JPH0415935Y2 - - Google Patents

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Publication number
JPH0415935Y2
JPH0415935Y2 JP1985138029U JP13802985U JPH0415935Y2 JP H0415935 Y2 JPH0415935 Y2 JP H0415935Y2 JP 1985138029 U JP1985138029 U JP 1985138029U JP 13802985 U JP13802985 U JP 13802985U JP H0415935 Y2 JPH0415935 Y2 JP H0415935Y2
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JP
Japan
Prior art keywords
intake
guide plate
combustion chamber
swirl
engine
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
Application number
JP1985138029U
Other languages
Japanese (ja)
Other versions
JPS6247733U (en
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Filing date
Publication date
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Priority to JP1985138029U priority Critical patent/JPH0415935Y2/ja
Publication of JPS6247733U publication Critical patent/JPS6247733U/ja
Application granted granted Critical
Publication of JPH0415935Y2 publication Critical patent/JPH0415935Y2/ja
Expired legal-status Critical Current

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  • Characterised By The Charging Evacuation (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

【考案の詳細な説明】 〈産業上の利用分野〉 本考案はヘリカル型吸気ポートを備えた内燃機
関の吸気装置に関する。
[Detailed Description of the Invention] <Industrial Application Field> The present invention relates to an intake system for an internal combustion engine having a helical intake port.

〈従来の技術〉 ヘリカル型吸気ポートは通常機関のシリンダヘ
ツド内吸気ポートの終端部に吸気弁を囲んで渦巻
部が設けられる。そして該渦巻部により吸気に旋
回流を与え、吸気弁開弁時にこの旋回流を燃焼室
に導入して燃焼室内に大きなスワールを形成し、
空気と燃料との混合を促進することにより燃焼を
改善しようとしている。
<Prior Art> A helical intake port is usually provided with a spiral portion surrounding an intake valve at the terminal end of the intake port in the cylinder head of an engine. Then, the swirl portion gives a swirling flow to the intake air, and when the intake valve is opened, this swirling flow is introduced into the combustion chamber to form a large swirl in the combustion chamber,
Attempts are made to improve combustion by promoting mixing of air and fuel.

ところで上記ヘリカル型吸気ポートを備えた直
接噴射式デイーゼル機関を例にとつてみると、第
4図に示すように、スワール比(機関のクランク
軸の回転速度に対する吸気旋回速度)は、その最
適値が機関の低速回転領域から高速回転領域に移
行するに従つて次第に減少するのが望ましいとさ
れている(第4図点線)。しかし上記のようなヘ
リカル型吸気ポートではポート形状が固定化され
ているため、第4図実線で示すように、機関回転
速度に対して略一定のスワール比しか得られず、
このためポート形状を低速領域にマツチングさせ
るべく設計すれば、高速領域ではスワール過剰
(オーバースワール)となり、燃焼が悪化して排
気中のスワールが増加し燃費低下を招くと共に、
スワールポートの余分な吸気抵抗(ポンピングロ
ス)を受けて吸気充填効率が悪化し高出力化の阻
害要因となる一方、高速領域にマツチングさせれ
ば低速領域ではスワール不足となつて燃焼効率が
低下する不都合がある。
By the way, if we take the above-mentioned direct injection diesel engine equipped with a helical intake port as an example, as shown in Fig. 4, the swirl ratio (intake swirl speed relative to the rotational speed of the engine crankshaft) is at its optimum value. It is said that it is desirable that the amount decreases gradually as the engine moves from a low-speed rotation region to a high-speed rotation region (dotted line in Figure 4). However, since the helical intake port described above has a fixed port shape, only a substantially constant swirl ratio can be obtained with respect to the engine rotational speed, as shown by the solid line in Figure 4.
Therefore, if the port shape is designed to match the low speed range, there will be excessive swirl (overswirl) in the high speed range, which will worsen combustion and increase the swirl in the exhaust, leading to a decrease in fuel efficiency.
Excess intake resistance (pumping loss) from the swirl port deteriorates intake air filling efficiency, which hinders high output. On the other hand, if it is matched to high-speed ranges, there will be insufficient swirl in low-speed ranges, reducing combustion efficiency. There is an inconvenience.

