JPH0643458Y2 - Engine intake system - Google Patents

Engine intake system

Info

Publication number
JPH0643458Y2
JPH0643458Y2 JP1986042628U JP4262886U JPH0643458Y2 JP H0643458 Y2 JPH0643458 Y2 JP H0643458Y2 JP 1986042628 U JP1986042628 U JP 1986042628U JP 4262886 U JP4262886 U JP 4262886U JP H0643458 Y2 JPH0643458 Y2 JP H0643458Y2
Authority
JP
Japan
Prior art keywords
intake
surge tank
intake passage
side wall
branch
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 - Lifetime
Application number
JP1986042628U
Other languages
Japanese (ja)
Other versions
JPS62154237U (en
Inventor
恒利 横倉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mazda Motor Corp
Original Assignee
Mazda Motor Corp
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 Mazda Motor Corp filed Critical Mazda Motor Corp
Priority to JP1986042628U priority Critical patent/JPH0643458Y2/en
Publication of JPS62154237U publication Critical patent/JPS62154237U/ja
Application granted granted Critical
Publication of JPH0643458Y2 publication Critical patent/JPH0643458Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【考案の詳細な説明】 (産業上の利用分野) 本考案はエンジンの吸気装置に関し、特に吸気慣性過給
を行なうようにしたものの改良に関する。
DETAILED DESCRIPTION OF THE INVENTION (Industrial field of application) The present invention relates to an intake device for an engine, and more particularly to an improvement of an intake air intake supercharger.

(従来の技術) 従来、この種のエンジンの吸気装置として、例えば特開
昭59-25071号公報に開示されるように、エンジンの各気
筒に吸気を供給する主吸気通路に所定の容積を有する容
積部であるサージタンクを設けると共に、該サージタン
クに各気筒と連通する分岐吸気通路を接続することによ
り、上記主吸気通路から供給された吸気を上記サージタ
ンクから各分岐吸気通路に均等に分配すると共に、分岐
吸気通路同士の吸気干渉を防止しつつ吸気の脈動を利用
した吸気慣性効果を得るようにしたものが知られてい
る。
(Prior Art) Conventionally, as an intake device for an engine of this type, as disclosed in, for example, Japanese Patent Laid-Open No. 59-25071, a main intake passage for supplying intake air to each cylinder of the engine has a predetermined volume. By providing a surge tank that is a capacity part and connecting a branch intake passage communicating with each cylinder to the surge tank, the intake air supplied from the main intake passage is evenly distributed from the surge tank to each branch intake passage. In addition, it is known that an intake inertia effect using the pulsation of intake air is obtained while preventing intake interference between the branch intake passages.

(考案が解決しようとする問題点) ところで、このようなエンジンの吸気装置においては、
サージタンクを簡単な正四角筒状に形成し、吸気流入側
側壁に主吸気通路を接続すると共に、吸気流出側側壁に
分岐吸気通路を接続することが行われる。
(Problems to be solved by the invention) By the way, in such an engine intake device,
The surge tank is formed in a simple square tube shape, and the main intake passage is connected to the intake inflow side wall and the branch intake passage is connected to the intake outflow side wall.

しかしながら、この場合、主吸気通路がサージタンクに
おける主吸気通路と対向する側壁と略垂直に位置するた
め、主吸気通路からの吸気の流れがこの対向する側壁に
正面から当たるので、サージタンク内において吸気の流
れが乱され、吸気抵抗が増大して充填効率が低いものと
なるという問題がある。
However, in this case, since the main intake passage is positioned substantially perpendicular to the side wall of the surge tank facing the main intake passage, the flow of intake air from the main intake passage strikes the facing side wall from the front, so that in the surge tank. There is a problem that the flow of intake air is disturbed, intake resistance increases, and charging efficiency becomes low.

上記に鑑み、本考案は吸気の流れをスムーズにして、吸
気慣性効果を良好にすることを目的とする。
In view of the above, it is an object of the present invention to smooth the flow of intake air and improve the effect of intake inertia.

