JPS6032929A - Combustion chamber of direct-injection type internal- combustion engine - Google Patents
Combustion chamber of direct-injection type internal- combustion engineInfo
- Publication number
- JPS6032929A JPS6032929A JP58141101A JP14110183A JPS6032929A JP S6032929 A JPS6032929 A JP S6032929A JP 58141101 A JP58141101 A JP 58141101A JP 14110183 A JP14110183 A JP 14110183A JP S6032929 A JPS6032929 A JP S6032929A
- Authority
- JP
- Japan
- Prior art keywords
- combustion chamber
- recess
- piston
- direct
- combustion engine
- 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.)
- Granted
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 40
- 238000002347 injection Methods 0.000 title claims abstract description 24
- 239000007924 injection Substances 0.000 title claims abstract description 24
- 239000000446 fuel Substances 0.000 claims abstract description 28
- 239000007921 spray Substances 0.000 claims abstract description 15
- 239000000779 smoke Substances 0.000 abstract description 6
- 239000000567 combustion gas Substances 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000003111 delayed effect Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0696—W-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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0648—Means or methods to improve the spray dispersion, evaporation or ignition
- F02B23/0651—Means or methods to improve the spray dispersion, evaporation or ignition the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0669—Details related to the fuel injector or the fuel spray having multiple fuel spray jets per injector nozzle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0672—Omega-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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/14—Direct injection into combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0618—Other 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
- F02B23/0624—Swirl flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Abstract
Description
【発明の詳細な説明】
本発明はピストン頂部に四部の主燃料室を有する直噴式
内燃機関の燃焼室に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a combustion chamber for a direct injection internal combustion engine having four main fuel chambers at the top of the piston.
従来、一般の直噴式内燃機関の燃焼室は、第1図の側断
面図及び第2図の平面図に示すごとく、ピストン1の頂
部に四部2の主燃焼室を有するトロイダル形のものが使
用されておシ、同一のシリンダ内径りに対して、この四
部2の径をdlとする谷径の比を、dz/D=0.45
〜0055にするのが通常であシ、また、この四部2の
内壁面は垂直方向に対して、dθ=θ°〜7°位に傾斜
するように設定されている。Conventionally, the combustion chamber of a general direct-injection internal combustion engine has been of a toroidal type, which has a main combustion chamber of four parts 2 at the top of a piston 1, as shown in the side cross-sectional view of Fig. 1 and the plan view of Fig. 2. Then, for the same cylinder inner diameter, the ratio of the valley diameter, where the diameter of these four parts 2 is dl, is dz/D=0.45.
The inner wall surface of the four parts 2 is set to be inclined at about dθ=θ° to 7° with respect to the vertical direction.
しかしながら、この内燃機関の低速・低力時においても
、燃料噴射弁6の各噴口からの燃料噴霧Fは圧縮行程の
末期の圧縮条件においても、ピストン1の四部2の内壁
面に衝突するが、その際、壁面温度が低いので、燃料蒸
発が遅れ、燃焼が完全に行なわれずに青白煙や排気刺激
臭を発生するという問題がある。However, even at low speed and low power of this internal combustion engine, the fuel spray F from each nozzle of the fuel injection valve 6 collides with the inner wall surface of the four parts 2 of the piston 1 even under compression conditions at the end of the compression stroke. At this time, since the wall surface temperature is low, fuel evaporation is delayed, and combustion is not completed completely, resulting in the generation of blue-white smoke and a pungent odor from the exhaust.
そこで本発明は、前記従来の問題点を解消し、直噴式内
燃機関の低速・低力時における青白煙及び排気刺激臭を
改善してその機関性能の向」二をはかることを目的とし
てなされたものである。SUMMARY OF THE INVENTION Therefore, the present invention has been made to solve the above-mentioned conventional problems and to improve the performance of direct injection internal combustion engines by improving the blue-white smoke and irritating exhaust odor at low speeds and low power. It is something.