上記不都合に対策するため従来では、第5図に
示すように、機関運転状態に応じヘリカル型吸気
ポートの渦流室に出没するスワール制御装置を設
けたものが開発されている(例えば特開昭57−
62927号、特開昭58−2425号、特開昭58−2426号
及び実開昭58−81319号参照)。
To counter the above-mentioned disadvantages, a device has been developed that is equipped with a swirl control device that appears in and out of the swirl chamber of the helical intake port depending on the engine operating condition, as shown in Fig. 5 (for example, in Japanese Patent Laid-Open No. 57 −
62927, JP-A-58-2425, JP-A-58-2426, and Utility Model JP-A-58-81319).

このうち特開昭57−62927号に例をとつて説明
すると、内燃機関のシリンダヘツド1内には、吸
気弁2のまわりに設けた渦巻部3と、該渦巻部3
の上流端に接続する略直線状の導入部4と、を備
えたヘリカル型吸気ポートが形成してあり、上記
渦巻部3の下流端内で機関運転状態に応じ吸気上
流側又は吸気弁2の弁軸方向に向け出没するスワ
ール制御装置5が設けてある。該スワール制御装
置5は、機関低速回転時に渦巻部3から退避し
て、渦巻部3内を吸気流が円滑に流れるようにし
もつて燃焼室内のスワール強化を図るが、高速回
転時には、渦巻部3内に先端ピストン部5aが突
出し吸気流に抵抗を与えてオーバースワールの防
止を図る。
To explain this using JP-A No. 57-62927 as an example, in the cylinder head 1 of an internal combustion engine there is a spiral portion 3 provided around the intake valve 2, and a spiral portion 3 provided around the intake valve 2.
A helical intake port is formed with a substantially linear introduction part 4 connected to the upstream end of the spiral part 3, and a helical intake port is formed with a substantially linear introduction part 4 connected to the upstream end of the spiral part 3. A swirl control device 5 that appears and retracts in the direction of the valve shaft is provided. The swirl control device 5 retreats from the swirl portion 3 when the engine rotates at low speed to strengthen the swirl in the combustion chamber by making the intake air flow smoothly through the swirl portion 3. However, when the engine rotates at high speed, the swirl control device 5 retreats from the swirl portion 3. A tip piston portion 5a protrudes inside to provide resistance to the intake air flow and prevent overswirl.

〈考案が解決しようとする問題点〉 第5図に示すようなスワール制御装置5を備え
たヘリカル型吸気ポートにあつては、特開昭57−
62927号に係る明細書が説明によると、高速時に
先端ピストン部5aが渦巻部3内に突出したと
き、この突出量に応じ吸気流の渦巻部3内の滞留
時間が短くなり、早期に燃焼室に入るので、吸気
充填効率が向上するとある。
<Problems to be solved by the invention> Regarding a helical intake port equipped with a swirl control device 5 as shown in FIG.
According to the specification of No. 62927, when the tip piston portion 5a protrudes into the spiral portion 3 at high speed, the residence time of the intake air flow within the spiral portion 3 is shortened according to the amount of protrusion, and the combustion chamber is quickly filled. It is said that this improves the intake air filling efficiency.

しかし実際には先端ピストン部5aは吸気流に
対して邪魔板のように立ち塞がり、先端ピストン
部5aに衝突後の吸気流に方向性を付与すること
なく渦巻部3内の吸気流を大きく乱すと共に単に
吸気抵抗となるのみで、渦巻部3内の吸気流の円
滑な流れを阻害し圧力損失を与えて、吸気充填効
率を低下させ、その結果高速回転領域で充分な出
力が得られないという惧れがあつた。
However, in reality, the tip piston portion 5a stands against the intake air flow like a baffle plate, and greatly disturbs the intake air flow in the spiral portion 3 without imparting directionality to the intake air flow after colliding with the tip piston portion 5a. At the same time, it simply becomes an intake resistance, which obstructs the smooth flow of the intake air flow in the spiral portion 3 and causes pressure loss, reducing the intake air filling efficiency, and as a result, sufficient output cannot be obtained in the high-speed rotation region. I was afraid.

