JPH04116258A - Intake structure for engine - Google Patents

Intake structure for engine

Info

Publication number
JPH04116258A
JPH04116258A JP2237871A JP23787190A JPH04116258A JP H04116258 A JPH04116258 A JP H04116258A JP 2237871 A JP2237871 A JP 2237871A JP 23787190 A JP23787190 A JP 23787190A JP H04116258 A JPH04116258 A JP H04116258A
Authority
JP
Japan
Prior art keywords
cylinder
independent intake
intake
independent
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.)
Granted
Application number
JP2237871A
Other languages
Japanese (ja)
Other versions
JP2828333B2 (en
Inventor
Nobumasa Takasaki
高崎 信昌
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 JP23787190A priority Critical patent/JP2828333B2/en
Publication of JPH04116258A publication Critical patent/JPH04116258A/en
Application granted granted Critical
Publication of JP2828333B2 publication Critical patent/JP2828333B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

PURPOSE:To compactly arrange independent intake passages with their data such as the passage lengths unified for individual cylinders by forming them so that the radius of curvature of the curve section for the independent intake passage of a cylinder near to the connection face of a collection section is made larger than that for the independent intake passage of a cylinder apart from the connection face. CONSTITUTION:Independent intake passages 5a-5d communicated to individual cylinders respectively are extended to one side in the cylinder train direction above an engine 1 and curved and collected on the connection face 11 of an intake collection section 6. The independent intake passage of a cylinder near to the connection face 11 of the intake collection section 6 is shorter than the independent intake passage of a cylinder apart from the connection face 11 of the intake collection section 6, i.e., in the order of the independent intake passages 5d, 5c, 5b, 5a, e.g. the independent intake passage 5b is shorter than the independent intake passage 5, thus the radius of curvature of the second curve section 22 is made larger than that of the first curve section 21 to extend the passage length, and the independent intake passages 5a-5d are connected to the connection face 11 of the intake collection section 6 respectively.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、エンジンの吸気構造に関し、特に、動的効果
(吸気慣性効果)を利用して吸気を過給するようにした
ものに関する。
DETAILED DESCRIPTION OF THE INVENTION (Industrial Application Field) The present invention relates to an intake structure for an engine, and particularly to one in which intake air is supercharged by utilizing a dynamic effect (intake inertia effect).

(従来の技術) 近来、エンジンの出力トルクを向上させるために、エン
ジンの気筒に供給される吸気を吸気慣性効果などの動的
効果を利用して過給することによリ、吸気の充填効率を
高めるようにすることが行われている。
(Prior art) In recent years, in order to improve the output torque of an engine, the filling efficiency of the intake air has been improved by supercharging the intake air supplied to the engine cylinders using dynamic effects such as the intake inertia effect. Efforts are being made to increase the

すなわち、吸気慣性効果による過給では、エンジンの所
定の回転域(同調回転域)において、各気筒の吸気行程
初期で吸気弁の開弁に伴って吸気ポートに吸気の負圧波
か発生したとき、この吸気負圧波を該吸気ポートに接続
された独立吸気通路内で上流側に向かって音速で伝播さ
せ、この負圧波を所定の容積部(ボリューム室)で正圧
波に反転させる。さらに、この正圧波を同一の経路で下
流側に音速で伝播させて吸気弁が閉弁する直前の吸気行
程終期に同じ気筒の吸気ポートに到達させ、この正圧波
により吸気を燃焼室に押し込んでその充填効率を高める
ようになっている。
In other words, in supercharging based on the intake inertia effect, when a negative pressure wave of intake air is generated at the intake port as the intake valve opens at the beginning of the intake stroke of each cylinder in a predetermined engine rotation range (tuned rotation range), This intake negative pressure wave is propagated at the speed of sound toward the upstream side within an independent intake passage connected to the intake port, and this negative pressure wave is reversed into a positive pressure wave in a predetermined volume portion (volume chamber). Furthermore, this positive pressure wave is propagated downstream along the same path at the speed of sound, reaching the intake port of the same cylinder at the end of the intake stroke just before the intake valve closes, and this positive pressure wave pushes the intake air into the combustion chamber. The filling efficiency is increased.

そして、吸気の圧力波を反転させる集合部としては、一
般にサージタンクが利用されているか、このサージタン
クでは、その内部における上流側通路から各独立吸気通
路までの長さか各気筒て異なるので、各気筒に対する吸
気の分配性や吸気慣性効果が均一にならない等の問題が
ある。
Generally, a surge tank is used as a gathering part to reverse the intake pressure waves.In this surge tank, the length from the upstream passage to each independent intake passage is different for each cylinder. There are problems such as uneven distribution of intake air to the cylinders and uneven intake inertia effect.

二のため、従来、実開昭60−88062号公報には、
エンジンの一側面側より各気筒にそれぞれ連通する独立
吸気通路の上流端集合部を略円錐台状の空間とし、その
小径側端に主吸気通路の下流端を、一方、大径側端に複
数の独立吸気通路をそれぞれ接続し、独立吸気通路の上
流端開口を主吸気通路の下IN端開口の軸心を通る軸線
に対し線対象に配置することが提案されている。このも
のによると、エンジンの気筒列方向の中央に位置してい
る集合部における主吸気通路の下流端開口から各独立吸
気通路の上流端開口までの距離か独立吸気通路について
略等しくなり、各気筒の吸気の配分性が均一化されると
ともに、主吸気通路から各気筒に至る吸気流動系路の急
激な屈曲がなくなって吸気抵抗が低減され、さらに、各
独立吸気通路上流端開口の近接配置により、各独立吸気
通路か他の独立吸気通路での吸気慣性効果の容積室とし
て利用されて、集合部自体の大きさをコンパクトにする
ことができる。
Therefore, conventionally, Utility Model Application Publication No. 60-88062 has
The upstream ends of the independent intake passages that communicate with each cylinder from one side of the engine are formed into a substantially truncated conical space, with the downstream end of the main intake passage at the small diameter end of the space, and the plurality of independent intake passages at the large diameter end. It has been proposed to connect the independent intake passages, respectively, and arrange the upstream end openings of the independent intake passages symmetrically with respect to an axis passing through the axis of the lower IN end opening of the main intake passage. According to this, the distance from the downstream end opening of the main intake passage to the upstream end opening of each independent intake passage in the gathering part located in the center of the cylinder row direction of the engine is approximately equal for each independent intake passage, and each cylinder The distribution of intake air is uniform, and the intake flow path from the main intake passage to each cylinder is no longer sharply curved, reducing intake resistance.Furthermore, the upstream end openings of each independent intake passage are arranged close to each other. , each independent intake passage or another independent intake passage can be used as a volume chamber for the intake inertia effect, so that the size of the gathering part itself can be made compact.

(発明が解決しようとする課題) ところで、直列型エンジンにおいて、独立吸気通路を気
筒列方向の中央で集合させると、その幅方向にスペース
を要して、エンジンの横方向の幅が増大することになる
(Problem to be Solved by the Invention) By the way, in an in-line engine, if the independent intake passages are gathered at the center in the direction of the cylinder rows, space is required in the width direction and the width of the engine in the lateral direction increases. become.

