JPS62255521A - Pent roof type piston - Google Patents

Pent roof type piston

Info

Publication number
JPS62255521A
JPS62255521A JP61098107A JP9810786A JPS62255521A JP S62255521 A JPS62255521 A JP S62255521A JP 61098107 A JP61098107 A JP 61098107A JP 9810786 A JP9810786 A JP 9810786A JP S62255521 A JPS62255521 A JP S62255521A
Authority
JP
Japan
Prior art keywords
cavity
piston
pin hole
pent roof
axial direction
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
JP61098107A
Other languages
Japanese (ja)
Inventor
Takashi Makimoto
槙本 隆
Shoichiro Miyashita
宮下 彰一郎
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 JP61098107A priority Critical patent/JPS62255521A/en
Publication of JPS62255521A publication Critical patent/JPS62255521A/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
    • 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
    • F02B23/0678Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets
    • F02B23/0693Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets the combustion space consisting of step-wise widened multiple zones of different depth
    • 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
    • F02B23/0624Swirl flow
    • 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
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/0669Details related to the fuel injector or the fuel spray having multiple fuel spray jets per injector nozzle
    • 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
    • F02F2001/241Cylinder heads specially adapted to pent roof shape of the combustion chamber
    • 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 suppress a quantity of atomized fuel running over a cavity, by further hollowing an inner wall under an opening of the cavity in a direction perpendicular to the axial direction of a piston pin hole, and thereby enlarging a radial dimension in the cavity. CONSTITUTION:In a pent roof type piston 1, a piston top surface 3 is projected at a portion just over a piston pin hole 2 along the axial direction of the piston pin hole 2, and the portion is inclined at its both ends. The piston top surface 3 is recessed at its central portion to form a cavity 4. An inner wall 6 under an opening 5 of the cavity 4 is further hollowed in a direction perpendicular to the axial direction of the piston pin hole 2 to thereby enlarge a radial dimension in the cavity. Accordingly, there is formed an overhung portion 7 over a small-height portion of the inner wall 6 of the cavity 4 in such a manner as to hang over the small-height portion. Further, the overhang of the overhung portion 7 is widened at the smallest-height portion of the inner wall 6. As a result, it is possible to suppress a quantity of atomized fuel running over the cavity 4 from the small-height portion of the inner wall 6 and thereby reduce the generation of HC and smoke.

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は燃料を直接燃焼室内に噴射供給する直噴式内燃
機関に採用するペントルーフ形ピストンに係り、特にピ
ストン冠面に凹設するキャビティ形状を改良したペント
ルーフ形ピストンに関する。
[Detailed Description of the Invention] [Field of Industrial Application] The present invention relates to a pent roof type piston employed in a direct injection internal combustion engine that directly injects fuel into a combustion chamber, and particularly relates to a pent roof type piston having a cavity shape recessed in the crown surface of the piston. Concerning an improved pent roof type piston.

[従来の技術1 一般に内燃機関にあっては、吸・排気弁の径を大径化し
たりあるいは各気筒当りの吸・排気弁の数を増加したり
して吸・排気ボートの流路断面積を増大させることによ
り、その吸・排気効率を改善することができる。
[Prior art 1] Generally, in internal combustion engines, the cross-sectional area of the flow path of the intake/exhaust boat is increased by increasing the diameter of the intake/exhaust valves or by increasing the number of intake/exhaust valves per cylinder. By increasing , the intake and exhaust efficiency can be improved.

