JPH084535A - Piston of direct injection type diesel engine - Google Patents

Piston of direct injection type diesel engine

Info

Publication number
JPH084535A
JPH084535A JP6134785A JP13478594A JPH084535A JP H084535 A JPH084535 A JP H084535A JP 6134785 A JP6134785 A JP 6134785A JP 13478594 A JP13478594 A JP 13478594A JP H084535 A JPH084535 A JP H084535A
Authority
JP
Japan
Prior art keywords
cavity
piston
guide groove
diesel engine
air
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
JP6134785A
Other languages
Japanese (ja)
Inventor
Setsuo Yamada
節男 山田
伸也 ▲高▼田
Shinya Takada
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.)
Kubota Corp
Original Assignee
Kubota 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 Kubota Corp filed Critical Kubota Corp
Priority to JP6134785A priority Critical patent/JPH084535A/en
Publication of JPH084535A publication Critical patent/JPH084535A/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
    • 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
    • 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

Abstract

PURPOSE:To expedite inflow of air to the combustion chamber of a direct injection type diesel engine so as to improve its combustion performance. CONSTITUTION:A plurality of swirl guide grooves 6 are formed on the outer ring 5 of a piston head 2, the more each swirl guide groove 6 is advanced, in the peripheral direction A of the outer ring 5, the more they are downwardly deeply recessed and formed in a tapering sliding way shape approaching to a cavity 3, the inlet parts 6a of the swirl guide grooves 6 on a peripheral direction upper side are formed flush with head surfaces 7, and outlet parts on lower sides are communicated with the cavity 3. Directivity of air flow is enhanced, while air is guided along the peripheral direction A of the swirl guide grooves 6 and slides down along a tapering sliding way, and also the air flow is converged by throttle action so as to be introduced to the cavity 3. Hereby, the inflow of the air to a combustion chamber is expedited so that intake swirl can be strengthened.

Description

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

【0001】[0001]

【産業上の利用分野】本発明は直接噴射式ディーゼルエ
ンジンのピストンに関し、エンジンにこのピストンを組
み込むことにより、燃焼室への空気の流入を促進してス
ワールを強化し、空気と燃料の混合を強力にして燃焼性
能を向上できるものを提供する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a piston for a direct injection diesel engine, and by incorporating this piston in the engine, it promotes the inflow of air into the combustion chamber to strengthen the swirl and to mix air and fuel. We will provide products that are strong and can improve combustion performance.

【0002】[0002]

【発明の背景】本発明の対象となる直接噴射式ディーゼ
ルエンジンのピストンの基本構造は、図1、図4又は図
5に示すように、ディーゼルエンジンEのピストン1の
ピストンヘッド2の中央部にキャビティー3を下向きに
凹設した形式のものである。
BACKGROUND OF THE INVENTION The basic structure of the piston of a direct injection diesel engine which is the subject of the present invention is, as shown in FIG. 1, FIG. 4 or FIG. 5, in the center of the piston head 2 of the piston 1 of the diesel engine E. The cavity 3 is of a type recessed downward.

【0003】[0003]

【従来の技術】この形式の従来技術1としては、特開平
3―168322号公報に示すように(図4参照)、ピス
トンヘッド2のキャビティー3の外周部に内径方向に近
付くほどヘッド面7からキャビティー3に落ち込み傾斜
するテーパ面50を形成し、テーパ面50にキャビティ
ー3の径方向から適宜傾斜させて複数の案内溝51を刻
設するとともに、シリンダヘッド10の下面に上記キャ
ビティー3に対向するように断面台形状の凸部52を設
けたものがある。
2. Description of the Related Art As prior art 1 of this type, as shown in Japanese Patent Application Laid-Open No. 3-168322 (see FIG. 4), the head surface 7 becomes closer to the outer peripheral portion of the cavity 3 of the piston head 2 in the inner diameter direction. A taper surface 50 is formed that is inclined from the bottom to the cavity 3 and a plurality of guide grooves 51 are engraved on the taper surface 50 from the radial direction of the cavity 3 as appropriate. 3 is provided with a convex portion 52 having a trapezoidal cross section so as to be opposed to No. 3.

