JP3301013B2 - Spark ignition combustion method - Google Patents

Spark ignition combustion method

Info

Publication number
JP3301013B2
JP3301013B2 JP34527995A JP34527995A JP3301013B2 JP 3301013 B2 JP3301013 B2 JP 3301013B2 JP 34527995 A JP34527995 A JP 34527995A JP 34527995 A JP34527995 A JP 34527995A JP 3301013 B2 JP3301013 B2 JP 3301013B2
Authority
JP
Japan
Prior art keywords
cavity
fuel
spray
cylinder
spark plug
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
Application number
JP34527995A
Other languages
Japanese (ja)
Other versions
JPH09158736A (en
Inventor
誠 小池
哲典 鈴置
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
Toyota Central R&D Labs Inc
Original Assignee
Toyota Motor Corp
Toyota Central R&D Labs Inc
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, Toyota Central R&D Labs Inc filed Critical Toyota Motor Corp
Priority to JP34527995A priority Critical patent/JP3301013B2/en
Publication of JPH09158736A publication Critical patent/JPH09158736A/en
Application granted granted Critical
Publication of JP3301013B2 publication Critical patent/JP3301013B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02F3/00Pistons 
    • F02F3/26Pistons  having combustion chamber in piston head
    • 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
    • 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

  • 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)
  • Fuel-Injection Apparatus (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Description

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

【0001】[0001]

【発明の属する技術分野】本発明は、シリンダ内に空気
を吸入し、ピストンにより吸入空気を圧縮するととも
に、燃料を直接筒内に噴射して点火、燃焼させる火花点
火式燃焼方法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a spark ignition type combustion method in which air is sucked into a cylinder, the intake air is compressed by a piston, and fuel is directly injected into a cylinder to ignite and burn.

【0002】[0002]

【従来の技術】従来の火花点火機関は、キャブレタもし
くは噴射弁により燃料を吸気管に供給し、予め空気と混
合させて、シリンダ内に吸入、点火、燃焼させるのが主
流である。そして、混合気は可燃範囲の濃度に調節され
るため、負荷の調整は吸入空気量を制御する、すなわち
スロットル弁を使うのが普通である。そのため、ガス交
換過程で仕事が必要になり、部分負荷の使用頻度の高
い、例えば自動車用機関などでは燃費が悪い。また、可
燃範囲に調整された混合気の比熱比は小さく熱効率的に
不利である。これに対して、空気を吸入し、燃料を直接
筒内に噴射して点火、燃焼させる方式が従来提案されて
いる(実開平1-173416号)。これは、低負荷では圧縮行
程末期に燃料を噴射し、点火プラグ30に燃料を集めて
燃焼させ、高負荷時には吸気行程で燃料を噴射し、燃料
と空気をよく混合させて点火燃焼させる方式である。こ
の場合、負荷の調整は燃料噴射量のみで行えるため、ガ
ス交換過程での仕事が不要となり、部分負荷においても
燃費がよい。また、空気の比率が高いため、比熱比も大
きく、熱効率が高い。
2. Description of the Related Art In a conventional spark ignition engine, fuel is mainly supplied to an intake pipe by a carburetor or an injection valve, mixed with air in advance, and then sucked, ignited, and burned in a cylinder. Since the mixture is adjusted to a concentration within the flammable range, the load is usually adjusted by controlling the intake air amount, that is, by using a throttle valve. Therefore, work is required in the gas exchange process, and fuel efficiency is poor in a frequently used partial load, for example, in an automobile engine. Further, the specific heat ratio of the air-fuel mixture adjusted to the flammable range is small, which is disadvantageous in terms of thermal efficiency. On the other hand, a system has been proposed in which air is sucked, fuel is directly injected into a cylinder to ignite and burn (Japanese Utility Model Laid-Open No. 1-173416). This is a system in which fuel is injected at the end of the compression stroke at low load, fuel is collected and burned in the ignition plug 30, and fuel is injected during the intake stroke at high load, and fuel and air are mixed well and ignited and burned. is there. In this case, since the load can be adjusted only by the fuel injection amount, the work in the gas exchange process becomes unnecessary, and the fuel efficiency is good even at the partial load. Further, since the ratio of air is high, the specific heat ratio is large, and the thermal efficiency is high.

【0003】しかし、この燃焼法は適正な混合気をつく
ることが難しい。すなわち、低負荷では点火プラグ近傍
に燃料を集めなくてはならないし、高負荷では逆に燃料
を分散させ、点火プラグりに過濃な混合気が集まらな
いようにしなくてはならない。点火プラグりの混合気
が濃いと、失火やプラグのくすぶり、スモーク発生など
の原因となるからである。また、ディーゼルと異なり、
主に火炎伝播で燃焼が進行するため、燃料の素早い気
化、混合が必要である。
[0003] However, it is difficult for this combustion method to produce a proper air-fuel mixture. That is, to a low load must collect fuel to the vicinity of the spark plug, the fuel is dispersed opposite to the high load, it has to be prevented rich Do mixture is gather the Ri spark plug periphery. When the air-fuel mixture of spark plug circumference Ri is a dark, smoldering of misfire or plug, because the cause of such smoke generated. Also, unlike diesel,
Since combustion proceeds mainly by flame propagation, it is necessary to quickly vaporize and mix the fuel.

【0004】[0004]

【発明が解決しようとする課題】本発明は、従来技術の
問題点を解消するもので、燃料を素早く気化、混合させ
て可燃混合気を点火プラグ周りに形成するとともに、低
負荷時の燃焼安定性を確保したまま、高負荷時の燃料分
散性、空気利用率を確保し得る火花点火式燃焼方法を提
供することを目的とする。
SUMMARY OF THE INVENTION The present invention solves the problems of the prior art, in which fuel is quickly vaporized and mixed to form a combustible air-fuel mixture around a spark plug, and combustion stability at low load is reduced. It is an object of the present invention to provide a spark-ignition combustion method capable of securing fuel dispersibility and air utilization under a high load while maintaining performance.

