JP2000291513A - diesel engine - Google Patents
diesel engineInfo
- Publication number
- JP2000291513A JP2000291513A JP11101164A JP10116499A JP2000291513A JP 2000291513 A JP2000291513 A JP 2000291513A JP 11101164 A JP11101164 A JP 11101164A JP 10116499 A JP10116499 A JP 10116499A JP 2000291513 A JP2000291513 A JP 2000291513A
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- fuel injection
- valve body
- valve
- injected
- 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
Links
- 239000000446 fuel Substances 0.000 claims abstract description 178
- 238000002347 injection Methods 0.000 claims abstract description 105
- 239000007924 injection Substances 0.000 claims abstract description 105
- 238000002485 combustion reaction Methods 0.000 claims abstract description 27
- 230000035515 penetration Effects 0.000 abstract description 13
- 239000000243 solution Substances 0.000 abstract 1
- 239000007921 spray Substances 0.000 description 10
- 238000005507 spraying Methods 0.000 description 5
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000000889 atomisation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/182—Discharge orifices being situated in different transversal planes with respect to valve member direction of movement
-
- 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
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/162—Means to impart a whirling motion to fuel upstream or near discharging orifices
- F02M61/163—Means being injection-valves with helically or spirally shaped grooves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/1813—Discharge orifices having different orientations with respect to valve member direction of movement, e.g. orientations being such that fuel jets emerging from discharge orifices collide with each other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/1846—Dimensional characteristics of discharge orifices
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
(57)【要約】
【課題】 直接噴射式ディーゼルエンジンにおいて、低
負荷時において貫徹力の比較的弱い燃料を噴射し、高い
負荷時において貫徹力の比較的強い燃料を噴射するディ
ーゼルエンジン用燃料噴射弁を提供する。
【解決手段】 燃焼室と燃焼室に直接的に燃料を噴射す
る燃料噴射弁とを具備するディーゼルエンジンにおい
て、燃料噴射弁は、旋回力付与手段を有し、機関低負荷
時において旋回力付与手段によって燃料に旋回力を付与
して燃料を中空円錐状に噴射し、機関高負荷時において
燃料に旋回力を付与せずに燃料を柱状に噴射することを
特徴とする。
PROBLEM TO BE SOLVED: To provide a direct injection type diesel engine fuel injection for a diesel engine which injects a fuel having a relatively low penetration force at a low load and injects a relatively strong fuel at a high load. Provide a valve. SOLUTION: In a diesel engine including a combustion chamber and a fuel injection valve for directly injecting fuel into the combustion chamber, the fuel injection valve has a turning force applying means, and the turning force applying means when the engine is under a low load. The fuel is injected in a hollow conical shape by applying a swirling force to the fuel, and the fuel is injected in a columnar shape without applying the swirling force to the fuel when the engine is under a high load.
Description
【0001】[0001]
【発明の属する技術分野】本発明は、ディーゼルエンジ
ンに関する。[0001] The present invention relates to a diesel engine.
【0002】[0002]
【従来の技術】ディーゼルエンジンにおいて燃焼室に燃
料を供給する方法として、ピストン頂面に形成された燃
焼室内へ直接的に燃料を噴射する直接噴射式が公知であ
る。直接噴射式の燃料噴射において、必要燃料量が比較
的少ない低負荷時においては、燃焼室の壁面の温度が比
較的に低いため、燃料が壁面に付着すると、燃料は十分
には気化せずに不完全燃焼してしまうので、燃料が壁面
に付着することのないように弱い貫徹力を有する燃料を
噴射させる必要がある。また、必要燃料量が比較的多い
高負荷時においては、燃焼室内の比較的多くの空気を利
用する必要があるために、燃料に強い貫徹力を持たせ、
燃料を積極的に燃焼室壁面に衝突させて微粒化分散させ
ることが好ましい。この際、燃料が付着しても、燃焼室
の壁面の温度が比較的に高いため、燃料は気化するので
低負荷時のような問題は発生しない。そこで、噴射燃料
の貫徹力の強さを切り換えることのできる燃料噴射弁と
して、特開平7−224739号公報に記載されている
燃料噴射弁が公知である。この燃料噴射弁は、噴孔径の
小さな第一噴孔と、噴孔径の大きな第二噴孔を有し、低
負荷時においては第一噴孔のみから燃料を噴射すること
によって比較的弱い貫徹力の燃料を噴射することを可能
とし、高負荷時においては第一噴孔に加えて第二噴孔か
ら燃料を噴射することによって、比較的強い貫徹力の燃
