Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPS6149494B2 - - Google Patents
[go: Go Back, main page]

JPS6149494B2 - - Google Patents

Info

Publication number
JPS6149494B2
JPS6149494B2 JP4589678A JP4589678A JPS6149494B2 JP S6149494 B2 JPS6149494 B2 JP S6149494B2 JP 4589678 A JP4589678 A JP 4589678A JP 4589678 A JP4589678 A JP 4589678A JP S6149494 B2 JPS6149494 B2 JP S6149494B2
Authority
JP
Japan
Prior art keywords
fuel
scavenging
passage
engine
combustion chamber
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
JP4589678A
Other languages
Japanese (ja)
Other versions
JPS54138914A (en
Inventor
Shigeru Oonishi
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.)
Nippon Clean Engine Laboratory Co
Original Assignee
Nippon Clean Engine Laboratory Co
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 Nippon Clean Engine Laboratory Co filed Critical Nippon Clean Engine Laboratory Co
Priority to JP4589678A priority Critical patent/JPS54138914A/en
Publication of JPS54138914A publication Critical patent/JPS54138914A/en
Publication of JPS6149494B2 publication Critical patent/JPS6149494B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Exhaust-Gas Circulating Devices (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Description

【発明の詳細な説明】 本発明は2サイクルデイーゼル機関に関する。[Detailed description of the invention] The present invention relates to a two-stroke diesel engine.

燃料消費率を大巾に向上でき、排気ガス中の有
害成分を大巾に低減でき、更に静粛な運転が得ら
れる2サイクルガソリン機関として、機関クラン
ク室と燃焼室とを連通する掃気通路の断面積をク
ランク室に近い側において絞ることにより燃焼室
内に新気を低速度で流入させて燃焼室内に活性熱
雰囲気を構成し、次いでこの雰囲気状態を圧縮行
程時中継続時に持続させて圧縮行程末期に新気が
点火栓によらず発火熱焼するようにした2サイク
ルガソリン機関が本発明者により既に提案されて
いる。
As a two-stroke gasoline engine, the fuel consumption rate can be greatly improved, harmful components in exhaust gas can be greatly reduced, and even quieter operation can be achieved. By narrowing the area on the side closer to the crank chamber, fresh air flows into the combustion chamber at a low speed to create an active thermal atmosphere within the combustion chamber, and this atmospheric state is then maintained during the compression stroke until the end of the compression stroke. The present inventor has already proposed a two-cycle gasoline engine in which fresh air is ignited and burned without using a spark plug.

本発明は2サイクルデイーゼル機関において上
述の如き活性熱雰囲気燃焼を行なわせ、それによ
つて燃料消費率を大巾に向上できると共に排気ガ
ス中の有害成分を大巾に低減でき、特にアイドル
ノツクの発生を阻止して静粛な運転が得られる2
サイクルデイーゼル機関を提供することにある。
The present invention performs active thermal atmosphere combustion as described above in a two-stroke diesel engine, thereby greatly improving the fuel consumption rate and greatly reducing harmful components in exhaust gas, especially the generation of idle knock. Silent operation can be achieved by preventing
Our goal is to provide cycle diesel engines.

以下、添付図面を参照して本発明を詳細に説明
する。
Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.

