JPH0196421A - Combustion chamber of diesel engine - Google Patents

Combustion chamber of diesel engine

Info

Publication number
JPH0196421A
JPH0196421A JP62253027A JP25302787A JPH0196421A JP H0196421 A JPH0196421 A JP H0196421A JP 62253027 A JP62253027 A JP 62253027A JP 25302787 A JP25302787 A JP 25302787A JP H0196421 A JPH0196421 A JP H0196421A
Authority
JP
Japan
Prior art keywords
combustion chamber
opening
engine
combustion
air
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
JP62253027A
Other languages
Japanese (ja)
Inventor
Yuzo Aoyanagi
青柳 友三
Yukihiro Tsuji
幸浩 辻
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.)
Hino Motors Ltd
Original Assignee
Hino 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 Hino Motors Ltd filed Critical Hino Motors Ltd
Priority to JP62253027A priority Critical patent/JPH0196421A/en
Publication of JPH0196421A publication Critical patent/JPH0196421A/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
    • F02B23/0645Details 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
    • 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
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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

PURPOSE:To utilize air in respective sections in combustion chamber sufficiently over the entire operating zone of an engine by providing a plurality of recesses opening in oval onto the inner circumferential face of the combustion chamber. CONSTITUTION:Shapes of reflection faces of fuel spray ejected through respective ejection ports are differentiated by forming four recesses 6 opening in oval shape formed with curved faces or approximately curved faces onto the inner circumferential face of a combustion chamber 2 arranged on the top face of a piston 1. Consequently, air flow entered into the recess 6 flows out in all directions along the profile of the opening. As a result, a three-dimensional complex air flow is produced in the combustion chamber 2 to double swirl suppression effect under high rotary speed region of engine, while air even in the bottom and the central section can be utilized sufficiently, resulting in a good combustion over the entire operating zone.

Description

【発明の詳細な説明】 〈産業上の利用分野〉 本発明は、ピストンの頂面に凹設した燃焼室の内周面に
向って燃料を噴射供給するようにしたディーゼル機関の
燃焼室に関するものである。
[Detailed Description of the Invention] <Industrial Application Field> The present invention relates to a combustion chamber of a diesel engine in which fuel is injected and supplied toward the inner peripheral surface of the combustion chamber recessed in the top surface of a piston. It is.

〈従来の技術〉 従来のこの種ディーゼル機関の燃焼室としては、特公昭
4q−1aain号公報、特公昭51−42249号公
報あるいは米国特許第3,302,627号明細書等に
見られるように、燃焼室の内周面に複数個の凹部又は突
部を設けて燃焼効率を改善するようにしたものがある。
<Prior Art> Conventional combustion chambers of this type of diesel engine are as described in Japanese Patent Publication No. 4Q-1AAIN, Japanese Patent Publication No. 51-42249, or U.S. Patent No. 3,302,627. Some combustion chambers have a plurality of recesses or protrusions on the inner circumferential surface of the combustion chamber to improve combustion efficiency.

これら燃焼室は、特に機関の高速回転域における燃焼室
内の吸入空気の旋回流(以下、スワールと云う)の速度
を燃焼室内周面に設けた凹部又は突部によって抑制する
と共に、突部又は凹部を設けることで銹起される小渦流
を積極的に利用して空気と燃料の混合を促進させること
により、燃焼効率を広範囲な運転域において改善しよう
とするものである。
These combustion chambers suppress the velocity of the swirling flow (hereinafter referred to as swirl) of the intake air within the combustion chamber, especially in the high-speed rotation range of the engine, by using recesses or protrusions provided on the peripheral surface of the combustion chamber. The aim is to improve combustion efficiency over a wide range of operating ranges by actively utilizing the small vortices created by the provision of a combustion engine to promote mixing of air and fuel.

〈発明か解決しようとする問題点〉 ところが、従来では矩形状に開口する凹部を設け、又は
柱状の突部を設けたに過ぎないためにスワール速度の抑
制効果及び凹部又は突部による小渦流の生成領域がピス
トン頂面に平行な平面内における二次元的な範囲に限定
されてしまう。従って、これらの影響が及び難い燃焼室
底部及び中心部の空気を十分に活用できず、燃焼効率を
向上させるにも限界があるという問題点があった。
<Problems to be Solved by the Invention> However, in the past, only a rectangular opening recess or a columnar protrusion was provided, so the effect of suppressing the swirl speed and the small vortex flow caused by the recess or protrusion were poor. The generation area is limited to a two-dimensional range within a plane parallel to the top surface of the piston. Therefore, there is a problem in that the air at the bottom and center of the combustion chamber, where these influences are difficult to reach, cannot be fully utilized, and there is a limit to how much combustion efficiency can be improved.