料を噴射することを可能とする。2. Description of the Related Art As a method of supplying fuel to a combustion chamber in a diesel engine, a direct injection type in which fuel is directly injected into a combustion chamber formed on a piston top surface is known. In the direct injection type fuel injection, when the load is relatively small and the load is low, the temperature of the wall of the combustion chamber is relatively low.If the fuel adheres to the wall, the fuel does not vaporize sufficiently. Since the fuel is incompletely burned, it is necessary to inject the fuel having a weak penetration force so that the fuel does not adhere to the wall surface. Also, at the time of high load where the required fuel amount is relatively large, it is necessary to use a relatively large amount of air in the combustion chamber, so that the fuel has a strong penetration force,
It is preferred that the fuel be positively collided with the wall of the combustion chamber to be atomized and dispersed. At this time, even if the fuel adheres, the fuel is vaporized because the temperature of the wall surface of the combustion chamber is relatively high, so that there is no problem such as when the load is low. Therefore, as a fuel injection valve capable of switching the strength of the penetration force of the injected fuel, a fuel injection valve described in Japanese Patent Application Laid-Open No. 7-224739 is known. This fuel injection valve has a first injection hole with a small injection hole diameter and a second injection hole with a large injection hole diameter, and at low load, a relatively weak penetration force by injecting fuel only from the first injection hole. By injecting the fuel from the second injection hole in addition to the first injection hole at the time of a high load, it is possible to inject the fuel having a relatively strong penetration force.
【0003】[0003]
【発明が解決しようとする課題】しかしながら、低負荷
時においては、燃料は噴孔径の小さな噴孔から噴射され
ても、燃料は柱状に噴射されるために、燃料の貫徹力が
比較的強くなって壁面に付着し、良好な燃焼が得られな
いという問題が生ずる。However, when the load is low, even if the fuel is injected from an injection hole having a small injection hole diameter, the fuel is injected in a columnar shape, so that the penetration force of the fuel becomes relatively strong. To the wall surface, and good combustion cannot be obtained.
【0004】したがって、本発明の目的は、ピストン頂
面に形成された凹状の燃焼室内へ燃料噴射弁から直接的
に燃料を噴射する直接噴射式ディーゼルエンジンにおい
て、機関負荷に係わらず良好な燃焼を実現することであ
る。Accordingly, an object of the present invention is to provide a direct injection type diesel engine in which fuel is directly injected from a fuel injection valve into a concave combustion chamber formed on a piston top surface, regardless of the engine load. It is to realize.
【0005】[0005]
【課題を解決するための手段】上記問題点を解決するた
めに、本発明による請求項1に記載のディーゼルエンジ
ンは、燃焼室と燃焼室に直接的に燃料を噴射する燃料噴
射弁とを具備するディーゼルエンジンにおいて、燃料噴
射弁は、旋回力付与手段を有し、機関低負荷時において
旋回力付与手段によって燃料に旋回力を付与して燃料を
中空円錐状に噴射し、機関高負荷時において燃料に旋回
力を付与せずに燃料を柱状に噴射することを特徴とす
る。In order to solve the above problems, a diesel engine according to the first aspect of the present invention comprises a combustion chamber and a fuel injection valve for directly injecting fuel into the combustion chamber. In a diesel engine, the fuel injection valve has a slewing force applying means, applies a slewing force to the fuel by the slewing force applying means at a low engine load, injects the fuel into a hollow conical shape, and at a high engine load. It is characterized in that the fuel is injected in a columnar shape without imparting a turning force to the fuel.
【0006】[0006]
【発明の実施の形態】以下、添付図面を用いて本発明の
第一実施例について説明する。図1に示すディーゼルエ
ンジンは、燃料噴射弁1と、ピストン3とを有し、ピス
トン3の頂面には凹状の燃焼室4が形成されている。燃
料噴射弁1は燃焼室4のほぼ中心上部に略垂直に配置さ
れている。燃料噴射弁1は、主に弁体5及び弁本体6で
構成されている。燃料噴射弁1は、弁体5が燃料噴射弁
1の軸線方向にリフトされる時に燃料を噴射する内開弁
である。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A first embodiment of the present invention will be described below with reference to the accompanying drawings. The diesel engine shown in FIG. 1 has a fuel injection valve 1 and a piston 3, and a concave combustion chamber 4 is formed on a top surface of the piston 3. The fuel injection valve 1 is disposed substantially vertically above the center of the combustion chamber 4. The fuel injection valve 1 mainly includes a valve body 5 and a valve body 6. The fuel injection valve 1 is an internal valve that injects fuel when the valve body 5 is lifted in the axial direction of the fuel injection valve 1.