【0005】[0005]

【課題を解決するための手段】請求項1記載の火花点火
式燃焼方法は、シリンダヘッド内壁面の中央部に点火プ
ラグを配置すると共にシリンダヘッド内壁面の周縁部に
燃料噴射弁を配置し、ピストン頂面上に燃料噴射弁の下
方から点火プラグの下方まで延びるキャビティを形成し
た内燃機関の火花点火式燃焼方法において、点火プラグ
側のキャビティの端部においてキャビティの底面から上
方に延びかつ燃料噴射弁とシリンダ中心軸とを含む平面
に対して横方向に円弧状に延びる壁面をキャビティに形
成し、シリンダの中心軸に対し傾斜して配設された燃料
噴射弁の噴口から、噴口とシリンダ中心軸を含む平面に
投影したときは扁平に、噴口とシリンダ中心軸を含む平
面に垂直で、噴口と、噴霧とシリンダ中心軸の交点を含
む平面に投影したときには略扇状の燃料噴霧をその全体
がキャビティの底面に向かうように噴射して燃料噴霧を
キャビティ内に分散させ、次いでキャビティ内に分散し
た燃料噴霧をキャビティ壁面によりキャビティの上方、
内側に向けて巻き上げることにより点火プラグの周りに
集め、次いで点火プラグ周りに集められた燃料噴霧を点
火プラグにより着火するようにしたことを特徴とする。
Means for Solving the Problems] spark ignition combustion method of claim 1, wherein the ignition-flops in a central portion of the inner wall surface of the cylinder head
Place the lug on the inner peripheral surface of the cylinder head
Position the fuel injection valve and place it below the fuel injection valve on the top of the piston.
To form a cavity that extends from
The spark-ignition combustion process of an internal combustion engine, the spark plug
From the bottom of the cavity at the end of the side cavity
Plane extending in the direction and including the fuel injection valve and the cylinder center axis
A wall extending in an arc shape in the lateral direction to the cavity
Form, from the nozzle hole of the fuel injection valve disposed to be inclined with respect to the center axis of the cylinder, so the when projected onto the plane containing the nozzle hole and the cylinder center axis flat, perpendicular to the plane containing the nozzle hole and the cylinder center axis its entirety the sector-shaped fuel spray when projected to a plane including the injection port, the intersection of the spray and the cylinder center axis
Spray toward the bottom of the cavity to spray fuel
Dispersed in the cavity, then dispersed in the cavity
The sprayed fuel is blown above the cavity by the cavity wall,
Around the spark plug by rolling it inwards
And then spray the collected fuel spray around the spark plug.
It is characterized by being ignited by a fire plug .

【0006】[0006]

【0007】[0007]

【0008】[0008]

【0009】[0009]

【0010】[0010]

【発明の作用・効果】上記構成からなる本発明の火花点
火式燃焼方法は、噴射弁から噴出する燃料噴霧を、噴口
とシリンダ中心軸を含む平面に投影したときは扁平に、
噴口とシリンダ中心軸を含む平面に垂直で、噴口と、噴
霧とシリンダ中心軸の交点を含む平面に投影したときに
は略扇状としたことにより、燃料をキャビティ内に素早
く分散させることができる。この扁平扇形の噴霧は周囲
空気を巻き込みやすいので、圧縮行程で燃料を噴射する
と圧縮によって高温となった空気を素早く取り込み、気
化、混合が早い。さらに、噴霧の巻き込んだ空気は噴霧
の運動量を奪うため、噴霧の飛翔速度が低下し、噴霧長
さが短くなる。このため、噴射時期を早くしても燃料が
シリンダ壁を濡らしたりすることはなく、また、逆に遅
くしてもピストン表面を液膜で覆うことがない。一方、
気化、混合したキャビティ内の噴霧はキャビティ壁面に
より案内されて点火プラグ位置に集まり、斯くして少な
い燃料でも効率よく燃焼させることができる。
According to the spark ignition type combustion method of the present invention having the above structure, when the fuel spray ejected from the injection valve is projected onto a plane including the nozzle and the cylinder center axis, the fuel spray becomes flat.
When projected onto a plane perpendicular to the plane including the injection port and the cylinder central axis and projected onto a plane including the intersection of the injection port, the spray and the cylinder central axis, the fuel can be quickly dispersed in the cavity by being substantially fan-shaped. Since this flat fan-shaped spray easily entrains the surrounding air, when the fuel is injected in the compression stroke, the air heated to a high temperature by the compression is quickly taken in, and vaporization and mixing are quick. Further, the air entrained by the spray deprives the momentum of the spray, so that the flying speed of the spray is reduced and the spray length is shortened. Therefore, even if the injection timing is advanced, the fuel does not wet the cylinder wall, and conversely, even if the injection timing is delayed, the piston surface is not covered with the liquid film. on the other hand,
Spray inside the cavity that has been vaporized and mixed
Ri Atsuma more guided by the spark plug position, can also be efficiently combusted in less <br/> have fuel and thus.

【0011】[0011]

【0012】以下、本発明の実施の形態を図に基づき説
明する。
An embodiment of the present invention will be described below with reference to the drawings.

