JPS5979032A - Direct-injection type diesel engine - Google Patents

Direct-injection type diesel engine

Info

Publication number
JPS5979032A
JPS5979032A JP57189234A JP18923482A JPS5979032A JP S5979032 A JPS5979032 A JP S5979032A JP 57189234 A JP57189234 A JP 57189234A JP 18923482 A JP18923482 A JP 18923482A JP S5979032 A JPS5979032 A JP S5979032A
Authority
JP
Japan
Prior art keywords
fuel
combustion chamber
forming
recess
piston
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
JP57189234A
Other languages
Japanese (ja)
Inventor
Shiro Ishida
石田 史郎
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.)
Isuzu Motors Ltd
Original Assignee
Isuzu Motors 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 Isuzu Motors Ltd filed Critical Isuzu Motors Ltd
Priority to JP57189234A priority Critical patent/JPS5979032A/en
Publication of JPS5979032A publication Critical patent/JPS5979032A/en
Pending 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
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0672Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis
    • 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
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/0648Means or methods to improve the spray dispersion, evaporation or ignition
    • F02B23/0651Means or methods to improve the spray dispersion, evaporation or ignition the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space
    • 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
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/0669Details related to the fuel injector or the fuel spray having multiple fuel spray jets per injector nozzle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14Direct injection into combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0621Squish flow
    • 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
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0624Swirl flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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
    • F02F2001/244Arrangement of valve stems in cylinder heads
    • F02F2001/247Arrangement of valve stems in cylinder heads the valve stems being orientated in parallel with the cylinder axis
    • 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)
  • Dispersion Chemistry (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

PURPOSE:To prevent generation of noises due to ignition lag and to reduce generation of hydrocarbon, by forming a combustion chamber by forming a recess in the top surface of a piston and forming a projection by projecting the central part of the bottom of said recess upward. CONSTITUTION:A combustion chamber 4 is formed by forming a recess in the top surface 2 of a piston 1 and forming a projection 3 by projecting the central part of the bottom of said recess upward. Fuel is injected from main injection holes 13 toward the side wall 7 of the recess, and the atomized fuel is mixed with compressed air by the function of swirl produced in the combustion chamber 4. Here, since the inner wall surface 11 is located at a fairly small distance from a subsidiary injection hole 14 and fuel ejected onto the inner wall surface 11 is scattered after collision to the same, fuel is atomized into fine particles and vaporized instaneously. During the above while, the piston is raised to a position corresponding to a crank angle C and the temperature of air is raised to the ignition temperature. Since the above while, i.e., the ignition lag T1 is lessened, pressure rise in the cylinder is made smooth, so that production of noises can be reduced.

Description

【発明の詳細な説明】 〔発明の技術分野〕 本発明は、直接噴射式ディーゼル機関に係退、特に、着
火遅tl17c伴う騒音の発生を可及的に防止すること
ができると共に、炭化水素の発生を低減することができ
る直接噴射式ディーゼル機関に関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention is capable of preventing as much as possible the generation of noise associated with ignition delay tl17c in a direct injection diesel engine. The present invention relates to a direct injection diesel engine that can reduce generation.

〔発明の技術的背景とその問題点〕[Technical background of the invention and its problems]