【0004】本従来技術1では、ピストン1の上死点移
行時に、テーパ面50と凸部52との接近でスキッシュ
流の流路53を狭窄してその流れを増速させるうえ、こ
のスキッシュ流を各案内溝51で収束させてその増速作
用を一層強力にできるので、燃料と空気との混合が促進
される。
In the prior art 1, when the piston 1 transitions to the top dead center, the passage of the squish flow 53 is narrowed by the proximity of the tapered surface 50 and the convex portion 52 to accelerate the flow, and the squish flow is also increased. Can be converged at each guide groove 51 to further enhance the speed increasing action, so that the mixing of fuel and air is promoted.

【0005】一方、従来技術2としては、特開平2―1
49719号公報に示すように(図5参照)、ピストンヘ
ッド2のキャビティー3の外周側に複数の空気供給穴5
4を包囲状に凹設し、各空気供給穴54を中央のキャビ
ティー3に火炎案内溝55を介して連通し、火炎案内溝
55を均等な深さで空気供給穴54より浅く形成すると
ともに、吸気スワールの向きSに方向付け、シリンダヘ
ッド10の下面に上記キャビティー3に対向するように
凸部56を設けたものがある。
On the other hand, as the prior art 2, Japanese Patent Laid-Open No. 2-1
As shown in Japanese Patent Publication No. 49719 (see FIG. 5), a plurality of air supply holes 5 are provided on the outer peripheral side of the cavity 3 of the piston head 2.
4, the air supply holes 54 are connected to the central cavity 3 through the flame guide groove 55, and the flame guide groove 55 is formed to have a uniform depth and shallower than the air supply hole 54. There is one in which a convex portion 56 is provided on the lower surface of the cylinder head 10 so as to face the cavity 3 and oriented in the direction S of the intake swirl.

【0006】本従来技術2では、ピストンの上死点移行
時に、キャビティー3はシリンダヘッド10側の凸部5
6により閉塞されるので、空気不足を起こして窒素酸化
物の生成が抑制される。また、上死点を過ぎた後の膨張
移行時には、キャビティー3の火炎や未燃蒸気は激しく
噴出して空気供給穴54の空気と出会い、2段目の混合
が行われる。この場合、火炎は火炎案内溝55により選
択的に空気供給穴54に向かうので、混合速度が高まる
うえ、高いスワール強度が維持される。
In the prior art 2, when the piston moves to the top dead center, the cavity 3 has the convex portion 5 on the cylinder head 10 side.
Since it is blocked by 6, the air shortage is caused and the generation of nitrogen oxides is suppressed. Further, at the time of expansion transition after passing through the top dead center, the flame and unburned vapor in the cavity 3 violently jet and meet the air in the air supply hole 54, and the second stage mixing is performed. In this case, the flame is selectively directed to the air supply hole 54 by the flame guide groove 55, so that the mixing speed is increased and high swirl strength is maintained.

【0007】[0007]

【発明が解決しようとする課題】上記従来技術1では、
キャビティー3の外周側にテーパ面50と案内溝51を
設けてスキッシュ流をある程度高められるが、テーパ面
50はピストンヘッド2に接する局部的な外周箇所に限
定して形成され、その他のヘッド面7には形成されない
ので、スキッシュ流の増速には限界がある。そのうえ、
本従来技術1は、実際には、シリンダヘッド10側の凸
部52とピストン1側のキャビティー3との組み合わせ
でスキッシュ流を増速させる機構なので、凸部52を形
成しない通常の平滑な下面を有するシリンダヘッド10
との組み合わせでは、上記スキッシュの増速作用も一層
制約を受ける。
In the above-mentioned prior art 1,
Although the squish flow can be enhanced to some extent by providing the tapered surface 50 and the guide groove 51 on the outer peripheral side of the cavity 3, the tapered surface 50 is formed only at a local outer peripheral portion in contact with the piston head 2 and other head surfaces. Since it is not formed in 7, there is a limit to the speedup of the squish flow. Besides,
Since the prior art 1 is actually a mechanism for accelerating the squish flow by the combination of the convex portion 52 on the cylinder head 10 side and the cavity 3 on the piston 1 side, an ordinary smooth lower surface without the convex portion 52 is formed. Cylinder head 10 having
In combination with, the squish acceleration effect is further restricted.

