JPH0826770B2 - Combustion chamber of direct injection diesel engine - Google Patents
Combustion chamber of direct injection diesel engineInfo
- Publication number
- JPH0826770B2 JPH0826770B2 JP4177985A JP17798592A JPH0826770B2 JP H0826770 B2 JPH0826770 B2 JP H0826770B2 JP 4177985 A JP4177985 A JP 4177985A JP 17798592 A JP17798592 A JP 17798592A JP H0826770 B2 JPH0826770 B2 JP H0826770B2
- Authority
- JP
- Japan
- Prior art keywords
- combustion chamber
- mesh member
- view
- nozzle
- injection
- 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
Links
- 238000002347 injection Methods 0.000 title claims description 55
- 239000007924 injection Substances 0.000 title claims description 55
- 238000002485 combustion reaction Methods 0.000 title claims description 50
- 239000007921 spray Substances 0.000 claims description 37
- 239000000446 fuel Substances 0.000 claims description 22
- 230000002093 peripheral effect Effects 0.000 claims description 15
- 239000000779 smoke Substances 0.000 description 16
- 239000007789 gas Substances 0.000 description 8
- 238000010586 diagram Methods 0.000 description 4
- 238000009826 distribution Methods 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 3
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 230000001737 promoting effect Effects 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 230000002238 attenuated effect Effects 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004581 coalescence Methods 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000008094 contradictory effect Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000001678 irradiating effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 230000007480 spreading Effects 0.000 description 1
- 238000003892 spreading Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 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
- F02B23/0645—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
- F02B23/0645—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
- F02B23/0696—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
- 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
- F02B23/0603—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 at least part of the interior volume or the wall of the combustion space being made of material different from the surrounding piston part, e.g. combustion space formed within a ceramic part fixed to a metal piston head
-
- 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
- F02B23/0621—Squish 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
- 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
- F02B23/0678—Unconventional, complex or non-rotationally symmetrical shapes of the combustion space, e.g. flower like, having special shapes related to the orientation of the fuel spray jets
- F02B23/0687—Multiple bowls in the piston, e.g. one bowl per fuel spray jet
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Dispersion Chemistry (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
【0001】[0001]
【産業上の利用分野】本発明は、スモークの発生を低レ
ベルに維持しつつNOX (窒素酸化物)を大幅に低減さ
せるための直接噴射式ディーゼル機関の燃焼室に関す
る。The present invention relates to a combustion chamber of direct-injection diesel engine in order to significantly reduce the NO X (nitrogen oxides) while maintaining the generation of smoke at a low level.
【0002】[0002]
【従来の技術】現在、ディーゼル機関において、スモー
クおよびNOX の低減は重要な課題であり、その低減に
向けて高圧噴射、燃焼方式の改善、排ガス再循環(EG
R)等、種々の提案が行われている。このうちEGR
は、燃費およびスモークの悪化、排ガスによるEGR装
置の腐食或いは機能低下等、耐久性および信頼性の問題
がある。2. Description of the Related Art At present, reduction of smoke and NO x is an important issue in diesel engines, and in order to reduce them, high pressure injection, improvement of combustion system, exhaust gas recirculation (EG
Various proposals such as R) have been made. EGR
Have problems of durability and reliability such as deterioration of fuel consumption and smoke, corrosion of EGR device due to exhaust gas or deterioration of function.
【0003】また、燃焼方式の観点からみれば、現在広
く用いられている低圧噴射の場合、噴霧はノズル近傍で
着火した後、全体が火炎に包まれながら進行し、この
時、噴霧は、空気と同時に自己の生成した既燃ガスを巻
き込みながら燃焼するので、噴霧中心部において高温
部、酸素不足部が形成されスモークの生成要因となり、
既燃ガスの巻き込みはマイナス要因として働くと言われ
ている。このためスモークを低減するには、燃料と空気
を迅速に混合する必要があり、スワール、スキッシュ等
により空気利用率を向上する方法が採られているが、こ
れでは着火遅れの間の燃料、空気混合速度も増大するた
め、予混合燃焼の増加により燃焼初期の熱発生率が増大
し、NOX の増大を招くという相反する問題を有してお
り、これがスモークとNOX の同時低減を困難にしてい
る。From the viewpoint of the combustion system, in the case of low pressure injection which is widely used at present, after the spray is ignited in the vicinity of the nozzle, it progresses while being wrapped in the whole flame. At this time, the spray is air. At the same time, it burns while energizing the burnt gas generated by itself, so a high temperature part and an oxygen deficient part are formed in the center of the spray, which becomes a cause of smoke generation,
It is said that the burning of burned gas acts as a negative factor. Therefore, in order to reduce smoke, it is necessary to mix fuel and air quickly, and methods such as swirl and squish are used to improve the air utilization rate. Since the mixing speed also increases, there is a contradictory problem that the heat generation rate in the early stage of combustion increases due to the increase in premixed combustion, leading to an increase in NO X , which makes it difficult to reduce smoke and NO X simultaneously. ing.