一般に直接噴射式ディーゼル機関(以下、直噴式ディー
ゼル機関と呼ぶ)にあってはピストンが上死点に達した
とき燃料が噴射ノズルから燃焼室に直接噴射さnる。こ
のとき、燃料と圧縮空気とを充分に混合させるために、
燃焼室に圧縮空気の渦流を生じさせるように構成さルて
いる。即ち、第1図に示す如く、ピストン10頭頂面2
が空洞状に陥没さt1且つその陥没部の底部略中央が上
方に突出さtて突起部3を形成し、トロイダル型燃焼室
4(以下、単に燃焼室と呼ぶ)が構成さルている。ピス
トン1がシリンダ5内の空気を圧縮すべく上昇すると、
この燃焼室4内で渦流が生じ、この渦流が生じている所
へ燃料が噴射ノズル6よジ噴射されるので圧縮空気と燃
料とは充分に混合することができる。
Generally, in a direct injection diesel engine (hereinafter referred to as a direct injection diesel engine), fuel is directly injected from an injection nozzle into a combustion chamber when the piston reaches top dead center. At this time, in order to mix the fuel and compressed air sufficiently,
The combustion chamber is configured to create a vortex of compressed air in the combustion chamber. That is, as shown in FIG.
is depressed into a hollow shape t1, and the approximate center of the bottom of the depression protrudes upward to form a protrusion 3, thereby forming a toroidal combustion chamber 4 (hereinafter simply referred to as a combustion chamber). When the piston 1 rises to compress the air in the cylinder 5,
A vortex is generated within the combustion chamber 4, and fuel is injected through the injection nozzle 6 into the area where the vortex is generated, so that the compressed air and fuel can be sufficiently mixed.

ところで、直噴式ディーゼル機関はシリンダ圧力の上昇
率が高いため、一般的に着火遅nが太きい。着火遅汎が
非常に大きいときは、機関の作動が円滑でなく、音が高
くなる。即ち、着火遅nの間に噴射さ2tた燃料のほと
んど全部が蓄積さnて一度に燃焼し、この急激な燃焼に
伴う圧力の急激な上昇により圧力波が生じ、そ扛がシリ
ンダ壁に衝突して音を発生することになる。着火遅f′
Lを短くするには圧縮比を大きくすることが考えら几る
が、シリンダ圧力が高いと燃料が霧化しにくくなり、未
燃焼あるいは不完全燃焼による炭化水素が排ガス中含有
成分として増大する問題がある。更には一定の軸有効仕
事量に対してシリンダの行程体積が増えるため軸平均有
効圧は低下し、軸トルク、軸馬力の低減も免汎ない問題
となる。
By the way, since a direct injection diesel engine has a high rate of increase in cylinder pressure, the ignition delay n is generally large. When the ignition delay is very large, the engine will not operate smoothly and will be noisy. In other words, almost all of the 2 tons of fuel injected during the ignition delay n accumulates and burns at once, and the sudden rise in pressure accompanying this rapid combustion creates a pressure wave, which collides with the cylinder wall. This will generate sound. Ignition delay f′
In order to shorten L, increasing the compression ratio can be considered, but if the cylinder pressure is high, it becomes difficult to atomize the fuel, and there is a problem that hydrocarbons due to unburned or incomplete combustion will increase as a component in the exhaust gas. be. Furthermore, since the stroke volume of the cylinder increases for a constant amount of shaft effective work, the shaft average effective pressure decreases, resulting in an inevitable reduction in shaft torque and shaft horsepower.

また、従来の燃焼室では第2図に示す如く、燃焼室4の
側壁面7に向かって燃料が噴射さnておジ、側壁面7に
衝突してからの噴霧燃料の粒径小化は、着火遅′n、’
i充分に解決するだけの効果に乏しい。即ち、噴射ノズ
ルから噴射さnた燃料が側壁面1に到達する前にすでに
着火は終了しており、捷た側啼面γ上では噴霧燃料のこ
nに衝突する勢いかすでに減衰さ汎て、充分にその粒径
小化がなさnないのである。
In addition, in the conventional combustion chamber, as shown in FIG. 2, fuel is injected toward the side wall surface 7 of the combustion chamber 4, and the particle size of the sprayed fuel decreases after colliding with the side wall surface 7. , ignition delay 'n,'
i It is not effective enough to solve the problem. That is, before the fuel injected from the injection nozzle reaches the side wall surface 1, ignition has already been completed, and the momentum of the sprayed fuel colliding with the side wall surface γ has already been attenuated. However, the particle size is not sufficiently reduced.

