JPH0517369B2 - - Google Patents

Info

Publication number
JPH0517369B2
JPH0517369B2 JP61098105A JP9810586A JPH0517369B2 JP H0517369 B2 JPH0517369 B2 JP H0517369B2 JP 61098105 A JP61098105 A JP 61098105A JP 9810586 A JP9810586 A JP 9810586A JP H0517369 B2 JPH0517369 B2 JP H0517369B2
Authority
JP
Japan
Prior art keywords
cavity
piston
crown surface
pent roof
fuel
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 - Lifetime
Application number
JP61098105A
Other languages
Japanese (ja)
Other versions
JPS62255520A (en
Inventor
Naoki Yanagisawa
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 JP61098105A priority Critical patent/JPS62255520A/en
Publication of JPS62255520A publication Critical patent/JPS62255520A/en
Publication of JPH0517369B2 publication Critical patent/JPH0517369B2/ja
Granted 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
    • F02B23/0696W-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 wall
    • 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

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)

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は燃焼室内に直接燃料を噴射供給する直
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ヤビテイ
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 that has a cavity shape recessed in the crown surface of the piston. Concerning an improved pent roof type piston.

[従来の技術] 一般に内燃機関にあつては、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・排気ポートの流路断面積
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] In general, in internal combustion engines, the cross-sectional area of the flow path of the intake and exhaust ports is increased by increasing the diameter of the intake and exhaust valves or by increasing the number of intake and 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・排気ポート
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ツド下面に形成する燃
焼室は、クランク軸の軸線に沿つて中央部分を最
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、かつ直接噴射式デイ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、18〜20という高圧縮比を確保するため
には、実願昭60−143456号に提案した「デイーゼ
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ツドの下面形状に相
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 areas of the intake and exhaust ports are increased in this way, the valve shafts of the intake and 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 upward at 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 In order to ensure this, as shown in ``Diesel Engine Combustion Chamber Structure'' proposed in Utility Application No. 143456/1980, the piston crown surface must be made to correspond to the shape of the bottom surface of the cylinder head, and conversely upwards. It would be necessary to create a pent roof shape with a protruding part.

[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
のキヤビテイが凹設されるが、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ではそのキヤビテイbは横断面が円形に、かつ
その内周壁面cの下端の底部dがピストンリング
溝eに対して平行(t=一定)に形成されてい
た。従つて、そのキヤビテイbの内周壁面cを展
開すると第7図に示すようになつており、キヤビ
テイbの開口の上端縁fは平坦な底部レベルに対
して周方向に沿つて連続的にその高さhbが変化
していた。このため、ペントルーフの屋根方向
(ピストンピン孔gの軸方向)に対してθ=45°を
なす2つの垂直面イ,ロでキヤビテイb内をA,
B,C,Dのエリアに4分割するとこれらの容量
VはVA=VC>VB=VDとなり、それぞれ異な
つていた。また、キヤビテイbの中心位置上方に
配設される噴射ノズルeからはそれら各エリア
A,B,C,D内に相互に90°の角度で同量の燃
料が噴射されるようになつていた。従つて、噴射
ノズルeから噴射された燃料噴霧FがスワールS
に流されてキヤビテイb内を旋回すると、キヤビ
テイ内周壁面cの高さが低く容積の小さなエリア
B,Dでは濃厚な混合気が生成され、一方、キヤ
ビテイ内周壁面cの高さが高く容積の大きなエリ
アA,Cでは稀薄な混合気が生成されてしまい、
キヤビテイb内には部分的に不均一な混合気が生
成されていた。この結果、充分な空気利用を計る
ことができず、多量のスモークの発生を招くと共
に、充分な出力を得られなかつた。
[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, in the conventional pent roof piston a, the cavity b has a circular cross section, and the bottom d at the lower end of the inner circumferential wall c is parallel to the piston ring groove e (t = constant). ) was formed. Therefore, when the inner circumferential wall surface c of the cavity b is developed, it becomes as shown in FIG. The height hb was changing. For this reason, the inside of the cavity b is A, B on two vertical planes A and B that form an angle of θ=45° with respect to the roof direction of the pent roof (the axial direction of the piston pin hole g).
When divided into four areas B, C, and D, the capacities V of these areas were VA=VC>VB=VD, and were different from each other. In addition, the same amount of fuel was injected into each area A, B, C, and D at an angle of 90° from the injection nozzle e located above the center of cavity b. . Therefore, the fuel spray F injected from the injection nozzle e swirls S.
When the air-fuel mixture rotates in cavity b, a rich air-fuel mixture is generated in areas B and D where the height of the inner peripheral wall c of the cavity is low and the volume is small, while on the other hand, the height of the inner peripheral wall c of the cavity is high and the volume is small. A lean mixture is generated in large areas A and C,
A partially non-uniform air-fuel mixture was generated within cavity b. As a result, sufficient air utilization could not be achieved, leading to the generation of a large amount of smoke, and sufficient output could not be obtained.