即ち、本発明はピストン頂部に凹部の主燃焼室を有する
直噴式内燃機関において、その四部を、底部の直径よシ
上部の直径が小さなきんぢやく状の回転体形状に形成す
ると共に、燃料噴射弁の各噴口から噴射される燃料の燃
料噴霧妙;衝突する四部の壁面に各燃料噴霧がほぼ直角
に衝突するような半円柱形状で、かつ上部が広がった形
状になる小凹部をそれぞれ形成したことを特徴としたも
のである。That is, the present invention provides a direct-injection internal combustion engine having a main combustion chamber with a concave portion at the top of the piston, in which the four parts are formed into the shape of an acrylic rotating body whose diameter at the top is smaller than the diameter at the bottom, and at which the fuel injection The fuel spray of the fuel injected from each nozzle of the valve is strange; each of the fuel sprays collides with the walls of the four colliding parts at almost right angles, forming a semi-cylindrical shape, and a small concave part with a widened top. It is characterized by this.
以下図面を参照して本発明の一実施例を説明するが、第
3図は本発明の実施例における直噴式内燃機関の燃焼室
を示す側断面図、第4図は第3図の平面図である。An embodiment of the present invention will be described below with reference to the drawings. FIG. 3 is a side sectional view showing a combustion chamber of a direct injection internal combustion engine in an embodiment of the present invention, and FIG. 4 is a plan view of FIG. 3. It is.
まず、この直噴式内燃機関は第3図に示すごとく、ピス
トン1の頂部に四部2の主燃焼室を有しておシ、この四
部2は、底部の直径d3 よシ上部の直径d2がd3
) dzのごとく小さくなった四部2の中心を軸とした
きんちゃく状の回転体形状に形成されている。First, as shown in Fig. 3, this direct injection internal combustion engine has a main combustion chamber of four parts 2 at the top of a piston 1, and these four parts 2 have a diameter d3 at the bottom and a diameter d2 at the top d3.
) It is formed in the shape of a revolving body centered on the center of the four parts 2 which have become smaller like dz.
次に、第4図のごとく燃料噴射弁6の各噴口から噴射さ
れる矢印Fで示す燃料噴霧がこの凹部2内に噴射された
時、はぼ直角に衝突するような半円柱形状で、かつその
上部が広がった形状になる小凹部4を各噴口に対応した
数だけこの四部2に形成している。Next, as shown in FIG. 4, when the fuel spray indicated by the arrow F injected from each nozzle of the fuel injection valve 6 is injected into this recess 2, it forms a semi-cylindrical shape such that it collides at approximately right angles, and A number of small recesses 4 whose upper portions are widened are formed in the four parts 2 in a number corresponding to each nozzle.
上記の小凹部4を設ける際には、内燃機関の低速・低力
時に噴射された燃料噴霧Fの噴射角θ4=10〜20°
より若干大きい小口部4を形成すると共に、燃料噴霧F
が小凹部4の壁面に付着することなしに完全燃焼する適
正な距離4=0.25〜0.35×Dを保つようにして
いる。When providing the above-mentioned small recess 4, the injection angle θ4 of the fuel spray F injected at low speed and low power of the internal combustion engine is 10 to 20 degrees.
While forming a slightly larger small mouth portion 4, the fuel spray F
An appropriate distance 4 = 0.25 to 0.35 x D is maintained for complete combustion without adhering to the wall surface of the small recess 4.
そのためには、ピストン1の上面の距離lの点と四部2
の底部の直径d3の点との間に半径R4の切削工具によ
る半円柱形状の小凹部4を形成するが、この小口部4の
第3図に示す壁面は燃料噴霧Fの噴射方向にほぼ直角、
例えばθ3=90°〜95°に形成される。To do this, we need to connect the point at distance l on the top surface of piston 1 and the fourth part 2.
