JPH04136415A - Auxiliary combustion chamber type diesel engine - Google Patents
Auxiliary combustion chamber type diesel engineInfo
- Publication number
- JPH04136415A JPH04136415A JP25959790A JP25959790A JPH04136415A JP H04136415 A JPH04136415 A JP H04136415A JP 25959790 A JP25959790 A JP 25959790A JP 25959790 A JP25959790 A JP 25959790A JP H04136415 A JPH04136415 A JP H04136415A
- Authority
- JP
- Japan
- Prior art keywords
- combustion chamber
- piston
- main combustion
- inclination
- projection
- 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
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 68
- 239000000446 fuel Substances 0.000 abstract description 9
- 239000000779 smoke Substances 0.000 abstract description 5
- 239000000567 combustion gas Substances 0.000 abstract description 3
- 238000009792 diffusion process Methods 0.000 abstract description 3
- 238000002347 injection Methods 0.000 abstract description 2
- 239000007924 injection Substances 0.000 abstract description 2
- 230000002093 peripheral effect Effects 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 12
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
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
- 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
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は、主燃焼室内での空気と部分燃焼ガスとの混合
が良好な副燃焼室式ディーゼルエンジンに関する。DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a sub-combustion chamber type diesel engine in which air and partially combusted gas are well mixed in the main combustion chamber.
(従来の技術)
従来の副燃焼室式ディーゼルエンジンは、圧縮時におけ
る副燃焼室内の空気量を燃焼室全体の空気量の約50%
となるように設定している。そして、圧縮行程終期にて
該副燃焼室内に噴射された燃料は副燃焼室内の空気と混
合し燃焼を開始するため、該副燃焼室内部は高温高圧状
態となる6該副燃焼室内の燃焼ガス及び未燃焼ガスの混
合気である部分燃焼ガスは、噴孔を介して主燃焼室へと
噴出し、主燃焼室内の空気と2次混合し燃焼を継続する
。尚、主燃焼室で燃焼が継続する時にはピストンが下降
途中であり、従って主燃焼室の体積が膨張途中であるた
め、燃焼温度は低温度で維持される。(Prior art) In a conventional sub-combustion chamber type diesel engine, the amount of air in the sub-combustion chamber during compression is approximately 50% of the total air amount in the combustion chamber.
It is set so that The fuel injected into the sub-combustion chamber at the end of the compression stroke mixes with the air in the sub-combustion chamber and starts combustion, so the inside of the sub-combustion chamber becomes high temperature and high pressure.6 Combustion gas in the sub-combustion chamber Partially burned gas, which is a mixture of unburned gas and unburned gas, is injected into the main combustion chamber through the nozzle hole, mixed with the air in the main combustion chamber, and continues combustion. Note that when combustion continues in the main combustion chamber, the piston is in the process of descending, and therefore the volume of the main combustion chamber is in the process of expanding, so that the combustion temperature is maintained at a low temperature.
上記のごと(、燃料が噴射される副燃焼室内には空気全
体の50%しか充填されないため、該副燃焼室内での当
量比C空気量に対する燃料の比率)が大となり、また主
燃焼室での燃焼は低温度状態で継続されるため、副燃焼
室を有さない直噴式ディーゼルエンジンと比較して、N
Oxの生成が抑制され排気ガスに含有されるNOxの排
出量が大幅に低下する。As mentioned above (because only 50% of the total air is filled in the auxiliary combustion chamber where fuel is injected, the equivalence ratio C in the auxiliary combustion chamber is the ratio of fuel to the amount of air), and in the main combustion chamber Since the combustion of N continues at a low temperature, the N
The generation of Ox is suppressed and the amount of NOx contained in the exhaust gas is significantly reduced.
(発明が解決しようとする課H)
このような従来の副燃焼室式ディーゼルエンジンでは、
ピストン上昇時には主燃焼室内の空気は副燃焼室内へと
スキッシュ流となって流入するものの、ピストン下降時
には副燃焼室内部から主燃焼室への逆スキッシュ流が殆
ど発生せず、副燃焼室内の部分燃焼ガスと主燃焼室内の
空気との混合は、副燃焼室での燃焼に伴う部分燃焼ガス
の噴出によってのみ行なわれる。(Problem H to be solved by the invention) In such a conventional sub-combustion chamber type diesel engine,
When the piston rises, the air in the main combustion chamber flows into the sub-combustion chamber as a squish flow, but when the piston descends, there is almost no reverse squish flow from inside the sub-combustion chamber to the main combustion chamber, and the air inside the sub-combustion chamber Combustion gas and air in the main combustion chamber are mixed only by ejection of partially combusted gas accompanying combustion in the auxiliary combustion chamber.