〔発明の目的〕[Purpose of the invention]

本発明は上述の如き問題点に鑑み、こnらを有効に解決
すべく創案さnたものである。
The present invention has been devised in view of the above problems and to effectively solve them.

本発明の目的は、着火遅几に伴う騒音の発生を防止する
ことができると共に、炭化水素の発生全低減することが
できる直接噴射式ディーゼル機関を提供することにある
SUMMARY OF THE INVENTION An object of the present invention is to provide a direct injection diesel engine that can prevent the generation of noise caused by delayed ignition and can completely reduce the generation of hydrocarbons.

〔発明の実施例〕[Embodiments of the invention]

以下、本発明の好適一実施例について添付図面に従って
説明する。
A preferred embodiment of the present invention will be described below with reference to the accompanying drawings.

本発明に係る直噴式ディーゼル機関は第3図に示す如く
、ピストン1の頭頂面2が空洞状に陥没さnており、こ
の陥没部の底部略中央は上方に突出さnて突起部3全形
成し、燃焼室4が構成さ几ている。
In the direct injection diesel engine according to the present invention, as shown in FIG. A combustion chamber 4 is formed.

燃焼室4の上方にはこnに臨んで噴射ノズル6が、シリ
ンダヘッド8のノズル孔9内に挿着さnて設けらnてい
る。このノズル孔9の下端部は、その下方へ噴射ノズル
6の先端部10の径よりも漸次拡径さnるように面取り
さnている。従って噴射ノズル6の先端部10周辺には
、上記面取りさnた面を内壁11としてこの噴射ノズル
6を内包し且つ燃焼室4に臨んで開放さnた室12が形
成さnる。
An injection nozzle 6 is provided above the combustion chamber 4 and is inserted into a nozzle hole 9 of a cylinder head 8. The lower end of the nozzle hole 9 is chamfered so that its diameter gradually increases downwardly from the diameter of the tip 10 of the injection nozzle 6. Therefore, a chamber 12 is formed around the tip 10 of the injection nozzle 6, which has the chamfered surface as the inner wall 11, encloses the injection nozzle 6, and is open facing the combustion chamber 4.

噴射ノズル6の先端部10には、燃焼室4の側壁面7上
に向って燃料を噴射すべく主噴口13が複数と、上記室
12の内壁11面、に、VC向って燃料を噴射すべく副
噴口14とが設けらnている。副噴口14の口径は主噴
口13のそnに対して小さく設定さ九ており、互いの噴
出量を制御するように構成さnている。
The tip 10 of the injection nozzle 6 has a plurality of main injection ports 13 for injecting fuel toward the side wall surface 7 of the combustion chamber 4, and a plurality of main injection ports 13 for injecting fuel toward the VC toward the inner wall 11 surface of the chamber 12. A sub-nozzle 14 is also provided. The diameter of the sub-nozzle 14 is set smaller than that of the main nozzle 13, and the two are configured to control each other's ejection amounts.

社に本発明の作用について説明する。The effect of the present invention will be explained to the company.

第5図は本発明に係る直噴式ディーゼル機関の着火燃焼
のノロセスを従来のものと比較したグラフ図である。図
中、縦軸はシリンダ内圧力と、ニードル弁リフト即ち、
噴射ノズル6の開閉とを示し、ニードル弁リフト0は開
状態、Sは閉状態を表わしている。横軸はクランク角度
を示し、Dは上死点位置を表わす。
FIG. 5 is a graph comparing the ignition combustion process of the direct injection diesel engine according to the present invention with that of a conventional engine. In the figure, the vertical axis represents the cylinder pressure and the needle valve lift, i.e.
The opening and closing of the injection nozzle 6 are shown, with needle valve lift 0 representing an open state and S representing a closed state. The horizontal axis indicates the crank angle, and D indicates the top dead center position.

