JPH0633768A - Subsidiary chamber ignition internal combustion engine - Google Patents

Subsidiary chamber ignition internal combustion engine

Info

Publication number
JPH0633768A
JPH0633768A JP4186862A JP18686292A JPH0633768A JP H0633768 A JPH0633768 A JP H0633768A JP 4186862 A JP4186862 A JP 4186862A JP 18686292 A JP18686292 A JP 18686292A JP H0633768 A JPH0633768 A JP H0633768A
Authority
JP
Japan
Prior art keywords
chamber
air
fuel
sub
internal combustion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP4186862A
Other languages
Japanese (ja)
Inventor
Hiroko Ogita
浩子 小木田
Tsutomu Nakada
勉 中田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP4186862A priority Critical patent/JPH0633768A/en
Publication of JPH0633768A publication Critical patent/JPH0633768A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/12Other methods of operation
    • F02B2075/125Direct injection in the combustion chamber for spark ignition engines, i.e. not in pre-combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/08Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • F02B23/10Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder
    • F02B23/101Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder the injector being placed on or close to the cylinder centre axis, e.g. with mixture formation using spray guided concepts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition

Landscapes

  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

PURPOSE:To perform stable lean combustion in a subsidiary chamber ignition internal combustion engine. CONSTITUTION:In a subsidiary chamber ignition internal combustion engine provided with a subsidiary chamber 6 of communicating with a combustion chamber 4 through a nozzle 8 and a spark plug 7 of appearing in the subchamber 6, the engine provides an assist air type subfuel injection valve 14 for injecting fuel and air together to the subsidiary chamber 6 in a compression stroke and only air in an exhaust stroke.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、副室点火式内燃機関の
改良に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an improvement of an auxiliary chamber ignition type internal combustion engine.

【0002】[0002]

【従来の技術】吸気通路に気化器や燃料噴射弁を備える
予混合式の点火式内燃機関では、過渡的運転時などに燃
料の輸送遅れにより出力特性や排気エミッションが悪化
するという問題があり、これを解決するため燃焼室と連
通する副室に点火栓を臨ませ、副室に燃料を直接的に噴
射供給する副室点火式内燃機関が考えられている。
2. Description of the Related Art In a premixed ignition type internal combustion engine having a carburetor and a fuel injection valve in an intake passage, there is a problem that output characteristics and exhaust emission are deteriorated due to fuel transportation delay during transient operation. In order to solve this, a sub-chamber ignition type internal combustion engine in which a spark plug is exposed to a sub-chamber communicating with the combustion chamber and fuel is directly injected into the sub-chamber is considered.

【0003】従来の副室点火式内燃機関として、例えば
特開昭52−47132号公報に開示されたものは、図
13に示すように、ピストン53によって画成される燃
焼室54と、燃焼室54に連通する副室55と、副室5
5に臨む燃料噴射弁56および点火栓57を備えてい
る。
As a conventional sub-chamber ignition type internal combustion engine, for example, the one disclosed in Japanese Unexamined Patent Publication No. 52-47132 discloses a combustion chamber 54 defined by a piston 53 and a combustion chamber as shown in FIG. Sub-chamber 55 communicating with 54 and sub-chamber 5
The fuel injection valve 56 and the spark plug 57 facing the fuel cell 5 are provided.

【0004】これは、ピストン53が下降する吸気行程
で、吸気弁51の開弁に伴って吸気通路52から燃焼室
54に空気が吸入されるとともに、燃料噴射弁56から
副室55に燃料が直接噴射され、圧縮上死点付近では副
室55に比較的濃い混合気をつくって、点火栓57によ
る着火性を高めるものである。
In the intake stroke in which the piston 53 descends, air is sucked into the combustion chamber 54 from the intake passage 52 as the intake valve 51 is opened, and fuel is injected from the fuel injection valve 56 into the sub chamber 55. The fuel is directly injected and creates a relatively rich air-fuel mixture in the sub chamber 55 near the compression top dead center to enhance the ignitability by the spark plug 57.

【0005】[0005]

【発明が解決しようとする課題】しかしながら、このよ
うな従来装置にあっては、燃料噴射弁56の噴射時期が
吸気行程に設定されているため、吸気行程で噴射された
燃料の大部分が圧縮行程で燃焼室54に逃げてしまい、
希薄燃焼をさせる場合に圧縮上死点付近では副室55に
おける混合気濃度を十分に高めることができず、点火栓
57による着火性が損なわれるという問題点があった。
However, in such a conventional device, since the injection timing of the fuel injection valve 56 is set in the intake stroke, most of the fuel injected in the intake stroke is compressed. I escaped to the combustion chamber 54 in the process,
When performing lean combustion, there is a problem in that the air-fuel mixture concentration in the sub chamber 55 cannot be sufficiently increased near the compression top dead center, and the ignitability by the spark plug 57 is impaired.