本考案は従来の吸気装置の上述のような不都合
に鑑み、機関低速回転領域等では強力なスワール
を燃焼室内に形成して燃焼効率を向上させる一
方、機関高速回転領域等では渦巻部の吸気流にス
ワールとは別方向の方向性を持たせて燃焼室内に
吸気流を円滑に導入し、もつて圧力損失なく吸気
充填効率を向上させることを目的とする。
In view of the above-mentioned disadvantages of conventional intake systems, the present invention improves combustion efficiency by forming a strong swirl in the combustion chamber in low engine speed ranges, etc., while improving combustion efficiency in high engine speed ranges. The purpose is to smoothly introduce the intake air flow into the combustion chamber by giving it a direction different from the swirl, thereby improving the intake air filling efficiency without pressure loss.

〈問題点を解決するための手段〉 吸気弁軸周りを囲むように、かつ上壁部が螺旋
を描いて徐々に燃焼室に近づくよう設けられた渦
巻通路により渦巻部を形成してなるヘリカル型吸
気ポートを備えた内燃機関において、渦巻部内に
設けられた吸気流を上流側面に衝突せしめて燃焼
室方向へ流線を変更させる位置と吸気流に略平行
な位置との間で回動自由に構成され、かつ、燃焼
室へ向かう程吸気弁軸へ接近するように吸気弁軸
に対して傾斜した回動軸上に設けられた案内板
と、該案内板を機関運転状態に応じて回動しその
回動位置を定める案内板回動装置とを備えて構成
される。
<Means for solving the problem> A helical type in which a spiral portion is formed by a spiral passage provided so as to surround the intake valve shaft and the upper wall gradually approaches the combustion chamber in a spiral manner. In an internal combustion engine equipped with an intake port, it can freely rotate between a position where the intake flow provided in the volute collides with the upstream side surface and changes the streamline toward the combustion chamber, and a position approximately parallel to the intake flow. and a guide plate provided on a rotating shaft that is inclined with respect to the intake valve axis so as to approach the intake valve axis as it goes toward the combustion chamber, and the guide plate is rotated according to the engine operating state. and a guide plate rotation device for determining the rotation position of the guide plate.

〈作用〉 これにより機関低速回転領域等スワールを必要
とする領域では案内板を可及的に吸気流に平行に
なるようその回動位置を案内板回動装置により位
置決めして、旋回流を円滑に渦巻部内に発生さ
せ、即ち吸気流の水平成分、旋回成分を強化し、
ヘリカル型吸気ポートの有する特徴を最大限に発
揮せしめてスワールを増大し、燃焼を良好にして
未然成分の排出を防止し燃費の向上を図る。特
に、案内板を、燃焼室へ向かう程吸気弁軸へ接近
するように吸気弁軸に対して傾斜した回動軸上に
設けたので、吸気流は渦巻部を弁軸の周りに旋回
して流れながら通路の上壁部に案内されて燃焼室
方向へ下降していく際、燃焼室へ近づく程弁軸に
近づけられることになり、その結果、吸気流は弁
軸を中心とする小さな回転半径の旋回を与えられ
て、旋回の角速度が増大し、燃焼室へ実際に導入
された吸気のスワールが十分に加速され、燃焼改
善、未燃成分の排出防止、燃費の向上等の上記効
果を更に高めることができる。また機関が高速回
転領域等高出力を必要とする領域では、案内板回
動装置を作動して案内板の回動位置をその上流側
面が吸気流に対向する方向に定め、渦巻部におい
て強化された水平成分の大きい吸気流に案内板に
より燃焼室方向に向く成分の大きい吸気流に変換
して吸気を円滑に即ち損失少なく燃焼室に導き、
充填効率の向上する。これによりもともと燃焼効
率が良い高速回転領域の燃焼効率を悪化させるこ
となく充填効率の向上により出力を増大させかつ
排気中のカーボン排出量を低減して燃費の向上を
図る。
<Operation> As a result, in areas where swirl is required, such as in low-speed engine rotation areas, the rotational position of the guide plate is determined by the guide plate rotation device so that the guide plate is parallel to the intake air flow as much as possible, thereby smoothing the swirl flow. In other words, the horizontal component and swirling component of the intake flow are strengthened.
The characteristics of the helical intake port are maximized to increase swirl, improve combustion, prevent the emission of unnatural components, and improve fuel efficiency. In particular, since the guide plate is installed on a rotation axis that is inclined to the intake valve axis so that it approaches the intake valve axis as it goes toward the combustion chamber, the intake air flow rotates around the valve axis through the spiral part. As it flows, it is guided by the upper wall of the passage and descends toward the combustion chamber, and the closer it gets to the combustion chamber, the closer it gets to the valve shaft.As a result, the intake flow has a small rotation radius around the valve shaft. As a result, the angular velocity of the swirl increases, and the swirl of the intake air actually introduced into the combustion chamber is sufficiently accelerated, further enhancing the above-mentioned effects such as improving combustion, preventing the emission of unburned components, and improving fuel efficiency. can be increased. In addition, in areas where the engine requires high output such as high-speed rotation areas, the guide plate rotation device is operated to set the rotation position of the guide plate in a direction where its upstream side faces the intake air flow, and the volute is strengthened. The intake air flow with a large horizontal component is converted into an intake air flow with a large horizontal component directed toward the combustion chamber by a guide plate, and the intake air is guided smoothly into the combustion chamber with less loss.
Improves filling efficiency. As a result, the output is increased by improving the charging efficiency without deteriorating the combustion efficiency in the high-speed rotation range where the combustion efficiency is originally high, and the amount of carbon emissions in the exhaust gas is reduced to improve fuel efficiency.