しかしながら、このようにして吸・排気ボートの流路断
面積の増大化を計ると、吸・排気弁はそれらの干渉を避
けるために互いにその弁軸をV型に傾斜せざるを得なく
なる。すると動弁機構の配置上の関係からシリンダヘッ
ド下面に形成する燃焼室は、クランク軸の軸線に沿って
中央部分を最も上方に窪ませると共にその両側を次第に
傾斜させてバルブ軸に対して略垂直となるように形成し
たペントルーフ形状(屋根形状)にする必要が生じ、か
つ直接噴射式ディーゼル機関等の直噴式内燃機関にこの
ペントルーフ形燃焼室を採用しようとすると、18〜2
0という高圧縮比を確保するためには、実願昭60−1
43456号に提案した「ディーゼル機関の燃焼室構造
」等に示したように、必然的にピストン冠面もシリンダ
ヘッドの下面形状に相応させて逆に上方に突出させたペ
ントルーフ形状にしなければならなくなる。
However, if the cross-sectional area of the flow path of the intake/exhaust boat is increased in this manner, the valve shafts of the intake/exhaust valves must be inclined in a V-shape to avoid interference between them. Then, due to the arrangement of the valve mechanism, the combustion chamber formed on the lower surface of the cylinder head is recessed upwards most in the center along the axis of the crankshaft, and gradually slopes on both sides to form a combustion chamber that is approximately perpendicular to the valve axis. It becomes necessary to create a pent roof shape (roof shape) formed so that it becomes 18 to 2.
In order to secure a high compression ratio of 0,
As shown in ``Diesel Engine Combustion Chamber Structure'' proposed in No. 43456, the piston crown surface must necessarily correspond to the lower surface shape of the cylinder head and have a pent roof shape that protrudes upward. .

[発明が解決しようとする問題点] ところで、直噴式内燃機関の場合、ピストン冠面の略中
央部には実質的な燃焼室を形成するためのキャビティが
凹設されるが、第5図及び第6図とに示すように、従来
のペントルーフ形ピストンaではそのキャビティbは横
断面が円形に形成されていた。従って、そのキャビティ
bの内周壁面Cを展開すると第7図に示すようになって
おり、キャビティbの開口の上端縁dは平坦な底部レベ
ルに対して周方向に沿って連続的にその高さhbが変化
していた。このため、噴射ノズルeがら噴射された燃料
噴霧「はスワールSに流されてキャビティb内を旋回す
ると、遠心力の影響でキャビティ内周壁面Cの低い部分
Qがらキャごディb外のピストン冠面iの上側へと飛び
出そうとし、更にこの部分は他の部分よりも逆スキッシ
ュが強くなるので噴霧の一部及び火炎が酸素量の少ない
ピストン冠面とシリンダヘッド間の隙間に吹きこぼれや
すくなっていた。その結果吹きこぼれた噴霧の一部及び
火炎は02不足を生じて多量のIIcやスモークを発生
させてしまうという問題を招いていた。
[Problems to be Solved by the Invention] Incidentally, in the case of a direct injection internal combustion engine, a cavity for forming a substantial combustion chamber is recessed approximately in the center of the crown surface of the piston. As shown in FIG. 6, the cavity b of the conventional pent roof piston a has a circular cross section. Therefore, when the inner circumferential wall surface C of the cavity b is developed, it becomes as shown in FIG. Sahb was changing. For this reason, when the fuel spray injected from the injection nozzle e is swept by the swirl S and turns inside the cavity b, the low part Q of the inner circumferential wall C of the cavity is caused by the influence of centrifugal force, and the piston crown outside the cavity b is It tried to jump out to the upper side of surface i, and the reverse squish was stronger in this part than in other parts, so part of the spray and the flame were likely to spill over into the gap between the piston crown surface and the cylinder head, where the amount of oxygen was low. As a result, a portion of the spray that spilled over and the flame caused a problem in that 02 was insufficient and a large amount of IIc and smoke were generated.

また、これを改善するために従来では、キャビテイ外ピ bの開口側の内周壁Cを径方向の内方に突出させた棚部
jを設けていたが、未だ改善の余地を残していた。
In order to improve this, conventionally, a shelf j was provided in which the inner circumferential wall C on the opening side of the cavity outer pin b protruded radially inward, but there was still room for improvement.

