JP2501299Y2 - Combustion chamber of diesel engine - Google Patents

Combustion chamber of diesel engine

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Publication number
JP2501299Y2
JP2501299Y2 JP1989143077U JP14307789U JP2501299Y2 JP 2501299 Y2 JP2501299 Y2 JP 2501299Y2 JP 1989143077 U JP1989143077 U JP 1989143077U JP 14307789 U JP14307789 U JP 14307789U JP 2501299 Y2 JP2501299 Y2 JP 2501299Y2
Authority
JP
Japan
Prior art keywords
combustion chamber
small
combustion
fuel
diesel engine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP1989143077U
Other languages
Japanese (ja)
Other versions
JPH0382830U (en
Inventor
俊一 森
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP1989143077U priority Critical patent/JP2501299Y2/en
Publication of JPH0382830U publication Critical patent/JPH0382830U/ja
Application granted granted Critical
Publication of JP2501299Y2 publication Critical patent/JP2501299Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【考案の詳細な説明】 〔産業上の利用分野〕 本考案は、デイーゼル機関の燃焼室及び燃料噴射弁に
関する。
DETAILED DESCRIPTION OF THE INVENTION [Industrial application] The present invention relates to a combustion chamber and a fuel injection valve of a diesel engine.

〔従来の技術〕 第3図、第4図に従来の直接噴射式デイーゼル機関の
燃焼室及び燃料噴射弁の配置の代表例を示す。図により
説明する。
[Prior Art] FIGS. 3 and 4 show typical examples of the arrangement of a combustion chamber and a fuel injection valve of a conventional direct injection type diesel engine. It will be described with reference to the drawings.

第3図のように従来の燃焼装置は、ピストン101のほ
ぼ中央に円筒形の燃焼室101aが1ケ配設され、シリンダ
ヘツド102に設けた燃料噴射弁103は数ケの噴孔を有し、
その円筒形燃焼室101aの中央上部より放射状に燃料噴霧
104を噴射し着火燃焼させている。
As shown in FIG. 3, in the conventional combustion apparatus, one cylinder-shaped combustion chamber 101a is arranged substantially in the center of the piston 101, and the fuel injection valve 103 provided in the cylinder head 102 has several injection holes. ,
Radial fuel spray from the upper center of the cylindrical combustion chamber 101a
104 is injected and ignited and burned.

従来形の燃焼装置では、燃焼室径が比較的大きいた
め、燃料噴霧104が燃焼室壁面101bに衝突する手前で着
火する。この時周辺に充分空気が存在するため火炎は急
激に拡散する。
In the conventional combustion apparatus, since the diameter of the combustion chamber is relatively large, the fuel spray 104 ignites before it collides with the wall surface 101b of the combustion chamber. At this time, since there is sufficient air around the flame, the flame spreads rapidly.

次に噴霧火炎は、燃焼室壁101bに沿つて左右に拡散
し、相隣る噴霧火炎と衝突、燃焼室中央方向へ折返し全
体に拡散する。
Next, the spray flame diffuses left and right along the combustion chamber wall 101b, collides with the adjacent spray flame, and returns toward the center of the combustion chamber and diffuses throughout.

又従来、燃焼室内に円周方向の渦流(スワール)SWを
発生させ燃焼の促進を計っているが、この場合、燃料噴
霧はスワールSW下流方向へ大部分が流され、噴霧火炎も
下流に向って拡散し燃焼室内を一方向へぐるぐる回転す
る。この時相隣る噴霧火炎どうしの干渉は比較的少く、
互のミクロ的拡散もほとんどないまゝ燃焼は進行し終了
する。
Conventionally, a swirl SW (circle) in the circumferential direction is generated in the combustion chamber to promote combustion, but in this case, most of the fuel spray is made to flow downstream of the swirl SW, and the spray flame also goes downstream. Diffuse and rotate in one direction in the combustion chamber. At this time, the interference between adjacent spray flames is relatively small,
Combustion proceeds and ends until there is almost no micro diffusion between them.