そこで、こうした問題を回避するには、各独立吸気通路
を彎曲させたのちその上流端をエンジンの上方で且つ気
筒列方向の一方側に延ばして、エンジンの気筒列方向に
対して略直交する集合部の接続面に接続する構造とすれ
ばよい。
Therefore, in order to avoid this problem, each independent intake passage is curved, and then its upstream end is extended above the engine and to one side in the direction of the cylinder row, so that a set of air passages that are approximately perpendicular to the direction of the cylinder row of the engine are formed. The structure may be such that it connects to the connection surface of the section.

しかしながら、全ての独立吸気通路がエンジンの上方で
且っ気筒列方向の一方側に延びた構造であると、独立吸
気通路自体の通路長さが各気筒毎で異なり、独立吸気通
路間での吸気の分配性や吸気慣性効果に差が生じる。
However, if all the independent intake passages are above the engine and extend to one side in the cylinder row direction, the passage length of the independent intake passages themselves will be different for each cylinder, and the intake air between the independent intake passages will be different. Differences occur in the distribution performance and intake inertia effect.

また、各独立吸気通路のうち、集合部の接続面に対して
近くに位置する気筒の独立吸気通路は、集合部の接続面
に対して遠くに位置する気筒の独立吸気通路に対してそ
の通路自体に急激な彎曲が要求されて吸気抵抗が増大し
、各気筒間における充填効率にばらつきが生じる。
Also, among the independent intake passages, the independent intake passage of the cylinder located near the connection surface of the gathering section is the same as the independent intake passage of the cylinder located far from the connection surface of the gathering section. The cylinder itself is required to make a sharp curvature, which increases intake resistance and causes variations in charging efficiency between cylinders.

本発明は斯かる諸点に鑑みてなされたものであり、その
目的は、各独立吸気通路の彎曲部の曲率半径を適宜設定
することにより、独立吸気通路を各気筒毎でその通路長
さ等の諸元を均一にしつつコンパクトに配置し、且つ通
路自体の急激な彎曲を無くして吸気抵抗を低減させ各気
筒間における充填効率のばらつきを解消することにある
The present invention has been made in view of these points, and its purpose is to adjust the length of the independent intake passage for each cylinder by appropriately setting the radius of curvature of the curved portion of each independent intake passage. The objective is to arrange the cylinder compactly with uniform specifications, eliminate sharp curvatures in the passage itself, reduce intake resistance, and eliminate variations in filling efficiency between cylinders.

また、上記の集合部の接続面に対する各独立吸気通路の
接続位置を特定することで、各独立吸気通路の取り回し
性を向上させることも目的とする。
Another object of the present invention is to improve the maneuverability of each independent intake passage by specifying the connection position of each independent intake passage with respect to the connection surface of the above-mentioned gathering portion.

(課題を解決するための手段) 上記目的を達成するため、請求項(1)に係る発明か講
じた解決手段は、複数の気筒を有するエンジンにその一
側面側より各気筒にそれぞれ連通する独立吸気通路が設
けられ、該各独立吸気通路は彎曲したのちその上流端が
一箇所に集合されるようにしたエンジンの吸気構造を前
提とする。そして、上記各独立吸気通路を、その上流端
の集合部に対してエンジンの気筒列方向と略直交する接
続面で接続するとともに、上記集合部をエンジンの上方
で且つ気筒列方向の一方側に位置させる。さらに、上記
各独立吸気通路のうち、上記集合部の接続面に対して近
くに位置する気筒の独立吸気通路を、集合部の接続面に
対して遠くに位置する気筒の独立吸気通路よりも彎曲部
の曲率半径が大きくなるように形成する構成としたもの
である。
(Means for Solving the Problem) In order to achieve the above object, the solving means taken by the invention according to claim (1) is to provide an engine having a plurality of cylinders with independent communication with each cylinder from one side of the engine. The present invention is based on an engine intake structure in which an intake passage is provided, and each of the independent intake passages is curved and then their upstream ends are gathered at one place. Each of the independent intake passages is connected to the gathering portion at the upstream end thereof through a connecting surface substantially orthogonal to the direction of the cylinder row of the engine, and the gathering portion is connected above the engine and on one side in the direction of the cylinder row. position. Furthermore, among the independent intake passages, the independent intake passage of the cylinder located closer to the connecting surface of the collecting part is curved more than the independent intake passage of the cylinder located farther from the connecting face of the collecting part. The structure is such that the radius of curvature of the portion is formed to be large.

また、請求項(2)に係る発明が講じた解決手段は、各
独立吸気通路のうち、集合部の接続面に対して近くに位
置する気筒の独立吸気通路を該集合部の接続面の上側に
接続する一方、集合部の接続面に対して遠くに位置する
気筒の独立吸気通路を該集合部の接続面の下側に接続す
る構成としたものである。
Furthermore, the solution taken by the invention according to claim (2) is to move the independent intake passages of the cylinders that are located close to the connection surface of the gathering section among the independent intake passages to the upper side of the connection surface of the gathering section. On the other hand, the independent intake passages of the cylinders located far from the connecting surface of the collecting section are connected to the lower side of the connecting surface of the collecting section.

さらに、請求項(3)に係る発明が講じた解決手段は、
気筒を3つ以上有し、各独立吸気通路のうち、両側方に
位置する気筒の独立吸気通路を集合部の接続面のエンジ
ン側に接続する一方、中央に位置する気筒の独立吸気通
路を集合部の接続面の反エンジン側に接続する構成とし
たものである。
Furthermore, the solution taken by the invention according to claim (3) is:
It has three or more cylinders, and among the independent intake passages, the independent intake passages of the cylinders located on both sides are connected to the engine side of the connection surface of the gathering part, while the independent intake passages of the cylinders located in the center are connected. The structure is such that it is connected to the side opposite to the engine on the connection surface of the section.

(作用) 上記の構成により、請求項(1)に係る発明では、各気
筒にそれぞれ連通ずる独立吸気通路は、エンジン上方で
且つ気筒列方向の一方側に向って延びるように彎曲して
互いに集合部に対して接続面で集合されて、エンジン横
方向への幅を増大させずにコンパクトに配置されている
。その場合、各独立吸気通路のうち、集合部の接続面に
対して近くに位置する気筒の独立吸気通路が、集合部の
接続面に対して遠くに位置する気筒の独立吸気通路に比
して短くなる分たけ彎曲部の曲率半径を大きくして通路
長を長くする糸路で集合部の接続面に接続されている一
方、集合部の接続面に対して遠くに位置する気筒の独立
吸気通路が、集合部の接続面に対して近くに位置する気
筒の独立吸気通路に比して長くなる分だけ彎曲部の曲率
半径を小さくして通路長を短くする糸路で集合部の接続
面に接続されている。このため、独立吸気通路自体の長
さか各気筒毎で等長となり、独立吸気通路間での吸気の
分配性が均一になるとともに、吸気慣性効果に差が生じ
ることはない。
(Function) With the above configuration, in the invention according to claim (1), the independent intake passages that communicate with each cylinder are curved and converge with each other so as to extend above the engine and toward one side in the cylinder row direction. The parts are gathered together at the connecting surface, and are arranged compactly without increasing the width in the lateral direction of the engine. In that case, among the independent intake passages, the independent intake passage of the cylinder located closer to the connecting surface of the gathering part is larger than the independent intake passage of the cylinder located far from the connecting surface of the collecting part. The passage length is increased by increasing the radius of curvature of the curved part as it becomes shorter.It is connected to the connecting surface of the gathering section by a thread path, while the independent intake passage of the cylinder is located far away from the connecting surface of the gathering section. However, the radius of curvature of the curved part is made smaller by the length of the independent intake passage of the cylinder located near the connecting surface of the collecting part, so that the passage length is shortened. It is connected. Therefore, the length of the independent intake passages themselves is the same for each cylinder, the distribution of intake air between the independent intake passages is uniform, and there is no difference in the intake inertia effect.

