JPS632008B2 - - Google Patents
Info
- Publication number
- JPS632008B2 JPS632008B2 JP57068435A JP6843582A JPS632008B2 JP S632008 B2 JPS632008 B2 JP S632008B2 JP 57068435 A JP57068435 A JP 57068435A JP 6843582 A JP6843582 A JP 6843582A JP S632008 B2 JPS632008 B2 JP S632008B2
- Authority
- JP
- Japan
- Prior art keywords
- combustion chamber
- nozzle
- fuel
- recesses
- collision
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0636—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston the combustion space having a substantially flat and horizontal bottom
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0648—Means or methods to improve the spray dispersion, evaporation or ignition
- F02B23/0651—Means 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0669—Details related to the fuel injector or the fuel spray having multiple fuel spray jets per injector nozzle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0672—Omega-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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/14—Direct injection into combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/40—Squish effect
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0618—Other 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
- F02B23/0621—Squish flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/24—Cylinder heads
- F02F2001/244—Arrangement of valve stems in cylinder heads
- F02F2001/247—Arrangement of valve stems in cylinder heads the valve stems being orientated in parallel with the cylinder axis
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving 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)
Description
【発明の詳細な説明】
本発明は、ピストンの頂面に凹設した燃焼室に
燃料を直接噴射供給するようにしたデイーゼル機
関の燃焼室に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a combustion chamber of a diesel engine in which fuel is directly injected and supplied to a combustion chamber recessed in the top surface of a piston.
この種デイーゼル機関の燃焼室としては、例え
ば、特公昭49―16881号公報、特公昭51―42249号
公報に記載されたようなものがある。ここに、前
者は、燃料噴霧の衝突面である燃焼室の側面を渦
流の方向に傾斜させて空気の渦流を助長させるよ
うにしたものであり、後者は、燃料噴霧の衝突面
である燃焼室の側面を平面状にしてこれに燃料を
傾斜衝突させるようにしたものである。 Examples of the combustion chamber of this type of diesel engine include those described in Japanese Patent Publications No. 49-16881 and Japanese Patent Publication No. 42249-1982. Here, in the former case, the side surface of the combustion chamber, which is the collision surface of the fuel spray, is inclined in the direction of the vortex to promote the vortex flow of air. The side surface of the fuel tank is flat so that the fuel collides with it at an angle.
従つて、これらのものでは、いずれも燃料と空
気との混合性能がある程度改善されるという利点
がありながらも、前者の場合は燃焼室の側面に突
部が残つてヒートスポツトとなり易いため、この
突部がピストンの亀裂の起点となり、あるいは、
前記突部が溶損するおそれがあつた。又、後者の
場合は、燃焼室の側面にコーナーが残されるので
不完全燃焼を起して排気特性が悪化し易いという
不具合があつた。 Therefore, although all of these have the advantage of improving the mixing performance of fuel and air to some extent, the former leaves a protrusion on the side of the combustion chamber that tends to become a heat spot. The protrusion becomes the starting point for cracks in the piston, or
There was a risk that the protrusion would be damaged by melting. Moreover, in the latter case, corners are left on the side surfaces of the combustion chamber, which causes incomplete combustion and tends to deteriorate exhaust characteristics.
このような事態を回避するためには、例えば実
開昭56―2020号公報に見られるように、中心に向
つて延びる絞り部を燃焼室入口部の全周縁に設け
る一方、燃焼室の側面に設けた凹部の間に該側面
を面として残すことが有効である。 In order to avoid this situation, for example, as seen in Japanese Utility Model Application Publication No. 56-2020, a constriction extending toward the center is provided on the entire periphery of the inlet of the combustion chamber, while a constriction is provided on the side of the combustion chamber. It is effective to leave the side surfaces as surfaces between the provided recesses.
