JPS5840648B2 - Internal combustion engine intake system - Google Patents
Internal combustion engine intake systemInfo
- Publication number
- JPS5840648B2 JPS5840648B2 JP53127888A JP12788878A JPS5840648B2 JP S5840648 B2 JPS5840648 B2 JP S5840648B2 JP 53127888 A JP53127888 A JP 53127888A JP 12788878 A JP12788878 A JP 12788878A JP S5840648 B2 JPS5840648 B2 JP S5840648B2
- Authority
- JP
- Japan
- Prior art keywords
- wall surface
- intake port
- spiral
- air
- intake
- 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
Links
Landscapes
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Description
【発明の詳細な説明】 本発明は内燃機関の吸気装置に関する。[Detailed description of the invention] The present invention relates to an intake system for an internal combustion engine.
従来より特にディーゼル機関においては吸気行程時に燃
焼室内に強力な旋回流を発生するためにほぼまっすぐに
延びる入口通路部と渦巻部とにより構成されるヘリカル
型吸気ポートが使用されている。BACKGROUND OF THE INVENTION Conventionally, a helical intake port is used, particularly in diesel engines, which is composed of an almost straight inlet passage and a spiral part in order to generate a strong swirling flow in a combustion chamber during an intake stroke.
しかしながらこのようなヘリカル型吸気ポートをガソリ
ン機関に応用し、機関低速運転時に必要な旋回流を燃焼
室内に発生できるようにディーゼル機関用ヘリカル型吸
気ポートに若干の変更を加えただけではガソリン機関の
使用回転数はディーゼルaJ]に比べてはるかに高いた
めにヘリカル型吸気ポート内を流れる混合気の流れ抵抗
が大きくなり、斯くして機関高速高負荷運転時における
充填効率が低下するという問題がある。However, applying such a helical intake port to a gasoline engine and making slight changes to the helical intake port for a diesel engine to generate the necessary swirling flow in the combustion chamber during low-speed engine operation will not work. Since the operating speed is much higher than that of the diesel AJ, the flow resistance of the air-fuel mixture flowing through the helical intake port becomes large, which causes the problem of reduced charging efficiency during engine high-speed, high-load operation. .
更に機関低速低負荷運転時のように吸気ポート内を流れ
る混合気の流速が遅い場合には吸気ポートをヘリカル形
状に形成しても燃料が十分に霧化混合されず、その結果
者サイクル毎に燃焼室内に供給される混合気の空燃比が
変動するので安定した燃焼を得ることができないという
問題がある。Furthermore, when the flow rate of the air-fuel mixture flowing through the intake port is slow, such as when the engine is running at low speed and low load, even if the intake port is formed into a helical shape, the fuel will not be sufficiently atomized and mixed, resulting in There is a problem in that stable combustion cannot be obtained because the air-fuel ratio of the air-fuel mixture supplied into the combustion chamber fluctuates.
特に吸気ポート内に向けて燃料を噴射するようにしたガ
ソリン噴射式内燃機関では焼料が液滴の状態で吸気ポー
ト内に噴射されるので機関低速低負荷運転時に吸気ポー
ト内において燃料の霧化を促進することが安定した燃焼
を得るために必要となる。In particular, in gasoline-injected internal combustion engines that inject fuel into the intake port, the combustion material is injected into the intake port in the form of droplets, so the fuel is atomized within the intake port during low-speed, low-load engine operation. It is necessary to promote stable combustion.
本発明は機関高速高負荷運転時において充填効率の低下
することのない新規な形状のヘリカル型吸気ポート内に
機関低負荷運転時に空気或いは混合気を噴出せしめ、そ
れによって低負荷運転時における焼料の霧化を促進する
と共に強力な旋回流を燃焼室内に発生せしめるようにし
た吸気装置を提供することにある。The present invention allows air or mixture to be blown out during low-load engine operation into a helical intake port with a new shape that does not reduce filling efficiency during engine high-speed, high-load operation. An object of the present invention is to provide an intake device that promotes atomization of fuel and generates a strong swirling flow inside a combustion chamber.
以下、添付図面を参照して本発明の詳細な説明する。Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.
第1図を参照すると、1は機関本体、2a+2b、2c
、2dは夫々1番気筒、2番気筒、3番気筒、4番気筒
、3は吸気弁、4はヘリカル型吸気ポート、5は排気弁
、6は排気ポートを夫々示す。Referring to Figure 1, 1 is the engine body, 2a+2b, 2c
, 2d are the first cylinder, the second cylinder, the third cylinder, and the fourth cylinder, 3 is an intake valve, 4 is a helical intake port, 5 is an exhaust valve, and 6 is an exhaust port, respectively.
第1図の■−■線に沿ってみた断面図を示す第2図を参
照すると、7はシリンダブロック、8はシリンダブロッ
ク7内に往復運動するピストン、9はシリンダブロック
7上に固締されたシリンダヘッド、10はピストン8と
シリンダヘッド9間に形成された燃焼室、11は点火栓
を夫々示す。Referring to FIG. 2, which is a cross-sectional view taken along the line ■-■ in FIG. 10 is a combustion chamber formed between the piston 8 and the cylinder head 9, and 11 is a spark plug.
第1図並びに第2図に示されるようにシリンダヘッド9
には4本のマニホルド枝管12を有する吸気マニホルド
13が固締され、これら各マニホルド枝管12は夫々対
応する吸気ポート4に接続される。As shown in FIGS. 1 and 2, the cylinder head 9
An intake manifold 13 having four manifold branch pipes 12 is fixed to the intake manifold 13 , and each of these manifold branch pipes 12 is connected to a corresponding intake port 4 .
なお、各マニホルド枝管12には対応する吸気ポート4
内に向けて燃料を噴射するための燃料噴射弁14が取付
けられる。Note that each manifold branch pipe 12 has a corresponding intake port 4.
A fuel injection valve 14 for injecting fuel inward is attached.
