JP3387185B2 - Combustion chamber with subchamber - Google Patents

Combustion chamber with subchamber

Info

Publication number
JP3387185B2
JP3387185B2 JP33920293A JP33920293A JP3387185B2 JP 3387185 B2 JP3387185 B2 JP 3387185B2 JP 33920293 A JP33920293 A JP 33920293A JP 33920293 A JP33920293 A JP 33920293A JP 3387185 B2 JP3387185 B2 JP 3387185B2
Authority
JP
Japan
Prior art keywords
chamber
sub
combustion chamber
main
main combustion
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 - Fee Related
Application number
JP33920293A
Other languages
Japanese (ja)
Other versions
JPH07158451A (en
Inventor
英男 河村
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 Motors Ltd
Original Assignee
Isuzu Motors 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 Motors Ltd filed Critical Isuzu Motors Ltd
Priority to JP33920293A priority Critical patent/JP3387185B2/en
Priority to US08/340,868 priority patent/US5515823A/en
Priority to DE69411683T priority patent/DE69411683T2/en
Priority to EP94308549A priority patent/EP0657635B1/en
Priority to DE0657635T priority patent/DE657635T1/en
Publication of JPH07158451A publication Critical patent/JPH07158451A/en
Application granted granted Critical
Publication of JP3387185B2 publication Critical patent/JP3387185B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/08Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • F02B23/10Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder
    • F02B23/104Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder the injector being placed on a side position of the cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/24Cylinder heads
    • F02F2001/244Arrangement of valve stems in cylinder heads
    • F02F2001/247Arrangement of valve stems in cylinder heads the valve stems being orientated in parallel with the cylinder axis
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)

Description

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

【0001】[0001]

【発明の属する技術分野】この発明は,ピストン側に副
室を備えた燃焼室に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combustion chamber having a sub chamber on the piston side.

【0002】[0002]

【従来の技術】従来,エンジンの燃焼改善を目的として
渦流室を持つ渦流室式エンジンが開発されている。この
ような渦流室式エンジンは,シリンダヘッド又はピスト
ンヘッドに形成した渦流室,該渦流室とシリンダ側に形
成した主室とを連通する連絡孔,及び渦流室内に燃料を
噴霧する燃料噴射ノズルを有する。上記渦流室式エンジ
ンは,連絡孔を通じて渦流室に流入する渦流と渦流室内
に噴射された燃料とで混合気を形成させ,該混合気を一
次燃焼させ,次いで渦流室から連絡孔を通じて主室へ火
炎,未燃混合気等のガスを噴出させて二次燃焼させてい
る。このような渦流室式エンジンの一例としては,特開
平2−112613号公報に開示された副燃焼室の構造
が知られている。
2. Description of the Related Art Conventionally, a swirl chamber type engine having a swirl chamber has been developed for the purpose of improving combustion of the engine. Such a swirl chamber engine has a swirl chamber formed in a cylinder head or a piston head, a communication hole for communicating the swirl chamber with a main chamber formed on the cylinder side, and a fuel injection nozzle for spraying fuel into the swirl chamber. Have. In the above swirl chamber type engine, an air-fuel mixture is formed by a swirl flow flowing into the swirl chamber through a communication hole and a fuel injected into the swirl chamber, the air-fuel mixture is primarily burned, and then the swirl chamber is passed through the communication hole to a main chamber. Gas such as flame and unburned mixture is ejected for secondary combustion. As an example of such a swirl chamber type engine, the structure of the auxiliary combustion chamber disclosed in Japanese Patent Laid-Open No. 2-112613 is known.

【0003】また,実開昭62−93141号公報に
は,セラミッククラウンとアルミスカートから成るピス
トンが開示されている。該ピストンは,キャビティを形
成したセラミッククラウンの外周を筒体状のアルミスカ
ートのヘッド部を嵌合し,燃焼室外周とヘッド部との間
隙に鋳鉄製リングを塑性流動材と共存させ,両者を固定
したものである。
Further, Japanese Utility Model Publication No. 62-93141 discloses a piston having a ceramic crown and an aluminum skirt. In this piston, the outer periphery of a ceramic crown having a cavity is fitted with the head portion of a cylindrical aluminum skirt, and a cast iron ring is made to coexist with a plastic fluid material in the gap between the outer periphery of the combustion chamber and the head portion. It is fixed.

【0004】また,特開平5−26111号公報には,
断熱ピストンが開示されている。該断熱ピストンは,ピ
ストンヘッドとピストンスカートとの間の断熱製を確保
し,両者の結合部に配置した断熱部材の割れ等の発生を
防止し,断熱部材の飛散を防止したものである。
Further, in Japanese Patent Laid-Open No. 5-26111,
Adiabatic pistons are disclosed. The heat insulating piston secures heat insulation between the piston head and the piston skirt, prevents cracks and the like of the heat insulating member arranged at the joint between the two, and prevents scattering of the heat insulating member.

【0005】[0005]

【発明が解決しようとする課題】一般に,副室での燃焼
温度は,高温であるため,NOX の生成を低減する対策
としては,燃料リッチで燃焼させることが効果的であ
る。また,燃焼温度が高温である時に,燃料リッチで燃
焼させるには,エンジン構造のタイプとしては副室式エ
ンジンで対応することが有効である。従来通りのエンジ
ンを副室式燃焼室を用いた場合に,副室式燃焼室の燃焼
スピードを速くするには,副室と主室とを連通する連通
孔の通路断面積を絞り,渦流を速め,主室への噴流速度
を大きくすることが必要である。ところが,副室式燃焼
室は,連通孔の通路断面積を小さくすると,副室から主
室へ流出する噴出スピードが大きくなるが,絞り損失が
大きくなり,また,主室での燃焼が十分に行われないと
いう問題がある。
To the 0005] Generally, the combustion temperature in the secondary chamber are the high temperature, as a measure to reduce the production of NO X, it is effective to combust the fuel-rich. Also, in order to burn fuel-rich when the combustion temperature is high, it is effective to use a sub-chamber engine as the type of engine structure. When the conventional engine uses a sub-chamber combustion chamber, in order to increase the combustion speed of the sub-chamber combustion chamber, the passage cross-sectional area of the communication hole that connects the sub-chamber with the main chamber is reduced to reduce the vortex flow. It is necessary to speed up and increase the jet velocity to the main chamber. However, in the sub-chamber type combustion chamber, when the passage cross-sectional area of the communication hole is made small, the jet speed flowing out from the sub-chamber to the main chamber becomes large, but the throttling loss becomes large and the combustion in the main chamber becomes sufficient. There is a problem that it is not done.