A small semi-cylindrical recess 4 is formed by a cutting tool with a radius R4 between the bottom and a point with a diameter d3, and the wall surface of this small opening 4 shown in FIG. ,
For example, θ3 is formed at 90° to 95°.
以上の構成からなる本発明の燃焼室において、ピストン
1の四部2内に噴射される燃料噴霧Fは、機藺の低速・
低力時には第5図のごとく、矢印Sで示すスワール速度
は小さいので、殆んど直進するが、本発明では小凹部4
が形成されているので、小凹部4内壁面4A到着までに
燃焼し、燃料噴霧Fの先端部の火炎が若干ふれる程度と
なシ、完全燃焼して青白煙及び排気刺激臭を発すること
がなくなる。In the combustion chamber of the present invention having the above configuration, the fuel spray F injected into the four parts 2 of the piston 1 is
When the force is low, as shown in Fig. 5, the swirl speed indicated by the arrow S is small, so it travels almost straight, but in the present invention, the small recess 4
is formed, the fuel will burn by the time it reaches the inner wall surface 4A of the small recess 4, and the flame at the tip of the fuel spray F will touch a little, but it will burn completely and will not emit blue-white smoke or irritating exhaust odor. .
また、機関の高速・高負荷時には、第6図に示すように
凹部2内に噴射された燃料噴霧Fは、凹部2内に流入し
た矢印Sの強いスワールによシ曲げられ々がら、第7図
に示すように小口部4の内壁面の溝状部にその大部分が
衝突する。Furthermore, when the engine is at high speed and under high load, the fuel spray F injected into the recess 2 is bent by the strong swirl indicated by the arrow S flowing into the recess 2, as shown in FIG. As shown in the figure, most of it collides with the groove-shaped portion on the inner wall surface of the edge portion 4.
そこで、上記燃料噴射中にもピストン1は上死点方向に
移行し、ピストン1の上面での従来よシ強いスキッシュ
力を発生し、かつスワールSと合成された気流は第8図
に示すように各小凹部4よシ凹部2内に流入し、第6図
及び第7図に示すごとく、小凹部4における燃料噴霧F
を斜め下向きに強く流し、気化あるいは空気と微粒燃料
などの混合を良好にする。Therefore, even during the above fuel injection, the piston 1 moves toward the top dead center, generating a stronger squish force than before on the upper surface of the piston 1, and the airflow combined with the swirl S is as shown in FIG. As shown in FIG. 6 and FIG.
Flows strongly diagonally downward to improve vaporization or mixing of air and particulate fuel.
更に、小口部4のスワールSの上流側の壁面の段差4B
で空気の乱れを与え、さらに下流側の壁面の段差4Cで
燃料と空気と未燃焼ガスに強い乱れを与えつつ、回転体
に形成されたきんちやく状の四部2内にて旋回して良好
な燃焼をする。Furthermore, a step 4B on the wall surface on the upstream side of the swirl S of the edge portion 4
gives turbulence to the air, and while giving strong turbulence to the fuel, air, and unburned gas at the step 4C on the downstream wall, it rotates within the cinquette-shaped four parts 2 formed on the rotating body, making it good. combustion.
ここで、このように開口部の直径d2が第1図の従来例
の直径d1よシも小さなきんちゃく状の四部2にするこ
とによシ、スキッシュ力は従来のトロイダル形の四部2
からなる燃焼室よりも拡大されることになる。Here, by forming the toroidal-shaped four parts 2 in which the diameter d2 of the opening is smaller than the diameter d1 of the conventional example shown in FIG.
The combustion chamber will be larger than the combustion chamber consisting of
更に、ピストン1が上死点より下降しはじめると、上記
の四部2内の一部未燃ガス、またはカーボンを含む燃焼
ガスは逆スキツシュカのため小口部4からピストン1の
上面に第9図のごとく流出する。Furthermore, when the piston 1 begins to descend from the top dead center, some of the unburned gas or the combustion gas containing carbon in the four parts 2 is reversed, so that it flows from the mouth part 4 to the upper surface of the piston 1 as shown in FIG. It leaks out.