【0006】また、狭い空間である副室55内に燃料噴
射弁56から直接燃料が噴射されるため、燃料の壁流が
生じやすく、燃料と空気の混合が十分に行われず、燃焼
性や排気エミッションの悪化を招くという問題点があっ
た。
Further, since the fuel is directly injected from the fuel injection valve 56 into the sub-chamber 55, which is a narrow space, a wall flow of the fuel is likely to occur, the fuel and air are not sufficiently mixed, and the combustibility and the exhaust gas are exhausted. There was a problem that the emission was deteriorated.

【0007】本発明は上記の問題点に着目し、副室点火
式内燃機関において、安定した希薄燃焼を実現すること
を目的とする。
In view of the above problems, the present invention has an object to realize stable lean combustion in a sub chamber ignition type internal combustion engine.

【0008】[0008]

【課題を解決するための手段】本発明は、燃焼室に噴口
を介して連通する副室と、副室に臨む点火栓とを備える
副室点火式内燃機関において、副室に燃料を直接噴射す
る燃料供給手段と、副室に空気を噴射して燃料供給手段
から噴射される燃料を微粒化する空気噴射手段と、副室
に少なくとも圧縮行程で燃料と空気を一緒に噴射させ、
排気行程で空気のみを噴射させる制御手段とを設ける。
According to the present invention, in a sub-chamber ignition type internal combustion engine having a sub-chamber communicating with a combustion chamber through a nozzle and an ignition plug facing the sub-chamber, fuel is directly injected into the sub-chamber. A fuel supply unit for injecting air into the sub chamber to atomize the fuel injected from the fuel supply unit, and to inject fuel and air into the sub chamber at least in the compression stroke.
And a control means for injecting only air in the exhaust stroke.

【0009】[0009]

【作用】ピストンが上昇する圧縮行程では、燃料供給手
段と空気噴射手段から副室に燃料と空気が一緒に噴射さ
れることにより、副室の混合気が燃焼室に逃げることが
抑えられ、副室の混合気は燃焼室の空燃比によらず所定
の濃い空燃比に保たれ、安定した着火性を維持できる。
In the compression stroke in which the piston rises, the fuel supply means and the air injection means inject the fuel and air into the sub chamber together, so that the air-fuel mixture in the sub chamber is prevented from escaping to the combustion chamber. The air-fuel mixture in the chamber is maintained at a predetermined rich air-fuel ratio regardless of the air-fuel ratio in the combustion chamber, and stable ignitability can be maintained.

【0010】同じく圧縮行程で、副室に燃料と空気が一
緒に噴射されることにより、副室における燃料の微粒化
および燃料と空気の混合を促進され、狭い空間である副
室内に燃料の壁流が生じることを防止でき、さらに噴射
される空気流により副室に強いガス流動が生起されるた
め、着火性を高められる。
Similarly, in the compression stroke, fuel and air are injected together into the sub-chamber, so that atomization of the fuel in the sub-chamber and mixing of the fuel and air are promoted, and the wall of the fuel in the sub-chamber is a narrow space. It is possible to prevent the flow from being generated, and since the strong gas flow is generated in the sub chamber due to the jetted air flow, the ignitability can be enhanced.

【0011】これにより、全体として理論空燃比よりか
なり薄い空燃比で希薄燃焼させる場合にも、点火栓の近
傍に燃料の多くを集める混合気の成層化をはかり、点火
に伴って副室内に安定した初期火炎核を生成し、噴口か
ら強い燃焼火炎を燃焼室に噴出させることで、円滑な希
薄燃焼を実現する。
As a result, even when lean-burning is performed at an air-fuel ratio that is considerably less than the stoichiometric air-fuel ratio as a whole, stratification of the air-fuel mixture that collects most of the fuel in the vicinity of the spark plug is achieved, and it is stabilized in the sub-chamber with ignition. By generating the initial flame kernel and ejecting a strong combustion flame from the injection port into the combustion chamber, smooth lean combustion is realized.

【0012】排気行程で空気供給手段から副室内に空気
が噴射されることにより、副室内の掃気が十分に行わ
れ、次のサイクルの安定した着火性を維持できる。
By injecting air from the air supply means into the sub-chamber during the exhaust stroke, the scavenging of the sub-chamber is sufficiently performed, and stable ignitability in the next cycle can be maintained.

【0013】[0013]

【実施例】以下、本発明を4ストローク内燃機関に適用
した実施例を添付図面に基づいて説明する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT An embodiment in which the present invention is applied to a four-stroke internal combustion engine will be described below with reference to the accompanying drawings.

