JPS5926772B2 - Pre-chamber internal combustion engine - Google Patents

Pre-chamber internal combustion engine

Info

Publication number
JPS5926772B2
JPS5926772B2 JP2771277A JP2771277A JPS5926772B2 JP S5926772 B2 JPS5926772 B2 JP S5926772B2 JP 2771277 A JP2771277 A JP 2771277A JP 2771277 A JP2771277 A JP 2771277A JP S5926772 B2 JPS5926772 B2 JP S5926772B2
Authority
JP
Japan
Prior art keywords
combustion chamber
fuel
sub
fuel injection
injection valve
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
JP2771277A
Other languages
Japanese (ja)
Other versions
JPS53112310A (en
Inventor
浩二 井元
敬造 後藤
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 JP2771277A priority Critical patent/JPS5926772B2/en
Publication of JPS53112310A publication Critical patent/JPS53112310A/en
Publication of JPS5926772B2 publication Critical patent/JPS5926772B2/en
Expired legal-status Critical Current

Links

Description

【発明の詳細な説明】 本発明は副室式内燃機関、特に副室内に生成される空気
渦流中に燃料を噴射して着火燃焼せしめるようにした副
室式ディーゼル機関における燃焼性能の改善に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to improving combustion performance in a pre-chamber internal combustion engine, particularly in a pre-chamber diesel engine in which fuel is injected into an air vortex generated in the pre-chamber for ignition and combustion.

従来の副室式ディーゼル機関の1例を第1図及び第2図
に示す。
An example of a conventional pre-chamber type diesel engine is shown in FIGS. 1 and 2.

かかる副室式ディーゼル機関においては、シリンダヘッ
ド1内に凹設された副燃焼室5内に臨んで、燃料噴射弁
8及び機関の始動時に副燃焼室5内を予熱するグロープ
ラグ4が設けられると共に、副燃焼室5は連絡孔6を介
してピストン2の上面に形成された主燃焼室7と連通さ
れる。
In such an auxiliary chamber type diesel engine, a fuel injection valve 8 and a glow plug 4 that preheats the inside of the auxiliary combustion chamber 5 at the time of starting the engine are provided facing into the auxiliary combustion chamber 5 recessed in the cylinder head 1. At the same time, the sub-combustion chamber 5 communicates with a main combustion chamber 7 formed on the upper surface of the piston 2 via a communication hole 6 .

3はシリンダである。しかして機関の運転時においては
、ピストン2の圧縮行程の後半に主燃焼室T内の空気が
連絡孔6を経て副燃焼室5内に流入し渦流Aを生成する
3 is a cylinder. During operation of the engine, air in the main combustion chamber T flows into the auxiliary combustion chamber 5 through the communication hole 6 during the latter half of the compression stroke of the piston 2, producing a vortex flow A.

そして該渦流Aの方向に沿って燃料噴射弁8より燃料を
噴射すると燃料は渦流Aとともに副燃焼室5内を旋回す
る。
When fuel is injected from the fuel injection valve 8 along the direction of the vortex A, the fuel swirls in the sub-combustion chamber 5 along with the vortex A.

この場合、混合気は上記渦流Aのみを利用して生成され
ることになるため、混合気生成が遅れがちになり、この
ため着火遅れ期間が長くなり、初期燃焼は悪化する。
In this case, since the mixture is generated using only the vortex A, the generation of the mixture tends to be delayed, which lengthens the ignition delay period and deteriorates the initial combustion.

す々わち、この長い着火遅れ期間中に生成された混合気
が瞬時にして、燃焼するために、副燃焼室5内における
最高ガス圧力、及びガス圧力の上昇率が大きくなる。
In other words, since the air-fuel mixture generated during this long ignition delay period is instantaneously combusted, the maximum gas pressure in the auxiliary combustion chamber 5 and the rate of increase in gas pressure become large.

このため機関の振動、騒音が過大になると同時に、すす
も発生しやすくなる。
As a result, engine vibration and noise become excessive, and at the same time, soot becomes more likely to be generated.

