JPH10339142A - Cylinder fuel injection internal combustion engine - Google Patents

Cylinder fuel injection internal combustion engine

Info

Publication number
JPH10339142A
JPH10339142A JP9147644A JP14764497A JPH10339142A JP H10339142 A JPH10339142 A JP H10339142A JP 9147644 A JP9147644 A JP 9147644A JP 14764497 A JP14764497 A JP 14764497A JP H10339142 A JPH10339142 A JP H10339142A
Authority
JP
Japan
Prior art keywords
cavity
inclined surface
fuel injection
exhaust port
port side
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
JP9147644A
Other languages
Japanese (ja)
Other versions
JP4291423B2 (en
Inventor
Masashi Matoba
雅司 的場
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP14764497A priority Critical patent/JP4291423B2/en
Publication of JPH10339142A publication Critical patent/JPH10339142A/en
Application granted granted Critical
Publication of JP4291423B2 publication Critical patent/JP4291423B2/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
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/08Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • F02B23/10Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder
    • F02B23/104Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder the injector being placed on a side position of the cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • 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
    • F02B75/12Other 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)

Abstract

PROBLEM TO BE SOLVED: To perform effective stratified charge combustion by holding an thick mixed gas layer in a cavity while concentrating the thick mixed gas around a spark plug at a center of a combustion chamber in a spark ignition engine in which fuel is directly injected to be supplied into a piston cavity. SOLUTION: An upper surface of a piston is formed swollen to comprise an inclined surface 1A facing an intake port 9 and an inclined surface 1B facing an exhaust port 13, a cavity 6 is formed in such a way that a main part 6A of it is opened in the intake port side inclined surface 1A to be close to a boundary L of both inclined surfaces 1A, 1B, and that only a range 6B to be on the up stream side of a spark plug to swirl is partially opened in the exhaust port side inclined surface 1B, and fuel injection is set to rise from an inner wall surface of the cavity main part 6A to be concentrated around a spark plug 3 at a center of a combustion chamber, while residual fuel is secured in the cavity 6 by an expansion part 6B to cause stratified charge combustion.

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】この発明は、筒内噴射式内燃
機関にの改良に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an improvement in a direct injection internal combustion engine.

【0002】[0002]

【従来の技術】従来の筒内噴射式内燃機関としては、例
えば特開平8−35429号公報に記載されたものがあ
る。これは、広い負荷範囲すなわち燃料噴射量の多寡に
関わらず安定した成層燃焼を可能とすることを目的とし
たもので、ピストン上面に設けたキャビティ(キャビテ
ィ部)の形状として点火プラグに近接した壁面を略直線
状するとともに、前記直線状壁面の後方にスワールによ
り燃料及び空気が拡散、混合する空間を構成している。
このため、高負荷時すなわち燃料量の多い状態において
も点火プラグ付近に過剰の燃料を停滞させることなく、
可燃空燃比の混合気を形成できるというものである。
2. Description of the Related Art A conventional in-cylinder injection type internal combustion engine is disclosed, for example, in JP-A-8-35429. The purpose of this is to enable stable stratified combustion regardless of the large load range, that is, the amount of fuel injection, and the shape of the cavity (cavity) provided on the upper surface of the piston as a wall close to the spark plug And a space in which fuel and air are diffused and mixed by swirl behind the linear wall surface.
For this reason, even at the time of high load, that is, in the state of a large amount of fuel, the excess fuel does not stagnate near the spark plug,
That is, a mixture having a combustible air-fuel ratio can be formed.

【0003】[0003]

【発明が解決しようとする課題】ところで、この筒内噴
射式内燃機関のキャビティは、詳細にはスワールに対し
て上流側から円弧状の第1の壁面区間、直線状の第2の
壁面区間、円弧状の第3の壁面区間を連続させた平面形
状となっており、また縦断面としては深さ方向の中央付
近が最も断面積が大きく、かつ第2の壁面区間はこれと
対向する壁面区間よりも高さが大きくなるように形成さ
れている。また、ピストンの上面には吸気ポートに面し
た傾斜面と排気ポートに面した傾斜面とからなる隆起形
状が付与されている。
The cavity of the in-cylinder injection type internal combustion engine has a first wall section having an arc shape, a second wall section having a straight line shape, and the like. The third wall section having a circular arc shape has a continuous plane shape. The vertical section has the largest cross-sectional area near the center in the depth direction, and the second wall section is a wall section facing the third wall section. It is formed so that the height is larger than that. The upper surface of the piston is provided with a raised shape including an inclined surface facing the intake port and an inclined surface facing the exhaust port.

