JPS588901Y2 - engine intake system - Google Patents

engine intake system

Info

Publication number
JPS588901Y2
JPS588901Y2 JP1977004348U JP434877U JPS588901Y2 JP S588901 Y2 JPS588901 Y2 JP S588901Y2 JP 1977004348 U JP1977004348 U JP 1977004348U JP 434877 U JP434877 U JP 434877U JP S588901 Y2 JPS588901 Y2 JP S588901Y2
Authority
JP
Japan
Prior art keywords
combustion chamber
cylinder head
intake port
intake
opening
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
JP1977004348U
Other languages
Japanese (ja)
Other versions
JPS5399410U (en
Inventor
桜井茂
Original Assignee
マツダ株式会社
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 マツダ株式会社 filed Critical マツダ株式会社
Priority to JP1977004348U priority Critical patent/JPS588901Y2/en
Publication of JPS5399410U publication Critical patent/JPS5399410U/ja
Application granted granted Critical
Publication of JPS588901Y2 publication Critical patent/JPS588901Y2/en
Expired legal-status Critical Current

Links

Description

【考案の詳細な説明】 この考案はエンジンの吸気装置に関する。[Detailed explanation of the idea] This invention relates to an engine intake system.

従来より、エンジンに供給される混合気を燃焼室に対し
て接線方向に流入させて、燃焼室内での混合気のスワー
ルを強化し、もって燃焼性能を向上させるようにした吸
気装置は周知である。
BACKGROUND ART Intake systems are conventionally known that allow the air-fuel mixture supplied to the engine to flow tangentially into the combustion chamber to strengthen the swirl of the air-fuel mixture within the combustion chamber, thereby improving combustion performance. .

上記の周知の吸気装置の具体例を第1図、第2図によっ
て説明すると、1はシリンダヘッド、2はシリンダブロ
ック、3はシリンダヘッド1とシリンダブロック2とに
よって形成される燃焼室、4はシリンダヘッド1に設け
られた吸気ポートで、その一端は燃焼室3に、他端はシ
リンダヘッド側壁1aに開口しており、このシリンダヘ
ッド側壁1aの開口は図示しない吸気管と連通している
A specific example of the above-mentioned well-known intake system will be explained with reference to FIGS. 1 and 2. 1 is a cylinder head, 2 is a cylinder block, 3 is a combustion chamber formed by the cylinder head 1 and the cylinder block 2, and 4 is a combustion chamber formed by the cylinder head 1 and the cylinder block 2. An intake port provided in the cylinder head 1 has one end opening into the combustion chamber 3 and the other end opening into the cylinder head side wall 1a, and the opening in the cylinder head side wall 1a communicates with an intake pipe (not shown).

5は吸気ポート4の燃焼室側開口6に設けた弁座6aを
開閉する吸気弁である。
Reference numeral 5 designates an intake valve that opens and closes a valve seat 6a provided at an opening 6 of the intake port 4 on the combustion chamber side.

上記吸気ポート4の燃焼室側聞口6とシリンダヘッド側
壁1aに開口する側壁側聞ロアとは水平方向に偏倚して
おり、吸気ポート4は、上記側壁側聞ロアからシリンダ
ヘッド側壁1aに対してほぼ直角方向(すなわち水平方
向)に延びる直線状部8と、この直線状部8に連続し、
直線状部8からシリンダの接線方向に湾曲して燃焼室側
聞口6に連通ずる曲線状部9とによって構成されている
The combustion chamber side opening 6 of the intake port 4 and the sidewall side lower opening to the cylinder head side wall 1a are offset in the horizontal direction, and the intake port 4 is located from the sidewall side lower to the cylinder head sidewall 1a. a linear portion 8 extending in a substantially perpendicular direction (i.e., horizontal direction);
It is composed of a straight part 8 and a curved part 9 that curves in the tangential direction of the cylinder and communicates with the combustion chamber side port 6.

なお、10はピストン、11は排気ポートの燃焼室側開
口、12は点火プラグである。
Note that 10 is a piston, 11 is an opening of an exhaust port on the combustion chamber side, and 12 is a spark plug.