また、上記の如く集合部に対して近い気筒の独立吸気通
路が、彎曲部の曲率半径を大きくして通路長を長くする
糸路で集合部の接続面に接続されていることから、集合
部に対して近い気筒の独立吸気通路は、その通路自体の
急激な彎曲が緩和されて、吸気抵抗が減少する。
In addition, as mentioned above, the independent intake passages of the cylinders near the collecting part are connected to the connection surface of the collecting part by a thread that increases the radius of curvature of the curved part and lengthens the passage length. In the independent intake passages of the cylinders that are close to each other, the steep curvature of the passage itself is relaxed, and intake resistance is reduced.

また、請求項(2)に係る発明では、各独立吸気通路の
うち、集合部の接続面に対して遠い気筒の独立吸気通路
が、集合部の接続面に対して近い気筒の独立吸気通路の
曲率半径の大きな彎曲部を迂回するよう、その近い気筒
の独立吸気通路に比して気筒列方向に長くなる分だけ曲
率半径の小さな彎曲部でもって上方へ延びて集合部の接
続面の上側に接続されている一方、集合部の接続面に対
して近い気筒の独立吸気通路が、集合部の接続面に対し
て遠い気筒の独立吸気通路に邪魔されることなく該独立
吸気通路に比して気筒列方向に短くなる分だけ曲率半径
を大きくした彎曲部が遠い気筒の独立吸気通路の下方に
おいて安易に取り回されて集合部の接続面の下側に接続
されている。このため、集合部に対して遠い気筒の独立
吸気通路が集合部の接続面の下側に接続されるもののよ
うに集合部に対して近い気筒の独立吸気通路が、集合部
に対して遠い気筒の独立吸気通路を避けながら接続され
て通路長を不要に長くしたり、彎曲部の曲率半径を小さ
くしたすせずに容易に取り回されることになる。
Furthermore, in the invention according to claim (2), among the independent intake passages, the independent intake passage of the cylinder farthest from the connection surface of the gathering part is different from the independent intake passage of the cylinder that is closer to the connection surface of the gathering part. In order to bypass the curved part with a large radius of curvature, it extends upward with a curved part with a small radius of curvature by the length of the independent intake passage in the cylinder row direction compared to the independent intake passage of the nearby cylinder, and is placed above the connection surface of the gathering part. On the other hand, the independent intake passages of the cylinders that are close to the connecting surface of the collecting section are not obstructed by the independent intake passages of the cylinders that are far from the connecting surface of the collecting section, compared to the independent intake passages. A curved portion whose radius of curvature is increased by an amount corresponding to the shortening in the cylinder row direction is easily routed below the independent intake passage of a distant cylinder and connected to the lower side of the connection surface of the gathering portion. For this reason, the independent intake passage of a cylinder that is far from the gathering section is connected to the lower side of the connecting surface of the gathering section, and the independent intake passage of a cylinder that is close to the gathering section is connected to the cylinder that is far from the gathering section. This makes it easy to route the intake passages without making the passage length unnecessarily long or reducing the radius of curvature of the curved portion.

また、請求項(3)に係る発明では、3つ以上の気筒を
有し、その各気筒に連通ずる独立吸気通路のうち、気筒
列方向中央に位置する気筒の独立吸気通路が、レイアウ
ト的に厳しい各気筒(エンジン)と集合部との間におい
て両側方に位置する各独立吸気通路の彎曲部の邪魔にな
らないよう、気筒列方向と直交する面上で彎曲して、エ
ンジンから離れる集合部の接続面の反エンジン側に接続
されている一方、両側方に位置する各独立吸気通路が、
気筒の存在しない側方となる気筒列方向で余裕をもって
彎曲して、集合部の接続面のエンジン側に接続されてい
る。このため、コンパクト化を図る上で集合部が各気筒
に近接配置されていても各気筒の独立吸気通路は彎曲部
の曲率半径に制約を受けることなく彎曲されて容易に取
り回されることになる。
Further, in the invention according to claim (3), among the independent intake passages that have three or more cylinders and communicate with each cylinder, the independent intake passage of the cylinder located in the center in the cylinder row direction is In order to avoid disturbing the curved parts of the independent intake passages located on both sides between each cylinder (engine) and the collecting part, the collecting part is curved on a plane perpendicular to the direction of the cylinder row and moves away from the engine. While connected to the opposite side of the connection surface, the independent intake passages located on both sides are
It is curved with a margin in the direction of the cylinder row, which is the side where no cylinders are present, and is connected to the engine side of the connection surface of the gathering part. Therefore, in order to achieve compactness, even if the gathering part is placed close to each cylinder, the independent intake passage of each cylinder can be curved and easily routed without being constrained by the radius of curvature of the curved part. Become.

(実施例) 以下、本発明の実施例を図面に基づいて説明する。(Example) Embodiments of the present invention will be described below based on the drawings.

第1図ないし第3図は本発明を直列4気筒エンジンに適
用した第1実施例を示す。図において、1は第1〜第4
の4つの気筒2a〜2dを有する直列4気筒エンジンで
あって、これら第1〜第4気筒2a〜2dはそれぞれ等
間隔をあけて直列に形成されている。そして、これら気
筒2a〜2dは例えば、第1気筒2a→第3気筒2C→
第2気筒2b=第4気筒2dの順序で吸気行程か進行す
るようになっている。
1 to 3 show a first embodiment in which the present invention is applied to an in-line four-cylinder engine. In the figure, 1 is the first to fourth
This is an in-line four-cylinder engine having four cylinders 2a to 2d, and these first to fourth cylinders 2a to 2d are formed in series at equal intervals. These cylinders 2a to 2d are, for example, first cylinder 2a→third cylinder 2C→
The intake stroke progresses in the order of second cylinder 2b=fourth cylinder 2d.

4は上記各気筒2a〜2dに吸気を供給する吸気通路で
、この吸気通路4は、下流端か各気筒2a  2b、2
C,2dの吸気ポート3にそれぞれ接続された4つの独
立吸気通路5a、5b、5c5dと、該各独立吸気通路
5a、5b、5c、5dの上流端に接続された略円錐台
状の吸気集合部6(集合部)と、該吸気集合部6の上流
端に接続された主吸気通路7とを備えている。これらは
エンジン1の一側(第2図では右側)に配置され、その
上流端は図外のエアクリーナに接続されている。このエ
アクリーナよりも下流側の主吸気通路7には吸入空気量
を検出するエアフローメータ(図示せず)が配設されて
いる。また、上記各独立吸気通路5a、5b、5c、5
dは、アルミニウム製のパイプ材よりなり、その上流端
は互いに近接した状態で吸気集合部6に集合されて、主
吸気通路7に連通している。
Reference numeral 4 denotes an intake passage that supplies intake air to each of the cylinders 2a to 2d.
Four independent intake passages 5a, 5b, 5c5d connected to the intake ports 3 of C and 2d, respectively, and a substantially truncated conical intake assembly connected to the upstream end of each independent intake passage 5a, 5b, 5c, 5d. The main air intake passage 7 is connected to the upstream end of the air intake collecting portion 6. These are arranged on one side of the engine 1 (on the right side in FIG. 2), and their upstream ends are connected to an air cleaner (not shown). An air flow meter (not shown) for detecting the amount of intake air is provided in the main intake passage 7 on the downstream side of the air cleaner. In addition, each of the independent intake passages 5a, 5b, 5c, 5
The upstream ends of the pipes d are made of aluminum pipe material, and the upstream ends of the pipes are gathered in the intake collecting section 6 in close proximity to each other, and communicated with the main intake passage 7.