(問題点を解決するための手段) 上記の目的を達成するため、本考案は、サージタンクの
形状、サージタンクと分岐吸気通路との接続部の形状及
び分岐吸気通路の形状を特定するものであって、具体的
には、吸気を導入する主吸気通路と、各気筒に吸気を供
給する気筒毎の分岐吸気通路と、上記主吸気通路と分岐
吸気通路との間に設けられた気筒列方向へ延びる角筒状
のサージタンクとを備えたエンジンの吸気装置を前提と
し、上記サージタンクは、互いに対向する吸気流入側側
壁及び吸気流出側側壁と、互いに平行状態で対向し且つ
相対的長さが異なる長辺側側壁及び短辺側側壁とを有し
ており、上記主吸気通路は上記サージタンクの吸気流入
側側壁における気筒列方向の中央部に接続されており、
上記主吸気通路から上記サージタンク内に流入した吸気
が上記長辺側側壁に斜め方向から当たるように上記主吸
気通路における上記サージタンク近傍部の軸線と上記サ
ージタンクの長辺側側壁とがなす角度は鈍角に設定され
ており、上記各分岐吸気通路は、U字状に湾曲し且つ気
筒列方向と直交する方向の開口幅を上流端側から下流端
側にかけて次第に小さくなる形状に形成されており、上
記各分岐吸気通路は上記サージタンクの吸気流出側側壁
に、各分岐吸気通路の上流端部同士の間隔が下流端部同
士の間隔より小もさくなるように接続されており、上記
各分岐吸気通路における上記サージタンクとの接続部
は、気筒列方向と直交する方向の開口幅が気筒列方向の
開口幅よりも大きくなると共に該接続部の外側の壁部が
上記サージタンクの長辺側側壁と連続し且つ該接続部の
内側の壁部が上記サージタンクの短辺側側壁と連続する
形状に形成されている構成とするものである。
(Means for Solving the Problems) In order to achieve the above object, the present invention specifies the shape of the surge tank, the shape of the connection between the surge tank and the branch intake passage, and the shape of the branch intake passage. Specifically, specifically, a main intake passage that introduces intake air, a branch intake passage for each cylinder that supplies intake air to each cylinder, and a cylinder row direction provided between the main intake passage and the branch intake passage. Assuming an engine intake device including a rectangular tubular surge tank extending to a side wall, the surge tank has an intake inflow side wall and an intake outflow side wall facing each other in parallel with each other and having a relative length. Have different long side walls and short side walls, and the main intake passage is connected to a central portion in the cylinder row direction on the intake inflow side wall of the surge tank,
The axial line of the main intake passage near the surge tank and the long side wall of the surge tank are formed so that the intake air flowing into the surge tank from the main intake passage strikes the long side wall obliquely. The angle is set to an obtuse angle, and each of the branch intake passages is formed in a shape that is curved in a U shape and has an opening width in the direction orthogonal to the cylinder row direction that gradually decreases from the upstream end side to the downstream end side. The branch intake passages are connected to the side wall of the surge tank on the intake / outflow side so that the intervals between the upstream ends of the branch intake passages are smaller than the intervals between the downstream ends. The connection portion of the branch intake passage with the surge tank has an opening width in the direction orthogonal to the cylinder row direction larger than the opening width in the cylinder row direction, and a wall portion outside the connection portion is the surge tank. Inner wall of the side sidewalls and continuous to and the connection portion is to a configuration that is formed in a shape continuous with the short side walls of the surge tank.

(作用) 上記の構成により、主吸気通路はサージタンクの吸気流
入側側壁における気筒列方向の中央部に接続されている
と共に、主吸気通路におけるサージタンク近傍部の軸線
とサージタンクの長辺側側壁とがなす角度が鈍角に設定
されているため、主吸気通路からサージタンク内に流入
した吸気はサージタンクの長手方向の両側に拡がると共
に長辺側側壁に斜め方向から当たるので、主吸気通路か
らサージタンク内に流入する吸気の流れはスムーズにな
る。
(Operation) With the above configuration, the main intake passage is connected to the center of the side wall of the surge tank in the cylinder column direction on the intake inflow side wall, and the main intake passage has an axis near the surge tank and the long side of the surge tank. Since the angle formed by the side wall is set to an obtuse angle, the intake air that has flowed into the surge tank from the main intake passage spreads to both sides of the surge tank in the longitudinal direction and strikes the long side wall obliquely. The flow of intake air flowing into the surge tank from becomes smooth.

