JPH07293344A - Thermal insulation type gas engine - Google Patents

Thermal insulation type gas engine

Info

Publication number
JPH07293344A
JPH07293344A JP6112061A JP11206194A JPH07293344A JP H07293344 A JPH07293344 A JP H07293344A JP 6112061 A JP6112061 A JP 6112061A JP 11206194 A JP11206194 A JP 11206194A JP H07293344 A JPH07293344 A JP H07293344A
Authority
JP
Japan
Prior art keywords
chamber
sub
piston
gas engine
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.)
Pending
Application number
JP6112061A
Other languages
Japanese (ja)
Inventor
Kohei Yamaishi
興平 山石
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.)
Isuzu Ceramics Research Institute Co Ltd
Original Assignee
Isuzu Ceramics Research Institute Co 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 Isuzu Ceramics Research Institute Co Ltd filed Critical Isuzu Ceramics Research Institute Co Ltd
Priority to JP6112061A priority Critical patent/JPH07293344A/en
Publication of JPH07293344A publication Critical patent/JPH07293344A/en
Pending legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/30Use of alternative fuels, e.g. biofuels

Landscapes

  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

PURPOSE:To improve thermal efficiency by setting high compression ratio of an engine. CONSTITUTION:In a cylindrical housing arranged on a lower side of a cylinder head 20, an upper subsidiary-chamber 9 and a lower subsidiary-chamber 10 are determined by means of a partition wall 12, and fuel injection nozzle 4 is arranged in an intermediate peripheral wall of the upper subsidiary-chamber 9. A subsidiary-piston 7 which is moved vertically interlockingly with intake/ exhaust valves 18, 16 is arranged inside the upper subsidiary-chamber 9. An opening/closing valve 6a which opens and closes a valve hole 13 formed on the partition wall 12 is connected to a lower end of the subsidiary-piston 7. A plurality of injection holes 14 communicated with a main combustion of injection hole 14 communicated with a main combustion chamber 25 of a cylinder main body 22 are formed on a lower end peripheral wall of the lower subsidiary-chamber 10.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は燃料として天然ガスを圧
縮点火する遮熱型ガスエンジンに関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a heat shield type gas engine for compression ignition of natural gas as a fuel.

【0002】[0002]

【従来の技術】天然ガスを燃料とするガスエンジンはノ
ツキングなどの問題で圧縮比を11〜13と低めにしか
設定できない。天然ガスは燃焼速度が遅く燃焼状態が不
安定であるので熱効率が低い。……などの問題がある。
2. Description of the Related Art In a gas engine using natural gas as a fuel, the compression ratio can be set to a low value of 11 to 13 due to problems such as knocking. Since natural gas has a slow burning rate and an unstable burning state, its thermal efficiency is low. There are problems such as ......

【0003】[0003]

【発明が解決しようとする課題】本発明の目的は上述の
問題に鑑み、圧縮比をより高く設定し、熱効率を向上し
得る、遮熱型ガスエンジンを提供することにある。
SUMMARY OF THE INVENTION In view of the above problems, an object of the present invention is to provide a heat shield type gas engine which can set a higher compression ratio and improve thermal efficiency.

【0004】[0004]

【課題を解決するための手段】上記目的を達成するため
に、本発明の構成はシリンダヘツドの下部に備えた円筒
形のハウジングに、隔壁により上副室と下副室とを区画
し、上副室の中間周壁に燃料噴射ノズルを配設し、上副
室に吸排気弁に連動して上下動する副ピストンを嵌装
し、副ピストンの下端に前記隔壁に設けた弁孔を開閉す
る開閉弁を結合し、下副室の下端周壁にシリンダ本体の
主燃焼室へ連通する複数の噴孔を備えたものである。
In order to achieve the above object, the structure of the present invention has a cylindrical housing provided in the lower portion of a cylinder head, and an upper sub-chamber and a lower sub-chamber are defined by a partition wall. A fuel injection nozzle is arranged on the intermediate peripheral wall of the sub chamber, a sub piston that moves up and down in conjunction with the intake and exhaust valves is fitted in the upper sub chamber, and a valve hole provided in the partition wall is opened and closed at the lower end of the sub piston. An opening / closing valve is connected, and a plurality of injection holes communicating with the main combustion chamber of the cylinder body are provided on the lower peripheral wall of the lower auxiliary chamber.