【0004】しかしながら、このようなキャビティ形状
によると、噴射された燃料噴霧の多くはキャビティ内に
保持されるため、ピストンが上死点近傍に到達するまで
点火ができず、最適点火時期よりも遅れて十分な出力性
能が得られなくなるおそれがある。
However, according to such a cavity shape, since most of the injected fuel spray is held in the cavity, ignition cannot be performed until the piston reaches the vicinity of top dead center, and the ignition timing is delayed from the optimum ignition timing. Therefore, sufficient output performance may not be obtained.

【0005】その一方、上述した各壁面区間はそれぞれ
ピストン上面の隆起形状の頂部よりも排気側に広がる領
域を有しているため、噴射された燃料がこれら壁面区間
の排気側領域へ比較的拡散しやすくなり、この結果とし
て点火プラグ付近の混合気が薄くなって着火性が悪化す
るおそれもある。
On the other hand, since each of the above-mentioned wall sections has a region which spreads to the exhaust side from the top of the raised shape of the piston upper surface, the injected fuel is relatively diffused to the exhaust-side region of these wall sections. As a result, the air-fuel mixture near the ignition plug becomes thin, and the ignitability may be deteriorated.

【0006】本発明は、このような従来の問題点を解消
することを目的としている。
An object of the present invention is to solve such a conventional problem.

【0007】[0007]

【課題を解決するための手段】請求項1の発明は、対向
的に配置された吸気ポートと排気ポートとの間の燃焼室
略中央部に点火プラグを位置させるとともに、上面に平
面上略円形のキャビティを形成したピストンと、吸気ポ
ート側から前記キャビティに向けて燃料を噴射供給する
燃料噴射弁と、シリンダ内にスワールを発生させる手段
とを備えた内燃機関において、ピストン上面を、吸気ポ
ートに面した傾斜面と排気ポートに面した傾斜面とから
なる隆起形状とするとともに、前記キャビティを、その
主要部が前記各傾斜面の境界部分に近接して吸気ポート
側傾斜面内に開口するように、かつスワールに対して点
火プラグの上流側となる領域のみが部分的に排気ポート
側傾斜面内に開口するように形成した。
According to a first aspect of the present invention, a spark plug is located at a substantially central portion of a combustion chamber between an intake port and an exhaust port disposed opposite to each other, and has a substantially circular shape on a top surface. A piston having a cavity formed therein, a fuel injection valve for injecting fuel from the intake port side toward the cavity, and a means for generating a swirl in the cylinder. The cavity has a protruding shape including a sloped surface facing the exhaust port and an inclined surface facing the exhaust port, and the main part of the cavity is opened in the intake port side inclined surface in the vicinity of a boundary portion between the respective inclined surfaces. Further, only the region upstream of the spark plug with respect to the swirl is formed so as to partially open into the exhaust port side inclined surface.

【0008】請求項2の発明は、上記請求項1の発明に
おいて、吸気ポート側傾斜面と排気ポート側傾斜面の境
界を燃焼室中央部よりも吸気ポート側に偏った位置に設
定した。
According to a second aspect of the present invention, in the first aspect of the invention, the boundary between the intake port side inclined surface and the exhaust port side inclined surface is set at a position deviated toward the intake port side from the center of the combustion chamber.

【0009】請求項3の発明は、上記請求項1の発明に
おいて、吸気ポート側傾斜面と排気ポート側傾斜面の境
界を燃焼室中央部よりも排気ポート側に偏った位置に設
定した。
According to a third aspect of the present invention, in the first aspect of the present invention, the boundary between the intake port side inclined surface and the exhaust port side inclined surface is set at a position deviated toward the exhaust port side from the center of the combustion chamber.

【0010】請求項4の発明は、上記各発明のキャビテ
ィを、その主要部の平面形状が円形であり、かつ排気ポ
ート側傾斜面内に開口する部分が前記円形状から膨出し
た態様で形成したものとする。
According to a fourth aspect of the present invention, the cavity of each of the above-mentioned inventions is formed in such a manner that the main part thereof has a circular planar shape, and a portion opening into the exhaust port side inclined surface bulges from the circular shape. Shall be done.

【0011】請求項5の発明は、上記請求項1から請求
項3の発明のキャビティを、その平面形状が、長軸が燃
料噴射弁付近からスワール下流方向に沿うように形成し
た楕円形状とする。
According to a fifth aspect of the invention, the cavity of the first to third aspects of the invention has an elliptical shape whose planar shape is formed so that a major axis extends from the vicinity of the fuel injection valve to the swirl downstream direction. .

【0012】請求項6の発明は、上記請求項1から請求
項3の発明のキャビティを、その平面形状が、部分的に
排気ポート側傾斜面に突出した円形状とする。
According to a sixth aspect of the present invention, the cavity of the first to third aspects of the present invention has a circular shape whose planar shape is partially projected to the inclined surface on the exhaust port side.

