JP2536351B2 - Direct injection internal combustion engine - Google Patents
Direct injection internal combustion engineInfo
- Publication number
- JP2536351B2 JP2536351B2 JP3251809A JP25180991A JP2536351B2 JP 2536351 B2 JP2536351 B2 JP 2536351B2 JP 3251809 A JP3251809 A JP 3251809A JP 25180991 A JP25180991 A JP 25180991A JP 2536351 B2 JP2536351 B2 JP 2536351B2
- Authority
- JP
- Japan
- Prior art keywords
- fuel
- combustion chamber
- injection
- peripheral wall
- inner peripheral
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0696—W-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder wall
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0648—Means or methods to improve the spray dispersion, evaporation or ignition
- F02B23/0651—Means or methods to improve the spray dispersion, evaporation or ignition the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0669—Details related to the fuel injector or the fuel spray having multiple fuel spray jets per injector nozzle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0678—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
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/14—Direct injection into combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
- F02B23/0621—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
- 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)
- Fuel-Injection Apparatus (AREA)
Description
【0001】[0001]
【産業上の利用分野】本発明は、燃焼室に直接燃料を噴
射させて燃焼させる直噴式内燃機関に関するものであ
る。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a direct injection type internal combustion engine in which fuel is directly injected into a combustion chamber for combustion.
【0002】[0002]
【従来の技術】燃焼室に直接燃料を噴射させて燃焼させ
る内燃機関(ディーゼルエンジン)として、直噴式内燃
機関が知られている。2. Description of the Related Art A direct injection type internal combustion engine is known as an internal combustion engine (diesel engine) in which fuel is directly injected into a combustion chamber for combustion.
【0003】図20及び図21に示すように、従来この
種の直噴式内燃機関は、ピストン1の頂部2に適宜窪ま
されたキャビティとして区画形成された燃焼室3と、シ
リンダヘッド4に設けられてこの燃焼室3に燃料を噴射
させるための燃料噴射ノズル5とを備えて構成されてい
る。燃料噴射ノズル5の先端には、燃焼室3の周側壁6
に対向するように適宜配置された噴孔7が形成され、燃
料ポンプ(図示せず)からの燃料を所定の圧力で噴射さ
せるようになっている。またその燃料の噴霧Lの形状
は、燃焼室3の形に合うようにして、できるだけどの方
向にも燃料を均等に分布させるようになっている。噴射
された燃料は、燃焼室3内に取り入れられた空気と適宜
混合されて、噴霧Lの先端側(周側壁6付近)から着火
され、中心(燃料噴射ノズル5付近)へと燃焼が進行し
て、所望の燃焼が得られるようになっている。As shown in FIGS. 20 and 21, a conventional direct injection type internal combustion engine of this type is provided in a cylinder head 4 and a combustion chamber 3 defined as a cavity which is appropriately recessed in a top portion 2 of a piston 1. A fuel injection nozzle 5 for injecting fuel into the lever combustion chamber 3 is provided. A peripheral side wall 6 of the combustion chamber 3 is provided at the tip of the fuel injection nozzle 5.
Is formed so as to oppose each other, and fuel from a fuel pump (not shown) is injected at a predetermined pressure. Further, the shape of the fuel spray L matches the shape of the combustion chamber 3, so that the fuel is evenly distributed in any direction as much as possible. The injected fuel is appropriately mixed with the air taken into the combustion chamber 3, ignited from the tip side of the spray L (near the peripheral side wall 6), and the combustion proceeds to the center (near the fuel injection nozzle 5). Thus, the desired combustion can be obtained.
【0004】また噴霧Lと空気とをよく混合させて良好
な燃焼を得るために、燃焼室3内の空気に適度な乱れ
(スワール,スキッシュ)を生じさせるための構成も種
々提案されている。In order to mix the spray L and air well to obtain good combustion, various structures have been proposed for producing appropriate turbulence (swirl, squish) in the air in the combustion chamber 3.
【0005】[0005]
【発明が解決しようとする課題】ところで近来にあって
は、燃料を完全に霧化させてスモーク,パティキュレー
トの低い燃焼を得るべく、噴射圧力を出来るかぎり高く
することが行われている。しかしながら、噴射圧力を過
度に高くすると均一な燃焼が行われなくなって、高温度
燃焼或いは過度な圧力上昇に起因するNOX が発生して
しまうという問題があった。By the way, recently, in order to completely atomize the fuel and obtain combustion with low smoke and particulates, the injection pressure is made as high as possible. However, if the injection pressure is excessively increased, uniform combustion is not performed, and there is a problem that NO X is generated due to high temperature combustion or excessive pressure rise.
