JPS58144623A - Ignition device for internal-combustion engine - Google Patents
Ignition device for internal-combustion engineInfo
- Publication number
- JPS58144623A JPS58144623A JP57027758A JP2775882A JPS58144623A JP S58144623 A JPS58144623 A JP S58144623A JP 57027758 A JP57027758 A JP 57027758A JP 2775882 A JP2775882 A JP 2775882A JP S58144623 A JPS58144623 A JP S58144623A
- Authority
- JP
- Japan
- Prior art keywords
- ignition
- swirl
- cylinder
- air
- ignition plug
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
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
- F02B23/08—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive 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)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
Description
【発明の詳細な説明】
本発明は主として燃料噴射式内燃機関にお【ノる燃料の
着火装置に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates primarily to a fuel ignition device for a fuel-injected internal combustion engine.
ガソリン機関など予混合式内燃機関において、加速応答
性等を高めるために、機関吸気ポートにffk110回
転に同期して燃料を噴射供給し、さらにシリンダ内の混
合気に旋回運動を付与すべくスワール発生手段を設けて
いるものがある。In premixed internal combustion engines such as gasoline engines, in order to improve acceleration response etc., fuel is injected and supplied to the engine intake port in synchronization with ffk110 rotation, and swirl is also generated to give swirling motion to the air-fuel mixture in the cylinder. Some have measures in place.
これを第1図によって説明すると、吸気マニホールド1
にはシリンダヘッド2の吸気ポート3の近傍に位置して
燃料噴射インジェクタ4が取りf−jけられる。To explain this with reference to Fig. 1, the intake manifold 1
A fuel injector 4 is installed near the intake port 3 of the cylinder head 2.
このインジェクタ4は吸気弁5の背面付近に向けて燃料
を噴射するように噴射方向が設定され例えば4サイクル
エンジンでは、1回転につき1回の割合で燃料を間欠的
に噴射し、燃料が吸気弁5の開弁に伴ってシリンダ6の
内部、すなわち燃焼室7へ空気とともに吸入される。The injection direction of this injector 4 is set so as to inject fuel toward the vicinity of the back of the intake valve 5. For example, in a 4-cycle engine, fuel is intermittently injected once per rotation, and the fuel is injected into the intake valve. When the valve 5 opens, the air is drawn into the cylinder 6, that is, into the combustion chamber 7 together with air.
このとき吸入空気流に旋回運動を付与するように、吸気
ポート3Gまスワール発生手段としてのヘリカルポート
3Aに形成される。At this time, the intake port 3G is formed into a helical port 3A as a swirl generating means so as to impart swirling motion to the intake air flow.
したがって、シリンダ内に流入した空気は、シリンダ軸
を中心としてのスワールを起こし、このスワールは吸入
行程から圧縮行程にかけて持続される。 ・
そして、ピストン9の上昇に伴い圧縮1死点f−1近で
、点火栓8がスパークfIi電して混合気を着火燃焼さ
せるのである。Therefore, the air flowing into the cylinder causes a swirl around the cylinder axis, and this swirl is sustained from the suction stroke to the compression stroke. - Then, as the piston 9 rises, near the first compression dead center f-1, the ignition plug 8 generates a spark fIi to ignite and burn the air-fuel mixture.
ところで、上記インジェクタ4から噴射された燃料は、
吸気弁5が開くまでの間、吸気弁5の背面や吸気ポート
3の内壁に付着し、吸気弁5が開いた吸入行程で吸入空
気流に乗ってシリンダ内に流入する。By the way, the fuel injected from the injector 4 is
Until the intake valve 5 opens, it adheres to the back surface of the intake valve 5 and the inner wall of the intake port 3, and during the intake stroke when the intake valve 5 opens, it flows into the cylinder along with the intake air flow.
したがって、吸入行程の初期に大部分の燃料はシリンダ
内へ吸い込まれ、シリンダ下部に濃い混合気層を形成す
るとともに、吸入空気のシリンダ内での旋回運動により
、燃料粒子は遠心力を受けて外側に押し付けられるため
、シリンダ内壁に沿っても比較的濃い混合気層が形成さ
れる。Therefore, most of the fuel is sucked into the cylinder at the beginning of the intake stroke, forming a rich mixture layer at the bottom of the cylinder, and due to the swirling movement of the intake air within the cylinder, the fuel particles are subjected to centrifugal force and moved outward. , a relatively dense mixture layer is also formed along the inner wall of the cylinder.