本発明は斯る従来の問題点を解消するためになされたも
のであり、燃焼室内各部の空気を機関のあらゆる運転域
において十分に活用して燃焼効率をより向上させること
を目的としている。
The present invention has been made to solve these conventional problems, and aims to further improve combustion efficiency by fully utilizing the air in each part of the combustion chamber in all operating ranges of the engine.

く問題点を解決するための手段〉 上記目的を達成するために本発明では、ピストンの頂面
に燃焼室を凹設し、シリンダヘッドに装着した燃料噴射
ノズルの先端に設けた噴口から前記燃焼室の内周面に向
って燃料を噴射供給するようにしたディーゼル機関にお
いて、長円又は楕円状に開口する複数個の凹部を前記燃
焼室の内周面に設けた構成としている。
Means for Solving the Problems> In order to achieve the above object, the present invention has a combustion chamber recessed in the top surface of the piston, and the combustion chamber is provided at the tip of the fuel injection nozzle attached to the cylinder head. In a diesel engine that injects fuel toward the inner peripheral surface of the combustion chamber, a plurality of recesses opening in an oval or elliptical shape are provided in the inner peripheral surface of the combustion chamber.

く作用〉 このように燃焼室の内周面に長円又は楕円状に開口する
凹部を設けているために、凹部に入った空気流は開口部
形状に沿ってあらゆる方向に流出する。従って、燃焼室
内には三次元的な複雑な空気流動が生成され、これによ
り、機関の高速回転域におけるスワール抑制効果を倍加
できると共に、燃焼室底部及び中心部の空気をも十分に
利用することができ、機関のあらゆる運転域において良
好な燃焼を行なわせることができる。
Effect> Since the recess opening in an oval or elliptical shape is thus provided on the inner peripheral surface of the combustion chamber, the airflow that enters the recess flows out in all directions along the shape of the opening. Therefore, a three-dimensional complex air flow is generated within the combustion chamber, which doubles the swirl suppression effect in the high-speed rotation range of the engine, and also makes full use of the air at the bottom and center of the combustion chamber. This allows for good combustion in all operating ranges of the engine.

〈実施例〉 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
<Example> Examples of the present invention will be described in detail below based on the drawings.

図示しないシリンダ内を往復運動するピストンlの頂面
に設けた燃焼室2の開口部全周に絞り4を設けている。
A throttle 4 is provided around the entire opening of a combustion chamber 2 provided on the top surface of a piston l that reciprocates within a cylinder (not shown).

又、燃焼室2の底面に円錐状の突起5を設ける一方、先
端に5個の噴口を等配形成したホール型の燃料噴射ノズ
ル3を図示しないシリンダヘッドに装着してディーゼル
機関を構成している。
Further, a diesel engine is constructed by providing a conical projection 5 on the bottom surface of the combustion chamber 2, and attaching a hole-type fuel injection nozzle 3, which has five nozzles equally spaced at the tip, to a cylinder head (not shown). There is.

又、前記燃焼室2の内周面には曲面若しくは曲面に近似
する面で形成された楕円状に開口する4個の凹部6を等
配形成することにより、各噴口から噴射された燃料噴霧
7の反射面(衝突面)の形状をそれぞれ異らせている。
Furthermore, by forming four concave portions 6 having an elliptical opening formed by a curved surface or a surface approximating a curved surface at equal intervals on the inner circumferential surface of the combustion chamber 2, the fuel spray 7 injected from each nozzle is prevented. The shape of the reflecting surface (collision surface) is different for each.

