JPH10148129A - Combustion chamber structure - Google Patents

Combustion chamber structure

Info

Publication number
JPH10148129A
JPH10148129A JP8306746A JP30674696A JPH10148129A JP H10148129 A JPH10148129 A JP H10148129A JP 8306746 A JP8306746 A JP 8306746A JP 30674696 A JP30674696 A JP 30674696A JP H10148129 A JPH10148129 A JP H10148129A
Authority
JP
Japan
Prior art keywords
combustion chamber
opening
piston
air
lip
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
JP8306746A
Other languages
Japanese (ja)
Inventor
Tomohiro Oohashi
朋宏 大橋
Setsuo Nishihara
節雄 西原
Atsuo Sato
淳夫 佐藤
Tetsuya Watanabe
哲也 渡邊
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Motors Corp
Original Assignee
Mitsubishi Motors Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Motors Corp filed Critical Mitsubishi Motors Corp
Priority to JP8306746A priority Critical patent/JPH10148129A/en
Publication of JPH10148129A publication Critical patent/JPH10148129A/en
Pending 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
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0672Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis
    • 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
    • F02F1/42Shape or arrangement of intake or exhaust channels in cylinder heads
    • F02F1/4214Shape or arrangement of intake or exhaust channels in cylinder heads specially adapted for four or more valves per cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14Direct injection into combustion chamber
    • 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
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/0621Squish flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • 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)

Abstract

PROBLEM TO BE SOLVED: To ensure durability against mechanical stress without deteriorating a combustion condition by taking a measure against cracking on a part where cracking is generated in an opening part of a combustion chamber of a reentrant type, and remaining acute angled lip on the other part. SOLUTION: In a combustion chamber 2, a cavity opening part 2a is defined as an acute angled lip 2h, and mixing of fuel at the time of reverse squish with air is promoted. An inclining surface which is contracted in a taper shape in the inner surface of an opening part 2a of a part in the specified direction receiving stress of a combustion chamber opening part 2a, to say concretely, in the piston pin 3 direction, is crossed with a vertical surface along the axial direction of a piston 1, the thickness of its crossing part is thickened, and thereby, durability against mechanical stress is improved. An angle formed by an inclining surface for forming the thick wall part and the vertical surface, is formed into an obtuse angle, air is easily separated in the boundary of both surfaces, and thereby, mixing of air and fuel is accelerated.

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】本発明は、直噴式ディーゼル
エンジンのピストン頂面に形成される燃焼室構造に関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a combustion chamber structure formed on a piston top surface of a direct injection diesel engine.

【0002】[0002]

【従来の技術】図6及び図7に示すように、直接噴射式
(以下「直噴式」という)ディーゼルエンジンでは、ピ
ストン10の頂面10aにキャビティが形成された燃焼
室11の開口部略中心に臨んでシリンダヘッドに取り付
けられた燃料噴射ノズル(図示せず)から当該燃焼室1
1内に燃料を噴射し、吸入空気のスワールにより旋回さ
せて燃焼室11の壁面に衝突させ、更にピストン頂面1
0aのスキッシュによって撹拌させて混合を行い燃焼さ
せるようにしている。尚、図6において、1点鎖線は、
ピストンピンの方向を示す。また、頂面10aには吸、
排気弁用のリセス10b、10cが形成されている。
2. Description of the Related Art As shown in FIGS. 6 and 7, in a direct injection type (hereinafter referred to as "direct injection type") diesel engine, a combustion chamber 11 having a cavity formed in a top surface 10a of a piston 10 is substantially at the center. From the fuel injection nozzle (not shown) attached to the cylinder head
The fuel is injected into the combustion chamber 11 and swirled by the swirl of the intake air to collide with the wall of the combustion chamber 11.
The mixture is stirred by a squish of 0a, and the mixture is burned. In FIG. 6, the dashed line indicates
2 shows the direction of a piston pin. In addition, the top surface 10a sucks,
Exhaust valve recesses 10b and 10c are formed.