しかしながら、このような従来例においてさえ
も、凹部の数とノズルに設けた噴口の数とを一致
させることによつて各噴口から噴射された燃料噴
霧の衝突面の形状を画一化していたために、特定
の運転条件のもとにおいては燃料噴霧が理想的に
拡散して着火に適した性状の混合気が生成される
ものの、運転条件が変ると燃料噴霧の拡散条件が
変化して混合気の性状を変えてしまうので必ずし
も着火に適した性状の混合気を得ることができな
い場合があり、これにより、着火性が悪化して着
火遅れ期間が長くなつてしまうという問題点があ
つた。 However, even in such conventional examples, the shape of the impact surface of the fuel spray injected from each nozzle was standardized by matching the number of recesses and the number of nozzles provided in the nozzle. Under certain operating conditions, the fuel spray is ideally diffused and a mixture with properties suitable for ignition is produced, but if the operating conditions change, the fuel spray diffusion conditions change and the mixture is Since the properties change, it may not always be possible to obtain an air-fuel mixture with properties suitable for ignition, which has the problem of deteriorating ignition performance and lengthening the ignition delay period.
尚、このように各噴口に対応して凹部を設ける
場合は、ノズルの組立誤差によつても混合気の性
状が悪化して着火困難に陥るおそれもあつた。 In addition, when a concave portion is provided corresponding to each nozzle in this manner, there is also a risk that the properties of the air-fuel mixture may deteriorate due to nozzle assembly errors, resulting in difficulty in ignition.
本発明はこのような実情に鑑みてなされたもの
であり、中心に向う絞り部を燃焼室入口の全周縁
に設けると同時に、燃焼室の側面に複数個の凹部
を設け、これら凹部の間にそれぞれ燃焼室の側面
を少なくとも面として残している。又、前記凹部
の数とノズルに設けられた噴口の数とを異ならせ
ることにより、各噴口から噴射された燃料噴霧の
衝突面の形状を各衝突位置ごとに異ならせたこと
を特徴としている。 The present invention has been made in view of the above circumstances, and includes providing a constriction toward the center on the entire periphery of the entrance of the combustion chamber, and at the same time providing a plurality of recesses on the side surface of the combustion chamber, and providing space between these recesses. In each case, at least the sides of the combustion chamber remain as surfaces. Furthermore, by varying the number of the recesses and the number of nozzles provided in the nozzle, the shape of the collision surface of the fuel spray injected from each nozzle is made different for each collision position.
このように、燃焼室入口の全周縁に絞り部を設
けているのでスキツシユを得ることができ、しか
も、凹部を設けたことでスワールによる小渦流が
生成されるために、燃料噴霧と空気との混合性能
が改善される。又、燃料噴霧の衝突面の形状を衝
突位置ごとに異ならせているために常に種々の性
状の混合気が生成されることになり、いかなる運
転条件のもとにおいても少なくとも一箇所には着
火に適した性状の混合気が存在する。よつて、常
に第1期燃焼を小さく(着火遅れ期間を短縮)す
ることができ、燃焼によつて生じる排ガス成分を
減少させつつ燃料消費率を向上させることができ
る。 In this way, the constriction is provided around the entire periphery of the inlet of the combustion chamber, making it possible to obtain a tight squeeze.Furthermore, the provision of the concave portion generates a small vortex due to the swirl, which improves the interaction between the fuel spray and the air. Mixing performance is improved. In addition, because the shape of the impact surface of the fuel spray differs depending on the impact location, mixtures with various properties are always generated, and under any operating conditions, at least one spot will not be able to ignite. A mixture of suitable properties exists. Therefore, the first stage combustion can be kept small (the ignition delay period can be shortened), and the fuel consumption rate can be improved while reducing the exhaust gas components generated by combustion.
以下に本発明の実施例を図面に基づいて詳細に
説明する。 Embodiments of the present invention will be described in detail below based on the drawings.
図示しないシリンダ内で往復動するピストン1
の頂面には、中心に向つて延びる絞り部2を入口
部の全周縁に形成した燃焼室3を凹設しており、
図示しないシリンダヘツドには、前記燃焼室3の
側面に向つて燃料を噴射するノズル4を装着して
デイーゼル機関を構成している。 A piston 1 that reciprocates within a cylinder (not shown)
A combustion chamber 3 is recessed in the top surface of the combustion chamber, with a constriction part 2 extending toward the center formed around the entire periphery of the inlet part.