【0004】上記問題を解決するために、高圧噴射(例
えば噴射圧1000kg/cm2 以上)、小噴孔径ノズ
ル、浅皿燃焼室および低スワールを組合せる方式が知ら
れている。これを図13により説明すると、1はピスト
ン、2はピストンリング、3はシリンダライナー、4は
ガスケット、5はシリンダヘッド、6はノズル7を有す
る燃料噴射弁を示し、ピストン1の頂部には燃焼室9が
形成されている。ピストン1が上昇し上死点付近に達し
たとき、ノズル7から噴射された燃料の噴霧Fは、壁面
10近傍で一気に着火した後、火炎Hは、燃焼室9中心
に向かって膨張するが、噴霧のもつエネルギーが大きい
ため噴射の終了まで中心部は不燃域として残る。すなわ
ち、噴霧は壁面10に到達するまで燃焼室9中心に近い
不燃域側で十分に空気を巻き込みながら進行し、壁面1
0側では既燃ガスを導入しながら壁面10に衝突する二
段の燃焼経路をたどるため、スモークは低く噴射時期を
大幅に遅らせても火がつくため、噴射時期遅延との組み
合わせで、低圧噴射と比較してスモークおよびNOX の
同時低減を図ることができる。In order to solve the above problems, there is known a system in which a high pressure injection (for example, an injection pressure of 1000 kg / cm 2 or more), a small injection hole nozzle, a shallow dish combustion chamber and a low swirl are combined. This will be described with reference to FIG. 13. 1 is a piston, 2 is a piston ring, 3 is a cylinder liner, 4 is a gasket, 5 is a cylinder head, and 6 is a fuel injection valve having a nozzle 7. A chamber 9 is formed. When the piston 1 rises and reaches the vicinity of the top dead center, the spray F of the fuel injected from the nozzle 7 ignites at once in the vicinity of the wall surface 10, and then the flame H expands toward the center of the combustion chamber 9, Since the energy of the spray is large, the central part remains as a non-combustible area until the end of injection. That is, the spray progresses while sufficiently entraining air in the non-combustible region side near the center of the combustion chamber 9 until it reaches the wall surface 10.
On the 0 side, since the burner gas is introduced and it follows the two-stage combustion path where it collides with the wall surface 10, the smoke is low, and even if the injection timing is greatly delayed, it ignites, so in combination with the injection timing delay, low pressure injection It is possible to reduce the smoke and the NO X at the same time as compared with the above.
【0005】[0005]
【発明が解決しようとする課題】しかしながら、現状で
は燃焼室内の空気(酸素)の利用が十分でなく、特に高
負荷時(燃料噴射量大)は、スモークを生成し排出する
という問題を有している。スモークを抑えるためには、
拡散燃焼を活発化させ燃焼後期まで強い乱れを保持し、
さらに、乱れ渦を細かい状態に保つことが必要である。
ところが、拡散燃焼は膨張行程で生じるため、一般にそ
の時点ではシリンダ内の空気流動が減衰してしまい、吸
入スワールなど圧縮行程中に与えた乱れによる燃焼活性
化の効果は比較的小さくなってしまう。また、高圧噴射
の場合、火炎の乱れ強さは拡散燃焼初期では大きいが、
燃焼後期では減衰し低圧噴射とあまり変わらなくなって
しまう。However, at present, the utilization of air (oxygen) in the combustion chamber is not sufficient, and there is a problem that smoke is generated and discharged, especially when the load is high (fuel injection amount is large). ing. To suppress smoke,
Activates diffusion combustion and maintains strong turbulence until the latter stage of combustion,
Furthermore, it is necessary to keep the turbulent vortices in a fine state.
However, since diffusion combustion occurs in the expansion stroke, the air flow in the cylinder is generally attenuated at that point, and the effect of combustion activation due to turbulence such as intake swirl given during the compression stroke becomes relatively small. Also, in the case of high pressure injection, the turbulence intensity of the flame is high at the beginning of diffusion combustion,
In the latter stage of combustion, it decays and does not differ much from low-pressure injection.
【0006】これを解決するために、シリンダヘッド内
に燃焼攪乱室を設け、この室に燃焼後期に少量の燃料を
噴射し、前記室内で生成した高圧燃焼ガスを燃焼室に噴
出させる方式や、燃焼室内に直接COガスを噴射する方
式が提案されているが、装置が複雑、大型化するという
問題を有している。In order to solve this, a combustion disturbance chamber is provided in the cylinder head, a small amount of fuel is injected into this chamber in the latter stage of combustion, and the high pressure combustion gas generated in the chamber is jetted into the combustion chamber. Although a method of directly injecting CO gas into the combustion chamber has been proposed, it has a problem that the device becomes complicated and becomes large in size.
【0007】この問題を解決するために、本発明者は、
前記燃料噴射弁を用いて噴霧内部の濃度分布を観察する
実験を行った。図14は実験装置の概略構成図であり、
111は高圧容器、112は観察用窓、113は燃料噴
射弁、114は真空ポンプ、115は窒素ガスボンベ、
116はイメージ変換カメラ、117は燃料供給装置、
118は噴射制御装置、119はレーザ制御装置、12
0は銅蒸気レーザを示し、高圧容器111内に噴射され
た噴霧にレーザ光を照射することにより、散乱光の状態
から噴霧内部の濃度分布を観察した。In order to solve this problem, the present inventor has
An experiment was conducted to observe the concentration distribution inside the spray using the fuel injection valve. FIG. 14 is a schematic configuration diagram of the experimental device,
111 is a high pressure container, 112 is an observation window, 113 is a fuel injection valve, 114 is a vacuum pump, 115 is a nitrogen gas cylinder,
116 is an image conversion camera, 117 is a fuel supply device,
118 is an injection control device, 119 is a laser control device, 12
Reference numeral 0 represents a copper vapor laser, and by irradiating the spray injected into the high-pressure container 111 with laser light, the concentration distribution inside the spray was observed from the state of scattered light.