吸気マニホルド13内には空気導入管15を介して空気
が導入され、この空気導入管15内に流入空気量を計測
するエアフローメーク16と、図示しないアクセルペダ
ルに連結されたスロットル弁17が設けられる。Air is introduced into the intake manifold 13 through an air introduction pipe 15, and an air flow make 16 for measuring the amount of incoming air and a throttle valve 17 connected to an accelerator pedal (not shown) are provided in the air introduction pipe 15. .
このエアフローメータ16は図示しない燃料噴射量制御
用電子制御回路に接続され、エアフローメータ16の出
力信号に基いて吸入空気量に比例した燃料が燃料噴射弁
14から噴射される。The air flow meter 16 is connected to an electronic control circuit for fuel injection amount control (not shown), and fuel proportional to the amount of intake air is injected from the fuel injection valve 14 based on the output signal of the air flow meter 16.
力、第1図並びに第2図に示されるように各マニホルド
枝管12の下方には機関本体1の長手方向に延びる共通
連通路18が形成され、この共通連通路18から各気筒
の吸気ポート4内に通ずる4本の連通枝路19が分岐さ
れる。As shown in FIGS. 1 and 2, a common communication passage 18 extending in the longitudinal direction of the engine body 1 is formed below each manifold branch pipe 12, and this common communication passage 18 connects to the intake port of each cylinder. Four communication branches 19 leading into the interior of the 4 are branched.
これら各連通枝路19は第2図に示すようにマニホルド
枝管12の下壁面上に開口し、これら各連通枝路19の
開口20は開口20よりも後流に位置する吸気ポート入
口部の上壁面に指向される。Each of these communication branches 19 opens on the lower wall surface of the manifold branch pipe 12, as shown in FIG. Directed towards the top wall.
−力、共通連通路18の中央部は空気供給管21並びに
アイドル調節用ネジ22を介してスロットル弁17上流
の空気導入管15内に連結される。- The central part of the common communication passage 18 is connected to the air introduction pipe 15 upstream of the throttle valve 17 via an air supply pipe 21 and an idle adjustment screw 22.
機関がアイドリング運転成いはそれに近い低負荷運転を
行なっているときには大部分の空気は空気供給管21並
びに共通連通路18を介して連通枝管19から各吸気ポ
ート4内に供給される。When the engine is idling or operating at a low load close to idling, most of the air is supplied into each intake port 4 from the communication branch pipe 19 via the air supply pipe 21 and the common communication passage 18.
このとき第2図に示すように連通枝路19の断面積が小
さいので空気は高速度で連通枝路19から吸気ポート4
内に噴出することになる。At this time, as shown in FIG. 2, since the cross-sectional area of the communication branch 19 is small, air flows from the communication branch 19 to the intake port 4 at high velocity.
It will erupt inside.
一方、スロットル弁17が開弁すると大部分の空気は吸
気マニホルド13を介して各吸気ポート4内に供給され
る。On the other hand, when the throttle valve 17 opens, most of the air is supplied into each intake port 4 via the intake manifold 13.
第4図から第7図は第1図のヘリカル型吸気ポート4の
形状を図解的に示す。4 to 7 schematically show the shape of the helical intake port 4 shown in FIG. 1. FIG.
ヘリカル型吸気ポート4は第5図に示されるように吸気
ポート軸線aがわずかに彎曲した入口通路部Aと渦巻部
Bとにより構成される。As shown in FIG. 5, the helical intake port 4 is composed of an inlet passage section A and a spiral section B, in which the intake port axis a is slightly curved.
入口通路部Aの開口端部は第8図に示されるように矩形
状に形成され、−力渦巻部Bの混合気出口部25は渦巻
部Bの渦巻軸線すと中心とする円筒状に形成される。The opening end of the inlet passage section A is formed in a rectangular shape as shown in FIG. be done.
第2図に示されるように吸気弁3の軸線はシリンダ軸線
に対して傾斜しており、−力入ロ通路部Aはほぼ水平に
延びる。As shown in FIG. 2, the axis of the intake valve 3 is inclined with respect to the cylinder axis, and the force input passage A extends substantially horizontally.
渦巻軸線すから離れた力の入口通路部Aの第1側壁面2
6はほぼ垂直に配置され、この第1側壁而26は渦巻軸
線すを中心として彎゛曲する渦巻部Bの側壁面27に滑
らかに接続する。The first side wall surface 2 of the force inlet passage section A away from the spiral axis
6 is arranged substantially vertically, and this first side wall 26 smoothly connects to the side wall surface 27 of the spiral portion B that curves around the spiral axis.
この側壁面27は第7図或いは第10図に示されるよう
に円筒状出口部25よりも外力に膨出しており、更にこ
の周壁面27は側壁面27と渦巻軸線すとの距離Rが始
めはほぼ一定であるが矢印Cで示す渦巻方向に行くに従
がって徐々に小さくなり力)つ渦巻終端部Eにおいて円
筒状出口部25の半径D/2とほぼ等しくなるように形
成される。As shown in FIG. 7 or 10, this side wall surface 27 bulges out more than the cylindrical outlet portion 25 due to the external force, and furthermore, this peripheral wall surface 27 has a distance R between the side wall surface 27 and the spiral axis. The force is approximately constant, but gradually decreases in the direction of the spiral shown by arrow C, and is formed to be approximately equal to the radius D/2 of the cylindrical outlet portion 25 at the spiral end E. .
−力、渦巻軸線すの入口通路部Aに近い力の第2側壁面
28の上方側壁面28aは下方を向いた傾斜面に形成さ
れ、この傾斜側壁部28aの巾は渦巻部Bに近づくに従
がって広くなり、入口通路部Aと渦巻部Bとの接続部に
おいては第9図に示すように第2側壁面28の全体が下
方に向いた傾斜壁面に形成される。- The upper side wall surface 28a of the force second side wall surface 28 near the inlet passage section A of the force and spiral axis is formed as a downwardly oriented inclined surface, and the width of this inclined side wall section 28a increases as it approaches the spiral section B. Accordingly, the second side wall surface 28 is widened, and the entire second side wall surface 28 at the connection portion between the inlet passage section A and the spiral section B is formed as an inclined wall surface facing downward, as shown in FIG.