各分岐吸気通路は、気筒列方向と直交する方向の開口幅
が上流端側から下流端側にかけて次第に小さくなる形状
に形成されているため、サージタンクから各分岐吸気通
路へ流れる吸気の流れがスムーズになると共に、各分岐
吸気通路からサージタンクに伝わる圧力波が減衰され難
い。
Since each branch intake passage is formed in a shape in which the opening width in the direction orthogonal to the cylinder row direction gradually decreases from the upstream end side to the downstream end side, the flow of intake air from the surge tank to each branch intake passage is smooth. In addition, the pressure wave transmitted from each branch intake passage to the surge tank is not easily attenuated.

各分岐吸気通路はサージタンクの吸気流出側側壁に、各
分岐吸気通路の上流端部同士の間隔が下流端部同士の間
隔よりも小さくなるように接続されているため、主吸気
通路はサージタンクの吸気流入側側壁の中央部に接続さ
れていると言う構成と相俟って主吸気通路からサージタ
ンクを通って各分岐吸気通路へ流れる吸気の流れがスム
ーズになると共に、各分岐吸気通路の上流開口部が互い
に接近しているので一つの分岐吸気通路からサージタン
クに伝わった圧力波は他の分岐吸気通路にスムーズに伝
わる。
Each branch intake passage is connected to the intake / outflow side wall of the surge tank so that the distance between the upstream ends of each branch intake passage is smaller than the distance between the downstream ends, so the main intake passage is a surge tank. In combination with the configuration that it is connected to the central part of the side wall of the intake inflow side, the flow of intake air flowing from the main intake passage to each branch intake passage through the surge tank becomes smooth, and Since the upstream openings are close to each other, the pressure wave transmitted from one branch intake passage to the surge tank is smoothly transmitted to the other branch intake passage.

各分岐吸気通路におけるサージタンクとの接続部は、気
筒列方向と直交する方向の開口幅が気筒列方向の開口幅
よりも大きくなり、外側の壁部がサージタンクの長辺側
側壁と連続し且つ内側の壁部がサージタンクの短辺側側
壁と連続する形状であるため、サージタンクから各分岐
吸気通路へ吸気がスムーズに流れるので吸気抵抗が低減
すると共に、一つの分岐吸気通路からサージタンクへの
圧力波の伝播及びサージタンクから他の分岐吸気通路へ
の圧力波の伝播が共にスムーズになる。
In the connection portion of each branch intake passage with the surge tank, the opening width in the direction orthogonal to the cylinder row direction is larger than the opening width in the cylinder row direction, and the outer wall portion is continuous with the long side wall of the surge tank. In addition, since the inner wall portion has a shape that is continuous with the short side wall of the surge tank, intake air smoothly flows from the surge tank to each branch intake passage, thereby reducing intake resistance and also from one branch intake passage to the surge tank. Of the pressure wave to and from the surge tank to the other branch intake passage is smooth.

(実施例) 以下、本考案の実施例を図面に基づいて説明する。Embodiment An embodiment of the present invention will be described below with reference to the drawings.