このような欠点を補なうために、燃料噴射弁8の噴霧角
αを大きくしても、大部分の燃料は噴霧中心線近傍に分
布するために、噴霧周辺のわずかな部分が空気渦流Aと
交叉するだけで、燃料の分散、微粒化促進効果は小さく
混合気生成を促進できないのが現状である。
Even if the spray angle α of the fuel injector 8 is increased to compensate for such drawbacks, most of the fuel is distributed near the center line of the spray, so a small portion around the spray is affected by the air vortex A. At present, the effect of promoting fuel dispersion and atomization is small and it is not possible to promote air-fuel mixture formation simply by intersecting with .

本発明は、上記に鑑み、副燃焼室内における空気渦流と
燃料噴霧との混合を改良せしめることによシシリンダ内
最高圧力の上昇を抑え機関の振動、騒音等を低減した副
室式内燃機関を提供することを目的としてなされたもの
であり、その特徴とするところは、副室式内燃機関にお
いて燃料噴射弁を上記連絡孔の中心延長線から外れ、か
つ該燃料噴射弁から噴射される燃料噴霧の中心線が空気
渦流の流線に対し斜め下流方向に交叉する位置に設置し
たことにある。
In view of the above, the present invention provides a pre-combustion internal combustion engine that suppresses the rise in maximum cylinder pressure and reduces engine vibration, noise, etc. by improving the mixing of air vortex and fuel spray in the sub-combustion chamber. It was developed with the purpose of This is because the center line intersects the streamline of the air vortex in the diagonal downstream direction.

以下第3図及び第4図を参照して本発明の1実施例につ
き説明する。
One embodiment of the present invention will be described below with reference to FIGS. 3 and 4.

1はシリンダヘッド、2はピストン、3はシリンダ、5
は該シリンダヘッド、1内に凹設された副燃焼室、7は
主燃焼室、6は上記副燃焼室5と主燃焼室7とを連通ず
る連絡孔であり、これらの構成は従来のものと同様であ
る。
1 is the cylinder head, 2 is the piston, 3 is the cylinder, 5
1 is a sub-combustion chamber recessed in the cylinder head, 7 is a main combustion chamber, and 6 is a communication hole that communicates the sub-combustion chamber 5 with the main combustion chamber 7, and these structures are conventional ones. It is similar to

8は上記副燃焼室5内に燃料を噴射するための燃料噴射
弁で、該燃料噴射弁8は、副燃焼室5内における平面位
置が上記連絡孔6の中心線6aから外れ、かつこれより
噴射される燃料噴霧の中心線が空気渦流Aの流線に対し
斜め下流方向に交叉する位置に設置される。
Reference numeral 8 denotes a fuel injection valve for injecting fuel into the auxiliary combustion chamber 5, and the fuel injection valve 8 has a planar position within the auxiliary combustion chamber 5 that is deviated from the center line 6a of the communication hole 6, and is further away from the center line 6a of the communication hole 6. It is installed at a position where the center line of the injected fuel spray intersects the streamline of the air vortex A in the diagonally downstream direction.

即ち燃料噴射弁8から噴射される燃料の噴霧の中心線り
が、空気渦流Aに対して該渦流Aの下流方向にYの角度
で交叉するように燃料噴射弁8を設置する。
That is, the fuel injection valve 8 is installed so that the center line of the fuel spray injected from the fuel injection valve 8 intersects the air vortex A in the downstream direction of the vortex A at an angle Y.

かかる構成を具えた副室式内燃機関を運転する際は、ピ
ストン2の圧縮行程において、ピストン2が上昇するこ
とにより、主燃焼室7内の空気が、圧縮されることによ
り、主燃焼室7・副燃焼室5間に千力差が生じるため、
主燃焼室7内の空気は連絡孔6を通って副燃焼室5内に
移動する。
When operating a sub-combustion internal combustion engine with such a configuration, the air in the main combustion chamber 7 is compressed as the piston 2 rises during the compression stroke of the piston 2.・Because there is a difference in power between the sub-combustion chambers 5,
Air in the main combustion chamber 7 moves into the sub-combustion chamber 5 through the communication hole 6.