【0013】[0013]

【発明の実施の形態】図1ないし図4は、本発明の第1
の実施の形態について示したもので、燃料噴射弁は、弁
体2の基端面に穿設した弁孔6に針弁1を摺嵌し針弁1
の基端部にコイルバネ5を装着する。弁孔6の先端部に
は、針弁1の円錐状の先端部7が当接する円錐状の弁座
部8を設けると共に、弁座部8から弁体2の先端面に開
口するスリット状の噴孔4を設けてある。スリット状の
噴孔4と弁座部8の間には、サック部3を設け、針弁1
の円柱状の本体部と円錐状の先端部7との境界付近
に位置する弁体2に円環状の圧力室12を形成する。弁
体2の基端部に穿設した燃料供給通路11の先端部は、
圧力室12の外周面に連通されている。針弁1と弁体2
の間には、圧力室12に接続する環状の接続通路13を
設ける。燃料供給通路11と接続通路13を経て針弁1
の先端部7に作用する燃料の圧力が上昇すると、針弁1
がコイルバネ5に抗して弁孔6の弁座部8から離脱す
る。
1 to 4 show a first embodiment of the present invention.
In the fuel injection valve, the needle valve 1 is slidably fitted into a valve hole 6 formed in the base end face of the valve body 2.
A coil spring 5 is attached to the base end of the coil spring 5. A conical valve seat 8 is provided at the distal end of the valve hole 6 with which the conical distal end 7 of the needle valve 1 contacts, and a slit-shaped opening from the valve seat 8 to the distal end surface of the valve body 2. An injection hole 4 is provided. A sack portion 3 is provided between the slit-shaped injection hole 4 and the valve seat portion 8, and the needle valve 1 is provided.
To form a cylindrical main body portion and the valve body 2 two annular pressure chambers 12 located Ri near the circumferential boundary between the conical tip 7. The distal end of the fuel supply passage 11 drilled at the base end of the valve body 2 is
It communicates with the outer peripheral surface of the pressure chamber 12. Needle valve 1 and valve body 2
An annular connection passage 13 connected to the pressure chamber 12 is provided therebetween. Needle valve 1 through fuel supply passage 11 and connection passage 13
When the pressure of the fuel acting on the tip 7 of the needle rises, the needle valve 1
Is disengaged from the valve seat portion 8 of the valve hole 6 against the coil spring 5.

【0014】このため、本第1の実施の形態の燃料噴射
弁は、針弁1の先端部7と弁孔6の弁座部8との隙間を
経て圧力室12が噴孔4に連通して開弁するように構成
されている。そして、燃料通路11、圧力室12、接続
通路13および針弁1の先端部7と弁孔6の弁座部8の
間の隙間によって、開弁時にスリット状の噴孔4に燃料
を供給する通路を構成して成る。この針弁1は燃料圧力
の他、電磁力等を利用して直接引き上げて開弁すること
もできる。また、スリット状の噴孔4が弁体2の外周側
の外端10と弁体2の内周側、すなわち、サック部3側
に内端9を有し、外端10と内端9は直線状あるいは円
弧状の通路で構成されている。
For this reason, in the fuel injection valve according to the first embodiment, the pressure chamber 12 communicates with the injection hole 4 through the gap between the tip 7 of the needle valve 1 and the valve seat 8 of the valve hole 6. The valve is configured to open. The fuel is supplied to the slit-shaped injection hole 4 when the valve is opened by the fuel passage 11, the pressure chamber 12, the connection passage 13, and the gap between the distal end portion 7 of the needle valve 1 and the valve seat portion 8 of the valve hole 6. It constitutes a passage. The needle valve 1 can be directly lifted and opened using an electromagnetic force or the like in addition to the fuel pressure. Further, the slit-shaped injection hole 4 has an outer end 10 on the outer peripheral side of the valve body 2 and an inner peripheral side of the valve body 2, that is, an inner end 9 on the side of the sack portion 3, and the outer end 10 and the inner end 9 It is composed of a straight or arcuate passage.

【0015】ここで、スリット状噴孔4における内端9
の幅(対向間距離)Wの範囲は、0.05mm以上で
0.24mm以下である。最適の数値範囲は、0.06
mm以上で0.20mm以下である。これにより、スリ
ット状噴孔4から噴射された燃料が扁平で扇形の形状と
なり、この液膜がスリット状噴孔4から遠ざかるに従っ
て、その厚みを減少し、周囲空気との接触面積を増大し
て、周囲空気によって液膜が引きちぎられ、急速に微細
な噴霧へと変化する。このようにして得られる噴霧の平
均粒径dsと幅Wの関係を図5に示す。図5に明らかな
ように幅Wが大きくなると平均粒径dsが大きくなるの
である。これは幅Wが大きくなると噴射された燃料液膜
の厚さも厚くなるからである。図5は幾多の実験等から
得られた結果であるが、図5から明らかなように、幅W
が0.24mm以上になると噴霧の平均粒径dsは急激
に大きくなる。そして、噴霧の平均粒径dsがほぼ一様
な値に保たれる幅Wは0.06mm以上で、0.20m
m以下である。
Here, the inner end 9 of the slit-shaped injection hole 4
Is in the range of 0.05 mm or more and 0.24 mm or less. The optimal numerical range is 0.06
mm or more and 0.20 mm or less. As a result, the fuel injected from the slit-shaped injection hole 4 becomes flat and fan-shaped, and as the liquid film moves away from the slit-shaped injection hole 4, its thickness decreases and the contact area with the surrounding air increases. The liquid film is torn off by the surrounding air, and rapidly changes to a fine spray. FIG. 5 shows the relationship between the average particle diameter ds and the width W of the spray thus obtained. As is apparent from FIG. 5, as the width W increases, the average particle diameter ds increases. This is because the greater the width W, the greater the thickness of the injected fuel liquid film. FIG. 5 shows the results obtained from various experiments and the like. As is apparent from FIG.
Is 0.24 mm or more, the average particle diameter ds of the spray increases rapidly. The width W at which the average particle diameter ds of the spray is maintained at a substantially uniform value is 0.06 mm or more and 0.20 m
m or less.