従って入口通路部Aの断面形状は入口通路部Aる渦巻部
Bとの接続部においてほぼ台形状をなす。Therefore, the cross-sectional shape of the inlet passage part A is approximately trapezoidal at the connection part between the inlet passage part A and the spiral part B.
第2側壁而28の上半分は第2図において吸気ポート4
内に突出する円筒状突起29の周壁面に滑らかに接続さ
れ、−力第2側壁面28の下半分は渦巻部Bの渦巻終端
部Eにおいて渦巻部Bの側壁面27に接続される。The upper half of the second side wall 28 is the intake port 4 in FIG.
The lower half of the second side wall surface 28 is connected to the side wall surface 27 of the spiral portion B at the spiral end E of the spiral portion B.
入口通路部Aの上壁面30は第2図に示すように入口通
路部Aの開口端部から渦巻部Bに向けてほぼ水平に延び
、次いで渦巻部Bの上壁面31は渦巻方向C(第5図)
に沿って徐々に下降し、次いでこの傾斜上壁面31は入
口通路部Aの第2側壁面28に接続する。As shown in FIG. 2, the upper wall surface 30 of the inlet passage section A extends almost horizontally from the open end of the inlet passage section A toward the spiral section B, and then the upper wall surface 31 of the spiral section B extends in the spiral direction C (the spiral direction C). Figure 5)
The inclined upper wall surface 31 then connects to the second side wall surface 28 of the inlet passage section A.
前述したように入口通路部Aの傾斜側壁部28aの巾が
渦巻部Bに向けて除徐に広がるように形成されているの
で入口通路部Aの土壁面30の巾は渦巻部Bに近ずくに
従がって徐々に狭くなり、一方前述したように渦巻部B
の側壁面27と渦巻軸線すとの距離Rは始めはほぼ一定
であるが渦巻方向Cに徐々に小さくなるように形成され
ているので渦巻部Bの上壁面31の巾は渦巻方向Cに向
かうに従がって徐々に狭くなる。As described above, since the width of the inclined side wall 28a of the entrance passage A is formed to gradually widen toward the spiral part B, the width of the earth wall surface 30 of the entrance passage A approaches the spiral part B. As mentioned above, the spiral part B gradually becomes narrower.
The distance R between the side wall surface 27 of the spiral portion B and the spiral axis is approximately constant at the beginning, but gradually decreases in the spiral direction C. Therefore, the width of the upper wall surface 31 of the spiral portion B tends toward the spiral direction C. It gradually becomes narrower.
従がって入口通路部Aの上壁面30は渦巻部Bに向かっ
てその巾が狭くなりつつほぼ水平に延び、次いでこの上
壁面30に滑らかに接続された渦巻部Bの土壁面31は
その巾が更に狭くなりつつ渦巻方向Cに向けて下降する
ことになる。Therefore, the upper wall surface 30 of the inlet passage section A extends almost horizontally while becoming narrower in width toward the spiral section B, and then the soil wall surface 31 of the spiral section B, which is smoothly connected to this upper wall surface 30, extends toward the spiral section B. The width becomes further narrower as it descends in the spiral direction C.
第2図に示すように入口通路部Aの下壁面32は上壁面
30とほぼ平行をなして渦巻MBに向けてほぼ水平に延
び、次いで第2図に示されるように滑らかな曲壁面33
を経て円筒状出口部25に接続される。As shown in FIG. 2, the lower wall surface 32 of the inlet passage A is approximately parallel to the upper wall surface 30 and extends approximately horizontally toward the spiral MB, and then, as shown in FIG. 2, a smooth curved wall surface 33
It is connected to the cylindrical outlet section 25 through the cylindrical outlet section 25 .
なお第5図かられかるように下壁面32の巾は渦巻部B
に近すくに従がって徐々に狭くなる。As can be seen from FIG. 5, the width of the lower wall surface 32 is the spiral part B.
It gradually narrows as it gets closer to .
機関がアイドリング運転成いはそれに近い低負荷運転を
行なっているとき前述したように大部分の空気が空気供
給管21並びに共通連通路18を介して吸気行程時の気
筒の吸気ポート4内に開口する連通枝路19から高速度
で噴出する。When the engine is idling or operating at a low load similar to idling, most of the air is released into the intake port 4 of the cylinder during the intake stroke via the air supply pipe 21 and the common communication passage 18, as described above. The water is ejected from the communication branch 19 at high speed.
連通枝路19から噴出した空気は第2図において矢印Z
で示すように吸気ポート4の上壁面30に向けて高速度
で前進するがその際傾斜側壁面部28aにより流路を第
1側壁面26側に偏向せしめられつつ前進し、次いで吸
気ポート4の上壁面30に沿って前進することになる。The air blown out from the communication branch 19 is indicated by the arrow Z in FIG.
As shown in , the intake port 4 moves forward toward the upper wall surface 30 at high speed, but at this time, the flow path is deflected toward the first side wall surface 26 side by the inclined side wall surface portion 28 a. It will move forward along the wall surface 30.
前述したように空気の進行方向に向けて土壁面30.3
1の巾は徐々に狭くなり、従がって上壁面30.31に
沿って形成される噴出空気の流路が次第に狭くなるため
に噴出空気の流速は増速されることになる。As mentioned above, the earth wall surface 30.3 is facing the direction of air movement.
1 becomes gradually narrower, and therefore the flow path of the ejected air formed along the upper wall surface 30, 31 becomes gradually narrower, so that the flow velocity of the ejected air is increased.