【0008】図15は噴霧状態を説明するための図であ
り、噴霧の構造および現象は大きく4つの領域に分けら
れ領域Iでは噴霧は高濃度で殆ど広がらずに直進し、領
域IIでは直進したものが不安定に蛇行し始め、領域III
では蛇行が変形して枝構造となり進むにつれて枝は間隔
を変え、分裂や合体を繰り返し、或いは周囲から徐々に
液滴を剥ぎ取られてゆく。領域IVではもはや枝構造は失
われそれぞれの縞は周囲気体との間に発生した渦の影響
を受け、独自の挙動を示し複雑な分布をとる。このよう
に、噴霧内部は非常に不均一であり、液滴が集まった高
濃度の縞がいくつも見られ、この不均一の高濃度の部分
は、多量のスモークの生成へつながる。FIG. 15 is a diagram for explaining the spray state. The structure and phenomenon of the spray are roughly divided into four regions, and in region I, the spray goes straight with high concentration and hardly spreads, and in region II, it goes straight. Things began to meander insecurely, Region III
Then, as the meander deforms to form a branch structure, the branches change intervals, repeat division and coalescence, or gradually drop droplets from the surroundings. In Region IV, the branch structure is no longer present and each fringe is affected by the vortex generated between it and the surrounding gas, and exhibits unique behavior and a complicated distribution. Thus, the inside of the spray is very non-uniform, and several high-density stripes of droplets are seen, and this non-uniform high-density portion leads to the production of a large amount of smoke.
【0009】上記実験において、噴霧内に金網を配置す
ると、噴霧内に大きな乱れを発生させ、高濃度の縞が小
さく、また噴霧も大きく拡がることが判明した。すなわ
ち、濃度分布としては均一に近く、かつ周囲気体を多く
取り込んで濃度も低くなる。In the above experiment, it was found that when a wire net was placed in the spray, a large turbulence was generated in the spray, a high-concentration fringe was small, and the spray was also spread widely. In other words, the concentration distribution is almost uniform, and a large amount of ambient gas is taken in, so that the concentration becomes low.
【0010】本発明は、上記問題、課題を解決するもの
であって、噴霧の乱れを促進させると同時に火炎の乱れ
を促進させることにより、噴霧と空気との混合を活発化
し、スモークの発生を低レベルに維持しつつ、NOX を
大幅に低減できる直接噴射式ディーゼル機関の燃焼室を
提供することを目的とする。The present invention solves the above problems and problems, and promotes the turbulence of the spray and the turbulence of the flame at the same time, thereby activating the mixing of the spray and the air, thereby causing the generation of smoke. An object of the present invention is to provide a combustion chamber of a direct injection diesel engine capable of significantly reducing NO X while maintaining the low level.
【0011】[0011]
【課題を解決するための手段】そのために本発明の直接
噴射式ディーゼル機関の燃焼室は、シリンダヘッド5に
設けられた燃料噴射弁6と、該燃料噴射弁6のノズル7
に形成された複数の噴孔と、ピストン1の上部に窪み部
を有するように形成された燃焼室1bと、該燃焼室1b
の外周壁1aと噴孔の間に前記ノズル7を囲むように燃
焼室上に立設された複数の中間壁1cと、該中間壁の間
に設けられたメッシュ部材11とを備え、前記噴孔から
噴射される噴霧を前記メッシュ部材11に衝突させるよ
うに構成したことを特徴とする。なお、前記メッシュ部
材を円筒形状またはボックス形状としてもよいし、ピス
トン1の上面に水平状のメッシュ部材を付加してもよ
い。ここで、上記構成に付加した番号は、本発明の理解
を容易にするために図面と対比させるためのもので、こ
れにより本発明の構成が何ら限定されるものではない。For this purpose, the combustion chamber of the direct injection type diesel engine of the present invention is provided with a fuel injection valve 6 provided on a cylinder head 5 and a nozzle 7 of the fuel injection valve 6.
A plurality of injection holes, a combustion chamber 1b formed so as to have a depression in the upper portion of the piston 1, and the combustion chamber 1b.
A plurality of intermediate walls 1c standing on the combustion chamber so as to surround the nozzle 7 between the outer peripheral wall 1a and the injection holes, and a mesh member 11 provided between the intermediate walls. It is characterized in that the spray injected from the holes collides with the mesh member 11. The mesh member may have a cylindrical shape or a box shape, or a horizontal mesh member may be added to the upper surface of the piston 1. Here, the numbers added to the above configuration are for comparison with the drawings in order to facilitate understanding of the present invention, and the configuration of the present invention is not limited thereby.
【0012】[0012]
【作用】本発明においては、例えば図1に示すように、
ノズル7の噴孔から噴射された噴霧は、メッシュ部材1
1に衝突し噴霧内に大きな乱れを発生させ、空気との混
合を促進させながら、外周壁1aに衝突して着火、燃焼
する。また、図4に示すように、ノズル7の噴孔から噴
射された燃料はA方向からメッシュ部材11に衝突し、
噴霧内に大きな乱れを発生させ、空気との混合を促進さ
せながら、外周壁1aに衝突して着火、燃焼した後、火
炎は左右のB、C方向に拡がると同時に、D方向のシリ
ンダヘッド5側に拡がり、再びメッシュ部材11を通過
することにより、火炎の乱れを促進させ、火炎と空気と
の混合を活発化しスモークを低レベルに抑える。In the present invention, for example, as shown in FIG.