【0003】燃焼室には種々の形状のものがあり、開口
部(口元)の径が燃焼室内部の径よりも小さく形成され
た即ち、燃焼室の開口部が絞られた形状のリエントラン
ト型のものは、ピストン下降時に逆スキッシュ(燃料と
空気とが燃焼室外に出て行く流れ)が生じる。このと
き、開口部先端(リップ)の形状が大きく作用し、図7
に示すように開口部11aのリップ11bを鋭角にする
と、燃料と空気とが良く混合されて燃焼が良くなる傾向
にある。この開口部リップ11bは、燃焼室の開口部の
全周に亘り形成されている。即ち、燃焼室開口部の鋭角
リップ11bは、逆スキッシュ時の燃料と空気との混合
を促進し、燃焼を改善することに極めて有効である。
There are various types of combustion chambers, and the diameter of the opening (mouth) is formed smaller than the diameter of the inside of the combustion chamber, that is, a reentrant type in which the opening of the combustion chamber is narrowed. In the case of an object, a reverse squish (flow in which fuel and air go out of the combustion chamber) occurs when the piston descends. At this time, the shape of the tip (lip) of the opening largely acts, and FIG.
When the lip 11b of the opening 11a is formed at an acute angle as shown in FIG. 7, the fuel and air tend to be mixed well and the combustion is improved. The opening lip 11b is formed over the entire circumference of the opening of the combustion chamber. That is, the acute angle lip 11b at the opening of the combustion chamber is extremely effective in promoting the mixing of fuel and air during reverse squish and improving combustion.

【0004】[0004]

【発明が解決しようとする課題】ところが、燃焼室の開
口部には機械的応力によってピストンピン方向に引っ張
り応力が加わり、或いは熱応力によってピストンピンと
直角方向に圧縮の応力が加わり、その繰り返し応力によ
り疲労破壊が起こり、亀裂が発生する。その亀裂対策と
して、リエントラント型の燃焼室11では、開口部リッ
プ11bを鈍角形状にしたり、又は、ある程度の厚みを
設けなければならなかった。そのため、燃料と空気との
混合を促進する効果が減少し、出力や、排気ガス悪化の
原因となっている。
However, tensile stress is applied to the opening of the combustion chamber in the direction of the piston pin due to mechanical stress, or compressive stress is applied in the direction perpendicular to the piston pin due to thermal stress. Fatigue failure occurs and cracks occur. As a countermeasure against the cracks, in the reentrant combustion chamber 11, the opening lip 11b has to be obtuse-angled or provided with a certain thickness. For this reason, the effect of promoting the mixing of fuel and air is reduced, which causes deterioration of output and exhaust gas.

【0005】本発明は、上述の点に鑑みてなされたもの
で、リエントラント型の燃焼室開口部の亀裂が発生する
部分に亀裂対策を施し、その他の部分は、鋭角リップを
残すことで、燃焼を悪化させることなく、機械的応力に
対する耐久性を確保するようにした燃焼室構造を提供す
ることを目的とする。
[0005] The present invention has been made in view of the above points, and measures are taken against cracks at the opening of the reentrant type combustion chamber opening, and the other portions are left with an acute lip to prevent combustion. It is an object of the present invention to provide a combustion chamber structure that ensures durability against mechanical stress without deteriorating the pressure.

【0006】[0006]

【課題を解決するための手段】上記目的を達成するため
に本発明によれば、ピストン頂面にキャビティが形成さ
れた燃焼室であって、前記燃焼室は、キャビティ開口部
が、当該キャビティ内部よりも小さく形成されたリエン
トラント型であり、前記キャビティの内面上部を形成し
開口部に臨んでテーパ状に縮径する傾斜面と、前記キャ
ビティ開口部の応力を受ける特定方向におけるピストン
軸方向に沿う縦面とが交わる構造としたものである。
According to the present invention, there is provided a combustion chamber having a cavity formed on a top surface of a piston, wherein the combustion chamber has a cavity opening formed inside the cavity. A reentrant type formed smaller than the inner surface of the cavity, and an inclined surface forming an upper portion of the inner surface of the cavity and tapered toward the opening, and along a piston axis direction in a specific direction receiving stress of the cavity opening. It is a structure that intersects with the vertical surface.

【0007】リエントラント型の燃焼室は、キャビティ
開口部が鋭角リップとされており、逆スキッシュ時の燃
料と空気の混合を促進する。この燃焼室開口部の応力を
受ける特定方向具体的には、ピストンピン方向の部分の
開口部内面がテーパ状に縮径する傾斜面とピストン軸方
向に沿う縦面とを交差させて当該部分の肉厚を厚くする
ことで、機械的応力に対する耐久性が向上する。また、
この肉厚部分を形成する傾斜面と縦面とのなす稜角を鈍
角とすることで、これら両面の境界において空気の剥離
が起き易くなり、空気と燃料との混合が促進される。
[0007] The reentrant combustion chamber has a sharp opening lip at the cavity opening to promote mixing of fuel and air during reverse squishing. The specific direction in which the stress of the combustion chamber opening is received.Specifically, the inner surface of the opening in the portion in the direction of the piston pin intersects the inclined surface whose diameter is reduced in a tapered shape and the vertical surface along the piston axial direction to intersect. By increasing the thickness, durability against mechanical stress is improved. Also,
By making the ridge angle between the inclined surface and the vertical surface forming the thick portion an obtuse angle, air separation easily occurs at the boundary between these two surfaces, and the mixing of air and fuel is promoted.