本発明は上記の問題点に鑑みてなされたものであり、そ
の目的は、キャビティ内周壁高ざの低い部分からキャビ
テイ外に吹きこぼれる燃料噴霧の聞を可及的に抑えてH
Cとスモークとの発生量を低減し得る直噴式内燃機関用
のペントルーフ形ピストンを提供することにある。
The present invention has been made in view of the above-mentioned problems, and its purpose is to suppress as much as possible the amount of fuel spray spilling over from the low height part of the cavity inner circumferential wall to the outside of the cavity.
An object of the present invention is to provide a pent roof type piston for a direct injection internal combustion engine that can reduce the amount of C and smoke generated.

[問題点を解決するための手段] 本発明は上記の目的を達成するために、ピストン冠面の
ピストンピン孔直上部をその軸方向に沿わせて突出させ
ると共にその両側部を傾斜させてペントルーフ状に形成
し、該ピストン冠面の゛中央部にピストンピン孔の軸方
向と直交する開口部下の内周壁を窪ませて径方向外方に
拡大したキャビティを形成してペントルーフ形ピストン
を構成する。
[Means for Solving the Problems] In order to achieve the above-mentioned object, the present invention makes the piston crown surface directly above the piston pin hole protrude along the axial direction, and both sides thereof are inclined to form a pent roof. A pent roof type piston is formed by forming a cavity in the central part of the piston crown surface under the opening perpendicular to the axial direction of the piston pin hole to form a cavity expanding outward in the radial direction. .

[作 用] ピストン冠面の中央部に凹設するキャビティの開口部下
の内周壁をピストンピン孔の軸方向と直交する方向に更
に窪ませて径方向外方に拡大形成することで、キャビテ
ィの内周壁高さの低い部分にその上方を覆う棚部を形成
し、かつその最も低い部分での棚部の張出しを大きくす
る。これにより内周壁高さの低い部分からキャビテイ外
に吹きこぼれる燃料噴霧のGを可及的に抑えて110.
スモーりの発生量を低減させる。
[Function] By further recessing the inner peripheral wall below the opening of the cavity recessed in the center of the piston crown surface in a direction perpendicular to the axial direction of the piston pin hole and expanding radially outward, the cavity is expanded. A shelf part covering the upper part of the inner circumferential wall is formed at a low height part, and the protrusion of the shelf part at the lowest part is made large. This suppresses as much as possible the G of the fuel spray spilling out of the cavity from the low-height portion of the inner circumferential wall.
Reduces the amount of smoke generated.

[実施例] 以下に本発明に係るペントルーフ形ピストンの好適一実
施例を添付図面に基づき詳述する。
[Embodiment] A preferred embodiment of the pent roof piston according to the present invention will be described in detail below with reference to the accompanying drawings.

第1図は直噴式ディーゼル機関等の直噴式内燃機関に用
いるペントルーフ形ピストンの平面図であり、第2図は
そのII−II線矢視断面図である。
FIG. 1 is a plan view of a pent roof type piston used in a direct injection internal combustion engine such as a direct injection diesel engine, and FIG. 2 is a sectional view taken along the line II--II.

図示するように、ピストン1はそのピストンピン孔2の
直上部のピストン冠面3がピストンピン孔2の軸方向(
即ち、クランク軸方向)に沿って上方に突出′され、か
つその両側部は傾斜されてペントルーフ形状(屋根形状
)に形成されており、このペントルーフ形状は図示して
いないが、・シリンダヘッドの下面に形成されるシリン
ダヘッド側の燃焼室形状に相応されている。
As shown in the figure, the piston 1 has a piston crown surface 3 directly above the piston pin hole 2 in the axial direction of the piston pin hole 2 (
In other words, it protrudes upward along the crankshaft direction, and its both sides are sloped to form a pent roof shape (roof shape). Although this pent roof shape is not shown, the lower surface of the cylinder head This corresponds to the shape of the combustion chamber on the cylinder head side, which is formed in the cylinder head.