The spray injected from the injection hole of the nozzle 7 is the mesh member 1
1 to generate a large turbulence in the spray, promote the mixing with air, and collide with the outer peripheral wall 1a to ignite and burn. Further, as shown in FIG. 4, the fuel injected from the injection hole of the nozzle 7 collides with the mesh member 11 from the A direction,
After generating a large turbulence in the spray and promoting mixing with air, after colliding with the outer peripheral wall 1a and igniting and burning, the flame spreads in the left and right B and C directions, and at the same time, the cylinder head 5 in the D direction. By spreading to the side and passing through the mesh member 11 again, the turbulence of the flame is promoted, the mixture of the flame and air is activated, and the smoke is suppressed to a low level.
【0013】[0013]
【実施例】以下、本発明の実施例を図面を参照しつつ説
明する。図1は本発明の直接噴射式ディーゼル機関の燃
焼室の1実施例を示し、図Aは斜視図、図Bは図AのB
−B線に沿って矢印方向に見た断面図である。Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 shows an embodiment of a combustion chamber of a direct injection type diesel engine of the present invention. FIG. A is a perspective view and FIG. B is B of FIG.
It is sectional drawing seen in the arrow direction along the -B line.
【0014】1はピストン、2はピストンリング、3は
シリンダライナー、4はガスケット、5はシリンダヘッ
ド、6はノズル7を有する燃料噴射弁を示し、ノズル7
には、燃料を噴射する複数の噴孔が形成されている。ピ
ストン1は、頂部に形成される外周壁1aと、その内側
に窪み部を有するように形成される燃焼室1bと、燃焼
室1b上にノズル7を囲むように同心状に立設される複
数の中間壁1cとを有し、各中間壁1cの間にメッシュ
状のメッシュ部材11が固定される。そして、ノズル7
の噴孔から噴射される各噴霧がそれぞれメッシュ部材1
1に衝突するように配置する。メッシュ部材11は、ス
テンレス等の耐熱性、耐久性を有する材料からなる。Reference numeral 1 is a piston, 2 is a piston ring, 3 is a cylinder liner, 4 is a gasket, 5 is a cylinder head, 6 is a fuel injection valve having a nozzle 7, and the nozzle 7 is a nozzle.
Has a plurality of injection holes for injecting fuel. The piston 1 includes an outer peripheral wall 1a formed at the top, a combustion chamber 1b formed so as to have a recessed portion inside thereof, and a plurality of concentrically erected on the combustion chamber 1b so as to surround the nozzle 7. The intermediate mesh wall 1c and the intermediate mesh wall 1c, and the mesh-like mesh member 11 is fixed between the intermediate walls 1c. And the nozzle 7
Each of the sprays injected from the injection holes of the mesh member 1
Arrange so as to collide with 1. The mesh member 11 is made of a material having heat resistance and durability such as stainless steel.
【0015】上記構成からなる本実施例の作用について
説明すると、ノズル7の噴孔から噴射された噴霧は、メ
ッシュ部材11に衝突し噴霧内に大きな乱れを発生さ
せ、空気との混合を促進させながら、外周壁1aに衝突
して着火、燃焼するので、スモークの発生を低レベルに
抑えることができる。The operation of the present embodiment having the above-mentioned structure will be described. The spray injected from the injection hole of the nozzle 7 collides with the mesh member 11 to generate a large turbulence in the spray, which promotes mixing with air. However, since it collides with the outer peripheral wall 1a and is ignited and burned, the generation of smoke can be suppressed to a low level.
【0016】図2は本発明の他の実施例を示し、図Aは
斜視図、図Bは図AのB−B線に沿って矢印方向に見た
断面図、図Cはメッシュ部材の分解斜視図である。な
お、以下の実施例においては、図1の実施例と同一の構
成については同一番号を付けて説明を省略する。本実施
例においては、メッシュ部材11を底部に固定用フラン
ジ11aを有する円筒形状とし、固定用フランジ11a
を固定用プレート12を介して固定用ビス13によりピ
ストン1に固定している。FIG. 2 shows another embodiment of the present invention, FIG. A is a perspective view, FIG. B is a sectional view taken along the line BB of FIG. A in the direction of the arrow, and FIG. C is an exploded view of the mesh member. It is a perspective view. In the following embodiments, the same configurations as those of the embodiment of FIG. In this embodiment, the mesh member 11 has a cylindrical shape having a fixing flange 11a at the bottom, and the fixing flange 11a is formed.
Is fixed to the piston 1 by a fixing screw 13 via a fixing plate 12.
【0017】図3は本発明の参考例を示し、図Aは平面
図、図Bは図AのB−B線に沿って矢印方向に見た断面
図、図Cは斜視図である。本例においては、ピストン1
の中央部に主燃焼室1dを設け、主燃焼室1dの外周に
これと連通する複数の副燃焼室1eを設け、主燃焼室1
dと副燃焼室1eの境界部にメッシュ部材11を設けた
例を示している。FIG. 3 shows a reference example of the present invention, FIG. A is a plan view, FIG. B is a sectional view taken along the line BB of FIG. A in the direction of the arrow, and FIG. C is a perspective view. In this example, the piston 1
The main combustion chamber 1d is provided at the center of the main combustion chamber 1d, and a plurality of auxiliary combustion chambers 1e communicating with the main combustion chamber 1d are provided at the outer periphery of the main combustion chamber 1d.