上記従来の吸気ポートの構造では、第1図に示すように
、曲がり方向側の直線状部側面8aの延長面P1は、燃
焼室側聞口6(好ましくは弁座6a)の周縁に接すると
共に直線状部側面8aに平行な面P2より下方tこ設定
されており、上記41面を22面より上方に設定するこ
とは配置上困難であった。
In the above conventional intake port structure, as shown in FIG. It is set t below the plane P2 parallel to the linear part side surface 8a, and it is difficult to set the 41st plane above the 22nd plane in terms of arrangement.

従ってこの場合、22面より上側を流れる混合気は曲線
状部9によって81方向に流れるが22面と41面との
間を流れる混合気はS2方向に流れる。
Therefore, in this case, the air-fuel mixture flowing above the 22nd surface flows in the 81 direction due to the curved portion 9, but the air-fuel mixture flowing between the 22nd surface and the 41st surface flows in the S2 direction.

すなわちS1方尚のスワールはS1方向と逆の82方向
の流れによって弱められるので、強いスワールを得るこ
とはできなかった。
In other words, the swirl in the S1 direction was weakened by the flow in the 82 direction opposite to the S1 direction, so a strong swirl could not be obtained.

またS2方尚の混合気が吸気ポート4の壁面に衝突する
際、燃料粒子が吸気ポート壁面に付着し、この燃料粒子
がフィルム状で燃焼室3内に流入して燃焼性の向上を阻
害していた。
Furthermore, when the air-fuel mixture on the S2 side collides with the wall of the intake port 4, fuel particles adhere to the wall of the intake port, and these fuel particles flow into the combustion chamber 3 in the form of a film, impeding the improvement of combustibility. was.

この考案は上記欠点を除去した吸気装置を提供するもの
である。
This invention provides an air intake device that eliminates the above-mentioned drawbacks.

この考案の実施例を第3図、第4図によって説明する。An embodiment of this invention will be explained with reference to FIGS. 3 and 4.

なお、第1,2図と同一部分は同じ符号を付し、その説
明を省略する。
Note that the same parts as in FIGS. 1 and 2 are designated by the same reference numerals, and their explanation will be omitted.

上記曲線状部9(こおいて、吸気ポート4上面より直線
状部底面8bの延長面P3に至る範囲内で垂下し、かつ
上記燃焼室側聞口6(好ましくは弁座6a)の周縁に接
すると共に直線状部8の側面8aに平行な面P2と、曲
り方向側の直線状部側面8aの延長面P1との間の範囲
内に、曲り方向とほぼ同方向に延びる案内翼13を設け
たものである。
The curved portion 9 (here, the curved portion 9 hangs down from the upper surface of the intake port 4 to the extension surface P3 of the straight portion bottom surface 8b, and extends to the periphery of the combustion chamber side opening 6 (preferably the valve seat 6a). A guide vane 13 extending in substantially the same direction as the bending direction is provided within a range between a plane P2 that is in contact with and parallel to the side surface 8a of the linear part 8 and an extended plane P1 of the linear part side surface 8a on the bending direction side. It is something that

上記に説明した実施例では、12面と11面との間を流
れる混合気は、上記案内翼13によって83方向の流れ
となり、S1方向の混合気流とともに燃焼室3の接線方
向に流入する。
In the embodiment described above, the air-fuel mixture flowing between the 12th surface and the 11th surface flows in 83 directions by the guide vanes 13, and flows in the tangential direction of the combustion chamber 3 together with the air-fuel mixture flow in the S1 direction.

また混合気に含まれる燃料粒子は、吸気ポート4壁面と
案内翼13とに2分されて付着することになり、従って
燃料粒子の混合気への拡散が良好となる。
Further, the fuel particles contained in the air-fuel mixture are divided into two parts and adhere to the wall surface of the intake port 4 and the guide vane 13, so that the fuel particles can be efficiently diffused into the air-fuel mixture.