この場合、例えば本実施例のごとく4個の噴口を有する
燃料噴射弁6の場合、4個の小凹部4よシ燃焼ガスがそ
れぞれ扇形に広がシ、相互に乱れが発生し、ピストン1
上面の空気利用率が向上し、燃焼が良好になシ、カーボ
ン発生などが改善され、特に噴射時期を遅くして筒内最
高圧を低くしても燃焼が良好になる3、なお、小凹部壁
とd2+ a3で形成されている壁とのつなぎ部は、熱
負荷低減のため若干の面取りを行なう場合がある。In this case, for example, in the case of the fuel injection valve 6 having four nozzles as in this embodiment, the combustion gas spreads out in a fan shape through the four small recesses 4, causing mutual turbulence and causing the piston 1
The air utilization rate on the upper surface is improved, resulting in better combustion, and carbon generation is improved, resulting in better combustion even when the injection timing is delayed and the maximum pressure in the cylinder is lowered. The joint between the wall and the wall formed by d2+a3 may be slightly chamfered to reduce the heat load.
従って、本発明を適用した直噴式内燃機関の燃焼室では
、低速・低力時における青白煙及び排気刺激臭をなくす
る上で有効であると共に、燃焼室内のスキッシュ力を拡
大し、燃料噴霧と空気などの混合を良好にして、燃焼性
能を向上させうるという効果がある。Therefore, in the combustion chamber of a direct injection internal combustion engine to which the present invention is applied, it is effective in eliminating blue-white smoke and irritating exhaust odor at low speeds and low power, and it also expands the squish force in the combustion chamber and improves fuel spray. It has the effect of improving combustion performance by improving mixing of air and the like.
特に、本発明は直接噴射式ディーゼル機関等に対して有
効に適用することができる。In particular, the present invention can be effectively applied to direct injection diesel engines and the like.
第1図は従来の直噴式内燃機関の燃焼室の側断面図、第
2図は第1図の平面図、第3図は本発明の実施例1にお
ける直噴式内燃機関の燃焼室を示す側断面図、第4図は
第3図の平面図、第5図及び第6図は第4図の小凹部の
要部拡大平面図、第7図は第6図の小凹部の要部斜視側
面図、第8図は第4図のピストン上面のピストン上死点
方向移行時の気流を示す平面図、第9図は第4図のピス
トン上面のピストン下降開始後の燃焼ガスを示す平面図
である。
1・・・ピストン、2・・・凹部、6・・・燃料噴射弁
14・・・小凹部、F・・・燃料噴霧。
代理人 弁理士 小 川 信 −
弁理士 野 口 賢 照
弁理士 斎 下 和 彦
第1図
第5図 第6図
第7図
第8図 第9図FIG. 1 is a side sectional view of a combustion chamber of a conventional direct injection internal combustion engine, FIG. 2 is a plan view of FIG. 1, and FIG. 3 is a side view showing a combustion chamber of a direct injection internal combustion engine in Embodiment 1 of the present invention 4 is a plan view of FIG. 3, FIGS. 5 and 6 are enlarged plan views of the main part of the small recess shown in FIG. 4, and FIG. 7 is a perspective side view of the main part of the small recess shown in FIG. 6. 8 is a plan view showing the airflow on the top surface of the piston in FIG. 4 when the piston moves toward the top dead center, and FIG. 9 is a plan view showing the combustion gas on the top surface of the piston in FIG. 4 after the piston starts to descend. be. DESCRIPTION OF SYMBOLS 1... Piston, 2... Recessed part, 6... Fuel injection valve 14... Small recessed part, F... Fuel spray. Agent Patent Attorney Shin Ogawa - Patent Attorney Masaru Noguchi Patent Attorney Kazuhiko Saishita Figure 1 Figure 5 Figure 6 Figure 7 Figure 8 Figure 9
Claims (1)
において、その凹部を、底部の直径よシ上部の直径が小
さなきんちゃく状の回転体形状に形成すると共に、燃料
噴射弁の各噴口から噴射される燃料の燃料噴霧が衝突す
る四部の壁面に各燃料噴霧がほぼ直角に衝突するような
半円柱形状で、かつ上部が広がった形状になる小凹部を
それぞれ形成したことを特徴とする直噴式内燃機関の燃