【0008】上記従来技術2では、窒素酸化物の生成の
抑制を主目的とするうえ、火炎案内溝55はキャビティ
ー3から空気供給穴54に向けて火炎を案内し、膨張移
行時の2段目の混合を促進するものである。従って、上
死点移行の前・後における燃料と空気との混合過程で
は、この混合の充分な促進には限界がある。また、本従
来技術2も、前記従来技術1と同様に、シリンダヘッド
10側の凸部56をピストン1側の凹部54・55と組
み合わせる機構なので、スワールの増速作用の制約は大
きい。本発明は、直接噴射式ディーゼルエンジンに関
し、燃焼室への空気の流入を促進して燃焼性能を向上で
きるピストンを開発することを技術的課題とする。
In the above-mentioned prior art 2, the main purpose is to suppress the production of nitrogen oxides, and the flame guide groove 55 guides the flame from the cavity 3 toward the air supply hole 54, so that the two stages at the time of expansion transition. It promotes eye mixing. Therefore, in the mixing process of the fuel and the air before and after the transition to the top dead center, there is a limit to the sufficient promotion of this mixing. Further, in the prior art 2 as well, as in the prior art 1, since the convex portion 56 on the cylinder head 10 side is combined with the concave portions 54, 55 on the piston 1 side, the swirl speed-up action is largely restricted. The present invention relates to a direct injection diesel engine, and has a technical problem to develop a piston capable of promoting the inflow of air into a combustion chamber to improve combustion performance.

【0009】[0009]

【課題を解決するための手段】上記課題を達成するため
の手段を、実施例を示す図1〜図3により以下に説明す
る。即ち、本発明は前記基本構造の直接噴射式ディーゼ
ルエンジンのピストンにおいて、上記ピストンヘッド2
の外周縁4とキャビティー3との間の帯状の外輪部5に
複数の渦流案内溝6を形成し、各渦流案内溝6は外輪部
5の周方向Aに進むほど下向きに深く凹設されるととも
に、キャビティー3に近付くように先絞り滑り台状に形
成され、その周方向Aの上手側に位置する渦流案内溝6
の入口部6aを外輪部5の径方向の幅一杯で、且つピス
トンヘッド2のヘッド面7と面一状に形成し、その周方
向Aの下手側に位置する渦流案内溝6の出口部6bをキ
ャビティー3に連通したことを特徴とするものである。
Means for achieving the above object will be described below with reference to FIGS. 1 to 3 showing an embodiment. That is, the present invention relates to the piston of the direct injection diesel engine having the basic structure described above, wherein the piston head 2
A plurality of swirl guide grooves 6 are formed in a strip-shaped outer ring portion 5 between the outer peripheral edge 4 and the cavity 3, and each swirl guide groove 6 is deeply recessed downward as it goes in the circumferential direction A of the outer ring portion 5. At the same time, the vortex flow guide groove 6 is formed in the shape of a tapered slide that approaches the cavity 3 and is located on the upper side of the circumferential direction A thereof.
Of the vortex flow guide groove 6 located on the lower side of the circumferential direction A of the piston head 2 is formed so as to have an inlet portion 6a which is as wide as the outer ring portion 5 in the radial direction and which is flush with the head surface 7. Is communicated with the cavity 3.

【0010】[0010]

【作用】上記ピストン1は、渦流案内溝6の周方向Aを
スワール方向に一致させてディーゼルエンジンに組み込
まれる。そこで、このディーゼルエンジンの作用を説明
する。
The piston 1 is incorporated in a diesel engine with the circumferential direction A of the vortex flow guide groove 6 aligned with the swirl direction. Therefore, the operation of this diesel engine will be described.