更に上壁面31は渦巻方向Cに向けて下降しているので
土壁111i1r30.31に沿う噴出空気流は下向き
の力を与えられる。Furthermore, since the upper wall surface 31 is descending in the spiral direction C, the ejected air flow along the earthen wall 111i1r30.31 is given a downward force.
斯くして渦巻部B内には旋回しつつ下降する旋回流が発
生する。In this way, a swirling flow that descends while swirling is generated within the spiral portion B.
一方、燃料噴射弁14から吸気ポート4内に向けて噴射
された燃料液滴は吸気ポート4内に発生した噴出空気の
強力な旋回流によってひきちぎられて微粒化し、斯くし
て燃料の霧化が促進されると共に燃料と空気の混合が促
進される。On the other hand, the fuel droplets injected from the fuel injection valve 14 into the intake port 4 are torn off and atomized by the powerful swirling flow of the jetted air generated in the intake port 4, thus atomizing the fuel. and the mixing of fuel and air is promoted.
上述の噴出空気の増速作用により発生せしめられた強力
な旋回流は次いで円筒状出口部25の内壁面に沿って側
ら抵抗を受けることなく滑らかに旋回し、それによって
渦巻軸線す回りの強力な旋回流が円筒状出口部25内に
おいて形成されることになる。The strong swirling flow generated by the speed-increasing effect of the ejected air then swirls smoothly along the inner wall surface of the cylindrical outlet portion 25 without receiving any side resistance, thereby creating a strong rotation around the spiral axis. A swirling flow is formed within the cylindrical outlet portion 25.
次いでこの旋回混合気は吸気弁3とその弁座間に形成さ
れた間隙を通して燃焼室10内に流入し、燃焼室10内
に強力な旋回流を発生せしめる。This swirling mixture then flows into the combustion chamber 10 through the gap formed between the intake valve 3 and its valve seat, generating a strong swirling flow within the combustion chamber 10.
上述のように燃料噴射弁14から噴射された燃料の霧化
混合が促進されかつ強力な旋回流が燃焼室10内に発生
せしめられるので燃焼速度は大巾に速められ、斯くして
安定したアイドリング運転を確保することができる。As described above, since the atomization and mixing of the fuel injected from the fuel injection valve 14 is promoted and a strong swirling flow is generated within the combustion chamber 10, the combustion speed is greatly increased, thus achieving stable idling. It is possible to secure driving.
一方、スロットル弁17が開弁すると大部分の空気は吸
気マニホルド13を介して各吸気ポート4内に供給され
る。On the other hand, when the throttle valve 17 opens, most of the air is supplied into each intake port 4 via the intake manifold 13.
吸気ポート4内に送り込まれた空気の一部は上壁面30
.31に沿って進行するが残りの空気は入口通路部Aの
傾斜側壁部28aに衝突して下向きの力を与えられ、そ
の結果旋回することなく滑らかな曲壁面33に沿って円
筒状出口部25内に流入する。A portion of the air sent into the intake port 4 is transferred to the upper wall surface 30.
.. 31, the remaining air collides with the inclined side wall 28a of the inlet passage A and is given a downward force, and as a result moves along the smooth curved wall surface 33 without turning to the cylindrical outlet 25. flow inside.
このように傾斜側壁部28aを設けることによって入口
通路部A内に送り込まれた空気の一部は通常の吸気ポー
ト内を流れる空気と同様に旋回することなく滑らかな曲
壁面33に沿って円筒状出口部25内に流入するために
流入抵抗は小さくなり、斯くして高速高負荷運転時にお
ける充填効率の低下を阻止することができる。By providing the inclined side wall portion 28a in this way, a portion of the air sent into the inlet passage A does not swirl like air flowing through a normal intake port, but forms a cylindrical shape along the smooth curved wall surface 33. Since it flows into the outlet portion 25, the inflow resistance becomes small, and thus it is possible to prevent a decrease in filling efficiency during high-speed, high-load operation.
第11図に別の実施例を示す。Another embodiment is shown in FIG.
第11図を参照すると、共通連通路18の中央部は空気
供給管35を介してスロットル弁17とエアフローメー
タ16間の空気導入管15内に連結され、この空気供給
管35内に副スロツトル弁36が設けられる。Referring to FIG. 11, the central part of the common communication passage 18 is connected to the air introduction pipe 15 between the throttle valve 17 and the air flow meter 16 via an air supply pipe 35, and the sub-throttle valve is connected to the air supply pipe 35. 36 are provided.
第12図にスロットル弁17と副スロツトル弁36の開
度関係を示す。FIG. 12 shows the opening relationship between the throttle valve 17 and the sub-throttle valve 36.
第12図において縦軸Pはスロットル弁開度を示し、横
軸りはアクセルペダルの踏込み量を示す。In FIG. 12, the vertical axis P shows the throttle valve opening, and the horizontal axis shows the amount of depression of the accelerator pedal.
なお、曲線Sは副スロットル弁36の開1度を示し、曲
線Tはスロットル弁17の開度を示す。Note that the curve S indicates the opening degree of the sub-throttle valve 36, and the curve T indicates the opening degree of the throttle valve 17.
第12図からアクセルペダルが踏込まれるとスロットル
弁17が全閉状態に保持されたまま副スロツトル弁36
が徐々に開弁じ、副スロツトル弁36がほぼ全開になる
と副スロツトル弁36が全開状態に保持されたままスロ
ットル弁17が徐々に開弁せしめられることがわかる。As shown in FIG. 12, when the accelerator pedal is depressed, the sub-throttle valve 36 remains closed while the throttle valve 17 remains fully closed.
It can be seen that when the sub-throttle valve 36 is gradually opened and the sub-throttle valve 36 is almost fully opened, the throttle valve 17 is gradually opened while the sub-throttle valve 36 is kept fully open.