ところで、ピストン冠面3のほぼ中央部には圧縮行程の
終了時にシリンダヘッドとによって実質的な燃焼室を形
成するためのキャビティ4が凹設されるが、本発明のペ
ントルーフ形ピストン1ではそのキャビティ4はその開
口部5下の内周壁6がピストンピン孔2の軸方向と直交
する方向に更に窪ませられて径方向外方に拡大形成され
ており、これによりそのキャビティ4の内周壁6の高さ
が低くなる部分に、その上方を覆う11部7を形成して
いる。
Incidentally, a cavity 4 is recessed approximately in the center of the piston crown surface 3 to form a substantial combustion chamber with the cylinder head at the end of the compression stroke. 4 has an inner circumferential wall 6 below the opening 5 which is further depressed in a direction perpendicular to the axial direction of the piston pin hole 2 and expanded radially outward. A part 11 7 is formed in the part where the height is lowered to cover the upper part.

即ち、本実施例ではその開口部5下のキャビティ4はそ
の横断面が楕円形状になっており、ピストンピン孔2の
軸方向と直交する方向に長袖を有している。従ってキャ
ビティ4の内周壁6の高さが最も低くなる部分での棚部
7の張出しt2が最大になっている。また図示例では、
キ17ビテイ4の開口部5はそのキャビティ上縁部の周
縁が更に径方向内方に延出されて真円状に絞られて開口
され、これにより周縁部にはこれに沿って一様にキャビ
ティ4の底部からの高さが等しい棚部7が形成されて、
キャビティ内周壁6の高さが最も高い部分での棚部7の
張出しtlが最小となっている。
That is, in this embodiment, the cavity 4 below the opening 5 has an elliptical cross section and has a long sleeve in the direction perpendicular to the axial direction of the piston pin hole 2. Therefore, the overhang t2 of the shelf portion 7 is maximized at the portion where the height of the inner peripheral wall 6 of the cavity 4 is the lowest. In addition, in the illustrated example,
The opening 5 of the cavity 4 is opened by extending the periphery of the upper edge of the cavity further inward in the radial direction and narrowing it into a perfect circle. A shelf 7 having the same height from the bottom of the cavity 4 is formed,
The overhang tl of the shelf portion 7 at the highest portion of the cavity inner circumferential wall 6 is the smallest.

尚、この棚部7の張出し長さはそのキャビティ4の開口
径dに対して最小値t 1= d150〜d/15.最
大値t2=d/10〜d/3程度に形成することが望ま
しい。
The overhang length of this shelf 7 is a minimum value t1=d150 to d/15 with respect to the opening diameter d of the cavity 4. It is desirable to form the maximum value t2=d/10 to about d/3.

一方、第1図に示ずようにキャビティ4の略中心部の上
方には、シリンダヘッドに取付けられてキャビティ4内
に燃料を噴射供給する噴射ノズル8が配設される。この
噴射ノズル8はキャビティ4の内周壁6に臨んでピスト
ンピン孔2の軸心に対して45°の角度で燃料を噴射す
る4つの噴口9を右しており、かつその各噴口9はそれ
らから噴射される燃料Il#霧Fが内周壁6の棚部7の
下側に衝突するように斜め下方に方向づけられ、衝突し
た燃料噴iF及びこれにより生成される混合気Gはスワ
ールSの下流方向に流下するようになっている。
On the other hand, as shown in FIG. 1, an injection nozzle 8 is disposed above the approximate center of the cavity 4 and is attached to the cylinder head to inject fuel into the cavity 4. This injection nozzle 8 faces the inner circumferential wall 6 of the cavity 4 and has four injection ports 9 on the right side that inject fuel at an angle of 45° to the axis of the piston pin hole 2, and each of the injection ports 9 The fuel Il# mist F injected from the is directed diagonally downward so as to collide with the lower side of the shelf 7 of the inner peripheral wall 6, and the collided fuel injection iF and the air-fuel mixture G generated thereby are downstream of the swirl S. It is designed to flow downward in the direction.