【0007】図1及び図2を参照して弁本体6の形状に
ついて説明する。弁本体6は、シリンダヘッド2によっ
て保持される円筒部分と円筒部分の下側に位置する円蓋
状部分からなる。弁本体6の円筒部分の内側の中央に
は、ほぼ円筒形状の弁体5が配置され、弁本体6の内面
と弁体5の外面の間には、円筒状の燃料通路12が形成
されている。燃料通路12の下流側に位置する弁本体6
の円蓋状部分の内面には、円錐状の弁本体傾斜部13が
形成され、弁本体傾斜部13の下流側には、円筒部分と
半球状部分からなる燃料溜15が形成されている。弁本
体傾斜部13における弁体5が着座する位置に、弁体シ
ート部14が形成されている。弁本体傾斜部13におい
て弁体シート部14より下流側に、第一燃料噴射通路1
6の入口が形成されている。燃料溜15において第二燃
料噴射通路17の入口が形成されている。第一燃料噴射
通路16及び第二燃料噴射通路17は、弁本体6の表面
に形成された噴口18において連通している。このよう
な第一燃料噴射通路16、第二燃料噴射通路17、及び
噴口18は、燃料噴射弁1の中心軸線に対してほぼ等間
隔で放射状に位置する。The shape of the valve body 6 will be described with reference to FIGS. The valve body 6 includes a cylindrical portion held by the cylinder head 2 and a forked portion located below the cylindrical portion. A substantially cylindrical valve body 5 is disposed at the center inside the cylindrical portion of the valve body 6, and a cylindrical fuel passage 12 is formed between the inner surface of the valve body 6 and the outer surface of the valve body 5. I have. Valve body 6 located downstream of fuel passage 12
A conical valve body inclined portion 13 is formed on the inner surface of the circular cap-shaped portion, and a fuel reservoir 15 composed of a cylindrical portion and a hemispherical portion is formed downstream of the valve body inclined portion 13. A valve body seat portion 14 is formed at a position on the valve body inclined portion 13 where the valve body 5 sits. The first fuel injection passage 1 is located downstream of the valve body seat portion 14 in the valve body inclined portion 13.
Six inlets are formed. An inlet of the second fuel injection passage 17 is formed in the fuel reservoir 15. The first fuel injection passage 16 and the second fuel injection passage 17 communicate with each other at an injection port 18 formed on the surface of the valve body 6. The first fuel injection passage 16, the second fuel injection passage 17, and the injection port 18 are radially located at substantially equal intervals with respect to the central axis of the fuel injection valve 1.
【0008】図1及び図2を参照して弁体5の形状につ
いて説明する。弁体5は、円筒状の弁体胴体部7、弁体
胴体部7の下側に形成された円錐状の弁体傾斜部8、弁
体傾斜部の下側に形成された円筒状のガイド部9及び弁
体ガイド部の下側に形成された弁体針部10からなる。
弁体胴体部7は、弁体5の上下動を制御する機構(図示
せず)と接続されるので弁体5は上下動することができ
る。弁体傾斜部8は、弁本体6の弁体傾斜部13と適合
するように、円錐状に形成されている。弁体傾斜部8
は、弁本体6において弁体シート部14に着座させられ
ることによって、第一燃料噴射通路16及び第二燃料噴
射通路17を燃料通路12から遮断することができる。
ガイド部9は、その断面形状が弁本体6の燃料溜15の
円筒部分の断面形状とと適合しており、弁体5が比較的
小さくリフトされても、第二燃料噴射通路17を燃料通
路12から遮断することができ、また、この時には、弁
体5が弁本体6の燃料溜15の円筒部分内でガイドされ
ることを可能とする。弁体5が弁本体6に着座する位置
よりも下流側において、弁体傾斜部8には第一燃料噴射
通路16に対向して楕円体形状の溝部11が弁体傾斜部
8の稜線に対して斜めに形成されている。各溝部11
は、比較的に弁体5のリフト量が小さい時に、対応する
第一燃料噴射通路16の入口に対して、入口周囲部だけ
に対向するように配置されている。溝部11は、弁体傾
斜部8の稜線に対して平行でもよい。また、溝部11の
断面形状は、円形に限らず、矩形でもよい。The shape of the valve body 5 will be described with reference to FIGS. The valve element 5 includes a cylindrical valve element body section 7, a conical valve element inclined section 8 formed below the valve element body section 7, and a cylindrical guide formed below the valve element inclined section. It comprises a portion 9 and a valve needle 10 formed below the valve guide.