【0008】[0008]

【発明の実施の形態】以下本発明の実施の態様を実施例
により説明する。図1及び図2に示すようにピストン1
の頂面1aの略中央には円形状のキャビティが形成され
て燃焼室2とされている。燃焼室2は、開口部(口元)
2aが内部よりも小径とされ、底面2bの中央部2cが
円錐形状をなして上方に膨出している。内面(壁面)
は、下部2dがドーナツ状をなして拡径し、僅かに縮径
した中央部2eが略垂直(ピストン1の軸方向)に立ち
上がり、続いてテーパ状に拡径する傾斜面2fをなし、
更に口元2aに臨んで内方にテーパ状に縮径する傾斜面
2gをなしている。このように燃焼室2は、側壁の略中
央部2e、開口部2aの先端2hが燃焼室内部の径より
も小さく形成されたリエントラント型とされている。
尚、中央部2e、開口部2aの先端2hは、夫々リップ
と称され、燃焼室2は、2段リップ形状のリエントラン
ト型とされている。尚、以後開口部2aの先端2hをリ
ップ2hと称する。
DESCRIPTION OF THE PREFERRED EMBODIMENTS The embodiments of the present invention will be described below by way of examples. As shown in FIG. 1 and FIG.
A circular cavity is formed substantially at the center of the top surface 1a of the top surface 1a to form a combustion chamber 2. The combustion chamber 2 has an opening (mouth)
2a is smaller in diameter than the inside, and the central portion 2c of the bottom surface 2b has a conical shape and bulges upward. Inner surface (wall surface)
The lower portion 2d forms a donut shape and expands its diameter, and a slightly reduced central portion 2e rises substantially vertically (in the axial direction of the piston 1), and then forms an inclined surface 2f which expands in a tapered shape.
Further, the inclined surface 2g is tapered inward toward the mouth 2a. Thus, the combustion chamber 2 is of a reentrant type in which the substantially central portion 2e of the side wall and the tip 2h of the opening 2a are formed smaller than the diameter of the inside of the combustion chamber.
The central portion 2e and the tip 2h of the opening 2a are respectively called lips, and the combustion chamber 2 is a two-stage lip-shaped reentrant type. The tip 2h of the opening 2a is hereinafter referred to as a lip 2h.

【0009】ピストン1には図1中上下方向にピストン
ピン3が設けられる。また、ピストン1の頂面1aには
ピストンピン3の左右両側に吸気弁用のリセス1b、1
b、及び排気弁用のリセス1c、1cが設けられてい
る。ところで、前述したように直噴式ディーゼルエンジ
ンにおけるピストンの燃焼室の開口部の亀裂は、主に機
械的応力、又は熱応力によって発生する。機械的応力に
よる亀裂は、ピストンピン3方向に発生するため、ピス
トンピン3方向にのみ亀裂対策を施し、その他の部分
は、開口部鋭角リップを残しておくことで、燃焼を大き
く悪化させることなく、耐久性を確保することが可能で
ある。
The piston 1 is provided with a piston pin 3 in a vertical direction in FIG. The top surface 1a of the piston 1 has recesses 1b, 1
b and exhaust valve recesses 1c, 1c. By the way, as described above, the crack in the opening of the combustion chamber of the piston in the direct injection diesel engine mainly occurs due to mechanical stress or thermal stress. Since cracks due to mechanical stress occur in the direction of the piston pin 3, countermeasures are taken only in the direction of the piston pin 3 and in the other parts, leaving the opening acute angle lip, without greatly deteriorating combustion , Durability can be ensured.