【0016】また、本噴射弁は噴霧角が大きいので、従
来のホールノズルに対して噴霧長さを短くできる利点が
ある。火花点火機関はシリンダ径の小さいものが多いの
で、ノズルから壁までの距離が短い。壁面を燃料でぬら
さないために、噴霧長さは適度に短い方がよい。噴霧は
運動量をほぼ保って成長する。本発明の第1の実施の形
態のノズルは、幅Wを決めれば、単位噴霧角当たりの運
動量は決まるので、噴霧角を変えても噴霧長さは変化し
ないが、流量当たりの噴霧長さは噴霧角を大きくとるこ
とで、噴霧長さは小さくなる。エンジンでは噴射期間に
制限があるため流量当たりの噴霧長さが重要である。図
6は、噴霧長さを同一流量を持つホールノズルと比較し
たものである。噴霧角を大きくするほど噴霧長さは短く
なり、例えば、噴霧角を90度にすると、その噴霧長さ
は従来の単孔ホールノズルの半分以下である。5孔ホー
ルノズルと比較しても70%である。ここでは、一つの
扇形噴霧と比較したが、スリットを複数開ければ、さら
に短くできる。
Further, since the injection valve of the present invention has a large spray angle, there is an advantage that the spray length can be reduced as compared with the conventional hole nozzle. Since many spark ignition engines have a small cylinder diameter, the distance from the nozzle to the wall is short. The spray length should be appropriately short so as not to wet the wall with fuel. The spray grows with almost the same momentum. In the nozzle according to the first embodiment of the present invention, if the width W is determined, the momentum per unit spray angle is determined. Therefore, even if the spray angle is changed, the spray length does not change, but the spray length per flow rate is By increasing the spray angle, the spray length is reduced. Since the injection period is limited in the engine, the spray length per flow rate is important. FIG. 6 compares the spray length with a hole nozzle having the same flow rate. As the spray angle increases, the spray length decreases. For example, when the spray angle is set to 90 degrees, the spray length is less than half that of a conventional single-hole nozzle. It is 70% compared to a 5-hole nozzle. Here, it is compared with one fan spray, but it can be further shortened by opening a plurality of slits.

【0017】本発明の第1の実施の形態においては、か
かる燃料噴射弁を図7、図8に示す内燃機関に配設す
る。内燃機関は吸気ポート27、吸気弁28、点火プラ
グ30および図示しない排気ポート、排気弁を備えたシ
リンダヘッド25、シリンダ24とシリンダ24に対し
て往復動可能に挿入されたピストン21で構成されてい
る。ピストン21には側面にピストンリング29が複数
設けられていて燃焼室31からのガスの吹き抜けを防止
している。燃料噴射弁23はシリンダヘッド25の吸気
弁28側にノズル先端23aが略シリンダ中心軸に向か
うよう傾斜して取り付けられている。本第1の実施の形
態は、吸気2弁であり、燃料噴射弁23は吸気弁28の
間にある。そして、噴霧流をシリンダ24の中心軸を含
む面内においては扁平に、シリンダ24の中心軸にほぼ
直角な面内においては扇形に拡開するように噴出せしめ
るが、噴霧中心が直接点火プラグ30に当たらぬよう、
やや下方に噴出する。噴射方向はエンジンによって異な
るが、概ねシリンダ下方20度から60度の範囲であ
る。
In the first embodiment of the present invention, such a fuel injection valve is provided in the internal combustion engine shown in FIGS. The internal combustion engine includes an intake port 27, an intake valve 28, a spark plug 30, an exhaust port (not shown), a cylinder head 25 equipped with an exhaust valve, and a cylinder 24 and a piston 21 reciprocally inserted into the cylinder 24. I have. A plurality of piston rings 29 are provided on the side surface of the piston 21 to prevent gas from flowing from the combustion chamber 31. The fuel injection valve 23 is attached to the cylinder head 25 on the intake valve 28 side so that the nozzle tip 23a is inclined substantially toward the cylinder center axis. The first embodiment has two intake valves, and the fuel injection valve 23 is located between the intake valves 28. Then, the spray flow is ejected so as to be flattened in a plane including the central axis of the cylinder 24 and spread in a fan shape in a plane substantially perpendicular to the central axis of the cylinder 24, but the spray center is directly directed to the ignition plug 30. Not to hit
Squirts slightly downward. The injection direction differs depending on the engine, but generally ranges from 20 degrees to 60 degrees below the cylinder.

【0018】ピストン21の頂面21aにはノズル先端
23aと点火プラグ30をほぼ両端としたキャビティ2
2を燃焼室31に開口せしめて形成する。キャビティ
は圧縮上死点で点火プラグ30のギャップ30aが概
略シリンダヘッド25とキャビティ22底面の略中心に
なる深さとしてある。また、キャビティ22の幅は、噴
霧先端がシリンダ中心に達したとき、シリンダ中心軸に
垂直な平面を投影した噴霧の幅以上の大きさがある。す
なわち、このときの燃焼室内空間にある噴霧はピストン
21の上昇によってキャビティ22内に収まる。また、
キャビティ22壁面のうち、少なくとも点火プラグ30
側はキャビティ22に対して凹の曲率を持っている。そ
して、その曲率Rは(曲率半径R)≦(ノズル先端から
キャビティ壁面までの距離L)としてある。
On the top surface 21a of the piston 21, a cavity 2 having a nozzle tip 23a and a spark plug 30 at substantially both ends is provided.
2 is formed by opening it into the combustion chamber 31. Cavity 2
Reference numeral 2 denotes a compression top dead center, which is a depth at which the gap 30a of the ignition plug 30 is approximately at the center of the cylinder head 25 and the bottom surface of the cavity 22. The width of the cavity 22 is larger than the width of the spray projected on a plane perpendicular to the cylinder center axis when the spray tip reaches the center of the cylinder. That is, the spray in the space in the combustion chamber at this time is contained in the cavity 22 by the rise of the piston 21. Also,
At least the spark plug 30 of the cavity 22
The side has a concave curvature with respect to the cavity 22. The curvature R is set to (radius of curvature R) ≦ (distance L from the nozzle tip to the cavity wall surface).