【0006】主燃焼室と副室とを連通する連絡孔をシリ
ンダ周辺部に設けた従来形エンジンの場合には,絞り損
失を減らすため,連絡孔の通路面積を大きくすると,副
室から主燃焼室へ噴出する火炎,未燃混合気等のガスの
貫徹力が小さくなり,シリンダの中心部にまで到達でき
ない状態が発生する。エンジンの熱効率を向上させるた
めには,主燃焼室での空気利用率を向上させて短期に燃
焼を完結し,白煙の発生を防止することが重要である。
In the case of a conventional engine in which a communication hole that connects the main combustion chamber and the sub chamber is provided in the peripheral portion of the cylinder, if the passage area of the communication hole is increased in order to reduce the throttling loss, the main combustion from the sub chamber will occur. The penetrating force of flames, unburned air-fuel mixture, and other gases ejected into the chamber becomes small, and the state where the central part of the cylinder cannot be reached occurs. In order to improve the thermal efficiency of the engine, it is important to improve the air utilization rate in the main combustion chamber to complete combustion in a short time and prevent the generation of white smoke.

【0007】また,従来形の渦流室式エンジンでは,上
記不具合を解決するため副室と主室とを連通する連絡孔
が小さいので,該連絡口による絞り損失が発生し,エン
ジン出力を低減する原因になる。また,一般に,主室と
副室とを連通する連絡孔は,直噴式ではリエントラント
式と言われ,シリンダ中心部に副室式では外周部に1つ
設けられているので,噴流の到達しなければならない距
離が長くなり,主室での空気との混合が不十分になり,
HC,スモークの発生原因になる。
Further, in the conventional swirl chamber type engine, in order to solve the above-mentioned problems, the communication hole that communicates the sub chamber and the main chamber is small, so throttling loss occurs due to the communication port and the engine output is reduced. Cause. Generally, the direct injection type has a communication hole that connects the main chamber and the sub-chamber to the reentrant type, and one is provided in the center of the cylinder on the outer periphery of the sub-chamber type, so the jet flow must reach. The distance that has to be extended becomes longer, the mixing with the air in the main room becomes insufficient,
It causes HC and smoke.

【0008】この発明の目的は,上記の課題を解決する
ことであり,ピストンスカートに固定したピストンヘッ
ドに副室を構成し,シリンダヘッドの下面部にキャビテ
ィを形成し,主燃焼室の形状と主燃焼室と副室とを連通
する連絡孔を最適構造に構成することによって,副室か
ら主燃焼室への火炎,未燃混合気等のガスの主燃焼室で
の貫徹力を向上させると共に,主燃焼室に存在する吸気
スワールを利用して副室から主燃焼室への火炎,未燃混
合気等のガスの主燃焼室での空気利用率を向上させ,主
燃焼室に存在する新気との混合を促進し,燃焼スピード
をアップし,燃焼期間を短縮して燃焼を短期に完結し,
熱効率を向上させ,NOX ,カーボン,スモーク等の発
生を低減する副室を備えた燃焼室を提供することであ
る。
An object of the present invention is to solve the above-mentioned problems. A sub-chamber is formed in a piston head fixed to a piston skirt, a cavity is formed in the lower surface of the cylinder head, and the shape of the main combustion chamber is By constructing the communication hole that connects the main combustion chamber and the sub chamber with an optimum structure, the penetration force of the flame from the sub chamber to the main combustion chamber and the gas such as unburned mixture in the main combustion chamber is improved. , The intake air swirl existing in the main combustion chamber is used to improve the air utilization rate in the main combustion chamber of gases such as flames from the sub chamber to the main combustion chamber and unburned air-fuel mixture. Promotes mixing with air, increases combustion speed, shortens combustion period, and completes combustion in a short period of time.
Improve thermal efficiency is to provide a combustion chamber with a sub-chamber to reduce NO X, carbon, generation of smoke and the like.

【0009】[0009]

【課題を解決するための手段】この発明は,シリンダヘ
ッド下面から突出するように配置された燃料噴射ノズ
ル,該燃料噴射ノズルの回りでシリンダヘッドの下面部
に形成されている複数のキャビティによって構成される
主燃焼室,ピストンヘッドのほぼ中央部に設けた副室,
前記ピストンヘッドのほぼ中央に形成され且つ上死点近
傍で前記燃料噴射ノズルの突入によって閉鎖される前記
主燃焼室と前記副室とを連通する主連絡孔,前記主連絡
孔の回りで前記キャビティに向かって且つシリンダ外側
から内側に傾斜して前記ピストンヘッドに形成され且つ
前記主燃焼室と前記副室とを連通する複数の副連絡孔,
及び前記燃料噴射ノズルに設けられた前記副室内に燃料
を噴射する多噴孔を有し,前記副連絡孔の形成方向は前
記副室中心から偏心して形成され,前記副室から前記副
連絡孔を通じて前記キャビティに向かって噴出する火炎
旋回流は前記主燃焼室に存在する吸気スワールに複合さ
れることを特徴とする副室を備えた燃焼室に関する。
The present invention comprises a fuel injection nozzle arranged so as to project from the lower surface of a cylinder head, and a plurality of cavities formed in the lower surface of the cylinder head around the fuel injection nozzle. The main combustion chamber, the sub-chamber provided almost at the center of the piston head,
A main communication hole, which is formed substantially in the center of the piston head and which is closed by the thrust of the fuel injection nozzle near the top dead center, connects the main combustion chamber and the sub chamber, and the cavity around the main communication hole. A plurality of sub-communication holes that are formed in the piston head and incline inward from the cylinder outer side to the inner side and that communicate the main combustion chamber and the sub chamber with each other,
And a multi-injection hole for injecting fuel into the sub-chamber provided in the fuel injection nozzle.
It is formed eccentrically from the center of the sub chamber,
Flames ejected toward the cavity through the communication hole
The swirl flow is combined with the intake swirl existing in the main combustion chamber.
And a combustion chamber provided with a sub chamber.