【0010】そこで、燃焼室2の開口部2aのピストン
ピン3の方向以外の部分は、開口部鋭角リップ2hを設
け、ピストンピン3の方向の部分には亀裂対策を施して
耐久性を確保する。即ち、図3に示すように、燃焼室2
の開口部2aのピストンピン3の方向を除く両側のリッ
プ2hは、開口端の内面を形成する傾斜面2gとピスト
ン頂面1aとのなす稜角αが鋭角とされている。即ち、
開口部リップ2hは、鋭角リップとされている。
Therefore, the opening 2a of the combustion chamber 2 is provided with an opening acute angle lip 2h in a portion other than the direction of the piston pin 3, and the portion in the direction of the piston pin 3 is cracked to ensure durability. . That is, as shown in FIG.
In the lip 2h on both sides of the opening 2a except for the direction of the piston pin 3, the ridge angle α formed by the inclined surface 2g forming the inner surface of the opening end and the piston top surface 1a is an acute angle. That is,
The opening lip 2h is an acute angle lip.

【0011】燃焼室2の開口部2aのピストンピン3方
向の吸気弁側先端2i、及び排気弁側先端2jは、図4
及び図5に示すように厚肉とされている。即ち、図4に
おいて、燃焼室2の開口部2aの吸気弁側先端2iを形
成する傾斜面2gは、その略中央位置において垂直(ピ
ストン1の軸方向)に立ち上がって縦面2mをなし、上
端部が円弧状に面取りされてピストン頂面1aに滑らか
に連設されている。縦面2mは、2点鎖線で示すように
カッタ5で切削加工されて形成される。従って、縦面2
mは、傾斜面2gと角をなして交わり、且つ傾斜面2g
と縦面2mとの稜角βは、鈍角をなしている。
The opening 2a of the combustion chamber 2 has a tip 2i on the intake valve side and a tip 2j on the exhaust valve side in the direction of the piston pin 3 as shown in FIG.
And it is made thick as shown in FIG. That is, in FIG. 4, the inclined surface 2 g that forms the intake valve-side tip 2 i of the opening 2 a of the combustion chamber 2 rises vertically (in the axial direction of the piston 1) at a substantially central position to form a vertical surface 2 m, The portion is chamfered in an arc shape and is smoothly connected to the piston top surface 1a. The vertical surface 2m is formed by cutting with the cutter 5 as shown by a two-dot chain line. Therefore, vertical surface 2
m intersects with the inclined surface 2g at an angle, and the inclined surface 2g
Is an obtuse angle with the vertical surface 2m.

【0012】また、図5に示すように燃焼室2の開口部
2aの排気弁側先端2jは、吸気側先端2iよりも僅か
に厚肉とされている。排気側は、吸気側に比べて温度が
高く、疲労強度の低下を招くこととなる。そこで、吸気
側よりも厚肉として、耐久性を確保するようにしてい
る。図5において、開口部先端2jを形成する傾斜面2
gは、中央よりも僅かに下方位置において垂直(ピスト
ン1の軸方向)に立ち上がって縦面2nをなし、上端部
が円弧状に面取りされてピストン頂面1aに滑らかに連
設されている。従って、縦面2nは、吸気側の縦面2m
よりも僅かに長くなり、この長くなった分だけ先端2j
が厚肉となる。この縦面2nは、縦面2mと同様にカッ
タにより切削加工されて形成される。従って、傾斜面2
gと縦面2jとは、角を持って交わり、稜角γは、鈍角
をなしている。
As shown in FIG. 5, the end 2j on the exhaust valve side of the opening 2a of the combustion chamber 2 is slightly thicker than the end 2i on the intake side. The temperature on the exhaust side is higher than that on the intake side, resulting in a decrease in fatigue strength. Therefore, the thickness is made thicker than the intake side to ensure durability. In FIG. 5, the inclined surface 2 forming the opening end 2j
g rises vertically (in the axial direction of the piston 1) slightly below the center to form a vertical surface 2n, and its upper end is chamfered in an arc shape and smoothly connected to the piston top surface 1a. Therefore, the vertical surface 2n is the vertical surface 2m on the intake side.
Is slightly longer than the tip 2j
Becomes thicker. This vertical surface 2n is formed by cutting with a cutter in the same manner as the vertical surface 2m. Therefore, the inclined surface 2
g and the vertical surface 2j intersect with a corner, and the ridge angle γ forms an obtuse angle.