Since the valve body 7 is connected to a mechanism (not shown) for controlling the vertical movement of the valve 5, the valve 5 can move up and down. The valve body inclined portion 8 is formed in a conical shape so as to fit with the valve body inclined portion 13 of the valve body 6. Valve body inclined part 8
The first fuel injection passage 16 and the second fuel injection passage 17 can be shut off from the fuel passage 12 by being seated on the valve body seat portion 14 in the valve body 6.
The guide section 9 has a cross-sectional shape that matches the cross-sectional shape of the cylindrical portion of the fuel reservoir 15 of the valve body 6, and allows the second fuel injection passage 17 to pass through the fuel passage even when the valve body 5 is lifted relatively small. 12 and at this time allows the valve body 5 to be guided in the cylindrical part of the fuel reservoir 15 of the valve body 6. On the downstream side of the position where the valve element 5 is seated on the valve body 6, an elliptical groove 11 is formed in the valve element inclined section 8 so as to face the first fuel injection passage 16 with respect to the ridge line of the valve element inclined section 8. It is formed diagonally. Each groove 11
When the lift amount of the valve element 5 is relatively small, it is disposed so as to face only the periphery of the entrance with respect to the entrance of the corresponding first fuel injection passage 16. The groove 11 may be parallel to the ridge line of the valve body inclined portion 8. The cross-sectional shape of the groove 11 is not limited to a circle, but may be a rectangle.
【0009】次に、燃料噴射の作用について説明する。
弁体5のリフト量が比較的小さい時、弁体傾斜部8と弁
本体傾斜部13の間に薄い円錐体形状の間隙部19が形
成される。高圧に貯留された燃料がこの間隙部19を通
る時、間隙部19の厚さに比べて溝部11は深いので、
燃料の一部分は減圧された溝部11に吸引されて溝部1
1に沿って流れる。こうして、溝部長手方向の速度成分
を付与された燃料は、溝部11に対向して弁本体傾斜部
13に形成された第一燃料噴射通路16の入口周囲部に
入口周囲部の接線方向に流入される。それにより、燃料
は第一燃料噴射通路16内において旋回しながら進行
し、噴射直後に中空円錐状となる。このように、溝部1
1は、リフト量が比較的に小さい時に燃料に対して第一
燃料噴射通路16内の旋回力を付与し、旋回力付与手段
を構成する。一方、この時、第二燃料噴射通路17は、
ガイド部9によって遮断されているため、燃料が噴射さ
れない。Next, the operation of the fuel injection will be described.
When the lift amount of the valve body 5 is relatively small, a thin conical gap 19 is formed between the valve body inclined portion 8 and the valve body inclined portion 13. When the fuel stored at a high pressure passes through the gap 19, the groove 11 is deeper than the thickness of the gap 19,
Part of the fuel is sucked into the depressurized groove 11 and the groove 1
Flows along 1. Thus, the fuel provided with the velocity component in the longitudinal direction of the groove flows into the peripheral portion of the first fuel injection passage 16 formed in the valve body inclined portion 13 in the tangential direction of the peripheral portion of the inlet. Is done. As a result, the fuel advances while turning in the first fuel injection passage 16, and has a hollow conical shape immediately after the injection. Thus, the groove 1
Reference numeral 1 designates a turning force applying means for applying a turning force in the first fuel injection passage 16 to the fuel when the lift amount is relatively small. On the other hand, at this time, the second fuel injection passage 17
The fuel is not injected because it is shut off by the guide portion 9.
【0010】弁体5のリフト量が比較的大きい時、弁体
傾斜部8と弁本体傾斜部13は大きく離間して弁体傾斜
部8と弁本体傾斜部13の間に厚い円錐体形状の間隙部
19が形成される。また、弁体5のガイド部9は燃料溜
15から離間する。高圧に貯留された燃料がこの間隙部
19を通る時、間隙部19の厚さに比べて溝部11は無
視できる形状であるので、燃料は間隙部19の稜線方向
に流れる。第一燃料噴射通路16の入口近傍の燃料は、
第一燃料噴射通路16に吸引されて直進して噴射され
る。一方、間隙部19において第一燃料噴射通路16に
吸引されなかった燃料は、下流の燃料溜15に流れ、第
二燃料噴射通路17の入口で吸引されて直進して噴射さ
れる。第一燃料噴射通路16及び第二燃料噴射通路17
の両方から出てくる燃料は、噴口18において合流して
一つの燃料流が形成される。When the lift amount of the valve body 5 is relatively large, the valve body inclined portion 8 and the valve body inclined portion 13 are largely separated from each other so that a thick conical body is formed between the valve body inclined portion 8 and the valve body inclined portion 13. A gap 19 is formed. Further, the guide portion 9 of the valve element 5 is separated from the fuel reservoir 15. When the fuel stored at a high pressure passes through the gap 19, the fuel flows in the ridge line direction of the gap 19 because the groove 11 has a shape that can be ignored compared to the thickness of the gap 19. The fuel near the inlet of the first fuel injection passage 16 is:
The fuel is sucked into the first fuel injection passage 16 and goes straight to be injected. On the other hand, the fuel that has not been sucked into the first fuel injection passage 16 in the gap portion 19 flows to the downstream fuel reservoir 15, is sucked at the inlet of the second fuel injection passage 17, and is straightly injected. First fuel injection passage 16 and second fuel injection passage 17
The fuel coming out of both of them joins at the injection port 18 to form one fuel flow.