〔考案が解決しようとする課題〕[Problems to be solved by the device]

従来の直接噴射式デイーゼル機関の燃焼室直径は、ピ
ストン径に対し、0.5〜0.6以上を有し比較的大きい。こ
のため燃焼室中央に配設した燃料弁から噴射された燃料
噴霧が、燃焼室壁に衝突するまで、充分な空間が有り、
空気が存在するため、着火後、急激な火炎伝播が起り、
高温度の燃焼となることから、燃焼の初期に多量の窒素
酸化物質発生の原因となっている。
The diameter of the combustion chamber of the conventional direct injection diesel engine is 0.5 to 0.6 or more relative to the piston diameter, which is relatively large. Therefore, there is sufficient space until the fuel spray injected from the fuel valve arranged in the center of the combustion chamber collides with the wall of the combustion chamber,
Due to the presence of air, a rapid flame spread occurs after ignition,
The high temperature combustion causes generation of a large amount of nitrogen oxides in the early stage of combustion.

又燃焼の中、後期では、燃焼室内での燃料と空気の混
合が均一にならないため、極部的な空気不足による黒煙
の発生や、燃費の悪化等が問題である。これは従来のよ
うな単純な円筒形では、燃焼室中央から単純に燃料を噴
射しても、燃料と空気とのミクロ的混合を時間的かつ空
間的に完全に均一化できないことが原因である。
Further, in the latter half of the combustion, the fuel and the air are not uniformly mixed in the combustion chamber, so that there is a problem that black smoke is generated due to the air shortage in the extreme part and the fuel consumption is deteriorated. This is because in the conventional simple cylindrical shape, even if the fuel is simply injected from the center of the combustion chamber, the microscopic mixing of the fuel and air cannot be completely made uniform both temporally and spatially. .

本考案は、噴射燃料の燃焼初期から後期に亘って比較
的均一な燃焼を行うことのできるデイーゼル機関の燃焼
室を提供することを目的とするものである。
An object of the present invention is to provide a combustion chamber of a diesel engine capable of performing relatively uniform combustion from the early stage to the late stage of combustion of the injected fuel.

〔課題を解決するための手段〕[Means for solving the problem]

ピストン頂部に形成する燃焼室として、中央に大燃焼
室1個、その左右に小燃焼室を各1個対称的に配置す
る。夫々の燃焼室は平面形状を円形とし、大燃焼室と左
右の小燃焼室は切欠き状の案内通路により連絡する。大
小燃焼空間の案内通路は、大燃焼室の外周方向にスワー
ルに合せて向けると共に、平面断面が大燃焼室側に拡大
する形状とする。
As a combustion chamber formed on the top of the piston, one large combustion chamber is arranged in the center and one small combustion chamber is arranged on the left and right of the large combustion chamber. Each combustion chamber has a circular planar shape, and the large combustion chamber and the left and right small combustion chambers are connected by a notched guide passage. The guide passages of the large and small combustion spaces are oriented so as to swirl in the outer peripheral direction of the large combustion chamber and have a planar cross-section that expands toward the large combustion chamber side.

縦断面形状は大燃焼室はくさび型形状とし、小燃焼室
は球形形状で上部を切り取った形状とする。大、小燃焼
室間の案内通路は、燃焼室夫々の上部で接合する。
As for the vertical cross section, the large combustion chamber has a wedge shape, and the small combustion chamber has a spherical shape with the upper part cut off. The guide passage between the large and small combustion chambers is joined at the upper part of each combustion chamber.

燃料噴射弁は、各小燃焼室の中央上部でシリンダヘツ
ドに、小燃焼室に向けて噴射するように各1個配設す
る。
One fuel injection valve is provided in the cylinder head above the center of each small combustion chamber so as to inject fuel toward the small combustion chamber.