上記吸気集合部6は、主吸気通路7の下流端か開口する
上流側端6aと、該上流側端よりも大きい断面積を有し
、各独立吸気通路5a、5b、5c、5dの各々の上流
端か上記主吸気通路7の下流端開口の中心軸線ρを囲む
よう、略正方形状に配置されて開口する下流側端6bと
を備え、かつ上流側端6aから下流側端6bにかけて断
面積か滑らかに増大している。そして、上記吸気集合部
6の下流側端6bは、エンジン1の気筒列方向と略直交
する接続面11に形成されていて、上記各独立吸気通路
5a、5b、5c、5dの上流端が接続されるようにな
っている。また、上記吸気集合部6は、エンジン1の上
方で且つ気筒列方向の一方側(第1図および第2図では
左側)に位置せしめられている。
The intake collecting section 6 has an upstream end 6a that opens at the downstream end of the main intake passage 7, and a cross-sectional area larger than the upstream end, and has a cross-sectional area larger than that of the upstream end, and has an upstream end 6a that opens at the downstream end of the main intake passage 7. The upstream end has a downstream end 6b that is arranged in a substantially square shape and opens so as to surround the central axis ρ of the downstream end opening of the main intake passage 7, and has a cross-sectional area from the upstream end 6a to the downstream end 6b. Or it is increasing smoothly. The downstream end 6b of the intake collecting portion 6 is formed in a connecting surface 11 that is substantially orthogonal to the cylinder row direction of the engine 1, and the upstream ends of the independent intake passages 5a, 5b, 5c, and 5d are connected to each other. It is now possible to do so. Further, the intake air collecting portion 6 is located above the engine 1 and on one side in the direction of the cylinder row (on the left side in FIGS. 1 and 2).

また、上記各独立吸気通路5a、5b、5c5dのうち
、上記吸気集合部6の接続面11 (下流側端6b)に
対して遠くに位置する第1気筒2aおよび第2気筒2b
の各独立吸気通路5a、5bには、これらの吸気管20
(パイプ材)をエンジン1側から離れる方向に水平に延
ばしたのち曲げ加工により彎曲させて上方へ延ばしなか
ら上流端を気筒列方向の一方側に向ける第1彎曲部21
および第2彎曲部22が設けられている。一方、上記吸
気集合部6に対して近くに位置する第3気筒2cおよび
第4気筒2dの各独立吸気通路5c。
Furthermore, among the independent intake passages 5a, 5b, and 5c5d, the first cylinder 2a and the second cylinder 2b are located far from the connection surface 11 (downstream end 6b) of the intake collecting section 6.
Each independent intake passage 5a, 5b has these intake pipes 20.
(pipe material) is horizontally extended in a direction away from the engine 1 side, then curved by bending and extended upward, and the first curved portion 21 has its upstream end directed toward one side in the cylinder row direction.
and a second curved portion 22 are provided. On the other hand, the independent intake passages 5c of the third cylinder 2c and the fourth cylinder 2d are located close to the intake collecting portion 6.

5dには、これらの吸気管20をエンジン1側から離れ
る方向に下方から上方へ円弧を描いて上流端を気筒列方
向の一方側に向ける第3彎曲部23および第4彎曲部2
4か設けられている。
5d, a third curved portion 23 and a fourth curved portion 2 are formed in which these intake pipes 20 draw an arc from below to above in a direction away from the engine 1 side, and whose upstream ends are directed toward one side in the cylinder row direction.
4 are provided.

そして、上記第3気筒2Cおよび第4気筒2dの各独立
吸気通路5c、5dは、そのうちの吸気集合部6の接続
面11に対して近い第4気筒2aの独立吸気通路5dの
第4彎曲部24の曲率半径R4が70m+*に、吸気集
合部6の接続面11に対して遠い第3気筒2Cの独立吸
気通路5Cの第3彎曲部23の曲率半径R3か60順に
それぞれ設定されて、第4彎曲部24の曲率半径R4か
第3彎曲部23の曲率半径R3よりも大きくなるように
形成されている。一方、上記第1気筒2aおよび第2気
筒2bは、そのうちの吸気集合部6の接続面11に対し
て近い第2気筒2bの第2彎曲部22の曲率半径R2が
50mmに、吸気集合部6の接続面11に対して遠い第
1気筒2aの第1彎曲部21の曲率半径R1が40關に
それぞれ設定されて、第2彎曲部22の曲率半径R2が
第1彎曲部21の曲率半径R1よりも大きくなるように
形成されている。この場合、上記各独立吸気通路2a〜
2dの第1〜第4彎曲部21〜24は、吸気集合部6の
接続面11に対して近い気筒の独立吸気通路の順、つま
り第4彎曲部24の曲率半径R4(70++++s) 
、第3彎曲部23の曲率半径R3(60m+s) 、第
2彎曲部22の曲率半径R2(50mm) 、第1彎曲
部21の曲率半径R1(40mm)の順で曲率半径が大
きく形成されている。
Each of the independent intake passages 5c and 5d of the third cylinder 2C and the fourth cylinder 2d has a fourth curved portion of the independent intake passage 5d of the fourth cylinder 2a, which is closer to the connecting surface 11 of the intake collecting portion 6. The radius of curvature R4 of the third curved portion 23 of the independent intake passage 5C of the third cylinder 2C which is far from the connection surface 11 of the intake collecting portion 6 is set to 70 m++, respectively, and the radius of curvature R4 of the The radius of curvature R4 of the fourth curved portion 24 is larger than the radius of curvature R3 of the third curved portion 23. On the other hand, in the first cylinder 2a and the second cylinder 2b, the radius of curvature R2 of the second curved part 22 of the second cylinder 2b, which is closer to the connection surface 11 of the intake collecting part 6, is 50 mm. The radius of curvature R1 of the first curved portion 21 of the first cylinder 2a, which is far from the connection surface 11 of It is designed to be larger than the In this case, each of the independent intake passages 2a~
The first to fourth curved portions 21 to 24 of 2d are arranged in the order of the independent intake passages of the cylinders closest to the connection surface 11 of the intake collecting portion 6, that is, the radius of curvature R4 (70++++s) of the fourth curved portion 24.
, the radius of curvature R3 (60 m+s) of the third curved part 23, the radius of curvature R2 (50 mm) of the second curved part 22, and the radius of curvature R1 (40 mm) of the first curved part 21. .