なお、スロットル弁17と副スロツトル弁36とは第1
2図に示す開度関係を有するように図示しないリンク機
構により互いに連結される。Note that the throttle valve 17 and the sub-throttle valve 36 are
They are connected to each other by a link mechanism (not shown) so as to have the opening relationship shown in FIG.
第12図から明らかなようにこの実施例では低負荷運転
時に全ての空気が空気供給管35並びに共通連通路18
を介して連通枝路19から吸気ポート4内に供給され、
斯くして低負荷運転時における燃料の霧化混合が促進さ
れると共に強力な旋回流を燃焼室10内に発生させるこ
とができる。As is clear from FIG. 12, in this embodiment, during low load operation, all the air is supplied to the air supply pipe 35 and the common communication path 18.
is supplied into the intake port 4 from the communication branch 19 via
In this way, atomization and mixing of fuel during low-load operation is promoted, and a strong swirling flow can be generated within the combustion chamber 10.
−力、高負荷運転時にはスロットル弁17が開弁するた
めに大部分の空気は流れ抵抗の小さな吸気マニホルド枝
管12を介して吸気ポート4内に供給され、斯くして高
い充填効率を確保することができる。- During high power and high load operation, the throttle valve 17 opens, so most of the air is supplied into the intake port 4 through the intake manifold branch pipe 12 with low flow resistance, thus ensuring high filling efficiency. be able to.
第13図並びに第14図は別の実施例を示す。13 and 14 show another embodiment.
この実施例では共通連通路18は各連通枝管19を介し
て各吸気ポート4内のみに連結される。In this embodiment, the common communication path 18 is connected only to each intake port 4 via each communication branch pipe 19.
またスロットル弁17にカロえて第2スロツトル弁40
が各マニホルド枝管12内に設けられる。Additionally, a second throttle valve 40 is added to the throttle valve 17.
is provided within each manifold branch 12.
これらの各第2スロツトル弁40は共通のスロットル軸
41に固定され、この共通スロットル軸41はマニホル
ド枝管12の底部内壁面上に形成された模型凹所42内
に配置される。Each of these second throttle valves 40 is fixed to a common throttle shaft 41, and this common throttle shaft 41 is arranged in a model recess 42 formed on the bottom inner wall surface of the manifold branch pipe 12.
スロットル弁17と第2スロツトル弁40とはスロット
ル弁17が開弁するにつれて第2スロツトル弁40が開
弁するように図示しないリンク機構を介して互いに連結
される。The throttle valve 17 and the second throttle valve 40 are connected to each other via a link mechanism (not shown) so that the second throttle valve 40 opens as the throttle valve 17 opens.
第13図に示すような4気筒内燃機関において点火順序
が例えば1−3−4−2の場合、1番気筒2aが吸気行
程時であるとすると3番気筒2cは排気行程にある。When the ignition order is, for example, 1-3-4-2 in a four-cylinder internal combustion engine as shown in FIG. 13, if the first cylinder 2a is in the intake stroke, the third cylinder 2c is in the exhaust stroke.
通常排気行程末期には吸気弁3と排気弁5とが共に開弁
する弁重合時期が存在するがこの排気行程末期の弁重合
時期には比較的高圧の既燃ガスが3番気筒の燃焼室10
内から3番気筒の吸気ポート4内に吹き返し、それによ
って3番気筒の吸気ポート4内は正圧となる。Normally, at the end of the exhaust stroke, there is a valve polymerization period when both the intake valve 3 and the exhaust valve 5 open, but during this valve polymerization period at the end of the exhaust stroke, relatively high pressure burnt gas flows into the combustion chamber of the No. 3 cylinder. 10
The air is blown back from the inside into the intake port 4 of the third cylinder, thereby creating a positive pressure inside the intake port 4 of the third cylinder.
−力、3番気筒2cが排気行程末期のときには1番気筒
2aの吸気ポート4内には大きな負圧が発生しており、
従がってこのとき3番気筒2cの吸気ポート4内の既燃
ガス或いは空気が3番気筒2cの吸気ポート4に開口す
る連通枝路19を介して共通連通路18内に押込まれ、
次いでこの押込まれた既燃ガス或いは空気が1番気筒2
aの吸気ポート4内に開口する連通枝路19を介して1
番気筒2aの吸気ポート4内に高速度で噴出することに
なる。-When the No. 3 cylinder 2c is at the end of its exhaust stroke, a large negative pressure is generated in the intake port 4 of the No. 1 cylinder 2a.
Therefore, at this time, the burned gas or air in the intake port 4 of the third cylinder 2c is forced into the common communication passage 18 via the communication branch 19 that opens to the intake port 4 of the third cylinder 2c,
Next, this pushed-in burned gas or air flows into the first cylinder 2.
1 through a communication branch 19 opening into the intake port 4 of a.
It will be ejected at high speed into the intake port 4 of the number cylinder 2a.
同様にして残りの気筒においても吸気行程時には他の気
筒から共通連通路18内に送り込まれた既燃ガス或いは
空気が連通枝路19から吸気ポート4内に噴出する。Similarly, in the remaining cylinders, during the intake stroke, the burnt gas or air sent into the common communication passage 18 from other cylinders is ejected from the communication branch passage 19 into the intake port 4.
なお、第13図並びに第14図に示すように特に低負荷
運転時には第2スロツトル弁40を設けることによって
吹き返し作用により昇圧した吸気ポート4内の圧力を減
衰させることなく正圧のまま暫くの間維持できるので連
通枝路19から長時間に亘って吸気ポート4内に既燃ガ
ス或いは空気を噴出せしめることができる。As shown in FIGS. 13 and 14, especially during low-load operation, by providing the second throttle valve 40, the pressure inside the intake port 4, which has increased due to the blowback effect, remains positive for a while without being attenuated. Since this can be maintained, burnt gas or air can be ejected from the communication branch 19 into the intake port 4 for a long period of time.