【0014】図1に示すように、エンジンブロック(シ
リンダヘッド)1とピストン3の間に燃焼室4が画成さ
れ、この燃焼室4の中央部にドーム状のキャップ5を介
して副室6が画成される。副室6には点火栓7が臨んで
いるとともに、連通管16を介してアシストエア式の副
燃料噴射弁14が臨んでいる。
As shown in FIG. 1, a combustion chamber 4 is defined between an engine block (cylinder head) 1 and a piston 3, and a sub chamber 6 is formed in the center of the combustion chamber 4 via a dome-shaped cap 5. Is defined. A spark plug 7 faces the sub chamber 6, and an assist air type sub fuel injection valve 14 faces a communication pipe 16.

【0015】ドーム状のキャップ5は点火栓ボス部18
から燃焼室4に挿入され、その上端つば部19が点火栓
ボス部18に螺合するスリーブ20を介して締結され、
スリーブ20の内側に点火栓7が螺合して取付けられ
る。
The dome-shaped cap 5 has a spark plug boss portion 18
Is inserted into the combustion chamber 4 from above, and the upper end flange portion 19 is fastened via a sleeve 20 screwed to the spark plug boss portion 18,
The spark plug 7 is screwed and attached to the inside of the sleeve 20.

【0016】キャップ5には複数の噴口8が形成され、
副室6はこの噴口8を介して燃焼室4と連通する。
A plurality of nozzles 8 are formed in the cap 5,
The sub chamber 6 communicates with the combustion chamber 4 via the injection port 8.

【0017】第一の燃料供給手段として、図2に示すよ
うに、吸気ポート11には主燃料噴射弁15が設けられ
る。燃焼室4には副室6のまわりに2つの吸気弁13と
排気弁12が設けられ、各吸気弁13は吸気ポート11
を、各排気弁12は排気ポート10をエンジン回転に同
期してそれぞれ所定のタイミングで開閉する。
As a first fuel supply means, a main fuel injection valve 15 is provided in the intake port 11 as shown in FIG. In the combustion chamber 4, two intake valves 13 and an exhaust valve 12 are provided around the sub chamber 6, and each intake valve 13 includes an intake port 11
Each exhaust valve 12 opens and closes the exhaust port 10 at a predetermined timing in synchronization with the engine rotation.

【0018】第二の燃料供給手段および空気噴射手段と
して設けられるアシストエア式の副燃料噴射弁14は、
図3にも示すように、燃料入口21と空気入口22およ
び出口23を備え、出口23から燃料と空気を同時に噴
射するようになっている。
The assist air type auxiliary fuel injection valve 14 provided as the second fuel supply means and the air injection means is
As shown in FIG. 3, a fuel inlet 21, an air inlet 22 and an outlet 23 are provided, and fuel and air are simultaneously injected from the outlet 23.

【0019】燃料入口21には図示しない燃料配管を介
して所定の加圧燃料が供給され、副燃料噴射弁14はこ
れに内蔵される電磁弁が駆動パルスを受けて開弁するこ
とにより開弁期間に応じた所定量の燃料が出口23から
噴射される。
A predetermined pressurized fuel is supplied to the fuel inlet 21 via a fuel pipe (not shown), and the sub fuel injection valve 14 is opened by opening a solenoid valve incorporated therein to receive a drive pulse. A predetermined amount of fuel corresponding to the period is injected from the outlet 23.

【0020】図3に示すように、空気入口22には空気
配管24が接続され、蓄圧容器27に蓄えられた加圧空
気が空気ギャラリー26を通り、各気筒毎に設けられる
電磁弁25を経て供給される。蓄圧容器27にはエアポ
ンプ28から吐出される加圧空気がレギュレータ29を
介して蓄えられる。これにより、電磁弁25の開弁に伴
って副燃料噴射弁14の出口23から加圧空気が噴出
し、上記噴射燃料と混合しながら連通管16を通って副
室6に供給される。
As shown in FIG. 3, an air pipe 24 is connected to the air inlet 22, and the pressurized air stored in the pressure accumulator 27 passes through the air gallery 26 and the solenoid valve 25 provided for each cylinder. Supplied. Pressurized air discharged from the air pump 28 is stored in the pressure accumulating container 27 via the regulator 29. As a result, when the solenoid valve 25 is opened, the pressurized air is ejected from the outlet 23 of the auxiliary fuel injection valve 14 and is supplied to the auxiliary chamber 6 through the communication pipe 16 while being mixed with the injected fuel.