A nozzle 4 for injecting fuel toward the side surface of the combustion chamber 3 is attached to a cylinder head (not shown) to constitute a diesel engine.
又、前記燃焼室3の側面の複数箇所には、該側
面に連続する凹部5を設けると共に、隣接する凹
部5の間に前記側面を少なくとも面(側面)6と
して残している。この凹部5は、燃焼室3の側面
6を形成する曲面より半径の小さい曲面等で構成
され、凹部5と側面6との接続部を例えば円弧状
に削成して凹部5と側面6とを円滑に連続させる
が、隣接する凹部5の間には必ず側面6を残して
おく必要があり、この凹部5を形成することによ
り、絞り部2の幅を部分的に大きくしている。
尚、凹部5の数は、燃焼室3の大きさによつても
相違するが、ノズル4に設けられている噴口の数
より多く又は少なくすることにより、各噴口から
噴射された燃料噴霧の衝突面の形状を衝突位置ご
とに異ならせている。 Further, concave portions 5 continuous to the side surface are provided at a plurality of locations on the side surface of the combustion chamber 3, and at least the side surface is left as a surface (side surface) 6 between adjacent concave portions 5. The recess 5 is composed of a curved surface having a smaller radius than the curved surface forming the side surface 6 of the combustion chamber 3, and the connecting portion between the recess 5 and the side surface 6 is cut into, for example, an arc shape to connect the recess 5 and the side surface 6. To ensure smooth continuity, it is necessary to leave side surfaces 6 between adjacent recesses 5, and by forming these recesses 5, the width of the narrowed portion 2 is partially increased.
Although the number of recesses 5 varies depending on the size of the combustion chamber 3, by making the number of recesses 5 larger or smaller than the number of nozzles provided in the nozzle 4, collision of fuel sprays injected from each nozzle can be prevented. The shape of the surface differs depending on the collision location.
上記の構成において、ノズル4から噴射された
燃料噴霧7は、スワールによつて押し流されつつ
空気と混合してその一部が燃焼室3の側面6に衝
突し、中心部に向つて反射する。このとき、ノズ
ル4の噴口の数と凹部5の数とを1つだけ異なら
せて両者を等配形成する等の方法により、各噴口
からの燃料噴霧の衝突条件(衝突面の形状)を異
ならせているために、衝突位置ごとに性状の異な
る混合気が生成される。従つて、機関の運転状態
の変化に対しても少なくともいずれか1箇所では
混合気の性状が理想的な状態になつて着実に着火
して燃焼を開始する。このために、いかなる運転
状況にあろうとも、着火遅れ期間が短かくなつて
燃焼が円滑化される。 In the above configuration, the fuel spray 7 injected from the nozzle 4 is mixed with air while being swept away by the swirl, and a part of it collides with the side surface 6 of the combustion chamber 3 and is reflected toward the center. At this time, the collision conditions (the shape of the collision surface) of the fuel spray from each nozzle can be varied by, for example, making the number of nozzles 4 and the number of recesses 5 different by one and forming them equally spaced. Because of this, a mixture with different properties is generated depending on the collision location. Therefore, even when the operating conditions of the engine change, the properties of the air-fuel mixture become ideal in at least one location, and the mixture steadily ignites and starts combustion. For this reason, the ignition delay period is shortened and combustion becomes smoother under any operating conditions.