さらに案内翼13は従来装置におけるS2方向の混合気
流れを阻止すべく必要最小限の範囲にのみ設けたので、
吸気抵抗を増大し吸気充填効率を低下するのを最小限に
押されることが可能となる。
Furthermore, since the guide vanes 13 were provided only in the minimum necessary range to prevent the mixture flow in the S2 direction in the conventional device,
Increase in intake resistance and decrease in intake air filling efficiency can be minimized.

さらにまた、案内翼13は、11面、12面で囲まれる
範囲で、吸気ポート4の曲がり方向とほぼ同方向に延び
るように適宜選択すればよいが、単一の案内翼13を設
ける場合は第3図に示すように吸気ポート4のほぼ中央
部に設けることが好ましい。
Furthermore, the guide vane 13 may be appropriately selected so as to extend in substantially the same direction as the bending direction of the intake port 4 within the range surrounded by the 11th and 12th faces, but when a single guide vane 13 is provided, As shown in FIG. 3, it is preferable to provide it approximately at the center of the intake port 4.

以上に説明したようにこの考案は、シリンダヘッドに設
けられる吸気ポートの燃焼室側開口とシリンダヘッド側
壁側開口とを水平方向に偏倚させると共に、上記吸気ポ
ートを、シリンダヘッド側壁側聞口からシリンダヘッド
側壁に対しほぼ直角に延びる直線状部と、該直線状部に
連続し、直線状部からシリンダの接線方向に埠曲して上
記燃焼室側開口に連通ずる曲線状部とによって構成し、
吸入混合気を燃焼室(こ対して接線方向に流入させるよ
うにしてなるエンジンの吸気装置において、上記曲線状
部において、吸気ポート上面より直線状部底面の延長面
に至る範囲で垂下し、かつ上記燃焼室側開口の周縁に接
すると共に直線状部の側面に平行な面と、曲がり方向側
の直線状部側面の延長面との間の範囲内に曲がり方向と
ほぼ同方向(こ延びる案内翼を設けたものであるから、
吸気ポートに導入された混合気は強力なスワールとなっ
て燃焼室内に流入され、燃焼室内での燃焼性は著しく向
上される。
As explained above, this invention horizontally deviates the combustion chamber side opening of the intake port provided in the cylinder head and the cylinder head side wall side opening, and also moves the intake port from the cylinder head side wall side opening to the cylinder head. Consisting of a straight part extending substantially perpendicular to the head side wall, and a curved part continuous with the straight part, curved from the straight part in the tangential direction of the cylinder, and communicating with the combustion chamber side opening,
In an engine intake system configured to allow the intake air-fuel mixture to flow tangentially into the combustion chamber, the above-mentioned curved portion hangs down from the top surface of the intake port to the extension surface of the bottom surface of the straight portion, and A guide vane extending in substantially the same direction as the bending direction within the range between a surface that is in contact with the periphery of the combustion chamber side opening and parallel to the side surface of the straight section and an extended surface of the side surface of the straight section on the bending direction side. Since it has been established,
The air-fuel mixture introduced into the intake port becomes a strong swirl and flows into the combustion chamber, and the combustibility within the combustion chamber is significantly improved.

また混合気に含まれる燃料粒子は、吸気ポート壁面のは
か(こ上記案内翼(こも分割されて付着し、この付着燃
料粒子は強力な方向性をもった混合気に均一に混合拡散
されるので、燃焼性はより改善される。
In addition, the fuel particles contained in the air-fuel mixture are separated and adhered to the guide vanes on the wall of the intake port, and these adhering fuel particles are uniformly mixed and diffused into the air-fuel mixture with strong directionality. Therefore, flammability is further improved.

また、案内翼は必要最小限の範囲にのみ設けたので吸気
充填効率の低下を最小限に押さえることができる。
Further, since the guide vanes are provided only in the minimum necessary range, the reduction in intake air filling efficiency can be suppressed to the minimum.