【0011】吸気ポートから燃焼室に侵入した空気は、
先ず、ピストンヘッド2の外輪部5にその幅一杯に形成
されて、且つヘッド面7と面一状である渦流案内溝6の
入口部6aに受け入れられる。このため、空気は渦流案
内溝6の周方向Aに沿いながら、先き絞りの滑り台を滑
り落ちるように渦流出口部6bに向かって案内される。
この間に、吸気スワールは流れの方向性を高められると
ともに、その絞り作用で流れを収束されて(即ち、増速さ
れて)、キャビティー3に導入される。従って、凸部を
突設した特殊なシリンダヘッド10をピストン1と組み
合わせる冒述の従来技術1又は2とは異なり、組み合わ
せるシリンダヘッド10の形態に拘わらず、燃焼室への
空気の流入を促進して吸気スワールを強化でき、空気と
燃料の混合を強力に促進できる。
The air that has entered the combustion chamber through the intake port is
First, it is received in the inlet portion 6a of the vortex flow guide groove 6 which is formed in the outer ring portion 5 of the piston head 2 to its full width and is flush with the head surface 7. Therefore, the air is guided toward the vortex flow outlet portion 6b so as to slide down the slide of the first throttle, along the circumferential direction A of the vortex flow guide groove 6.
During this time, the flow direction of the intake swirl is enhanced, and the flow is converged (that is, accelerated) by its throttling action and introduced into the cavity 3. Therefore, unlike the above-mentioned prior art 1 or 2 in which a special cylinder head 10 having a protruding portion is combined with the piston 1, regardless of the form of the cylinder head 10 to be combined, the inflow of air into the combustion chamber is promoted. The intake swirl can be strengthened, and the mixture of air and fuel can be strongly promoted.

【0012】[0012]

【発明の効果】燃焼室に侵入した空気を渦流案内溝によ
り強力にピストンのキャビティーに案内するので、空気
と燃料の混合を強力にして燃焼性能を向上できる。この
ため、排気中の有害成分(スス、CO、NOX、SOXなど)
の発生量を低減するとともに、燃料消費率を改善して、
ディーゼルエンジンの最大出力を高められる。
Since the air that has entered the combustion chamber is strongly guided to the cavity of the piston by the swirl guide groove, it is possible to strongly mix the air and the fuel and improve the combustion performance. Thus, harmful components in the exhaust (soot, CO, NO X, SO X, etc.)
The fuel consumption rate is improved and
The maximum output of the diesel engine can be increased.

【0013】[0013]

【実施例】以下、本発明の実施例を図面に基づいて述べ
る。図1は縦型直接噴射式ディーゼルエンジンのピスト
ンの要部斜視図、図2は同ピストンの平面図、図3は同
ディーゼルエンジンの要部縦断面図である。
Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a perspective view of a main part of a piston of a vertical direct injection diesel engine, FIG. 2 is a plan view of the piston, and FIG. 3 is a vertical sectional view of a main part of the diesel engine.

【0014】図3に示すように、縦型直接噴射式ディー
ゼルエンジンEのシリンダ11の上側にシリンダヘッド
10を組み付け、燃料噴射ポンプ12をシリンダヘッド
10の上方から燃焼室13に、シリンダ11に近付くほ
ど燃焼室13の中心に傾くように突入する。上記シリン
ダヘッド10に吸気ポート15を開け、吸気ポート15
の出口15aに吸気弁16を開閉可能に臨ませる。
As shown in FIG. 3, the cylinder head 10 is assembled on the upper side of the cylinder 11 of the vertical direct injection diesel engine E, and the fuel injection pump 12 is brought from above the cylinder head 10 into the combustion chamber 13 and close to the cylinder 11. It rushes toward the center of the combustion chamber 13 so as to tilt. The intake port 15 is opened in the cylinder head 10 and the intake port 15
The intake valve 16 is opened and closed at the outlet 15a of the.

【0015】図1〜図3に示すように、上記シリンダ1
1にシリンダボア14を形成し、シリンダボア14にピ
ストン1を上下摺動自在に嵌挿し、ピストンヘッド2の
中央部にキャビティー3を下向きに凹設する。上記キャ
ビティー3の外周部3aはピストンヘッド2のヘッド面
7から下方に曲面状に落ち窪み、その中央部3bには円
錐状の墳丘が突設され、前記燃料噴射ポンプ12の噴孔
12aはこのキャビティー3に方向付けられる。
As shown in FIGS. 1 to 3, the cylinder 1
1, a cylinder bore 14 is formed, a piston 1 is vertically slidably fitted in the cylinder bore 14, and a cavity 3 is formed downward in the center of the piston head 2. The outer peripheral portion 3a of the cavity 3 is depressed downward from the head surface 7 of the piston head 2 in a curved shape, and a conical mound is projected in the central portion 3b thereof, and the injection hole 12a of the fuel injection pump 12 is It is directed to this cavity 3.

