On the other hand, the exhaust valve 7 is not provided with a mask wall that covers the opening between the exhaust valve 7 and the valve seat 11. Therefore, when the exhaust valve 7 opens, a mask wall is formed between the exhaust valve 7 and the valve seat 11. The entire opening is the combustion chamber 4
It will open inward.

【0007】シリンダヘッド3内には給気弁6に対して
給気ポート12が形成され、排気弁7に対して排気ポー
ト13が形成される。一方、両給気弁6の間のシリンダ
ヘッド内壁面3aの周縁部にはエアブラスト弁14が配
置される。このエアブラスト弁14はそのハウジング1
5内に形成されかつ図示しない圧縮空気源に接続された
圧縮空気通路16と、圧縮空気通路16内に配置された
燃料噴射弁17と、図示しないソレノイドにより駆動さ
れて燃焼室4内に配置されたノズル口18の開閉作用を
行う弁体19とを具備する。圧縮空気通路16内は常時
圧縮空気で満たされており、圧縮空気通路16内の圧縮
空気中に燃料噴射弁17から燃料が噴射される。次いで
弁体19がノズル口18を開口せしめるとノズル口18
から燃料が圧縮空気と共に燃焼室4内に噴射される。
[0007] In the cylinder head 3, an air intake port 12 is formed for the air intake valve 6, and an exhaust port 13 is formed for the exhaust valve 7. On the other hand, an air blast valve 14 is disposed at the peripheral edge of the cylinder head inner wall surface 3 a between both the air supply valves 6 . This air blast valve 14 has its housing 1
A compressed air passage 16 formed in the combustion chamber 5 and connected to a compressed air source (not shown), a fuel injection valve 17 arranged in the compressed air passage 16, and a fuel injection valve 17 arranged in the combustion chamber 4 driven by a solenoid (not shown). and a valve body 19 that opens and closes the nozzle port 18. The compressed air passage 16 is always filled with compressed air, and fuel is injected from the fuel injection valve 17 into the compressed air within the compressed air passage 16. Next, when the valve body 19 opens the nozzle port 18, the nozzle port 18 opens.
Fuel is injected into the combustion chamber 4 together with compressed air.