その移動した空気は副燃焼室5内において、副燃焼室5
の内壁に沿った渦流Aを生ずる。
The moved air is stored in the sub-combustion chamber 5.
produces a vortex A along the inner wall of the

この渦流Aに対し燃料の噴口を副燃焼室5内に臨ませて
設置された燃料噴射弁8から燃料を噴射する。
Fuel is injected into this vortex A from a fuel injection valve 8 installed with a fuel nozzle facing into the sub-combustion chamber 5.

そして噴射された燃料噴霧は、空気渦流Aと交叉、衝突
するために燃料と空気との間に小さな乱れを生起し燃料
噴霧の微粒化、分散が促進される。
The injected fuel spray intersects and collides with the air vortex A, causing small turbulence between the fuel and air, which promotes atomization and dispersion of the fuel spray.

第5図は本発明の他の実施例を示し、この場合は2個の
燃料噴射弁8ay sbを副燃焼室5内において連絡孔
6の中心線6aをはさみ、かつ個個の燃料噴射弁8ap
sbから噴射される燃料噴霧の中心線Da p Db
が空気渦流Aに対し斜め下流方向に交叉する位置に夫々
設置する。
FIG. 5 shows another embodiment of the present invention, in which two fuel injection valves 8ay sb are sandwiched between the center line 6a of the communication hole 6 in the auxiliary combustion chamber 5, and the individual fuel injection valves 8ap
Center line of fuel spray injected from sb Da p Db
are installed at positions where they intersect with the air vortex A in a diagonal downstream direction.

この場合は、空気渦流Aの両側面に燃料噴霧が衝突する
ので燃料噴霧の微粒化、分散が第1実施例の場合よりも
更に促進される。
In this case, since the fuel spray collides with both sides of the air vortex A, atomization and dispersion of the fuel spray are further promoted than in the first embodiment.

以上述べたように本発明に係る副室式内燃機関は、燃料
噴射弁を、副燃焼室内における平面位置が連絡孔の中心
線から外れ、かつ燃料噴霧の中心線が空気渦流に対し斜
め下流方向に交叉する位置に設置I〜だので、 (1) ピストンの圧縮行程の終り近くで、副燃焼室
内の空気渦流に対し、燃料が斜め方向から衝突し、小さ
な乱れをひきおこすと同時に燃料の微粒化、分散を促進
し、混合気形成、着火、咀には、空気利用率の向上を図
ることができる。
As described above, the auxiliary chamber type internal combustion engine according to the present invention has a fuel injection valve whose planar position in the auxiliary combustion chamber is off the center line of the communication hole, and where the center line of the fuel spray is diagonally downstream with respect to the air vortex. (1) Near the end of the piston's compression stroke, the fuel collides with the air vortex in the sub-combustion chamber from an oblique direction, causing small turbulence and at the same time atomizing the fuel. , promotes dispersion, and improves air utilization efficiency for mixture formation, ignition, and mastication.

このためシリンダ内の最高川内及び川内上昇率が低減さ
れ、機関の振動、騒音を低減することができる。
Therefore, the maximum inflow and inflow rate of rise in the cylinder are reduced, and vibration and noise of the engine can be reduced.

(2)混合気形成が促進されるため、燃料噴射時期を遅
くすることができ、この点からも機関の振動、騒音が低
減される。
(2) Since mixture formation is promoted, fuel injection timing can be delayed, and from this point of view as well, engine vibration and noise are reduced.

(3)連絡孔におけるガス流動損失を低減するために、
連絡孔の通路面積を拡大するような場合に起る副燃焼室
内での空気渦流の弱体化を、燃料噴霧を空気渦流に対し
斜め下流方向に交叉、衝突させることによる乱れ発生の
利用により、補足することができる。
(3) To reduce gas flow loss in the communication hole,
The weakening of the air vortex in the sub-combustion chamber, which occurs when the passage area of the communication hole is expanded, can be compensated for by utilizing the turbulence generated by causing the fuel spray to cross and collide diagonally downstream with the air vortex. can do.