〔作用〕[Action]

2個の小燃焼室中央上方に配設した燃料噴射弁の数個
又は1個の噴孔より、小燃焼室に向け噴射すると、燃料
噴霧は球形の壁面に沿って分散し、小さい燃焼室内はす
ぐに燃料噴霧で満される。この濃混合状態で着火される
が空気不足のため初期の急激な燃焼は抑制される。
When injected toward the small combustion chamber from several or one injection holes of the fuel injection valves arranged above the center of the two small combustion chambers, the fuel spray is dispersed along the spherical wall surface, and inside the small combustion chamber Immediately filled with fuel spray. Ignition is performed in this rich mixture state, but the rapid combustion in the initial stage is suppressed due to lack of air.

次に噴霧火炎に満された小燃焼室から、案内通路を通
つて、完全に燃焼していない噴霧火炎が大燃焼室に噴出
する。この時左右の小燃焼室からの噴霧火炎は、同時に
中央の大燃焼室の外周方向に互にぶつかり合わないよう
に、且つ大燃焼室に与えた渦流(スワール)の方向と同
一方向に噴出する。
Next, from the small combustion chamber filled with the spray flame, the spray flame which is not completely burned is ejected into the large combustion chamber through the guide passage. At this time, the spray flames from the left and right small combustion chambers are ejected in the same direction as the direction of the swirl (swirl) given to the large combustion chamber so that they do not collide with each other in the outer peripheral direction of the central large combustion chamber at the same time. .

こうすることによって、大燃焼室へ噴出した半燃焼状
態の噴霧火炎は、充分な空気が存在するため燃焼が促進
される。更に大燃焼室に与えたスワールを利用するよう
噴出させることにより、空気との混合を燃焼の後期まで
持続し改善することが可能となり、完全燃焼が計れる。
By doing so, the spray flame in the semi-combustion state ejected to the large combustion chamber is promoted to burn because there is sufficient air. Furthermore, by ejecting the swirl given to the large combustion chamber so as to utilize it, it becomes possible to continue and improve the mixing with air until the latter stage of combustion, and complete combustion can be measured.

〔実施例〕〔Example〕

第1,2図により本考案の実施例について説明する。第
1図は実施例の燃焼室の平面図、第2図は第1図のII-I
I断面図である。図においてピストン1の頂部に設けら
れた燃焼室は、中央に大燃焼室1a、その左右に頭部を切
った様な球形の小燃焼室1b及び1cを有し、共に水平断面
は円形で、大燃焼室1aと小燃焼室1b,1cは案内通路1d,1e
により接合されている。この案内通路1d,1eは大燃焼室
の外周部に接合し、かつ案内通路1d,1eは互いに干渉し
ないよう逆方向に接合している。
An embodiment of the present invention will be described with reference to FIGS. FIG. 1 is a plan view of the combustion chamber of the embodiment, and FIG. 2 is II-I of FIG.
It is I sectional drawing. In the figure, the combustion chamber provided at the top of the piston 1 has a large combustion chamber 1a at the center and spherical small combustion chambers 1b and 1c at the left and right sides thereof with the heads cut off. The large combustion chamber 1a and the small combustion chambers 1b, 1c have guide passages 1d, 1e
Are joined by. The guide passages 1d and 1e are joined to the outer peripheral portion of the large combustion chamber, and the guide passages 1d and 1e are joined in opposite directions so as not to interfere with each other.

また縦断面は、大燃焼室1aは底面がフラツトで、側面
は上面が内側に傾斜したクサビ形々状としている。小燃
焼室1b,1cは球形燃焼室とし火炎の流出をし易くしてい
る。
Further, the vertical cross section has a wedge-shaped shape in which the bottom surface of the large combustion chamber 1a is flat and the side surfaces are inclined inward. The small combustion chambers 1b and 1c are spherical combustion chambers to facilitate the outflow of flame.

一方シリンダヘツド2に取付けられた燃料噴射弁3a,3
bは、小燃焼室1b,1cの上方に配設されている。
On the other hand, the fuel injection valves 3a, 3 mounted on the cylinder head 2
The b is arranged above the small combustion chambers 1b and 1c.