【0006】そこで本発明は、上記事情に鑑み、スモー
ク,パティキュレートの低減と同時に、NOX を低減さ
せることのできる直噴式内燃機関を提供すべく創案され
たものである。なお、本発明に関連する従来技術として
は、実開昭59−150943号公報及び実開昭62−
135号公報がある。 [0006] The present invention has been made in view of the above circumstances, smoke, at the same time as the reduction of particulates, it was conceived to provide a direct injection internal combustion engine which can reduce the NO X. As a conventional technique related to the present invention,
No. 59-150943 and 62-62.
There is a 135 publication.
【0007】[0007]
【課題を解決するための手段】本発明は、ピストン頂部
に窪まされたキャビティにより形成された燃焼室と燃焼
室に高圧で燃料を噴射する燃料噴射ノズルとを有した直
噴式内燃機関において、キャビティの周側壁から所定の
間隔を隔てて設けられ、燃焼室を径方向内方の内側燃焼
室と周側壁との間の外側燃焼室とに区画する内周壁体
と、内周壁体の一部が適宜切り欠かれて成る切欠部と、
燃料噴射ノズルに設けられ切欠部を通して周側壁へ燃料
を噴射するための第一噴孔と、第一噴孔とともに燃料噴
射ノズルに設けられ、内側燃焼室が外側燃焼室よりも燃
料が濃い空燃比となるように内周壁体に燃料を噴射する
と共に外側燃焼室と同時着火するように第一噴孔よりも
小さい開口面積で形成された第二噴孔とを備えたもので
ある。SUMMARY OF THE INVENTION The present invention is directed to a combustion chamber and combustion formed by a cavity recessed in the top of the piston.
Direct injection with a fuel injection nozzle for injecting fuel at high pressure into the chamber
In injection internal combustion engine,
Inner combustion of the combustion chamber radially inwardly provided with a space
Inner peripheral wall body that divides into an outer combustion chamber between the chamber and the peripheral side wall
And a notch formed by appropriately notching a part of the inner peripheral wall body,
Fuel is injected to the peripheral wall through the notch provided in the fuel injection nozzle.
The first injection hole for injecting
It is installed in the injection nozzle, and the inner combustion chamber burns more than the outer combustion chamber.
Fuel is injected into the inner wall so that the fuel has a rich air-fuel ratio
With the first injection hole so that it simultaneously ignites with the outer combustion chamber
And a second injection hole formed with a small opening area .
【0008】また上記内側燃焼室は、第二噴孔に対向す
るように設けられた突起及びこの突起の対向する面に形
成され内周壁体の適宜位置へ向けられた溝を有して構成
されるのが望ましい。Further, the inner combustion chamber has a projection provided so as to face the second injection hole and a groove formed on an opposite surface of the projection and directed to an appropriate position of the inner peripheral wall body. Is desirable.
【0009】[0009]
【作用】上記構成によって、燃焼室の周側壁に第一噴孔
から燃料が噴射されると共に内側燃焼室に第二噴孔から
の噴霧が供給され、周側壁及び内周壁体の内側近傍にて
同時に着火される。内側燃焼室のガスは内周壁体を越え
て押し出され、未燃分が空気と撹乱されて混合が促進さ
れると共に二段燃焼される。With the above structure, the fuel is injected from the first injection hole to the peripheral side wall of the combustion chamber, and the spray from the second injection hole is supplied to the inner side combustion chamber. It is ignited at the same time. The gas in the inner combustion chamber is pushed out over the inner peripheral wall, and the unburned components are disturbed with the air to promote mixing, and the two-stage combustion is performed.
【0010】また内側燃焼室が突起及び溝を有した構成
によって、第二噴孔から噴射された燃料は突起に衝突し
た後、溝に導かれて内周壁体の所定位置へと拡散され
る。Further, since the inner combustion chamber has the projection and the groove, the fuel injected from the second injection hole collides with the projection and is guided to the groove and diffused to a predetermined position of the inner peripheral wall.
【0011】[0011]
【実施例】以下、本発明の実施例を添付図面に従って説
明する。Embodiments of the present invention will be described below with reference to the accompanying drawings.
【0012】図1及び図2は、本発明に係わる直噴式内
燃機関の第一の実施例を示したものである。1 and 2 show a first embodiment of a direct injection type internal combustion engine according to the present invention.