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、キヤビテイ内の全体に均一な
混合気を生成することができ、もつて空気利用率
を高めてスモークの発生量を低減し得、かつ充分
な出力を得ることができ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 was made in view of the above problems, and its purpose is to be able to generate a uniform air-fuel mixture throughout the cavity, thereby increasing the air utilization rate and reducing the amount of smoke generated. It is an object of the present invention to provide a pent roof type piston for a direct injection internal combustion engine which is capable of achieving sufficient output.

[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、かつその両側部を傾斜させてペ
ントルーフ状に形成し、このピストン冠面の中央
部にピストンの軸方向に沿わせてキヤビテイを凹
設したペントルーフ形ピストンにおいて、上記キ
ヤビテイが、そのキヤビテイ凹設前のピストン冠
面上の各点からほぼ同一深さで形成されているも
のである。
[Means for Solving the Problems] In order to achieve the above object, the present invention protrudes directly above the piston pin hole on the piston crown surface along the axial direction, and both sides thereof are inclined. In a pent-roof type piston that is formed in a pent-roof shape and has a cavity recessed in the center of the piston crown surface along the axial direction of the piston, the cavity is formed from each point on the piston crown surface before the cavity is recessed. They are formed at approximately the same depth.

[作用] 上記構成により、キヤビテイの容積はその円周
方向においてほぼ一様になり、キヤビテイの底面
は、円周方向において波打つように変化する。
[Function] With the above configuration, the volume of the cavity becomes substantially uniform in the circumferential direction, and the bottom surface of the cavity changes in a undulating manner in the circumferential direction.

[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図は直噴式内燃機関に用いるペントルーフ
形ピストンの側断面図であり、第2図はその−
線矢視断面図である。
Figure 1 is a side sectional view of a pent roof type piston used in a direct injection internal combustion engine, and Figure 2 is a side sectional view of the pent roof type piston used in a direct injection internal combustion engine.
It is a sectional view taken along the line.

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)に沿つて
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
ンダヘツドの下面に形成されるシリンダヘツド側
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 that protrudes upward along the axial direction of the piston pin hole 2 (i.e., the crankshaft direction), and both sides thereof are inclined. It is formed into a pent roof shape (roof shape),
Although this pent roof shape is not shown, it corresponds to the shape of the combustion chamber on the cylinder head side, which is formed on the lower surface of 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ツドとによつて実質
的な燃焼室を形成するためのキヤビテイ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、そのキヤビテイ4の開口周縁部5から底部6
までの内周壁面7の高さh7がその周側に亙つて略
均一に形成される。
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. , from the opening periphery 5 to the bottom 6 of the cavity 4
The height h 7 of the inner circumferential wall surface 7 is formed substantially uniformly over its circumferential side.

即ち、本実施例ではキヤビテイ4はその横断面
が円形状に形成されているが、そのキヤビテイ4
の開口周縁部5の高さはピストンリング溝8を基
準にしてそのレベルが周側に沿つて連続的に変化
しており、ピストンピン孔2直上部位置でのレベ
ルが最高になり、その両側90°位置でのレベルが
最低になつている。そしてキヤビテイ4の内周壁
面7は第4図の展開図にも示すようにその高さh7
が周側に沿つて均一に形成され、これにより底部
6は開口周縁部5の高さのレベル変動に合わせて
平行とされ波打形状になつている。
That is, in this embodiment, the cavity 4 has a circular cross section;
The height of the opening periphery 5 changes continuously along the circumference with the piston ring groove 8 as a reference, and the level is highest at the position directly above the piston pin hole 2, and the level on both sides thereof is the highest. The level at the 90° position is the lowest. The inner peripheral wall surface 7 of the cavity 4 has a height h 7 as shown in the developed view of FIG.
are formed uniformly along the circumferential side, so that the bottom portion 6 is parallel to the level variation of the height of the opening peripheral portion 5 and has a wavy shape.