従って、第1図及び第3図に示すようにA点と0点とに
向けて噴射された燃料噴nF乃至その混合気Gは、スワ
ールSに流されてキャビティ4の内周壁6に沿ってその
高さh6が最も低い部分へと流れていく。しかしながら
、このとき本案のキャビティ4では、上述したように内
周壁6の高さh6が低くなるに従い棚部7の張出しは大
きくなり、その最低部において棚部7の張出しt2が最
大になってキャビティ4の棚下部は奥深くなっている。
Therefore, as shown in FIGS. 1 and 3, the fuel injection nF or the mixture G injected toward the A point and the 0 point is flowed into the swirl S and flows along the inner circumferential wall 6 of the cavity 4. The height h6 flows to the lowest part. However, in this case, in the cavity 4 of the present invention, as the height h6 of the inner circumferential wall 6 decreases, the overhang of the shelf 7 increases, and the overhang t2 of the shelf 7 becomes maximum at the lowest part, and the cavity The lower part of the 4th shelf is deep.

このため、そのキャビティ4の内周壁高さh6の低い部
分の両側のピストン冠面3上側に強い逆スキッシュが生
じてもキャビティ4内の噴霧・混合気及び火炎等は流出
しにくい状態にあり、その最低部近傍の内周壁高さh6
の低い部分からピストン冠面3の上側への吹きこぼれ鎖
は可及的に抑えられ、その結果スモーク及びHCの排出
量を低減させて出力を増加できるようになる。
Therefore, even if a strong reverse squish occurs above the piston crown surface 3 on both sides of the lower part of the inner peripheral wall height h6 of the cavity 4, the spray, air-fuel mixture, flame, etc. inside the cavity 4 are difficult to flow out. Inner peripheral wall height near the lowest part h6
The spillover chain from the lower part of the piston to the upper side of the piston crown surface 3 is suppressed as much as possible, and as a result, the amount of smoke and HC discharged can be reduced and the output can be increased.

尚、キャビティ4内のスワールSは、吸気ボートからの
吸気により生成され、そのスワールSはキャビティ開口
部5が円形となっているのでキャビティ4内に流入し易
く、その減衰は可及的に抑えられている。また、キャビ
ティ4の棚下部形状は第4図に示すような長円形状とし
ても良く、このように長円形状(または楕円形状)に形
成すると、キャビティ4内に生成されたスワールSは円
形状に旋回しようとするのに対して長軸側の内周壁6は
徐々に離間・近接して変化するのでその長軸部付近でタ
ービュランスが惹起され、ここにマイクロスワール3m
を生じさせて燃料と空気との混合を更に計れるようにな
る。
Note that the swirl S in the cavity 4 is generated by intake air from the intake boat, and since the cavity opening 5 is circular, the swirl S easily flows into the cavity 4, and its attenuation is suppressed as much as possible. It is being Further, the shape of the lower part of the shelf of the cavity 4 may be an oval shape as shown in FIG. As the inner circumferential wall 6 on the long axis side gradually moves away from and approaches the long axis, turbulence is induced near the long axis, and a micro swirl of 3 m is created here.
This makes it possible to further measure the mixing of fuel and air.

[発明の効果] 以上型するに本発明によれば、ペントルーフ形ピストン
の冠面に凹設したキャビティの開口部下の内周壁をピス
トンピン孔の軸方向と直交する方向に窪まぜて拡大形成
したので、キャビティ内周壁高さの低い部分の棚部の張
出しを大きくすることができ、これによりピストン冠面
の上側へと吹きこぼれるキャビティ内の燃料噴霧及び混
合気・火炎の分を可及的に抑えてスモーク・IIC等の
排出量の低減及び出力の向上とを計ることができる。
[Effects of the Invention] To summarize, according to the present invention, the inner circumferential wall below the opening of the cavity recessed in the crown surface of the pent roof piston is enlarged and recessed in a direction perpendicular to the axial direction of the piston pin hole. Therefore, it is possible to increase the overhang of the shelf in the low height part of the cavity inner circumferential wall, thereby reducing as much as possible the fuel spray, air-fuel mixture, and flame inside the cavity that spill over onto the top of the piston crown. It is possible to reduce emissions of smoke, IIC, etc. and improve output.

