JPH05149137A - Piston and setting of fuel injection direction - Google Patents

Piston and setting of fuel injection direction

Info

Publication number
JPH05149137A
JPH05149137A JP3332889A JP33288991A JPH05149137A JP H05149137 A JPH05149137 A JP H05149137A JP 3332889 A JP3332889 A JP 3332889A JP 33288991 A JP33288991 A JP 33288991A JP H05149137 A JPH05149137 A JP H05149137A
Authority
JP
Japan
Prior art keywords
piston
combustion chamber
fuel injection
injection
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.)
Pending
Application number
JP3332889A
Other languages
Japanese (ja)
Inventor
Masamichi Tanaka
正道 田中
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.)
Komatsu Ltd
Original Assignee
Komatsu 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 Komatsu Ltd filed Critical Komatsu Ltd
Priority to JP3332889A priority Critical patent/JPH05149137A/en
Publication of JPH05149137A publication Critical patent/JPH05149137A/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
    • F02B23/0696W-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
    • F02B23/0645Details 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

PURPOSE:To set and define the cooling position by way of adjusting the direction of fuel spray in consideration of the fact that fuel is cooled by heat of vaporization of the fuel. CONSTITUTION:In case of cooling a combustion chamber 2 of a piston 1 of direct injection type of a diesel engine, at least one of injections from a nozzle hole 4 of a fuel injection nozzle is injected to margins 6 of the combustion chamber 2 right above a piston pin shaft 5. consequently, the injected margin 6 of the combustion chamber 2 is cooled, and accordingly, it is possible to prevent occurrence of cracking and others previously occurred.

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4サイクルディ−ゼル機
関のピストンの燃焼室と燃料噴射ノズルの噴霧による冷
却に係り、詳しくは噴射弁の噴射方向の設定方法に関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to cooling by spraying a combustion chamber of a piston and a fuel injection nozzle of a four-cycle diesel engine, and more particularly to a method of setting an injection direction of an injection valve.

【0002】[0002]

【従来の技術】ディ−ゼル機関の排気エミッション低減
における燃焼の改善において、リエンラント形の燃焼室
はその主流をなす燃焼室形状となっている。しかしなが
らリエントラント形の燃焼室においても、燃焼室とピス
トン上面とでなす周縁部は温度上昇を伴うのでその耐久
性や信頼性が懸念される。そのために従来から温度低減
手段を講じているが、これには ピストンの燃焼室下面
のオイル冷却、例えば実開昭60−116021号公報
によるもの、 リム部冷却空洞によるオイル冷却等の種
々の対応策が考えられてきた。
2. Description of the Related Art In improving combustion in reducing exhaust emission of a diesel engine, a reentrant type combustion chamber has a main combustion chamber shape. However, even in a reentrant type combustion chamber, the peripheral edge formed by the combustion chamber and the upper surface of the piston is accompanied by a temperature rise, and therefore its durability and reliability are concerned. For that purpose, a temperature reducing means has been conventionally adopted, but various measures such as oil cooling of the lower surface of the combustion chamber of the piston, for example, according to Japanese Utility Model Publication No. 60-116021, oil cooling by a rim cooling cavity, etc. Has been considered.

【0003】[0003]

【発明が解決しようとする課題】しかしこれらの冷却で
は、ピストン上面近くの燃焼室部分、すなわち、周縁部
は前記冷却から離れているため冷却効果が薄れてしま
う。一方、燃焼性能の面からは周縁部はよりシャ−プな
形状が求められており、信頼性や耐久性の点で相反する
ことになる。したがって周縁部の冷却は特に必要である
が従来、上記のような理由で不可能であった。また、一
般に燃焼室周縁部の亀裂は燃焼室とバルブリセス(逃
げ)の交差部や、周縁部のピストンピン方向に引張応力
(亀裂につながる)が、直交方向には圧縮応力が発生す
るため、各々のピストンにおいて冷却部位を限定する必
要があった。
However, in these types of cooling, since the combustion chamber portion near the upper surface of the piston, that is, the peripheral portion is separated from the cooling, the cooling effect is weakened. On the other hand, in terms of combustion performance, the peripheral portion is required to have a sharper shape, which conflicts with respect to reliability and durability. Therefore, cooling of the peripheral portion is particularly necessary, but conventionally it has been impossible for the above reasons. In general, cracks in the periphery of the combustion chamber cause tensile stress (which leads to cracks) in the intersection of the combustion chamber and valve recess (relief) and in the direction of the piston pin in the periphery, but compressive stress occurs in the orthogonal direction. It was necessary to limit the cooling area in the piston.