尚、本実施例では燃料噴射ノズル3の噴口数より1個多
ない数の凹部6を設けているが、逆に噴口数より1個多
い数の凹部6を設けてもよく、要するに噴口の数と凹部
6の数を異らせることにより各噴口からの燃料噴n7の
反射面の形状(反射条件)をそれぞれ異らせることが望
まれるが、噴口と凹部6を同数としてもよい。
In this embodiment, the number of recesses 6 is one less than the number of nozzles in the fuel injection nozzle 3, but conversely, the number of recesses 6 may be one more than the number of nozzles. Although it is desirable to vary the shape (reflection condition) of the reflecting surface of the fuel injection n7 from each nozzle by varying the number of concave portions 6, the number of nozzles and concave portions 6 may be the same.

このように構成されたディーゼル機関において、機関の
運転にともなって燃焼室2内には機関回転速度に比例し
たスワール速度を有する空気が満たされ、燃料噴射ノズ
ル3の噴口から燃焼室2の内周面に向って燃料が噴射供
給される。この時、燃焼室2の内周面に凹部6を設けて
いるために、この凹部6との接触によってスワール速度
が適度に抑制される。又、凹部6に流入した空気がその
開口形状(楕円形状)に沿って流出する結果、燃焼室2
内にはあらゆる方向への空気流が生成される。
In the diesel engine configured in this manner, as the engine operates, the combustion chamber 2 is filled with air having a swirl speed proportional to the engine rotational speed, and the air flows from the nozzle of the fuel injection nozzle 3 to the inner periphery of the combustion chamber 2. Fuel is injected towards the surface. At this time, since the recess 6 is provided on the inner peripheral surface of the combustion chamber 2, the swirl speed is appropriately suppressed by contact with the recess 6. In addition, as a result of the air flowing into the recess 6 flowing out along the opening shape (elliptical shape), the combustion chamber 2
Inside, airflow is generated in all directions.

一方、燃料噴霧7が衝突する内周面の形状がそれぞれ異
っているため種々の異る反射状態(衝突状態)となる。
On the other hand, since the shape of the inner peripheral surface with which the fuel spray 7 collides is different, various different reflection states (collision states) occur.

従って、機関の運転条件に応じて燃料噴霧7の拡散状態
が変化したとしても、燃焼室2内に多様な性状の混合気
が生成される。
Therefore, even if the diffusion state of the fuel spray 7 changes depending on the operating conditions of the engine, air-fuel mixtures with various properties are generated within the combustion chamber 2.

よって、燃焼室2内のいずれかには着火に適した性状の
混合気が存在することになり、着火遅れが短縮される。
Therefore, an air-fuel mixture with properties suitable for ignition exists somewhere in the combustion chamber 2, and the ignition delay is shortened.

さらに、着火後においても燃焼室2内の混合状態が良好
なため燃焼機関が比較的短くてすみ、これらにより、N
Ox等の排ガス成分の生成が少なくかつ燃料消費率に優
れた理想的な燃焼状態を得ることができる。
Furthermore, even after ignition, the mixing condition in the combustion chamber 2 is good, so the combustion engine can be relatively short, and as a result, the N
It is possible to obtain an ideal combustion state with less generation of exhaust gas components such as Ox and excellent fuel consumption.

尚、実施例では燃焼室2の開口部の全周に絞り4を設け
ているが、この絞り4を設けないオーブンチャンバ型の
燃焼室に本発明を適用しても所期の目的を達成できる。
In the embodiment, the throttle 4 is provided around the entire circumference of the opening of the combustion chamber 2, but the intended purpose can also be achieved even if the present invention is applied to an oven chamber type combustion chamber that does not have the throttle 4. .

さらに、底部に円錐状突起5を設けない平皿型の燃焼室
についても同様であり、凹部6の開口形状を長円あるい
は長円に類似した形状にしても同様のことがいえる。
Furthermore, the same holds true for a flat dish type combustion chamber in which the conical protrusion 5 is not provided at the bottom, and the same holds true even if the opening shape of the recess 6 is made into an ellipse or a shape similar to an ellipse.

(発明の効果〉 以上説明したように本発明によれば、燃焼室の内周面に
長円又は楕円状に開口する凹部を設けて燃焼室内に多方
向に向う空気流を誘起しつつ、スワール速度を適度に抑
制するように構成しているために、燃料と空気の混合状
態を改善することができる。従って、機関のいかなる運
転領域においてもNし等の排ガス成分の生成が少なく、
燃料消費率に優れた理想的な燃焼を行なわせることがで
きる。
(Effects of the Invention) As explained above, according to the present invention, a concave portion opening in an oval or elliptical shape is provided on the inner circumferential surface of the combustion chamber to induce airflow in multiple directions within the combustion chamber, while creating a swirl. Since the engine is configured to moderate the speed, it is possible to improve the mixing state of fuel and air.Therefore, the generation of exhaust gas components such as nitrogen is small in any operating range of the engine.
Ideal combustion with excellent fuel consumption can be performed.