【0013】この直噴式内燃機関は、ピストン1の頂部
2に窪まされたキャビティ11の周側壁12よりも径方
向内方に形成されて内側燃焼室13を区画する内周壁体
14を有した燃焼室15と、周側壁12へ燃料を噴射さ
せる第一噴孔16及び内側燃焼室13に臨む第二噴孔1
7を有した燃料噴射ノズル18とにより主として構成さ
れている。This direct injection type internal combustion engine has a combustion having an inner peripheral wall body 14 which is formed radially inward of a peripheral side wall 12 of a cavity 11 recessed in a top portion 2 of a piston 1 to define an inner combustion chamber 13. The chamber 15, the first injection hole 16 for injecting fuel to the peripheral side wall 12, and the second injection hole 1 facing the inner combustion chamber 13.
7 and a fuel injection nozzle 18 having a fuel injection nozzle 7.
【0014】キャビティ11は、平面視上円形を呈し、
その底面19は、周側壁12近傍で最も深く、中央へ向
かって単調に上昇傾斜して、燃料噴射ノズル18の真下
の位置で最も浅くなるように形成されている。そして周
側壁12と内周壁体14とは所定の間隔が隔てられてお
り、その間に、内側燃焼室13を囲むような外側燃焼室
20が区画されていることになる。The cavity 11 has a circular shape in plan view,
The bottom surface 19 is formed so that it is deepest in the vicinity of the peripheral side wall 12, monotonically inclined upward toward the center, and becomes shallowest at a position directly below the fuel injection nozzle 18. The peripheral side wall 12 and the inner peripheral wall 14 are separated by a predetermined distance, and the outer combustion chamber 20 surrounding the inner combustion chamber 13 is defined between them.
【0015】内周壁体14は、周側壁12と同心状の円
形を呈して形成され、そのうちの一部が、等間隔に四箇
所切り欠かれている。本実施例にあっては、図3に示す
ように、上端から下端まで矩形状に切り通された切欠部
21が形成されている。The inner peripheral wall body 14 is formed in a circular shape concentric with the peripheral side wall 12, and a part of the inner peripheral wall body 14 is cut out at four equal intervals. In the present embodiment, as shown in FIG. 3, a notch 21 is formed which is cut in a rectangular shape from the upper end to the lower end.
【0016】燃料噴射ノズル18の第一噴孔16は、切
欠部21に正対するように四個配置されており、この切
欠部21を通って周側壁12に達する噴霧L1 を形成す
るようになっている。また第二噴孔17は、切欠部21
の間の内周壁体14に向けて位置されている。従って、
第二噴孔17及び第一噴孔16は、交互に等間隔に合計
8 個周設されていることになる。The four first injection holes 16 of the fuel injection nozzle 18 are arranged so as to face the notch 21 and form the spray L 1 which reaches the peripheral side wall 12 through the notch 21. Has become. Further, the second injection hole 17 has a cutout portion 21.
It is located toward the inner peripheral wall body 14 between. Therefore,
The second injection holes 17 and the first injection holes 16 are alternately added up at equal intervals.
It means that there are eight laps.
【0017】 そして図4に示すように、第二噴孔17
は、第一噴孔16よりも小さい開口面積で成り、内周壁
体14に到達して着火するような噴霧L 2 を形成するよ
うになっている。また内側燃焼室13における空燃比
(空気/燃料)は、公知の副室式内燃機関の副室におけ
るものと同様に、比較的燃料が濃くなるように、すなわ
ち外側燃焼室20よりも燃料が濃い空燃比となるように
設定され、二段燃焼がなされるようになっている。Then, as shown in FIG. 4, the second injection hole 17
Has an opening area smaller than that of the first injection hole 16 and forms a spray L 2 which reaches the inner peripheral wall 14 and is ignited. Air-fuel ratio (air / fuel) also in the inner combustion chamber 13, similar to those in sub-chamber of the known pre-combustion chamber internal combustion engine, so that relatively fuel becomes darker, Sunawa
The fuel is set to have an air-fuel ratio that is richer than that of the outer combustion chamber 20 , and two-stage combustion is performed.
【0018】次に実施例の作用を説明する。Next, the operation of the embodiment will be described.