【0004】本発明はピストン冷却にはオイルを用いる
以外に燃料の気化熱による冷却があるところから、噴射
され噴霧の当たる部分は気化され、気化熱により冷却さ
れることに着目して噴霧の方向を調整し、冷却位置を限
定することのできるピストンと燃料噴射方向の設定方法
を提供して従来技術の持つ欠点の解消を図ることを目的
としてなされたものである。
In the present invention, in addition to the use of oil for cooling the piston, there is cooling by the heat of vaporization of the fuel. Therefore, paying attention to the fact that the portion where the spray is hit is vaporized and cooled by the heat of vaporization The purpose of this invention is to solve the drawbacks of the prior art by providing a piston and a method of setting the fuel injection direction that can limit the cooling position.

【0005】[0005]

【課題を解決するための手段および作用】上記従来技術
の問題点を解決する手段として本発明はディ−ゼル機関
の直接噴射方式におけるピストン燃焼室の冷却におい
て、燃料噴射ノズルの噴孔からの噴射のうち、少なくと
も1つはピストンピン軸の真上の燃焼室周縁に噴射され
るようにしたことを特徴とする。
As a means for solving the above-mentioned problems of the prior art, the present invention is directed to injection from a nozzle hole of a fuel injection nozzle in cooling a piston combustion chamber in a direct injection system of a diesel engine. At least one of them is characterized in that it is injected into the periphery of the combustion chamber just above the piston pin axis.

【0006】[0006]

【実施例】図1乃至図6は本発明のピストンと燃料噴射
方向の設定方法の一実施例を示し、図7乃至図12は本
発明の他の実施例を示す。
1 to 6 show an embodiment of a method of setting a piston and a fuel injection direction according to the present invention, and FIGS. 7 to 12 show another embodiment of the present invention.

【0007】本発明はディ−ゼル機関の直接噴射方式に
おけるピストン1燃焼室2の冷却において、燃料噴射ノ
ズル3の噴孔4からの噴射のうち、少なくとも1つはピ
ストンピン軸5の真上の燃焼室周縁6に噴射されるよう
にした方法である。
According to the present invention, in cooling the piston 1 combustion chamber 2 in the direct injection system of a diesel engine, at least one of the injections from the injection holes 4 of the fuel injection nozzle 3 is directly above the piston pin shaft 5. In this method, the fuel is injected to the peripheral edge 6 of the combustion chamber.