【0019】ピストン21が吸気を完了した下死点位置
から上死点に向かう圧縮行程で燃焼室31内の空気は圧
縮される。この圧縮過程において噴射弁23の噴孔から
燃料を噴出せしめると、噴霧粒群は図示のように、シリ
ンダ中心軸とノズル23aを含む平面に投影したときに
は扁平に、シリンダ中心軸に垂直な平面に投影したとき
には扇状に、かつ点火プラグ30に対して略対称に飛散
する。燃料は噴孔を出た後、急速に広がるので、シリン
ダ24の壁に高速で噴霧粒が衝突したり、キャビティ2
2の壁面を多量の液状噴霧で濡らすことはない。また、
扁平な形状のため、周囲の高温空気と素早く混合するの
で、蒸発のために顕熱、潜熱をとられても噴霧内の混合
気温度はさほど下がらない。噴霧はキャビティ22の壁
面によってキャビティ22の上方、内側に向かって巻き
上がる流れとなる。これとピストン21の上昇が相まっ
て圧縮上死点前には可燃混合気が点火プラグ30にでき
る。点火プラグ30により点火された火炎は火炎伝播に
より燃焼する。
The air in the combustion chamber 31 is compressed in the compression stroke from the bottom dead center position where the piston 21 completes the intake to the top dead center. When fuel is ejected from the injection hole of the injection valve 23 in the compression process, the spray particles are flattened when projected onto a plane including the cylinder center axis and the nozzle 23a, as shown in FIG. When projected, they scatter in a fan shape and substantially symmetrically with respect to the spark plug 30. Since the fuel spreads rapidly after leaving the injection hole, the spray particles collide with the wall of the cylinder 24 at high speed,
The wall of No. 2 is not wet with a large amount of liquid spray. Also,
Because of its flat shape, it mixes quickly with the surrounding high-temperature air, so even if sensible heat or latent heat is taken for evaporation, the temperature of the mixture in the spray does not drop so much. The spray becomes a flow that winds upward and inward of the cavity 22 by the wall surface of the cavity 22. Combined with the rise of the piston 21, a combustible air-fuel mixture is formed in the ignition plug 30 before the compression top dead center. The flame ignited by the ignition plug 30 burns by flame propagation.

【0020】このとき、キャビティ22とピストン頂面
21aによるスキッシュ流により、混合気はキャビティ
22内に収まり、燃焼室外への飛散が避けられるので、
点火プラグ30によって形成した火炎はキャビティ22
内に発達する。したがって失火や消炎の心配がない。さ
らに、本発明の第1の実施の形態における噴霧は、扇状
の噴霧であるから、濃度むらが小さく、火炎伝播が途切
れることがないことも失火や消炎に対して有利である。
負荷の変化に対しては、噴射量の少ない低負荷の時は、
噴射時期を遅くし、燃料が拡散しないうちに点火する、
一方、噴射量の多い高負荷の時は、噴射時期を早くし、
過濃な混合気が点火プラグ30に集まりすぎることを避
けるのが良い。
At this time, due to the squish flow between the cavity 22 and the piston top surface 21a, the air-fuel mixture is contained in the cavity 22 and is prevented from scattering outside the combustion chamber.
The flame formed by the spark plug 30
Develop within. Therefore, there is no fear of misfiring or extinguishing. Furthermore, since the spray in the first embodiment of the present invention is a fan-shaped spray, the unevenness in concentration is small, and the flame propagation is not interrupted.
When the load is low and the load is small,
Delay the injection timing, ignite before the fuel spreads,
On the other hand, when the load is high and the injection amount is high, the injection timing is advanced,
It is good to avoid that the rich air-fuel mixture collects too much in the spark plug 30.

【0021】第1の実施の形態の内燃機関では、噴射時
期を遅らせたとき、図9、図10に示すように、噴霧は
比較的早くキャビティ22に衝突するが、噴霧が扁平
で、かつキャビティ22の底面に対しては扇状の形をし
ているため、ピストン21、および空気から有効に熱を
もらい、すばやく気化混合できる。したがって、噴射か
ら点火までの時間を短くした燃焼が可能である。さら
に、キャビティの曲率Rを(曲率半径R)≦(ノズル先
端からキャビティ壁面までの距離L)としておくと、こ
の曲率に沿って点火プラグ30に燃料が集まるため、よ
り少ない燃料で運転が可能である。一方、噴射時期を早
めたとき、本第1の実施の形態の噴霧は噴霧長さが短い
ために、キャビティに衝突するまでの時間が長くなる
が、噴霧は扇状に分散し、かつ扁平なため周囲の空気か
ら有効に熱をもらい、気化混合が遅れることはない。そ
して、図11に示すように、初期に噴射された燃料はキ
ャビティ22に衝突後、空中で拡散するので、点火プラ
グ30に過濃な混合気が集まることなく、安定な点火が
可能となる。
In the internal combustion engine of the first embodiment, when the injection timing is delayed, as shown in FIGS. 9 and 10, the spray collides with the cavity 22 relatively quickly, but the spray is flat and the Since the bottom surface of the fan 22 has a fan-like shape, heat is effectively received from the piston 21 and the air, and vaporization and mixing can be performed quickly. Therefore, combustion in which the time from injection to ignition is shortened is possible. Further, if the curvature R of the cavity is set to (radius of curvature R) ≦ (distance L from the tip of the nozzle to the cavity wall), the fuel is collected in the ignition plug 30 along this curvature, so that operation with less fuel is possible. is there. On the other hand, when the injection timing is advanced, the spray of the first embodiment has a short spray length, so the time until collision with the cavity is long. However, since the spray is dispersed in a fan shape and is flat, Effective heat is obtained from the surrounding air, and there is no delay in evaporative mixing. Then, as shown in FIG. 11, the initially injected fuel collides with the cavity 22 and then diffuses in the air, so that a rich mixture is not collected in the ignition plug 30 and stable ignition is possible.