従って、主燃焼室内での空気と部分燃焼ガスとの混合に
要する時間が長時間化し、不完全燃焼状態で燃焼が停止
する場合がある。すると、排気ガス中に含まれる黒煙の
量が増加し、また、エンジンの出力や効率が低下する。Therefore, the time required for mixing the air and the partially combusted gas in the main combustion chamber becomes long, and combustion may stop in an incomplete combustion state. As a result, the amount of black smoke contained in the exhaust gas increases, and the output and efficiency of the engine decrease.
本発明は、上記の点に鑑みてなされたもので、主燃焼室
内での空気と部分燃焼ガスとの混合時間を短縮し、黒煙
の排出量を抑制すると共に、出力や効率が低下しない副
燃焼室式ディーゼルエンジンを提供しようとするもので
ある。The present invention has been made in view of the above points, and it shortens the mixing time of air and partially combusted gas in the main combustion chamber, suppresses the amount of black smoke emission, and reduces the amount of black smoke emitted. The aim is to provide a combustion chamber type diesel engine.
(課題を解決するための手段)
本発明によれば、ピストンの端面上に設けられ該端面に
対する傾斜角度が漸次増加する斜面を有する突起と、該
突起を形成する斜面と対向しピストンの上死点位置にて
該斜面との間に一定厚みの主燃焼室を形成するシリンダ
内端面と、上記突起頂部と対向する位置に設けられ副燃
焼室と上記主燃焼室とを連通する噴孔とを有することを
特徴とする副燃焼室式ディーゼルエンジンを提供できる
。(Means for Solving the Problems) According to the present invention, a projection having a slope provided on an end surface of a piston and having a slope whose inclination angle with respect to the end surface gradually increases; an inner end surface of the cylinder forming a main combustion chamber with a constant thickness between the slope and the slope at a point position, and a nozzle hole provided at a position facing the top of the protrusion and communicating the sub-combustion chamber with the main combustion chamber. It is possible to provide a sub-combustion chamber type diesel engine having the following features.
(作用)
本発明の副燃焼室式ディーゼルエンジンでは、ピストン
下降時における主燃焼室の体積増加速度は、ピストンに
設けられた突起斜面の傾斜が急な部分より緩やかな部分
の方が大であるため、部分燃焼ガスの逆スキッシュ流速
が加速され、主燃焼室内への拡散が促進される。(Function) In the auxiliary combustion chamber type diesel engine of the present invention, the volume increase rate of the main combustion chamber when the piston descends is greater in the part where the slope of the protrusion provided on the piston is gentler than in the steep part. Therefore, the reverse squish flow velocity of the partially combusted gas is accelerated, and its diffusion into the main combustion chamber is promoted.
(実施例) 以下、本発明の実施例を図面を用いて詳細に説明する。(Example) Embodiments of the present invention will be described in detail below with reference to the drawings.
第1図は、本発明によるエンジンの一実施例の構造を示
す断面図である。FIG. 1 is a sectional view showing the structure of an embodiment of an engine according to the present invention.
1はエンジン本体であり、該エンジン本体1の内部には
ピストン2が配設されている。該ピストン2の上端部の
中央には、突起21が突設されている。そして、該突起
21が有する斜面の傾斜は中央部が急であり、周辺部に
行くに従い漸次縁やかになるように形成されている。尚
、本図は該ピストン2が上死点位置にある場合を示して
おり、主燃焼室は一定の厚みに形成されている。1 is an engine body, and a piston 2 is disposed inside the engine body 1. A protrusion 21 is provided at the center of the upper end of the piston 2 . The slope of the protrusion 21 is steep at the center and gradually becomes steeper toward the periphery. Note that this figure shows a case where the piston 2 is at the top dead center position, and the main combustion chamber is formed to have a constant thickness.
3は副燃焼室であり、該副燃焼室3内部に燃料を噴射す
る燃料噴射ノズル31と、エンジン始動時等に燃料の着
火を補助するグロープラグ32とが配設されている。3 is an auxiliary combustion chamber, and a fuel injection nozzle 31 that injects fuel into the auxiliary combustion chamber 3 and a glow plug 32 that assists in igniting the fuel at the time of starting the engine, etc. are disposed.
次に、上記構成によるエンジンの作用について説明する
。Next, the operation of the engine with the above configuration will be explained.