第1図並びに第2図に本発明をループ掃気式2
サイクルデイーゼル機関に適用した場合を示す。
無論本発明は排気弁を具えたユニフロー式2サイ
クルデイーゼル機関等の他の形式のデイーゼル機
関にも適用できることは云うまでもない。第1図
並びに第2図を参照すると、1はクランクケー
ス、2はクランクケース1上に固締されたシリン
ダブロツク、3はシリンダブロツク2上に固締さ
れたシリンダヘツド、4はほぼ平坦な頂面を有し
かつシリンダブロツク2内に嵌着されたシリンダ
ライナ5内で往復動可能なピストン、6はシリン
ダヘツド3とピストン4間に形成された燃焼室、
7は燃焼室6の頂点に配置された燃料噴射弁、8
はクランクケース1内に形成されたクランク室、
9はバランスウエイト、10は連接棒、11はシ
リンダライナ5に形成された複数個の掃気孔、1
2はシリンダライナ5に形成された複数個の排気
孔、13は排気通路、14は空気或いは燃料空気
混合気をクランク室8内に導入するための吸気通
路、15は吸気通路14からクランク室8内に向
けてのみ流通可能なリード弁、16は機関駆動の
燃料噴射ポンプを夫々示し、この燃料噴射ポンプ
16は燃料導管17を介して燃料噴射弁7に接続
される。なお、第1図に示すデイーゼル機関の圧
縮比は12から14の低い圧縮比に設定されている。
シリンダブロツク2とクランクケース1内には開
口18においてクランク室8内に開口する掃気通
路19が形成され、この掃気通路19は分岐した
掃気通路枝路20を介して掃気孔11に連結され
る。開口18近傍の掃気通路19内には掃気制御
弁21が配置され、この掃気制御弁21の弁軸2
2に固定されたアーム23の先端はワイヤ24を
介してアクセルペダル25に連結される。この掃
気制御弁21の開口量とアクセルペダル25の踏
込み量の関係は第3図において曲線Aで示され
る。なお第3図において縦軸Rは掃気制御弁21
の開口量を示し、一方横軸Lはアクセルペダル2
5の踏込み量、即ち負荷を示す。第3図から掃気
制御弁21は負荷が全負荷の40パーセント程度に
達するまで徐々に開弁し、それ以上負荷が高くな
ると全開することがわかる。第1図に示されるよ
うにエアフイルタ26下流の吸気通路14内には
燃料供給装置27が設けられる。第1図に示す実
施例ではこの燃料供給装置27はスモールベンチ
ユリ28内に開口する燃料噴出ノズル29と、こ
の燃料噴出ノズル29からフロート室(図示せ
ず)に通ずる燃料通路30内に設けられて燃料の
供給制御を行なう電磁弁31から構成される。こ
の電磁弁31のソレノイドはアクセルペダル25
の踏込み動作に応動するスイツチ32を介して電
源に接続される。第4図において縦軸Sはスイツ
チ32のオン・オフ動作を示し、横軸Lはアクセ
ルペダル25の踏込み量、即ち負荷を示す。第4
図から明らかなように負荷がL0以下の低負荷時
にはスイツチ32がオフ状態となり、このとき電
磁弁31は第1図に示すように燃料通路30を開
口する。従つてこのとき燃料が吸気通路14内に
供給され、斯くして燃料空気混合気がリード弁1
5を介してクランク室8内に送り込まれることに
なる。なお、この燃料としては軽油は無論のこと
ガソリンを使用することもでき、更に燃料供給量
は空燃比が15から20の範囲内になるように設定さ
れている。一方、機関負荷が負荷L0以上になる
とスイツチ32はオン状態となつて燃料通路30
は電磁弁31によつて遮断され、従つてこのとき
空気のみがクランク室8内に供給される。なお燃
料噴射弁7からは負荷の増大に伴なつて燃料噴射
量が徐々に増大するように常時燃料が噴射され、
更に燃料噴射弁7の燃料噴射時期は負荷の増大に
伴なつて徐々に進められるように設定されてい
る。
Figures 1 and 2 show the loop scavenging type 2 according to the present invention.
The case where it is applied to a cycle diesel engine is shown.
It goes without saying that the present invention can also be applied to other types of diesel engines, such as a uniflow two-stroke diesel engine equipped with an exhaust valve. Referring to FIGS. 1 and 2, 1 is a crankcase, 2 is a cylinder block fixed on the crankcase 1, 3 is a cylinder head fixed on the cylinder block 2, and 4 is a substantially flat top. A piston having a surface and capable of reciprocating within a cylinder liner 5 fitted in the cylinder block 2; 6 a combustion chamber formed between the cylinder head 3 and the piston 4;
7 is a fuel injection valve arranged at the apex of the combustion chamber 6;
is the crank chamber formed in the crankcase 1,
9 is a balance weight, 10 is a connecting rod, 11 is a plurality of scavenging holes formed in the cylinder liner 5, 1
2 is a plurality of exhaust holes formed in the cylinder liner 5; 13 is an exhaust passage; 14 is an intake passage for introducing air or a fuel-air mixture into the crank chamber 8; and 15 is a passage from the intake passage 14 to the crank chamber 8. The reed valves 16, which can only flow inward, each represent an engine-driven fuel injection pump, which is connected to the fuel injection valve 7 via a fuel conduit 17. The compression ratio of the diesel engine shown in FIG. 1 is set to a low compression ratio of 12 to 14.