また第14図に示されるようにこの実施例では低負荷運
転時に第2スロツトル弁40における空気流通間隙43
が第2スロツトル弁40の上縁部とマニホルド枝管12
の上部内壁面間に形成されるために第2スロツトル弁4
0を通過した空気は吸気ポート4の土壁面30.31に
沿って進むことになる。Furthermore, as shown in FIG. 14, in this embodiment, the air flow gap 43 in the second throttle valve 40 during low load operation is
is the upper edge of the second throttle valve 40 and the manifold branch pipe 12.
The second throttle valve 4 is formed between the upper inner wall surfaces of the second throttle valve 4.
The air that has passed through 0 will proceed along the soil wall surface 30, 31 of the intake port 4.
従って低負荷運転時には連通枝路19から噴出した既燃
ガス或いは空気と空気流通間隙43を通過した空気とに
より吸気ポート4内に強力な旋回流が発生せしめられる
ことになる。Therefore, during low load operation, a strong swirling flow is generated in the intake port 4 by the burnt gas or air ejected from the communication branch 19 and the air passing through the air circulation gap 43.
第15図並びに第16図に本発明を気化器付内燃機関に
適中した場合を示す。FIG. 15 and FIG. 16 show the case where the present invention is applied to an internal combustion engine with a carburetor.
第15図並びに第16図を参照すると、シリンダヘッド
9に気化器45を備えた吸気マニホルド46が固定され
、この吸気マニホルド46の各マニホルド枝管47は夫
々対応する吸気ポート4に連結される。Referring to FIGS. 15 and 16, an intake manifold 46 including a carburetor 45 is fixed to the cylinder head 9, and each manifold branch pipe 47 of the intake manifold 46 is connected to a corresponding intake port 4.
気化器スロットル弁48にカロえて更に各マニホルド枝
管47内には第2スロツトル弁49が設けられ、これら
各第2スロツトル弁49は共通のスロットル軸50に固
定される。In addition to the carburetor throttle valve 48, a second throttle valve 49 is provided in each manifold branch pipe 47, and each of the second throttle valves 49 is fixed to a common throttle shaft 50.
共通スロットル軸50にはアーム51が固定され、この
アーム51θ)先端部に負圧ダイヤフラム装置52の制
御ロッド53が枢着される。An arm 51 is fixed to the common throttle shaft 50, and a control rod 53 of a negative pressure diaphragm device 52 is pivotally attached to the tip of the arm 51θ).
負圧ダイヤフラム装置52はダイヤフラム54により隔
成された負圧室55と大気圧室56とを有し、負圧室5
5内にダイヤフラム押圧用圧縮はね57が挿入される。The negative pressure diaphragm device 52 has a negative pressure chamber 55 and an atmospheric pressure chamber 56 separated by a diaphragm 54.
A compression spring 57 for pressing the diaphragm is inserted into the diaphragm 5 .
この負圧室55は負圧導管58を介してスロットル弁4
8後流の吸気マニホルド46内に連結される。This negative pressure chamber 55 is connected to the throttle valve 4 via a negative pressure conduit 58.
8 downstream of the intake manifold 46.
一方、この実施例では第15図に示すように各連通枝路
19の開口20は吸気ポート4の入口通路部Aの軸線力
向に指向される。On the other hand, in this embodiment, the opening 20 of each communication branch 19 is oriented in the axial direction of the inlet passage A of the intake port 4, as shown in FIG.
また、第15図並びに第16図に示すように共通連結路
18の中央部は副吸気通路59を介して吸気マニホルド
集合部46aに連結される。Further, as shown in FIGS. 15 and 16, the central portion of the common connecting passage 18 is connected to the intake manifold gathering portion 46a via a sub-intake passage 59.
第16図に示すように気化器スロットル弁48の開度が
小さな低負荷運転時には気化器スロットル弁48後流の
吸気マニホルド46内の負圧は大きく、この犬さな負圧
が負圧ダイヤフラム装置52の負圧室55内に加わるた
めにダイヤフラム54は圧縮はね57を抗して上昇し、
その結果第2スロツトル弁49は第16図に示されるよ
うに全閉位置をとる。As shown in FIG. 16, during low-load operation with a small opening degree of the carburetor throttle valve 48, the negative pressure in the intake manifold 46 downstream of the carburetor throttle valve 48 is large, and this small negative pressure is applied to the negative pressure diaphragm device. The diaphragm 54 rises against the compression spring 57 in order to enter the negative pressure chamber 55 of 52,
As a result, the second throttle valve 49 assumes the fully closed position as shown in FIG.
一方、気化器スロットル弁48が大きく開かれて高負荷
運転が行なわると負圧室55内の負圧が小さくなるため
にダイヤフラム54は圧縮ばね57のばね力により下降
し、その結果第2スロツトル弁49は全開する。On the other hand, when the carburetor throttle valve 48 is wide open and high-load operation is performed, the negative pressure in the negative pressure chamber 55 becomes small, so the diaphragm 54 is lowered by the spring force of the compression spring 57, and as a result, the second throttle Valve 49 is fully opened.
上述したように低負荷運転時には第2スロツトル弁49
が全閉状態に保持されているので気化器45において形
成された混合気は副吸気通路59並びに共通連通路18
を介して連通枝路19から各吸気ポート4内に噴出する
。As mentioned above, during low load operation, the second throttle valve 49
is maintained in a fully closed state, the air-fuel mixture formed in the carburetor 45 flows through the sub-intake passage 59 and the common communication passage 18.
The air is ejected from the communication branch 19 into each intake port 4 through the communication branch 19 .
第16図に示すように副吸気通路59並びに共通連通路
18は比較的小さな断面積を有するために混合気はこれ
ら通路59.18内を高速度で流れ、その結果これら通
路59.18内において燃料の気化が促進される。As shown in FIG. 16, since the sub-intake passage 59 and the common communication passage 18 have a relatively small cross-sectional area, the air-fuel mixture flows at a high velocity in these passages 59.18, and as a result, the mixture flows in these passages 59.18 at a high velocity. Fuel vaporization is promoted.