今、燃料噴射弁3a,3bから噴射された燃料は、小燃焼
室1b,1c内の壁面に衝突し着火、壁面に沿つて火炎は拡
散する。小燃焼室1b,1cは壁面までの距離が短く、容積
も小さく、濃混合気状態になっているため、急激な燃焼
には至らず比較的緩やかなものとなる。
Now, the fuel injected from the fuel injection valves 3a and 3b collides with the wall surface in the small combustion chambers 1b and 1c, ignites, and the flame spreads along the wall surface. The small combustion chambers 1b and 1c have a short distance to the wall surface, a small volume, and are in a rich air-fuel mixture state, so that rapid combustion does not occur and the combustion is relatively gentle.

次に着火した噴霧火炎は、この時期ピストントツプク
リアランスlcが極く小さいため、ピストン上部方向への
火炎流出は少く、大部分は小燃焼室1b,1cの側壁に接合
した案内通路1d,1eを通り、大燃焼室1a内に流入する。
この流入方向は案内通路1d,1eが大燃焼室1aの外周方向
に接続されているため、外周に向かって流入し大燃焼室
1a内で旋回運動をする。また大燃焼室1a内に与えた空気
渦流SWを、上記旋回運動方向と同一方向になるよう配設
することにより、旋回運動は一層強いものになる。
In the spray flame that ignited next, since the piston top clearance lc was extremely small at this time, the flame outflow toward the upper part of the piston was small, and most of the And flows into the large combustion chamber 1a.
In this inflow direction, since the guide passages 1d and 1e are connected to the outer peripheral direction of the large combustion chamber 1a, the inflow direction flows toward the outer periphery and the large combustion chamber 1a.
It makes a turning motion within 1a. Further, the swirling motion is further strengthened by arranging the air swirl flow SW provided in the large combustion chamber 1a in the same direction as the swirling motion direction.

大燃焼室1aに流入する時の噴霧火炎は、空気不足のた
め、半燃焼状態で流入するが、流入後空気量を充分確保
できるため、燃焼が促進され、更に旋回運動を与える事
により燃焼後期迄充分空気を確得でき燃焼改善を計る事
ができる。
The spray flame when flowing into the large combustion chamber 1a flows in a semi-combustion state due to lack of air, but after the inflow it is possible to secure a sufficient amount of air, so combustion is promoted, and further swirling motion is given Up to this point, air can be obtained sufficiently and combustion can be improved.

以上により初期の燃焼を適度に抑制すると共に、中、
後期燃焼を従来以上に活発にする事が可能となり、窒素
酸化物の生成を抑え、黒煙発生を防止し、燃費改善を計
ることができる。
By the above, while suppressing the initial combustion moderately, medium,
It is possible to activate late combustion more actively than before, suppress the generation of nitrogen oxides, prevent the generation of black smoke, and improve fuel efficiency.

〔考案の効果〕[Effect of device]

本考案は、ピストン頂部に燃焼室を設けたデイーゼル
機関の燃焼室において、ピストン頂部の中央に凹設され
た大燃焼室と、該大燃焼室の周囲に対称的に配置された
複数の小燃焼室と、該大燃焼室と小燃焼室とを連通し且
つ大燃焼室室内のスワール流と一致する方向で大燃焼室
の円周方向に開口する複数の案内通路と、各小燃焼室の
中央部上方のシリンダヘツドに装着され各小燃焼室に向
けて燃料を噴射する燃料噴射弁とを具えたものであるか
ら、シリンダの中央に配設される大燃焼室のスワール
は、その大燃焼室の周囲に対称的に配置された複数の小
燃焼室から噴出する噴霧運動により増強されると共に大
燃焼室内の空気との拡散を促進して燃焼を良好にし、更
に複数の小燃焼室への燃料噴射は、その時期、量等を夫
々自由に変化することができるため大燃焼室への噴出す
る時期、量等がある程度制御されて、大燃焼室での燃焼
を一層良好に制御することが可能となる等の効果を有す
る。
The present invention relates to a combustion chamber of a diesel engine having a combustion chamber at the top of the piston, and a large combustion chamber recessed at the center of the piston top and a plurality of small combustion chambers symmetrically arranged around the large combustion chamber. Chamber, a plurality of guide passages communicating between the large combustion chamber and the small combustion chamber and opening in the circumferential direction of the large combustion chamber in a direction coinciding with the swirl flow in the large combustion chamber, and the center of each small combustion chamber. And a fuel injection valve for injecting fuel toward each small combustion chamber, the swirl of the large combustion chamber arranged in the center of the cylinder is Is enhanced by the spray motion ejected from a plurality of small combustion chambers symmetrically arranged around the fuel cell, promotes diffusion with air in the large combustion chamber to improve combustion, and further fuels to a plurality of small combustion chambers. For injection, change the timing, amount, etc. freely. Timing for jetting to large combustion chamber because it, by an amount or the like is controlled to some extent, an effect such that the combustion in a large combustion chamber it is possible to better control.