【0010】また,前記キャビティは,前記シリンダヘ
ッドに配置したバルブ逃げ部又は該バルブ逃げ部以外の
領域に形成されているものである。
Further, the cavity is formed in the valve relief portion arranged in the cylinder head or in an area other than the valve relief portion.

【0011】また,この発明は,シリンダヘッド下面か
ら突出するように配置された燃料噴射ノズル,該燃料噴
射ノズルの回りでシリンダヘッドの下面部に形成されて
いる複数のキャビティによって構成される主燃焼室,ピ
ストンヘッドのほぼ中央部に設けた副室,前記ピストン
ヘッドのほぼ中央に形成され且つ上死点近傍で前記燃料
噴射ノズルの突入によって閉鎖される前記主燃焼室と前
記副室とを連通する主連絡孔,前記主連絡孔の回りで前
記キャビティに向かって且つシリンダ外側から内側に傾
斜して前記ピストンヘッドに形成され且つ前記主燃焼室
と前記副室とを連通する複数の副連絡孔,及び前記燃料
噴射ノズルに設けられた前記副室内に燃 料を噴射する多
噴孔を有し,前記キャビティには,前記副室から前記副
連絡孔を通じて前記主燃焼室へ噴出する火炎旋回流れの
周方向に拡大した火炎逃げ部が形成されていることを特
徴とする副室を備えた燃焼室に関する。
Further, the present invention is not limited to the bottom surface of the cylinder head.
Fuel injection nozzle arranged so as to project from the
Formed on the lower surface of the cylinder head around the injection nozzle
The main combustion chamber composed of multiple cavities
Sub-chamber provided almost at the center of the stone head, the piston
The fuel is formed near the center of the head and near the top dead center.
In front of the main combustion chamber closed by the injection of the injection nozzle
Main communication hole that communicates with the auxiliary chamber, around the main communication hole
Tilt toward the cavity and from the outside to the inside of the cylinder
The main combustion chamber is formed obliquely on the piston head and
And a plurality of sub-communication holes communicating between the sub-chamber and the fuel, and the fuel.
Multi for injecting fuel into the auxiliary combustion chamber provided in the injection nozzle
Has a nozzle hole, the cavity, especially in that the flame relief portion which is enlarged in the circumferential direction of the flame swirl flow ejected into the main combustion chamber from the sub-chamber through the sub communication holes are formed
The present invention relates to a combustion chamber provided with a sub chamber for collection.

【0012】この副室を備えた燃焼室は,上記のように
構成されているので,副室から副連絡孔を通じて主燃焼
室へ噴出する火炎,未燃混合気等のガスはキャビティへ
火炎ジェット旋回流となって前記主燃焼室に存在する吸
気スワールと複合して混合燃焼が促進される。
Since the combustion chamber provided with this sub-chamber is configured as described above, flames, unburned air-fuel mixture, and other gases ejected from the sub-chamber to the main combustion chamber through the sub-communication holes are jetted to the cavity. It becomes a swirling flow and is mixed with the intake swirl existing in the main combustion chamber to promote mixed combustion.

【0013】また,前記副室はピストン中央に位置し,
前記副連絡孔がシリンダ周辺に延びているので,前記副
連絡孔は,前記主連絡孔の回りに均等な間隔に隔置して
放射方向に複数形成され,前記副室から前記主燃焼室へ
の火炎,未燃混合気等のガスがシリンダ周辺に向かって
前記キャビティへ噴射されるように構成される。しか
も,前記副連絡孔を前記主連絡孔の回りに設けることに
よって,前記副室から前記主燃焼室へ噴き出される火
炎,未燃混合気等のガスのシリンダ周辺までの到達距離
が均等に短くなり,シリンダ周辺への到達時間が短縮さ
れると共に,速度を圧力に変換して短期にシリンダ周辺
に到達でき,前記主燃焼室に存在する新気との混合が短
期に行われ,燃焼を促進して短期に完結させることがで
きる。また,前記副連絡孔を複数個形成して連絡孔通路
面積を全体で大きく形成できるので,しぼり損を低減で
きる。
The sub chamber is located at the center of the piston,
Since the sub-communication holes extend around the cylinder, the sub-communication holes are radially formed at equal intervals around the main communication hole so as to extend from the sub-chamber to the main combustion chamber. The flame, the unburned air-fuel mixture, and other gases are injected into the cavity toward the cylinder periphery. Moreover, by providing the sub-communication hole around the main communication hole, the reaching distance of the flame, unburned air-fuel mixture, and other gases ejected from the sub-chamber to the main combustion chamber to the cylinder periphery is evenly shortened. As a result, the time to reach the cylinder periphery is shortened, and the velocity can be converted into pressure to reach the cylinder periphery in a short period of time, and the fresh air existing in the main combustion chamber is mixed in a short period of time to promote combustion. And can be completed in a short time. Further, since a plurality of the sub-communication holes can be formed and the passage area of the communication holes can be made large as a whole, squeezing loss can be reduced.

【0014】[0014]

【発明の実施の形態】以下,図1を参照して,この発明
による副室を備えた燃焼室の実施例を説明する。図1は
この発明による副室を備えた燃焼室の一実施例を示す断
面図,及び図2はシリンダヘッドの下面を示す説明図で
ある。
BEST MODE FOR CARRYING OUT THE INVENTION An embodiment of a combustion chamber having a sub chamber according to the present invention will be described below with reference to FIG. FIG. 1 is a sectional view showing an embodiment of a combustion chamber having a sub chamber according to the present invention, and FIG. 2 is an explanatory view showing a lower surface of a cylinder head.