【0005】[0005]

【作用】本発明によれば、天然ガスを主とするガス燃料
は吸気行程の終期に上副室へ噴射され、次いで副ピスト
ンが下降すると開閉弁が開き、上副室のガス燃料が弁孔
を経て下副室へ入り、吸気と混合しつつ着火し、圧縮行
程の終期に多数の噴孔から主燃焼室へ噴出する。
According to the present invention, the gas fuel mainly composed of natural gas is injected into the upper sub chamber at the end of the intake stroke, and then the opening / closing valve is opened when the sub piston is lowered, and the gas fuel in the upper sub chamber is opened. After entering the lower sub-chamber, it is ignited while being mixed with intake air, and ejected from a large number of injection holes to the main combustion chamber at the end of the compression stroke.

【0006】[0006]

【実施例】本発明によるガスエンジンはシリンダ本体2
2に主ピストン24を嵌装する一方、吸気通路17と排
気通路15を有するシリンダヘツド20を、ガスケツト
21を挟んでシリンダ本体22の上端に結合して構成さ
れる。図示の実施例では、シリンダヘツド20は各シリ
ンダに2つずつの吸気通路17と排気通路15を備えて
いる。主ピストン24の上端にはセラミツクスなどの耐
熱構造材からなる遮熱板23が結合される。各吸気ポー
ト17には下端の弁座17aに離接する吸気弁18が、
排気通路15には下端の弁座15aに離接する排気弁1
6がそれぞれ配設され、吸気弁18と排気弁16の各ス
テムは、シリンダヘツド20の上部に配した動弁機構
(図示せず)により開閉される。このような構成は普通
のデイーゼルエンジンとほぼ同様である。
EXAMPLE A gas engine according to the present invention is a cylinder body 2
The main piston 24 is fitted to the cylinder 2, and the cylinder head 20 having the intake passage 17 and the exhaust passage 15 is connected to the upper end of the cylinder body 22 with the gasket 21 interposed therebetween. In the illustrated embodiment, the cylinder head 20 has two intake passages 17 and two exhaust passages 15 for each cylinder. A heat shield plate 23 made of a heat resistant structural material such as ceramics is coupled to the upper end of the main piston 24. At each intake port 17, an intake valve 18 that is separated from and in contact with the valve seat 17a at the lower end,
In the exhaust passage 15, the exhaust valve 1 which is in contact with and separates from the valve seat 15a at the lower end.
6 are provided, and the stems of the intake valve 18 and the exhaust valve 16 are opened and closed by a valve mechanism (not shown) arranged above the cylinder head 20. Such a structure is almost the same as a normal diesel engine.