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

第1図は本考案の実施例に係る燃焼室の平面図、第2図
は同上のII-II断面図、第3図は従来の燃焼室を示す平
面図、第4図は第3図のIV-IV断面図である。 1……ピストン、1a……大燃焼室 1b,1c……小燃焼室、1d,1e……案内通路 2……シリンダヘツド、3a,3b……燃料噴射弁
FIG. 1 is a plan view of a combustion chamber according to an embodiment of the present invention, FIG. 2 is a sectional view taken along line II-II of the same, FIG. 3 is a plan view showing a conventional combustion chamber, and FIG. It is a IV-IV sectional view. 1 ... Piston, 1a ... Large combustion chamber 1b, 1c ... Small combustion chamber, 1d, 1e ... Guide passage 2 ... Cylinder head, 3a, 3b ... Fuel injection valve

Claims (1)

(57)【実用新案登録請求の範囲】(57) [Scope of utility model registration request] 【請求項1】ピストン頂部に燃焼室を設けたデイーゼル
機関の燃焼室において、ピストン頂部の中央に凹設され
た大燃焼室と、該大燃焼室の周囲に対称的に配置された
複数の小燃焼室と、該大燃焼室と各小燃焼室とを連通し
且つ大燃焼室内のスワール流と一致する方向で大燃焼室
の円周方向に開口する複数の案内通路と、各小燃焼室の
中央部上方のシリンダヘツドに装着され各小燃焼室に向
けて燃料を噴射する燃料噴射弁とを具えたことを特徴と
するデイーゼル機関の燃焼室。
1. A combustion chamber of a diesel engine having a combustion chamber at the top of a piston, wherein a large combustion chamber is provided at the center of the piston top and a plurality of small chambers symmetrically arranged around the large combustion chamber. A combustion chamber, a plurality of guide passages communicating with the small combustion chamber and the large combustion chamber and opening in the circumferential direction of the large combustion chamber in a direction coinciding with the swirl flow in the large combustion chamber, and of the small combustion chambers. A combustion chamber for a diesel engine, comprising: a fuel injection valve that is mounted on a cylinder head above a central portion and injects fuel toward each small combustion chamber.
JP1989143077U 1989-12-13 1989-12-13 Combustion chamber of diesel engine Expired - Lifetime JP2501299Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1989143077U JP2501299Y2 (en) 1989-12-13 1989-12-13 Combustion chamber of diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1989143077U JP2501299Y2 (en) 1989-12-13 1989-12-13 Combustion chamber of diesel engine

Publications (2)

Publication Number Publication Date
JPH0382830U JPH0382830U (en) 1991-08-23
JP2501299Y2 true JP2501299Y2 (en) 1996-06-12

Family

ID=31689877

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1989143077U Expired - Lifetime JP2501299Y2 (en) 1989-12-13 1989-12-13 Combustion chamber of diesel engine

Country Status (1)

Country Link
JP (1) JP2501299Y2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01130026U (en) * 1988-03-01 1989-09-05

Also Published As

Publication number Publication date
JPH0382830U (en) 1991-08-23

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