【0015】この副室を備えた燃焼室は,シリンダ8を
備えたシリンダブロック20,シリンダブロック20に
ガスケット29を介して固定されているシリンダヘッド
15,シリンダヘッド15に取り付けた燃料噴射ノズル
10及びシリンダ8内を往復運動するピストン3から構
成されている。この副室を備えた燃焼室は,ピストン3
側に副室2を形成されているものである。シリンダブロ
ック20にはエンジンの気筒数に対応する孔部24が形
成され,該孔部24にシリンダ8を形成したシリンダラ
イナ21を嵌合してもく,又は,図示していないが,こ
れらの孔部24によってシリンダ8を構成してもよいも
のである。また,シリンダヘッド15には,吸排気ポー
ト14が形成され,吸排気ポート14には吸排気バルブ
13が配置されている。
The combustion chamber including the sub chamber includes a cylinder block 20 having a cylinder 8, a cylinder head 15 fixed to the cylinder block 20 via a gasket 29, a fuel injection nozzle 10 attached to the cylinder head 15, and It is composed of a piston 3 which reciprocates in a cylinder 8. The combustion chamber with this sub-chamber is the piston 3
The sub chamber 2 is formed on the side. The cylinder block 20 is formed with holes 24 corresponding to the number of cylinders of the engine, and the cylinder liner 21 having the cylinders 8 formed therein may be fitted into the holes 24. The cylinder 24 may be configured by the hole 24. An intake / exhaust port 14 is formed in the cylinder head 15, and an intake / exhaust valve 13 is arranged in the intake / exhaust port 14.

【0016】この副室を備えた燃焼室は,アルミニウム
合金,FC等の金属で作製されたピストンスカート9,
ピストンスカート9に固定された耐熱性を有するSi3
4等の高強度セラミックスで作製されたピストンヘッ
ド7,及びピストンヘッド7に一体構造に作製された副
室壁部11から構成されている。ピストンスカート9に
は,ピストンリング25を装着するピストンリング溝が
形成され,ピストンスカート9の上部壁体19の中央に
は取付孔16が形成されている。ピストンヘッド7は,
その中央下部に環状ボス部となる副室壁部11を有して
いる。ピストンヘッド7は,その周辺部には下方に延び
る環状リング部18を有し,その中央には副室2を形成
する下方に延びる副室壁部11を有している。
The combustion chamber provided with this sub-chamber includes a piston skirt 9 made of a metal such as aluminum alloy or FC,
Heat-resistant Si 3 fixed to the piston skirt 9
The piston head 7 is made of high-strength ceramics such as N 4 , and the sub-chamber wall portion 11 is integrally formed with the piston head 7. A piston ring groove for mounting the piston ring 25 is formed in the piston skirt 9, and a mounting hole 16 is formed in the center of the upper wall body 19 of the piston skirt 9. The piston head 7 is
The sub-chamber wall portion 11 serving as an annular boss portion is provided in the lower center portion. The piston head 7 has an annular ring portion 18 extending downward in the peripheral portion thereof, and a sub chamber wall portion 11 forming the sub chamber 2 and extending downward in the center thereof.

【0017】ピストンヘッド7とピストンスカート9と
は,ピストンスカート9の取付孔16にピストンヘッド
7の副室壁部11を嵌合し,両者の間に固定金属リング
23をメタルフローで埋め込むことによって両者を互い
に固定することができる。この時,ピストンヘッド7に
おける環状リング部18の下面とピストンスカート9に
おける上部壁体19の外周上面との間に,両者間のシー
ルと遮熱のため,遮熱ガスケット(図示せず)を介在さ
せる。ピストンヘッド7の環状リング部18の下端面を
ピストンスカート9における上部壁体19の外周上面に
当接させて両者を固定することによって,ピストンヘッ
ド7の下面とピストンスカート3における上部壁体19
の上面との間に,両者間の遮熱のため,遮熱空気層17
が形成されている。
The piston head 7 and the piston skirt 9 are formed by fitting the sub chamber wall portion 11 of the piston head 7 into the mounting hole 16 of the piston skirt 9 and embedding the fixed metal ring 23 between them by metal flow. Both can be fixed to each other. At this time, a heat shield gasket (not shown) is interposed between the lower surface of the annular ring portion 18 of the piston head 7 and the outer peripheral upper surface of the upper wall body 19 of the piston skirt 9 in order to seal and heat the both. Let The lower end surface of the annular ring portion 18 of the piston head 7 is brought into contact with the outer peripheral upper surface of the upper wall body 19 of the piston skirt 9 to fix them to each other, whereby the lower surface of the piston head 7 and the upper wall body 19 of the piston skirt 3 are fixed.
The heat-shielding air layer 17 between the upper surface of the
Are formed.

【0018】この副室を備えた燃焼室は,シリンダヘッ
ド下面26から突出してシリンダヘッド15に配置され
た燃料噴射ノズル10,燃料噴射ノズル10の回りでシ
リンダヘッド15の下面部に形成されている複数のキャ
ビティ4によって構成される主燃焼室1,ピストンヘッ
ド7のほぼ中央部に設けた副室2,ピストンヘッド7の
ほぼ中央に形成され且つ上死点近傍で燃料噴射ノズル1
0の突入によって閉鎖される主燃焼室1と副室2とを連
通する主連絡孔5,主連絡孔5の回りでキャビティ4に
向かって且つシリンダ外側から内側に傾斜してピストン
ヘッド7に形成され且つ主燃焼室1と副室2とを連通す
る複数の副連絡孔6,及び燃料噴射ノズル10に設けら
れた副室2内に燃料を噴射する多噴孔22を有している
ものである。
The combustion chamber with the auxiliary chamber, the fuel injection nozzle 10 arranged in the cylinder head 15 to protrude from the sheet cylinder head lower surface 26, around the fuel injection nozzle 10 is formed on the lower surface of the cylinder head 15 Main combustion chamber 1 formed by a plurality of cavities 4 that are formed in the main chamber, sub chamber 2 that is provided in the substantially central portion of piston head 7, and substantially the center of piston head 7, and fuel injection nozzle 1 near the top dead center
Formed in the piston head 7 toward the cavity 4 around the main communication hole 5 and the main communication hole 5 that connect the main combustion chamber 1 and the sub chamber 2 that are closed by the inrush of 0 toward the cavity 4 and inward from the outside of the cylinder And has a plurality of sub-communication holes 6 that connect the main combustion chamber 1 and the sub-chamber 2 and multiple injection holes 22 that inject fuel into the sub-chamber 2 provided in the fuel injection nozzle 10. is there.