【0021】点火栓7は、点火装置31からイグニッシ
ョンコイルに発生した高電圧が供給されることにより、
その電極9間に火花放電を起こして、副室6内で圧縮さ
れた混合気に着火させるようになっている。
The spark plug 7 is supplied with the high voltage generated in the ignition coil from the ignition device 31,
A spark discharge is generated between the electrodes 9 to ignite the mixture gas compressed in the sub chamber 6.

【0022】制御装置32は、各種運転状態の検出信号
を入力して、主燃料噴射弁15、副燃料噴射弁14から
の燃料噴射量および噴射時期を制御し、電磁弁25を介
して空気噴出時期を制御するとともに、点火栓7を点火
する点火装置31の点火時期を制御する。
The control device 32 inputs detection signals of various operating states, controls the fuel injection amount and injection timing from the main fuel injection valve 15 and the sub fuel injection valve 14, and ejects air through the solenoid valve 25. In addition to controlling the timing, the ignition timing of the ignition device 31 that ignites the spark plug 7 is controlled.

【0023】制御装置32では、図4に示すように、点
火時期が圧縮上死点前に設定され、主燃料噴射弁15の
燃料噴射時期が吸気行程から圧縮行程の初期にかけて設
定され、副燃料噴射弁14の燃料噴射時期が圧縮行程に
設定され、同じく副燃料噴射弁14の空気噴射時期が圧
縮行程と排気行程の2回に分けて設定される。すなわ
ち、副燃料噴射弁14は圧縮行程では燃料と空気を同時
に噴射し、排気行程では空気のみを噴射するようになっ
ている。
In the control device 32, as shown in FIG. 4, the ignition timing is set before the compression top dead center, the fuel injection timing of the main fuel injection valve 15 is set from the intake stroke to the beginning of the compression stroke, and the auxiliary fuel is set. The fuel injection timing of the injection valve 14 is set to the compression stroke, and the air injection timing of the auxiliary fuel injection valve 14 is also set to be divided into the compression stroke and the exhaust stroke. That is, the auxiliary fuel injection valve 14 is configured to inject fuel and air simultaneously in the compression stroke and inject only air in the exhaust stroke.

【0024】制御装置32は、主燃料噴射弁15の燃料
噴射量を機関負荷に応じて変化させるが、副燃料噴射弁
14の燃料噴射量を運転状態によらず一定に制御する。
これにより、副燃料噴射弁14からは常に少量の燃料が
噴射されて、副燃料噴射弁14が噴射を終える圧縮上死
点の手前では副室6内に点火栓7による着火に適した所
定の空燃比の混合気が充填される。
The control device 32 changes the fuel injection amount of the main fuel injection valve 15 according to the engine load, but controls the fuel injection amount of the sub fuel injection valve 14 to be constant regardless of the operating state.
As a result, a small amount of fuel is always injected from the auxiliary fuel injection valve 14, and before the compression top dead center at which the auxiliary fuel injection valve 14 finishes injection, a predetermined amount suitable for ignition by the spark plug 7 is provided in the auxiliary chamber 6. The air-fuel ratio mixture is filled.

【0025】次に、作用について説明する。Next, the operation will be described.

【0026】ピストン3が下降する吸気行程では、主燃
料噴射弁15から噴射された燃料が吸気通路を通って空
気と混合しながら燃焼室4に吸入され、燃焼室4に所定
の濃度の混合気が充填される。
In the intake stroke in which the piston 3 descends, the fuel injected from the main fuel injection valve 15 is sucked into the combustion chamber 4 while mixing with the air through the intake passage, and the mixture gas having a predetermined concentration is mixed in the combustion chamber 4. Is filled.

【0027】続いてピストン3が上昇する圧縮行程で
は、副燃料噴射弁14から副室6に燃料と空気が一緒に
噴射されることで、副室6から混合気が燃焼室4に逃げ
ることを抑えられ、副室6の混合気は燃焼室4の空燃比
によらず所定の濃い空燃比に保たれ、安定した着火性能
を維持できる。
Subsequently, in the compression stroke in which the piston 3 rises, fuel and air are injected together from the sub-fuel injection valve 14 into the sub-chamber 6, thereby preventing the air-fuel mixture from escaping from the sub-chamber 6 to the combustion chamber 4. As a result, the air-fuel mixture in the sub chamber 6 is kept at a predetermined rich air-fuel ratio regardless of the air-fuel ratio in the combustion chamber 4, and stable ignition performance can be maintained.