A scavenging passage 19 opening into the crank chamber 8 at an opening 18 is formed in the cylinder block 2 and crankcase 1, and this scavenging passage 19 is connected to the scavenging hole 11 via a branched scavenging passage branch 20. A scavenging control valve 21 is arranged in the scavenging passage 19 near the opening 18, and the valve shaft 2 of this scavenging control valve 21
The tip of an arm 23 fixed to 2 is connected to an accelerator pedal 25 via a wire 24. The relationship between the opening amount of the scavenging control valve 21 and the depression amount of the accelerator pedal 25 is shown by curve A in FIG. In addition, in FIG. 3, the vertical axis R represents the scavenging control valve 21.
The horizontal axis L indicates the opening amount of the accelerator pedal 2.
It shows the amount of depression of No. 5, that is, the load. It can be seen from FIG. 3 that the scavenging control valve 21 gradually opens until the load reaches about 40% of the full load, and when the load increases beyond that, it opens fully. As shown in FIG. 1, a fuel supply device 27 is provided within the intake passage 14 downstream of the air filter 26. In the embodiment shown in FIG. 1, this fuel supply device 27 is provided with a fuel injection nozzle 29 opening in a small bench lily 28 and a fuel passage 30 leading from this fuel injection nozzle 29 to a float chamber (not shown). It is comprised of a solenoid valve 31 that controls the supply of fuel. The solenoid of this electromagnetic valve 31 is the accelerator pedal 25
It is connected to a power source via a switch 32 that responds to the depression of the switch. In FIG. 4, the vertical axis S shows the on/off operation of the switch 32, and the horizontal axis L shows the amount of depression of the accelerator pedal 25, that is, the load. Fourth
As is clear from the figure, when the load is low (lower than L0) , the switch 32 is turned off, and at this time the solenoid valve 31 opens the fuel passage 30 as shown in FIG. Therefore, at this time, fuel is supplied into the intake passage 14, and thus the fuel-air mixture is supplied to the reed valve 1.
5 into the crank chamber 8. Incidentally, not only light oil but also gasoline can be used as this fuel, and the amount of fuel supplied is set so that the air-fuel ratio is within the range of 15 to 20. On the other hand, when the engine load exceeds the load L0 , the switch 32 is turned on and the fuel passage 30 is turned on.
is shut off by the solenoid valve 31, so that only air is supplied into the crank chamber 8 at this time. Note that fuel is constantly injected from the fuel injection valve 7 so that the fuel injection amount gradually increases as the load increases.
Further, the fuel injection timing of the fuel injection valve 7 is set to be gradually advanced as the load increases.