第2図は、上記ピストン2の下降途中の状態を示す図で
ある。FIG. 2 is a diagram showing a state in which the piston 2 is in the middle of its descent.
ピストン2の下降に伴い主燃焼室の内部容積は増加する
が、ピストン2の上端面の傾斜が一定で無いため、該内
部容積の増加速度は主燃焼室内の箇所により異なる。The internal volume of the main combustion chamber increases as the piston 2 descends, but since the slope of the upper end surface of the piston 2 is not constant, the rate of increase in the internal volume varies depending on the location within the main combustion chamber.
第2図のaにて示す部分はピストン2の上端面の傾斜が
緩やかであり、はぼ水平状態にある部分である。これに
対しbにて示す部分は傾斜が急であり、はぼ垂直な部分
である。The portion indicated by a in FIG. 2 is a portion where the upper end surface of the piston 2 has a gentle slope and is in a nearly horizontal state. On the other hand, the part indicated by b has a steep slope and is almost vertical.
第2図から明らかなごとく、傾斜が緩やかであるa部と
、傾斜が急なり部とでは内部容積の増加速度が異なり、
傾斜が緩やかであるa部の方が内部容積増加速度が大と
なる。As is clear from Fig. 2, the rate of increase in internal volume is different between section a, where the slope is gentle, and section a, where the slope is steep.
The rate of increase in internal volume is higher in section a where the slope is gentler.
また、ピストン2の上端面の傾斜は副燃焼室3との連通
孔である噴孔近傍が急であり、該噴孔から離れるに従っ
て緩やかとなるため、逆スキッシュ流はより傾斜が緩や
かな部分へと加速され、主燃焼室内に拡散することにな
る。In addition, the slope of the upper end surface of the piston 2 is steep near the nozzle hole that communicates with the sub-combustion chamber 3, and becomes gentler as it moves away from the nozzle hole, so the reverse squish flow flows toward the part with a gentler slope. It is accelerated and diffused into the main combustion chamber.
ところで、上記にて突起がピストン上端面の中央部分に
設けられた実施例について説明したが、該突起を設ける
箇所はピストン上端面の中央部に限定されるものではな
い。By the way, although the embodiment in which the protrusion is provided at the center of the upper end surface of the piston has been described above, the location where the protrusion is provided is not limited to the center of the upper end surface of the piston.
第3図は、他の実施例におけるエンジンの構造を示す断
面図である。FIG. 3 is a sectional view showing the structure of an engine in another embodiment.
4はピストンであり、該ピストン4の上端部には周辺部
に偏心された突起41が設けられている。そして、該突
起41に対応する部分には副燃焼室5が設けられている
。4 is a piston, and the upper end of the piston 4 is provided with a protrusion 41 that is eccentric around the periphery. A sub-combustion chamber 5 is provided in a portion corresponding to the protrusion 41.
上記突起41の有する斜面は噴孔近傍部分が最も急であ
り、本図の右方向すなわち噴孔から離れるに従って緩や
かになるように形成されている。The slope of the protrusion 41 is steepest in the vicinity of the nozzle hole, and becomes gentler toward the right in the figure, that is, as it moves away from the nozzle hole.
従って、該ピストン4の下降に伴い、副燃焼室5からの
逆スキッシュ流は本図の右方向へと加速され主燃焼室内
に拡散される。Therefore, as the piston 4 descends, the reverse squish flow from the auxiliary combustion chamber 5 is accelerated to the right in the figure and diffused into the main combustion chamber.
上記において、本発明の実施例について詳細に説明した
が、本発明の精神から逸れないかぎりで、種々の異なる
実施例は容易に構成できるから、本発明は上記特許請求
の範囲において記載した限定以外、特定の実施例に制約
されるのものではない。Although the embodiments of the present invention have been described in detail above, various different embodiments can be easily constructed without departing from the spirit of the invention, and therefore, the present invention is not limited to any limitations other than those set forth in the claims. , and is not limited to any particular implementation.
(発明の効果)
以上説明したように、本発明によれば、ピストン下降時
における主燃焼室の体積増加速度が、ピストンに設けら
れた突起斜面の傾斜が急な部分より緩やかな部分の方が
大であるため、部分燃焼ガスの逆スキッシュ流速が加速
され、主燃焼室内への拡散が促進され、従って、主燃焼
室内での空気と部分燃焼ガスとの混合時間が短縮され、
黒煙の排出量が抑制されると共に、出力や効率が低下し
ない副燃焼室式ディーゼルエンジンを提供できる。(Effects of the Invention) As explained above, according to the present invention, the volume increase rate of the main combustion chamber when the piston descends is slower in the part where the slope of the protrusion provided on the piston is steeper than in the part where the slope is steeper. Because of the large size, the reverse squish flow velocity of the partially combusted gas is accelerated, the diffusion into the main combustion chamber is promoted, and therefore the mixing time of the air and the partially combusted gas in the main combustion chamber is shortened.