【0022】また、さらに負荷が上がって、全負荷に近
いときには圧縮行程に限らず、吸気行程に燃料を噴射す
ることも可能である。このとき噴霧は噴霧長さの短い、
低貫徹力の噴霧であるから、ピストン21が下がっても
シリンダ24の壁面を濡らすことはないうえ、吸気流動
に乗ってシリンダ内に分散し、空気利用度が高くなる。
本発明の第1の実施の形態の内燃機関は、このように負
荷の大小に関わらず、点火プラグ30には安定した可燃
混合気が形成されることになり、負荷変動の大きい例え
ば、自動車用内燃機関としては優れた性能を供する。
Further, when the load further increases and is close to the full load, it is possible to inject fuel not only in the compression stroke but also in the intake stroke. At this time, the spray length is short,
Since the spray has a low penetration force, even if the piston 21 goes down, it does not wet the wall surface of the cylinder 24 and is dispersed in the cylinder by the flow of the intake air, thereby increasing the air utilization.
In the internal combustion engine according to the first embodiment of the present invention, a stable combustible air-fuel mixture is formed in the ignition plug 30 regardless of the magnitude of the load as described above. Provides excellent performance as an internal combustion engine.

【0023】[0023]

【第2の実施の形態】本発明の第2の実施の形態例は、
図12のように、キャビティ22の縦壁面をR形状と
し、ピストン頂面21aがキャビティ22の内壁より飛
び出すリップ形状を有するようにしたものである。その
他の燃料噴射弁23、噴霧形状、ピストン21などは第
1の実施例と同様である。
[Second Embodiment] A second embodiment of the present invention is as follows.
As shown in FIG. 12, the vertical wall surface of the cavity 22 has an R shape, and the piston top surface 21a has a lip shape protruding from the inner wall of the cavity 22. Other fuel injection valves 23, spray shapes, pistons 21 and the like are the same as in the first embodiment.

【0024】上記構成からなる本発明の第2の実施の形
態例は、第1の実施の形態例と同様、噴霧がキャビティ
22の壁面に衝突後、上方へ方向を変えるが、キャビテ
ィ22の壁面はR形状(曲率半径r1 )をしているた
め、燃料はキャビティ22の内側に向かって巻き上がる
流れとなる。このため、燃料はキャビティ22外側に流
出することがより少なくなり、点火後火炎がキャビティ
22外側に出て冷やされ消炎することが少ない。また、
スキッシュ流と複合して強い乱れをつくるため燃焼期間
が短縮されるなどの利点を有する。
In the second embodiment of the present invention having the above-described structure, the spray changes its direction after collision with the wall surface of the cavity 22 as in the first embodiment. Has a round shape (radius of curvature r 1 ), so that the fuel flows in such a manner as to wind up toward the inside of the cavity 22. For this reason, the fuel is less likely to flow out of the cavity 22, and the flame after ignition is less likely to flow out of the cavity 22 to be cooled and extinguished. Also,
There is an advantage that the combustion period is shortened because strong turbulence is created in combination with the squish flow.

【0025】[0025]

【第3の実施の形態】本発明の第3の実施の形態例は、
キャビティ22を2段とし、図13、図14に示すよう
に浅いキャビティ22の内側にさらにキャビティ22
aを形成したものである。その他の燃料噴射弁23、噴
霧形状、ピストン21などは第1の実施の形態例と同様
である。
[Third Embodiment] A third embodiment of the present invention is as follows.
The cavity 22 is a two-stage, 13, further cavity 22 inside the shallow cavity 22 b as shown in FIG. 14
a is formed. Other fuel injection valves 23, spray shapes, pistons 21 and the like are the same as those in the first embodiment.

【0026】本発明の第3の実施の形態例キャビティ
22を用いれば、低負荷時にはより燃料を点火プラグ3
0に集め、高負荷時にはより燃料を拡散させて燃焼させ
ることができる。すなわち、図15、図16に示すよう
に小噴射量時に噴射時期を遅らせると、噴射した燃料は
内側のキャビティ22に入り、その内壁面を通って上
方に曲げられ点火プラグ30にいたる。そのため、燃料
が過度に分散することなく、点火プラグ30に集中し、
非常に少ない燃料でも点火、燃焼が可能となる。一方、
高負荷時には噴射時期を早める。このため、燃料は図1
7、図18に示すように、外側の大きいキャビティ22
bと内側のキャビティ22aに分けられる。外側のキャ
ビティ22bは第1の実施例のように上方内側に曲げら
れて点火プラグ30にいたるが、内側のキャビティ22
aの燃料は下側に曲げられ、点火プラグ30にいたるこ
となく、キャビティ22内に分散する。これによって点
火プラグ30には負荷の大小に関わらず、安定した可燃
混合気が形成されることになり、負荷変動の大きい例え
ば自動車用内燃機関としては優れた性能を供する。
When the cavity 22 according to the third embodiment of the present invention is used, the fuel can be more easily ignited when the load is low.
At high load, the fuel can be more diffused and burned. That is, FIG. 15, when delaying the fuel injection timing to a small injection quantity at the time, as shown in FIG. 16, the injected fuel enters the inside of the cavity 22 b, leading to the ignition plug 30 is bent upwardly through the inner wall surface thereof. Therefore, the fuel concentrates on the spark plug 30 without being excessively dispersed,
Ignition and combustion are possible with very little fuel. on the other hand,
When the load is high, the injection timing is advanced. Therefore, the fuel is
7, the outer large cavity 22 as shown in FIG.
b and the inner cavity 22a. The outer cavity 22b is bent upward and inward to reach the spark plug 30 as in the first embodiment.
The fuel a is bent downward and is dispersed in the cavity 22 without reaching the spark plug 30. As a result, a stable combustible air-fuel mixture is formed in the ignition plug 30 irrespective of the magnitude of the load, and excellent performance is provided, for example, as an automotive internal combustion engine having a large load variation.