掃気制御弁21がいくらか開弁しており、燃料
供給装置27から燃料が吸気通路14内に供給さ
れている低負荷運転時には、リード弁15を介し
てクランク室8内に導入された燃料空気混合気は
ピストン4の下降に伴なつて圧縮され、次いで開
口18を介して掃気通路19内に押込まれる。こ
のとき掃気制御弁21の絞り作用によつて掃気通
路19内を流れる燃料空気混合気は減速せしめら
れ、次いで燃料空気混合気は掃気通路枝路20を
介して掃気孔11から燃焼室6内に低速度で流入
する。また燃焼空気混合気が掃気制御弁21を通
過する際に燃料空気混合気内に乱れが発生するが
第1図に示すように掃気制御弁21を掃気孔11
から離れた位置、即ち開口18の近傍に設けるこ
とによつて燃料空気混合気流は掃気孔11に達す
る前に掃気通路19内で乱れが減衰せしめられ
る。上述したように燃焼室6内に流入する燃料空
気混合気流は低速度でありしかも乱れが減衰して
いるので燃料空気混合気が燃焼室6内に流入した
際に燃焼室6内における残留既燃ガスの流動はほ
とんど生ぜず、斯くして残留既燃ガスの熱の逸散
が阻止され、それにより残留既燃ガスは高温に保
持される。しかも燃焼室6内に流入した燃料空気
混合気はその周囲を高温の残留既燃ガスにより包
囲されたような形となる。特に低負荷運転時の圧
縮始めには燃焼室6内に多量の残留既燃ガスが存
在し、従つて燃料空気混合気は多量かつ高温の残
留既燃ガスにより包囲されるので燃料空気合気と
残留既燃ガスとの接触境界面の燃料は熱分解され
る。その結果、燃料空気混合気と残留既燃との接
触面の気相内にはOH・、CH・、C2・、H・等
の多量のラジカルを発生し、斯くして燃焼室6内
に活性熱雰囲気(このようなラジカルが多量に発
生している雰囲気を活性熱雰囲気という)が形成
される。圧縮行程時中燃焼室6内におけるガス流
動が非常に小さいので燃焼室壁面への熱エネルギ
損失が少なく、従つて燃焼室6内のガスは圧縮が
進むにつれて益々高温となり、その結果一層ラジ
カルが発生する。このように圧縮行程中に多量の
ラジカルが発生するが未だ燃焼室6内のガス温が
十分に高くならず、従つて急速に燃焼するには至
らない。次いで圧縮行程末期になつて燃焼室6内
のガス温が十分に高くなると自己着火して急速燃
焼に移行する。一方、圧縮行程末期に燃料噴射弁
7から噴射された燃料は雰囲気温度が高温に保持
されているために即座に気化してラジカルを発生
し、圧縮行程末期に熱炎を発して同様に自己着火
する。次いでピストン4が下降して排気孔12を
開口すると燃焼室6内の既燃ガスが排気通路13
内に排出される。
During low load operation when the scavenging control valve 21 is slightly open and fuel is being supplied into the intake passage 14 from the fuel supply device 27, the fuel-air mixture introduced into the crank chamber 8 via the reed valve 15. The air is compressed as the piston 4 descends, and then forced into the scavenging passage 19 through the opening 18. At this time, the fuel-air mixture flowing in the scavenging passage 19 is decelerated by the throttling action of the scavenging control valve 21, and then the fuel-air mixture flows from the scavenging hole 11 into the combustion chamber 6 via the scavenging passage branch 20. Inflow at low velocity. Further, when the combustion air mixture passes through the scavenging control valve 21, turbulence occurs in the fuel/air mixture; however, as shown in FIG.
By arranging the fuel-air mixture at a location remote from the opening 18, that is, in the vicinity of the opening 18, the turbulence of the fuel-air mixture is attenuated in the scavenging passage 19 before reaching the scavenging hole 11. As mentioned above, the fuel-air mixture flowing into the combustion chamber 6 has a low velocity and the turbulence is attenuated, so that when the fuel-air mixture flows into the combustion chamber 6, there is no residual burnt gas in the combustion chamber 6. Little gas flow occurs, thus preventing the dissipation of heat from the residual burnt gases, thereby keeping them at a high temperature. Moreover, the fuel-air mixture that has flowed into the combustion chamber 6 is surrounded by high-temperature residual burnt gas. Particularly at the beginning of compression during low-load operation, a large amount of residual burnt gas exists in the combustion chamber 6, and the fuel-air mixture is surrounded by a large amount of high-temperature residual burnt gas. The fuel at the contact interface with the residual burnt gas is thermally decomposed. As a result, a large amount of radicals such as OH・, CH・, C 2・, H・, etc. are generated in the gas phase at the contact surface between the fuel-air mixture and the residual burnt gas, and thus they are released into the combustion chamber 6. An activated thermal atmosphere (an atmosphere in which a large amount of radicals are generated is referred to as an active thermal atmosphere) is formed. During the compression stroke, the gas flow in the combustion chamber 6 is very small, so there is little thermal energy loss to the combustion chamber wall, and therefore the gas in the combustion chamber 6 becomes increasingly hot as compression progresses, and as a result, more radicals are generated. do. Although a large amount of radicals are thus generated during the compression stroke, the gas temperature within the combustion chamber 6 is still not high enough to cause rapid combustion. Then, at the end of the compression stroke, when the gas temperature in the combustion chamber 6 becomes sufficiently high, self-ignition occurs and rapid combustion occurs. On the other hand, since the ambient temperature is maintained at a high temperature, the fuel injected from the fuel injection valve 7 at the end of the compression stroke immediately vaporizes and generates radicals, which generates a hot flame and self-ignites at the end of the compression stroke. do. Next, when the piston 4 descends and opens the exhaust hole 12, the burned gas in the combustion chamber 6 flows into the exhaust passage 13.
discharged inside.