また、上記第1気筒2aおよび第2気筒2bの各独立吸
気通路5a、5bは、上記吸気集合部6の接続面11に
対し、上記主吸気通路7の中心軸線gと共通の吸気集合
部6の中心軸線gを通る水平線mよりも上側に接続され
ている。一方、上記第3気筒2Cおよび第4気筒2dの
各独立吸気通路5c、5dは、上記吸気集合部6の接続
面11に対し、上記吸気集合部6の中心軸線gを通る水
平線mよりも下側に接続されている。また、第2気筒2
bおよび第3気筒2cの各独立吸気通路5b、5cは、
上記吸気集合部6の接続面11に対し、上記吸気集合部
6の中心軸線Ωを通る鉛直線pよりも反エンジン1側(
第3図では右側)に接続されている。一方、上記第1気
筒2aおよび第4気筒2dの各独立吸気通路5a、5d
は、上記吸気集合部6の接続面11に対し、上記吸気集
合部6の中心軸線gを通る鉛直線pよりもエンジン1側
(第3図では左側)に接続されている。
Further, each of the independent intake passages 5a, 5b of the first cylinder 2a and the second cylinder 2b is connected to the connecting surface 11 of the intake collecting part 6, and the intake collecting part 6 is common to the central axis g of the main intake passage 7. It is connected above the horizontal line m passing through the central axis g of. On the other hand, each of the independent intake passages 5c and 5d of the third cylinder 2C and the fourth cylinder 2d is located below a horizontal line m passing through the central axis g of the intake collecting part 6 with respect to the connecting surface 11 of the intake collecting part 6. connected to the side. Also, the second cylinder 2
Each independent intake passage 5b, 5c of the third cylinder 2c and the third cylinder 2c is
With respect to the connecting surface 11 of the intake air collecting section 6, the side opposite to the engine 1 (
In Fig. 3, it is connected to the right side). On the other hand, each independent intake passage 5a, 5d of the first cylinder 2a and the fourth cylinder 2d
is connected to the connecting surface 11 of the intake air collecting portion 6 on the side closer to the engine 1 (on the left side in FIG. 3) than the vertical line p passing through the central axis g of the air intake collecting portion 6.

したかって、上記実施例では、各気筒2a、2b、2c
、  2dにそれぞれ連通する独立吸気通路5a、5b
、5c、5dは、エンジン1上方で且つ気筒列方向の一
方側に向って延びるように彎曲して互いに吸気集合部6
に対して接続面11て集合されて、エンジン1横方向へ
の幅を増大させずにコンパクトに配置されている。その
場合、各独立吸気通路5a、5b、5c、5dのうち、
吸気集合部6の接続面11に対して近くに位置する気筒
の独立吸気通路の順、つまり第4気筒2dの独立吸気通
路5d、第3気筒2Cの独立吸気通路5c1第2気筒2
bの独立吸気通路5b、第1気筒2aの独立吸気通路5
aの互いに隣り合う順で、吸気集合部6の接続面11に
対して最も遠くに位置する第1気筒2aの独立吸気通路
5aに比して第2気筒2bの独立吸気通路5bが短くな
る分だけ第2彎曲部22の曲率半径R2(50mm)を
第1彎曲部21の曲率半径R1(40mm)よりも10
+om大きくして通路長を長くする糸路で吸気集合部6
の接続面11に、第2気筒2bの独立吸気通路5bに比
して第3気筒2Cの独立吸気通路5Cが短くなる分だけ
第3彎曲部23の曲率半径R3(60闘)を第2彎曲部
22の曲率半径R2(5011111)よりも10mm
大きくして通路長を長くする糸路で吸気集合部6の接続
面11に、第3気筒2Cの独立吸気通路5Cに比して第
4気筒2dの独立吸気通路5dか短くなる分たけ第4彎
曲部24の曲率半径R4(70mm)を第3彎曲部23
の曲率半径R3(60mm+)よりも10+am大きく
して通路長を長くする糸路て吸気集合部6の接続面11
にそれぞれ接続されている。
Therefore, in the above embodiment, each cylinder 2a, 2b, 2c
, 2d, independent intake passages 5a, 5b, respectively communicating with
.
The connecting surfaces 11 are gathered together to provide a compact arrangement without increasing the width of the engine 1 in the lateral direction. In that case, among the independent intake passages 5a, 5b, 5c, 5d,
The order of the independent intake passages of the cylinders located close to the connection surface 11 of the intake collecting part 6, that is, the independent intake passage 5d of the fourth cylinder 2d, the independent intake passage 5c of the third cylinder 2C, the second cylinder 2
b, independent intake passage 5b, first cylinder 2a independent intake passage 5
The independent intake passage 5b of the second cylinder 2b is shorter than the independent intake passage 5a of the first cylinder 2a, which is located farthest from the connection surface 11 of the intake collecting section 6 in the order of adjacent parts a. The radius of curvature R2 (50 mm) of the second curved part 22 is 10 times smaller than the radius of curvature R1 (40 mm) of the first curved part 21.
Intake gathering part 6 with yarn path that increases +om and lengthens the passage length.
The radius of curvature R3 (60°) of the third curved portion 23 is curved into a second curve on the connection surface 11 of 10 mm larger than the radius of curvature R2 (5011111) of part 22
By increasing the length of the thread to lengthen the passage length, a fourth line is formed on the connection surface 11 of the intake collecting portion 6 to compensate for the length of the independent intake passage 5d of the fourth cylinder 2d being shorter than that of the independent intake passage 5C of the third cylinder 2C. The radius of curvature R4 (70 mm) of the curved portion 24 is the third curved portion 23.
The connecting surface 11 of the suction gathering portion 6 is made by increasing the curvature radius R3 (60 mm+) by 10+am to lengthen the passage length.
are connected to each.

このため、独立吸気通路5a、5b、5c、5dの吸気
管21.・・・自体の長さか各気筒2a、2b、2c、
2d毎で等長となり、独立吸気通路5g、5b、5c、
5d間での吸気の分配性を均一なものにできるとともに
、吸気慣性効果による過給を効果的に行うことかできる
For this reason, the intake pipes 21. of the independent intake passages 5a, 5b, 5c, 5d. ...The length of each cylinder 2a, 2b, 2c,
Equal length every 2d, independent intake passages 5g, 5b, 5c,
In addition to making the distribution of intake air uniform between 5d, it is also possible to effectively perform supercharging due to the intake inertia effect.

また、上記の如く各独立吸気通路5a、5b5c、5d
か、吸気集合部6に対して近い第4気筒2d〜第1気筒
2aの独立吸気通路5d、5c。
In addition, as described above, each independent intake passage 5a, 5b5c, 5d
Or, the independent intake passages 5d and 5c of the fourth cylinder 2d to the first cylinder 2a, which are close to the intake collecting part 6.

5b、5aの順で、それぞれの彎曲部の曲率半径を10
龍ずつ大きくした通路長を長くする糸路でもって吸気集
合部6の接続面11に接続されていることから、吸気集
合部6に対して近い第4気筒2dおよび第3気筒2Cの
各独立吸気通路5d。
In the order of 5b and 5a, the radius of curvature of each curved part is 10
Since it is connected to the connecting surface 11 of the intake collecting section 6 by a thread that lengthens the passage length by increasing the length of the passage, each independent intake of the fourth cylinder 2d and the third cylinder 2C, which are close to the intake collecting section 6, Passage 5d.