【0019】ピストンヘッド7は,ピストンスカート9
に形成された中央の取付孔16に副室2を形成する副室
壁部11が嵌合して固定されている。副連絡孔6の形成
方向は,副室2中心から偏心して形成されている。副室
2から副連絡孔6を通じてキャビティ4に向かって噴出
する火炎ジェット旋回流ISは,主燃焼室1に存在する
吸気スワールSに複合される。
The piston head 7 has a piston skirt 9
The sub-chamber wall portion 11 forming the sub-chamber 2 is fitted and fixed in the central mounting hole 16 formed in the sub chamber 2. The formation direction of the sub communication hole 6 is eccentric from the center of the sub chamber 2. The flame jet swirling flow IS ejected from the sub chamber 2 toward the cavity 4 through the sub communication hole 6 is combined with the intake swirl S existing in the main combustion chamber 1.

【0020】キャビティ4は,シリンダヘッド15に複
数(図4では4箇所)形成されており,シリンダヘッド
15に配置した吸排気バルブ13のバルブ逃げ部又は該
バルブ逃げ部以外の領域に形成されている。キャビティ
4は,シリンダヘッド15の下面部を凹部に形成してバ
ルブ逃げ部を兼用してもよく,吸排気バルブ13のバル
ブ逃げ部が形成されていないシリンダヘッド15の下面
部に凹部を形成してキャビティ4に構成することもでき
る。また,キャビティ4には,副室2から副連絡孔6を
通じて主燃焼室1へ噴出する火炎旋回流れの周方向に拡
大した火炎逃げ部28がそれぞれ形成されている。副室
2から主燃焼室1へ噴出する火炎ジェット旋回流ISの
噴出エネルギーは,火炎逃げ部28で増幅され,主燃焼
室1に残存している吸気スワールS,即ち,新気と火炎
との混合が促進され,空気利用率を向上させ,燃焼スピ
ードをアップし,燃焼期間を短縮して燃焼を短期に完結
し,熱効率をアップしてNOX ,HC等の発生を抑制す
る。
A plurality of cavities 4 (four locations in FIG. 4) are formed in the cylinder head 15, and the cavities 4 are formed in the valve escape portion of the intake / exhaust valve 13 arranged in the cylinder head 15 or in an area other than the valve escape portion. There is. In the cavity 4, the lower surface of the cylinder head 15 may be formed as a recess to serve also as a valve relief portion, or the concave portion may be formed in the lower surface of the cylinder head 15 where the valve relief portion of the intake / exhaust valve 13 is not formed. Alternatively, the cavity 4 can be formed. Further, in the cavity 4, a flame escape portion 28 is formed which is enlarged in the circumferential direction of the flame swirling flow ejected from the sub chamber 2 to the main combustion chamber 1 through the sub communication hole 6. The ejection energy of the flame jet swirling flow IS ejected from the sub chamber 2 to the main combustion chamber 1 is amplified by the flame escape portion 28, and the intake swirl S remaining in the main combustion chamber 1, that is, between the fresh air and the flame. Mixing is promoted, the air utilization rate is improved, the combustion speed is increased, the combustion period is shortened to complete the combustion in a short time, and the thermal efficiency is increased to suppress the generation of NO x , HC and the like.

【0021】複数の副連絡孔6は,シリンダヘッド下面
26に対してはシリンダ周辺側へ傾斜方向に開口し,主
連絡孔5の回りに均等な間隔に隔置して放射方向に複
数,例えば,4〜6個形成され,副室2から主燃焼室1
への火炎,未燃混合気等のガスがシリンダ8の周辺方向
に向かってキャビティ4へ噴射されるように構成されて
いる。また,副連絡孔6を主連絡孔5の回りに設けるこ
とによって,副室2から主燃焼室1へ噴き出される火
炎,未燃混合気等のガスは,シリンダ周辺までの到達距
離が均等に短くなり,シリンダ周辺への到達期間が短縮
される。
The plurality of sub-communication holes 6 are opened in the inclined direction toward the cylinder peripheral side with respect to the lower surface 26 of the cylinder head, are spaced at equal intervals around the main communication hole 5, and are plural in the radial direction, for example. , 4 to 6 are formed, and from the sub chamber 2 to the main combustion chamber 1
Gas such as flame to the cylinder, unburned air-fuel mixture and the like is injected into the cavity 4 toward the peripheral direction of the cylinder 8. Further, by providing the sub communication hole 6 around the main communication hole 5, gases such as flames and unburned gas mixture ejected from the sub chamber 2 to the main combustion chamber 1 can reach the cylinder periphery uniformly. This shortens the time required to reach the area around the cylinder.

【0022】また,燃料噴射ノズル10は,外周部が遮
熱カバー12で覆われており,主燃焼室1,副室2及び
主連絡孔5における熱から遮熱保護されている。燃料噴
射ノズル10は,ピストン上死点近傍で主連絡孔5に突
入して副室2の中央に位置し,副室2内に中央から副室
周辺に向かってキャビティ4で構成される主燃焼室1へ
燃料を噴射するように,多噴孔22を備えている。ま
た,ピストンヘッド7は,ピストン上死点におけるピス
トン上面27とシリンダヘッド下面26とのクリアラン
スが小さくなるように形成され,キャビティ4の形成領
域で大きくなるように,平らな面に形成されている。
Further, the fuel injection nozzle 10 has an outer peripheral portion covered with a heat shield cover 12 to protect it from heat in the main combustion chamber 1, the sub chamber 2 and the main communication hole 5. The fuel injection nozzle 10 is located in the center of the sub chamber 2 by penetrating into the main communication hole 5 in the vicinity of the top dead center of the piston. Multiple injection holes 22 are provided to inject fuel into the chamber 1. Further, the piston head 7 is formed so that the clearance between the piston upper surface 27 and the cylinder head lower surface 26 at the piston top dead center is small, and is formed in a flat surface so as to be large in the formation region of the cavity 4. .