第1図ないし第3図は本考案の実施例に係るエンジンの
吸気装置を示し、第1図はその正面図、第2図は平面
図、第3図は側面図である。同図において、1は直列4
気筒のエンジンであって、該エンジン1にはその長手方
向に4つの第1〜第4気筒2a〜2dが配置されている。上
記エンジン1の上方には、上記各気筒2a〜2dに吸気を供
給する主吸気通路3が、気筒列と直交する方向に延びる
ように設けられている。また、エンジン1の斜め上側方
には、上記主吸気通路3に設けられ、該主吸気通路3の
吸気を導入するサージタンクとしての容積部4が配置さ
れている。さらに、該容積部4は各気筒ごとの縦長の断
面略楕円形の分岐吸気通路5によって上記各気筒2a〜2d
に接続されており、上記主吸気通路3に吸入された吸気
を、上記容積部4に貯溜させてその動圧を緩和してから
各分岐吸気通路5に均等に分配すると共に、吸気の脈動
を利用して各分岐吸気通路5の等価管長に応じた吸気慣
性効果を得てエンジンの過給を行なうようになされてい
る。
1 to 3 show an intake system for an engine according to an embodiment of the present invention. FIG. 1 is a front view thereof, FIG. 2 is a plan view, and FIG. 3 is a side view. In the figure, 1 is a series 4
This is a cylinder engine, and four first to fourth cylinders 2a to 2d are arranged in the engine 1 in the longitudinal direction thereof. A main intake passage 3 for supplying intake air to each of the cylinders 2a to 2d is provided above the engine 1 so as to extend in a direction orthogonal to the cylinder row. Further, on the diagonally upper side of the engine 1, there is disposed a volume portion 4 provided in the main intake passage 3 and serving as a surge tank for introducing intake air of the main intake passage 3. Further, the volume portion 4 is provided with a vertically long, substantially elliptical branch intake passage 5 for each cylinder, thereby forming the cylinders 2a to 2d.
The intake air sucked into the main intake passage 3 is stored in the volume portion 4 to relieve its dynamic pressure and then evenly distributed to the respective branch intake passages 5. The engine is supercharged by utilizing the intake inertia effect according to the equivalent pipe length of each branch intake passage 5.

また、上記容積部4は、角筒状に形成され且つ気筒列と
平行に配置され、側壁のうち主吸気通路3が接続された
流入側側壁としての縦壁6は第1図から判るように略垂
直に設けられており、主吸気通路3は縦壁6における気
筒列方向の中央部に接続されている。そして、上記主吸
気通路3と対向する長辺側側壁としての外壁壁7aは、容
積部4への吸気流入方向つまり主吸気通路3の方向に対
して斜め下方に傾斜して形成されていると共に、上記各
分岐吸気通路5は、外側壁7aと該外側壁7aに平行で吸気
取入口3a下方に形成された短辺側側壁としての内側壁7b
に沿って該両側壁7a,7bと同一方向に連続して接続され
ており、第1図に示すように、上記容積部4への吸気流
入方向と上記容積部4から各気筒2a〜2dへの吸気流出方
向との成す角度θが鈍角に形成されている。
Further, the volume portion 4 is formed in a rectangular tube shape and arranged in parallel with the cylinder row, and the vertical wall 6 as an inflow side wall to which the main intake passage 3 is connected is seen from FIG. It is provided substantially vertically, and the main intake passage 3 is connected to the central portion of the vertical wall 6 in the cylinder row direction. The outer wall 7a as a long side wall facing the main intake passage 3 is formed obliquely downward with respect to the intake air inflow direction into the volume 4, that is, the direction of the main intake passage 3. Each of the branch intake passages 5 has an outer wall 7a and an inner wall 7b as a short side wall formed in parallel with the outer wall 7a and below the intake intake 3a.
Are connected continuously in the same direction as the both side walls 7a, 7b along with, as shown in FIG. 1, the intake air inflow direction to the volume section 4 and the cylinders 2a to 2d from the volume section 4 The angle θ formed between the intake air flow direction and the intake air flow direction is formed as an obtuse angle.