【0008】図1は4バルブでピストン1の中心とリエ
ントラント型またはトロイダル型の燃焼室2の中心とが
一致している場合の噴射ノズル3の噴孔4からの噴射を
示したものである。図2以下に噴孔4の個数の違いによ
る噴射方法(設定)を順に示す。図2は図1における燃
料噴射ノズル3の噴孔4が4個ある場合を示し、この場
合は少なくとも噴孔4のうち、2個が点線で示すピスト
ンピン軸5の真上にあるため、2個所の噴射方向の設定
が可能である。図3は図1における燃料噴射ノズル3の
噴孔4が5個ある場合を示し、この場合はピストンピン
軸5の真上にある噴孔4は1個のみの設定となり排気バ
ルブ側を優先している。図4は同様に燃料噴射ノズル3
の噴孔4が6個ある場合を示し、この場合は偶数である
から、図2と同様2個所の噴射方向の設定が可能であ
る。図5は燃料噴射ノズル3の噴孔4が7個ある場合を
示し、この場合は奇数であるから、図3と同様1個のみ
の設定となる。図6は燃料噴射ノズル3の噴孔4が8個
ある場合を示し、この場合は偶数であるから、2ヵ所の
噴射方向の設定が可能である。したがって噴孔4が偶数
の場合は2個所、奇数の場合は1個所となるが、ピスト
ンピン軸5と交差する燃焼室周縁6部分の冷却が可能と
なる。各図において7は排気バルブの逃げで7´は吸気
バルブの逃げでありピストン上面8より0.5〜3mm
程度低くなっている。
FIG. 1 shows the injection from the injection hole 4 of the injection nozzle 3 when the center of the piston 1 and the center of the reentrant type or toroidal type combustion chamber 2 are coincident with each other with four valves. The injection method (setting) depending on the number of the injection holes 4 will be shown in order from FIG. 2 onward. FIG. 2 shows a case in which there are four injection holes 4 of the fuel injection nozzle 3 in FIG. 1, and in this case, at least two of the injection holes 4 are right above the piston pin shaft 5 indicated by the dotted line. It is possible to set the injection direction at each point. FIG. 3 shows a case where there are five injection holes 4 of the fuel injection nozzle 3 in FIG. 1. In this case, only one injection hole 4 is located directly above the piston pin shaft 5, and the exhaust valve side is given priority. ing. FIG. 4 similarly shows the fuel injection nozzle 3
6 shows the case where there are six injection holes 4, and in this case the number is even, so it is possible to set the injection directions at two locations as in FIG. FIG. 5 shows a case where there are seven injection holes 4 of the fuel injection nozzle 3. In this case, since the number is odd, only one is set as in FIG. FIG. 6 shows a case where there are eight injection holes 4 of the fuel injection nozzle 3. In this case, since the number is even, two injection directions can be set. Therefore, when the number of the injection holes 4 is even, the number is two, and when the number is odd, the number is one, but the peripheral portion 6 of the combustion chamber intersecting the piston pin shaft 5 can be cooled. In each figure, 7 is the relief of the exhaust valve and 7'is the relief of the intake valve, which is 0.5 to 3 mm from the piston upper surface 8.
It is getting lower.

【0009】図7は2バルブでピストン1′の中心Oと
リエントラント型またはトロイダル型の燃焼室2′の中
心O1 とが不一致(偏心)の場合の噴射ノズル3の噴孔
4からの噴射を示したもので、図8以下に噴孔4の個数
の違いによる噴射方法(設定)を順に示す。図8は図7
における燃料噴射ノズル3の噴孔4が4個ある場合を示
し、この場合は少なくとも噴孔4のうち、2個が点線で
示すピストンピン軸5の真上にあるため、2個所の噴射
方向の設定が可能である。図9は図7における燃料噴射
ノズル3の噴孔4が5個ある場合を示し、この場合はピ
ストンピン軸5の真上にある噴孔4は1個のみの設定と
なり排気バルブ側を優先している。図10は同様に燃料
噴射ノズル3の噴孔4が6個ある場合を示し、この場合
は偶数であるから、図8と同様2個所の噴射方向の設定
が可能である。図11は燃料噴射ノズル3の噴孔4が7
個ある場合を示し、この場合は奇数ではあるから、図9
と同様1個の設定が可能となる。図12は燃料噴射ノズ
ル3の噴孔4が8個ある場合を示し、この場合は偶数で
あるから、2ヵ所の噴射方向の設定が可能である。した
がって噴孔4が偶数の場合は2個所、奇数の場合は図1
1の例外を除き1個所となるが、ピストンピン軸5と交
差する燃焼室周縁6′部分の冷却が可能である。各図に
おいて7は排気バルブの逃げで7´は吸気バルブの逃げ
でありピストン上面8より0.5〜3mm程度低くなっ
ている。
FIG. 7 shows the injection from the injection hole 4 of the injection nozzle 3 in the case where the center O of the piston 1'and the center O1 of the reentrant or toroidal combustion chamber 2'are not coincident (eccentric) in the two valve type. The injection method (setting) depending on the difference in the number of injection holes 4 is shown in order from FIG. 8 onward. FIG. 8 is FIG.
4 shows the case where there are four injection holes 4 of the fuel injection nozzle 3. In this case, at least two of the injection holes 4 are right above the piston pin shaft 5 indicated by the dotted line, Can be set. FIG. 9 shows a case in which there are five injection holes 4 of the fuel injection nozzle 3 in FIG. 7. In this case, only one injection hole 4 is located directly above the piston pin shaft 5, and the exhaust valve side is given priority. ing. Similarly, FIG. 10 shows a case where there are six injection holes 4 of the fuel injection nozzle 3. In this case, since the number is even, two injection directions can be set as in FIG. In FIG. 11, the injection hole 4 of the fuel injection nozzle 3 is 7
FIG. 9 shows the case where there are individual pieces, which is an odd number in this case.
It becomes possible to set one as in the above. FIG. 12 shows a case where there are eight injection holes 4 of the fuel injection nozzle 3. In this case, since the number is even, it is possible to set the injection directions at two locations. Therefore, if the injection holes 4 are even, there are two;
Although there is one exception with the exception of 1, it is possible to cool the peripheral portion 6'of the combustion chamber intersecting the piston pin shaft 5. In each figure, 7 is the relief of the exhaust valve and 7'is the relief of the intake valve, which is lower than the piston upper surface 8 by about 0.5 to 3 mm.