【0023】シリンダヘッド7における副室壁部11
は,薄肉の壁体によってピストン中央に副室2が形成さ
れるように構成されている。ピストンヘッド7とピスト
ンスカート9とは,環状リング部18と上部壁体19の
上面とが接触し,副室壁部11と取付穴16の内壁面と
の接触する以外は,両者は遮熱空気層17によって隔置
されている。また,燃料噴射ノズル10は,シリンダヘ
ッド下面26から下方に延び,ピストン上死点近傍で主
連絡孔5から副室2内に突入し,燃料噴射ノズル10に
設けた多噴孔22から副室2に燃料を噴射するように設
定されている。また,副室壁部11に形成された副室2
は,シリンダ8の中央にほぼ位置しており,副室2と主
燃焼室1とを連通する副連絡孔6は,副室2の外周部に
位置するように形成されている。
Sub chamber wall portion 11 of the cylinder head 7.
Is configured such that the sub chamber 2 is formed in the center of the piston by the thin wall body. The piston head 7 and the piston skirt 9 are in contact with each other except that the annular ring portion 18 and the upper surface of the upper wall body 19 are in contact with each other and the sub chamber wall portion 11 and the inner wall surface of the mounting hole 16 are in contact with each other. Separated by layers 17. Further, the fuel injection nozzle 10 extends downward from the cylinder head lower surface 26, projects into the sub chamber 2 from the main communication hole 5 in the vicinity of the piston top dead center, and from the multiple injection holes 22 provided in the fuel injection nozzle 10 to the sub chamber. 2 is set to inject fuel. In addition, the sub chamber 2 formed in the sub chamber wall portion 11
Is located substantially at the center of the cylinder 8, and the auxiliary communication hole 6 that connects the auxiliary chamber 2 and the main combustion chamber 1 is formed so as to be positioned on the outer peripheral portion of the auxiliary chamber 2.

【0024】この副室を備えた燃焼室は,上記のように
構成されているので,次のような作用をする。この副室
を備えた燃焼室では,吸気行程において吸気ポート14
を通じてシリンダ8内に導入された吸入空気は,圧縮行
程で圧縮されると共に,主連絡孔5及び副連絡孔6を通
じて副室2に導入される。圧縮上死点前近傍で燃料噴射
ノズル10が主連絡孔5を閉鎖すると,副連絡孔6を通
じて副室2に高圧縮された圧縮空気が更に導入される。
この状態で,燃料噴射ノズル10の多噴孔22から燃料
が副室2に噴射され,副室2で燃料と空気とが混合して
燃料リッチな状態で着火燃焼し,副室2での燃焼状態を
燃料リッチで燃焼させ,NOX の発生を抑制できる。次
いで,膨張行程へ移行して膨張行程初期では,燃料噴射
ノズル10が主連絡孔5を閉鎖しているので,副室2の
火炎,未燃混合気等のガスは副室2から副連絡孔6を通
じてキャビティ4で構成されている主燃焼室1へ噴出す
る。
Since the combustion chamber provided with this sub-chamber is constructed as described above, it operates as follows. In the combustion chamber equipped with this sub chamber, the intake port 14 is used in the intake stroke.
The intake air introduced into the cylinder 8 through is compressed in the compression stroke and is introduced into the sub chamber 2 through the main communication hole 5 and the sub communication hole 6. When the fuel injection nozzle 10 closes the main communication hole 5 in the vicinity of the compression top dead center, highly compressed compressed air is further introduced into the sub chamber 2 through the sub communication hole 6.
In this state, the fuel is injected from the multiple injection holes 22 of the fuel injection nozzle 10 into the sub chamber 2, the fuel and the air are mixed in the sub chamber 2 and ignited and burned in a fuel rich state, and the combustion in the sub chamber 2 is performed. state is combusted in the fuel-rich, it is possible to suppress the generation of NO X. Next, since the fuel injection nozzle 10 closes the main communication hole 5 at the beginning of the expansion stroke after shifting to the expansion stroke, gas such as flame and unburned air-fuel mixture in the sub-chamber 2 is discharged from the sub-chamber 2 to the sub-communication hole. It is jetted to the main combustion chamber 1 constituted by the cavity 4 through 6.

【0025】この時,主燃焼室1と副室2とを連通する
副連絡孔6は,副室2の周方向に複数個形成されている
ので,通路面積が副連絡孔6の合計で全体として大きく
形成でき,しぼり損失を低減できる。更に,副室2をピ
ストン中央即ちシリンダ中央に形成し,副室2の外周か
ら副連絡孔6を通じて主燃焼室1へ噴出する火炎,未燃
混合気等のガスは,副連絡孔6及びキャビティ4即ちバ
ルブ逃げ部にガイドされて火炎ジェット旋回流ISとな
って主燃焼室1に存在する吸気スワールSに複合され
て,主燃焼室1に存在する新気を巻き込み,更に火炎逃
げ部28に存在する空気を巻き込んで空気利用率を向上
し,混合燃焼が促進され,次いで,ピストン3が下降し
て燃料噴射ノズル10が主連絡孔5から抜け出て,主連
絡孔5が開放し,副室2から主連絡孔5を通じて主燃焼
室1へ火炎,未燃混合気等のガスが噴出し,主燃焼室1
の中央に存在する空気との混合を促進して燃焼スピード
を速くして燃焼期間を短縮でき,NOX ,HC,スモー
クの発生を抑制した燃焼を行わせることができる。
At this time, since a plurality of sub-communication holes 6 that connect the main combustion chamber 1 and the sub-chamber 2 are formed in the circumferential direction of the sub-chamber 2, the total passage area is the total of the sub-communications holes 6. As a result, a large size can be formed, and the squeezing loss can be reduced. Further, the sub-chamber 2 is formed in the center of the piston, that is, in the center of the cylinder. 4. That is, the flame jet swirl flow IS is guided by the valve escape portion to be combined with the intake swirl S existing in the main combustion chamber 1, and the fresh air existing in the main combustion chamber 1 is entrained, and further into the flame escape portion 28. The existing air is entrained to improve the air utilization rate, the mixed combustion is promoted, then the piston 3 descends, the fuel injection nozzle 10 comes out from the main communication hole 5, the main communication hole 5 opens, and the sub chamber Gas such as flame and unburned air-fuel mixture is ejected from the main combustion chamber 1 through the main communication hole 5 from the main combustion chamber 1
Of promoting mixing of the air present in the center to increase the combustion speed can reduce the combustion period, NO X, HC, it is possible to perform combustion while suppressing generation of smoke.