【0008】図1および図3に示されるようにピストン
2の頂面上には点火栓10の下方からエアブラスト弁1
4の先端部の下方まで延びる凹溝20が形成される。図
1および図3に示す実施例ではこの凹溝20は点火栓1
0とエアブラスト弁14とを含む垂直平面K−Kに対し
て対称的な形状を有する。図4に示されるように図1か
ら図3に示す実施例では排気弁7が給気弁6よりも先に
開弁し、排気弁7が給気弁6よりも先に開弁する。また
、図4においてIは燃料噴射時期を示している。従って
図1および図3においてFで示されるように圧縮行程の
後半にエアブラスト弁14のノズル口18から、圧縮空
気と共に燃料が円錐状をなす燃料噴霧の形で噴射される
。このとき燃料噴霧Fはノズル口18から垂直平面K−
Kに沿って噴射されしかも凹溝20の底壁面20aに沿
いつつ点火栓10下方の凹溝20内に向けて噴射される
。図3からわかるように燃料噴霧Fの軸線に対して直角
方向、即ち垂直平面K−Kに対して直角方向の凹溝20
の横巾Sは燃料噴霧Fの軸線方向、即ち垂直平面K−K
に沿う方向の凹溝20の縦巾Lよりも狹く形成されてい
る。また、凹溝20の横巾Sを画定する凹溝20の両側
壁面20bはほぼ垂直をなしており、これら両側壁面2
0bは燃料噴霧Fの外側面よりもわずかばかり外方に位
置せしめられている。また、図3に示されるようにエア
ブラスト弁14と反対側に位置する凹溝20の上縁部2
0cの輪郭形状は円弧状をなしており、エアブラスト弁
14と反対側において凹溝20の底壁面20aから点火
栓10に向けて立ち上る凹溝20の端面上には図1に示
されるように上縁部20cに対しエアブラスト弁14か
ら離れる方向に後退した断面円弧状の凹部20dが形成
される。一方、図1に示されるように上縁部20cに関
して凹溝20と反対側のピストン2の頂面部分2aは傾
斜したほぼ平坦面から形成され、ピストン2が上死点に
達するとシリンダヘッド内壁面部分3cとピストン頂面
部分2a間にはスキッシュエリアが形成される。
As shown in FIGS. 1 and 3, an air blast valve 1 is placed on the top surface of the piston 2 from below the ignition plug 10.
A concave groove 20 is formed that extends to below the tip of 4. In the embodiment shown in FIGS. 1 and 3, this groove 20 is
0 and the air blast valve 14. As shown in FIG. 4, in the embodiment shown in FIGS. 1 to 3, the exhaust valve 7 opens before the intake valve 6, and the exhaust valve 7 opens before the intake valve 6. Further, in FIG. 4, I indicates the fuel injection timing. Therefore, as shown by F in FIGS. 1 and 3, fuel is injected together with compressed air in the form of a conical fuel spray from the nozzle port 18 of the air blast valve 14 in the latter half of the compression stroke. At this time, the fuel spray F flows from the nozzle port 18 to the vertical plane K-
K and is injected into the groove 20 below the ignition plug 10 along the bottom wall surface 20a of the groove 20. As can be seen from FIG. 3, the groove 20 is perpendicular to the axis of the fuel spray F, that is, perpendicular to the vertical plane K-K.
The width S is in the axial direction of the fuel spray F, that is, in the vertical plane K-K.
It is formed narrower than the vertical width L of the groove 20 in the direction along the direction. Further, both side wall surfaces 20b of the groove 20 that define the width S of the groove 20 are substantially vertical, and these side wall surfaces 20b are substantially vertical.
0b is positioned slightly outward from the outer surface of the fuel spray F. Further, as shown in FIG. 3, the upper edge 2 of the groove 20 located on the opposite side from the air blast valve 14
The outline shape of 0c is an arc shape, and on the end face of the groove 20 rising from the bottom wall surface 20a of the groove 20 toward the ignition plug 10 on the opposite side from the air blast valve 14, as shown in FIG. A recessed portion 20d having an arc-shaped cross section is formed with respect to the upper edge portion 20c, receding in a direction away from the air blast valve 14. On the other hand, as shown in FIG. 1, the top surface portion 2a of the piston 2 on the opposite side of the groove 20 with respect to the upper edge portion 20c is formed as an inclined, substantially flat surface, and when the piston 2 reaches the top dead center, the inside of the cylinder head is A squish area is formed between the wall surface portion 3c and the piston top surface portion 2a.

【0009】次に図1、図3および図5を参照しつつ混
合気の形成方法について説明する。図5に示すように給
気弁6および排気弁7が開弁すると給気弁6を介して燃
焼室4内に空気が流入する。このとき、排気弁7側の給
気弁6の開口はマスク壁8aによって覆われているので
空気はマスク壁8aと反対側の給気弁6の開口から燃焼
室4内に流入する。この空気は矢印Wで示すように給気
弁6下方のシリンダボア内壁面に沿って下降する。次い
でこの空気Wの一部W1 は凹溝20内に流入し、斯く
してこの空気W1 によって凹溝20が掃気される。一
方、空気Wの残りの部分W2 はピストン2の頂面に沿
い進んで排気弁7下方のシリンダボア内壁面に沿い上昇
し、斯くして空気W2 は燃焼室4内をループ状に流れ
ることになる。このループ状に流れる空気W2 によっ
て燃焼室4内の既燃ガスが排気弁7を介して排出され、
更にこのループ状に流れる空気W2 によって燃焼室4
内には垂直面内で旋回する旋回流Xが発生せしめられる
。次いでピストン2が下死点BDCを過ぎて上昇を開始
し、給気弁6および排気弁7が開弁して圧縮行程末期に
なると図1および図3に示されるようにエアブラスト弁
14から燃料噴霧Fが凹溝20の底壁面20aに沿いつ
つ点火栓10下方の凹溝20内に向けて噴射される。
Next, a method for forming an air-fuel mixture will be explained with reference to FIGS. 1, 3, and 5. As shown in FIG. 5, when the intake valve 6 and the exhaust valve 7 are opened, air flows into the combustion chamber 4 via the intake valve 6. At this time, since the opening of the intake valve 6 on the side of the exhaust valve 7 is covered by the mask wall 8a, air flows into the combustion chamber 4 from the opening of the intake valve 6 on the side opposite to the mask wall 8a. This air descends along the inner wall surface of the cylinder bore below the air supply valve 6 as shown by arrow W. Then, a portion W1 of this air W flows into the groove 20, and the groove 20 is thus scavenged by this air W1. On the other hand, the remaining portion W2 of the air W travels along the top surface of the piston 2 and rises along the inner wall surface of the cylinder bore below the exhaust valve 7, so that the air W2 flows in a loop inside the combustion chamber 4. . The air W2 flowing in a loop causes the burnt gas in the combustion chamber 4 to be discharged via the exhaust valve 7.
Furthermore, the air W2 flowing in this loop shape causes the combustion chamber 4 to
A swirling flow X that swirls in a vertical plane is generated inside the tube. Next, the piston 2 passes the bottom dead center BDC and begins to rise, and the intake valve 6 and the exhaust valve 7 open to reach the end of the compression stroke. As shown in FIGS. 1 and 3, fuel is discharged from the air blast valve 14. The spray F is injected into the groove 20 below the ignition plug 10 along the bottom wall surface 20a of the groove 20.