【0013】請求項7の発明は、上記各発明の燃料噴射
弁を、その噴霧中心が、キャビティの排気ポート側傾斜
面への突出部を指向するように設けたものとする。
According to a seventh aspect of the present invention, the fuel injection valve of each of the above-mentioned inventions is provided such that the spray center thereof is directed to a protruding portion of the cavity toward the exhaust port side inclined surface.

【0014】[0014]

【作用・効果】上記各発明において、吸気ポート側に位
置する燃料噴射弁から噴射された燃料噴霧の一部は対向
するキャビティ内壁面に衝突する。キャビティの主要部
は隆起形状の境界部分に近接して吸気ポート側傾斜面に
位置しているため、前記燃料噴霧が衝突する内壁面はピ
ストン上面までの高さが最も高く、かつ燃焼室の中央部
に近い。このため、前記キャビティの対向壁面に衝突し
てキャビティ外へと上昇した燃料噴霧が点火プラグ付近
へと集中し、点火プラグの近傍に濃混合気層を形成す
る。これにより、ピストンが上死点に達するよりも早期
に着火可能となるため良好な出力性能が発揮される。
In each of the above inventions, part of the fuel spray injected from the fuel injection valve located on the intake port side collides with the opposing cavity inner wall surface. Since the main portion of the cavity is located on the intake port side inclined surface close to the boundary portion of the raised shape, the inner wall surface against which the fuel spray collides has the highest height up to the piston upper surface and the center of the combustion chamber. Close to the department. Therefore, the fuel spray that collides with the opposing wall surface of the cavity and rises out of the cavity concentrates near the spark plug, and forms a rich mixture layer near the spark plug. As a result, the piston can be ignited earlier than reaching the top dead center, so that good output performance is exhibited.

【0015】一方、燃料噴霧の一部はスワールにより該
スワールの下流方向へと輸送されるが、このときキャビ
ティがスワール下流方向について排気ポート側傾斜面に
突出した形状となっているため、スワールに対して点火
プラグの上流側のキャビティ内に多くの燃料を確保して
おくことができ、これにより濃混合気層を維持しつつキ
ャビティ内の吸気流動を活用して良好な燃焼性能が得ら
れる。
On the other hand, a part of the fuel spray is transported to the downstream side of the swirl by the swirl. At this time, since the cavity has a shape protruding from the exhaust port side inclined surface in the swirl downstream direction, the swirl causes the swirl. On the other hand, a large amount of fuel can be ensured in the cavity on the upstream side of the ignition plug, whereby good combustion performance can be obtained by utilizing the intake air flow in the cavity while maintaining a rich mixture layer.

【0016】請求項2の発明によれば、燃焼室内でのキ
ャビティ容量が比較的小となるので、ボア・ストローク
比の比較的大きい機関において、キャビティ内での燃料
の分散を規制し、層状化を維持して良好な燃費性能を確
保することができる。
According to the second aspect of the present invention, since the cavity capacity in the combustion chamber is relatively small, in an engine having a relatively large bore-stroke ratio, the dispersion of the fuel in the cavity is regulated and the stratification is achieved. , And good fuel economy performance can be secured.

【0017】請求項3の発明によれば、燃料噴射弁から
キャビティの対向壁面までの距離が大きくなるので燃料
気化時間が長期化して未燃HCやスモークが低減する。
また、ボア・ストローク比の比較的小さい機関において
燃料噴霧を保持しうるだけのキャビティ容量を確保でき
るという利点もある。
According to the third aspect of the present invention, since the distance from the fuel injection valve to the opposed wall surface of the cavity is increased, the fuel vaporization time is prolonged, and unburned HC and smoke are reduced.
Another advantage is that a cavity capacity sufficient to hold fuel spray can be ensured in an engine having a relatively small bore / stroke ratio.

【0018】請求項4の発明では、キャビティ主要部の
平面形状が円形であり、かつ排気ポート側傾斜面内に開
口する部分が前記円形状から膨出した態様で形成してあ
るので、円形形状によりキャビティ内へのスワールの導
入及び維持を容易にしつつ、スワール下流域にキャビテ
ィ容積を確保して多くの燃料を保持させておくことがで
き、成層燃焼の改善効果が向上する。
According to the fourth aspect of the present invention, the planar shape of the main portion of the cavity is circular, and the portion opening into the inclined surface on the exhaust port side is formed so as to bulge from the circular shape. This facilitates introduction and maintenance of the swirl into the cavity, while securing a large volume of the cavity in the swirl downstream area to hold a large amount of fuel, thereby improving the effect of improving stratified combustion.