〈実施例〉 以下に本考案を実施例に基づいて説明する。<Example> The present invention will be explained below based on examples.

第1図及び第2図は本考案の一実施例を示すも
ので、機関のシリンダヘツド11には各燃焼室1
2に夫々連通するヘリカル型吸気ポート13を有
する。ヘリカル型吸気ポート13は、図示しない
吸気マニホルドに連通する略直線上の導入部14
と、その下流に接続されかつ吸気弁15を介して
燃焼室12に連通する渦巻部20と、からなる。
渦巻部20は吸気弁15周りを囲むようにかつ上
壁21が縲線を描いて徐々に燃焼室12に近づく
ように形成され、その下流端は燃焼室12近くで
再び渦巻部20上流端部に連通接続されている。
1 and 2 show an embodiment of the present invention, in which each combustion chamber 1 is provided in a cylinder head 11 of an engine.
It has a helical intake port 13 that communicates with each of the two ports. The helical intake port 13 has a substantially linear introduction portion 14 that communicates with an intake manifold (not shown).
and a spiral portion 20 connected downstream thereof and communicating with the combustion chamber 12 via the intake valve 15.
The spiral portion 20 is formed so as to surround the intake valve 15 and gradually approach the combustion chamber 12 with the upper wall 21 drawing a straight line, and its downstream end is near the combustion chamber 12 and returns to the upstream end of the spiral portion 20. is connected to.

渦巻部20の終端部には、吸気弁15の弁軸を
含む平面内に配設された案内板22を有する。案
内板22は略方形状となつており、渦巻部20の
終端部上壁のシリンダヘツド11内に設けられた
凹部23内を回動自由であつて、上端に設けた円
板24が前記凹部23の上底壁に対し回転摺動自
由又は多少のクリアランスを介して回動自由にな
つている。案内板22の上端にはシリンダヘツド
11内を回動自由に貫通するシヤフト25が設け
てあり、該シヤフト25の上端にはナツト26に
よりレバー27の一端が固定され、該レバー27
の他端には案内板回動装置30が連結されてい
る。
The terminal end of the spiral portion 20 has a guide plate 22 disposed within a plane containing the valve shaft of the intake valve 15 . The guide plate 22 has a substantially rectangular shape, and is freely rotatable within a recess 23 provided in the cylinder head 11 on the upper wall of the terminal end of the spiral portion 20, and a disc 24 provided at the upper end moves into the recess. It is free to rotate and slide with respect to the upper bottom wall of 23, or to be free to rotate through some clearance. A shaft 25 that freely rotates through the cylinder head 11 is provided at the upper end of the guide plate 22. One end of a lever 27 is fixed to the upper end of the shaft 25 with a nut 26.
A guide plate rotation device 30 is connected to the other end.