【0011】燃料の合流する噴口18は、第一燃料噴射
通路16又は第二燃料噴射通路17から流入してくる二
つの異なる方向成分を有する燃料流を壁面でガイドする
ことにより、燃料を噴口18の壁面方向に整える役割を
する。噴口18の表面からの深さが大きいほど、合流す
る燃料流の噴霧角は小さくなる。合流された燃料流は、
第一燃料噴射通路16の断面積及び第二燃料噴射通路1
7の断面積の合計の噴孔面積を持つことに匹敵する。す
なわち、合流された燃料流は大きな貫徹力を持つことが
できる。機関高負荷時に二つの燃料流を合流させること
によって、合流された燃料流は、各燃料噴射通路の噴孔
面積が小さいということによって燃焼に良好である燃料
の微粒化を実現させる一方で、各燃料噴射通路16、1
7からの燃料の貫徹力よりも大きな貫徹力を持つことが
できる。The fuel injection port 18 joins the fuel by guiding the fuel flow having two different directional components flowing from the first fuel injection passage 16 or the second fuel injection passage 17 on the wall surface. It plays the role of trimming in the direction of the wall. The greater the depth from the surface of the nozzle 18, the smaller the spray angle of the combined fuel flows. The combined fuel flow is
Cross-sectional area of first fuel injection passage 16 and second fuel injection passage 1
Equivalent to having a total orifice area of 7 cross-sectional areas. That is, the merged fuel flow can have a large penetration force. By combining the two fuel flows at a high engine load, the combined fuel flows realize atomization of fuel which is good for combustion due to the small injection hole area of each fuel injection passage. Fuel injection passage 16, 1
7 can have a greater penetration force than the fuel penetration force.
【0012】噴射時の弁体5のリフト量を選択すること
によって、燃料の噴射形態を変えることができる。例え
ば、中空円錐状噴霧時に大きな弁体リフト量で噴射され
ると、小さな噴射角の中空円錐状噴霧となり、小さな弁
体リフト量で噴射されると、大きな噴射角の中空円錐状
噴霧となる。また、弁体5のガイド部9の長さを変える
ことによっても、燃料の噴射形態を変えることができ
る。例えば、ガイド部9を短くすると、小さな弁体リフ
ト量で燃料通路12が第一燃料噴射通路16及び第二燃
料噴射通路17両方と同時に連通し、中空円錐状噴霧が
第一燃料噴射通路16から噴射される時に、第二燃料噴
射通路17からも柱状噴霧が同時に噴射されるようにす
ることもできる。好ましくは、弁体5のリフト量が全リ
フト量の30〜50%のリフト量の時に第一燃料噴射通
路16のみから燃料が中空円錐状に噴射され、全リフト
量の100%のリフト量の時に第一燃料噴射通路16及
び第二燃料噴射通路17から燃料が柱状に噴射されるよ
うに、弁体5のガイド部の長さが選択される。また、燃
料噴射時期は弁体5のリフト時期を調整することによっ
て制御され、燃料噴射量は、噴射時間すなわち弁体5の
リフト時間を調整することによって制御される。By selecting the amount of lift of the valve body 5 at the time of injection, the fuel injection mode can be changed. For example, when spraying with a large valve body lift during hollow cone spraying, a hollow cone-shaped spray with a small spray angle is formed, and when spraying with a small valve body lift, a hollow cone-shaped spray with a large spray angle is formed. The fuel injection mode can also be changed by changing the length of the guide portion 9 of the valve element 5. For example, when the guide portion 9 is shortened, the fuel passage 12 communicates simultaneously with both the first fuel injection passage 16 and the second fuel injection passage 17 with a small valve body lift, and the hollow conical spray is discharged from the first fuel injection passage 16. When the fuel is injected, the columnar spray can also be simultaneously injected from the second fuel injection passage 17. Preferably, when the lift amount of the valve body 5 is a lift amount of 30 to 50% of the total lift amount, fuel is injected in a hollow conical shape only from the first fuel injection passage 16 and the lift amount of 100% of the total lift amount is The length of the guide portion of the valve element 5 is selected so that the fuel is sometimes injected in a column shape from the first fuel injection passage 16 and the second fuel injection passage 17. Further, the fuel injection timing is controlled by adjusting the lift timing of the valve element 5, and the fuel injection amount is controlled by adjusting the injection time, that is, the lift time of the valve element 5.