この結果、点火栓8が取り付けられるシリンダ中央部は
、混合気がS薄な状態になり、点火栓8がスパーク放電
しても、運転状態によっては安定して着火が行なわれな
かったり、あるいは着火後の火炎伝播が円滑に行なわれ
ず、燃焼が不安定となることがあった。As a result, the air-fuel mixture in the center of the cylinder where the ignition plug 8 is attached becomes S-lean, and even if the ignition plug 8 discharges a spark, depending on the operating conditions, ignition may not occur stably, or ignition may not occur stably. Subsequent flame propagation was not carried out smoothly, and combustion sometimes became unstable.
本発明はこのような問題を解決するために提案されたも
ので、点火栓を濃混合気の存在するシリ。The present invention was proposed in order to solve this problem.
ンダ外周に近接して設けるとともに、この点火栓の近傍
に防風部材を配設し、強スワールのもとでも確実に濃混
合気層に着火させ、安定した燃焼を確保するようにした
内燃機関の着火装置を提供する。The spark plug is installed close to the outer periphery of the spark plug, and a windproof member is placed near the spark plug to reliably ignite the rich air-fuel mixture layer and ensure stable combustion even under strong swirls. Provide an ignition device.
以下、本発明の実施例を図面にもとづいて説明する。Embodiments of the present invention will be described below based on the drawings.
第2図、第3図において、吸気弁5から吸い込まれた混
合気がシリンダ内でスワールを生じるように、吸気ポー
ト3の出口部はヘリカルポート3Aに形成される。In FIGS. 2 and 3, the outlet of the intake port 3 is formed into a helical port 3A so that the air-fuel mixture sucked in from the intake valve 5 swirls within the cylinder.
そして、燃焼室7の周辺部、すなわちスワールの外側部
分に位置して点火キャップ15が存在するように点火栓
8が、シリンダヘッド2に装着される。The ignition plug 8 is attached to the cylinder head 2 so that the ignition cap 15 is located at the periphery of the combustion chamber 7, that is, at the outer side of the swirl.
点火栓8のスワール空気流に対する上流側近(完には、
第4図(A>、(B)にも示すような防風部材16が形
成される(ただし、第4図(B ) 1.i、点火栓8
を傾けである)。The upstream side of the spark plug 8 with respect to the swirl air flow (completely,
A windproof member 16 as shown in FIGS. 4(A> and 4B) is formed (however, FIG. 4(B) 1.
).
防風部材16は半円状の突起16Aとして形成され、点
火キャップ15での火炎の吹き消えを防止する。The windproof member 16 is formed as a semicircular projection 16A, and prevents the flame from blowing out at the ignition cap 15.
なお、18は排気弁、19は排気ポートで、この場合吸
排気ポート3.19はクロスフロー構造どなっている。Note that 18 is an exhaust valve, 19 is an exhaust port, and in this case, the intake and exhaust ports 3 and 19 have a cross-flow structure.
その他の構成において第1図と同一部材には同符号を付
し、次にその作用を説明すると、燃料噴射インジェクタ
4から噴射された燃料は、吸気弁5が開きピストン9が
降下し始めると、空気とともに吸気弁5の回りを旋回し
ながらシリンダ内へ吸い込まれ、シリンダ6の内壁に沿
ってのスワールを生じる。In other parts of the structure, the same members as in FIG. The air is sucked into the cylinder while swirling around the intake valve 5 along with the air, creating a swirl along the inner wall of the cylinder 6.
このとき既に気化している燃料は空気とともにシリ゛、
・ダ中央部にも分布する。しかし、吸気弁5の上流に噴
射された燃料は全てが即座に気化するのではなく、多く
が液滴の状態でシリンダ内に吸入される。At this time, the already vaporized fuel goes into series with the air.
・Also distributed in the central part of Da. However, all of the fuel injected upstream of the intake valve 5 does not immediately vaporize, but much of it is sucked into the cylinder in the form of droplets.