案内板回動装置30は、レバー27先端にボー
ルジヨイント28を介して各気筒毎のレバー27
を一連に連結するコネクテイングバー31と、該
バー31を移動する電磁アクチユエータ32と、
機関回転速度を検出する速度スイツチ33と、該
速度スイツチ33が所定値以上の機関回転速度を
検出したときに電磁アクチユエータ32を作動し
てコネクテイングバー31を変位させレバー27
を介して案内板22を吸気弁15の弁軸を含む平
面内に位置すべく回動する制御手段34と、を含
んで構成される。機関回転速度が所定値以下の低
速回転領域にある場合には、これを速度スイツチ
33が検出し、電磁アクチユエータ32が消磁さ
れて、案内板22を吸気弁15の弁軸を中心軸と
する円上面内に略位置するように図示しないリタ
ーンスプリングの弾性復元力により回動させる。
The guide plate rotating device 30 connects the lever 27 for each cylinder via a ball joint 28 at the tip of the lever 27.
a connecting bar 31 that connects the bar 31 in series; an electromagnetic actuator 32 that moves the bar 31;
A speed switch 33 detects the engine rotation speed, and when the speed switch 33 detects an engine rotation speed equal to or higher than a predetermined value, the electromagnetic actuator 32 is actuated to displace the connecting bar 31 and the lever 27 is operated.
and a control means 34 that rotates the guide plate 22 to position it within a plane containing the valve shaft of the intake valve 15 via the control means 34. When the engine rotation speed is in a low rotation range below a predetermined value, the speed switch 33 detects this, the electromagnetic actuator 32 is demagnetized, and the guide plate 22 is rotated in a circle with the valve shaft of the intake valve 15 as the central axis. It is rotated by the elastic restoring force of a return spring (not shown) so that it is located approximately within the upper surface.

尚、この場合速度スイツチ33が所定の機関回
転速度を境としてオンオフする上記の如き構成で
あれば、制御手段34を省略することもできる
が、機関回転速度を連続的に検出する速度センサ
である場合には、制御手段34は案内板22の回
動位置を機関回転速度に応じて定めるように構成
してもよい。
In this case, if the speed switch 33 is configured as described above to turn on and off at a predetermined engine rotation speed, the control means 34 may be omitted, but it is possible to omit the control means 34, but instead of using a speed sensor that continuously detects the engine rotation speed. In some cases, the control means 34 may be configured to determine the rotational position of the guide plate 22 in accordance with the engine rotation speed.

従つて上記構成によると、機関回転速度が所定
値以下の低速回転領域にあることを速度スイツチ
33が検出した場合には、電磁アクチユエータ3
2が消磁されて、図示しないリターンスプリング
により、コネクテイングバー31を移動し、各気
筒毎のレバー27を回動して、吸気弁15の弁軸
に対し、燃焼室12へ向かう程接近するように傾
斜した回動軸25を介し、案内板22を吸気弁1
5の弁軸を中心軸とする断面円弧状の面に略位置
するように回動する。一方、導入部14から導入
された吸気は渦巻部20内に流入し、吸気弁15
の弁軸周りを旋回すると同時に渦巻部20の上壁
21に案内されて燃焼室12方向に押し下げられ
る。
Therefore, according to the above configuration, when the speed switch 33 detects that the engine rotation speed is in a low rotation range below a predetermined value, the electromagnetic actuator 3
2 is demagnetized, the connecting bar 31 is moved by a return spring (not shown), and the lever 27 for each cylinder is rotated so that it approaches the valve shaft of the intake valve 15 toward the combustion chamber 12. The guide plate 22 is connected to the intake valve 1 via the rotating shaft 25 inclined to
It rotates so that it is approximately located on a plane having an arcuate cross section with the valve shaft of No. 5 as the central axis. On the other hand, the intake air introduced from the introduction part 14 flows into the spiral part 20 and the intake valve 15
At the same time, it is guided by the upper wall 21 of the spiral portion 20 and pushed down toward the combustion chamber 12.

ここにおいて案内板22は上記の如く吸気弁1
5周りの吸気流に対して略平行となつているから
吸気流を何ら阻害する要因を持たず、このため吸
気旋回流Aは円滑に燃焼室12内に導かれて内部
に強いスワールを形成する。その結果、空気と燃
焼室内で噴射供給される燃料との混合が促進さ
れ、空気利用率が向上して燃焼が良好になること
により未燃成分の排出量が低減して燃費を向上さ
せることができる。
Here, the guide plate 22 is connected to the intake valve 1 as described above.
Since it is approximately parallel to the intake air flow around 5, there is no factor that obstructs the intake air flow, and therefore the intake air swirl flow A is smoothly guided into the combustion chamber 12, forming a strong swirl inside. . As a result, mixing of air and fuel injected into the combustion chamber is promoted, improving air utilization efficiency and improving combustion, which reduces emissions of unburned components and improves fuel efficiency. can.