【0013】次に、各機関負荷を通した燃料噴射につい
て説明する。機関低負荷の場合、図3に示すように、圧
縮行程において、弁体5のガイド部9を弁本体5の燃料
溜15に保持された状態で弁体5を所定の量で所定時間
だけリフトすることによって、第一燃料噴射通路16か
ら中空円錐状に燃料が噴射される。燃料が中空円錐状に
噴射されることによって、貫徹力の弱い燃料が噴射さ
れ、燃料が壁面に付着せずに空気との混合が図られるこ
とができる。Next, the fuel injection through each engine load will be described. In the case of a low engine load, as shown in FIG. 3, during the compression stroke, the valve element 5 is lifted by a predetermined amount for a predetermined time while the guide portion 9 of the valve element 5 is held in the fuel reservoir 15 of the valve body 5. Thereby, the fuel is injected from the first fuel injection passage 16 in a hollow conical shape. By injecting the fuel in a hollow conical shape, the fuel having a low penetration force is injected, and the fuel can be mixed with air without adhering to the wall surface.
【0014】機関中負荷の場合、圧縮行程初期において
図3に示すように、第一燃料噴射通路16のみから中空
円錐状に噴射され、圧縮行程末期においてさらに図4に
示すように、弁体5のガイド部9が燃料溜15から離間
された状態で、弁体5をより大きな所定の量で所定時間
だけリフトすることによって、第一燃料噴射通路16だ
けでなく、第二燃料噴射通路17から燃料が噴射され
る。これらの二つの燃料流が噴口18で合流して一つの
柱状噴霧が形成される。中空円錐状噴霧と柱状噴霧がそ
れぞれ噴射されることによって、一回分の噴射量を少な
くすることができるので、燃料を可能な限り壁面への付
着を阻止することができるという利点と、別の形態の燃
料が噴射されるので、燃焼室内の広範囲の空気を利用で
きるという利点がある。In the case of the engine middle load, as shown in FIG. 3, at the beginning of the compression stroke, the fuel is injected in a hollow conical form only from the first fuel injection passage 16, and at the end of the compression stroke, as shown in FIG. By lifting the valve body 5 for a predetermined time by a larger predetermined amount in a state where the guide portion 9 is separated from the fuel reservoir 15, not only the first fuel injection passage 16 but also the second fuel injection passage 17 Fuel is injected. These two fuel streams merge at the nozzle 18 to form one columnar spray. The advantage that the fuel can be prevented from adhering to the wall surface as much as possible, because the amount of injection in one shot can be reduced by injecting the hollow conical spray and the columnar spray, respectively. Is injected, so that there is an advantage that a wide range of air in the combustion chamber can be used.
【0015】機関高負荷の場合、図5に示すように、圧
縮行程において、機関中負荷時の柱状噴霧時の弁体リフ
ト量よりも大きな所定の量で弁体5を所定時間だけリフ
トすることによって、第一燃料噴射通路16と第二燃料
噴射通路17の出口から比較的多くの燃料が柱状に噴射
される。こうして貫徹力の強い燃料が噴射されて燃焼室
壁面に衝突して燃料は良好に分散される。以上のよう
に、機関負荷に係わらず良好な燃焼が得られることがで
きる。燃料噴射時期は、以上に説明した時期に限らず、
本発明を実施することができる。In the case of a high engine load, as shown in FIG. 5, in the compression stroke, the valve element 5 is lifted for a predetermined time by a predetermined amount larger than the valve element lift amount at the time of columnar spraying at a medium engine load. Accordingly, a relatively large amount of fuel is injected in a column shape from the outlets of the first fuel injection passage 16 and the second fuel injection passage 17. In this way, the fuel having a strong penetration force is injected and collides with the combustion chamber wall surface, and the fuel is well dispersed. As described above, good combustion can be obtained regardless of the engine load. The fuel injection timing is not limited to the timing described above,
The present invention can be implemented.
