JPS6319544Y2 - - Google Patents

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Publication number
JPS6319544Y2
JPS6319544Y2 JP15648680U JP15648680U JPS6319544Y2 JP S6319544 Y2 JPS6319544 Y2 JP S6319544Y2 JP 15648680 U JP15648680 U JP 15648680U JP 15648680 U JP15648680 U JP 15648680U JP S6319544 Y2 JPS6319544 Y2 JP S6319544Y2
Authority
JP
Japan
Prior art keywords
chamber
combustion
throat
trench
width
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
Application number
JP15648680U
Other languages
Japanese (ja)
Other versions
JPS5778724U (en
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 filed Critical
Priority to JP15648680U priority Critical patent/JPS6319544Y2/ja
Publication of JPS5778724U publication Critical patent/JPS5778724U/ja
Application granted granted Critical
Publication of JPS6319544Y2 publication Critical patent/JPS6319544Y2/ja
Expired legal-status Critical Current

Links

Description

【考案の詳細な説明】 本案は渦室(渦流式燃焼室)を備えたデイーゼ
ルエンジンの燃焼室の改良に関する。
[Detailed Description of the Invention] The present invention relates to an improvement of the combustion chamber of a diesel engine equipped with a swirl chamber (vortex type combustion chamber).

渦室付デイーゼルエンジンはピストンの頂上部
に形成された主室(主燃焼室)とシリンダヘツド
に配設された渦室とを有していて、その間を渦室
のスロート部にて連絡している。そして吸気行程
でシリンダ内に吸入した空気を圧縮行程に於て主
室よりスロート部を介して渦室内に押し込み、圧
縮行程の終期に燃料を渦室に噴射する。それによ
つて渦室内に形成された混合気が着火して燃焼が
始まり、渦室内の燃焼ガスはスロート部を介して
主室に噴出され、主室内にある空気と混合して更
に燃焼するように成つている。
A diesel engine with a vortex chamber has a main chamber (main combustion chamber) formed at the top of the piston and a vortex chamber located in the cylinder head, and the two are connected at the throat of the vortex chamber. There is. The air sucked into the cylinder during the intake stroke is forced into the vortex chamber from the main chamber through the throat portion during the compression stroke, and fuel is injected into the vortex chamber at the end of the compression stroke. As a result, the air-fuel mixture formed in the vortex chamber ignites and combustion begins, and the combustion gas in the vortex chamber is ejected into the main chamber through the throat section, where it mixes with the air in the main chamber and is further combusted. It is completed.

この燃焼原理に基づく燃焼室構造としては、第
1図、第2図に示すように、主室1がクローバー
形の凹部として、ピストン2の頂上部3にその縁
部近傍からピストン中心に向けて形成されている
ものが広く用いられている。
As shown in FIGS. 1 and 2, the combustion chamber structure based on this combustion principle is such that the main chamber 1 is a clover-shaped recess that extends from near the edge of the piston 2 toward the center of the piston. Those formed are widely used.

この主室1は図から明らかなように、クローバ
ーの葉に相当する2つの円形部分11a,11b
から成る拡散部11と、クローバーの莖に相当す
るトレンチ部12とを有していて、シリンダヘツ
ド4側に配設された内部に空気渦流を生成する渦
室5のスロート部51を介して噴出した燃焼ガス
は上記トレンチ部12からの拡散部11に流入し
て拡散部11の円形状の偏向壁13によりその進
路を変向して旋回流を形成しつつ外部に拡散し、
シリンダ内の空気と混合して燃焼させるように構
成されている。
As is clear from the figure, this main chamber 1 has two circular parts 11a and 11b corresponding to clover leaves.
The air is ejected through the throat part 51 of the vortex chamber 5, which has a diffusion part 11 consisting of a crowbar and a trench part 12 corresponding to a clover pod, and which generates an air vortex inside the cylinder head 4 side. The combustion gas flows into the diffusion section 11 from the trench section 12, changes its course by the circular deflection wall 13 of the diffusion section 11, and diffuses to the outside while forming a swirling flow.
It is configured to be mixed with the air in the cylinder and combusted.

尚、第1図中、6はシリンダボデー、7は燃料
噴射ノズル、8はグロープラグを示している。と
ころが、このような燃焼室構造においては上記ス
ロート部51の巾toを大きくすると、高負荷時に
おける出力が増大すると共に第3図に示すように
渦室5におけるNox(N)の生成率は低減する反
面、スモーク(S)の生成率が増大するという不
具合があり、上記スロート部51の巾toを高負荷
時における出力増大とNox低減効果のための理
想値よりも小さいものにしなければならないとい
う欠点があつた。
In FIG. 1, 6 indicates a cylinder body, 7 indicates a fuel injection nozzle, and 8 indicates a glow plug. However, in such a combustion chamber structure, when the width of the throat portion 51 is increased, the output at high loads increases and the generation rate of Nox (N) in the vortex chamber 5 decreases as shown in FIG. 3. On the other hand, there is a problem that the generation rate of smoke (S) increases, and the width of the throat portion 51 must be made smaller than the ideal value for increasing output and reducing Nox under high loads. There were flaws.