一方、第3図に示すように、キヤビテイ4の略
中心部の上方には、シリンダヘツドに取付けられ
てキヤビテイ4内に燃料を噴射する噴射ノズル9
が配設される。この噴射ノズル9は、キヤビテイ
4の内周壁面7に臨んで斜め下方に方向づけられ
て開口された4つの噴口(図示せず)を有してお
り、かつその各噴口は、ピストンピン孔2の軸心
に対して45°をなす2つの垂直面イ,ロで区分さ
れるキヤビテイ4内の4つのエリアA,B,C,
D内のスワールS上流側に、相互に90°の角度を
なしてそれぞれ同量の燃料を噴射供給するように
なつている。
On the other hand, as shown in FIG. 3, above the approximate center of the cavity 4 is an injection nozzle 9 that is attached to the cylinder head and injects fuel into the cavity 4.
will be placed. The injection nozzle 9 has four injection ports (not shown) facing the inner circumferential wall surface 7 of the cavity 4 and opening diagonally downward. Four areas A, B, C,
The same amount of fuel is injected and supplied to the upstream side of the swirl S in D at an angle of 90 degrees to each other.

従つて、第3図及び第4図に示すように、キヤ
ビテイ4内の各エリアA,B,C,Dにそれぞれ
噴射された燃料噴霧F及びその混合気Gは、スワ
ールSに流されてキヤビテイ4の内周壁面7に沿
つて旋回するが、このとき本案のキヤビテイ4で
は、上述したように内周壁面7の高さh7がその周
側に沿つて均一に形成されているため、開口周縁
部5の高さレベルが高い部分のエリアA,Cと、
低い部分のエリアB,Dとの容積VA,VB,
VC,VDは全て同一になつている。
Therefore, as shown in FIGS. 3 and 4, the fuel spray F and its mixture G injected into each area A, B, C, and D in the cavity 4 are flowed into the swirl S and sent to the cavity. At this time, in the cavity 4 of the present invention, since the height h7 of the inner peripheral wall surface 7 is formed uniformly along its peripheral side as described above, the opening Areas A and C where the height level of the peripheral portion 5 is high,
The volume of the lower part with areas B and D is VA, VB,
VC and VD are all the same.

このため、各エリアA,B,C,D内に存在す
る空気量は等しく、その結果各エリアA,B,
C,D内に生成される混合気Gの濃度が略等しく
なつて、キヤビテイ4内には全体として濃度の等
しい混合気Gを略均一に存在させることができる
ようになる。これにより、空気利用率が向上され
てスモークの発生量が可及的に抑えられ、かつ出
力の増大を計れるようになる。
Therefore, the amount of air existing in each area A, B, C, and D is equal, and as a result, each area A, B,
The concentrations of the air-fuel mixtures G generated in C and D are approximately equal, so that the air-fuel mixture G having the same concentration as a whole can be uniformly present in the cavity 4. As a result, the air utilization rate is improved, the amount of smoke generated is suppressed as much as possible, and the output can be increased.

また、キヤビテイ4の底部6が波打たされた形
状となつているため、キヤビテイ4内に生成され
るスワールSにはその流れ方向に対して底部6が
下降する部分6aに縦方向のマイクロスワールS
を発生させることができ、燃料と空気との混合を
更に良好にすることができる。
Moreover, since the bottom part 6 of the cavity 4 has a wavy shape, the swirl S generated in the cavity 4 has a vertical micro-swirl in the part 6a where the bottom part 6 descends with respect to the flow direction. S
can be generated, making it possible to further improve the mixing of fuel and air.

尚、キヤビテイ4内のスワールSは、吸気ポー
トからの吸気によつて生成される。
Note that the swirl S in the cavity 4 is generated by intake air from the intake port.

[発明の効果] 以上要するに本発明によれば、次の如き優れた
効果を発揮する。
[Effects of the Invention] In summary, according to the present invention, the following excellent effects are achieved.

(1) キヤビテイ内をその周方向に沿つて同角度で
複数のエリアに区分してもその各エリアの容積
を同一にすることができる。
(1) Even if the inside of the cavity is divided into a plurality of areas at the same angle along the circumferential direction, the volume of each area can be made the same.

(2) その結果その各エリア毎に同量の燃料を噴射
供給してもキヤビテイ内にはその全体として略
均一な混合気を存在させることが可能になつ
て、空気利用率を高めてスモークの発生量を可
及的に低減させると共に出力の増大を計れるよ
うになる。
(2) As a result, even if the same amount of fuel is injected and supplied to each area, it is possible to maintain a substantially uniform air-fuel mixture within the cavity as a whole, increasing the air utilization rate and reducing smoke. It becomes possible to reduce the amount of generation as much as possible and increase the output.

(3) スワールの流れ方向に対してキヤビテイ底部
の下降する部分に縦方向のマイクロスワールを
発生させることができ、燃料と空気との混合を
更に良好となすことができる。
(3) Vertical microswirls can be generated in the descending portion of the bottom of the cavity with respect to the flow direction of the swirl, making it possible to achieve even better mixing of fuel and air.