次いて混合気は連通枝路19から矢印Zで示すように噴
出した後吸気ポート4内に吸気ポート上壁面30に沿っ
て進行し、斯くして吸気ポート4内には強力な旋回流が
発生する。Next, the air-fuel mixture is ejected from the communication branch 19 as shown by the arrow Z, and then advances into the intake port 4 along the intake port upper wall surface 30, thus generating a strong swirling flow inside the intake port 4. do.
その結果燃料の気化が更に促進され、しかも燃焼室10
内に強力な旋回流が発生せしめられるので燃焼速度は速
められ、斯くして安定した燃焼を得ることができる9
この実施例では各マニホルド枝管47内に夫々第2スロ
ツトル弁49や設けることによって各連通枝路19から
噴出する混合気の噴出速度を速めることができる。As a result, the vaporization of the fuel is further promoted, and the combustion chamber 10
Since a strong swirling flow is generated within the manifold branch pipes 47, the combustion speed is increased, and stable combustion can thus be obtained.9 In this embodiment, a second throttle valve 49 or a The jetting speed of the air-fuel mixture jetting out from each communication branch 19 can be increased.
即ち、第2スロツトル弁49がマニホルド枝管47内に
設けられていないとすると例えば1番気筒2aの吸気行
程時には他の気筒2b、2c、2dの吸気ポート4内に
夫々対応すする連通枝路19から噴出しれ混合気が吸気
マニホルド46を介して1番気筒2aの吸気ポート4内
に供給され、その結果1番気筒2aの吸気ポート4内に
開口する連通枝路19力)ら噴出する混合気量が減少し
、斯くして連通枝路19から噴出する混合気の速度が低
下する。That is, if the second throttle valve 49 is not provided in the manifold branch pipe 47, for example, during the intake stroke of the first cylinder 2a, the communication branch pipes corresponding to the intake ports 4 of the other cylinders 2b, 2c, and 2d, respectively. The air-fuel mixture blown out from 19 is supplied into the intake port 4 of the No. 1 cylinder 2a through the intake manifold 46, and as a result, the mixture is blown out from the communication branch 19 which opens into the intake port 4 of the No. 1 cylinder 2a. The air volume decreases and thus the speed of the air-fuel mixture emerging from the communication branch 19 decreases.
しかしながら第15図に示すように第2スロツトル弁4
9をマニホルド枝管47内に配置することによって混合
気は連通枝路19のみから供給されるので連通枝管19
から噴出する混合気の流速を速めることができ、斯くし
て吸気ポート4内に強力な旋回流を発生させることがで
きる。However, as shown in FIG.
9 in the manifold branch pipe 47, the air-fuel mixture is supplied only from the communication branch pipe 19.
The flow velocity of the air-fuel mixture ejected from the intake port 4 can be increased, and a strong swirling flow can be generated within the intake port 4.
一力、高負荷運転時には前述したように第2スロツトル
弁49が全開するので気化器45において形成された混
合気の大部分は流れ抵抗の小さな吸気マニホルド46を
介して各吸気ポート4内に供給され、斯くして高速高負
荷運転時における高い充填効率を確保することができる
。During high-load operation, the second throttle valve 49 is fully opened as described above, so most of the air-fuel mixture formed in the carburetor 45 is supplied into each intake port 4 through the intake manifold 46 with low flow resistance. In this way, high filling efficiency can be ensured during high-speed, high-load operation.
以上述べたように本発明によれば高速高負荷運転時にお
いても充填効率の低下しない新規な構造のヘリカル型吸
気ポート内に低負荷運転時にヘリカル型吸気ポートの土
壁面に沿うように空気或いは混合気を高速度で噴出せし
め、それによって燃料の霧化或いは気化を促進すること
ができると共に燃焼室内に強力な旋回流を発生せしめる
ことができる。As described above, according to the present invention, air or mixture is distributed along the soil wall surface of the helical intake port during low-load operation into the helical-type intake port, which has a novel structure that does not reduce filling efficiency even during high-speed, high-load operation. Air is ejected at high speed, thereby promoting atomization or vaporization of fuel and generating a strong swirling flow within the combustion chamber.
その結果、低負荷運転時における燃焼速度は大巾に増大
し、安定した燃焼を確保することができる。As a result, the combustion speed during low-load operation increases significantly, making it possible to ensure stable combustion.
第1図は本発明に係る内燃機関の平面図、第2図は第1
図の■−■線に沿ってみた側面断面図、第3図は第2図
のIII −III線に沿ってみた断面図、第4図は第
2図のヘリカル型吸気ポートを図解的に示す斜視図、第
5図は第4図の矢印■に沿ってみたヘリカル型吸気ポー
トの平面図、第6図は第4図の矢印■に沿ってみたヘリ
カル型吸気ポートの側面図、第7図は第4図の矢印■に
沿ってみたヘリカル型吸気ポートの側面図、第8図は第
5図の■−■線に沿ってみた断面図、第9図は第5図の
■−■線に沿ってみた断面図、第10図は第5図のX−
X線に沿ってみた断面図、第11図は別の実施例の側面
図、第12図は第11図のスロットル弁と副スロツトル
弁の開度変化を示すグラフ、第13図は更に別の実施例
の平面図、第14図は第13図の側面断面図、第15図
は更に別の実施例の平面図、第16図は第15図の側面
断面図である。
3・・・・・・吸気弁、4・・・・・・ヘリカル型吸気
ポート、5・・・・・・排気弁、10・・・・・・燃焼
室、11・・・・・・点火栓、13.46・・・・・・
吸気マニホルド、14・・・・・・燃料噴射弁、16・
・・・・・エアクローメータ、17・・・・・・スロッ
トル弁、18・・・・・・共通連通路、19・・・・・
・連通枝路、21.35・・・・・・空気供給管、36
・・・・・・副スロツトル弁、40.49・・・・・・
第2スロツトル弁、45・・・・・・気化器。FIG. 1 is a plan view of an internal combustion engine according to the present invention, and FIG.