一方、掃気制御弁21が全開し、燃料供給装置
27からの燃料の供給が停止された高負荷運転時
は従来のデイーゼル機関と同様な圧縮着火が行な
われる。
On the other hand, during high-load operation when the scavenging control valve 21 is fully opened and the supply of fuel from the fuel supply device 27 is stopped, compression ignition is performed as in a conventional diesel engine.

前述したように燃焼室6内におけるラジカルの
発生を促進するには燃焼室6内の残留既燃ガスの
熱の逸散を阻止することにあり、このためには燃
焼室6内の残留既燃ガスの乱れ並びに流動を極め
て小さくする必要がある。このような乱れ並びに
流動を与える原因として更に排気孔12からの排
気ガスの急激な噴出並びに排気脈動干渉がある。
これらの排気ガスの急激な噴出並びに排気脈動干
渉を阻止するために第1図において破線で示すよ
うに排気制御弁34を排気通路13内に配設する
ことが好ましい。この排気制御弁34は図示しな
いリンク機構を介してアクセルペタル25に連結
され、第3図において破線Bに示されるように低
負荷運転から負荷が大きくなるにつれて徐々に開
弁し、掃気制御弁21が全開する前に排気制御弁
34は全開状態となる。
As mentioned above, in order to promote the generation of radicals in the combustion chamber 6, it is necessary to prevent the heat dissipation of the residual burned gas in the combustion chamber 6. Gas turbulence and flow must be kept extremely small. Further causes of such turbulence and flow include the rapid ejection of exhaust gas from the exhaust hole 12 and exhaust pulsation interference.
In order to prevent these sudden jets of exhaust gas and interference with exhaust pulsation, it is preferable to dispose an exhaust control valve 34 in the exhaust passage 13, as shown by the broken line in FIG. The exhaust control valve 34 is connected to the accelerator pedal 25 via a link mechanism (not shown), and gradually opens as the load increases from low-load operation, as shown by the broken line B in FIG. The exhaust control valve 34 is fully opened before the exhaust gas is fully opened.

一般的に云つて燃焼過程は次のように考えられ
ている。即ち、燃料が高温にさらされると燃料が
熱分解してラジカルとなる。このラジカルは激し
い活性を有し、ラジカル同士が反応して熱炎を発
生し、燃焼に移行する。従つて燃焼を生じさせる
ためには多量のラジカルを発生させることが必要
であるかあまり急速に多量のラジカルを発生させ
ると一気に燃焼するためにいわゆるデイーゼルノ
ツクを生ずる。しかしながら本発明の低負荷運転
時のように圧縮行程中の早い時期からラジカルを
発生させておくと圧縮行程中から既にラジカル同
志の反応が開始されており、従つてこのような状
態で燃料が噴射されると先に噴射された燃料から
順次燃焼が開始される。その結果、圧力上昇率が
低くなるためにデイーゼルノツクの発生が阻止さ
れる。
Generally speaking, the combustion process is considered as follows. That is, when the fuel is exposed to high temperatures, it thermally decomposes and becomes radicals. These radicals have intense activity, and the radicals react with each other to generate a hot flame, leading to combustion. Therefore, in order to cause combustion, it is necessary to generate a large amount of radicals, and if a large amount of radicals are generated too quickly, they will burn all at once, resulting in so-called diesel knock. However, if radicals are generated early in the compression stroke as in the case of low-load operation in the present invention, reactions between the radicals will have already started during the compression stroke, and therefore the fuel will not be injected in this state. When this happens, combustion starts sequentially starting from the fuel injected first. As a result, the rate of pressure rise is reduced, thereby preventing diesel knock from occurring.

以上述べたように本発明によれば圧縮行程中に
多量のラジカルを発生せしめることによつてアイ
ドルノツクの発生を阻止することができ、斯くし
て静粛な運転を行なうことができる。
As described above, according to the present invention, by generating a large amount of radicals during the compression stroke, generation of idle knock can be prevented, and quiet operation can thus be achieved.

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

第1図は本発明に係る2サイクルデイーゼル機
関の側面断面図、第2図は第1図の−線に沿
つてみた断面図、第3図は排気制御弁並びに掃気
制御弁の開度変化を示す線図、第4図は第1図の
スイツチの作動状態を示す図である。 5……燃焼室、7……燃料噴射弁、8……クラ
ンク室、11……掃気孔、12……排気孔、14
……吸気通路、19……掃気通路、21……掃気
制御弁、27……燃料供給装置。
Fig. 1 is a side sectional view of a two-stroke diesel engine according to the present invention, Fig. 2 is a sectional view taken along the - line in Fig. 1, and Fig. 3 shows changes in the opening degrees of the exhaust control valve and the scavenging control valve. The diagram shown in FIG. 4 is a diagram showing the operating state of the switch of FIG. 1. 5...Combustion chamber, 7...Fuel injection valve, 8...Crank chamber, 11...Scavenging hole, 12...Exhaust hole, 14
...Intake passage, 19...Scavenging passage, 21...Scavenging control valve, 27...Fuel supply device.