焼室。In a direct-injection internal combustion engine that has four main combustion chambers at the top of the piston, the concave part is formed in the shape of a rotating body with a smaller diameter at the top than at the bottom, and the fuel is injected from each nozzle of the fuel injection valve. A direct-injection internal combustion engine characterized in that each of the four wall surfaces on which the fuel spray collides is formed with a semi-cylindrical shape such that each fuel spray collides at a nearly right angle, and a small concave part with a widened upper part. combustion chamber of the engine.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58141101A JPS6032929A (en) | 1983-08-03 | 1983-08-03 | Combustion chamber of direct-injection type internal- combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP58141101A JPS6032929A (en) | 1983-08-03 | 1983-08-03 | Combustion chamber of direct-injection type internal- combustion engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6032929A true JPS6032929A (en) | 1985-02-20 |
JPH0147606B2 JPH0147606B2 (en) | 1989-10-16 |
Family
ID=15284208
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP58141101A Granted JPS6032929A (en) | 1983-08-03 | 1983-08-03 | Combustion chamber of direct-injection type internal- combustion engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6032929A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0214423U (en) * | 1988-07-11 | 1990-01-30 | ||
JPH0387823U (en) * | 1989-12-21 | 1991-09-06 | ||
US6732703B2 (en) | 2002-06-11 | 2004-05-11 | Cummins Inc. | Internal combustion engine producing low emissions |
EP1528233A1 (en) * | 2003-11-03 | 2005-05-04 | Renault s.a.s. | Piston for a combustion chamber for reducing soot emission |
US7210448B2 (en) | 2002-06-11 | 2007-05-01 | Cummins, Inc. | Internal combustion engine producing low emissions |
US8677970B2 (en) | 2011-03-17 | 2014-03-25 | Cummins Intellectual Property, Inc. | Piston for internal combustion engine |
WO2018168692A1 (en) * | 2017-03-17 | 2018-09-20 | マツダ株式会社 | Diesel engine |
-
1983
- 1983-08-03 JP JP58141101A patent/JPS6032929A/en active Granted
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0214423U (en) * | 1988-07-11 | 1990-01-30 | ||
JPH0387823U (en) * | 1989-12-21 | 1991-09-06 | ||
US6732703B2 (en) | 2002-06-11 | 2004-05-11 | Cummins Inc. | Internal combustion engine producing low emissions |
US6966294B2 (en) | 2002-06-11 | 2005-11-22 | Cummins Inc. | Internal combustion engine producing low emissions |
US7210448B2 (en) | 2002-06-11 | 2007-05-01 | Cummins, Inc. | Internal combustion engine producing low emissions |
EP1528233A1 (en) * | 2003-11-03 | 2005-05-04 | Renault s.a.s. | Piston for a combustion chamber for reducing soot emission |
FR2861809A1 (en) * | 2003-11-03 | 2005-05-06 | Renault Sas | PISTON FOR COMBUSTION CHAMBER FOR REDUCING SOOT EMISSIONS |
US8677970B2 (en) | 2011-03-17 | 2014-03-25 | Cummins Intellectual Property, Inc. | Piston for internal combustion engine |
USRE46806E1 (en) | 2011-03-17 | 2018-04-24 | Cummins Intellectual Property, Inc. | Piston for internal combustion engine |
WO2018168692A1 (en) * | 2017-03-17 | 2018-09-20 | マツダ株式会社 | Diesel engine |
Also Published As
Publication number | Publication date |
---|---|
JPH0147606B2 (en) | 1989-10-16 |
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