第1図に示すように、各分岐吸気通路5は、容積部4か
らエンジン1にかけてU字状に湾曲する形状に形成され
ていると共に、気筒列方向と直交する方向の開口幅が上
流端側から下流端側にかけて次第に小さくなる形状に形
成されている。また、各分岐吸気通路5における容積部
5との接続部は、気筒列方向と直交する方向の開口幅が
気筒列方向の開口幅よりも大きくなると共に、各分岐吸
気通路5の外側の壁部が容積部4の外側壁7aと連続し且
つ各分岐吸気通路5の内側の壁部が容積部4の内側壁7b
と連続する形状に形成されている。
As shown in FIG. 1, each branch intake passage 5 is formed in a U-shaped curve from the volume portion 4 to the engine 1, and has an opening width in the direction orthogonal to the cylinder row direction on the upstream end side. To the downstream end side, the shape is gradually reduced. Further, in the connection portion of each branch intake passage 5 with the volume portion 5, the opening width in the direction orthogonal to the cylinder row direction becomes larger than the opening width in the cylinder row direction, and the wall portion outside the branch intake passage 5 is formed. Is continuous with the outer wall 7a of the volume 4 and the inner wall of each branch intake passage 5 is the inner wall 7b of the volume 4.
Is formed in a continuous shape.

さらに、第2図に示すように、各分岐吸気通路5は、容
積部5の内側壁7bに各分岐吸気通路5の上流端部同士の
間隔が下流端部同士の間隔よりも小さくなるように接続
されている。
Further, as shown in FIG. 2, in each branch intake passage 5, the distance between the upstream end portions of each branch intake passage 5 is smaller than the distance between the downstream end portions on the inner wall 7b of the volume portion 5. It is connected.

したがって、上記実施例においては、容積室5で主吸気
通路3に吸入された吸気の動圧が緩和されるので、吸気
を各分岐吸気通路5に均等に分配することができる。
Therefore, in the above embodiment, the dynamic pressure of the intake air sucked into the main intake passage 3 in the volume chamber 5 is relieved, so that the intake air can be evenly distributed to the respective branch intake passages 5.

また、主吸気通路3から容積部4への吸気流入方向と容
積部4から各分岐吸気通路5への吸気流出方向とが鈍角
を成すので、吸気の流れがスムーズになり、吸気抵抗が
少なくなって充填効率が高いものになる。しかも、上記
容積部4による各分岐吸気通路5は容積部4の幅と略一
致する長軸を有する長円断面に形成されるため、各分岐
吸気通路5を密着・隣接して配置することができ、容積
部の気筒配列方向の長さを短縮することが可能となり、
一層均等分配効果を高めることができる。
Further, since the intake air inflow direction from the main intake passage 3 to the volume portion 4 and the intake air outflow direction from the volume portion 4 to each branch intake passage 5 form an obtuse angle, the flow of intake air becomes smooth and the intake resistance decreases. The filling efficiency is high. Moreover, since each branch intake passage 5 formed by the volume portion 4 is formed in an oval cross section having a major axis that substantially matches the width of the volume portion 4, the branch intake passages 5 can be arranged in close contact with each other. It is possible to shorten the length of the volume part in the cylinder arrangement direction,
The even distribution effect can be further enhanced.

さらに、容積部4の縦壁6から内側壁にかけて外側にリ
ブを設けたことによりその剛性が高められる。
Further, by providing ribs on the outer side from the vertical wall 6 of the volume part 4 to the inner side wall, the rigidity thereof is enhanced.

(考案の効果) 以上説明したように、本考案のエンジンの吸気装置によ
ると、主吸気通路はサージタンクの吸気流入側側壁にお
ける気筒列方向の中央部に接続されていると共に、主吸
気通路におけるサージタンク近傍部の軸線とサージタン
クの長辺側側壁とがなす角度が鈍角に設定されているた
め、主吸気通路からサージタンク内に流入する吸気の流
れはスムーズになり、吸気抵抗が小さくなる。
(Effect of the Invention) As described above, according to the engine intake system of the present invention, the main intake passage is connected to the central portion of the surge tank on the intake inflow side wall in the cylinder column direction, and The angle between the axis near the surge tank and the long side wall of the surge tank is set to an obtuse angle, so the flow of intake air flowing from the main intake passage into the surge tank becomes smooth, and the intake resistance decreases. .