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

第1図はエンジンの吸気装置の従来の例の模型的平面図
、第2図;ま第1図の■−■線切断側面図、第3図はこ
の考案の実施例の第1図同様の平面図、第4図は第3図
のIV−■線切断側面図である。 1・・・・・・シリンダヘッド、1a・・・・・・シリ
ンダヘッド側壁、4・・・・・・吸気ポート、6・・・
・・・燃焼室側開口、7・・・・・・シリンダヘッド側
壁側開口、8・・・・・・直線状部、8a・・・・・・
直線状部側面、8b・・・・・・直線状部底面、9・・
・・・・曲線状部、13・・・・・・案内翼、Pl・・
・・・・曲がり方向側の直線状部側面の延長面、P2・
・・・・・燃焼室側開口の周縁に接するとともに直線状
部側面(こ平行な面、P3・・・・・・直線状部底面の
延長面。
Fig. 1 is a schematic plan view of a conventional example of an engine intake system, Fig. 2 is a side view cut along the line ■-■ of Fig. 1, and Fig. 3 is a schematic plan view of a conventional example of an engine intake system; The plan view and FIG. 4 are side views taken along the line IV--■ in FIG. 3. 1... Cylinder head, 1a... Cylinder head side wall, 4... Intake port, 6...
...Combustion chamber side opening, 7...Cylinder head side wall side opening, 8...Straight portion, 8a...
Linear part side surface, 8b... Linear part bottom surface, 9...
...Curved portion, 13...Guide vane, Pl...
・・・Extension surface of the side surface of the straight part on the bending direction side, P2・
...The side surface of the linear part that is in contact with the periphery of the opening on the combustion chamber side (parallel to this, P3... An extension of the bottom surface of the linear part.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] シリンダヘッドに設けられる吸気ポートの燃焼室側開口
とシリンダヘッド側壁側開口とを水平方向に偏倚させる
と共に、上記吸気ポートをシリンダヘット側壁側開口か
らシリンダヘッドIP&に対してほぼ直角に延びる直線
状部と、この直線状部に連続し、直線状部からシリンダ
の接線方向に湾曲して燃焼室側開口に連通ずる曲線状部
とによって構成し、吸入混合気を燃焼室に対して接線方
向に流入させるようにしてなるエンジンの吸気装置にお
いて、上記曲線状部において吸気ポート上面より直線状
部底面の延長面に至る範囲で垂下し、かつ上記燃焼室側
開口の周縁に接すると共に直線状部の側面に平行な面と
、曲がり方向側の直線状部側面の延長面との間の範囲内
に曲がり方向とほぼ同方向に延びる案内翼を設けたこと
を特徴とするエンジンの吸気装置。
The combustion chamber side opening of the intake port provided in the cylinder head and the cylinder head side wall side opening are offset in the horizontal direction, and the intake port is formed into a linear portion extending from the cylinder head side wall side opening at a substantially right angle to the cylinder head IP&. and a curved part that is continuous with this straight part, curves from the straight part in the tangential direction of the cylinder, and communicates with the combustion chamber side opening, so that the intake air-fuel mixture flows tangentially into the combustion chamber. In the intake system for an engine, the curved portion hangs down from the upper surface of the intake port to the extension surface of the bottom surface of the straight portion, and is in contact with the periphery of the opening on the combustion chamber side, as well as the side surface of the straight portion. An intake system for an engine, characterized in that a guide vane is provided within a range between a plane parallel to the curve and an extension plane of a side surface of the straight portion on the bending direction side, and extending in substantially the same direction as the bending direction.
JP1977004348U 1977-01-17 1977-01-17 engine intake system Expired JPS588901Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1977004348U JPS588901Y2 (en) 1977-01-17 1977-01-17 engine intake system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1977004348U JPS588901Y2 (en) 1977-01-17 1977-01-17 engine intake system

Publications (2)

Publication Number Publication Date
JPS5399410U JPS5399410U (en) 1978-08-11
JPS588901Y2 true JPS588901Y2 (en) 1983-02-17

Family

ID=28691217

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1977004348U Expired JPS588901Y2 (en) 1977-01-17 1977-01-17 engine intake system

Country Status (1)

Country Link
JP (1) JPS588901Y2 (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4986709A (en) * 1972-09-15 1974-08-20

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4986709A (en) * 1972-09-15 1974-08-20

Also Published As

Publication number Publication date
JPS5399410U (en) 1978-08-11

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