【0019】請求項5の発明では、キャビティの平面形
状を、長軸が燃料噴射弁付近からスワール下流方向に沿
うように形成した楕円形状としてあるので、シリンダ内
に生じるスワール全体の流れがキャビティ内に導入され
やすく、これにより点火プラグ付近への燃料噴霧の集中
を促して着火性をより向上させることができる。
According to the fifth aspect of the present invention, since the plane shape of the cavity is an elliptical shape whose major axis extends along the downstream direction of the swirl from the vicinity of the fuel injection valve, the flow of the entire swirl generated in the cylinder is reduced within the cavity. This facilitates the concentration of the fuel spray near the spark plug, thereby further improving the ignitability.

【0020】請求項6の発明では、キャビティの平面形
状を、部分的に排気ポート側傾斜面に突出した円形状と
してあるので、キャビティ内のスワールが減衰しにく
く、それだけ点火プラグ近傍への燃料輸送機会が増大し
て着火性が良好になるとともに活発な燃焼が得られる。
またピストンの加工も容易である。
According to the sixth aspect of the present invention, since the planar shape of the cavity is a circular shape partially projecting from the inclined surface on the exhaust port side, the swirl in the cavity is hardly attenuated, and the fuel is transported to the vicinity of the ignition plug accordingly. Opportunity is increased, ignitability is improved, and active combustion is obtained.
Also, machining of the piston is easy.

【0021】請求項7の発明では、燃料噴射弁を、その
噴霧中心が、キャビティの排気ポート側傾斜面への突出
部を指向するように設けたものとしたことより、キャビ
ティ主要部に衝突して点火プラグ方向に案内すべき燃料
噴霧の割合を調整しつつ噴射燃料の多くを確実にキャビ
ティ内に確保しておくことが可能となる。
According to the seventh aspect of the present invention, the fuel injection valve is provided so that the spray center thereof is directed to the protruding portion of the cavity toward the exhaust port side inclined surface. While adjusting the proportion of the fuel spray to be guided in the direction of the spark plug, most of the injected fuel can be reliably secured in the cavity.

【0022】[0022]

【発明の実施の形態】以下、本発明のいくつかの実施の
形態につき図面に基づいて説明する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Some embodiments of the present invention will be described below with reference to the drawings.

【0023】図1、図2はこの発明の一実施形態を示し
ている。まず構成を説明すると、1はピストン、2はシ
リンダ内に直接燃料を噴射する噴射弁、3は点火プラ
グ、4はシリンダ、5はシリンダヘッド、6はピストン
上面に形成されたキャビティを示す。また7は吸気弁、
8は排気弁であり本実施形態では吸気弁7、排気弁8は
それぞれ2本づつ備えられた4弁形式である。点火プラ
グ3は前記吸排気弁間の燃焼室12の略中央部に位置し
ている。9a,9bは吸気ポート、10a,10bは前
記各ポート9a,9bに接続された吸気マニホールド、
11は一方の吸気マニホールド10bに介装されたスワ
ール発生手段としての吸気制御弁、12は燃焼室、13
a,13bは排気ポートを示している。
FIG. 1 and FIG. 2 show an embodiment of the present invention. First, the structure will be described. 1 is a piston, 2 is an injection valve for directly injecting fuel into a cylinder, 3 is a spark plug, 4 is a cylinder, 5 is a cylinder head, and 6 is a cavity formed on the upper surface of the piston. 7 is an intake valve,
Reference numeral 8 denotes an exhaust valve. In this embodiment, each of the intake valve 7 and the exhaust valve 8 is a four-valve type provided with two each. The ignition plug 3 is located substantially at the center of the combustion chamber 12 between the intake and exhaust valves. 9a and 9b are intake ports, 10a and 10b are intake manifolds connected to the ports 9a and 9b,
Reference numeral 11 denotes an intake control valve as a swirl generating means interposed in one intake manifold 10b, 12 denotes a combustion chamber, 13
Reference numerals a and 13b denote exhaust ports.

【0024】上記吸気制御弁11は予め定められた比較
的負荷及び回転数の低い運転域で閉弁保持され、この場
合図2で反時計方向のスワールを生起する。
The intake control valve 11 is kept closed in a predetermined operating range where the load and the number of revolutions are relatively low. In this case, a swirl is generated in a counterclockwise direction in FIG.

【0025】ピストン1の上面は、点火プラグ3の直下
部分を境界として吸気ポート9a,9b側の傾斜面1A
と排気ポート13a,13b側の傾斜面1Bとからなる
隆起形状となっている。
The upper surface of the piston 1 has a slope 1A on the intake port 9a, 9b side with the boundary immediately below the spark plug 3 as a boundary.
And an inclined surface 1B on the exhaust port 13a, 13b side.