【0010】圧縮空気を用いて燃料を噴射すると燃料が
良好に微粒化せしめられるので燃料噴霧Fはただちに着
火可能な状態となるがこの燃料噴霧Fはガス状であるた
めに燃焼室4内全体に広がりやすくなる。ところが燃料
噴霧Fが燃焼室4内全体に広がると特に燃料噴射量の少
ない低負荷運転時には点火栓10の周りに比較的濃い混
合気を集めることができないので良好な着火が得られな
いことになる。しかしながら図1および図3に示す実施
例では前述したように凹溝20の横巾Sを画定する凹溝
20の両側壁面20bが円錐状をなす燃料噴霧Fの外側
面よりもわずかばかり外方に位置せしめられている。従
って燃料噴霧Fは凹溝20の両側壁面20bにより挾ま
れたような形となり、斯くして燃料噴霧Fが横方向に拡
散されるのが阻止される。従って、点火栓10下方の凹
溝20内に混合気が集まることになり、この混合気が点
火栓10によって着火せしめられる。斯くして点火栓1
0による良好な着火作用を確保できることになる。また
、前述したように凹溝20の端面に形成された凹部20
dはエアブラスト弁14と反対側に向けて凹状をなして
いるので燃料噴霧Fはこの凹部20dによって排気弁7
下方の燃焼室4内に拡散するのが阻止される。従ってこ
のような凹部20dを設けることによって更に点火栓1
0下方の凹溝20内に混合気を集めることができるよう
になる。また、図5に示すように燃焼室4内には旋回流
Xが発生せしめられ、この旋回流Xによって燃料噴霧F
の進行方向が凹溝20内に向けて偏向せしめられる。従
ってこの旋回流Xによっても混合気の拡散が阻止される
ことになる。
When the fuel is injected using compressed air, the fuel is atomized well, so the fuel spray F becomes ready to be ignited immediately. However, since the fuel spray F is gaseous, it spreads throughout the combustion chamber 4. It becomes easier to spread. However, if the fuel spray F spreads throughout the combustion chamber 4, a relatively rich mixture cannot be collected around the spark plug 10, especially during low-load operation with a small amount of fuel injection, and good ignition cannot be achieved. . However, in the embodiment shown in FIGS. 1 and 3, as described above, both side wall surfaces 20b of the groove 20 defining the width S of the groove 20 are slightly outward from the outer surface of the conical fuel spray F. It is located. Therefore, the fuel spray F is shaped as if it is sandwiched between both side wall surfaces 20b of the groove 20, and thus the fuel spray F is prevented from being spread in the lateral direction. Therefore, the air-fuel mixture gathers in the groove 20 below the ignition plug 10, and this air-fuel mixture is ignited by the ignition plug 10. Thus the spark plug 1
This means that a good ignition effect can be ensured due to the zero. Further, as described above, the recess 20 formed on the end face of the recess groove 20
d has a concave shape toward the side opposite to the air blast valve 14, so the fuel spray F flows through the concave portion 20d to the exhaust valve 7.
Diffusion into the combustion chamber 4 below is prevented. Therefore, by providing such a recess 20d, the spark plug 1 can be further tightened.
The air-fuel mixture can now be collected in the groove 20 below zero. Further, as shown in FIG. 5, a swirling flow X is generated in the combustion chamber 4, and this swirling flow X causes fuel spray F.
The traveling direction of the groove 20 is deflected toward the inside of the groove 20. Therefore, this swirling flow X also prevents the mixture from diffusing.