【0010】なお、前記冷却は何れの場合も排気バルブ
側を優先して行うものとし、また、噴射ノズル3の噴霧
角は不等ピッチとしてできるだけピストンピン軸5上に
2個位置させるようにしても良い。特に前記他の実施例
の場合(ピストン1′の中心Oと燃焼室2′の中心O1
とが不一致の場合)は面積を均等割とするため不等ピッ
チが採用される。
In any case, the cooling is performed by giving priority to the exhaust valve side, and the spray angles of the injection nozzles 3 are made to have unequal pitches, and two spray pins are positioned on the piston pin shaft 5 as much as possible. Is also good. Particularly in the case of the other embodiment (center O of piston 1'and center O1 of combustion chamber 2 ')
If and do not match), the uneven pitch is used to evenly divide the area.

【0011】[0011]

【発明の効果】以上説明したように本発明は、ディ−ゼ
ル機関の直接噴射方式におけるピストン燃焼室の冷却に
おいて、燃料噴射ノズルの噴孔からの噴射のうち、少な
くとも1つはピストンピン軸の真上の燃焼室周縁に噴射
されるようにしたから、噴射された燃焼室の周縁は冷却
され、これにより従来生じた亀裂等の発生は防止される
ことになる。
As described above, according to the present invention, in cooling the piston combustion chamber in the direct injection system of the diesel engine, at least one of the injections from the injection holes of the fuel injection nozzle is the piston pin shaft. Since the fuel is injected directly above the peripheral edge of the combustion chamber, the peripheral edge of the injected combustion chamber is cooled, thereby preventing the occurrence of cracks and the like that conventionally occur.

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

【図1】本発明にかかるピストンの燃焼室と燃料噴射ノ
ズルの関係を示す一実施例の断面を示す説明図である。
FIG. 1 is an explanatory view showing a cross section of an embodiment showing a relationship between a combustion chamber of a piston and a fuel injection nozzle according to the present invention.

【図2】図1において、燃料噴射ノズルの噴孔が4の場
合の噴霧位置を示す上面の説明図である。
FIG. 2 is an explanatory diagram of an upper surface showing a spray position when the number of injection holes of the fuel injection nozzle is 4 in FIG.

【図3】図1において、燃料噴射ノズルの噴孔が5の場
合の噴霧位置を示す上面の説明図である。
FIG. 3 is an explanatory diagram of an upper surface showing a spray position when the number of injection holes of the fuel injection nozzle is 5 in FIG.

【図4】図1において、燃料噴射ノズルの噴孔が6の場
合の噴霧位置を示す上面の説明図である。
FIG. 4 is an explanatory diagram of an upper surface showing a spraying position when there are 6 injection holes in the fuel injection nozzle in FIG. 1.

【図5】図1において、燃料噴射ノズルの噴孔が7の場
合の噴霧位置を示す上面の説明図である。
FIG. 5 is an explanatory view of the upper surface showing the spray position when the injection hole of the fuel injection nozzle is 7 in FIG.