An example in which the mesh member 11 is provided at the boundary between the d and the auxiliary combustion chamber 1e is shown.
【0018】図4は本発明のさらに他の実施例を示し、
図Aは斜視図、図Bは図AのB−B線に沿って矢印方向
に見た断面図、図Cはメッシュ部材の斜視図、図D、図
Eはメッシュ部材の他の例を示す斜視図である。本実施
例においては、メッシュ部材11を円弧状のボックス形
状とし、側面と上面にメッシュを有し、ノズル7の噴孔
から噴射される各噴霧がそれぞれメッシュ部材11に衝
突するように配置する。メッシュ部材11には、前後方
向に固定用フランジ11a、11bを設け、固定用フラ
ンジ11aを固定用プレート12を介して固定用ビス1
3によりピストン1に固定し、固定用フランジ11bを
固定用リング14を介して固定用ビス15によりピスト
ン1の外周壁1aに固定している。なお、メッシュ部材
11の形状は、図Dに示すように、箱体形状、或いは図
Eに示すように、噴霧が当たる面を曲面形状としてもよ
い。FIG. 4 shows still another embodiment of the present invention,
FIG. A is a perspective view, FIG. B is a sectional view taken along the line BB of FIG. A as seen in the direction of the arrow, FIG. C is a perspective view of a mesh member, and FIGS. D and E show other examples of the mesh member. It is a perspective view. In the present embodiment, the mesh member 11 has an arc-shaped box shape, has meshes on the side surface and the upper surface, and is arranged so that each spray ejected from the injection hole of the nozzle 7 collides with the mesh member 11. The mesh member 11 is provided with fixing flanges 11a and 11b in the front-rear direction, and the fixing flange 11a is fixed to the fixing screw 1 via the fixing plate 12.
3, the fixing flange 11b is fixed to the outer peripheral wall 1a of the piston 1 by the fixing screw 15 via the fixing ring 14. The mesh member 11 may have a box shape as shown in FIG. D, or may have a curved surface as the surface on which the spray hits, as shown in FIG. E.
【0019】本実施例の作用について説明すると、ノズ
ル7の噴孔から噴射された噴霧は、図Cに示すように、
A方向からメッシュ部材11に衝突し噴霧内に大きな乱
れを発生させ、空気との混合を促進させながら、外周壁
1aに衝突して着火、燃焼した後、火炎は左右のB、C
方向に拡がると同時にD方向のシリンダヘッド側に拡が
り、再びメッシュ部材11を通過することにより、火炎
の乱れを促進させ火炎と空気との混合を活発化し、スモ
ークの発生を低レベルに抑える。The operation of this embodiment will be described. The spray injected from the injection hole of the nozzle 7 is as shown in FIG.
After colliding with the mesh member 11 from the A direction to generate a large turbulence in the spray and promoting mixing with air, the flame collides with the outer peripheral wall 1a and ignites and burns.
In the same direction, it spreads to the cylinder head side in the D direction and passes through the mesh member 11 again to accelerate the turbulence of the flame, activate the mixture of the flame and air, and suppress the generation of smoke to a low level.
【0020】図5は本発明のさらに他の実施例を示し、
図Aは斜視図、図Bは図AのB−B線に沿って矢印方向
に見た断面図、図Cはメッシュ部材の斜視図である。本
実施例が図3の実施例と相違する点は、メッシュ部材1
1の上面を曲面形状にした点である。FIG. 5 shows still another embodiment of the present invention,
FIG. A is a perspective view, FIG. B is a cross-sectional view taken along the line BB of FIG. A as seen in the direction of the arrow, and FIG. C is a perspective view of a mesh member. This embodiment is different from the embodiment of FIG. 3 in that the mesh member 1
The upper surface of 1 is a curved surface.
【0021】図6は本発明のさらに他の実施例を示し、
図Aは斜視図、図Bは図AのB−B線に沿って矢印方向
に見た断面図、図Cは分解斜視図である。本実施例にお
いては、側面および上面にメッシュを有するメッシュ部
材11をリング状の固定枠17に固着し、これをピスト
ン1の外周壁1a内に貫入し、その上面を固定用リング
14を介して固定用ビス15により固定している。FIG. 6 shows still another embodiment of the present invention,
FIG. A is a perspective view, FIG. B is a sectional view taken along the line BB of FIG. A as seen in the direction of the arrow, and FIG. C is an exploded perspective view. In this embodiment, the mesh member 11 having the mesh on the side surface and the upper surface is fixed to the ring-shaped fixed frame 17, and this is penetrated into the outer peripheral wall 1a of the piston 1, and the upper surface is fixed via the fixing ring 14. It is fixed by fixing screws 15.