【0019】ピストン1が上死点に達したタイミング
で、燃料噴射ノズル18の各噴孔16,17から所定の
高圧力で燃料が噴射され、第一噴孔16からの噴霧L1
が周側壁12に達してその近傍で着火される。同時に第
二噴孔17からの噴霧L2 は、内周壁体14に達して着
火される。空燃比の小さい内側燃焼室13のガスは、そ
の燃焼圧力により内周壁体14を越えて押し出されて全
体燃焼となり、温度勾配の急激な上昇のない二段燃焼が
なされると共に、その未燃分が外側燃焼室20の未燃分
と共に空気と撹乱されて、混合が促進される。このと
き、火炎(既燃焼ガス)の巻き込みにより排気が還流さ
れた形になって、燃焼温度の低下がなされる。At the timing when the piston 1 reaches the top dead center, fuel is injected from the injection holes 16 and 17 of the fuel injection nozzle 18 at a predetermined high pressure, and the spray L 1 from the first injection hole 16 is reached.
Reaches the peripheral side wall 12 and is ignited in the vicinity thereof. At the same time, the spray L 2 from the second injection hole 17 reaches the inner peripheral wall body 14 and is ignited. The gas in the inner combustion chamber 13 having a small air-fuel ratio is pushed out over the inner peripheral wall body 14 by the combustion pressure to become a total combustion, and a two-stage combustion without a sharp rise in the temperature gradient is performed and the unburned gas Are disturbed with the air together with the unburned matter in the outer combustion chamber 20, and the mixing is promoted. At this time, the exhaust gas is recirculated by the inclusion of the flame (burned gas), and the combustion temperature is lowered.
【0020】このように、キャビティ11内に立設させ
た内周壁体14により二重の燃焼室13,20を区画
し、開口面積の異なる噴孔16,17を有した燃料噴射
ノズル18により周側壁12及び内周壁体14に燃料を
噴射させるようにしたので、供給された燃料はキャビテ
ィ11内の径方向外方と内方とで同時に着火されると共
に、二段燃焼及び火炎の吹き出しによる混合促進がなさ
れて、均一で良好な燃焼が達成される。すなわち、高圧
燃料噴射によるスモーク,パティキュレートの低減が達
成されると共に、NOX の低減が達成される。そして火
炎の巻き込みにより、いわば内部EGR(Exhaust Gas
Recirculation )が作用して、より一層のNOX 低減が
期待できる。As described above, the inner combustion chamber 14 is erected in the cavity 11 to divide the double combustion chambers 13 and 20, and the fuel injection nozzle 18 having the injection holes 16 and 17 having different opening areas surrounds the combustion chambers 13 and 20. Since the fuel is injected to the side wall 12 and the inner peripheral wall body 14, the supplied fuel is simultaneously ignited radially outward and inward in the cavity 11, and is mixed by the two-stage combustion and flame blowing. Acceleration is made to achieve uniform and good combustion. That is, the reduction of smoke and particulates due to the high-pressure fuel injection and the reduction of NO X are achieved. Then, due to the involvement of the flame, the internal EGR (Exhaust Gas)
Recirculation) acts, more of the NO X reduction can be expected.
【0021】次に図5及び図6によって、本発明の第二
の実施例を説明する。Next, a second embodiment of the present invention will be described with reference to FIGS.
【0022】この実施例においては、燃焼室31の内周
壁体32の切欠部33が、上端から半円形状に切り欠か
れて形成されている(図7参照)。この切欠部33の大
きさは、第一噴孔16からの噴霧L1 が通過する時点で
の大きさに相当するものであって、内側燃焼室13にお
ける二段燃焼などの作用が充分に発揮できるようになっ
ている。In this embodiment, the notch 33 of the inner peripheral wall 32 of the combustion chamber 31 is formed by notching in a semicircular shape from the upper end (see FIG. 7). The size of the notch 33 corresponds to the size at the time when the spray L 1 from the first injection hole 16 passes, and the action such as the two-stage combustion in the inner combustion chamber 13 is sufficiently exerted. You can do it.
【0023】その他の構成及び作用効果は、前記第一の
実施例と同様なので、同一の符号を付し、説明を省略す
る。Other constitutions and effects are the same as those of the first embodiment, and therefore, the same reference numerals are given and the description thereof will be omitted.