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

第1図は本発明に係る燃焼室の一実施例を備えたピスト
ンの縦断面図、第2図は第1図のA−A断面図である。 1・・・ピストン     2・・・燃焼室3・・・燃
料噴射ノズル  4・・・開口部絞り5・・・底面突起
     6・・・凹部7・・・燃料噴露
FIG. 1 is a longitudinal sectional view of a piston equipped with an embodiment of a combustion chamber according to the present invention, and FIG. 2 is a sectional view taken along line AA in FIG. 1... Piston 2... Combustion chamber 3... Fuel injection nozzle 4... Opening throttle 5... Bottom protrusion 6... Recess 7... Fuel injection

Claims (1)

【特許請求の範囲】[Claims] ピストンの頂面に燃焼室を凹設する一方、燃料噴射ノズ
ルの先端に設けた噴口から前記燃焼室の内周面に向って
燃料を噴射供給するようにしたディーゼル機関において
、長円又は楕円状に開口する複数個の凹部を前記燃焼室
の内周面に設けたことを特徴とするディーゼル機関の燃
焼室。
In a diesel engine in which a combustion chamber is recessed in the top surface of the piston, and fuel is injected and supplied from a nozzle provided at the tip of a fuel injection nozzle toward the inner circumferential surface of the combustion chamber, an oval or elliptical shape is used. A combustion chamber for a diesel engine, characterized in that a plurality of recesses opening into the combustion chamber are provided on an inner circumferential surface of the combustion chamber.
JP62253027A 1987-10-07 1987-10-07 Combustion chamber of diesel engine Pending JPH0196421A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62253027A JPH0196421A (en) 1987-10-07 1987-10-07 Combustion chamber of diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62253027A JPH0196421A (en) 1987-10-07 1987-10-07 Combustion chamber of diesel engine

Publications (1)

Publication Number Publication Date
JPH0196421A true JPH0196421A (en) 1989-04-14

Family

ID=17245462

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62253027A Pending JPH0196421A (en) 1987-10-07 1987-10-07 Combustion chamber of diesel engine

Country Status (1)

Country Link
JP (1) JPH0196421A (en)

Similar Documents

Publication Publication Date Title
JPS6037289B2 (en) spark ignition internal combustion engine
US4538566A (en) Combustion chamber in a diesel engine
US3872841A (en) Construction arrangement of combustion chamber for use in direct fuel injection type diesel engines
EP0148888A1 (en) Internal combustion engine piston.
JPH06185366A (en) Combustion chamber for air compression type and self-ignition type internal combustion engine
US4108116A (en) Combustion chamber and nozzle arrangement for direct fuel injection type diesel engine
JPH0196421A (en) Combustion chamber of diesel engine
JPS62255524A (en) Pent roof type direct injection internal combustion engine
JPS60224920A (en) Combustion chamber structure in piston-top surface
JPH06221163A (en) Combustion chamber structure of direct injection type diesel engine
JPH0147606B2 (en)
JPH11117748A (en) Combustion chamber for direct injection type diesel engine
JPH05272432A (en) Fuel injecting valve
JPH08121171A (en) Combustion chamber for direct injection type diesel engine
JPH108965A (en) Combustion chamber for diesel engine
KR920007246B1 (en) Combustion chamber in piesel engine
JPS6329016A (en) Subchamber type diesel combustion chamber
JPS603312Y2 (en) Combustion chamber of direct injection diesel engine
JPH05240052A (en) Cylinder injection type internal combustion engine
JPS58185925A (en) Combustion chamber for diesel engine
JPH0540270Y2 (en)
JPH0736089Y2 (en) Direct injection diesel engine
JPS5849689B2 (en) direct injection diesel engine
JPH04116632U (en) Combustion chamber structure of direct injection diesel engine
JPH0196422A (en) Combustion chamber for diesel engine