5Cの吸気管21.・・・自体の急激な彎曲か緩和され
て、吸気抵抗を減少できる。その上、各独立吸気通路5
a、5b、5c、5dが、吸気集合部6に対して近い第
4気筒2d〜第1気筒2aの独立吸気通路5d〜5aの
順で、吸気管21.・・・自体の彎曲を緩和しているの
で、各気筒2a〜2dの独立吸気通路5a、5b、5c
、5dの吸気抵抗が均一なものとなり、各気筒2a〜2
d間における充填効率のばらつきを解消できる。
5C intake pipe 21. ...The sharp curvature of the body itself is alleviated, and intake resistance can be reduced. Moreover, each independent intake passage 5
a, 5b, 5c, and 5d are the independent intake passages 5d to 5a of the fourth cylinder 2d to the first cylinder 2a, which are closer to the intake collecting portion 6, in that order, and are the intake pipes 21. ...Since the curvature of the cylinder itself is relaxed, the independent intake passages 5a, 5b, 5c of each cylinder 2a to 2d
, 5d becomes uniform, and each cylinder 2a to 2
It is possible to eliminate variations in filling efficiency between d.

さらに、各独立吸気通路5a、5b、5c、5dのうち
、吸気集合部6の接続面11に対して遠い第1気筒2a
および第2気筒2bの各独立吸気通路5a、5bが、吸
気集合部6の接続面11に対して近い第3気筒2cおよ
び第4気筒2dの各独立吸気通路5c、5dの曲率半径
R3,R4の大きな第1彎曲部21および第2彎曲部2
2を迂回するよう1曲率半径R3,R4の小さな第3彎
曲部23および第4彎曲部24でもって上方へ延びて、
吸気集合部6の中心軸線gを通る水平線mよりも上側の
接続面11に接続されている。一方、吸気集合部6の接
続面11に対して近い第3気筒2cおよび第4気筒2d
の各独立吸気通路5c、5dが、吸気集合部6の接続面
11に対して遠い第1気筒2aおよび第2気筒2bの各
独立吸気通路5a。
Furthermore, among the independent intake passages 5a, 5b, 5c, and 5d, the first cylinder 2a that is farthest from the connection surface 11 of the intake collecting section 6
And the radius of curvature R3, R4 of each independent intake passage 5c, 5d of the third cylinder 2c and fourth cylinder 2d, where each independent intake passage 5a, 5b of the second cylinder 2b is close to the connection surface 11 of the intake collecting part 6. Large first curved portion 21 and second curved portion 2
2, extending upward with a third curved portion 23 and a fourth curved portion 24 having small curvature radii R3 and R4,
It is connected to the connection surface 11 above the horizontal line m passing through the central axis g of the intake air collection section 6 . On the other hand, the third cylinder 2c and the fourth cylinder 2d which are close to the connection surface 11 of the intake collecting part 6
The independent intake passages 5a of the first cylinder 2a and the second cylinder 2b are far from the connection surface 11 of the intake collecting portion 6.

5bに邪魔されることなく該各独立吸気通路5a。Each independent intake passage 5a without being obstructed by 5b.

5bの下方において曲率半径R3,R4の大きな第1彎
曲部21および第2彎曲部22が安易に取り回されて吸
気集合部6の接続面11に対して吸気集合部6の中心軸
線pを通る水平線mよりも下側に接続されている。この
ため、吸気集合部に対して遠い第1および第2気筒の各
独立吸気通路が吸気集合部の接続面の下側に接続される
もののように吸気集合部に対して近い第3および第4気
筒の各独立吸気通路が、吸気集合部に対して遠い第1お
よび第2気筒の各独立吸気通路を避けながら接続されて
通路長を不要に長くしたり、彎曲部の曲率半径を小さく
したすせずに容易に取り回され、各独立吸気通路5a、
5b、5c、5dの取り回し性を良好にできる。
5b, the first curved part 21 and the second curved part 22 with large curvature radii R3 and R4 are easily routed and pass through the central axis p of the intake collecting part 6 with respect to the connection surface 11 of the intake collecting part 6. It is connected below the horizontal line m. For this reason, the independent intake passages of the first and second cylinders, which are far from the intake collecting part, are connected to the lower side of the connection surface of the intake collecting part, and the independent intake passages of the third and fourth cylinders, which are far from the intake collecting part, are connected to the lower side of the connection surface of the intake collecting part. The independent intake passages of the cylinders are connected while avoiding the independent intake passages of the first and second cylinders that are far away from the intake gathering part, thereby making the passage length unnecessarily long or reducing the radius of curvature of the curved part. Each independent intake passage 5a,
5b, 5c, and 5d can be easily handled.

しかも、各独立吸気通路5a、5b、5c、5dのうち
、気筒列方向中央に位置する第2気筒2bおよび第3気
筒2Cの各独立吸気通路5b、5Cが、レイアウト的に
厳しい各気筒(エンジン)と集合部との間において両側
方に位置する第1気筒2aおよび第4気筒2dの各独立
吸気通路5a。
Moreover, among the independent intake passages 5a, 5b, 5c, and 5d, the independent intake passages 5b and 5C of the second cylinder 2b and the third cylinder 2C, which are located in the center in the cylinder row direction, ) and the gathering portion, the independent intake passages 5a of the first cylinder 2a and the fourth cylinder 2d are located on both sides.

5dの彎曲部21.24の邪魔にならないよう。Be careful not to get in the way of the curved parts 21 and 24 of 5d.

気筒列方向と直交する面上で彎曲して、吸気集合部6の
接続面11に対して吸気集合部6の中心軸線gを通る鉛
直線pよりも反エンジン1側に接続されている。一方、
両側方に位置する第1気筒2aおよび第4気筒2dの各
独立吸気通路5a、5dが、気筒の存在しない側方とな
る気筒列方向で余裕をもって彎曲して、吸気集合部6の
接続面11に対して吸気集合部6の中心軸線gを通る鉛
直線mよりもエンジン1側に接続されている。このため
、吸気集合部6がコンパクト化を図る上で各気筒2a、
  2b、  2c、  2d (!ンジン1)に近接
配置されていても、各気筒2a〜2dの独立吸気通路5
8〜5dは、彎曲部21,22,23゜24の曲率半径
R1,R2,R3,R4に制約を受けることなく彎曲さ
れて容易に取り回され、各独立吸気通路5a、5b、5
c、5dの取り回し性をさらに良好にできる。
It is curved on a plane perpendicular to the direction of the cylinder row, and is connected to the connection surface 11 of the intake collecting section 6 on the side opposite to the engine 1 from the vertical line p passing through the central axis g of the intake collecting section 6. on the other hand,
The independent intake passages 5a and 5d of the first cylinder 2a and the fourth cylinder 2d located on both sides are curved with a margin in the direction of the cylinder row on the side where no cylinder exists, so that the connecting surface 11 of the intake collecting portion 6 In contrast, it is connected to the engine 1 side with respect to a vertical line m passing through the central axis g of the intake air gathering portion 6. Therefore, in order to make the intake collecting section 6 more compact, each cylinder 2a,
2b, 2c, 2d (! engine 1), the independent intake passages 5 of each cylinder 2a to 2d
8 to 5d are curved and easily routed without being restricted by the curvature radii R1, R2, R3, and R4 of the curved portions 21, 22, 23°24, and the independent intake passages 5a, 5b, 5
c, 5d can be more easily handled.

尚、本発明は上記実施例に限定されるものではなく、そ
の他種々の変形例を包含するものである。
It should be noted that the present invention is not limited to the above embodiments, but includes various other modifications.