【0026】キャビティ6は、この場合図2に示したよ
うにその主要部6Aの平面形状は円形であり、該円形の
中心はほぼ燃料噴霧の中心線上に位置している。ただ
し、このキャビティ6はスワール下流域となる一部が排
気ポート側傾斜面1B内に膨出して開口する部分(以下
「拡張部6B」という。)を有している。
In this case, as shown in FIG. 2, the cavity 6 has a main part 6A having a circular planar shape, and the center of the circle is located substantially on the center line of the fuel spray. However, the cavity 6 has a portion (hereinafter, referred to as an “expansion portion 6B”) in which a part of the swirl downstream region swells and opens inside the exhaust port side inclined surface 1B.

【0027】成層燃焼時における新気は、吸気行程にお
いて、吸気マニホールド10bに設けられた吸気制御弁
11が、吸気ポート9bからの新気導入を抑制するた
め、略直線形状に形成された吸気ポート9aより選択的
に流入し、吸気マニホールド10aおよび吸気ポート9
aでの流入抵抗が小さな状態で、シリンダ4内に旋回流
を発生させる。キャビティ6内のスワールは前記シリン
ダ内旋回流が、吸気および圧縮行程にかけてキャビティ
6内に導入されることにより発生する。また、成層燃焼
時における燃料は、圧縮行程においてキャビティ6の底
面を指向するように噴射弁2により噴射される。
During the stratified charge combustion, the fresh air is supplied to an intake port formed in a substantially linear shape so that the intake control valve 11 provided in the intake manifold 10b suppresses the introduction of fresh air from the intake port 9b during the intake stroke. 9a, the intake manifold 10a and the intake port 9
A swirl flow is generated in the cylinder 4 with the inflow resistance at a being small. The swirl in the cavity 6 is generated by the swirl flow in the cylinder being introduced into the cavity 6 during the intake and compression strokes. In addition, fuel during stratified combustion is injected by the injection valve 2 so as to face the bottom surface of the cavity 6 during the compression stroke.

【0028】次に作用を説明する。Next, the operation will be described.

【0029】図2に示したように、吸気ポート側に位置
する燃料噴射弁2から噴射された燃料噴霧の一部は対向
するキャビティ内壁面に衝突する。キャビティ主要部6
Aは隆起形状の境界部分(稜線L)に近接して吸気ポー
ト側傾斜面1Aに位置しているため、前記燃料噴霧が衝
突する内壁面はピストン上面までの高さが最も高く、か
つ燃焼室12の中央部に近い。このため、前記キャビテ
ィ対向壁面に衝突してキャビティ外へと上昇した燃料噴
霧が点火プラグ3付近へと集中し(図2のF部参照)、
点火プラグ3の近傍に濃混合気層を形成する。これによ
り、ピストン1が上死点に達するよりも早期に着火可能
となるため、適切な点火時期を設定して成層燃焼に特有
の良好な燃費性能とともに高出力を発揮させることが可
能となる。
As shown in FIG. 2, a part of the fuel spray injected from the fuel injection valve 2 located on the intake port side collides with the opposed inner wall surface of the cavity. Main part of cavity 6
Since A is located on the intake port side inclined surface 1A close to the boundary portion (ridge line L) of the raised shape, the inner wall surface against which the fuel spray collides has the highest height up to the piston upper surface and the combustion chamber. Close to the center of 12. For this reason, the fuel spray that collides with the cavity facing wall surface and rises out of the cavity concentrates near the spark plug 3 (see the F portion in FIG. 2).
A rich mixture layer is formed near the ignition plug 3. As a result, the piston 1 can be ignited earlier than reaching the top dead center, so that it is possible to set an appropriate ignition timing and exhibit high fuel economy performance and high output unique to stratified combustion.

【0030】一方、燃料噴霧の一部はスワールにより該
スワールの下流方向へと輸送されるが、このときキャビ
ティ6がスワール下流方向について排気ポート側傾斜面
1Bに突出した拡張部6Bを有しているため、スワール
に対して点火プラグ3の上流側のキャビティ6内に多く
の燃料を確保しておくことができ、これにより濃混合気
層を維持しつつキャビティ6内の吸気流動を活用して良
好な燃焼性能が得られる。
On the other hand, a part of the fuel spray is transported by the swirl in the downstream direction of the swirl. At this time, the cavity 6 has an expanded portion 6B protruding from the exhaust port side inclined surface 1B in the swirl downstream direction. Therefore, a large amount of fuel can be ensured in the cavity 6 on the upstream side of the spark plug 3 with respect to the swirl, and the intake air flow in the cavity 6 can be utilized while maintaining a rich mixture layer. Good combustion performance is obtained.