【0028】同じく圧縮行程で、筒内圧が所定値以下の
ときに副室6に燃料と共に空気が一緒に噴射されること
により、副室6における燃料の微粒化および燃料と空気
の混合が促進され、狭い空間である副室6内に燃料の壁
流が生じることを防止でき、さらに噴射される空気流に
より副室6に強いガス流動が生起されるため、着火性を
高められる。
Similarly, in the compression stroke, when the in-cylinder pressure is equal to or lower than a predetermined value, the fuel and the air are injected into the sub chamber 6 together, so that atomization of the fuel in the sub chamber 6 and mixing of the fuel and the air are promoted. It is possible to prevent a wall flow of the fuel from being generated in the sub-chamber 6 which is a narrow space, and a strong gas flow is generated in the sub-chamber 6 by the injected air flow, so that the ignitability is enhanced.

【0029】これにより、全体として理論空燃比よりか
なり薄い空燃比で希薄燃焼させる場合にも、副室6の空
燃比を燃焼室4の平均空燃比より濃くして、圧縮上死点
の手前で点火時期を迎える点火栓7の近傍に燃料の多く
を集めて混合気の成層化をすることができ、副室6内に
安定した初期火炎核を生成し、強い燃焼火炎を各噴口8
から燃焼室4に噴出させ、燃焼室4の混合気を拡散燃焼
させる。このようにして安定した着火にもとづく円滑な
希薄燃焼を実現し、燃費の低減、排気エミッションの改
善、高出力化がはかれる。
As a result, even when lean-burning is performed at an air-fuel ratio that is considerably thinner than the stoichiometric air-fuel ratio as a whole, the air-fuel ratio of the sub-chamber 6 is made thicker than the average air-fuel ratio of the combustion chamber 4 and before the compression top dead center. Most of the fuel can be collected in the vicinity of the spark plug 7, which is at the ignition timing, to stratify the air-fuel mixture, generate a stable initial flame kernel in the sub chamber 6, and generate a strong combustion flame at each nozzle 8
From the above to the combustion chamber 4 to diffuse and burn the air-fuel mixture in the combustion chamber 4. In this way, a smooth lean burn based on stable ignition is realized, and fuel consumption is reduced, exhaust emission is improved, and high output is achieved.

【0030】また副燃料噴射弁14からの噴射燃料が空
気と共に高温となったキャップ5に衝突することで、燃
料の気化潜熱によりキャップ5を冷却し、自着火を防止
するとともに、キャップ5の過熱を防止することができ
る。
Further, the fuel injected from the auxiliary fuel injection valve 14 collides with the cap 5 having a high temperature together with the air, thereby cooling the cap 5 by the latent heat of vaporization of the fuel, preventing self-ignition, and overheating the cap 5. Can be prevented.

【0031】排気行程で副室6内に副燃料噴射弁14か
ら加圧空気が噴射されることにより、副室6内の掃気が
十分に行われ、次のサイクルの着火を安定させることが
できる。
By injecting the pressurized air from the sub fuel injection valve 14 into the sub chamber 6 in the exhaust stroke, the scavenging inside the sub chamber 6 is sufficiently performed and the ignition of the next cycle can be stabilized. .

【0032】次に、図5に示した他の実施例は、蓄圧容
器27に蓄えられた加圧空気が空気ギャラリー26から
分配器33を介して空気配管24に分配されるものであ
る。
Next, in another embodiment shown in FIG. 5, the pressurized air stored in the pressure accumulating container 27 is distributed from the air gallery 26 to the air pipe 24 through the distributor 33.

【0033】分配器33は機関回転に同期して回転する
ロータリーバルブ34を備え、ロータリーバルブ34は
圧縮行程で各空気配管24と連通するポート34aと、
圧縮行程から引き続いて膨張行程と排気行程に渡って空
気配管24と連通する切欠き34bを有し、点火順序に
したがって各気筒の副燃料噴射弁14に空気を分配する
ようになっている。
The distributor 33 includes a rotary valve 34 that rotates in synchronization with the engine rotation. The rotary valve 34 has a port 34a that communicates with each air pipe 24 in the compression stroke.
There is a notch 34b communicating with the air pipe 24 from the compression stroke to the expansion stroke and the exhaust stroke, and the air is distributed to the auxiliary fuel injection valve 14 of each cylinder according to the ignition order.

【0034】なお、上記分配器33や前記実施例におけ
る電磁弁25を廃止して、副燃料噴射弁14に常時加圧
空気を供給する構成としてもよい。
The distributor 33 and the solenoid valve 25 in the above embodiment may be omitted and the pressurized air may be constantly supplied to the auxiliary fuel injection valve 14.