【0007】本発明によれば、シリンダヘツド20の下
面のほぼ軸心に円筒部19が形成され、円筒状のハウジ
ング8が円筒部19に嵌合支持される。ハウジング8は
隔壁12により上副室9と下副室10とを区画される。
上副室9に副ピストン7が嵌装され、副ピストン7に結
合したステム6が上方へ突出される。副ピストン7は低
摩擦セラミツクス製のシールリングを嵌装される。ステ
ム6の上端にコツタを介して結合したばね座2と、シリ
ンダヘツド20の上壁に配設したばね座5との間にばね
3が介装される。ステム6も上端部に図示してないタペ
ツトを結合され、動弁機構により吸気弁または排気弁を
駆動するカム機構により上下動される。副ピストン7の
下端に、隔壁12の円錐状の弁孔13を開閉する開閉弁
6aのステムが結合される。上副室9は上下中間の周壁
に燃料噴射ノズル4を配設される。燃料噴射ノズル4は
主ピストン24の往復動に関連してガス燃料を間歇的に
上副室9へ噴射する。ハウジング8の下端部は主燃焼室
25へ僅かに突出し、下副室10の下端周壁に斜め下方
へ延びる複数の噴孔14を備えられる。遮熱板23はハ
ウジング8の下端部と干渉しないようにくぼみ23aを
備えられる。
According to the present invention, the cylindrical portion 19 is formed on the lower surface of the cylinder head 20 substantially at the axial center, and the cylindrical housing 8 is fitted and supported by the cylindrical portion 19. The housing 8 is partitioned by a partition wall 12 into an upper sub chamber 9 and a lower sub chamber 10.
The sub piston 7 is fitted in the upper sub chamber 9, and the stem 6 coupled to the sub piston 7 is projected upward. The sub piston 7 is fitted with a seal ring made of low friction ceramics. A spring 3 is interposed between a spring seat 2 connected to the upper end of the stem 6 via a cotter and a spring seat 5 arranged on the upper wall of the cylinder head 20. A stem (not shown) is also coupled to the upper end of the stem 6, and is vertically moved by a cam mechanism that drives an intake valve or an exhaust valve by a valve mechanism. A stem of an on-off valve 6 a that opens and closes the conical valve hole 13 of the partition wall 12 is coupled to the lower end of the sub piston 7. The fuel injection nozzle 4 is disposed on the peripheral wall between the upper sub chamber 9 and the upper and lower intermediate chambers. The fuel injection nozzle 4 intermittently injects the gas fuel into the upper sub chamber 9 in association with the reciprocating movement of the main piston 24. The lower end of the housing 8 slightly protrudes into the main combustion chamber 25, and a plurality of injection holes 14 extending obliquely downward are provided in the lower end peripheral wall of the lower auxiliary chamber 10. The heat shield plate 23 is provided with a recess 23a so as not to interfere with the lower end of the housing 8.

【0008】図3に示すように、噴孔14の向きは平面
的にみて接線方向に延びており、下副室10のガス燃料
が主燃焼室25へ噴出する時、渦流を形成するように構
成される。ガス燃料の高圧縮比による大なる熱負荷に耐
えるよう、主ピストン24の冠部、副室9,10、開閉
弁6aはセラミツクスなどの耐熱構造材により構成され
る。
As shown in FIG. 3, the directions of the injection holes 14 extend in a tangential direction when seen in a plan view, and when the gas fuel in the lower sub chamber 10 is ejected into the main combustion chamber 25, a swirl flow is formed. Composed. In order to withstand a large heat load due to the high compression ratio of the gas fuel, the crown portion of the main piston 24, the auxiliary chambers 9 and 10, and the on-off valve 6a are made of a heat resistant structural material such as ceramics.

【0009】次に、本発明による遮熱型ガスエンジンの
作動について説明する。下副室10を高温にし、ガス燃
料を圧縮行程の終期(上死点)付近で確実に着火させる
ために、圧縮比は17〜18に設定される。図4に示す
ように、開閉弁6aは主ピストン24の圧縮行程の終期
(上死点)付近から吸気行程の始期(上死点)付近まで
開き、吸気行程の終期(下死点)では閉じている。
Next, the operation of the heat shield type gas engine according to the present invention will be described. The compression ratio is set to 17 to 18 in order to raise the temperature of the lower sub chamber 10 and surely ignite the gas fuel near the end of the compression stroke (top dead center). As shown in FIG. 4, the on-off valve 6a opens from near the end of the compression stroke of the main piston 24 (top dead center) to near the beginning of the intake stroke (top dead center), and closes at the end of the intake stroke (bottom dead center). ing.