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

第1図は本発明に係るペントルーフ形ピストンの好適一
実施例を示す平面図、第2図は第1図のII−II線矢
視断面図、第3図は第1図に示すキャビティの内周壁の
展開図、第4図はキャビティの開口部下(棚下)形状の
変形例を示す断面図、第5図は従来のペントルーフ形ピ
ストン゛の平面図、第6図は第5図の側断面図、第7図
は従来のキャビティの展開図である。 図中、1はピストン、2はビス!・ンビン孔、3はピス
トン冠面、4はキャビティ、5は間口部、6は内周壁、
7は棚部である。
FIG. 1 is a plan view showing a preferred embodiment of the pent roof type piston according to the present invention, FIG. 2 is a sectional view taken along the line II-II in FIG. 1, and FIG. FIG. 4 is a sectional view showing a modified example of the shape of the cavity under the opening (below the shelf), FIG. 5 is a plan view of a conventional pent roof piston, and FIG. 6 is a side sectional view of FIG. 5. , FIG. 7 is a developed view of a conventional cavity. In the diagram, 1 is a piston and 2 is a screw!・Piston hole, 3 is the piston crown surface, 4 is the cavity, 5 is the frontage, 6 is the inner peripheral wall,
7 is a shelf.

Claims (3)

【特許請求の範囲】[Claims] (1)ピストン冠面のピストンピン孔直上部をその軸方
向に沿わせて突出させると共にその両側部を傾斜させて
ペントルーフ状に形成し、該ピストン冠面の中央部にピ
ストンピン孔の軸方向と直交する開口部下の内周壁を窪
ませて径方向外方に拡大したキャビティを形成したこと
を特徴とするペントルーフ形ピストン。
(1) The area directly above the piston pin hole on the piston crown surface is made to protrude along its axial direction, and its both sides are sloped to form a pent roof shape, and the piston pin hole is formed in the central part of the piston crown surface in the axial direction. A pent roof type piston characterized by forming a cavity that expands radially outward by recessing the inner circumferential wall below the opening perpendicular to the opening.
(2)上記キャビティが上記ピストンピン孔の軸方向と
直交する方向に長軸を有する長円形状あるいは楕円形状
に形成された上記特許請求の範囲第1項に記載のペント
ルーフ形ピストン。
(2) The pent roof type piston according to claim 1, wherein the cavity is formed in an oval or elliptical shape having a long axis in a direction perpendicular to the axial direction of the piston pin hole.
(3)上記キャビティ開口部がその周縁部に径方向内方
に延出されて真円状に絞られた棚部を有する上記特許請
求の範囲第1項または第2項に記載のペントルーフ形ピ
ストン。
(3) The pent roof type piston according to claim 1 or 2, wherein the cavity opening has a shelf portion extending radially inward and narrowed into a perfect circle at its peripheral edge. .
JP61098107A 1986-04-30 1986-04-30 Pent roof type piston Pending JPS62255521A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61098107A JPS62255521A (en) 1986-04-30 1986-04-30 Pent roof type piston

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61098107A JPS62255521A (en) 1986-04-30 1986-04-30 Pent roof type piston

Publications (1)

Publication Number Publication Date
JPS62255521A true JPS62255521A (en) 1987-11-07

Family

ID=14211102

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61098107A Pending JPS62255521A (en) 1986-04-30 1986-04-30 Pent roof type piston

Country Status (1)

Country Link
JP (1) JPS62255521A (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS567494A (en) * 1979-07-02 1981-01-26 Hitachi Ltd Printed circuit board
JPS58185925A (en) * 1982-04-23 1983-10-29 Hino Motors Ltd Combustion chamber for diesel engine
JPS6198104A (en) * 1984-10-19 1986-05-16 三菱電機株式会社 Gas insulated switchgear

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS567494A (en) * 1979-07-02 1981-01-26 Hitachi Ltd Printed circuit board
JPS58185925A (en) * 1982-04-23 1983-10-29 Hino Motors Ltd Combustion chamber for diesel engine
JPS6198104A (en) * 1984-10-19 1986-05-16 三菱電機株式会社 Gas insulated switchgear

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