燃料液滴は質量が大きいため、強力なスワールが発生す
ると、遠心力によりほとんどがシリンダ6の内壁に向【
プて飛ばされる。Since fuel droplets have a large mass, when a strong swirl occurs, most of them are directed toward the inner wall of cylinder 6 due to centrifugal force.
I was thrown and blown away.
ピストン9がhuを始める圧縮行程で、燃料の気化は進
んでも、シリンダ6の壁面近傍には濃いU含気の旋回層
が維持される。In the compression stroke in which the piston 9 begins hu, even though the fuel vaporization progresses, a swirling layer containing dense U air is maintained near the wall surface of the cylinder 6.
この結果、圧縮上死点付近において点火栓B LL全全
体平均空燃比よりも濃いシリンダ外周部の沢合気域に着
火することができ、このとき外周側けどスワール流が強
いのであるが、点火栓8の上流側に設けた防風部材16
があるため、点火 ヤップ15に飛んだ火花の吹き消え
が防止され、安定した着火が行なわれるのである。As a result, near compression top dead center, it is possible to ignite the spark plug B LL in the Sawa Aiki region on the outer periphery of the cylinder, which is richer than the overall average air-fuel ratio.At this time, although the swirl flow is strong on the outer periphery, Windproof member 16 provided on the upstream side of plug 8
As a result, the sparks that fly to the ignition valve 15 are prevented from blowing out, and stable ignition is achieved.
着火後にはスワール本来の働きもあって、火炎は乱流を
起こしつつ中央部の比較的稀薄な混合気層に円滑に伝播
し、安定した燃焼を確保する。After ignition, due to the inherent function of swirl, the flame creates a turbulent flow while smoothly propagating into the relatively dilute air-fuel mixture layer in the center, ensuring stable combustion.
第5図は、第2図のように吸排気ポートの配置1゛がク
ロス70−に対するものではなく、カウンターフローに
対する配置とした場合の実施例であって、この場合も、
点火栓8がシリンダ外周側に位置し、かつスワール上流
側に防風部材16か設【ノである。したがって、中央に
比べて濃い混合気か存在するシリンダ外周域に着火する
ので、安定した燃焼が確保できる。FIG. 5 shows an embodiment in which the arrangement 1'' of the intake and exhaust ports is not relative to the cross 70- as shown in FIG. 2, but is relative to the counter flow.
The ignition plug 8 is located on the outer peripheral side of the cylinder, and a windproof member 16 is provided on the upstream side of the swirl. Therefore, ignition occurs in the outer peripheral region of the cylinder where the mixture is richer than in the center, so stable combustion can be ensured.
第6図、第7図の、実施例は、クロスフロータイブの吸
排気ボートをもつものにおいて、吸気ボ−i−〇と排気
ボー1〜19をシリンダ中心からAフセッ1〜して吸気
スワールを発生させるようにしたものである。The embodiments shown in FIGS. 6 and 7 have cross-flow type intake and exhaust boats, and the intake boats I-0 and exhaust boats 1 to 19 are moved from the center of the cylinder to A face 1 to create an intake swirl. It is designed to occur.
この場合、点火栓の位置は、図中8Δもしくは8Bの、
シリンダ外周域で吸気弁5と排気弁18の中間付近に設
定される。In this case, the position of the spark plug is 8Δ or 8B in the figure.
It is set near the middle between the intake valve 5 and the exhaust valve 18 in the cylinder outer peripheral area.
防風部材16として点火栓8のネジ穴20の凹所21を
利用する。すなわち、点火栓8を傾【ノて装着し、点火
ギャップ15がシリンダヘッド壁面から突出しない程度
に設定することにより、凹所21を形成する。なお、ス
ワールの方向に対して点火栓8の背面が向くように点火
栓8を傾斜させる。A recess 21 in a screw hole 20 of a spark plug 8 is used as a windproof member 16. That is, the recess 21 is formed by installing the ignition plug 8 at an angle and setting the ignition gap 15 to such an extent that it does not protrude from the cylinder head wall surface. Note that the ignition plug 8 is tilted so that the back side of the ignition plug 8 faces in the direction of the swirl.