【0026】[0026]

【発明の効果】この発明による副室を備えた燃焼室は,
上記のように構成されているので,副連絡孔はシリンダ
ヘッドに形成した各キャビティに対して傾斜して開口す
ることになり,副室から副連絡孔を通じて主燃焼室へ噴
出する火炎,未燃混合気等のガスはキャビティの前記主
燃焼室に向けてスムースに高速で噴出し,前記キャビテ
ィにガイドされて火炎ジェット旋回流を形成する。これ
らの火炎ジェット旋回流は,前記主燃焼室に残存してい
る吸気スワールに複合し,混合が促進して燃焼スピード
をアップして燃焼期間が短縮され,燃焼を短期に完結す
ることができ,熱効率を向上させてNOX ,HC,スモ
ークの発生を抑制できる。
The combustion chamber provided with the auxiliary chamber according to the present invention is
With the above-mentioned structure, the sub-communication holes are inclined and opened with respect to the cavities formed in the cylinder head, and the flames and unburned flames ejected from the sub-chamber to the main combustion chamber through the sub-communications holes are opened. Gas such as air-fuel mixture is smoothly ejected toward the main combustion chamber of the cavity at high speed, and is guided by the cavity to form a flame jet swirl flow. These flame jet swirl flows are combined with the intake swirl remaining in the main combustion chamber, mixing is promoted, combustion speed is increased, combustion period is shortened, and combustion can be completed in a short period of time. It is possible to improve the thermal efficiency and suppress the generation of NO X , HC and smoke.

【0027】また,前記副室をピストンの中央部に配置
し,しかも前記主燃焼室と前記副室とを連通する前記副
連絡孔を前記副室の周方向に複数個形成したので,前記
副室から前記主燃焼室のシリンダ周辺への火炎,未燃混
合気等のガスの到達が均等になり且つ短期間に進展す
る。前記主燃焼室に存在する新気に対してシリンダ壁面
までの到達距離が短くなり,前記主燃焼室での空気利用
率を向上して混合が促進される。しかも,前記副連絡孔
の通路面積が前記副連絡孔の合計で全体として大きく形
成でき,しぼり損失を低減できる。
Further, since the sub chamber is arranged in the center of the piston, and a plurality of the sub communication holes for connecting the main combustion chamber and the sub chamber are formed in the circumferential direction of the sub chamber, the sub chamber is formed. Gases such as flame and unburned air-fuel mixture from the chamber to the periphery of the cylinder of the main combustion chamber are evenly distributed and progress in a short period of time. The reaching distance of the fresh air existing in the main combustion chamber to the wall surface of the cylinder is shortened, the air utilization rate in the main combustion chamber is improved, and mixing is promoted. Moreover, the passage area of the sub-communication holes can be made large as a whole as the total of the sub-communication holes, and the squeezing loss can be reduced.

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

【図1】この発明による副室を備えた燃焼室の一実施例
を示す断面図である。
FIG. 1 is a sectional view showing an embodiment of a combustion chamber having a sub chamber according to the present invention.

【図2】図1の副室を備えた燃焼室におけるシリンダヘ
ッドの下面の一実施例を示す説明図である。
FIG. 2 is an explanatory view showing an example of a lower surface of a cylinder head in a combustion chamber including the sub chamber of FIG.

【符号の説明】[Explanation of symbols]

1 主燃焼室 2 副室 3 ピストン 4 キャビティ 5 主連絡孔 6 副連絡孔 7 ピストンヘッド 8 シリンダ 10 燃料噴射ノズル 13 吸排気バルブ 14 吸排気ポート 15 シリンダヘッド 22 多噴孔 26 シリンダヘッド下面 28 火炎逃げ部 1 Main combustion chamber 2 Sub-chamber 3 pistons 4 cavities 5 main communication holes 6 Secondary communication hole 7 piston head 8 cylinders 10 Fuel injection nozzle 13 Intake and exhaust valves 14 intake / exhaust port 15 cylinder head 22 Multiple injection holes 26 Lower surface of cylinder head 28 Flame escape area

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.7 識別記号 FI F02F 3/26 F02F 3/26 C D F02M 61/14 310 F02M 61/14 310D 310P 61/18 320 61/18 320Z (58)調査した分野(Int.Cl.7,DB名) F02B 23/06 F02F 3/00 301 F02F 3/00 302 F02F 3/26 F02M 61/14 310 F02M 61/18 320 ─────────────────────────────────────────────────── ─── Continuation of front page (51) Int.Cl. 7 Identification code FI F02F 3/26 F02F 3/26 C D F02M 61/14 310 F02M 61/14 310D 310P 61/18 320 61/18 320Z (58) Fields investigated (Int.Cl. 7 , DB name) F02B 23/06 F02F 3/00 301 F02F 3/00 302 F02F 3/26 F02M 61/14 310 F02M 61/18 320