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

【図1】本発明の第1の実施の形態における燃料噴射弁
を示す縦断面図
FIG. 1 is a longitudinal sectional view showing a fuel injection valve according to a first embodiment of the present invention.

【図2】本発明の第1の実施の形態における燃料噴射弁
を示す縦断面図
FIG. 2 is a longitudinal sectional view showing a fuel injection valve according to the first embodiment of the present invention.

【図3】本発明の第1の実施の形態における燃料噴射弁
の噴霧状態を示す縦断面図
FIG. 3 is a longitudinal sectional view showing a spray state of a fuel injection valve according to the first embodiment of the present invention.

【図4】本発明の第1の実施の形態における燃料噴射弁
の噴霧状態を示す縦断面図
FIG. 4 is a longitudinal sectional view showing a spray state of a fuel injection valve according to the first embodiment of the present invention.

【図5】第1の実施の形態における燃料噴射弁の噴霧の
平均粒径と幅の関係を示す線図
FIG. 5 is a diagram showing the relationship between the average particle size and the width of the spray of the fuel injection valve in the first embodiment.

【図6】第1の実施の形態における燃料噴射弁の噴霧角
と噴霧長さの比の関係を示す線図
FIG. 6 is a diagram showing a relationship between a spray angle and a spray length ratio of a fuel injection valve in the first embodiment.

【図7】第1の実施の形態における内燃機関を示す平面
FIG. 7 is a plan view showing the internal combustion engine according to the first embodiment;
Figure

【図8】第1の実施の形態における内燃機関を示す縦断
面図
FIG. 8 is a longitudinal sectional view showing the internal combustion engine according to the first embodiment.

【図9】第1の実施の形態における内燃機関の噴霧状態
を示す平面図
FIG. 9 is a plan view showing a spray state of the internal combustion engine in the first embodiment .

【図10】第1の実施の形態における内燃機関の噴霧状
態を示す縦断面図
FIG. 10 is a longitudinal sectional view showing a spray state of the internal combustion engine according to the first embodiment.

【図11】第1の実施の形態における内燃機関の噴霧状
態を示す縦断面図
FIG. 11 is a longitudinal sectional view showing a spray state of the internal combustion engine in the first embodiment.

【図12】第2の実施の形態における内燃機関を示す部
分断面図
FIG. 12 is a partial cross-sectional view illustrating an internal combustion engine according to a second embodiment.

【図13】第3の実施の形態における内燃機関を示す
面図
FIG. 13 is a plan view showing an internal combustion engine according to a third embodiment.
Front view

【図14】第3の実施の形態における内燃機関を示す縦
断面図
FIG. 14 is a longitudinal sectional view showing an internal combustion engine according to a third embodiment.

【図15】第3の実施の形態における内燃機関の噴霧状
態を示す平面図
FIG. 15 is a plan view showing a spray state of an internal combustion engine according to a third embodiment .

【図16】第3の実施の形態における内燃機関の噴霧状
態を示す縦断面図
FIG. 16 is a longitudinal sectional view showing a spray state of an internal combustion engine according to a third embodiment.

【図17】第3の実施の形態における内燃機関の噴霧状
態を示す平面図
FIG. 17 is a plan view showing a spray state of an internal combustion engine in a third embodiment .

【図18】第3の実施の形態における内燃機関の噴霧状
態を示す縦断面図
FIG. 18 is a longitudinal sectional view showing a spray state of an internal combustion engine according to a third embodiment.

【符号の説明】[Explanation of symbols]

1 針弁 2 弁体 3 サック部 4 噴孔 5 コイルバネ 6 弁孔 7 先端部 8 弁座部 9 内端 10 外端 22、22a キャビティ 23 燃料噴射弁 21 ピストン 24 シリンダ 31 燃焼室 30 点火プラグ DESCRIPTION OF SYMBOLS 1 Needle valve 2 Valve element 3 Sack part 4 Injection hole 5 Coil spring 6 Valve hole 7 Tip part 8 Valve seat part 9 Inner end 10 Outer end 22, 22a Cavity 23 Fuel injection valve 21 Piston 24 Cylinder 31 Combustion chamber 30 Spark plug

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.7 識別記号 FI F02M 61/18 360 F02M 61/18 360J (56)参考文献 特開 平3−78562(JP,A) 特開 平8−144762(JP,A) 特開 昭57−13215(JP,A) 特開 平5−1544(JP,A) 実開 平2−122123(JP,U) 実開 平3−27829(JP,U) 実開 平1−173416(JP,U) (58)調査した分野(Int.Cl.7,DB名) F02B 23/10 F02B 17/00 F02M 61/18 F02M 61/14 ──────────────────────────────────────────────────続 き Continuation of front page (51) Int.Cl. 7 Identification code FI F02M 61/18 360 F02M 61/18 360J (56) References JP-A-3-78562 (JP, A) JP-A-8-144762 (JP, A) JP-A-57-13215 (JP, A) JP-A-5-1544 (JP, A) JP-A-2-122123 (JP, U) JP-A-3-27829 (JP, U) Kaihei 1-173416 (JP, U) (58) Fields investigated (Int. Cl. 7 , DB name) F02B 23/10 F02B 17/00 F02M 61/18 F02M 61/14