【0016】図1〜図3に示すように、上記ピストンヘ
ッド2の外周縁4とキャビティー3との間の帯状の外輪
部5に3個の渦流案内溝6を形成する。図1〜図2に示
すように、各渦流案内溝6は外輪部5の周方向A(具体
的には、左方向)に進むほど下向きに深く凹設されるとと
もに、キャビティー3に近付くように、先絞り滑り台状
に形成される。但し、吸気スワールの方向は、例えば、
吸気ポート15のスワール室から燃焼室13に空気が侵
入する方向で決まるが、上記渦流案内溝6が絞られて行
く周方向Aは、このスワール方向に一致するように設定
される。
As shown in FIGS. 1 to 3, three swirl guide grooves 6 are formed in a belt-shaped outer ring portion 5 between the outer peripheral edge 4 of the piston head 2 and the cavity 3. As shown in FIGS. 1 and 2, each vortex flow guide groove 6 is deeply recessed downward as it goes in the circumferential direction A (specifically, leftward direction) of the outer ring portion 5 and approaches the cavity 3. In addition, it is formed in the shape of a tapered slide. However, the direction of the intake swirl is, for example,
Although it is determined by the direction in which air enters the combustion chamber 13 from the swirl chamber of the intake port 15, the circumferential direction A in which the swirl guide groove 6 is narrowed is set so as to coincide with this swirl direction.

【0017】図2に示すように、上記渦流案内溝6を平
面視すると、細長い三角形の底辺を動かさずに、その頂
点を一定方向に捩り旋回させたような形状を呈する。こ
のため、図1に示すように、スワール方向Aの上手側に
位置する渦流案内溝6の入口部6aは、外輪部5の径方
向の幅一杯で、且つピストンヘッド2のヘッド面7と面
一状に形成される。また、そのスワール方向Aの下手側
に位置する渦流案内溝6の出口部6bはキャビティー3
に連通される。しかも、ピストンヘッド2を平面視する
と、各渦流案内溝6の入口部6aは隣接する渦流案内溝
6の出口部6bに接するように配置される。
As shown in FIG. 2, when the vortex flow guide groove 6 is viewed in plan, it has a shape in which the base of an elongated triangle is not moved but its apex is twisted and swung in a certain direction. Therefore, as shown in FIG. 1, the inlet portion 6a of the swirl guide groove 6 located on the upper side of the swirl direction A has the full width in the radial direction of the outer ring portion 5 and is flush with the head surface 7 of the piston head 2. Formed in a uniform shape. Further, the outlet portion 6b of the vortex flow guide groove 6 located on the lower side of the swirl direction A has the cavity 3
Be communicated to. Moreover, when the piston head 2 is viewed in a plan view, the inlet portion 6a of each vortex flow guide groove 6 is arranged so as to contact the outlet portion 6b of the adjacent vortex flow guide groove 6.

【0018】そこで、本実施例のピストンを組み込んだ
直接噴射式ディーゼルエンジンの機能を説明する。ピス
トンヘッド2に凹設される渦流案内溝6の入口部6a
は、帯状の外輪部5の幅一杯に形成されて、且つヘッド
面7と面一状に形成されるので、吸気ポート15から燃
焼室13に侵入した空気は、先ず、この3個の渦流案内
溝6の入口部6aに夫々受け入れられる。
The function of the direct injection diesel engine incorporating the piston of this embodiment will be described. Inlet 6a of swirl guide groove 6 recessed in piston head 2
Is formed so as to fill the width of the belt-shaped outer ring portion 5 and to be flush with the head surface 7, so that the air that has entered the combustion chamber 13 through the intake port 15 is first guided by these three vortex flow guides. It is received in the inlet portion 6a of the groove 6, respectively.