【0035】次に、図6、図7に示した他の実施例は、
各気筒に吸気弁12と排気弁11の1本づつ備える機関
において、キャップ5を所定角度θだけ傾斜させて配置
するものである。ピストン3の頂面3aは凹状に窪んで
いる。
Next, another embodiment shown in FIG. 6 and FIG.
In an engine having one intake valve 12 and one exhaust valve 11 in each cylinder, the cap 5 is arranged with a predetermined angle θ. The top surface 3a of the piston 3 is recessed.

【0036】この場合、キャップ5はその外側にエンジ
ンブロックの点火栓ボス部に螺合するネジ部35と、そ
の外側に点火栓7を螺合させるネジ部36を有する。キ
ャップ5には単一の噴口8が吸気弁12と排気弁11の
間に向けて開口している。
In this case, the cap 5 has a screw portion 35 which is screwed to the spark plug boss portion of the engine block on the outside thereof and a screw portion 36 which is screwed to the spark plug 7 on the outside thereof. A single injection port 8 is opened in the cap 5 between the intake valve 12 and the exhaust valve 11.

【0037】また、キャップ5には図8に示すように2
つの噴口8を、図9に示すように3つの噴口8を、図1
0に示すように4つの噴口8をそれぞれ形成してもよ
い。
Further, as shown in FIG.
One nozzle 8 is shown in FIG. 9, and three nozzles 8 are shown in FIG.
As shown in 0, four injection holes 8 may be formed respectively.

【0038】副室6の容積をV、噴口8の開口面積の総
和をSとすると、V/Sが大きくなる程、噴口8から燃
焼室4に噴出する燃焼ガスの噴出速度が高まって、燃焼
室4における燃焼が速まるため、点火時期を遅らせるよ
うにすればよい。またV/Sが小さくなる程、燃焼室4
の空燃比の限界値が拡がる傾向にある。さらに燃焼室4
に生起される吸気スワールが強い程、噴口8からの燃焼
ガスがキャップ5の周囲に回り込むため、噴口8の数は
少なくてよい。
Assuming that the volume of the sub-chamber 6 is V and the sum of the opening areas of the injection ports 8 is S, the ejection speed of the combustion gas ejected from the injection ports 8 into the combustion chamber 4 increases as V / S increases, and combustion is performed. Since the combustion in the chamber 4 is accelerated, the ignition timing may be delayed. Further, as V / S becomes smaller, the combustion chamber 4
There is a tendency that the limit value of the air-fuel ratio of the Further combustion chamber 4
The stronger the intake swirl generated at 1, the more the combustion gas from the nozzles 8 goes around the cap 5, so the number of nozzles 8 may be smaller.

【0039】次に、図11に示した他の実施例は、副室
6に臨んで光ビーム式点火栓41が設けられるものであ
る。
Next, in another embodiment shown in FIG. 11, a light beam type ignition plug 41 is provided facing the sub chamber 6.

【0040】光ビーム式点火栓41はキャップ5の上部
に凸レンズ42を備え、凸レンズ42の焦点距離は10
mm程度に設定され、図示しない発光装置から所定の点
火時期に送られる光ビーム(レーザ光)を副室6の中央
部に集めるようになっている。
The light beam type ignition plug 41 is provided with a convex lens 42 on the upper portion of the cap 5, and the focal length of the convex lens 42 is 10
The light beam (laser light), which is set to about mm and is sent at a predetermined ignition timing from a light emitting device (not shown), is collected in the central portion of the sub chamber 6.

【0041】このようにして、光ビーム式点火栓41は
副室6の中央部で混合気に点火するため、前記実施例の
ように副室6の上部に位置する電極9によって混合気に
着火するものに比べて、各噴口8から燃焼室4への火炎
の噴き出しを早められ、燃焼性を高めることができる。
In this way, the light beam type spark plug 41 ignites the air-fuel mixture in the central portion of the sub-chamber 6, so that the electrode 9 located above the sub-chamber 6 ignites the air-fuel mixture as in the above-described embodiment. As compared with the above-mentioned one, the ejection of flame from each ejection port 8 to the combustion chamber 4 can be accelerated, and the combustibility can be improved.

【0042】また、キャップ5はその材質をステンレス
材とし、その内面5aを鏡面仕上げを施すか、あるいは
その内面5aに多層膜を蒸着して、内面5aの反射率を
90〜95%に仕上げる。
The cap 5 is made of stainless steel and its inner surface 5a is mirror-finished, or a multilayer film is vapor-deposited on its inner surface 5a to finish the reflectance of the inner surface 5a to 90 to 95%.