例えば、上記実施例では、第1気筒2aおよび第2気筒
2bの各独立吸気通路5a、5bを吸気集合部6の中心
軸線gを通る水平線mよりも上側の接続面11に接続す
る一方、第3気筒2cおよび第4気筒2dの各独立吸気
通路5c、5dを吸気集合部6の中心軸線gを通る水平
線mよりも下側の接続面11に接続したが、第1気筒お
よび第2気筒の各独立吸気通路が吸気集合部の中心軸線
を通る水平線よりも下側の接続面に接続される一方、第
3気筒および第4気筒の各独立吸気通路が吸気集合部の
中心軸線を通る水平線よりも上側の接続面に接続される
ようにしても良い。また、第2気筒2bおよび第3気筒
2Cの各独立吸気通路5b。
For example, in the above embodiment, the independent intake passages 5a and 5b of the first cylinder 2a and the second cylinder 2b are connected to the connecting surface 11 above the horizontal line m passing through the central axis g of the intake collecting section 6, while the Although the independent intake passages 5c and 5d of the third cylinder 2c and the fourth cylinder 2d are connected to the connecting surface 11 below the horizontal line m passing through the central axis g of the intake collecting section 6, Each independent intake passage is connected to a connecting surface below a horizontal line passing through the central axis of the intake collecting section, while each independent intake passage of the third and fourth cylinders is connected to a connecting surface below a horizontal line passing through the central axis of the intake collecting part. may also be connected to the upper connection surface. Moreover, each independent intake passage 5b of the second cylinder 2b and the third cylinder 2C.

5cを吸気集合部6の中心軸線Ωを通る鉛直線pよりも
反エンジン1側の接続面11に接続する一方、第1気筒
2aおよび第4気筒2dの各独立吸気通路5a、5dを
吸気集合部6の中心軸線gを通る鉛直線mよりもエンジ
ン1側の接続面11に接続したが、第2気筒および第3
気筒の各独立吸気通路が吸気集合部の中心軸線を通る鉛
直線よりもエンジン側の接続面に接続される一方、第1
気筒および第4気筒の各独立吸気通路が吸気集合部の中
心軸線を通る鉛直線よりも反エンジン側の接続面に接続
されるようにしても良い。これらの場合には、独立吸気
通路の吸気管自体の長さが各気筒毎で等長となって独立
吸気通路間での吸気の分配性を均一なものにして吸気慣
性効果による過給を効果的に行うことができるとともに
、吸気集合部に対して近い第4気筒および第3気筒の各
独立吸気通路の吸気管自体の急激な彎曲を緩和して吸気
抵抗を減少できる上、各気筒の独立吸気通路の吸気抵抗
を均一なものにして各気筒間における充填効率のばらつ
きを解消できる。
5c is connected to the connection surface 11 on the side opposite to the engine 1 from the vertical line p passing through the center axis Ω of the intake collecting section 6, while the independent intake passages 5a and 5d of the first cylinder 2a and the fourth cylinder 2d are connected to the intake collecting part 6. Although it was connected to the connection surface 11 on the engine 1 side with respect to the vertical line m passing through the central axis g of the section 6, the second cylinder and the third cylinder
Each independent intake passage of the cylinder is connected to a connecting surface on the engine side from a vertical line passing through the central axis of the intake collecting section, while the first
Each independent intake passage of the cylinder and the fourth cylinder may be connected to a connecting surface on the side opposite to the engine from a vertical line passing through the central axis of the intake collecting section. In these cases, the length of the intake pipe itself of the independent intake passages is made equal for each cylinder, and the distribution of intake air between the independent intake passages is made uniform, thereby achieving supercharging due to the intake inertia effect. In addition, it is possible to reduce the intake resistance by alleviating the sharp curvature of the intake pipes themselves in the independent intake passages of the fourth and third cylinders, which are close to the intake collecting part, and By making the intake resistance of the intake passage uniform, variations in filling efficiency between cylinders can be eliminated.

さらに、上記実施例は、直列4気筒エンジン1に適用し
た例であるが、複数の気筒を有する直列型エンジンに適
用することができる。例えば、直列6気筒エンジンの場
合、吸気集合部に対して遠(に位置する気筒および近く
に位置する気筒をそれぞれ3気筒ずつに分け、これら3
つの気筒毎の各独立吸気通路を吸気集合部の上側および
下側に連通させる他、吸気集合部に対して遠くに位置す
る気筒、近くに位置する気筒および中間に位置する気筒
をそれぞれ2気筒ずつに分け、これら2つの気筒毎の各
独立吸気通路を吸気集合部の上側。
Further, although the above embodiment is an example applied to an in-line four-cylinder engine 1, the present invention can be applied to an in-line engine having a plurality of cylinders. For example, in the case of an in-line six-cylinder engine, the cylinders located far away from the intake collecting section and the cylinders located close to it are divided into three cylinders each.
In addition to communicating the independent intake passages of each cylinder with the upper and lower sides of the intake collecting part, two cylinders each are connected to each cylinder located far away from the intake collecting part, two cylinders are located close to the intake part, and two cylinders are located in the middle. Separate the independent intake passages for each of these two cylinders into the upper part of the intake collecting section.

下側および中央に連通させることも可能である。It is also possible to communicate with the lower side and the center.

(発明の効果) 以上説明したように、請求項(1)に係る発明によると
、各気筒の独立吸気通路のうち、集合部の接続面に対し
て近い気筒の独立吸気通路を、集合部の接続面に対して
遠い気筒の独立吸気通路に比して気筒列方向に短くなる
分たけ彎曲部の曲率半径を大きくした通路長の長い糸路
て集合部の接続面に接続させたので、独立吸気通路自体
の各気筒毎での長さを等長にしつつコンパクトに配置で
き、独立吸気通路間での吸気の分配性を均一にてきると
ともに、動的効果による過給を効果的に行うことができ
る。しかも、集合部に対して近い気筒の独立吸気通路の
通路自体の急激な彎曲か緩和されて吸気抵抗を減少でき
る上、各気筒の独立吸気通路の吸気抵抗を均一なものに
して各気筒間における充填効率のばらつきを解消できる
(Effects of the Invention) As explained above, according to the invention according to claim (1), among the independent intake passages of each cylinder, the independent intake passages of the cylinders that are closer to the connection surface of the collecting part are connected to the connecting face of the collecting part. Compared to the independent intake passages of cylinders that are far from the connection surface, the radius of curvature of the curved part is increased by the length of the passage, which is shorter in the direction of the cylinder row. The intake passage itself can be arranged compactly by making the length of each cylinder equal, ensuring uniform distribution of intake air between independent intake passages, and effectively performing supercharging through dynamic effects. I can do it. Moreover, the sharp curvature of the independent intake passages of the cylinders near the gathering part can be alleviated to reduce intake resistance, and the intake resistance of the independent intake passages of each cylinder can be made uniform, so that the air flow between each cylinder can be reduced. Can eliminate variations in filling efficiency.