【0031】図3と図4にそれぞれ本発明の第2、第3
の実施の形態を示す。図3は、キャビティ6の平面形状
を、長軸が燃料噴射弁2の付近からスワール下流方向に
沿うように形成した楕円形状とし、その一部を拡張部6
Bとして排気ポート側傾斜面1B内に突出させたもの、
図4はキャビティ6の平面形状を、一部を拡張部6Bと
して排気ポート側傾斜面1Bに突出させた円形状とした
ものである。
FIGS. 3 and 4 show the second and third embodiments of the present invention, respectively.
An embodiment will be described. FIG. 3 shows that the planar shape of the cavity 6 is an elliptical shape formed so that the long axis extends from the vicinity of the fuel injection valve 2 to the swirl downstream direction, and a part of the extended portion 6
B projecting into the exhaust port side inclined surface 1B as B,
FIG. 4 shows a plan view of the cavity 6 in which a part of the cavity 6 is formed into a circular shape with the extended portion 6B protruding from the exhaust port side inclined surface 1B.

【0032】図3の実施形態によれば、燃料噴射弁2の
直下からスワール下流方向に沿った楕円形状のキャビテ
ィ形状としてあるので、シリンダ内に生じるスワール全
体の流れがキャビティ6内に導入されやすく、これによ
り点火プラグ3付近への燃料噴霧の集中を促して着火性
をより向上させることができる。また、図4の実施形態
によれば、キャビティ6の平面形状を、部分的に排気ポ
ート側傾斜面1Bに突出した円形状としてあるので、キ
ャビティ内のスワールが減衰しにくく、それだけ点火プ
ラグ3近傍への燃料輸送機会が増大して着火性が良好に
なるとともに活発な燃焼が得られる。またピストン1の
加工が容易であるという利点もある。
According to the embodiment of FIG. 3, since the elliptical cavity shape extends from immediately below the fuel injection valve 2 to the swirl downstream direction, the entire swirl flow generated in the cylinder is easily introduced into the cavity 6. Thereby, the concentration of the fuel spray near the ignition plug 3 is promoted, and the ignitability can be further improved. Further, according to the embodiment of FIG. 4, since the planar shape of the cavity 6 is a circular shape partially projecting to the exhaust port side inclined surface 1B, the swirl in the cavity is hardly attenuated, and accordingly the vicinity of the spark plug 3 The opportunity for transporting fuel to the fuel cell increases, the ignitability is improved, and active combustion is obtained. There is also an advantage that machining of the piston 1 is easy.

【0033】図5〜図7は本発明の第4〜第6の実施形
態を示しており、それぞれキャビティ6の形状として
は、図5は図2のものに、図6は図3のものに、図7は
図4の物に、それぞれ対応している。ただし、これらの
実施形態は、ピストン上面の稜線Lつまり吸気ポート側
傾斜面1Aと排気ポート側傾斜面1Bの境界を燃焼室1
2中央部よりも吸気ポート9側に偏った位置に設定して
ある点で先の実施形態とは異なる。
FIGS. 5 to 7 show fourth and sixth embodiments of the present invention. The shapes of the cavities 6 are shown in FIGS. 5 and 6, respectively, and FIG. , FIG. 7 respectively correspond to those of FIG. However, in these embodiments, the ridge line L of the piston upper surface, that is, the boundary between the intake port side inclined surface 1A and the exhaust port side inclined surface 1B is defined by the combustion chamber 1
2 is different from the previous embodiment in that the position is set closer to the intake port 9 side than the center.

【0034】これらの実施形態によれば、燃焼室12内
でのキャビティ6の容量が比較的小となるので、ボア・
ストローク比の比較的大きい機関において、キャビティ
6内での燃料の分散を規制し、混合気の層状化を維持し
て良好な燃費性能を確保することができる。
According to these embodiments, since the capacity of the cavity 6 in the combustion chamber 12 is relatively small, the bore
In an engine having a relatively large stroke ratio, the dispersion of fuel in the cavity 6 can be regulated, and the stratification of the air-fuel mixture can be maintained to ensure good fuel economy.

【0035】図8〜図10は本発明の第7〜第9の実施
形態を示しており、それぞれキャビティ6の形状として
は、図8は図2のものに、図9は図3のものに、図10
は図4の物に、それぞれ対応している。ただし、これら
の実施形態は、ピストン上面の稜線Lを燃焼室12中央
部よりも排気ポート13側に偏った位置に設定してある
点で先の実施例とは異なる。
FIGS. 8 to 10 show seventh to ninth embodiments of the present invention. The shapes of the cavities 6 are shown in FIG. 8 and FIG. 3, respectively. , FIG.
Respectively correspond to those in FIG. However, these embodiments are different from the preceding embodiments in that the ridge line L on the upper surface of the piston is set at a position closer to the exhaust port 13 side than the center of the combustion chamber 12.