【0016】また、旋回力付与手段の別の実施例につい
て説明する。弁本体傾斜部13において弁体シート部1
4の下側に、第一燃料噴射通路16の入口周囲部に入口
周囲部の接線方向に連通するように溝部を形成する。弁
体5の少量のリフト時には、溝部は、燃料に対して第一
燃料噴射通路16内で旋回して中空円錐状に噴射され、
旋回力付与手段を構成する。Another embodiment of the turning force applying means will be described. The valve body seat portion 1 in the valve body inclined portion 13
4, a groove is formed in the periphery of the inlet of the first fuel injection passage 16 so as to communicate tangentially to the periphery of the inlet. When the valve body 5 is lifted by a small amount, the groove portion is swirled in the first fuel injection passage 16 to inject the fuel into a hollow conical shape,
It constitutes a turning force applying means.
【0017】以上の説明において、第一燃料噴射通路1
6と第二燃料噴射通路17は噴口18において合流して
いるが、第一燃料噴射通路16と第二燃料噴射通路17
が合流せずに別々に噴孔が配置される別の実施例も考え
られる。この実施例では、機関中負荷時の柱状噴霧時に
おいて各燃料噴射通路からの燃料流が合流されないので
低い貫徹力を有するという点と、燃焼室内のより広範囲
の空気を利用することができるという点で好ましい。In the above description, the first fuel injection passage 1
6 and the second fuel injection passage 17 merge at the injection port 18, but the first fuel injection passage 16 and the second fuel injection passage 17
Another embodiment is also conceivable in which injection holes are separately arranged without merging. In this embodiment, the fuel flow from each fuel injection passage is not merged at the time of columnar spraying at the time of medium load of the engine, so that it has a low penetration force, and a wider range of air in the combustion chamber can be used. Is preferred.
【0018】以上の説明において、燃料噴射弁、弁体、
弁本体、燃焼室等の形状は、好適な実施例として記述さ
れているが、発明を限定する要件ではない。In the above description, the fuel injection valve, valve body,
The shapes of the valve body, combustion chamber, etc. are described as preferred embodiments, but are not required to limit the invention.
【0019】[0019]
【発明の効果】本発明によれば、燃焼室と燃焼室に直接
的に燃料を噴射する燃料噴射弁とを具備するディーゼル
エンジンにおいて、燃料噴射弁は、旋回力付与手段を有
し、機関低負荷時において旋回力付与手段によって燃料
に旋回力を付与して燃料を中空円錐状に噴射し、機関高
負荷時において燃料に旋回力を付与せずに燃料を柱状に
噴射するために、機関低負荷時には燃料は中空円錐状に
噴射されるので燃料は燃焼室壁面に付着されずに分布さ
れることができ、機関高負荷時には燃料は貫徹力の大き
な柱状に噴射されて壁面に衝突して多くの燃料を微粒化
分散することができ、機関負荷に係わらず良好な燃焼が
実現されることができる。According to the present invention, in a diesel engine having a combustion chamber and a fuel injection valve for directly injecting fuel into the combustion chamber, the fuel injection valve has a turning force applying means, In order to inject the fuel in a hollow conical shape by applying a turning force to the fuel by the turning force applying means at the time of load, and to inject the fuel in a columnar shape without applying the turning force to the fuel at the time of high engine load, the engine low At the time of load, the fuel is injected in a hollow conical shape so that the fuel can be distributed without adhering to the combustion chamber wall surface. Can be atomized and dispersed, and good combustion can be realized regardless of the engine load.
【図1】本発明の燃料噴射弁の断面図である。FIG. 1 is a sectional view of a fuel injection valve of the present invention.
【図2】本発明の燃料噴射弁の拡大断面図である。FIG. 2 is an enlarged sectional view of the fuel injection valve of the present invention.
【図3】本発明の機関低負荷時における燃料の噴射時期
を示す図である。FIG. 3 is a diagram showing a fuel injection timing at a low engine load according to the present invention.
【図4】本発明の機関中負荷時における燃料の噴射時期
を示す図である。FIG. 4 is a diagram showing a fuel injection timing at the time of an engine middle load according to the present invention.
【図5】本発明の機関高負荷時における燃料の噴射時期
を示す図である。FIG. 5 is a diagram showing a fuel injection timing when the engine is under a high load according to the present invention.