又、凹部5を設けたことによつて絞り部2の長
さが部分的に大きくなつているために、充分なス
キツシユが発生して燃焼効率が向上する。そし
て、燃焼室の内面が凹部5を設けたことで滑らか
な凹凸状になつているために、スワールによつて
局部的な渦流(小渦流)がひき起されて燃焼室側
面に付着している燃料の蒸発が促進され、燃焼期
間が短縮される。更に、全体としての絞り部をさ
ほど大きくすることなく前記のように充分な強さ
のスキツシユを得ることができるために、絞り部
によつて一旦燃焼室に閉じ込められていた火炎が
適当な時期にスキツシユエリアにも噴出する。こ
のために、排ガス成分の生成が抑制されると同時
に空気利用率が高くなつて排煙濃度及び燃料消費
率が改善される。更にまた、燃焼室3の側面6の
一部を凹部5の間に面として残しているため、熱
負荷的にも有利な燃焼室形状となる。 Further, since the length of the throttle part 2 is partially increased by providing the recess 5, sufficient squishing occurs and combustion efficiency is improved. Since the inner surface of the combustion chamber has a smooth uneven shape due to the provision of the recess 5, a local vortex (small vortex) is caused by the swirl and adheres to the side surface of the combustion chamber. Fuel evaporation is promoted and the combustion period is shortened. Furthermore, since it is possible to obtain a sufficiently strong squeeze as described above without increasing the overall size of the constriction, the flame that was once confined in the combustion chamber by the constriction can be released at an appropriate time. It also erupts in the Sukitsuyu area. For this reason, the generation of exhaust gas components is suppressed, and at the same time, the air utilization rate is increased, and the exhaust gas concentration and fuel consumption rate are improved. Furthermore, since a part of the side surface 6 of the combustion chamber 3 is left as a surface between the recesses 5, the combustion chamber has a shape that is advantageous in terms of heat load.
以上説明したように本発明によれば、絞り部を
さほど大きくすることなく強いスキツシユを得る
ことができると共に、燃焼室内に生じる渦流によ
つて局部的な渦流(乱れ)を誘発させて空気と燃
料との混合を良くでき、しかも、火炎の閉じ込め
期間が過度に長くなれない。このために、燃料の
噴射時期を遅らせることなく排ガス成分の生成を
抑制できると共に、燃焼効率が高くなつて燃料消
費率及び排煙濃度が改善される。又、燃焼室の内
面にエツジ及びコーナーがないので、ヒートスポ
ツトがなくなると同時に、不完全燃焼にともなう
未燃成分の排出量をも低減できる。さらに、ノズ
ルに設けられた噴口の数と燃焼室の側面に設けら
れた凹部の数とを異ならせることにより、噴口か
ら噴射された燃料噴霧の衝突面の形状を衝突位置
ごとに異ならせるようにしているために、機関の
運転条件の変化に伴なつて燃料噴霧の拡散状態が
変化したとしても、燃焼室内には依然として種々
の性状の混合気が生成される。従つて、いかなる
運転条件のもとにおいても少なくとも一箇所には
着火に適した性状の混合気が存在して着火遅れを
短縮することができ、機関の出力特性、排気特性
及び燃料消費率等を悉く改善できる。さらに又、
噴口の数と凹部の数とを異ならせることによつて
各噴口からの燃料噴霧の衝突面の形状を異ならせ
るようにしているために、ノズルの組付誤差が大
きくなつたとしても全体としての燃料噴霧の拡散
状態(反射状態)が大きく変化することはない。
このために、ノズルの組付許容誤差を大きくする
ことができ、ノズルの組付作業性を高くしてデイ
ーゼル機関の製造コストを低減することもでき
る。 As explained above, according to the present invention, it is possible to obtain strong squishing without making the throttle part very large, and also to induce local vortices (turbulence) by the vortices generated in the combustion chamber, so that air and fuel This allows for good mixing with the flame, and also prevents the flame confinement period from becoming excessively long. For this reason, the generation of exhaust gas components can be suppressed without delaying the fuel injection timing, and combustion efficiency is increased to improve fuel consumption rate and exhaust gas concentration. Furthermore, since there are no edges or corners on the inner surface of the combustion chamber, there are no heat spots, and at the same time, the amount of unburned components emitted due to incomplete combustion can be reduced. Furthermore, by varying the number of nozzles provided in the nozzle and the number of recesses provided on the side surface of the combustion chamber, the shape of the collision surface of the fuel spray injected from the nozzle can be varied depending on the collision position. Therefore, even if the diffusion state of the fuel spray changes as the engine operating conditions change, air-fuel mixtures with various properties are still generated within the combustion chamber. Therefore, under any operating conditions, an air-fuel mixture with properties suitable for ignition exists in at least one location, reducing ignition delay and improving engine output characteristics, exhaust characteristics, fuel consumption rate, etc. Everything can be improved. Furthermore,
By varying the number of nozzles and the number of recesses, the shape of the collision surface of the fuel spray from each nozzle is made to differ, so even if the nozzle assembly error becomes large, the overall The diffusion state (reflection state) of the fuel spray does not change significantly.