【0022】図7は本発明のさらに他の実施例を示し、
図Aは斜視図、図Bは図AのB−B線に沿って矢印方向
に見た断面図、図Cはメッシュ部材の斜視図である。本
実施例においては、メッシュ部材11は、内周側に筒状
のメッシュ11cとこの筒状のメッシュ11cの外側上
面に形成される水平状メッシュ11dとを有し、固定用
フランジ11aを固定用プレート12を介して固定用ビ
ス13によりピストン1に固定し、固定用フランジ11
bを固定用リング14を介して固定用ビス15によりピ
ストン1の外周壁1aに固定している。FIG. 7 shows still another embodiment of the present invention,
FIG. A is a perspective view, FIG. B is a cross-sectional view taken along the line BB of FIG. A as seen in the direction of the arrow, and FIG. C is a perspective view of a mesh member. In the present embodiment, the mesh member 11 has a cylindrical mesh 11c on the inner peripheral side and a horizontal mesh 11d formed on the outer upper surface of the cylindrical mesh 11c, and the fixing flange 11a is fixed. It is fixed to the piston 1 by the fixing screw 13 via the plate 12, and the fixing flange 11
b is fixed to the outer peripheral wall 1a of the piston 1 by a fixing screw 15 via a fixing ring 14.
【0023】図8は本発明の参考例を示し、図Aは斜視
図、図Bは図AのB−B線に沿って矢印方向に見た断面
図である。本例は、図6の筒状のメッシュ11cを外周
壁1a側に近づけた例を示している。FIG. 8 shows a reference example of the present invention, FIG. A is a perspective view, and FIG. B is a sectional view taken along the line BB of FIG. This example shows an example in which the cylindrical mesh 11c of FIG. 6 is brought closer to the outer peripheral wall 1a side.
【0024】図9は本発明のさらに他の実施例を示し、
図Aは斜視図、図Bは図AのB−B線に沿って矢印方向
に見た断面図である。本実施例においては、図6のメッ
シュ部材11内部に径方向に複数のメッシュ11eを設
けている。FIG. 9 shows still another embodiment of the present invention,
FIG. A is a perspective view, and FIG. B is a sectional view taken along the line BB in FIG. In this embodiment, a plurality of meshes 11e are provided in the radial direction inside the mesh member 11 of FIG.
【0025】図10は本発明の参考例を示し、図Aは斜
視図、図Bは図AのB−B線に沿って矢印方向に見た断
面図である。本例においては、補強用ステー16上に張
られたメッシュを有するメッシュ部材11をピストン1
の上面のみに設けた例を示し、ピストン1の上昇または
下降時に噴霧は、メッシュA部に当たり混合が促進さ
れ、B部のメッシュにより上方への火炎の乱れが促進さ
れる。FIG. 10 shows a reference example of the present invention, FIG. A is a perspective view, and FIG. B is a sectional view taken along the line BB of FIG. In this example, the mesh member 11 having a mesh stretched on the reinforcing stay 16 is attached to the piston 1
In this example, only when the piston 1 is moved up or down, the spray hits the mesh A portion to promote mixing, and the mesh in the portion B promotes upward turbulence of the flame.
【0026】図11は本発明の参考例を示し、図Aは斜
視図、図Bは図AのB−B線に沿って矢印方向に見た断
面図、図Cがメッシュ部材の斜視図である。本例は、リ
エントラント型ピストンへのメッシュ部材11の取付例
を示す。FIG. 11 shows a reference example of the present invention, FIG. A is a perspective view, FIG. B is a sectional view taken along the line BB of FIG. A in the direction of the arrow, and FIG. C is a perspective view of a mesh member. is there. This example shows an example of attaching the mesh member 11 to the reentrant piston.
【0027】図12は本発明の参考例を示す斜視図であ
り、図11の例の副燃焼室1e内に、固定用フランジ1
1aに設けられた筒状のメッシュ部材11を挿入し固定
用ビス13にて固定する例を示している。FIG. 12 is a perspective view showing a reference example of the present invention. The fixing flange 1 is provided in the auxiliary combustion chamber 1e of the example of FIG.
An example is shown in which the tubular mesh member 11 provided in 1a is inserted and fixed with fixing screws 13.
【0028】[0028]
【発明の効果】以上の説明から明らかなように本発明に
よれば、噴霧直後に燃料をメッシュ部材に衝突させるこ
とにより、噴霧の乱れを促進させると同時に火炎の乱れ
を促進させることにより、噴霧と空気との混合を活発化
し、スモークの発生を低レベルに維持しつつ、NOX を
大幅に低減できる。また、噴霧はメッシュ部材により冷
却されるとともに、メッシュ部材による触媒作用も加わ
ってNOX を大幅に低減できる。As is apparent from the above description, according to the present invention, the fuel is collided with the mesh member immediately after the spraying to promote the turbulence of the spray and at the same time to promote the turbulence of the flame, whereby the spray is produced. and intensified mixing of the air, while maintaining the generation of smoke at a low level, it is possible to significantly reduce the NO X. Further, the spray is cooled by the mesh member, and the catalytic action of the mesh member is added, so that NO X can be greatly reduced.
【図1】本発明の直接噴射式ディーゼル機関の燃焼室の
1実施例を示し、図Aは斜視図、図Bは図AのB−B線
に沿って矢印方向に見た断面図である。1 shows an embodiment of a combustion chamber of a direct injection type diesel engine of the present invention, FIG. A is a perspective view, and FIG. B is a sectional view taken along the line BB of FIG. .
【図2】本発明の他の実施例を示し、図Aは斜視図、図
Bは図AのB−B線に沿って矢印方向に見た断面図、図
Cはメッシュ部材の分解斜視図である。2 shows another embodiment of the present invention, FIG. A is a perspective view, FIG. B is a sectional view taken along the line BB of FIG. A in the direction of the arrow, and FIG. C is an exploded perspective view of a mesh member. Is.