1…燃料噴射弁 4…燃焼室 1. Fuel injection valve 4. Combustion chamber
───────────────────────────────────────────────────── フロントページの続き (72)発明者 阪田 一郎 愛知県豊田市トヨタ町1番地 トヨタ自動 車株式会社内 (72)発明者 中村 己喜男 愛知県豊田市トヨタ町1番地 トヨタ自動 車株式会社内 (72)発明者 藤原 清 愛知県豊田市トヨタ町1番地 トヨタ自動 車株式会社内 (72)発明者 岡田 晋 愛知県豊田市トヨタ町1番地 トヨタ自動 車株式会社内 Fターム(参考) 3G066 AA07 AB02 AD12 BA03 BA04 CC14 CC18 CC23 CC26 CC30 CC42 CC48 DA09 DB06 DB08 DB09 ──────────────────────────────────────────────────続 き Continuing from the front page (72) Inventor Ichiro Sakata 1 Toyota Town, Toyota City, Aichi Prefecture Inside Toyota Motor Corporation (72) Inventor Mikio Nakamura 1 Toyota Town, Toyota City, Aichi Prefecture Inside Toyota Motor Corporation (72) Inventor Kiyoshi Fujiwara 1 Toyota Town, Toyota City, Aichi Prefecture Toyota Motor Corporation (72) Inventor Susumu 1 Toyota Town Toyota City, Aichi Prefecture Toyota Motor Corporation F-term (reference) 3G066 AA07 AB02 AD12 BA03 BA04 CC14 CC18 CC23 CC26 CC30 CC42 CC48 DA09 DB06 DB08 DB09
Claims (1)
射する燃料噴射弁とを具備するディーゼルエンジンにお
いて、前記燃料噴射弁は、旋回力付与手段を有し、機関
低負荷時において前記旋回力付与手段によって燃料に旋
回力を付与して燃料を中空円錐状に噴射し、機関高負荷
時において燃料に旋回力を付与せずに燃料を柱状に噴射
することを特徴とするディーゼルエンジン。1. A diesel engine comprising a combustion chamber and a fuel injection valve for directly injecting fuel into the combustion chamber, wherein the fuel injection valve has a turning force applying means, and when the engine is under a low load, A diesel engine characterized in that a swirling force is applied to fuel by a swirling force applying means and the fuel is injected in a hollow conical shape, and the fuel is injected in a columnar shape without applying a swirling force to the fuel when the engine is under a high load.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11101164A JP2000291513A (en) | 1999-04-08 | 1999-04-08 | diesel engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11101164A JP2000291513A (en) | 1999-04-08 | 1999-04-08 | diesel engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2000291513A true JP2000291513A (en) | 2000-10-17 |
Family
ID=14293407
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11101164A Pending JP2000291513A (en) | 1999-04-08 | 1999-04-08 | diesel engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2000291513A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10124745A1 (en) * | 2001-05-21 | 2003-03-27 | Bosch Gmbh Robert | Fuel injector |
GB2389390A (en) * | 2002-06-06 | 2003-12-10 | Delphi Tech Inc | Fuel injection nozzle with inclined grooves formed in the valve needle |
WO2008120086A2 (en) | 2007-04-02 | 2008-10-09 | Toyota Jidosha Kabushiki Kaisha | Fuel injection device |
JP2010151018A (en) * | 2008-12-25 | 2010-07-08 | Honda Motor Co Ltd | Fuel injection device |
CN102182600A (en) * | 2011-05-02 | 2011-09-14 | 大连理工大学 | Internal Combustion Engine Injector with Disturbance Zone |
CN110439721A (en) * | 2018-05-04 | 2019-11-12 | 罗伯特·博世有限公司 | The nozzle of internal combustion engine |
-
1999
- 1999-04-08 JP JP11101164A patent/JP2000291513A/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10124745A1 (en) * | 2001-05-21 | 2003-03-27 | Bosch Gmbh Robert | Fuel injector |
GB2389390A (en) * | 2002-06-06 | 2003-12-10 | Delphi Tech Inc | Fuel injection nozzle with inclined grooves formed in the valve needle |
WO2008120086A2 (en) | 2007-04-02 | 2008-10-09 | Toyota Jidosha Kabushiki Kaisha | Fuel injection device |
JP2010151018A (en) * | 2008-12-25 | 2010-07-08 | Honda Motor Co Ltd | Fuel injection device |
CN102182600A (en) * | 2011-05-02 | 2011-09-14 | 大连理工大学 | Internal Combustion Engine Injector with Disturbance Zone |
CN110439721A (en) * | 2018-05-04 | 2019-11-12 | 罗伯特·博世有限公司 | The nozzle of internal combustion engine |
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