【0036】これらの実施形態によれば、燃料噴射弁2
からキャビティ6の対向壁面までの距離が大きくなるの
で噴射されてからキャビティ壁面に衝突するまでの燃料
気化時間が長期化して未燃HCやスモークがそれだけ低
減する効果が期待できる。また、ボア・ストローク比の
比較的小さい機関において燃料噴霧を保持しうるだけの
キャビティ容量を確保できるという利点もある。
According to these embodiments, the fuel injection valve 2
Therefore, the effect that the fuel vaporization time from injection to collision with the cavity wall surface is prolonged and unburned HC and smoke are reduced accordingly can be expected. Another advantage is that a cavity capacity sufficient to hold fuel spray can be ensured in an engine having a relatively small bore / stroke ratio.

【0037】ところで、上記各実施形態において、その
燃料噴射弁2の向きを、噴霧中心がキャビティ拡張部6
Bを指向するよう設定することができる。これにより、
キャビティ主要部6Aの壁面に衝突して点火プラグ3方
向に案内すべき燃料噴霧の割合を調整しつつ噴射燃料の
多くを確実にキャビティ6内に確保して層状燃焼の効果
を高めることができる。
In each of the above embodiments, the direction of the fuel injection valve 2 is adjusted so that the spray center is
B can be set to point. This allows
While adjusting the proportion of the fuel spray to be guided toward the spark plug 3 by colliding with the wall surface of the cavity main portion 6A, most of the injected fuel can be reliably secured in the cavity 6 to enhance the effect of stratified combustion.

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

【図1】 本発明による筒内噴射式機関の第1の実施形
態を示す概略縦断面図。
FIG. 1 is a schematic longitudinal sectional view showing a first embodiment of a direct injection engine according to the present invention.

【図2】 第1の実施形態のピストンの平面図。FIG. 2 is a plan view of a piston according to the first embodiment.

【図3】 本発明の第2の実施形態のピストンの平面
図。
FIG. 3 is a plan view of a piston according to a second embodiment of the present invention.

【図4】 本発明の第3の実施形態のピストンの平面
図。
FIG. 4 is a plan view of a piston according to a third embodiment of the present invention.

【図5】 本発明の第4の実施形態のピストンの平面
図。
FIG. 5 is a plan view of a piston according to a fourth embodiment of the present invention.

【図6】 本発明の第5の実施形態のピストンの平面
図。
FIG. 6 is a plan view of a piston according to a fifth embodiment of the present invention.

【図7】 本発明の第6の実施形態のピストンの平面
図。
FIG. 7 is a plan view of a piston according to a sixth embodiment of the present invention.

【図8】 本発明の第7の実施形態のピストンの平面
図。
FIG. 8 is a plan view of a piston according to a seventh embodiment of the present invention.

【図9】 本発明の第8の実施形態のピストンの平面
図。
FIG. 9 is a plan view of a piston according to an eighth embodiment of the present invention.

【図10】 本発明の第9の実施形態のピストンの平面
図。
FIG. 10 is a plan view of a piston according to a ninth embodiment of the present invention.

【符号の説明】[Explanation of symbols]

1 ピストン 1A 吸気ポート側傾斜面 1B 排気ポート側傾斜面 2 燃料噴射弁 3 点火プラグ 4 シリンダ 5 シリンダヘッド 6 キャビティ 6A キャビティ主要部 6B キャビティ拡張部 7 吸気バルブ 8 排気バルブ 9a,9b 吸気ポート 10a,10b 吸気マニホールド 11 吸気制御弁 12 燃焼室 13a,13b 排気ポート L 傾斜面の境界(稜線) Reference Signs List 1 piston 1A intake port side inclined surface 1B exhaust port side inclined surface 2 fuel injection valve 3 spark plug 4 cylinder 5 cylinder head 6 cavity 6A main cavity 6B cavity extension 7 intake valve 8 exhaust valve 9a, 9b intake port 10a, 10b Intake manifold 11 Intake control valve 12 Combustion chamber 13a, 13b Exhaust port L Boundary of slope (ridgeline)

Claims (7)