また、各分岐吸気通路は、気筒列方向と直交する方向の
開口幅が上流端側から下流端側にかけて次第に小さくな
る形状に形成されているため、サージタンクから各分岐
吸気通路へ流れる吸気の吸気抵抗が小さくなると共に、
各分岐吸気通路からサージタンクに伝わる圧力波が減衰
され難いので吸気の脈動効果が向上する。
Further, since each branch intake passage is formed in such a shape that the opening width in the direction orthogonal to the cylinder row direction becomes gradually smaller from the upstream end side to the downstream end side, intake air from the surge tank to each branch intake passage is intaken. As the resistance decreases,
Since the pressure wave transmitted from each branch intake passage to the surge tank is not easily attenuated, the pulsation effect of intake air is improved.

また、各分岐吸気通路はサージタンクの吸気流出側側壁
に、各分岐吸気通路の上流端部同士の間隔が下流端部同
士の間隔よりも小さくなるように接続されているため、
サージタンクから各分岐吸気通路への吸気の流れがスム
ーズになると共に、一の分岐吸気通路からサージタンク
に伝わった圧力波が他の分岐吸気通路にスムーズに伝わ
り、サージタンクで反転した圧力波は他の分岐吸気通路
にスムーズに伝播されるので吸気の脈動効果は向上す
る。
Further, each branch intake passage is connected to the intake-outlet side wall of the surge tank so that the interval between the upstream end portions of each branch intake passage is smaller than the interval between the downstream end portions,
The flow of intake air from the surge tank to each branch intake passage becomes smooth, and the pressure wave transmitted from one branch intake passage to the surge tank is smoothly transmitted to the other branch intake passage. Since it is smoothly propagated to other branch intake passages, the pulsation effect of intake air is improved.

また、各分岐吸気通路におけるサージタンクとの接続部
は、気筒列方向と直交する方向の開口幅が吸気列方向の
開口幅よりも大きくなり、その外側の壁部がサージタン
クの長辺側側壁と連続し且つその内側の壁部がサージタ
ンクの短辺側側壁と連続する形状であるため、サージタ
ンクから各分岐吸気通路へ流れる吸気の吸気抵抗が低減
すると共に、圧力波の一の分岐吸気通路からサージタン
クを介して他の分岐吸気通路への伝播がスムーズになる
ので吸気の脈動効果は向上する。
Further, in the connection portion of each branch intake passage with the surge tank, the opening width in the direction orthogonal to the cylinder row direction becomes larger than the opening width in the intake row direction, and the outer wall portion is the long side wall of the surge tank. Since the inner wall portion is continuous with the short side wall of the surge tank, the intake resistance of the intake air flowing from the surge tank to each branch intake passage is reduced, and at the same time, one branch of the pressure wave Since the propagation from the passage to the other branch intake passage via the surge tank becomes smooth, the pulsation effect of intake air is improved.

このため、本考案によると、主吸気通路からサージタン
クを通って各分岐吸気通路へ流れる吸気の吸気抵抗が低
減すると共に、一の分岐吸気通路からサージタンクを介
して他の分岐吸気通路に伝播される圧力波の減衰が低減
するので、吸気の動的効果が著しく向上し、エンジン性
能が大きく向上する。
Therefore, according to the present invention, the intake resistance of the intake air flowing from the main intake passage through the surge tank to each branch intake passage is reduced, and at the same time, it is propagated from one branch intake passage to the other branch intake passage through the surge tank. Since the attenuation of the pressure wave generated is reduced, the dynamic effect of intake air is significantly improved and engine performance is greatly improved.

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

図面は本考案の実施例に係るエンジンの吸気装置を示
し、第1図は正面図、第2図は平面図、第3図は側面図
である。 1……エンジン、2a〜2d……気筒、3……主吸気通路、
4……容積部(サージタンク)5……分岐吸気通路、7a
……外側壁(長辺側側壁)、7b……内側壁(短辺側側
壁)。
The drawings show an intake system for an engine according to an embodiment of the present invention. FIG. 1 is a front view, FIG. 2 is a plan view, and FIG. 3 is a side view. 1 ... Engine, 2a-2d ... Cylinder, 3 ... Main intake passage,
4 ... Volume (surge tank) 5 ... Branch intake passage, 7a
…… Outside wall (long side wall), 7b …… Inner wall (short side wall).