【0024】なお上記第一及び第二実施例にあっては、
燃焼室15,31の上端開口縁が略垂直に切り立った形
状としたが、公知のリエントラント型燃焼室のように、
棚部を設けるようにしてもよい。この場合、図8に示す
ように内周壁体41にのみ棚部42を設ける構成、また
図9に示すように周側壁51にのみ棚部52を設ける構
成、さらに図10に示すように内周壁体61及び周側壁
62の双方にそれぞれ棚部63,64を設ける構成が考
えられる。これら棚部42,52,63,64によっ
て、各燃焼室13,20内には圧縮行程の終期に所定の
強さのスキッシュ(軸方向の空気の乱れ)が形成され、
燃料と空気との混合がより一層促進されて、良好な燃焼
に貢献できる。In the above first and second embodiments,
Although the upper opening edges of the combustion chambers 15 and 31 are formed to rise substantially vertically, like a known reentrant combustion chamber,
You may make it provide a shelf. In this case, as shown in FIG. 8, a configuration in which the shelf portion 42 is provided only on the inner peripheral wall body 41, a configuration in which the shelf portion 52 is provided only at the peripheral side wall 51 as shown in FIG. 9, and as shown in FIG. A configuration in which shelves 63 and 64 are provided on both the body 61 and the peripheral side wall 62 can be considered. These shelves 42, 52, 63, 64 form a squish (air turbulence in the axial direction) of a predetermined strength at the end of the compression stroke in each combustion chamber 13, 20.
The mixing of fuel and air is further promoted, which contributes to good combustion.
【0025】さらに以上実施例では円形のキャビティで
区画された燃焼室を示したが、図11に示すように角形
のキャビティ71であっても本発明は適用できる。この
場合の内周壁体72は、キャビティ71の周壁73と相
似形状の正方形に連ねることができ、その角の部分に切
欠部74が形成される。従って内部燃焼室75も角形に
区画されるものである。なお燃料噴射ノズル(図示せ
ず)による噴霧供給は、前記実施例と同様に行うことが
できる。また図12に示すように、円形のキャビティ1
1に正方形状の内周壁体72を形成しても構わない。Further, in the above embodiment, the combustion chamber divided by the circular cavity is shown, but the present invention can be applied to the rectangular cavity 71 as shown in FIG. In this case, the inner peripheral wall body 72 can be connected in a square shape similar to the peripheral wall 73 of the cavity 71, and a cutout portion 74 is formed at a corner portion thereof. Therefore, the internal combustion chamber 75 is also divided into a rectangular shape. The spray supply by the fuel injection nozzle (not shown) can be performed in the same manner as in the above embodiment. Further, as shown in FIG. 12, the circular cavity 1
The inner peripheral wall 72 having a square shape may be formed in one.
【0026】次に図13及び図14によって、本発明の
第三の実施例を説明する。Next, a third embodiment of the present invention will be described with reference to FIGS.
【0027】この実施例は、前記第二の実施例と同様の
内周壁体32により区画形成された内側燃焼室81の中
央底部に、上面82が略平らな台状の突起83が設けら
れていると共に、燃料噴射ノズル84の第二噴孔85
が、この突起83に正対されて形成されているものであ
る。In this embodiment, a trapezoidal projection 83 having a substantially flat upper surface 82 is provided at the central bottom portion of an inner combustion chamber 81 defined by an inner peripheral wall 32 similar to the second embodiment. The second injection hole 85 of the fuel injection nozzle 84
Are formed so as to face the protrusions 83.
【0028】このように構成したことで、燃料の一部は
燃料噴射ノズル84の真下に噴射され、突起83の上面
82に衝突した後、略水平に屈折して万遍無く半径方向
に飛散し、横に偏平な噴霧L3 が形成される。すなわ
ち、噴射圧力を過度に増大させること無く噴霧の微細化
が達成されて、スモーク,パティキュレートの低減が為
し得る。With this structure, a part of the fuel is injected just below the fuel injection nozzle 84, collides with the upper surface 82 of the projection 83, and then is refracted substantially horizontally and scattered in the radial direction evenly. A horizontal spray L 3 is formed. That is, atomization of the spray can be achieved without excessively increasing the injection pressure, and smoke and particulates can be reduced.
【0029】その他の構成及び作用効果は、前記第二の
実施例と同様なので、同一の符号を付し、説明を省略す
る。The other constructions and effects are the same as those of the second embodiment, so the same reference numerals are given and the description thereof is omitted.
【0030】次に図15及び図16によって、本発明の
第四の実施例を説明する。Next, a fourth embodiment of the present invention will be described with reference to FIGS.