また機関回転速度が所定値以上の高速回転領域
になると、これを速度スイツチ33が検出して制
御手段34を介し電磁アクチユエータ32を通電
励磁し、コネクテイングバー31、レバー27を
介して案内板22を第1図、第2図示位置即ち吸
気弁15の弁軸を含む平面内に持ちきたす。この
ため渦巻部20内の前記吸気旋回流は、案内板2
2の上流側面に衝突し吸気弁15のステム方向に
偏流され旋回流が弱められる。吸気流は案内板2
2に衝突してこれより上方と下方とに分流しよう
とするが、上方位置には凹部23及び円盤24が
あり、吸気の上方向流が阻止されて、全量が下方
即ち燃焼室12内に向けて円滑に流れる。その結
果吸気は流路変更による圧力損失を最小限に抑え
つつ吸気弁15軸方向成分の強い流れとなり、充
填効率が増大して出力向上を図ることができ、更
にはオーバースワールを防止して燃焼効率を向上
させ、もつて燃費の向上を図ることができる。
When the engine rotational speed reaches a high rotational speed range equal to or higher than a predetermined value, the speed switch 33 detects this and energizes the electromagnetic actuator 32 via the control means 34, and controls the guide plate 22 via the connecting bar 31 and the lever 27. is brought to the position shown in FIGS. 1 and 2, that is, within a plane containing the valve shaft of the intake valve 15. Therefore, the intake air swirling flow in the spiral portion 20 is caused by the guide plate 2
The air collides with the upstream side of the intake valve 15 and is deflected toward the stem of the intake valve 15, weakening the swirling flow. Intake flow is guided by guide plate 2
However, there is a recess 23 and a disk 24 in the upper position, which prevents the upward flow of intake air and directs the entire amount downward, that is, into the combustion chamber 12. flows smoothly. As a result, the intake air has a strong flow in the axial direction of the intake valve 15 while minimizing the pressure loss caused by changing the flow path, increasing the charging efficiency and improving the output.Furthermore, it prevents overswirl and combustion. Efficiency can be improved, and fuel efficiency can also be improved.

尚、上記実施例において案内板22の形状を略
方形としたが、下流端を曲縁にする等その形状は
上記実施例に限るものではない。例えば第3図に
示すように、案内板22Aを吸気弁15の弁軸を
中心軸とする円錐状の断面翼形にすると、低速回
転領域においては、渦巻部20内の吸気旋回流と
全く平行となつて吸気流に対する圧力損失、乱れ
の発生をより良く防止することができ、これによ
り燃焼室内に吸入される吸気スワールは強化され
る。案内板22Aの両側縁を滑らかな曲面形状に
すると上記効果は更に助長される。第3図に示す
実施例では、高速回転時に案内板22Aの凹面を
吸気旋回流の上流側に位置させると、案内板22
Aは吸気流を確実に捕集してこれを燃焼室12方
向に向かわせることができるので、吸気充填効率
は更に向上する。
In the above embodiment, the shape of the guide plate 22 is approximately rectangular, but the shape is not limited to the above embodiment, such as having a curved edge at the downstream end. For example, as shown in FIG. 3, if the guide plate 22A is made into a conical cross-sectional airfoil shape with the valve axis of the intake valve 15 as the center axis, in the low speed rotation region, the guide plate 22A is completely parallel to the intake swirl flow in the spiral portion 20. As a result, it is possible to better prevent pressure loss and turbulence in the intake flow, thereby strengthening the intake swirl sucked into the combustion chamber. The above effect is further enhanced by forming both side edges of the guide plate 22A into a smooth curved shape. In the embodiment shown in FIG. 3, when the concave surface of the guide plate 22A is positioned on the upstream side of the intake swirl flow during high-speed rotation, the guide plate 22A
Since A can reliably collect the intake air flow and direct it toward the combustion chamber 12, the intake air filling efficiency is further improved.