【0010】吸気行程の終期(下死点)で燃料噴射ノズ
ル4から上副室9へガス燃料の噴射が始まる。圧縮行程
で主ピストン24が上昇し始めると、下副室10の温度
が高くなるが、上副室9のガス燃料は過濃であるので着
火できない状態にある。主ピストン24が圧縮行程の終
期(上死点)付近に達すると、主燃焼室25と下副室1
0の温度は高くなり、また、開閉弁6aが開き、上副室
9のガス燃料が下副室10へ流入し、高温・高圧の吸気
と混合する。下副室10の混合気は着火可能な空気過剰
率になり着火する。開閉弁6aが開くと同時に副ピスト
ン7が下降し、上副室9のガス燃料を弁孔13を経て下
副室10へ押し出す。下副室10の濃い混合気は噴孔1
4を経て主燃焼室25へ噴出し、下副室10に残る未燃
ガスは僅かなものになる。混合気は噴孔14から主燃焼
室25へ接線方向ないし周方向に吹き出すので、吸気と
の混合が促進され、短時間の内に燃焼を完結する。
At the end of the intake stroke (bottom dead center), injection of gas fuel from the fuel injection nozzle 4 into the upper sub chamber 9 starts. When the main piston 24 starts to rise in the compression stroke, the temperature of the lower sub chamber 10 rises, but the gas fuel in the upper sub chamber 9 is too rich to ignite. When the main piston 24 reaches the end of the compression stroke (top dead center), the main combustion chamber 25 and the lower sub chamber 1
The temperature of 0 rises, the on-off valve 6a opens, and the gas fuel in the upper subchamber 9 flows into the lower subchamber 10 and mixes with the high temperature, high pressure intake air. The air-fuel mixture in the lower sub-chamber 10 is ignited with an excess air ratio capable of being ignited. At the same time as the opening / closing valve 6a is opened, the sub piston 7 descends, and the gas fuel in the upper sub chamber 9 is pushed out to the lower sub chamber 10 through the valve hole 13. The dense mixture in the lower sub-chamber 10 is the injection hole 1
The amount of unburned gas that is ejected into the main combustion chamber 25 via 4 and remains in the lower sub chamber 10 becomes small. Since the air-fuel mixture blows out from the injection hole 14 to the main combustion chamber 25 in the tangential direction or the circumferential direction, mixing with the intake air is promoted, and combustion is completed within a short time.

【0011】図2に示すように、副ピストン7の下降に
伴い、燃料噴射ノズル4は副ピストン7の上側に位置す
るので、燃料噴射ノズル4が火炎に曝される時間は短
く、熱負荷も小さい。
As shown in FIG. 2, as the auxiliary piston 7 descends, the fuel injection nozzle 4 is positioned above the auxiliary piston 7, so that the fuel injection nozzle 4 is exposed to the flame for a short period of time and also has a heat load. small.

【0012】[0012]

【発明の効果】本発明は上述のように、シリンダヘツド
の下部に備えた円筒形のハウジングに、隔壁により上副
室と下副室とを区画し、上副室の中間周壁に燃料噴射ノ
ズルを配設し、上副室に吸排気弁に連動して上下動する
副ピストンを嵌装し、副ピストンの下端に前記隔壁に設
けた弁孔を開閉する開閉弁を結合し、下副室の下端周壁
にシリンダ本体の主燃焼室へ連通する複数の噴孔を備え
たものであり、圧縮行程の終期に少量の吸気が下副室へ
充填され、上副室のガス燃料が副ピストンにより下副室
へ供給されて燃焼を開始し、下副室のガス燃料が複数の
噴孔から主燃焼室へ供給されるので、圧縮比を17〜1
8と高く設定することができ、エンジンの熱効率を向上
できる。
As described above, according to the present invention, the upper sub-chamber and the lower sub-chamber are partitioned by the partition wall in the cylindrical housing provided in the lower portion of the cylinder head, and the fuel injection nozzle is provided on the intermediate peripheral wall of the upper sub-chamber. A sub-piston that moves up and down in conjunction with the intake and exhaust valves is fitted in the upper sub-chamber, and an opening / closing valve that opens and closes a valve hole provided in the partition wall is connected to the lower end of the sub-piston to form a lower sub-chamber. The lower peripheral wall of the cylinder is equipped with multiple injection holes that communicate with the main combustion chamber of the cylinder body.At the end of the compression stroke, a small amount of intake air is filled into the lower sub chamber, and the gas fuel in the upper sub chamber is charged by the sub piston. Since it is supplied to the lower sub chamber to start combustion and the gas fuel in the lower sub chamber is supplied to the main combustion chamber from the plurality of injection holes, the compression ratio is 17 to 1
It can be set as high as 8, and the thermal efficiency of the engine can be improved.