【0043】そして、図12に示すように、光ビームは
凸レンズ42で副室6の中央部に位置するA点で集光し
た後、凹状に湾曲して窪むキャップ内面5aに反射して
副室6の中央部に位置するB点で再び集光させること
で、副室6の混合気に対してこの2点で着火作用が得ら
れ、さらに燃焼性を高めることができる。
Then, as shown in FIG. 12, the light beam is condensed by the convex lens 42 at the point A located in the center of the sub chamber 6, and then reflected on the inner surface 5a of the cap which is concavely curved and recessed. By condensing light again at the point B located in the center of the chamber 6, the ignition effect can be obtained at these two points with respect to the air-fuel mixture in the sub chamber 6, and the combustibility can be further enhanced.

【0044】また、キャップ内面5aに対するカーボン
等の付着物は光ビームによって焼き切られる自己浄化作
用があるため、光ビームが当たる部分は常に所定の反射
率を維持できる。
Further, since the deposits such as carbon on the inner surface 5a of the cap have a self-cleaning action of being burned off by the light beam, the portion where the light beam hits can always maintain a predetermined reflectance.

【0045】[0045]

【発明の効果】以上説明したように本発明は、燃焼室に
噴口を介して連通する副室と、副室に臨む点火栓とを備
える副室点火式内燃機関において、副室に燃料を直接噴
射する燃料供給手段と、副室に空気を噴射して燃料供給
手段から噴射される燃料を微粒化する空気噴射手段と、
副室に少なくとも圧縮行程で燃料と空気を一緒に噴射さ
せ、排気行程で空気のみを噴射させる制御手段とを設け
たため、副室の混合気は燃焼室の空燃比によらず所定の
空燃比に保たれ、かつ十分な掃気も確保され、安定した
着火にもとづく円滑な希薄燃焼を実現し、燃費の低減、
排気エミッションの改善、高出力化がはかれる。
As described above, according to the present invention, in a sub-chamber ignition type internal combustion engine including a sub-chamber communicating with a combustion chamber via a nozzle and a spark plug facing the sub-chamber, fuel is directly fed to the sub-chamber. Fuel supply means for injecting, and air injection means for injecting air into the sub chamber to atomize the fuel injected from the fuel supply means,
Since the control means for injecting fuel and air together at least in the compression stroke and injecting only air in the exhaust stroke is provided in the sub-chamber, the air-fuel mixture in the sub-chamber has a predetermined air-fuel ratio regardless of the air-fuel ratio of the combustion chamber. Maintained, sufficient scavenging is secured, smooth lean combustion based on stable ignition is realized, fuel consumption is reduced,
Exhaust emissions are improved and higher output is achieved.

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

【図1】本発明の実施例を示す機関の縦断面図である。FIG. 1 is a longitudinal sectional view of an engine showing an embodiment of the present invention.

【図2】同じく機関の概略平面図である。FIG. 2 is a schematic plan view of the same engine.

【図3】同じく空気供給系の構成図である。FIG. 3 is a block diagram of an air supply system of the same.

【図4】同じく燃料および空気噴射時期を示すタイミン
グチャートである。
FIG. 4 is a timing chart showing fuel and air injection timings.

【図5】他の実施例を示す空気供給系の構成図である。FIG. 5 is a configuration diagram of an air supply system showing another embodiment.

【図6】さらに他の実施例を示す機関の概略平面図であ
る。
FIG. 6 is a schematic plan view of an engine showing still another embodiment.

【図7】同じく図6のX−X線に沿う縦断面図である。FIG. 7 is a vertical sectional view taken along line XX of FIG.

【図8】さらに他の実施例を示す機関の概略平面図であ
る。
FIG. 8 is a schematic plan view of an engine showing still another embodiment.

【図9】さらに他の実施例を示す機関の概略平面図であ
る。
FIG. 9 is a schematic plan view of an engine showing still another embodiment.

【図10】さらに他の実施例を示す機関の概略平面図で
ある。
FIG. 10 is a schematic plan view of an engine showing still another embodiment.

【図11】さらに他の実施例を示す機関の縦断面図であ
る。
FIG. 11 is a longitudinal sectional view of an engine showing still another embodiment.

【図12】同じく光ビーム式点火栓の構成図である。FIG. 12 is a configuration diagram of the light beam type ignition plug.

【図13】従来例を示す機関の縦断面図である。FIG. 13 is a vertical sectional view of an engine showing a conventional example.