Claims (1)

【特許請求の範囲】[Claims] 1 掃気行程時に機関燃焼室とクランク室とを連
通する掃気通路を具備すると共にクランク室内に
空気を供給するための吸気通路を具備し、更に機
関燃焼室内に燃料を噴射するための燃料噴射弁を
具備した2サイクルデイーゼル機関において、機
関低負荷運転時に掃気通路を絞ると共に機関高負
荷運転時に掃気通路を全開する掃気制御弁をクラ
ンク室に近い側の掃気通路内に配置し、機関低負
荷運転時に吸気通路内に燃料を供給して燃料空気
混合気を掃気通路から燃焼室内に供給すると共に
機関高負荷運転時に吸気通路内への燃料の供給を
停止して空気のみを掃気通路から燃焼室内に供給
する燃料供給装置を具備し、機関負荷にかかわら
ずに上記燃料噴射弁から燃料を噴射するようにし
た2サイクルデイーゼル機関。
1 A scavenging passage that communicates the engine combustion chamber and the crank chamber during the scavenging stroke, an intake passage for supplying air into the crank chamber, and a fuel injection valve for injecting fuel into the engine combustion chamber. In the equipped two-stroke diesel engine, a scavenging control valve that throttles the scavenging passage when the engine is running at low load and fully opens the scavenging passage when the engine is running at high load is placed in the scavenging passage near the crankcase. Fuel is supplied into the intake passage and a fuel-air mixture is supplied from the scavenging passage into the combustion chamber, and when the engine is operating under high load, the fuel supply to the intake passage is stopped and only air is supplied from the scavenging passage into the combustion chamber. A two-stroke diesel engine equipped with a fuel supply device that injects fuel from the fuel injection valve regardless of the engine load.
JP4589678A 1978-04-20 1978-04-20 Fuel injection type active thermal atmospheric internal combustion engine Granted JPS54138914A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4589678A JPS54138914A (en) 1978-04-20 1978-04-20 Fuel injection type active thermal atmospheric internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4589678A JPS54138914A (en) 1978-04-20 1978-04-20 Fuel injection type active thermal atmospheric internal combustion engine

Publications (2)

Publication Number Publication Date
JPS54138914A JPS54138914A (en) 1979-10-27
JPS6149494B2 true JPS6149494B2 (en) 1986-10-29

Family

ID=12731997

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4589678A Granted JPS54138914A (en) 1978-04-20 1978-04-20 Fuel injection type active thermal atmospheric internal combustion engine

Country Status (1)

Country Link
JP (1) JPS54138914A (en)

Also Published As

Publication number Publication date
JPS54138914A (en) 1979-10-27

Similar Documents

Publication Publication Date Title
US6032617A (en) Dual fuel engine which ignites a homogeneous mixture of gaseous fuel, air, and pilot fuel
US4445468A (en) 2-Stroke internal combustion engine and an ignition-combustion method of an internal combustion engine
US4181100A (en) Internal combustion engine operated on injected fuel supplemented with hydrogen
RU2108471C1 (en) Internal combustion engine and method of its operation
US4079703A (en) Internal combustion engine operated on injected fuel supplemented with hydrogen
US4185598A (en) Internal combustion engine
US5027759A (en) Fuel injection and gasifying system for two-stroke engine
US5042442A (en) Internal combustion engine
JP2004522899A (en) Method for controlling injection of fluid into an internal combustion engine
JP4086440B2 (en) engine
CN118361337A (en) Hydrogen Engine
JP3379177B2 (en) Subchamber gas engine
US3967611A (en) Stratified-combustion type internal combustion engine with pre-combustion-chamber
JPS6149494B2 (en)
JPS5836183B2 (en) multi-cylinder internal combustion engine
TWI910774B (en) Engine with pre-combustion chamber ignition
JP2003254063A (en) Engine combustion chamber and engine combustion method
JP2000328974A (en) Diesel engine with EGR device
JPS6131287B2 (en)
JPS5851373Y2 (en) 2-stroke internal combustion engine
JPS6124526B2 (en)
JP3342483B2 (en) Two-stroke internal combustion engine
JPS62253920A (en) In-cylinder injection internal combustion engine
JPH03115725A (en) Fuel injection device for auxiliary chamber type insulated engine
TW202607222A (en) Engine with pre-combustion chamber ignition