本案は上述の欠点を克服するために案出したも
ので、その目的は、高負荷時における出力の増大
とNoxの低減効果とを図るように渦室のスロー
ト部の巾を理想値に保持しつつスモークを低減せ
しめるようにした渦室付デイーゼルエンジンの燃
焼室を提供せんとするもので、以下その実施例を
図について説明する。
This project was devised to overcome the above-mentioned drawbacks, and its purpose is to maintain the width of the throat portion of the vortex chamber at an ideal value in order to increase output and reduce NOx under high loads. It is an object of the present invention to provide a combustion chamber for a diesel engine with a vortex chamber that reduces smoke while reducing smoke, and an embodiment thereof will be described below with reference to the drawings.

前述の如き、渦室5のスロート部51と連絡す
るトレンチ部12から拡大分岐せる略々円形状の
2つの円形部分11a,11bを持つた拡散部1
1とをピストン2の縁部近傍からその中心に向け
て頂上部3に形成して成る渦室付デイーゼルエン
ジンにおいて、上記トレンチ部12の巾tを上記
渦室のスロート部51の巾toよりも小さく形成し
たものである。
As described above, the diffusion section 1 has two substantially circular circular sections 11a and 11b that expand and branch from the trench section 12 that communicates with the throat section 51 of the vortex chamber 5.
1 is formed on the top portion 3 of the piston 2 from near the edge toward its center, the width t of the trench portion 12 is greater than the width to of the throat portion 51 of the vortex chamber. It is made small.

上述の如き構成を有する燃焼室においては、ス
ロート部51の巾toが比較的大なるものにしたの
で、高負荷時における出力増大とNox低減が図
れると共に、渦室5よりの燃焼ガスBがスロート
部51を介して主室1側に噴出されるが、トレン
チ部12の巾tが小さいためにここで絞られて流
速が増大されて拡散部11へと流入するため、主
室1における燃焼ガスと未燃空気との混合燃焼が
促進されるため渦室5内での燃焼時に生成された
スモークは主室1での燃焼においてほとんど消去
されてしまう。
In the combustion chamber configured as described above, the width of the throat portion 51 is made relatively large, so that output can be increased and Nox reduced during high loads, and the combustion gas B from the vortex chamber 5 can flow through the throat. The combustion gas in the main chamber 1 is ejected to the main chamber 1 side through the section 51, but because the width t of the trench section 12 is small, it is narrowed here and the flow velocity is increased and flows into the diffusion section 11. Since mixed combustion of the fuel and unburned air is promoted, the smoke generated during combustion in the vortex chamber 5 is almost eliminated during combustion in the main chamber 1.

よつて、エンジン全体としては、高負荷時の出
力増大が図れると共に、排気有害成分としての
Noxやスモークの少ない理想的な燃焼状態が得
られる利点がある。
Therefore, the overall engine output can be increased during high loads, and the harmful components of exhaust gas can be reduced.
It has the advantage of providing ideal combustion conditions with less Nox and smoke.

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

第1図は本案実施例における燃焼室付近を示す
縦断面図、第2図は同実施例における渦室と主室
との関係を示す概略平面図、第3図は渦室のスロ
ート部toによる排気特性を示す特性図である。 1;主室、2;ピストン、5;渦室、11;拡
散部、12;トレンチ部、51;スロート部、
B;燃焼ガス。
Fig. 1 is a longitudinal sectional view showing the vicinity of the combustion chamber in this embodiment, Fig. 2 is a schematic plan view showing the relationship between the vortex chamber and the main chamber in the same embodiment, and Fig. 3 is a view of the throat section of the vortex chamber. FIG. 3 is a characteristic diagram showing exhaust characteristics. 1; Main chamber, 2; Piston, 5; Vortex chamber, 11; Diffusion part, 12; Trench part, 51; Throat part,
B; Combustion gas.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 渦室のスロート部と連絡するトレンチ部とその
トレンチ部から拡大分岐せる略々円形状の2つの
円形部分を持つた拡散部とをピストンの縁部近傍
からその中心に向けて頂上部に形成して成る渦室
付デイーゼルエンジンの燃焼室において、上記ト
レンチ部の巾tを上記渦室のスロート部の巾toよ
りも小さくしたことを特徴とする渦室付デイーゼ
ルエンジンの燃焼室。
A trench part communicating with the throat part of the vortex chamber and a diffusion part having two substantially circular parts expanding and branching from the trench part are formed at the top part from near the edge of the piston toward the center thereof. 1. A combustion chamber for a diesel engine with a swirl chamber, characterized in that the width t of the trench portion is smaller than the width to of the throat portion of the swirl chamber.
JP15648680U 1980-10-31 1980-10-31 Expired JPS6319544Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15648680U JPS6319544Y2 (en) 1980-10-31 1980-10-31

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15648680U JPS6319544Y2 (en) 1980-10-31 1980-10-31

Publications (2)

Publication Number Publication Date
JPS5778724U JPS5778724U (en) 1982-05-15
JPS6319544Y2 true JPS6319544Y2 (en) 1988-06-01

Family

ID=29515641

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15648680U Expired JPS6319544Y2 (en) 1980-10-31 1980-10-31

Country Status (1)

Country Link
JP (1) JPS6319544Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100729293B1 (en) 2006-04-11 2007-06-15 국제종합기계 주식회사 Swirl chamber type diesel engine

Also Published As

Publication number Publication date
JPS5778724U (en) 1982-05-15

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