Therefore, the nozzle assembly tolerance can be increased, the nozzle assembly work efficiency can be increased, and the manufacturing cost of the diesel engine can be reduced.
第1図は本発明の一実施例を備えたピストンの
斜視図、第2図は第1図の断面図、第3図は第2
図の―断面図である。
1…ピストン、2…絞り部、3…燃焼室、4…
ノズル、5…凹部、6…側面。
FIG. 1 is a perspective view of a piston equipped with an embodiment of the present invention, FIG. 2 is a sectional view of FIG. 1, and FIG.
This is a sectional view of the figure. 1... Piston, 2... Throttle part, 3... Combustion chamber, 4...
Nozzle, 5... recess, 6... side surface.
Claims (1)
記燃焼室の側面に向つて燃料を噴射するノズルを
設けたデイーゼル機関において、燃焼室の入口部
全周縁に中心に向つて延びる絞り部を形成し、該
燃焼室の側面の複数位置に該側面と連続する凹部
を設け、前記ノズルに設けた噴口の数と前記凹部
の数とを異ならせて各噴口から噴射された燃料噴
霧の衝突面の形状を衝突位置ごとに異ならせると
共に、隣接する凹部間に燃焼室の側面を少なくと
も面として残したことを特徴とするデイーゼル機
関の燃焼室。1. In a diesel engine in which a combustion chamber is recessed in the top surface of the piston and a nozzle is provided for injecting fuel toward the side surface of the combustion chamber, a throttle portion extending toward the center is provided on the entire periphery of the inlet portion of the combustion chamber. a collision surface of fuel spray injected from each nozzle by forming recesses continuous with the side surface at a plurality of positions on the side surface of the combustion chamber, and making the number of nozzles provided in the nozzle different from the number of the recesses; A combustion chamber for a diesel engine, characterized in that the shape of the combustion chamber differs depending on the collision position, and at least a side surface of the combustion chamber is left between adjacent recesses as a surface.
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57068435A JPS58185925A (en) | 1982-04-23 | 1982-04-23 | Combustion chamber for diesel engine |
| DE8383901232T DE3373694D1 (en) | 1982-04-23 | 1983-04-23 | Combustion chamber of diesel engine |
| AT83901232T ATE29764T1 (en) | 1982-04-23 | 1983-04-23 | COMBUSTION CHAMBER OF A DIESEL ENGINE. |
| PCT/JP1983/000128 WO1983003875A1 (en) | 1982-04-23 | 1983-04-23 | Combustion chamber of diesel engine |
| EP83901232A EP0105933B2 (en) | 1982-04-23 | 1983-04-23 | Combustion chamber of diesel engine |
| US06/545,039 US4538566A (en) | 1982-04-23 | 1983-04-23 | Combustion chamber in a diesel engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57068435A JPS58185925A (en) | 1982-04-23 | 1982-04-23 | Combustion chamber for diesel engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS58185925A JPS58185925A (en) | 1983-10-29 |
| JPS632008B2 true JPS632008B2 (en) | 1988-01-16 |
Family
ID=13373619
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP57068435A Granted JPS58185925A (en) | 1982-04-23 | 1982-04-23 | Combustion chamber for diesel engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58185925A (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS62148731U (en) * | 1986-03-13 | 1987-09-19 | ||
| JPS62255521A (en) * | 1986-04-30 | 1987-11-07 | Isuzu Motors Ltd | Pent roof type piston |
| JPS6387227U (en) * | 1986-11-28 | 1988-06-07 | ||
| JPH0218619U (en) * | 1988-07-18 | 1990-02-07 |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS562020U (en) * | 1979-06-20 | 1981-01-09 |
-
1982
- 1982-04-23 JP JP57068435A patent/JPS58185925A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS58185925A (en) | 1983-10-29 |
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