【図3】本発明の参考例を示し、図Aは斜視図、図Bは
図AのB−B線に沿って矢印方向に見た断面図、図Cは
メッシュ部材の斜視図、図D、図Eはメッシュ部材の他
の例を示す斜視図である。3 shows a reference example of the present invention, FIG. A is a perspective view, FIG. B is a sectional view taken along the line BB of FIG. A in the direction of the arrow, FIG. C is a perspective view of a mesh member, and FIG. FIG. E is a perspective view showing another example of the mesh member.
【図4】本発明のさらに他の実施例を示し、図Aは斜視
図、図Bは図AのB−B線に沿って矢印方向に見た断面
図、図Cはメッシュ部材の斜視図である。4 shows another embodiment of the present invention, FIG. A is a perspective view, FIG. B is a sectional view taken along the line BB in FIG. A in the direction of the arrow, and FIG. C is a perspective view of a mesh member. Is.
【図5】本発明のさらに他の実施例を示し、図Aは斜視
図、図Bは図AのB−B線に沿って矢印方向に見た断面
図、図Cは分解斜視図である。5 shows another embodiment of the present invention, FIG. A is a perspective view, FIG. B is a sectional view taken along the line BB of FIG. A in the direction of the arrow, and FIG. C is an exploded perspective view. .
【図6】本発明のさらに他の実施例を示し、図Aは斜視
図、図Bは図AのB−B線に沿って矢印方向に見た断面
図、図Cはメッシュ部材の斜視図である。6 shows another embodiment of the present invention, FIG. A is a perspective view, FIG. B is a sectional view taken along the line BB of FIG. A in the direction of the arrow, and FIG. C is a perspective view of a mesh member. Is.
【図7】本発明のさらに他の実施例を示し、図Aは斜視
図、図Bは図AのB−B線に沿って矢印方向に見た断面
図である。7 shows another embodiment of the present invention, FIG. A is a perspective view, and FIG. B is a cross-sectional view taken along the line BB of FIG.
【図8】本発明の参考例を示し、図Aは斜視図、図Bは
図AのB−B線に沿って矢印方向に見た断面図である。8 shows a reference example of the present invention, FIG. A is a perspective view, and FIG. B is a cross-sectional view taken along the line BB of FIG.
【図9】本発明のさらに他の実施例を示し、図Aは斜視
図、図Bは図AのB−B線に沿って矢印方向に見た断面
図である。9 shows another embodiment of the present invention, FIG. A is a perspective view, and FIG. B is a sectional view taken along the line BB of FIG.
【図10】本発明の参考例を示し、図Aは斜視図、図B
は図AのB−B線に沿って矢印方向に見た断面図、図C
はメッシュ部材の斜視図である。10 shows a reference example of the present invention, FIG. A is a perspective view, and FIG.
Is a cross-sectional view taken along the line BB of FIG.
FIG. 4 is a perspective view of a mesh member.
【図11】本発明の参考例を示し、図Aは平面図、図B
は図AのB−B線に沿って矢印方向に見た断面図、図C
は斜視図である。11 shows a reference example of the present invention, FIG. A is a plan view, and FIG.
Is a cross-sectional view taken along the line BB of FIG.
Is a perspective view.
【図12】本発明の参考例を示す斜視図である。FIG. 12 is a perspective view showing a reference example of the present invention.
【図13】従来の直接噴射式ディーゼル機関の例を示
し、図Aは断面図、図Bは平面図である。FIG. 13 shows an example of a conventional direct injection diesel engine, FIG. A being a sectional view and FIG. B being a plan view.
【図14】本発明に係わる実験装置の概略構成図であ
る。FIG. 14 is a schematic configuration diagram of an experimental apparatus according to the present invention.
【図15】本発明の課題を説明するための噴霧状態を示
す図である。FIG. 15 is a diagram showing a spray state for explaining the problems of the present invention.
1…ピストン、1a…外周壁、1b…燃焼室、1c…中
間壁、5…シリンダヘッド、6…燃料噴射弁、7…ノズ
ル、11…メッシュ部材11a、11b…固定用フラン
ジ、12…固定用プレート13、15…固定用ビス、1
4…固定用リングDESCRIPTION OF SYMBOLS 1 ... Piston, 1a ... Outer peripheral wall, 1b ... Combustion chamber, 1c ... Intermediate wall, 5 ... Cylinder head, 6 ... Fuel injection valve, 7 ... Nozzle, 11 ... Mesh member 11a, 11b ... Fixing flange, 12 ... Fixing Plates 13, 15 ... Fixing screws, 1
4… Fixing ring
───────────────────────────────────────────────────── フロントページの続き (56)参考文献 実開 昭57−20528(JP,U) 実開 昭62−14127(JP,U) 実開 平4−127837(JP,U) ─────────────────────────────────────────────────── ─── Continuation of the front page (56) Bibliography Shown 57-20528 (JP, U) Shown 62-14127 (JP, U) Shown flat 4-127837 (JP, U)
Claims (4)
と、該燃料噴射弁のノズルに形成された複数の噴孔と、
ピストンの上部に窪み部を有するように形成された燃焼
室と、該燃焼室の外周壁と噴孔の間に前記ノズルを囲む
ように燃焼室上に立設された複数の中間壁と、該中間壁
の間に設けられたメッシュ部材とを備え、前記噴孔から
噴射される噴霧を前記メッシュ部材に衝突させるように
構成したことを特徴とする直接噴射式ディーゼル機関の
燃焼室。1. A fuel injection valve provided in a cylinder head, and a plurality of injection holes formed in a nozzle of the fuel injection valve,
A combustion chamber formed to have a depression at the top of the piston; a plurality of intermediate walls that are erected on the combustion chamber so as to surround the nozzle between the outer peripheral wall of the combustion chamber and the injection holes; A combustion chamber of a direct injection type diesel engine, comprising: a mesh member provided between the intermediate walls, wherein the spray injected from the injection hole collides with the mesh member.