Claims (3)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 シリンダヘッド下面から突出するように
配置された燃料噴射ノズル,該燃料噴射ノズルの回りで
シリンダヘッドの下面部に形成されている複数のキャビ
ティによって構成される主燃焼室,ピストンヘッドのほ
ぼ中央部に設けた副室,前記ピストンヘッドのほぼ中央
に形成され且つ上死点近傍で前記燃料噴射ノズルの突入
によって閉鎖される前記主燃焼室と前記副室とを連通す
る主連絡孔,前記主連絡孔の回りで前記キャビティに向
かって且つシリンダ外側から内側に傾斜して前記ピスト
ンヘッドに形成され且つ前記主燃焼室と前記副室とを連
通する複数の副連絡孔,及び前記燃料噴射ノズルに設け
られた前記副室内に燃料を噴射する多噴孔を有し,前記
副連絡孔の形成方向は前記副室中心から偏心して形成さ
れ,前記副室から前記副連絡孔を通じて前記キャビティ
に向かって噴出する火炎旋回流は前記主燃焼室に存在す
る吸気スワールに複合されることを特徴とする副室を備
えた燃焼室。
1. A fuel injection nozzle arranged so as to project from a lower surface of a cylinder head, a main combustion chamber constituted by a plurality of cavities formed in a lower surface portion of the cylinder head around the fuel injection nozzle, and a piston head. A sub-chamber provided substantially in the center of the piston head, and a main communication hole for communicating the sub-chamber with the main combustion chamber, which is formed approximately in the center of the piston head and is closed by the thrust of the fuel injection nozzle near the top dead center. A plurality of sub-communication holes that are formed in the piston head around the main communication hole toward the cavity and inward from the cylinder outer side to communicate with the main combustion chamber and the sub-chamber; The sub-chamber provided in the injection nozzle has multiple injection holes for injecting fuel ,
The direction of formation of the sub communication hole is eccentric from the center of the sub chamber.
From the sub chamber through the sub communication hole to the cavity
The swirling flow of flame ejected toward the main combustion chamber exists in the main combustion chamber.
Combustion chamber with an auxiliary chamber characterized by being combined with an intake swirl .
【請求項2】 前記キャビティは,前記シリンダヘッド
に配置したバルブ逃げ部又は該バルブ逃げ部以外の領域
に形成されていることを特徴とする請求項1に記載の副
室を備えた燃焼室。
2. The combustion chamber having a sub chamber according to claim 1, wherein the cavity is formed in a valve relief portion arranged in the cylinder head or in an area other than the valve relief portion.
【請求項3】 シリンダヘッド下面から突出するように
配置された燃料噴射ノズル,該燃料噴射ノズルの回りで
シリンダヘッドの下面部に形成されている複数のキャビ
ティによって構成される主燃焼室,ピストンヘッドのほ
ぼ中央部に設けた副室,前記ピストンヘッドのほぼ中央
に形成され且つ上死点近傍で前記燃料噴射ノズルの突入
によって閉鎖される前記主燃焼室と前記副室とを連通す
る主連絡孔,前記主連絡孔の回りで前記キャビティに向
かって且つシリンダ外側から内側に傾斜して前記ピスト
ンヘッドに形成され且つ前記主燃焼室と前記副室とを連
通する複数の副連絡孔,及び前記燃料噴射ノズルに設け
られた前記副室内に燃料を噴射する多噴孔を有し,前記
キャビティには,前記副室から前記副連絡孔を通じて前
記主燃焼室へ噴出する火炎旋回流れの周方向に拡大した
火炎逃げ部が形成されていることを特徴とする副室を備
えた燃焼室。
3. A cylinder head so as to project from a lower surface thereof.
The fuel injection nozzles arranged, around the fuel injection nozzle
A plurality of cavities formed on the lower surface of the cylinder head
Main combustion chamber composed of tee, piston head
Sub-chamber at the center of the chamber, approximately the center of the piston head
Of the fuel injection nozzle near the top dead center
Connects the main combustion chamber and the sub chamber, which are closed by
Main connection hole, facing the cavity around the main connection hole
Once and tilted inward from the outside of the cylinder
Is formed on the head and connects the main combustion chamber and the sub chamber.
A plurality of sub-communication holes through which the fuel injection nozzle is provided
A plurality of injection holes for injecting fuel into the sub chamber, and a flame escape portion that is enlarged in the circumferential direction of the flame swirl flow ejected from the sub chamber to the main combustion chamber through the sub communication hole in the cavity. a combustion chamber provided with an auxiliary chamber you characterized in that There are formed.
JP33920293A 1993-12-06 1993-12-06 Combustion chamber with subchamber Expired - Fee Related JP3387185B2 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP33920293A JP3387185B2 (en) 1993-12-06 1993-12-06 Combustion chamber with subchamber
US08/340,868 US5515823A (en) 1993-12-06 1994-11-15 Engine with precombustion chambers
DE69411683T DE69411683T2 (en) 1993-12-06 1994-11-18 Internal combustion engine with pre-combustion chambers
EP94308549A EP0657635B1 (en) 1993-12-06 1994-11-18 Engine with precombustion chambers
DE0657635T DE657635T1 (en) 1993-12-06 1994-11-18 Internal combustion engine with pre-combustion chambers.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP33920293A JP3387185B2 (en) 1993-12-06 1993-12-06 Combustion chamber with subchamber

Publications (2)

Publication Number Publication Date
JPH07158451A JPH07158451A (en) 1995-06-20
JP3387185B2 true JP3387185B2 (en) 2003-03-17

Family

ID=18325213

Family Applications (1)

Application Number Title Priority Date Filing Date
JP33920293A Expired - Fee Related JP3387185B2 (en) 1993-12-06 1993-12-06 Combustion chamber with subchamber

Country Status (1)

Country Link
JP (1) JP3387185B2 (en)

Also Published As

Publication number Publication date
JPH07158451A (en) 1995-06-20

Similar Documents

Publication Publication Date Title
US6073605A (en) Gas engine with pre-combustion chamber
US5645028A (en) Piston structure with a combustion chamber
JP2814346B2 (en) Diesel engine combustion chamber structure
JPH04194314A (en) Two-stroke diesel engine
US5515823A (en) Engine with precombustion chambers
JP3387185B2 (en) Combustion chamber with subchamber
JP2722374B2 (en) Combustion chamber with subchamber
JPS5934417A (en) 2-cycle engine
EP0909893A2 (en) Direct injection diesel engine
JP3918361B2 (en) Sub-chamber gas engine
EP0775810B1 (en) A piston structure with a combustion chamber
JPH07208170A (en) Auxiliary chamber structure in auxiliary chamber type engine
JPH0777105A (en) Structure of piston provided with auxiliary chamber
JP2853209B2 (en) Subchamber insulation engine
JPH06341322A (en) Auxiliary chamber type engine
JPH09324629A (en) Pre-chamber type engine
JP3284671B2 (en) Subchamber type engine with subchamber in piston
JPH0821245A (en) Auxiliary chamber type engine having auxiliary chamber in piston
JPS5968518A (en) Combustion chamber for engine with pre-chamber
JP2500395B2 (en) Sub-chamber insulation engine
JPH06341321A (en) Auxiliary chamber type engine
JPH08260985A (en) Combustion chamber of diesel engine having auxiliary chamber in piston
JPH06307246A (en) Auxiliary chamber type engine
JPH06317158A (en) Auxiliary chamber type engine
JPH10131804A (en) Structure of piston with auxiliary chamber

Legal Events

Date Code Title Description
FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20090110

Year of fee payment: 6

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20100110

Year of fee payment: 7

LAPS Cancellation because of no payment of annual fees