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】吸気を導入する主吸気通路と、各気筒に吸
気を供給する気筒毎の分岐吸気通路と、上記主吸気通路
と分岐吸気通路との間に設けられた気筒列方向へ延びる
角筒状のサージタンクとを備えたエンジンの吸気装置で
あって、 上記サージタンクは、互いに対向する吸気流入側側壁及
び吸気流出側側壁と、互いに平行状態で対向し且つ相対
的長さが異なる長辺側側壁及び短辺側側壁とを有し、 上記主吸気通路は上記サージタンクの吸気流入側側壁に
おける気筒列方向の中央部に接続され、 上記主吸気通路から上記サージタンク内に流入した吸気
が上記長辺側側壁に斜め方向から当たるよう上記主吸気
通路における上記サージタンク近傍部の軸線と上記サー
ジタンクの長辺側側壁とがなす角度は鈍角に設定され、 上記各分岐吸気通路は、U字状に湾曲し且つ気筒列方向
と直交する方向の開口幅が上流端側から下流端側にかけ
て次第に小さくなる形状に形成され、 上記各分岐吸気通路は上記サージタンクの吸気流出側側
壁に、各分岐吸気通路の上流端部同士の間隔が下流端部
同士の間隔よりも小さくなるように接続され、 上記各分岐吸気通路における上記サージタンクとの接続
部は、気筒列方向と直交する方向の開口幅が気筒列方向
の開口幅よりも大きくなると共に該接続部の外側の壁部
が上記サージタンクの長辺側側壁と連続し且つ該接続部
の内側の壁部が上記サージタンクの短辺側側壁と連続す
る形状に形成されていることを特徴とするエンジンの吸
気装置。
1. A main intake passage for introducing intake air, a branch intake passage for each cylinder that supplies intake air to each cylinder, and an angle extending in the cylinder row direction provided between the main intake passage and the branch intake passage. An intake system for an engine, comprising: a cylindrical surge tank, wherein the surge tank has a pair of intake inflow side walls and an intake outflow side wall facing each other in parallel with each other and having different relative lengths. A side wall and a short side wall, and the main intake passage is connected to a center portion of the intake tank inflow side wall of the surge tank in the cylinder column direction, and the intake air flowing into the surge tank from the main intake passage. The angle formed by the axis of the surge tank vicinity portion in the main intake passage and the long side wall of the surge tank is set to an obtuse angle so that it hits the long side wall obliquely. The branch intake passage is formed in a U-shape and has an opening width in the direction orthogonal to the cylinder row direction that gradually decreases from the upstream end side to the downstream end side. The branch intake passages are connected such that the distance between the upstream ends thereof is smaller than the distance between the downstream ends thereof, and the connection portion of each of the branch intake passages with the surge tank is in a direction orthogonal to the cylinder row direction. The opening width is larger than the opening width in the cylinder row direction, the outer wall portion of the connection portion is continuous with the long side wall of the surge tank, and the inner wall portion of the connection portion is the short side of the surge tank. An intake device for an engine, which is formed in a shape that is continuous with a side wall.
JP1986042628U 1986-03-24 1986-03-24 Engine intake system Expired - Lifetime JPH0643458Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1986042628U JPH0643458Y2 (en) 1986-03-24 1986-03-24 Engine intake system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1986042628U JPH0643458Y2 (en) 1986-03-24 1986-03-24 Engine intake system

Publications (2)

Publication Number Publication Date
JPS62154237U JPS62154237U (en) 1987-09-30
JPH0643458Y2 true JPH0643458Y2 (en) 1994-11-14

Family

ID=30858718

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1986042628U Expired - Lifetime JPH0643458Y2 (en) 1986-03-24 1986-03-24 Engine intake system

Country Status (1)

Country Link
JP (1) JPH0643458Y2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6139431U (en) * 1984-08-16 1986-03-12 トヨタ自動車株式会社 Intake system structure of internal combustion engine

Also Published As

Publication number Publication date
JPS62154237U (en) 1987-09-30

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