圧縮行程に従ってピストン1は上昇し、こnに伴ってシ
リンダ内圧力も上昇する。このとき、燃焼室4内では、
圧縮空気が渦流を形成していく。
The piston 1 rises according to the compression stroke, and the pressure inside the cylinder also rises accordingly. At this time, inside the combustion chamber 4,
Compressed air forms a vortex.

クランク角度Aの位置までピストン1が上昇したとき噴
射ノズル6が開かn、第3図に示す如く燃料が燃焼室4
内に噴射さnる。主噴口13からは側壁面7vC向けて
噴射し、燃焼室4内に生じている渦流によって圧縮空気
と霧化した燃料とが混合する。副噴口14からは室12
の内壁11面に向けて噴射する。この内壁11面は副噴
口14から充分に近い距離にあり、こf’LK吹き付け
らnる燃料はその勢いが強く、内壁11面に衝突したの
ち飛散し、微細な液滴群となって瞬時に気化する。
When the piston 1 rises to the position of the crank angle A, the injection nozzle 6 opens, and the fuel flows into the combustion chamber 4 as shown in FIG.
Inject inside. The main injection port 13 injects toward the side wall surface 7vC, and the vortex generated within the combustion chamber 4 mixes compressed air and atomized fuel. From the sub-nozzle 14, the chamber 12
The liquid is injected toward the inner wall 11 of the This inner wall 11 is located at a sufficiently close distance from the sub-nozzle 14, and the fuel sprayed by this f'LK has a strong force, and after colliding with the inner wall 11, it scatters, forming a group of fine droplets and instantaneously. vaporizes into

第4図ではこの間にクランク角度Cまでピストン1が上
昇しており、シリンダ内圧力は上昇し、圧縮空気の温度
が着火温度に達している。この間が着火遅へで、本発明
によればTI となる。尚、図中Toは従来例による着
火遅nで、クランク角はAからEまでの時間を要する。
In FIG. 4, during this period, the piston 1 has risen to the crank angle C, the pressure inside the cylinder has increased, and the temperature of the compressed air has reached the ignition temperature. This period is the ignition delay, and according to the present invention, it is TI. In the figure, To is the ignition delay n according to the conventional example, and the crank angle requires time from A to E.

A、B間は燃料噴対時間。The period between A and B is the fuel injection time.

着火遅九が小さくなることによってシリンダ内圧力の上
昇も滑らかになり、従って騒音は大幅に低減することが
できる。
By reducing the ignition delay, the increase in cylinder pressure becomes smoother, and therefore noise can be significantly reduced.

また、主噴口13から噴射さ几た燃料は、着火が早くな
ることによって側壁面7に到達する前にその気化が促進
さn、、霧化燃料(液滴状態)が比較的低温の側壁面7
に達する割合は低減さルることになる。従って不完全燃
焼あるいは未燃焼による炭化水素の発生も低減さnる。
Furthermore, the vaporization of the atomized fuel injected from the main nozzle 13 is accelerated before it reaches the side wall surface 7 due to its early ignition. 7
The rate at which this happens will be reduced. Therefore, generation of hydrocarbons due to incomplete combustion or unburned combustion is also reduced.

〔発明の効果〕〔Effect of the invention〕

以上の説明よジ明らかなように本発明によnば次の如き
優nた効果が発揮される。
As is clear from the above explanation, the present invention provides the following excellent effects.

1 着火遅nf可及的に短縮することができ、着火遅へ
に伴う騒音の発生を低減することができる。
1. The ignition delay nf can be shortened as much as possible, and the generation of noise caused by the ignition delay can be reduced.

2、燃焼室内に噴射さnた燃料の気化を促進することに
より、排ガス中に含まnる炭化水素全低減することがで
きる。
2. By promoting the vaporization of the fuel injected into the combustion chamber, the total amount of hydrocarbons contained in the exhaust gas can be reduced.