案内板22,22Aの軸心は、吸気弁15の弁
軸に対し、案内板22,22Aの下端を上端に較
べやや吸気下流側に傾斜させるようにしてもよ
い。このようにすると、案内板22,22Aに衝
突した後の吸気流はより滑らかに圧力損失なく燃
焼室12へと導入され吸気流の大きな乱れを防止
することができるから、充填効率がより向上す
る。このようにしても吸気旋回流を阻止する作用
に変わりはない。
The axes of the guide plates 22 and 22A may be such that the lower ends of the guide plates 22 and 22A are inclined slightly toward the intake downstream side compared to the upper ends with respect to the valve axis of the intake valve 15. In this way, the intake air flow after colliding with the guide plates 22, 22A is introduced into the combustion chamber 12 more smoothly without pressure loss, and large turbulence of the intake air flow can be prevented, so that the charging efficiency is further improved. . Even if this is done, there is no change in the effect of blocking the intake swirl flow.

案内板回動装置も上記実施例に限るものではな
いことは言うまでもない。機関運転状態を検出す
るのに速度スイツチ33或いは速度センサを用い
たが、機関の吸入負圧、吸気スロツトルバルブ開
度、アクセルペダル開度位置、デイーゼル機関の
燃焼噴射ポンプのコントロールレバー位置、燃料
噴射弁の制御バルス幅等の1つ、またこれらの組
み合わせを用いることができる。電磁アクチユエ
ータ32の代わりに他の動力源例えば吸入負圧、
オイル圧等を用いてもよい。
It goes without saying that the guide plate rotating device is not limited to the above embodiment. The speed switch 33 or speed sensor is used to detect the engine operating state, but the engine's intake negative pressure, intake throttle valve opening, accelerator pedal opening position, diesel engine combustion injection pump control lever position, fuel One or a combination of these can be used, such as the control pulse width of the injector. Instead of the electromagnetic actuator 32, other power sources such as suction negative pressure,
Oil pressure or the like may also be used.

案内板22の回動位置は全開全閉の2位置間で
機関運転状態に応じた値をとることができるよう
にしてもよいことは既述した。これによりスワー
ル及び充填効率の機関運転状態に応じた最適値を
得ることができる。
As described above, the rotational position of the guide plate 22 may be set to a value depending on the engine operating state between two positions, fully open and fully closed. This makes it possible to obtain optimum values of swirl and charging efficiency according to the engine operating conditions.

〈考案の効果〉 以上述べたように本考案によると、ヘリカル型
吸気ポートにおいて渦巻部にその上流側面で吸気
流を受けて燃焼室方向へ流線を変更させる位置
と、吸気旋回流に略平行な位置と、の間で、機関
運転状態に応じ案内板を回動するようにしたの
で、特に機関低速回転領域におけるスワールの確
保が図られ、もつて燃焼改善、未燃成分の排出防
止、燃費向上、が図られる一方、特に機関高速回
転領域におけるオーバースワールの防止、吸気充
填効率ひいては出力の増大が図られる。また、案
内板を、燃焼室へ向かう程吸気弁軸へ接近するよ
うに吸気弁軸に対して傾斜した回動軸上に設けた
ので、案内板を吸気流に略平行な位置に設定した
状態においては、吸気流は渦巻部を弁軸の周りに
旋回して流れながら渦巻部上壁により燃焼室方向
へ下降していく際、燃焼室へ近づく程吸気弁軸を
中心とする小さな回転半径の旋回を与えられて旋
回の角速度が増大し、燃焼室へ実際に導入された
吸気のスワールを十分に加速することができ、燃
焼改善、未燃成分の排出防止、燃費の向上等の上
記効果を更に高めることができる。
<Effects of the invention> As described above, according to the invention, the spiral portion of the helical intake port receives the intake air flow at its upstream side face and changes its streamline toward the combustion chamber, and the position is approximately parallel to the intake swirl flow. Since the guide plate rotates between the two positions depending on the engine operating condition, it is possible to ensure swirl, especially in the low engine speed range, which improves combustion, prevents the emission of unburned components, and improves fuel efficiency. At the same time, it is possible to prevent overswirl, particularly in the engine high-speed rotation region, and to increase the intake air filling efficiency and thus the output. In addition, since the guide plate is installed on a rotation axis that is inclined with respect to the intake valve axis so that it approaches the intake valve axis as it goes toward the combustion chamber, the guide plate is set at a position approximately parallel to the intake flow. In the , when the intake air flows through the spiral part swirling around the valve shaft and descends toward the combustion chamber by the upper wall of the spiral part, the closer it gets to the combustion chamber, the smaller the radius of rotation around the intake valve shaft becomes. The rotation increases the angular velocity of the rotation, and the swirl of the intake air actually introduced into the combustion chamber can be sufficiently accelerated, resulting in the above-mentioned effects such as improving combustion, preventing the emission of unburned components, and improving fuel efficiency. It can be further increased.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本考案に係る吸気装置の一実施例を示
す第2図の−矢視断面図、第2図は同上の
−矢視断面図、第3図は本考案の他の実施例を
示す第1図相当図、第4図は機関回転速度とスワ
ール比との関係図、第5図は従来の内燃機関の吸
気装置を示す図である。 11……シリンダヘツド、12……燃焼室、1
3……ヘリカル型吸気ポート、14……導入部、
15……吸気弁、20……渦巻部、22……案内
板、30……案内板回動装置。
Fig. 1 is a cross-sectional view taken in the direction - arrow of Fig. 2 showing one embodiment of the intake device according to the present invention, Fig. 2 is a sectional view taken in the - arrow direction of the same as above, and Fig. 3 shows another embodiment of the present invention. FIG. 4 is a diagram corresponding to FIG. 1, FIG. 4 is a diagram showing the relationship between engine rotational speed and swirl ratio, and FIG. 5 is a diagram showing a conventional intake system for an internal combustion engine. 11... Cylinder head, 12... Combustion chamber, 1
3...Helical intake port, 14...Introduction part,
15... Intake valve, 20... Spiral section, 22... Guide plate, 30... Guide plate rotation device.