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

第1図は本発明に係るペントルーフ形ピストン
の側断面図、第2図は第1図の−線矢視側断
面図、第3図はピストン冠面の平面図、第4図は
キヤビテイ内周壁の展開図、第5図は従来のピス
トン冠面の平面図、第6図は第5図の−線矢
視断面図、第7図は従来のキヤビテイ内周壁面の
展開図である。 図中、1はピストン、2はピストンピン孔、3
はピストン冠面、4はキヤビテイ、5は開口周縁
部、6は底部、7は内周壁面、h7は内周壁面の高
さである。
Fig. 1 is a side sectional view of a pent roof type piston according to the present invention, Fig. 2 is a side sectional view taken from the - line arrow in Fig. 1, Fig. 3 is a plan view of the crown surface of the piston, and Fig. 4 is a cavity inner peripheral wall. FIG. 5 is a plan view of a conventional piston crown surface, FIG. 6 is a sectional view taken along the line -- in FIG. 5, and FIG. 7 is a developed view of a conventional inner peripheral wall surface of a cavity. In the figure, 1 is a piston, 2 is a piston pin hole, and 3 is a piston.
is the piston crown surface, 4 is the cavity, 5 is the opening periphery, 6 is the bottom, 7 is the inner peripheral wall surface, and h7 is the height of the inner peripheral wall surface.

Claims (1)

【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、かつその両側部を傾
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の軸方向に沿わせてキヤビ
テイを凹設したペントルーフ形ピストンにおい
て、上記キヤビテイが、そのキヤビテイ凹設前の
ピストン冠面上の各点からほぼ同一深さで形成さ
れていることを特徴とするペントルーフ形ピスト
ン。
1. The piston crown surface directly above the piston pin hole protrudes along its axial direction, and its both sides are sloped to form a pent roof shape, and the piston crown surface extends along the axial direction of the piston at the center of the piston crown surface. A pent roof type piston having a recessed cavity, characterized in that the cavity is formed at approximately the same depth from each point on the crown surface of the piston before the cavity is recessed.
JP61098105A 1986-04-30 1986-04-30 Pent roof type piston Granted JPS62255520A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61098105A JPS62255520A (en) 1986-04-30 1986-04-30 Pent roof type piston

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61098105A JPS62255520A (en) 1986-04-30 1986-04-30 Pent roof type piston

Publications (2)

Publication Number Publication Date
JPS62255520A JPS62255520A (en) 1987-11-07
JPH0517369B2 true JPH0517369B2 (en) 1993-03-09

Family

ID=14211046

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61098105A Granted JPS62255520A (en) 1986-04-30 1986-04-30 Pent roof type piston

Country Status (1)

Country Link
JP (1) JPS62255520A (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
MX174016B (en) * 1989-06-29 1994-04-14 Orbital Eng Pty INTERNAL COMBUSTION ENGINE
JP4757112B2 (en) 2006-06-26 2011-08-24 本田技研工業株式会社 Direct fuel injection diesel engine
JP4929012B2 (en) * 2007-04-06 2012-05-09 本田技研工業株式会社 Direct fuel injection engine
US8474431B2 (en) 2007-04-06 2013-07-02 Honda Motor Co., Ltd. Direct fuel-injected engine
JP4929013B2 (en) * 2007-04-06 2012-05-09 本田技研工業株式会社 Direct fuel injection engine
JP4879873B2 (en) * 2007-12-21 2012-02-22 本田技研工業株式会社 Direct fuel injection engine
WO2014106904A1 (en) * 2013-01-07 2014-07-10 トヨタ自動車株式会社 Internal combustion engine
US20150361867A1 (en) * 2013-01-31 2015-12-17 Toyota Jidosha Kabushiki Kaisha Internal combustion engine

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5233242A (en) * 1975-09-05 1977-03-14 Howaldtswerke Deutsche Werft Float crane with unloadable main jib
JPS5832919A (en) * 1981-08-20 1983-02-26 Nissan Motor Co Ltd Direct injection type diesel engine

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5996323U (en) * 1982-12-18 1984-06-29 マツダ株式会社 engine combustion chamber

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5233242A (en) * 1975-09-05 1977-03-14 Howaldtswerke Deutsche Werft Float crane with unloadable main jib
JPS5832919A (en) * 1981-08-20 1983-02-26 Nissan Motor Co Ltd Direct injection type diesel engine

Also Published As

Publication number Publication date
JPS62255520A (en) 1987-11-07

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