3 圧縮比が増大しないので、軸平均有効圧全維持する
ことができる。
3. Since the compression ratio does not increase, the entire axial average effective pressure can be maintained.

4 構造が簡単で容易に採用し得る。4. The structure is simple and can be easily adopted.

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

第1図は直接噴射式ディーゼル機関の概略構成図、第2
図は従来の燃料噴射状況を示すltl断面図、第3図は
本発明の一実施例における燃料噴射状況を示す側断面図
、第4図は本発明の一実施flJと従来例との着火・燃
焼プロセス全比較するグラフ図である。 尚、図中1はピストン、2は頭頂面、4は燃焼室、6は
噴射ノズル、8はシリンタ゛ヘッド、10は噴射ノズル
の先端部、12は室、11はその内壁である。 特許出願人 いすソ自動車株式会社 代理人 弁理士  絹  谷  信  雄第1図 第2図 @3図
Figure 1 is a schematic configuration diagram of a direct injection diesel engine, Figure 2
The figure is an ltl sectional view showing a conventional fuel injection situation, FIG. 3 is a side sectional view showing a fuel injection situation in an embodiment of the present invention, and FIG. FIG. 2 is a graph diagram comparing the entire combustion process. In the figure, 1 is a piston, 2 is a top surface, 4 is a combustion chamber, 6 is an injection nozzle, 8 is a cylinder head, 10 is a tip of the injection nozzle, 12 is a chamber, and 11 is its inner wall. Patent Applicant Isuso Jidosha Co., Ltd. Agent Patent Attorney Nobuo Kinutani Figure 1 Figure 2 @ Figure 3

Claims (1)

【特許請求の範囲】[Claims] ピストンの頭頂面に圧縮空気の渦流を生じさせるべく空
洞状に陥没したトロイダル型燃焼室を有すると共に、シ
リンダヘッドに、上記燃焼室に臨んで支持さnて設けら
nた多孔式噴射ノズルを有する直接噴射式ディーゼル機
関において、上記シリンダヘッドに、上記噴射ノズルの
先端部より、拡径さnると共に上記燃焼室に臨んで開放
さnた室を形成し、該室の内壁に燃料全衝突させて霧化
させるために上記噴射ノズルに副噴口を設けたことを特
徴とする直接噴射式ディーゼル機関。
It has a hollow toroidal combustion chamber on the top surface of the piston to generate a vortex flow of compressed air, and has a multi-hole injection nozzle supported on the cylinder head facing the combustion chamber. In the direct injection diesel engine, a chamber is formed in the cylinder head, the diameter of which is expanded from the tip of the injection nozzle, and which is open facing the combustion chamber, and all of the fuel impinges on the inner wall of the chamber. A direct injection diesel engine, characterized in that the injection nozzle is provided with a sub-nozzle for atomization.
JP57189234A 1982-10-29 1982-10-29 Direct-injection type diesel engine Pending JPS5979032A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57189234A JPS5979032A (en) 1982-10-29 1982-10-29 Direct-injection type diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57189234A JPS5979032A (en) 1982-10-29 1982-10-29 Direct-injection type diesel engine

Publications (1)

Publication Number Publication Date
JPS5979032A true JPS5979032A (en) 1984-05-08

Family

ID=16237842

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57189234A Pending JPS5979032A (en) 1982-10-29 1982-10-29 Direct-injection type diesel engine

Country Status (1)

Country Link
JP (1) JPS5979032A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05209527A (en) * 1992-01-31 1993-08-20 Hino Motors Ltd Combustion chamber of direct injection type diesel engine
KR20040032364A (en) * 2002-10-09 2004-04-17 현대자동차주식회사 Mounting apparatus for injector

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05209527A (en) * 1992-01-31 1993-08-20 Hino Motors Ltd Combustion chamber of direct injection type diesel engine
KR20040032364A (en) * 2002-10-09 2004-04-17 현대자동차주식회사 Mounting apparatus for injector

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