この場合には、燃焼室7の内表面に突出物がないため、
スワールが減衰されにくく、十分な効果を元種できる。In this case, since there is no protrusion on the inner surface of the combustion chamber 7,
Swirl is less likely to be attenuated and sufficient effect can be achieved.
]ス[−のように本発明によれば、点火栓を濃混合気の
存在するシリンダ外周域に配設し、かつ強スI)−ルに
より点火火炎が吹き消えないJ、うに防風部材を形成し
たので、濃い混合気層に安定した6火を行なうことがで
き、特に、トータルとして幅薄燃焼を可能にすると共に
燃焼効率の改善にし35づく燃費の向上がはかれる。According to the present invention, the ignition plug is arranged in the outer peripheral area of the cylinder where a rich air-fuel mixture exists, and the ignition flame is not blown out by a strong spark. As a result, stable combustion can be carried out in a rich air-fuel mixture layer, and in particular, it is possible to achieve wide and lean combustion as a whole, and improve fuel efficiency by 35% due to improved combustion efficiency.
第1図は従来装置の断面図である。
第2図は本発明の第1実施例の断面図、第3図(i同じ
くそのI−I線矢印断面図、第4図(A)。
(B)は防風部材の断面図、第5図は第2実施例の断面
図、第6図は?83実施例のシリンダヘッド底面図、第
7図は同じく防風部材の断面図である。
1・・・吸気マニホールド、2・・−シリンダヘッド、
3・・・吸気ポート、3Δ・・・へりカルポー1〜.4
川燃料噴射インジエクタ、5・・・吸気弁、7・・・燃
焼室、8・・・点火栓、15・・・点火ギャップ、16
・・・防風部(イ、19・・・排気ポート。
特許出願人 日産自動車株式会社
第1図
第2図
第3図
第6図
第7図FIG. 1 is a sectional view of a conventional device. FIG. 2 is a sectional view of the first embodiment of the present invention, FIG. is a sectional view of the second embodiment, FIG. 6 is a bottom view of the cylinder head of the ?83 embodiment, and FIG. 7 is a sectional view of the windshield member. 1...Intake manifold, 2...-Cylinder head,
3... Intake port, 3Δ... Edge Calport 1~. 4
River fuel injection injector, 5... Intake valve, 7... Combustion chamber, 8... Spark plug, 15... Ignition gap, 16
...Windbreak part (A, 19...Exhaust port. Patent applicant: Nissan Motor Co., Ltd. Figure 1 Figure 2 Figure 3 Figure 6 Figure 7
Claims (1)
ともに、吸気系にスワール発生手段を備えた内燃機関に
おいて、上記点火栓をシリンダの外周近傍に配設し、こ
の点火栓のシリンダ内スワール流に対して上流側に防風
部材を設けたことを特徴とする内燃機関の着火装置。-In an internal combustion engine that is equipped with an ignition plug that ignites and burns the air-fuel mixture in the combustion chamber and is equipped with a swirl generating means in the intake system, the above-mentioned ignition plug is arranged near the outer periphery of the cylinder, and the cylinder of this ignition plug is An ignition device for an internal combustion engine, characterized in that a windproof member is provided on the upstream side with respect to an internal swirl flow.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57027758A JPS58144623A (en) | 1982-02-23 | 1982-02-23 | Ignition device for internal-combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57027758A JPS58144623A (en) | 1982-02-23 | 1982-02-23 | Ignition device for internal-combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS58144623A true JPS58144623A (en) | 1983-08-29 |
Family
ID=12229907
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57027758A Pending JPS58144623A (en) | 1982-02-23 | 1982-02-23 | Ignition device for internal-combustion engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58144623A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2016200150A (en) * | 2009-08-20 | 2016-12-01 | ピナクル・エンジンズ・インコーポレイテッドPinnacle Engines, Inc. | High swirl engine |
-
1982
- 1982-02-23 JP JP57027758A patent/JPS58144623A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2016200150A (en) * | 2009-08-20 | 2016-12-01 | ピナクル・エンジンズ・インコーポレイテッドPinnacle Engines, Inc. | High swirl engine |
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