【0019】このため、空気は渦流案内溝6のスワール
方向Aに沿いながら、先き絞りの滑り台(図1及び図2
の斜線部参照)を滑り落ちる状態で渦流案内溝6の出口
部6bに案内される。この間に、空気はその流れの方向
性を高められるとともに、渦流案内溝6の絞り作用で流
れを収束されて(即ち、増速されて)、渦流案内溝6の出
口部6bからキャビティー3に導入される。従って、こ
の渦流案内溝6の案内作用と絞り作用により、空気の流
入を促進して吸気スワールを強化できるので、燃料噴射
ポンプ12からキャビティー3に向かって噴射される燃
料と当該空気の混合を強力に促進して、ディーゼルエン
ジンEの燃焼性能を高められるとともに、排気中の有害
成分の発生量を低減できる。
For this reason, the air flows along the swirl direction A of the vortex flow guide groove 6 while moving along the swirl direction A (see FIGS. 1 and 2).
It is guided to the outlet portion 6b of the vortex flow guide groove 6 in a state of sliding down. During this time, the direction of the flow of the air is enhanced, and the flow is converged (that is, accelerated) by the throttling action of the vortex flow guide groove 6 to move from the outlet portion 6b of the vortex flow guide groove 6 to the cavity 3. be introduced. Therefore, the guide action of the vortex flow guide groove 6 and the throttle action can promote the inflow of air to strengthen the intake swirl, so that the fuel injected from the fuel injection pump 12 toward the cavity 3 is mixed with the air. The combustion performance of the diesel engine E can be enhanced strongly, and the amount of harmful components in the exhaust gas can be reduced.

【0020】尚、本発明は、ピストンヘッド2の外輪部
5に先き絞り滑り台状の渦流案内溝6を凹設することを
特徴とするので、この案内溝6の個数は2個、或は3個
以上でも良い。また、各渦流案内溝6の入口部6aは隣
接する渦流案内溝6の出口部6bに接することなく、離
間していても差し支えない。一方、本発明は、シリンダ
ボアが縦向きである縦型ディーゼルエンジンに限らず、
シリンダボアが横向きの横型エンジンにも適用できる。
Since the present invention is characterized in that the outer ring portion 5 of the piston head 2 is provided with a squeezing slide groove-like vortex guide groove 6 in advance, the number of the guide groove 6 is two or two. Three or more may be used. Further, the inlet portion 6a of each vortex flow guide groove 6 may be separated without contacting the outlet portion 6b of the adjacent vortex flow guide groove 6. On the other hand, the present invention is not limited to a vertical diesel engine in which the cylinder bore is oriented vertically,
It can also be applied to horizontal engines with the cylinder bore facing sideways.

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

【図1】縦型直接噴射式ディーゼルエンジンのピストン
の要部斜視図である。
FIG. 1 is a perspective view of a main part of a piston of a vertical direct injection diesel engine.

【図2】同ピストンの平面図である。FIG. 2 is a plan view of the piston.

【図3】同ディーゼルエンジンの要部縦断面図である。FIG. 3 is a longitudinal sectional view of a main part of the diesel engine.

【図4】従来技術1を示し、図4Aは直接噴射式ディー
ゼルエンジンの要部縦断面図、図4Bはピストンヘッド
の要部斜視図である。
FIG. 4 shows Prior Art 1, FIG. 4A is a longitudinal sectional view of a main part of a direct injection diesel engine, and FIG. 4B is a perspective view of a main part of a piston head.

【図5】従来技術2を示し、図5Aは直接噴射式ディー
ゼルエンジンの要部縦断面図、図5Bはピストンヘッド
の平面図である。
FIG. 5 shows Prior Art 2, FIG. 5A is a longitudinal sectional view of a main part of a direct injection diesel engine, and FIG. 5B is a plan view of a piston head.

【符号の説明】[Explanation of symbols]