【0013】尚、開口部2aの吸気側先端2i、排気側
先端2jにおける、吸気側の左右のリセス1bと1bと
の連設部分、排気側の左右のリセス1cと1cとの連設
部分を、開口部2aから僅かに外側に後退させて形成し
ても良い。燃焼室2の吸気側先端2i、排気側先端2j
の周方向に沿う長さは、短いと耐久性の確保が困難とな
り、長くすると燃料と空気との混合を促進することが困
難となる。そこで、本発明では、開口部2aの先端2
i、2jの周方向に沿う長さを、燃焼室2の中心に対し
て張る角度θが略60°となるように設定した。しかし
ながら、この角度θは、60°に限るものではなく、耐
久性、燃焼効果の向上等の上記性能が確保されればよ
く、60°以下でも良い。
In addition, at the intake end 2i and the exhaust end 2j of the opening 2a, a continuous portion between the left and right recesses 1b and 1b on the intake side and a continuous portion between the left and right recesses 1c and 1c on the exhaust side. Alternatively, it may be formed by slightly retreating outward from the opening 2a. Intake end 2i, exhaust end 2j of combustion chamber 2
When the length along the circumferential direction is short, it is difficult to ensure durability, and when the length is long, it becomes difficult to promote mixing of fuel and air. Therefore, in the present invention, the tip 2 of the opening 2a
The lengths of i and 2j along the circumferential direction were set such that the angle θ with respect to the center of the combustion chamber 2 was approximately 60 °. However, the angle θ is not limited to 60 °, and may be 60 ° or less as long as the above-mentioned performance such as durability and improvement of the combustion effect is ensured.

【0014】以下に作用を説明する。燃焼室2は、開口
部鋭角リップ2hの部位において逆スキッシュ時の燃料
と空気の混合を促進する。また、ピストンピン3方向の
開口部先端2i、2jは、厚肉とされていることで、機
械的応力に対する耐久性が確保される。そして、これら
の開口部先端2i、2jにおいては、傾斜面2gと縦面
2m、2nとのなす各稜角β、γが鈍角をなしているこ
とで、傾斜面2gと縦面2m、2nとの境界において傾
斜面2gから空気の剥離が起き易くなり、これにより燃
料と空気とが混ざり易くなる。この結果、燃焼室2の開
口部2aの全周を鋭角リップとした場合と略同等の燃焼
性能、排気ガス効果が得られる。
The operation will be described below. The combustion chamber 2 promotes mixing of fuel and air at the time of reverse squishing at the portion of the opening acute angle lip 2h. Further, since the opening ends 2i and 2j in the direction of the piston pin 3 are thick, durability against mechanical stress is secured. At these opening ends 2i and 2j, the ridge angles β and γ formed by the inclined surface 2g and the vertical surfaces 2m and 2n form obtuse angles, so that the inclined surface 2g and the vertical surfaces 2m and 2n At the boundary, the separation of the air from the inclined surface 2g is likely to occur, whereby the fuel and the air are easily mixed. As a result, substantially the same combustion performance and exhaust gas effect as when the entire circumference of the opening 2a of the combustion chamber 2 is formed as an acute lip can be obtained.

【0015】尚、上記実施例では、2段リップのリエン
トラント型の燃焼室に適用した場合について記述した
が、これに限るものではなく、開口部だけにリップを有
する通常のリエントラント型の燃焼室に適用してもよい
ことは勿論である。しかしながら、実施例のように2段
リップ形状と組み合わせるとより効果的である。また、
上記実施例では、4弁タイプのエンジンについて適用し
たが、2弁タイプのものに適用しても良い。
In the above embodiment, the case where the present invention is applied to a two-stage lip reentrant type combustion chamber is described. However, the present invention is not limited to this, and the present invention is applied to a normal reentrant type combustion chamber having a lip only at an opening. Of course, it may be applied. However, it is more effective when combined with a two-step lip shape as in the embodiment. Also,
In the above embodiment, the present invention is applied to a four-valve engine, but may be applied to a two-valve engine.

【0016】[0016]

【発明の効果】以上説明したように本発明によれば、ピ
ストン頂面にキャビティが形成された燃焼室であって、
前記燃焼室は、キャビティ開口部が、当該キャビティ内
部よりも小さく形成されたリエントラント型であり、前
記キャビティの内面上部を形成し開口部に臨んでテーパ
状に縮径する傾斜面と、前記キャビティ開口部の応力を
受ける特定方向におけるピストン軸方向に沿う縦面とが
交わる構造としたことにより、開口部全周に鋭角リップ
を設けた燃焼室と比べて燃焼を悪化させることなく略同
等の性能を有し、且つピストンの機械的応力に対する耐
久性を確保することが可能となる。
As described above, according to the present invention, there is provided a combustion chamber having a cavity formed on the top surface of a piston,
The combustion chamber is a reentrant type in which a cavity opening is formed smaller than the inside of the cavity, and an inclined surface which forms an upper portion of the inner surface of the cavity and has a tapered diameter facing the opening; With a structure that intersects the vertical surface along the piston axis direction in the specific direction that receives the stress of the part, almost the same performance without deteriorating the combustion as compared to the combustion chamber with an acute angle lip all around the opening And durability of the piston against mechanical stress can be ensured.