【0031】この実施例は、前記第三の実施例と同様な
台状の突起91が内側燃焼室92の中央底部に設けられ
ていると共に、燃料噴射ノズル94の第二噴孔99に対
向する面である上面93に、内周壁体94の所定位置に
向けられた溝95が形成されている。そして燃料噴射ノ
ズル96の第一噴孔97は等間隔に三個設けられてお
り、内周壁体94の切欠部98がこれにあわせて三箇所
に設けられ、溝95はこれら切欠部98同士の間の三方
向に、突起中央から放射状に延長されている。In this embodiment, a trapezoidal projection 91 similar to that of the third embodiment is provided in the central bottom portion of the inner combustion chamber 92 and faces the second injection hole 99 of the fuel injection nozzle 94. A groove 95 directed to a predetermined position of the inner peripheral wall body 94 is formed on the upper surface 93 which is a surface. The three first injection holes 97 of the fuel injection nozzle 96 are provided at equal intervals, and the cutout portions 98 of the inner peripheral wall body 94 are provided at three positions corresponding to the cutout portions 98, and the groove 95 is formed between these cutout portions 98. Radially extending from the center of the protrusion in three directions.
【0032】従って、第一噴孔97による噴霧L1 は直
接周側壁12まで達すると共に、真下に向けられた第二
噴孔99からの噴霧L4 は、突起91の上面93に衝突
した後、三方向に屈折されるように溝95に導かれて内
周壁体94に達する。そして内側燃焼室92のガスが内
周壁体94を越えて押し出されて全体燃焼となり、温度
勾配の急激な上昇のない二段燃焼がなされると共に、そ
の未燃分が外側燃焼室20の未燃分と共に空気と撹乱さ
れて、混合が促進される。Therefore, the spray L 1 from the first injection hole 97 directly reaches the peripheral side wall 12, and the spray L 4 from the second injection hole 99 which is directed directly below is collided with the upper surface 93 of the projection 91. The groove 95 is guided so as to be bent in three directions and reaches the inner peripheral wall body 94. Then, the gas in the inner combustion chamber 92 is pushed out over the inner peripheral wall body 94 to become the whole combustion, and the two-stage combustion without a sharp rise in the temperature gradient is performed, and the unburned portion thereof is unburned in the outer combustion chamber 20. Agitated with air along with the minutes to promote mixing.
【0033】このように、この実施例は一個の第二噴孔
99により内側燃焼室92内に放射状の噴霧が形成でき
るものであり、その方向及び噴霧の規模(周方向の幅)
を溝95で規制することが可能である。例えば図17に
示すように、スワールSの上流側に位置する溝101 を、
内周壁体94の中間位置から上流側にずれた位置102
に、最も下流側の溝103 は下流側にずれた位置104 に、
それらの間の溝105 は中間位置106 にそれぞれ向くよう
にすると共に、溝の太さ(幅)を下流側のものほど狭く
して、スワールSの強い側に比較的大きな噴霧L4 を形
成させる。これでスワールSによる燃料と空気との混合
が適切に促進される。As described above, in this embodiment, the radial spray can be formed in the inner combustion chamber 92 by the single second injection hole 99, and the direction and the scale of the spray (width in the circumferential direction).
Can be regulated by the groove 95. For example, as shown in FIG. 17, the groove 101 located on the upstream side of the swirl S is
Position 102 displaced from the middle position of the inner peripheral wall body 94 to the upstream side
In addition, the most downstream groove 103 is located at the position 104 displaced to the downstream side,
The grooves 105 between them are respectively directed to the intermediate position 106, and the thickness (width) of the grooves is made narrower toward the downstream side so that a relatively large spray L 4 is formed on the strong swirl side. . This properly promotes the mixing of fuel and air by the swirl S.
【0034】この他の作用効果は、前記第一及び第二の
実施例と同様である。Other functions and effects are similar to those of the first and second embodiments.
【0035】次に図18及び図19によって本発明の第
五の実施例を説明する。Next, a fifth embodiment of the present invention will be described with reference to FIGS.
【0036】この実施例は、前記第二の実施例と同様な
内周壁体111 が形成されていると共に、燃料噴射ノズル
112 の第一噴孔113 及び第二噴孔114 が、周側壁12及
び内周壁体111 に対して上下幅が小さい横扇形の噴霧L
5 ,L6 を形成するようになっている。そして内周壁体
111 に形成された切欠部115 は、その噴霧L5 に合わせ
た周方向に細長い形状になっている。In this embodiment, the same inner peripheral wall body 111 as that of the second embodiment is formed, and the fuel injection nozzle is also used.
The first injection hole 113 and the second injection hole 114 of 112 are horizontal fan-shaped spray L having a smaller vertical width with respect to the peripheral side wall 12 and the inner peripheral wall body 111.
5 and L 6 are formed. And inner wall
The notch 115 formed in 111 is elongated in the circumferential direction according to the spray L 5 .