【符号の説明】[Explanation of symbols]

3 ピストン 4 燃焼室 5 キャップ 6 副室 7 点火栓 8 噴口 11 吸気ポート 14 副燃料噴射弁(燃料供給手段および空気供給手
段) 15 主燃料噴射弁 24 空気配管 25 電磁弁 32 制御装置
3 Pistons 4 Combustion chambers 5 Caps 6 Sub-chambers 7 Spark plugs 8 Injection ports 11 Intake ports 14 Sub-fuel injection valves (fuel supply means and air supply means) 15 Main fuel injection valves 24 Air piping 25 Solenoid valves 32 Control device

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.5 識別記号 庁内整理番号 FI 技術表示箇所 F02M 63/00 P 7825−3G 69/00 310 E 7825−3G ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 5 Identification number Office reference number FI technical display location F02M 63/00 P 7825-3G 69/00 310 E 7825-3G

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 燃焼室に噴口を介して連通する副室と、
副室に臨む点火栓とを備える副室点火式内燃機関におい
て、副室に燃料を直接噴射する燃料供給手段と、副室に
空気を噴射して燃料供給手段から噴射される燃料を微粒
化する空気噴射手段と、副室に少なくとも圧縮行程で燃
料と空気を一緒に噴射させ、排気行程で空気のみを噴射
させる制御手段とを設けたことを特徴とする副室点火式
内燃機関。
1. A sub-chamber communicating with the combustion chamber through a nozzle,
In a sub-chamber ignition type internal combustion engine having a spark plug facing the sub-chamber, fuel supply means for directly injecting fuel into the sub-chamber and air injected into the sub-chamber to atomize the fuel injected from the fuel supply means An auxiliary chamber ignition type internal combustion engine, comprising: an air injection means; and a control means for injecting fuel and air together into the auxiliary chamber at least in a compression stroke and injecting only air in an exhaust stroke.
JP4186862A 1992-07-14 1992-07-14 Subsidiary chamber ignition internal combustion engine Pending JPH0633768A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4186862A JPH0633768A (en) 1992-07-14 1992-07-14 Subsidiary chamber ignition internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4186862A JPH0633768A (en) 1992-07-14 1992-07-14 Subsidiary chamber ignition internal combustion engine

Publications (1)

Publication Number Publication Date
JPH0633768A true JPH0633768A (en) 1994-02-08

Family

ID=16195967

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4186862A Pending JPH0633768A (en) 1992-07-14 1992-07-14 Subsidiary chamber ignition internal combustion engine

Country Status (1)

Country Link
JP (1) JPH0633768A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007177755A (en) * 2005-12-28 2007-07-12 Honda Motor Co Ltd Self ignition engine
JP2019120170A (en) * 2017-12-28 2019-07-22 本田技研工業株式会社 Internal combustion engine
US10837355B2 (en) 2017-12-28 2020-11-17 Honda Motor Co., Ltd. Internal combustion engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007177755A (en) * 2005-12-28 2007-07-12 Honda Motor Co Ltd Self ignition engine
JP4493593B2 (en) * 2005-12-28 2010-06-30 本田技研工業株式会社 Self-igniting engine
JP2019120170A (en) * 2017-12-28 2019-07-22 本田技研工業株式会社 Internal combustion engine
US10837355B2 (en) 2017-12-28 2020-11-17 Honda Motor Co., Ltd. Internal combustion engine

Similar Documents

Publication Publication Date Title
US7814883B2 (en) Internal combustion engine with auxiliary combustion chamber
US6213086B1 (en) Combustion engine
US4446830A (en) Method of operating an engine with a high heat of vaporization fuel
US7171953B2 (en) Method for operating an internal combustion engine with direct fuel injection
US6948474B2 (en) Cylinder direct injection type internal combustion engine
JPH11132135A (en) Operation method of direct injection type gasoline internal combustion engine
US5915349A (en) Gasoline internal combustion engine
JPH0633769A (en) Subsidiary chamber ignition internal combustion engine
US5477822A (en) Spark ignition engine with cylinder head combustion chamber
JPH0633768A (en) Subsidiary chamber ignition internal combustion engine
GB2311327A (en) Combined fuel injector and spark plug arrangement in an engine cylinder
GB1394408A (en) Internal combustion engine
US3983847A (en) Jet ignition engine with prechamber fuel injection
GB2108581A (en) Fuel injection stratified charge internal combustion engine
US4043309A (en) Internal combustion engine having auxiliary combustion chamber
US7404390B2 (en) Method for operating an externally ignited internal combustion engine
JPH0633770A (en) Subsidiary chamber ignition internal combustion engine
US4182284A (en) Divided auxiliary combustion chamber for internal combustion spark ignition engines
JPH06229318A (en) High-compression ratio sub chamber-type gas engine
JPS5855325B2 (en) internal combustion engine
JPH06229319A (en) High-compression ratio sub chamber-type gas engine
JP7238970B2 (en) Fuel injection control system for pre-chamber internal combustion engine
JPS6045716A (en) Internal-combustion engine
JP2000110646A (en) Diesel engine
EP0958451B1 (en) Direct injection spark ignition engine