【0011】[0011]

【発明の効果】エアブラスト弁を用いた場合において燃
料噴射量が少ない機関低負荷運転時であっても点火栓の
周りに着火可能な混合気を集めることができ、斯くして
良好な着火を得ることができる。
[Effects of the Invention] When an air blast valve is used, even when the engine is operating at low load with a small amount of fuel injection, it is possible to collect an ignitable air-fuel mixture around the spark plug, thus ensuring good ignition. Obtainable.

【図面の簡単な説明】[Brief explanation of the drawing]

【図1】2サイクル内燃機関の側面断面図である。FIG. 1 is a side sectional view of a two-stroke internal combustion engine.

【図2】シリンダヘッドの底面図である。FIG. 2 is a bottom view of the cylinder head.

【図3】ピストンの平面図である。FIG. 3 is a plan view of the piston.

【図4】給排気弁の開弁時期および燃料噴射時期を示す
線図である。
FIG. 4 is a diagram showing the opening timing of the supply and exhaust valves and the fuel injection timing.

【図5】給排気弁が開弁したところを示す2サイクル内
燃機関の側面断面図である。
FIG. 5 is a side cross-sectional view of the two-stroke internal combustion engine showing the supply and exhaust valves opened.

【符合の説明】[Explanation of sign]

6…給気弁 7…排気弁 8a…マスク壁 10…点火栓 14…エアブラスト弁 20…凹溝 6...Air supply valve 7...Exhaust valve 8a...Mask wall 10...Spark plug 14...Air blast valve 20...concave groove

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】  シリンダヘッド内壁面の中心部に点火
栓を配置し、圧縮空気によって燃料を噴射するエアブラ
スト弁をシリンダヘッド内壁面の周縁部に配置し、点火
栓の下方からエアブラスト弁の下方まで延びる凹溝をピ
ストン頂面上に形成してエアブラスト弁から噴射された
燃料噴霧が凹溝の底壁面に沿いつつ点火栓下方の凹溝内
に向かうようにエアブラスト弁から凹溝内に向けて燃料
噴霧を噴射し、燃料噴霧軸線に対して直角方向の凹溝の
横巾を燃料噴霧軸線方向の凹溝の縦巾よりも狹くすると
共に該横巾を画定する凹溝の両側壁面を燃料噴霧の外側
面よりもわずかばかり外側に位置せしめた筒内噴射式内
燃機関。
Claim 1: An ignition plug is arranged in the center of the inner wall of the cylinder head, and an air blast valve that injects fuel using compressed air is arranged at the periphery of the inner wall of the cylinder head. A concave groove extending downward is formed on the top surface of the piston so that the fuel spray injected from the air blast valve is directed from the air blast valve into the concave groove below the ignition plug while following the bottom wall of the concave groove. The width of the groove in the direction perpendicular to the fuel spray axis is narrower than the vertical width of the groove in the direction of the fuel spray axis, and both sides of the groove defining the width are A direct-injection internal combustion engine in which the wall surface is located slightly outside the outer surface of the fuel spray.
JP40681790A 1990-12-26 1990-12-26 Inner cylinder injection type internal combustion engine Pending JPH04224231A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP40681790A JPH04224231A (en) 1990-12-26 1990-12-26 Inner cylinder injection type internal combustion engine
US07/736,692 US5115774A (en) 1990-12-26 1991-07-26 Internal combustion engine
DE91112766T DE69100803T2 (en) 1990-12-26 1991-07-30 Internal combustion engine.
EP91112766A EP0496029B1 (en) 1990-12-26 1991-07-30 An internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP40681790A JPH04224231A (en) 1990-12-26 1990-12-26 Inner cylinder injection type internal combustion engine