と、該燃料噴射弁のノズルに形成された複数の噴孔と、
ピストンの上部に窪み部を有するように形成された燃焼
室と、該燃焼室の外周壁と噴孔の間に前記ノズルを囲む
ように燃焼室上に固定された円筒形状のメッシュ部材と
を備え、前記噴孔から噴射される噴霧を前記メッシュ部
材に衝突させるように構成したことを特徴とする直接噴
射式ディーゼル機関の燃焼室。2. A fuel injection valve provided in a cylinder head, a plurality of injection holes formed in a nozzle of the fuel injection valve,
A piston is provided with a combustion chamber formed to have a recessed portion in the upper portion, and a cylindrical mesh member fixed on the combustion chamber so as to surround the nozzle between the outer peripheral wall of the combustion chamber and the injection hole. A combustion chamber of a direct injection type diesel engine, wherein the spray injected from the injection hole is made to collide with the mesh member.
と、該燃料噴射弁のノズルに形成された複数の噴孔と、
ピストンの上部に窪み部を有するように形成された燃焼
室と、該燃焼室の外周壁と噴孔の間に前記ノズルを囲む
ように燃焼室上に固定されたボックス形状のメッシュ部
材とを備え、前記噴孔から噴射される噴霧を前記メッシ
ュ部材に衝突させるように構成したことを特徴とする直
接噴射式ディーゼル機関の燃焼室。3. A fuel injection valve provided in a cylinder head, a plurality of injection holes formed in a nozzle of the fuel injection valve,
A piston, and a box-shaped mesh member fixed on the combustion chamber so as to surround the nozzle between the outer peripheral wall of the combustion chamber and the injection hole. A combustion chamber of a direct injection type diesel engine, wherein the spray injected from the injection hole is made to collide with the mesh member.
材を固定したことを特徴とする請求項1ないし請求項3
のいずれかに記載の直接噴射式ディーゼル機関の燃焼
室。4. A horizontal mesh member is fixed to the upper surface of the piston, as claimed in any one of claims 1 to 3.
A combustion chamber of a direct injection diesel engine according to any one of 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4177985A JPH0826770B2 (en) | 1992-07-06 | 1992-07-06 | Combustion chamber of direct injection diesel engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4177985A JPH0826770B2 (en) | 1992-07-06 | 1992-07-06 | Combustion chamber of direct injection diesel engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0617651A JPH0617651A (en) | 1994-01-25 |
| JPH0826770B2 true JPH0826770B2 (en) | 1996-03-21 |
Family
ID=16040520
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4177985A Expired - Lifetime JPH0826770B2 (en) | 1992-07-06 | 1992-07-06 | Combustion chamber of direct injection diesel engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0826770B2 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9587606B2 (en) | 2015-04-13 | 2017-03-07 | Caterpillar Inc. | Ducted combustion systems utilizing tubular ducts |
| US9803538B2 (en) | 2015-04-13 | 2017-10-31 | Caterpillar Inc. | Ducted combustion systems utilizing duct structures |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20030005478A (en) * | 2001-07-09 | 2003-01-23 | 현대자동차주식회사 | Structure of piston |
| DE10254016A1 (en) * | 2002-11-19 | 2004-06-03 | Behr Gmbh & Co. Kg | Device for cooling charging air for turbocharger with first cooling stage has second cooling stage(s), cooling device with coolant circuit with evaporator and/or refrigerant circuit |
| CA2406209C (en) * | 2002-10-02 | 2007-04-17 | Westport Research Inc. | Direct injection combustion chamber geometry |
| DE102010027637A1 (en) * | 2010-07-19 | 2012-01-19 | Mtu Friedrichshafen Gmbh | Piston for internal combustion engines, and internal combustion engine for this purpose |
| JP7040309B2 (en) * | 2018-06-14 | 2022-03-23 | トヨタ自動車株式会社 | Diesel engine control system |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5720528U (en) * | 1980-07-11 | 1982-02-02 | ||
| JPS6214127U (en) * | 1985-07-10 | 1987-01-28 | ||
| JP2525744Y2 (en) * | 1991-05-16 | 1997-02-12 | 日野自動車工業株式会社 | Diesel engine pistons |
-
1992
- 1992-07-06 JP JP4177985A patent/JPH0826770B2/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9587606B2 (en) | 2015-04-13 | 2017-03-07 | Caterpillar Inc. | Ducted combustion systems utilizing tubular ducts |
| US9803538B2 (en) | 2015-04-13 | 2017-10-31 | Caterpillar Inc. | Ducted combustion systems utilizing duct structures |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0617651A (en) | 1994-01-25 |
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