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

【図1】本発明に係る燃焼室構造を適用したピストンの
平面図である。
FIG. 1 is a plan view of a piston to which a combustion chamber structure according to the present invention is applied.

【図2】図1の矢線II−IIに沿う断面図である。FIG. 2 is a sectional view taken along the line II-II in FIG.

【図3】図2の開口部リップの拡大図である。FIG. 3 is an enlarged view of the opening lip of FIG. 2;

【図4】図1の矢線IV−IVに沿う断面図である。FIG. 4 is a sectional view taken along the line IV-IV in FIG. 1;

【図5】図1の矢線V−Vに沿う断面図である。FIG. 5 is a sectional view taken along the line VV in FIG. 1;

【図6】従来の燃焼室構造を適用したピストンの平面図
である。
FIG. 6 is a plan view of a piston to which a conventional combustion chamber structure is applied.

【図7】図6の矢線VII−VIIに沿う断面図である。FIG. 7 is a sectional view taken along the line VII-VII in FIG. 6;

【符号の説明】[Explanation of symbols]

1 ピストン 2 燃焼室 2a 開口部 2b 底面 2d〜2g、2m、2n 内面 2h 開口部リップ 2i、2j ピストンピン方向開口部先端 3 ピストンピン DESCRIPTION OF SYMBOLS 1 Piston 2 Combustion chamber 2a Opening 2b Bottom surface 2d-2g, 2m, 2n Inner surface 2h Opening lip 2i, 2j Piston pin direction opening tip 3 Piston pin

───────────────────────────────────────────────────── フロントページの続き (72)発明者 渡邊 哲也 東京都港区芝五丁目33番8号 三菱自動車 工業株式会社内 ──────────────────────────────────────────────────続 き Continued on the front page (72) Inventor Tetsuya Watanabe Mitsubishi Motors Corporation, 5-33-8, Shiba 5-chome, Minato-ku, Tokyo

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 ピストン頂面にキャビティが形成された
燃焼室であって、 前記燃焼室は、キャビティ開口部が、当該キャビティ内
部よりも小さく形成されたリエントラント型であり、 前記キャビティの内面上部を形成し開口部に臨んでテー
パ状に縮径する傾斜面と、前記キャビティ開口部の応力
を受ける特定方向におけるピストン軸方向に沿う縦面と
が交わることを特徴とする燃焼室構造。
1. A combustion chamber having a cavity formed on a top surface of a piston, wherein the combustion chamber is a reentrant type in which a cavity opening is formed smaller than the inside of the cavity. A combustion chamber structure, wherein an inclined surface formed and tapered in diameter toward the opening intersects a vertical surface along a piston axis direction in a specific direction subjected to stress of the cavity opening.
JP8306746A 1996-11-18 1996-11-18 Combustion chamber structure Pending JPH10148129A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8306746A JPH10148129A (en) 1996-11-18 1996-11-18 Combustion chamber structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8306746A JPH10148129A (en) 1996-11-18 1996-11-18 Combustion chamber structure

Publications (1)

Publication Number Publication Date
JPH10148129A true JPH10148129A (en) 1998-06-02

Family

ID=17960819

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8306746A Pending JPH10148129A (en) 1996-11-18 1996-11-18 Combustion chamber structure

Country Status (1)

Country Link
JP (1) JPH10148129A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2879247A1 (en) * 2004-12-13 2006-06-16 Renault Sas Combustion chamber for direct injection internal combustion engine, has central injector delivering fuel jet along reduced cord angle, and peripheral part, of tulip, with bursting units to burst injected fuel jets against part along angle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2879247A1 (en) * 2004-12-13 2006-06-16 Renault Sas Combustion chamber for direct injection internal combustion engine, has central injector delivering fuel jet along reduced cord angle, and peripheral part, of tulip, with bursting units to burst injected fuel jets against part along angle

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