Publications (1)

Publication Number Publication Date
JPH04224231A true JPH04224231A (en) 1992-08-13

Family

ID=18516442

Family Applications (1)

Application Number Title Priority Date Filing Date
JP40681790A Pending JPH04224231A (en) 1990-12-26 1990-12-26 Inner cylinder injection type internal combustion engine

Country Status (1)

Country Link
JP (1) JPH04224231A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996030632A1 (en) * 1995-03-28 1996-10-03 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Cylinder injection type internal combustion engine
WO1996030633A1 (en) * 1995-03-28 1996-10-03 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Cylinder injection type internal combustion engine
US5806482A (en) * 1995-03-28 1998-09-15 Mitsubishi Jidosha Kogyo Kabushiki Kaisha In-cylinder injection internal combustion engine
EP0881368A1 (en) * 1997-05-29 1998-12-02 Renault Direct injection type engine with controlled ignition
JPH11182251A (en) * 1997-12-22 1999-07-06 Nissan Motor Co Ltd Piston for in-cylinder injection type internal combustion engine
EP0875670A3 (en) * 1997-04-30 1999-07-14 Yamaha Hatsudoki Kabushiki Kaisha Direct injection type internal combustion engine
EP1063398A3 (en) * 1997-05-20 2001-01-03 Nissan Motor Co., Ltd. Piston for a direct injection gasoline engine
KR100365114B1 (en) * 1996-11-22 2003-03-15 기아자동차주식회사 Piston head shape structure of direct injection gasoline engine
JP2016121567A (en) * 2014-12-24 2016-07-07 三菱自動車工業株式会社 In-cylinder injection engine

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU702939B2 (en) * 1995-03-28 1999-03-11 Mitsubishi Jidosha Kogyo Kabushiki Kaisha In-cylinder injection internal combustion engine
US5711269A (en) * 1995-03-28 1998-01-27 Mitsubishi Jidosha Kogyo Kabushiki Kaisha In-cylinder injection internal combustion engine
US5806482A (en) * 1995-03-28 1998-09-15 Mitsubishi Jidosha Kogyo Kabushiki Kaisha In-cylinder injection internal combustion engine
WO1996030633A1 (en) * 1995-03-28 1996-10-03 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Cylinder injection type internal combustion engine
WO1996030632A1 (en) * 1995-03-28 1996-10-03 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Cylinder injection type internal combustion engine
CN1083527C (en) * 1995-03-28 2002-04-24 三菱自动车工业株式会社 Cylinder oil injection type IC engine
KR100365114B1 (en) * 1996-11-22 2003-03-15 기아자동차주식회사 Piston head shape structure of direct injection gasoline engine
EP0875670A3 (en) * 1997-04-30 1999-07-14 Yamaha Hatsudoki Kabushiki Kaisha Direct injection type internal combustion engine
US6116211A (en) * 1997-04-30 2000-09-12 Yamaha Hatsudoki Kabushiki Kaisha Injection control for direct injected engine
US6035822A (en) * 1997-04-30 2000-03-14 Yamaha Hatsudoki Kabushiki Kaisha Combustion chamber for direct injected engine
EP1063398A3 (en) * 1997-05-20 2001-01-03 Nissan Motor Co., Ltd. Piston for a direct injection gasoline engine
EP0881368A1 (en) * 1997-05-29 1998-12-02 Renault Direct injection type engine with controlled ignition
FR2763995A1 (en) * 1997-05-29 1998-12-04 Renault DIRECT INJECTION ENGINE AND CONTROLLED IGNITION
JPH11182251A (en) * 1997-12-22 1999-07-06 Nissan Motor Co Ltd Piston for in-cylinder injection type internal combustion engine
JP2016121567A (en) * 2014-12-24 2016-07-07 三菱自動車工業株式会社 In-cylinder injection engine

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