【特許請求の範囲】[Claims] 【請求項1】 対向的に配置された吸気ポートと排気ポ
ートとの間の燃焼室略中央部に点火プラグを位置させる
とともに、上面に平面上略円形のキャビティを形成した
ピストンと、吸気ポート側から前記キャビティに向けて
燃料を噴射供給する燃料噴射弁と、シリンダ内にスワー
ルを発生させる手段とを備えた内燃機関において、 ピストン上面を、吸気ポートに面した傾斜面と排気ポー
トに面した傾斜面とからなる隆起形状とするとともに、 前記キャビティを、その主要部が前記各傾斜面の境界部
分に近接して吸気ポート側傾斜面内に開口するように、
かつスワールに対して点火プラグの上流側となる領域の
みが部分的に排気ポート側傾斜面内に開口するように、
形成したことを特徴とする筒内燃料噴射式内燃機関。
A piston having a substantially circular cavity formed on a top surface thereof, a piston located at a substantially central portion of a combustion chamber between an intake port and an exhaust port disposed opposite to each other; An internal combustion engine comprising: a fuel injection valve for injecting fuel from the cavity toward the cavity; and a means for generating a swirl in the cylinder, wherein a piston upper surface has an inclined surface facing an intake port and an inclined surface facing an exhaust port. And the cavity has a main portion which is opened in the intake port side inclined surface in the vicinity of a boundary portion between the inclined surfaces.
And so that only the region on the upstream side of the spark plug with respect to the swirl partially opens into the exhaust port side inclined surface,
An in-cylinder fuel injection type internal combustion engine characterized by being formed.
【請求項2】 吸気ポート側傾斜面と排気ポート側傾斜
面の境界を燃焼室中央部よりも吸気ポート側に偏った位
置に設定したことを特徴とする請求項1に記載の筒内燃
料噴射式内燃機関。
2. The in-cylinder fuel injection according to claim 1, wherein the boundary between the intake port side inclined surface and the exhaust port side inclined surface is set at a position deviated toward the intake port side from the center of the combustion chamber. Type internal combustion engine.
【請求項3】 吸気ポート側傾斜面と排気ポート側傾斜
面の境界を燃焼室中央部よりも排気ポート側に偏った位
置に設定したことを特徴とする請求項1に記載の筒内燃
料噴射式内燃機関。
3. The in-cylinder fuel injection according to claim 1, wherein the boundary between the intake port side inclined surface and the exhaust port side inclined surface is set at a position deviated toward the exhaust port side from the center of the combustion chamber. Type internal combustion engine.
【請求項4】 キャビティは、その主要部の平面形状が
円形であり、かつ排気ポート側傾斜面内に開口する部分
が前記円形状から膨出した態様で形成されていることを
特徴とする請求項1から請求項3の何れかに記載の筒内
燃料噴射式内燃機関。
4. The cavity according to claim 1, wherein a main portion thereof has a circular planar shape, and a portion that opens into the exhaust port-side inclined surface is formed in a manner bulging from the circular shape. An in-cylinder fuel injection type internal combustion engine according to any one of claims 1 to 3.
【請求項5】 キャビティは、その平面形状が、長軸が
燃料噴射弁付近からスワール下流方向に沿うように形成
された楕円形状であることを特徴とする請求項1から請
求項3の何れかに記載の筒内燃料噴射式内燃機関。
5. The cavity according to claim 1, wherein a plane shape of the cavity is an elliptical shape formed such that a major axis extends from a vicinity of the fuel injection valve to a swirl downstream direction. 8. The in-cylinder fuel injection internal combustion engine according to item 1.
【請求項6】 キャビティは、その平面形状が、部分的
に排気ポート側傾斜面に突出した円形状であることを特
徴とする請求項1から請求項3の何れかに記載の筒内燃
料噴射式内燃機関。
6. The in-cylinder fuel injection according to any one of claims 1 to 3, wherein the cavity has a planar shape that is partially circular and protrudes from the inclined surface on the exhaust port side. Type internal combustion engine.
【請求項7】 燃料噴射弁は、その噴霧中心が、キャビ
ティの排気ポート側傾斜面への突出部を指向するように
設けられていることを特徴とする請求項1から請求項6
の何れかに記載の筒内燃料噴射式内燃機関。
7. The fuel injection valve according to claim 1, wherein a spray center of the fuel injection valve is provided so as to point to a protruding portion of the cavity toward the inclined surface on the exhaust port side.
The in-cylinder fuel injection type internal combustion engine according to any one of the above.
JP14764497A 1997-06-05 1997-06-05 In-cylinder fuel injection internal combustion engine Expired - Lifetime JP4291423B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14764497A JP4291423B2 (en) 1997-06-05 1997-06-05 In-cylinder fuel injection internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14764497A JP4291423B2 (en) 1997-06-05 1997-06-05 In-cylinder fuel injection internal combustion engine

Publications (2)

Publication Number Publication Date
JPH10339142A true JPH10339142A (en) 1998-12-22
JP4291423B2 JP4291423B2 (en) 2009-07-08

Family

ID=15435007

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14764497A Expired - Lifetime JP4291423B2 (en) 1997-06-05 1997-06-05 In-cylinder fuel injection internal combustion engine

Country Status (1)

Country Link
JP (1) JP4291423B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1111216A2 (en) * 1999-12-21 2001-06-27 Ford Global Technologies, Inc. Combustion chamber for DISI engines with swirl airflows

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1111216A2 (en) * 1999-12-21 2001-06-27 Ford Global Technologies, Inc. Combustion chamber for DISI engines with swirl airflows

Also Published As

Publication number Publication date
JP4291423B2 (en) 2009-07-08

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