【0037】このように構成したことで、噴霧L5 が通
る位置においても内周壁体91を比較的高く形成でき、
内側燃焼室13による二段燃焼などをより確実に機能さ
せることができる。With this structure, the inner wall 91 can be formed relatively high even at the position where the spray L 5 passes.
The two-stage combustion or the like by the inner combustion chamber 13 can be made to function more reliably.
【0038】その他の構成及び作用効果は、前記第二の
実施例と同様なので、同一の符号を付し、説明を省略す
る。The other constructions and effects are the same as those of the second embodiment, so the same reference numerals are given and the description thereof is omitted.
【0039】なお上記第三ないし第五実施例において
も、図8乃至図10に示した棚部42,52,63,6
4を設けることができるし、図11及び図12に示した
角型のキャビティ71或いは内側燃焼室75に適用する
ことも可能である。In the third to fifth embodiments, the shelves 42, 52, 63 and 6 shown in FIGS. 8 to 10 are also used.
4 can be provided, and it is also possible to apply to the rectangular cavity 71 or the inner combustion chamber 75 shown in FIGS. 11 and 12.
【0040】[0040]
【発明の効果】以上要するに本発明によれば、次のよう
な優れた効果を発揮する。In summary, according to the present invention, the following excellent effects are exhibited.
【0041】(1) 請求項1記載の構成によれば、噴射さ
れた燃料はキャビティの径方向内側及び外側で同時に着
火されると共に、二段燃焼及び火炎の吹き出しによる混
合促進がなされることで均一で良好な燃焼が達成され、
高圧燃料噴射によるスモーク,パティキュレートの低減
が達成されると共に、NOXの低減が達成される。(1) According to the configuration of claim 1, the injected fuel is simultaneously ignited inside and outside of the cavity in the radial direction, and the two-stage combustion and the flame blowout promote the mixing. Uniform and good combustion is achieved,
Smoke by the high-pressure fuel injection, with a reduction in particulates is achieved, reducing of the NO X is achieved.
【0042】(2) 請求項2記載の構成によれば、さら
に、内側燃焼室内における噴霧の分布を簡単にスワール
などに適応させることができ、良好な燃焼を促進でき
る。(2) According to the second aspect of the invention, the spray distribution in the inner combustion chamber can be easily adapted to swirl and the like, and good combustion can be promoted.
【図1】本発明に係わる直噴式内燃機関の第一の実施例
を示した平面図である。FIG. 1 is a plan view showing a first embodiment of a direct injection internal combustion engine according to the present invention.
【図2】図1のA−A線矢視断面図である。FIG. 2 is a sectional view taken along line AA of FIG.
【図3】図2のB−B線矢視断面図である。FIG. 3 is a sectional view taken along the line BB of FIG.
【図4】図1の燃焼噴射ノズルの噴孔を示した拡大図で
ある。FIG. 4 is an enlarged view showing injection holes of the combustion injection nozzle of FIG.
【図5】本発明の第二の実施例を示した平面図である。FIG. 5 is a plan view showing a second embodiment of the present invention.
【図6】図5のC−C線矢視断面図である。6 is a sectional view taken along the line CC of FIG.
【図7】図6のD−D線矢視断面図である。7 is a sectional view taken along the line DD of FIG.
【図8】図2及び図6の他の実施例を示した要部断面図
である。FIG. 8 is a cross-sectional view of essential parts showing another embodiment of FIGS. 2 and 6.
【図9】図2及び図6のその他の実施例を示した要部断
面図である。FIG. 9 is a cross-sectional view of essential parts showing another embodiment of FIGS. 2 and 6.
【図10】図2及び図6のさらにその他の実施例を示し
た要部断面図である。10 is a cross-sectional view of a main part showing still another embodiment of FIGS. 2 and 6. FIG.
【図11】図1及び図5の他の実施例を示した平面図で
ある。11 is a plan view showing another embodiment of FIGS. 1 and 5. FIG.
【図12】図1及び図5のその他の実施例を示した平面
図である。12 is a plan view showing another embodiment of FIGS. 1 and 5. FIG.
【図13】本発明の第三の実施例を示した平面図であ
る。FIG. 13 is a plan view showing a third embodiment of the present invention.
【図14】図13のE−E線矢視断面図である。FIG. 14 is a cross-sectional view taken along the line EE of FIG.
【図15】本発明の第四の実施例を示した平面図であ
る。FIG. 15 is a plan view showing a fourth embodiment of the present invention.
【図16】図15のH−H線矢視断面図である。16 is a sectional view taken along line HH of FIG.