Claims (1)

【実用新案登録請求の範囲】 吸気弁軸周りを囲むように、かつ上壁部が螺旋
を描いて徐々に燃焼室に近づくよう設けられた渦
巻通路により渦巻部を形成してなるヘリカル型吸
気ポートを備えた内燃機関において、 渦巻部内に設けられた吸気流を上流側面に衝突
せしめて燃焼室方向へ流線を変更させる位置と吸
気流に略平行な位置との間で回動自由に構成さ
れ、かつ、燃焼室へ向かう程吸気弁軸へ接近する
ように吸気弁軸に対して傾斜した回動軸上に設け
られた案内板と、 該案内板を機関運転状態に応じて回動しその回
動位置を定める案内板回動装置と、 を備えたことを特徴とする内燃機関の吸気装置。
[Scope of Claim for Utility Model Registration] A helical intake port in which a spiral portion is formed by a spiral passage provided so as to surround the intake valve shaft and gradually approach the combustion chamber as the upper wall draws a spiral. In an internal combustion engine with and a guide plate provided on a rotating shaft that is inclined with respect to the intake valve axis so as to approach the intake valve axis toward the combustion chamber, and the guide plate is rotated according to the engine operating state. An intake device for an internal combustion engine, comprising: a guide plate rotation device that determines a rotation position;
JP1985138029U 1985-09-11 1985-09-11 Expired JPH0415935Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1985138029U JPH0415935Y2 (en) 1985-09-11 1985-09-11

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1985138029U JPH0415935Y2 (en) 1985-09-11 1985-09-11

Publications (2)

Publication Number Publication Date
JPS6247733U JPS6247733U (en) 1987-03-24
JPH0415935Y2 true JPH0415935Y2 (en) 1992-04-09

Family

ID=31042635

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1985138029U Expired JPH0415935Y2 (en) 1985-09-11 1985-09-11

Country Status (1)

Country Link
JP (1) JPH0415935Y2 (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60175732A (en) * 1984-02-21 1985-09-09 Komatsu Ltd Intake-air port

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS588906Y2 (en) * 1978-06-12 1983-02-17 ヤンマーディーゼル株式会社 Variable swirl device for internal combustion engine
JPS60192226U (en) * 1984-05-30 1985-12-20 日野自動車株式会社 Internal combustion engine intake system

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60175732A (en) * 1984-02-21 1985-09-09 Komatsu Ltd Intake-air port

Also Published As

Publication number Publication date
JPS6247733U (en) 1987-03-24

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