という実用的効果を奏することができる。This practical effect can be achieved.

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

第1図及び第2図は、従来の副室式ディーゼル機関の1
例を示し、第1図は副燃焼室近傍の断面図、第2図は第
1図のB−B線に沿う断面図である。 第3図及び第4図は本発明の1実施例を示し、第3図は
第1図に相当する断面図、第4図は第3図のC−C線に
沿う断面図である。 第5図は本発明の他の実施例を示した第4図に相当する
断面図である。 1・・・・・・シリンダヘッド、2・・・・・・ピスト
ン、3・・・・・・シリンダ、4・・・・・・グロープ
ラグ、5・・・・・・副燃焼室、6・・・・・・連絡孔
、7・・・・・・主燃焼室、8,8a。 8b・・・・・・燃料噴射弁、A・・・・・・空気渦流
、Dt DayDb・・・・・・燃料噴霧中心線。
Figures 1 and 2 show one example of a conventional pre-chamber diesel engine.
As an example, FIG. 1 is a cross-sectional view of the vicinity of the sub-combustion chamber, and FIG. 2 is a cross-sectional view taken along line BB in FIG. 1. 3 and 4 show one embodiment of the present invention, with FIG. 3 being a sectional view corresponding to FIG. 1, and FIG. 4 being a sectional view taken along the line CC in FIG. 3. FIG. 5 is a sectional view corresponding to FIG. 4 showing another embodiment of the present invention. 1... Cylinder head, 2... Piston, 3... Cylinder, 4... Glow plug, 5... Sub-combustion chamber, 6 ...Communication hole, 7...Main combustion chamber, 8, 8a. 8b...Fuel injection valve, A...Air vortex, Dt DayDb...Fuel spray center line.

Claims (1)

【特許請求の範囲】[Claims] 1 連絡孔を介して主燃焼室に連通される副燃焼室と該
副燃焼室内に生成される空気渦流中に燃料を噴射する燃
料噴射弁とを具えた内燃機関において、上記燃料噴射弁
を、上記副燃焼室内における平面位置が上記連絡孔の中
心線から外れ、かつ該燃料噴射弁から噴射される燃料噴
霧の中心線が上記渦流に対し斜め下流方向に交叉する位
置に設置したことを特徴とする副室式内燃機関。
1. In an internal combustion engine comprising a sub-combustion chamber that communicates with a main combustion chamber via a communication hole and a fuel injection valve that injects fuel into an air vortex generated within the sub-combustion chamber, the fuel injection valve: The planar position in the auxiliary combustion chamber is located away from the center line of the communicating hole, and the center line of the fuel spray injected from the fuel injection valve intersects the vortex in a diagonal downstream direction. A pre-chamber internal combustion engine.
JP2771277A 1977-03-14 1977-03-14 Pre-chamber internal combustion engine Expired JPS5926772B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2771277A JPS5926772B2 (en) 1977-03-14 1977-03-14 Pre-chamber internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2771277A JPS5926772B2 (en) 1977-03-14 1977-03-14 Pre-chamber internal combustion engine

Publications (2)

Publication Number Publication Date
JPS53112310A JPS53112310A (en) 1978-09-30
JPS5926772B2 true JPS5926772B2 (en) 1984-06-30

Family

ID=12228599

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2771277A Expired JPS5926772B2 (en) 1977-03-14 1977-03-14 Pre-chamber internal combustion engine

Country Status (1)

Country Link
JP (1) JPS5926772B2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5960170U (en) * 1982-10-13 1984-04-19 則直 学 Self-heating or cooling containers
JPH01100070U (en) * 1987-12-22 1989-07-05

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5592030U (en) * 1978-12-21 1980-06-25

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5960170U (en) * 1982-10-13 1984-04-19 則直 学 Self-heating or cooling containers
JPH01100070U (en) * 1987-12-22 1989-07-05

Also Published As

Publication number Publication date
JPS53112310A (en) 1978-09-30

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