【0013】下副室の噴孔の向きを接線方向にしたこと
により、主燃焼室に強い旋回流が生じ、吸気とガス燃料
とが均一に混合されかつ稀薄な状態で非常に良好な燃焼
が得られ、排ガス成分に問題がない。
By making the injection holes of the lower auxiliary chamber tangential to each other, a strong swirling flow is generated in the main combustion chamber, and the intake air and the gas fuel are uniformly mixed and very good combustion is achieved in a lean state. There is no problem with the exhaust gas component obtained.

【0014】上副室のガス燃料は副ピストンにより下副
室へ押し出されるので、ガス燃料は下副室の吸気と混合
しながら主燃焼室へ噴出され、噴孔の向きが接線方向に
なつているので、混合気の噴出エネルギが有効に利用さ
れ、短期間のうちに火炎が主燃焼室へ広がる結果、主燃
焼室での燃焼期間が短く熱効率が向上する。
Since the gas fuel in the upper sub-chamber is pushed out to the lower sub-chamber by the sub-piston, the gas fuel is jetted into the main combustion chamber while being mixed with the intake air in the lower sub-chamber, and the direction of the injection holes is tangential. Therefore, the jetting energy of the air-fuel mixture is effectively used and the flame spreads to the main combustion chamber within a short period of time, resulting in a shorter combustion period in the main combustion chamber and improved thermal efficiency.

【0015】燃料噴射ノズルはガス燃料の着火と同時に
副ピストンの上側に位置するので、燃料噴射ノズルの熱
負荷が軽減される。
Since the fuel injection nozzle is located above the auxiliary piston at the same time as the gas fuel is ignited, the heat load on the fuel injection nozzle is reduced.

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

【図1】本発明に係る遮熱型ガスエンジンの主要部を示
す正面断面図である。
FIG. 1 is a front sectional view showing a main part of a heat shield type gas engine according to the present invention.

【図2】同ガスエンジンにおける副ピストンの下降状態
を示す正面断面図である。
FIG. 2 is a front sectional view showing a lowered state of a sub piston in the gas engine.

【図3】図1の線3A−3Aによる下半部を省略して示
す底面断面図である。
FIG. 3 is a bottom cross-sectional view showing the lower half portion of FIG. 1 taken along the line 3A-3A.

【図4】遮熱型ガスエンジンの行程を表す線図である。FIG. 4 is a diagram showing a stroke of a heat shield type gas engine.

【符号の説明】[Explanation of symbols]

4:燃料噴射ノズル 6a:開閉弁 7:副ピストン
8:ハウジング 9:上副室 10:下副室 12:隔
壁 13:弁孔 14:噴孔 16:排気弁 18:吸
気弁 20:シリンダヘツド 22:シリンダ本体 2
4:主ピストン 25:主燃焼室
4: Fuel injection nozzle 6a: Open / close valve 7: Sub piston
8: Housing 9: Upper sub chamber 10: Lower sub chamber 12: Partition wall 13: Valve hole 14: Injection hole 16: Exhaust valve 18: Intake valve 20: Cylinder head 22: Cylinder body 2
4: Main piston 25: Main combustion chamber