It is possible to provide a sub-combustion chamber type diesel engine in which the amount of black smoke emission is suppressed and the output and efficiency do not decrease.
第1図は、本発明によるエンジンの一実施例の構造を示
す断面図、第2図は、上記ピストン2の下降途中の状態
を示す図、第3図は、他の実施例におけるエンジンの構
造を示す断面図である。
1・・・、エンジン本体、2・・・ピストン、3・・・
副燃焼室、4・・・ピストン、5・・・副燃焼室、21
・・・突起、41・・・突起。FIG. 1 is a cross-sectional view showing the structure of one embodiment of the engine according to the present invention, FIG. 2 is a diagram showing the state in which the piston 2 is in the middle of its descent, and FIG. 3 is the structure of the engine in another embodiment. FIG. 1... Engine body, 2... Piston, 3...
Sub-combustion chamber, 4... Piston, 5... Sub-combustion chamber, 21
...Protrusion, 41...Protrusion.
Claims (2)
角度が漸次増加する斜面を有する突起と、該突起を形成
する斜面と対向しピストンの上死点位置にて該斜面との
間に一定厚みの主燃焼室を形成するシリンダ内端面と、
上記突起頂部と対向する位置に設けられ副燃焼室と上記
主燃焼室とを連通する噴孔とを有することを特徴とする
副燃焼室式ディーゼルエンジン。(1) A constant thickness exists between a protrusion provided on the end face of the piston and having a slope whose inclination angle with respect to the end face gradually increases, and the slope that faces the slope forming the protrusion and is located at the top dead center position of the piston. an inner end surface of the cylinder forming the main combustion chamber;
A sub-combustion chamber type diesel engine, comprising a nozzle hole provided at a position facing the top of the protrusion and communicating the sub-combustion chamber with the main combustion chamber.
れたことを特徴とする請求項(1)記載の副燃焼室式デ
ィーゼルエンジン。(2) The auxiliary combustion chamber type diesel engine according to claim (1), wherein the protrusion is provided at the center of the end surface of the piston.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25959790A JPH04136415A (en) | 1990-09-28 | 1990-09-28 | Auxiliary combustion chamber type diesel engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25959790A JPH04136415A (en) | 1990-09-28 | 1990-09-28 | Auxiliary combustion chamber type diesel engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH04136415A true JPH04136415A (en) | 1992-05-11 |
Family
ID=17336315
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP25959790A Pending JPH04136415A (en) | 1990-09-28 | 1990-09-28 | Auxiliary combustion chamber type diesel engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH04136415A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2879658A1 (en) * | 2004-12-21 | 2006-06-23 | Renault Sas | Internal combustion engine e.g. diesel engine, for use in automobile field, has piston to control communication of main and auxiliary combustion chambers, where auxiliary chamber has its rate of compression higher than that of main chamber |
US10125666B2 (en) | 2016-01-14 | 2018-11-13 | Nautilus Engineering, Llc | Systems and methods of compression ignition engines |
US10927750B2 (en) | 2016-01-14 | 2021-02-23 | Nautilus Engineering, Llc | Systems and methods of compression ignition engines |
-
1990
- 1990-09-28 JP JP25959790A patent/JPH04136415A/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2879658A1 (en) * | 2004-12-21 | 2006-06-23 | Renault Sas | Internal combustion engine e.g. diesel engine, for use in automobile field, has piston to control communication of main and auxiliary combustion chambers, where auxiliary chamber has its rate of compression higher than that of main chamber |
US10125666B2 (en) | 2016-01-14 | 2018-11-13 | Nautilus Engineering, Llc | Systems and methods of compression ignition engines |
US10669926B2 (en) | 2016-01-14 | 2020-06-02 | Nautilus Engineering, Llc | Systems and methods of compression ignition engines |
US10927750B2 (en) | 2016-01-14 | 2021-02-23 | Nautilus Engineering, Llc | Systems and methods of compression ignition engines |
US11608773B2 (en) | 2016-01-14 | 2023-03-21 | Nautilus Engineering, Llc | Systems and methods of compression ignition engines |
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