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 シリンダヘッド内壁面の中央部に点火プ
ラグを配置すると共にシリンダヘッド内壁面の周縁部に
燃料噴射弁を配置し、ピストン頂面上に燃料噴射弁の下
方から点火プラグの下方まで延びるキャビティを形成し
た内燃機関の火花点火式燃焼方法において、点火プラグ
側のキャビティの端部においてキャビティの底面から上
方に延びかつ燃料噴射弁とシリンダ中心軸とを含む平面
に対して横方向に円弧状に延びる壁面をキャビティに形
成し、シリンダの中心軸に対し傾斜して配設された燃料
噴射弁の噴口から、噴口とシリンダ中心軸を含む平面に
投影したときは扁平に、噴口とシリンダ中心軸を含む平
面に垂直で、噴口と、噴霧とシリンダ中心軸の交点を含
む平面に投影したときには略扇状の燃料噴霧をその全体
がキャビティの底面に向かうように噴射して燃料噴霧を
キャビティ内に分散させ、次いでキャビティ内に分散し
た燃料噴霧を上記キャビティ壁面によりキャビティの上
方、内側に向けて巻き上げることにより点火プラグの周
りに集め、次いで点火プラグ周りに集められた燃料噴霧
を点火プラグにより着火するようにした火花点火式燃焼
方法。
An ignition plug is provided at a central portion of an inner wall surface of a cylinder head.
Place the lug on the inner peripheral surface of the cylinder head
Position the fuel injection valve and place it below the fuel injection valve on the top of the piston.
To form a cavity that extends from
The spark-ignition combustion process of an internal combustion engine, the spark plug
From the bottom of the cavity at the end of the side cavity
Plane extending in the direction and including the fuel injection valve and the cylinder center axis
A wall extending in an arc shape in the lateral direction to the cavity
Form, from the nozzle hole of the fuel injection valve disposed to be inclined with respect to the center axis of the cylinder, so the when projected onto the plane containing the nozzle hole and the cylinder center axis flat, perpendicular to the plane containing the nozzle hole and the cylinder center axis its entirety the sector-shaped fuel spray when projected to a plane including the injection port, the intersection of the spray and the cylinder center axis
Spray toward the bottom of the cavity to spray fuel
Dispersed in the cavity, then dispersed in the cavity
The sprayed fuel is sprayed over the cavity by the cavity wall.
To the inside of the spark plug
And then the fuel spray collected around the spark plug
Spark ignition combustion method in which a spark plug is ignited by a spark plug .
JP34527995A 1995-12-06 1995-12-06 Spark ignition combustion method Expired - Lifetime JP3301013B2 (en)

Priority Applications (1)

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JP34527995A JP3301013B2 (en) 1995-12-06 1995-12-06 Spark ignition combustion method

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Application Number Priority Date Filing Date Title
JP34527995A JP3301013B2 (en) 1995-12-06 1995-12-06 Spark ignition combustion method

Related Child Applications (1)

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JP31503798A Division JP3330336B2 (en) 1995-12-06 1998-11-05 Spark ignition internal combustion engine

Publications (2)

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JPH09158736A JPH09158736A (en) 1997-06-17
JP3301013B2 true JP3301013B2 (en) 2002-07-15

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Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5915353A (en) * 1997-05-21 1999-06-29 Nissan Motor Co., Ltd Cylinder direct injection spark-ignition engine
US6035823A (en) * 1998-06-15 2000-03-14 Toyota Jidosha Kabushiki Kaisha Spark-ignition type engine
JP3353709B2 (en) * 1998-07-08 2002-12-03 トヨタ自動車株式会社 In-cylinder injection spark ignition internal combustion engine
JP3548688B2 (en) 1998-07-08 2004-07-28 トヨタ自動車株式会社 In-cylinder injection spark ignition internal combustion engine
JP3903657B2 (en) * 1998-12-02 2007-04-11 トヨタ自動車株式会社 In-cylinder injection spark ignition internal combustion engine
JP3611471B2 (en) * 1999-01-28 2005-01-19 株式会社日立製作所 In-cylinder internal combustion engine
JP3389873B2 (en) 1999-02-05 2003-03-24 トヨタ自動車株式会社 In-cylinder injection spark ignition internal combustion engine
JP3362690B2 (en) 1999-03-02 2003-01-07 トヨタ自動車株式会社 In-cylinder injection spark ignition internal combustion engine
JP3401206B2 (en) 1999-03-16 2003-04-28 トヨタ自動車株式会社 In-cylinder injection spark ignition internal combustion engine
JP3405261B2 (en) 1999-03-30 2003-05-12 トヨタ自動車株式会社 In-cylinder injection spark ignition internal combustion engine
JP3537347B2 (en) 1999-04-02 2004-06-14 トヨタ自動車株式会社 In-cylinder injection spark ignition internal combustion engine
JP3370947B2 (en) 1999-04-09 2003-01-27 トヨタ自動車株式会社 In-cylinder injection spark ignition internal combustion engine
JP3997781B2 (en) 2002-01-09 2007-10-24 日産自動車株式会社 In-cylinder direct injection engine
US6832594B2 (en) 2002-01-09 2004-12-21 Nissan Motor Co., Ltd. Direct fuel injection engine
JP2015218614A (en) 2014-05-15 2015-12-07 トヨタ自動車株式会社 Internal combustion engine fuel injection control device
JP6398700B2 (en) * 2014-12-24 2018-10-03 三菱自動車工業株式会社 In-cylinder injection engine

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