また、請求項(2)に係る発明によると、各独立吸気通
路のうち、集合部の接続面に対して遠い気筒の独立吸気
通路を、集合部の接続面に対して近い気筒の独立吸気通
路に比して長くなる分たけ曲率半径を小さくした彎曲部
でもって上方へ延ばして近い気筒の独立吸気通路の彎曲
部を迂回させつつ集合部の接続面の上側に接続する一方
、集合部の接続面に対して近い気筒の独立吸気通路を、
集合部の接続面に対して遠い気筒の独立吸気通路に比し
て短くなる分だけ曲率半径を大きくした彎曲部を該独立
吸気通路の下方において彎曲させて集合部の接続面の下
側に接続されている。このため、各独立吸気通路は通路
長を不要に長くしたり、彎曲部の曲率半径を小さくした
すせずに容易に取り回され、各独立吸気通路の取り回し
性を良好にできる。
Further, according to the invention according to claim (2), among the independent intake passages, the independent intake passage of a cylinder far from the connection surface of the gathering portion is replaced with the independent intake passage of a cylinder close to the connection surface of the gathering portion. The curved part has a smaller radius of curvature due to its length compared to the above, and is extended upward to bypass the curved part of the independent intake passage of the nearby cylinder and connect to the upper side of the connecting surface of the collecting part. The independent intake passage of the cylinder close to the surface,
A curved portion with a radius of curvature that is shorter than the independent intake passage of a cylinder far from the connection surface of the gathering portion is curved below the independent intake passage and connected to the lower side of the connection surface of the gathering portion. has been done. Therefore, each independent intake passage can be easily routed without unnecessarily lengthening the passage length or reducing the radius of curvature of the curved portion, thereby improving the maneuverability of each independent intake passage.

また、請求項(3)に係る発明によると、各独立吸気通
路のうち、中央の気筒の独立吸気通路を、レイアウト的
に厳しい各気筒と集合部との間において気筒列方向と直
交する面上で彎曲させて集合部の接続面の反エンジン側
に接続する一方、両側方の各独立吸気通路を気筒列方向
で余裕をもって彎曲させて集合部の接続面のエンジン側
に接続したので、集合部がコンパクト化を図る上で各気
筒に近接されてレイアウト的に厳しい各気筒と集合部と
の間に各独立吸気通路が配置されていても、各気筒の独
立吸気通路は彎曲部の曲率半径に制約を受けることなく
彎曲されてさらに容易に取り回され、各独立吸気通路の
取り回し性をより良好にできる。
Further, according to the invention according to claim (3), among the independent intake passages, the independent intake passage of the central cylinder is arranged on a plane perpendicular to the cylinder row direction between each cylinder and the gathering part, which is difficult in terms of layout. At the same time, each independent intake passage on both sides was curved with a margin in the direction of the cylinder row and connected to the engine side of the connecting surface of the gathering section, so that the connecting section of the gathering section Even if each independent intake passage is arranged between each cylinder and the gathering part, which is close to each cylinder in order to make it more compact, the layout is difficult. It can be curved without any restrictions and can be routed more easily, making it possible to improve the maneuverability of each independent intake passage.

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

第1図ないし第3図は本発明の実施例を示し、第1図は
エンジンおよび吸気系の平面図、第2図は第1図に関わ
る側面図、第3図は第1図に関わる正面図である。 1・・・エンジン 2a〜2d・・・気筒 5a〜5d・・・独立吸気通路 6・・・吸気集合部(集合部) 11・・・接続面 21〜24・・・彎曲部 ほか1名
1 to 3 show an embodiment of the present invention, FIG. 1 is a plan view of the engine and intake system, FIG. 2 is a side view related to FIG. 1, and FIG. 3 is a front view related to FIG. 1. It is a diagram. 1... Engine 2a to 2d... Cylinder 5a to 5d... Independent intake passage 6... Intake gathering part (gathering part) 11... Connection surface 21 to 24... Curved part and 1 other person

Claims (3)

【特許請求の範囲】[Claims] (1)複数の気筒を有するエンジンにその一側面側より
各気筒にそれぞれ連通する独立吸気通路が設けられ、該
各独立吸気通路は彎曲したのちその上流端が一箇所に集
合されるようにしたエンジンの吸気構造において、上記
各独立吸気通路は、その上流端の集合部に対してエンジ
ンの気筒列方向と略直交する接続面で接続されていると
ともに、上記集合部はエンジンの上方で且つ気筒列方向
の一方側に位置しており、上記各独立吸気通路のうち、
上記集合部の接続面に対して近くに位置する気筒の独立
吸気通路は、集合部の接続面に対して遠くに位置する気
筒の独立吸気通路よりも彎曲部の曲率半径が大きくなる
ように形成されていることを特徴とするエンジンの吸気
構造。
(1) An engine having a plurality of cylinders is provided with independent intake passages that communicate with each cylinder from one side of the engine, and each independent intake passage is curved and then its upstream ends are gathered in one place. In the intake structure of the engine, each of the independent intake passages is connected to a gathering portion at the upstream end thereof at a connecting surface substantially orthogonal to the cylinder row direction of the engine, and the gathering portion is above the engine and connected to the cylinders. It is located on one side in the column direction, and among the above independent intake passages,
The independent intake passages of cylinders located close to the connection surface of the gathering section are formed so that the radius of curvature of the curved section is larger than that of the independent intake passages of cylinders located far from the connection surface of the gathering section. An engine intake structure characterized by:
(2)各独立吸気通路のうち、集合部の接続面に対して
近くに位置する気筒の独立吸気通路は該集合部の接続面
の上側に接続されている一方、集合部の接続面に対して
遠くに位置する気筒の独立吸気通路は該集合部の接続面
の下側に接続されている請求項(1)記載のエンジンの
吸気構造。
(2) Among the independent intake passages, the independent intake passage of the cylinder located close to the connecting surface of the collecting section is connected to the upper side of the connecting surface of the collecting section, while the independent intake passage of the cylinder located near the connecting surface of the collecting section 2. The engine intake structure according to claim 1, wherein the independent intake passages of the cylinders located far away from each other are connected to the lower side of the connection surface of the gathering portion.
(3)気筒を3つ以上有し、各独立吸気通路のうち、両
側方に位置する気筒の独立吸気通路は集合部の接続面の
エンジン側に接続されている一方、中央に位置する気筒
の独立吸気通路は集合部の接続面の反エンジン側に接続
されている請求項(1)記載のエンジンの吸気構造。
(3) It has three or more cylinders, and among the independent intake passages, the independent intake passages of the cylinders located on both sides are connected to the engine side of the connecting surface of the gathering part, while the independent intake passages of the cylinders located in the center are 2. The engine intake structure according to claim 1, wherein the independent intake passage is connected to a side opposite to the engine of a connection surface of the gathering portion.
JP23787190A 1990-09-06 1990-09-06 Engine intake structure Expired - Lifetime JP2828333B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP23787190A JP2828333B2 (en) 1990-09-06 1990-09-06 Engine intake structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP23787190A JP2828333B2 (en) 1990-09-06 1990-09-06 Engine intake structure

Publications (2)

Publication Number Publication Date
JPH04116258A true JPH04116258A (en) 1992-04-16
JP2828333B2 JP2828333B2 (en) 1998-11-25

Family

ID=17021652

Family Applications (1)

Application Number Title Priority Date Filing Date
JP23787190A Expired - Lifetime JP2828333B2 (en) 1990-09-06 1990-09-06 Engine intake structure

Country Status (1)

Country Link
JP (1) JP2828333B2 (en)

Also Published As

Publication number Publication date
JP2828333B2 (en) 1998-11-25

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