【図6】図1において、燃料噴射ノズルの噴孔が8の場
合の噴霧位置を示す上面の説明図である。
FIG. 6 is an explanatory view of the upper surface showing the spray position when the number of injection holes of the fuel injection nozzle is 8 in FIG.

【図7】本発明にかかるピストンの燃焼室と燃料噴射ノ
ズルの関係を示す他の実施例の断面を示す説明図であ
る。
FIG. 7 is an explanatory view showing a cross section of another embodiment showing the relationship between the combustion chamber of the piston and the fuel injection nozzle according to the present invention.

【図8】図7において、燃料噴射ノズルの噴孔が4の場
合の噴霧位置を示す上面の説明図である。
FIG. 8 is an explanatory diagram of the upper surface showing the spray position when the number of the injection holes of the fuel injection nozzle is 4 in FIG.

【図9】図7において、燃料噴射ノズルの噴孔が5の場
合の噴霧位置を示す上面の説明図である。
FIG. 9 is an explanatory diagram of the upper surface showing the spray position when the number of injection holes of the fuel injection nozzle is 5 in FIG.

【図10】図7において、燃料噴射ノズルの噴孔が6の
場合の噴霧位置を示す上面の説明図である。
FIG. 10 is an explanatory diagram of the upper surface showing the spray position when the injection hole of the fuel injection nozzle is 6 in FIG.

【図11】図7において、燃料噴射ノズルの噴孔が7の
場合の噴霧位置を示す上面の説明図である。
FIG. 11 is an explanatory view of the upper surface showing the spray position when the injection hole of the fuel injection nozzle is 7 in FIG.

【図12】図7において、燃料噴射ノズルの噴孔が8の
場合の噴霧位置を示す上面の説明図である
FIG. 12 is an explanatory diagram of the upper surface showing the spray position when the injection hole of the fuel injection nozzle is 8 in FIG.

【符号の説明】[Explanation of symbols]

1,1′ ピストン 2,2′ 燃焼室 3 燃料噴射ノズル 4 噴孔 5 ピストンピン軸および穴 6,6′ 燃焼室
周縁 7 排気バルブの逃げ 7′ 吸気バ
ルブの逃げ
1,1 'Piston 2,2' Combustion chamber 3 Fuel injection nozzle 4 Injection hole 5 Piston pin shaft and hole 6,6 'Combustion chamber peripheral edge 7 Exhaust valve escape 7'Intake valve escape

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 ディ−ゼル機関の直接噴射方式における
ピストン燃焼室の冷却において、燃料噴射ノズルの噴孔
からの噴射のうち、少なくとも1つはピストンピン軸の
真上の燃焼室周縁に噴射されるようにしたことを特徴と
するピストンと燃料噴射方向の設定方法。
1. In cooling a piston combustion chamber in a direct injection system of a diesel engine, at least one of injections from injection holes of a fuel injection nozzle is injected to a peripheral edge of the combustion chamber immediately above a piston pin axis. The method for setting the piston and the fuel injection direction is characterized in that
JP3332889A 1991-11-22 1991-11-22 Piston and setting of fuel injection direction Pending JPH05149137A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3332889A JPH05149137A (en) 1991-11-22 1991-11-22 Piston and setting of fuel injection direction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3332889A JPH05149137A (en) 1991-11-22 1991-11-22 Piston and setting of fuel injection direction

Publications (1)

Publication Number Publication Date
JPH05149137A true JPH05149137A (en) 1993-06-15

Family

ID=18259936

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3332889A Pending JPH05149137A (en) 1991-11-22 1991-11-22 Piston and setting of fuel injection direction

Country Status (1)

Country Link
JP (1) JPH05149137A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1344914A1 (en) * 2002-03-15 2003-09-17 Institut Francais Du Petrole Internal combustion engine having fuel injection device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1344914A1 (en) * 2002-03-15 2003-09-17 Institut Francais Du Petrole Internal combustion engine having fuel injection device
FR2837238A1 (en) * 2002-03-15 2003-09-19 Inst Francais Du Petrole INTERNAL COMBUSTION ENGINE WITH FUEL INJECTION DEVICE
US6675767B2 (en) 2002-03-15 2004-01-13 Institut Francais Du Petrole Internal-combustion engine with fuel injection device

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