1…ピストン、2…ピストンヘッド、3…キャビティ
ー、4…ピストンの外周縁、5…ピストンヘッドの外輪
部、6…渦流案内溝、6a…渦流案内溝の入口部、6b
…渦流案内溝の出口部、7…ヘッド面、A…外輪部の周
方向、E…直接噴射式ディーゼルエンジン。
DESCRIPTION OF SYMBOLS 1 ... Piston, 2 ... Piston head, 3 ... Cavity, 4 ... Piston outer peripheral edge, 5 ... Piston head outer ring part, 6 ... Vortex guide groove, 6a ... Vortex guide groove inlet part, 6b
... outlet of swirl guide groove, 7 ... head surface, A ... circumferential direction of outer ring, E ... direct injection diesel engine.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 ディーゼルエンジン(E)のピストン(1)
のピストンヘッド(2)の中央部にキャビティー(3)を下
向きに凹設した直接噴射式ディーゼルエンジンのピスト
ンにおいて、 上記ピストンヘッド(2)の外周縁(4)とキャビティー
(3)との間の帯状の外輪部(5)に複数の渦流案内溝(6)
を形成し、 各渦流案内溝(6)は外輪部(5)の周方向(A)に進むほど
下向きに深く凹設されるとともに、キャビティー(3)に
近付くように先絞り滑り台状に形成され、 その周方向(A)の上手側に位置する渦流案内溝(6)の入
口部(6a)を外輪部(5)の径方向の幅一杯で、且つピス
トンヘッド(2)のヘッド面(7)と面一状に形成し、その
周方向(A)の下手側に位置する渦流案内溝(6)の出口部
6(b)をキャビティー(3)に連通したことを特徴とする
直接噴射式ディーゼルエンジンのピストン。
1. A piston (1) for a diesel engine (E)
In a piston of a direct injection diesel engine in which a cavity (3) is recessed downward in the center of the piston head (2), the outer peripheral edge (4) of the piston head (2) and the cavity
A plurality of swirl guide grooves (6) are formed in the strip-shaped outer ring part (5) between (3) and
And each vortex flow guide groove (6) is deeply recessed downward as it goes in the circumferential direction (A) of the outer ring portion (5), and is formed in a pre-sliding slide shape so as to approach the cavity (3). The inlet portion (6a) of the vortex flow guide groove (6) located on the upper side of the circumferential direction (A) is filled with the radial width of the outer ring portion (5) and the head surface of the piston head (2) ( 7) is formed so as to be flush with, and the outlet portion 6 (b) of the vortex flow guide groove (6) located on the lower side of the circumferential direction (A) is communicated with the cavity (3). Injection diesel engine piston.
JP6134785A 1994-06-17 1994-06-17 Piston of direct injection type diesel engine Pending JPH084535A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6134785A JPH084535A (en) 1994-06-17 1994-06-17 Piston of direct injection type diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6134785A JPH084535A (en) 1994-06-17 1994-06-17 Piston of direct injection type diesel engine

Publications (1)

Publication Number Publication Date
JPH084535A true JPH084535A (en) 1996-01-09

Family

ID=15136500

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6134785A Pending JPH084535A (en) 1994-06-17 1994-06-17 Piston of direct injection type diesel engine

Country Status (1)

Country Link
JP (1) JPH084535A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006090884A1 (en) * 2005-02-24 2006-08-31 Toyota Jidosha Kabushiki Kaisha Inernal combustion engine
CN100392230C (en) * 2003-08-19 2008-06-04 扬动股份有限公司 IC engine piston for improving air availability
JP2012057566A (en) * 2010-09-10 2012-03-22 Hino Motors Ltd Combustion chamber structure for direct injection type diesel engine
CN109854359A (en) * 2018-10-30 2019-06-07 中国北方发动机研究所(天津) A kind of eddy flow groove profile combustion chamber suitable for turbulence burning system
US10415456B2 (en) * 2014-04-29 2019-09-17 Volvo Truck Corporation Combustion chamber for an internal combustion engine and an internal combustion engine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100392230C (en) * 2003-08-19 2008-06-04 扬动股份有限公司 IC engine piston for improving air availability
WO2006090884A1 (en) * 2005-02-24 2006-08-31 Toyota Jidosha Kabushiki Kaisha Inernal combustion engine
JP2006233839A (en) * 2005-02-24 2006-09-07 Toyota Motor Corp Internal combustion engine
US7681550B2 (en) 2005-02-24 2010-03-23 Toyota Jidosha Kabushiki Kaisha Internal combustion engine
JP2012057566A (en) * 2010-09-10 2012-03-22 Hino Motors Ltd Combustion chamber structure for direct injection type diesel engine
US10415456B2 (en) * 2014-04-29 2019-09-17 Volvo Truck Corporation Combustion chamber for an internal combustion engine and an internal combustion engine
CN109854359A (en) * 2018-10-30 2019-06-07 中国北方发动机研究所(天津) A kind of eddy flow groove profile combustion chamber suitable for turbulence burning system

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