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】シリンダヘツドの下部に備えた円筒形のハ
ウジングに、隔壁により上副室と下副室とを区画し、上
副室の中間周壁に燃料噴射ノズルを配設し、上副室に吸
排気弁に連動して上下動する副ピストンを嵌装し、副ピ
ストンの下端に前記隔壁に設けた弁孔を開閉する開閉弁
を結合し、下副室の下端周壁にシリンダ本体の主燃焼室
へ連通する複数の噴孔を備えたことを特徴とする、遮熱
型ガスエンジン。
1. A cylindrical housing provided in the lower part of a cylinder head, which divides an upper sub chamber and a lower sub chamber by a partition wall, and a fuel injection nozzle is arranged on an intermediate peripheral wall of the upper sub chamber. A sub-piston that moves up and down in conjunction with the intake and exhaust valves is fitted to the bottom of the sub-chamber, and an opening / closing valve that opens and closes a valve hole is connected to the lower end of the sub-piston. A heat shield type gas engine having a plurality of injection holes communicating with the combustion chamber.
【請求項2】前記複数の噴孔は下副室の下端周壁に周方
向等間隔に配設され、かつ噴孔の向きは接線方向であ
る、請求項1に記載の遮熱型ガスエンジン。
2. The heat shield type gas engine according to claim 1, wherein the plurality of injection holes are arranged at equal intervals in the circumferential direction on the lower peripheral wall of the lower sub chamber, and the directions of the injection holes are tangential.
【請求項3】前記ハウジングと主ピストンの冠部は耐熱
構造材により構成されている、請求項1に記載の遮熱型
ガスエンジン。
3. The heat shield type gas engine according to claim 1, wherein the housing and the crown portion of the main piston are made of a heat resistant structural material.
【請求項4】前記上副室に嵌装した副ピストンは上方へ
突出するステムを、吸排気弁と同期して副ピストンを上
下動させる動弁機構に係合される、請求項1に記載の遮
熱型ガスエンジン。
4. The auxiliary piston fitted in the upper auxiliary chamber has a stem protruding upwardly engaged with a valve mechanism for moving the auxiliary piston up and down in synchronization with an intake / exhaust valve. Heat shield type gas engine.
JP6112061A 1994-04-27 1994-04-27 Thermal insulation type gas engine Pending JPH07293344A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6112061A JPH07293344A (en) 1994-04-27 1994-04-27 Thermal insulation type gas engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6112061A JPH07293344A (en) 1994-04-27 1994-04-27 Thermal insulation type gas engine

Publications (1)

Publication Number Publication Date
JPH07293344A true JPH07293344A (en) 1995-11-07

Family

ID=14577071

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6112061A Pending JPH07293344A (en) 1994-04-27 1994-04-27 Thermal insulation type gas engine

Country Status (1)

Country Link
JP (1) JPH07293344A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0971106A2 (en) * 1998-07-08 2000-01-12 Isuzu Ceramics Research Institute Co., Ltd. Prechamber gas-combustion engine with gaseous fuel compressor
JP2003286849A (en) * 2002-03-29 2003-10-10 Mitsubishi Heavy Ind Ltd Gas engine with sub-chamber
KR101459955B1 (en) * 2013-10-11 2014-11-10 현대자동차주식회사 Apparatus for jet ignition
US10202891B2 (en) 2012-09-20 2019-02-12 Mitsubishi Heavy Industries, Ltd. Precombustion chamber gas engine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0971106A2 (en) * 1998-07-08 2000-01-12 Isuzu Ceramics Research Institute Co., Ltd. Prechamber gas-combustion engine with gaseous fuel compressor
EP0971106A3 (en) * 1998-07-08 2000-08-23 Isuzu Ceramics Research Institute Co., Ltd. Prechamber gas-combustion engine with gaseous fuel compressor
JP2003286849A (en) * 2002-03-29 2003-10-10 Mitsubishi Heavy Ind Ltd Gas engine with sub-chamber
US10202891B2 (en) 2012-09-20 2019-02-12 Mitsubishi Heavy Industries, Ltd. Precombustion chamber gas engine
KR101459955B1 (en) * 2013-10-11 2014-11-10 현대자동차주식회사 Apparatus for jet ignition

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