【図17】図15の他の実施例を示した要部平面図であ
る。FIG. 17 is a plan view of a principal portion showing another embodiment of FIG.
【図18】本発明の第五の実施例を示した平面図であ
る。FIG. 18 is a plan view showing a fifth embodiment of the present invention.
【図19】図18のF−F線矢視断面図である。19 is a sectional view taken along the line FF of FIG.
【図20】従来の直噴式内燃機関を示した平面図であ
る。FIG. 20 is a plan view showing a conventional direct injection internal combustion engine.
【図21】図20のG−G線矢視断面図である。21 is a sectional view taken along the line GG of FIG.
2 ピストン頂部 11 キャビティ 12 周側壁 13 内側燃焼室 14 内周壁体 15 燃焼室 16 第一噴孔 17 第二噴孔 18 燃料噴射ノズル 91 突起 95 溝 2 Piston top part 11 Cavity 12 Peripheral side wall 13 Inner combustion chamber 14 Inner peripheral wall body 15 Combustion chamber 16 First injection hole 17 Second injection hole 18 Fuel injection nozzle 91 Protrusion 95 Groove
Claims (2)
より形成された燃焼室と該燃焼室に高圧で燃料を噴射す
る燃料噴射ノズルとを有した直噴式内燃機関において、
上記キャビティの周側壁から所定の間隔を隔てて設けら
れ、上記燃焼室を径方向内方の内側燃焼室と径方向外方
の外側燃焼室とに区画する内周壁体と、該内周壁体の一
部が適宜切り欠かれて成る切欠部と、上記燃料噴射ノズ
ルに設けられ上記切欠部を通して上記周側壁へ燃料を噴
射するための第一噴孔と、該第一噴孔とともに上記燃料
噴射ノズルに設けられ、上記内側燃焼室が上記外側燃焼
室よりも燃料が濃い空燃比となるように上記内周壁体に
燃料を噴射すると共に上記外側燃焼室と同時着火するよ
うに上記第一噴孔よりも小さい開口面積で形成された第
二噴孔とを備えたことを特徴とする直噴式内燃機関。 To 1. A cavity is recessed in the piston top
And the combustion chamber formed by the injection of fuel at high pressure
In a direct injection internal combustion engine having a fuel injection nozzle
Provided at a specified distance from the peripheral side wall of the cavity.
The above combustion chamber is divided into the inner combustion chamber radially inward and the outer radial direction.
An inner peripheral wall body that is partitioned into the outer combustion chamber of the
And the fuel injection nozzle.
Fuel is injected into the peripheral side wall through the notch provided in the
For injecting fuel, and the fuel with the first injection hole
Provided on the injection nozzle, the inner combustion chamber is the outer combustion
The inner peripheral wall is designed to have an air-fuel ratio that is richer than that in the chamber.
It will inject fuel and simultaneously ignite the outer combustion chamber.
The first opening formed with a smaller opening area than the first injection hole
A direct injection internal combustion engine having two injection holes .
するように設けられた突起及び該突起の対向する面に形
成され上記内周壁体の適宜位置へ向けられた溝を有した
請求項1記載の直噴式内燃機関。2. The inner combustion chamber has a protrusion provided so as to face the second injection hole, and a groove formed on an opposite surface of the protrusion and directed to an appropriate position of the inner peripheral wall body. The direct injection internal combustion engine according to claim 1.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3251809A JP2536351B2 (en) | 1991-03-22 | 1991-09-30 | Direct injection internal combustion engine |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5888691 | 1991-03-22 | ||
JP3-58886 | 1991-03-22 | ||
JP3251809A JP2536351B2 (en) | 1991-03-22 | 1991-09-30 | Direct injection internal combustion engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH051542A JPH051542A (en) | 1993-01-08 |
JP2536351B2 true JP2536351B2 (en) | 1996-09-18 |
Family
ID=26399904
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3251809A Expired - Lifetime JP2536351B2 (en) | 1991-03-22 | 1991-09-30 | Direct injection internal combustion engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2536351B2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2539852T3 (en) * | 2010-02-18 | 2015-07-06 | Volvo Technology Corporation | A piston positioned for reciprocating movement in a cylinder of a combustion engine |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59155529A (en) * | 1983-02-25 | 1984-09-04 | Agency Of Ind Science & Technol | Pilot injection device of direct injection type diesel engine |
-
1991
- 1991-09-30 JP JP3251809A patent/JP2536351B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH051542A (en) | 1993-01-08 |
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