Figure 3 is a cross-sectional view taken along line III--III in Figure 2, Figure 4 schematically shows the helical intake port in Figure 2. A perspective view, Figure 5 is a plan view of the helical intake port taken along the arrow ■ in Figure 4, Figure 6 is a side view of the helical intake port taken along the arrow ■ in Figure 4, and Figure 7. is a side view of the helical intake port taken along the arrow ■ in Figure 4, Figure 8 is a sectional view taken along the line ■-■ in Figure 5, and Figure 9 is a cross-sectional view taken along the line ■-■ in Figure 5. Figure 10 is a cross-sectional view taken along the line X- in Figure 5.
11 is a side view of another embodiment, FIG. 12 is a graph showing changes in the opening of the throttle valve and sub-throttle valve of FIG. 11, and FIG. 13 is a diagram of another embodiment. FIG. 14 is a plan view of the embodiment, FIG. 14 is a side sectional view of FIG. 13, FIG. 15 is a plan view of yet another embodiment, and FIG. 16 is a side sectional view of FIG. 15. 3...Intake valve, 4...Helical intake port, 5...Exhaust valve, 10...Combustion chamber, 11...Ignition Stopper, 13.46...
Intake manifold, 14...Fuel injection valve, 16.
...Air crow meter, 17...Throttle valve, 18...Common communication path, 19...
・Communication branch, 21.35... Air supply pipe, 36
・・・・・・Sub-throttle valve, 40.49・・・・・・
2nd throttle valve, 45... carburetor.
Claims (1)
構成されたヘリカル型吸気ポートであって、該入口通路
部が渦巻部渦巻軸線から離れた側に位置するほぼ垂直位
置の第1側壁面と、該渦巻軸線側に位置しかつ該第1側
壁面と対面するほぼ垂直配置の第2側壁面と、はぼ水平
面内を延びる土壁面および下壁面とにより構成され、そ
れによって該入口通路部が全長に亘ってほぼ矩形断面形
状を有する・\リカル型吸気ポートを具備した内燃機関
において、上記渦巻軸線側に位置する第2側壁面の上方
部を下向きの傾斜面に形成すると共に該傾斜面の巾を上
記渦巻部に近づくにつれて次第に広くして該入口通路部
の上壁面の巾を該渦巻部に向けて徐々に狭くし、該入口
通路部と渦巻部の接続部において該第2側壁面のほぼ全
体を下向きの傾斜面に形成して該接続部における入口通
路部の断面形状を上壁面の巾が下壁面の巾よりも狭い台
形状に形成し、該渦巻部の土壁面を渦巻方向に向けて徐
々に下降せしめ、上記吸気ポートに通ずる吸気通路とは
別個に共通連通路を設けて該共通連通路を連通枝路を介
して夫々各気筒の吸気ポート内に連結し、該連通枝路を
該吸気ポート入口部の下壁面上に開口せしめると共に該
連通枝路開口から噴出した空気或いは混合気が上記傾斜
面に向けて流れるように連通枝路開口を該連通枝路開口
下流の吸気ポート上壁面に指向せしめた内燃機関の吸気
装置。1 is a helical intake port composed of an inlet passage portion extending approximately straight and a spiral portion, wherein the inlet passage portion has a first side wall surface located at a substantially vertical position on a side away from the spiral axis of the spiral portion; , a second side wall surface located on the spiral axis side and facing the first side wall surface and arranged substantially vertically, and a soil wall surface and a lower wall surface extending in a substantially horizontal plane, thereby forming the inlet passage section. In an internal combustion engine equipped with a rectangular-type intake port having a substantially rectangular cross-sectional shape over the entire length, the upper part of the second side wall surface located on the spiral axis side is formed into a downwardly inclined surface, and the inclined surface is The width of the upper wall surface of the inlet passage section is gradually narrowed toward the spiral section by gradually increasing the width as it approaches the spiral section, and the width of the second side wall surface is gradually narrowed toward the spiral section. The cross-sectional shape of the inlet passage in the connection part is formed into a trapezoidal shape in which the width of the upper wall surface is narrower than the width of the lower wall surface, and the soil wall surface of the spiral part is formed in a spiral direction. A common communication passage is provided separately from the intake passage leading to the intake port, and the common communication passage is connected to the intake port of each cylinder through a communication branch, and the communication branch is opened on the lower wall surface of the intake port inlet portion, and the communication branch passage opening is connected to the intake port downstream of the communication branch passage opening so that the air or air-fuel mixture ejected from the communication branch passage opening flows toward the inclined surface. An internal combustion engine intake system directed toward the upper wall.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP53127888A JPS5840648B2 (en) | 1978-10-19 | 1978-10-19 | Internal combustion engine intake system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP53127888A JPS5840648B2 (en) | 1978-10-19 | 1978-10-19 | Internal combustion engine intake system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5554627A JPS5554627A (en) | 1980-04-22 |
| JPS5840648B2 true JPS5840648B2 (en) | 1983-09-07 |
Family
ID=14971134
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP53127888A Expired JPS5840648B2 (en) | 1978-10-19 | 1978-10-19 | Internal combustion engine intake system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5840648B2 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0742861B2 (en) * | 1986-03-10 | 1995-05-15 | ヤマハ発動機株式会社 | Internal combustion engine intake system |
| JP4975218B2 (en) * | 2001-04-19 | 2012-07-11 | いすゞ自動車株式会社 | Power transmission gear parking brake |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5317822A (en) * | 1976-08-04 | 1978-02-18 | Mitsubishi Motors Corp | Intake apparatus for engine |
-
1978
- 1978-10-19 JP JP53127888A patent/JPS5840648B2/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5554627A (en) | 1980-04-22 |
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