JP2839657B2 - Intake manifold for internal combustion engine - Google Patents

Intake manifold for internal combustion engine

Info

Publication number
JP2839657B2
JP2839657B2 JP16056990A JP16056990A JP2839657B2 JP 2839657 B2 JP2839657 B2 JP 2839657B2 JP 16056990 A JP16056990 A JP 16056990A JP 16056990 A JP16056990 A JP 16056990A JP 2839657 B2 JP2839657 B2 JP 2839657B2
Authority
JP
Japan
Prior art keywords
intake
curved
pipe section
chamber
internal combustion
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 - Fee Related
Application number
JP16056990A
Other languages
Japanese (ja)
Other versions
JPH0450430A (en
Inventor
伸一 難波
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.)
Daihatsu Motor Co Ltd
Original Assignee
Daihatsu Kogyo KK
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 Daihatsu Kogyo KK filed Critical Daihatsu Kogyo KK
Priority to JP16056990A priority Critical patent/JP2839657B2/en
Publication of JPH0450430A publication Critical patent/JPH0450430A/en
Application granted granted Critical
Publication of JP2839657B2 publication Critical patent/JP2839657B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、エアクリーナからの吸気を、各気筒に分配
する吸気マニホールドの改良に関するものである。
Description: TECHNICAL FIELD The present invention relates to an improvement of an intake manifold that distributes intake air from an air cleaner to each cylinder.

〔従来の技術〕[Conventional technology]

最近の内燃機関には、気筒列の方向に延びるように配
設したチャンバーと、各気筒における吸気ポートとを、
各気筒の各々について互いに独立した分岐吸気管路を介
して接続することによって、慣性過給の効果を得ること
ができるようにした吸気マニホールドが適用されてい
る。
In recent internal combustion engines, a chamber arranged to extend in the direction of the cylinder row, and an intake port in each cylinder,
An intake manifold is applied in which each cylinder is connected via a branch intake pipe independent of each other to thereby obtain an inertia supercharging effect.

そして、この種の吸気マニホールドにおける各分切吸
気管路は、所定の慣性過給の効果を得るために、比較的
長くしなければならないので、この各分岐吸気管路は、
例えば、実開昭61−75665号公報等に記載されているよ
うに、内燃機関の側方に気筒列の方向に延びるように配
設したチャンバーから一旦下向きに突出し、適宜湾曲半
径で略水平横向きに湾曲したのち、シリンダヘッドの側
面に開口する吸気ポートに接続するように、換言する
と、前記各分岐吸気管路のうち吸気ポートに接続する部
分を略直線状に延びる横向き管部に、前記チャンバーに
接続する部分を略直線状に延びる立上り管部に、その間
の部分を上向きに湾曲した湾曲管部に構成して、前記各
分岐吸気管路を、内燃機関のクランク軸方向から見て略
L字状に湾曲するようにしている。
Each of the divided intake lines in this type of intake manifold must be relatively long in order to obtain a predetermined inertia supercharging effect.
For example, as described in Japanese Utility Model Laid-Open Publication No. 61-75665 and the like, it once protrudes downward from a chamber arranged so as to extend in the direction of the cylinder row to the side of the internal combustion engine, and is appropriately horizontally oriented with a radius of curvature. After connecting to the intake port opened on the side surface of the cylinder head, in other words, a portion of each of the branch intake pipes connected to the intake port is connected to the laterally extending pipe portion that extends substantially linearly. Is connected to a riser pipe portion extending substantially linearly, and a portion between the riser pipe portions is formed as a curved pipe portion curved upward, so that each of the branch intake pipes is substantially L when viewed from the crankshaft direction of the internal combustion engine. It is made to curve in a letter shape.

〔発明が解決しようとする課題〕[Problems to be solved by the invention]

しかし、各分岐吸気管路を、略L字状に湾曲する場
合、この各分岐吸気管路内における吸気流れの抵抗は、
当該各分岐吸気管路のうち前記湾曲管部における湾曲角
度に比例し、湾曲管部における湾曲半径に反比例し、湾
曲角度が大きいとき及び湾曲半径が小さいとき大きく、
湾曲角度が小さいとき及び湾曲半径が大きいとき小さい
一方、各分岐吸気管路には、慣性過給を達成することの
ために所定の長さ寸法が必要である。
However, when each branch intake pipe is curved in a substantially L-shape, the resistance of the intake flow in each branch intake pipe becomes
Of the respective branch intake pipes, proportional to the bending angle in the bending pipe portion, inversely proportional to the bending radius in the bending pipe portion, large when the bending angle is large and when the bending radius is small,
While small when the bend angle is small and large when the bend radius is large, each branch intake line requires a predetermined length dimension to achieve inertial supercharging.

そこで、吸気マニホールドの小型化と、剛性のアップ
とを図るためには、この吸気マニホールドにおけるチャ
ンバーを、内燃機関に近付けるように構成しなければな
らないが、チャンバーを内燃機関に近付けると、前記各
分岐吸気管路のうち湾曲管部における湾曲角度が、直角
よりも大きくなると共に、前記湾曲管部における湾曲半
径も小さくなるから、吸気の流れ抵抗が大きくなり、ひ
いては、出力の低下を招来すると言う問題があった。
Therefore, in order to reduce the size of the intake manifold and increase the rigidity, the chamber in the intake manifold must be configured to be close to the internal combustion engine. Since the bending angle in the curved pipe portion of the intake pipe becomes larger than the right angle and the bending radius in the curved pipe portion also becomes smaller, the flow resistance of the intake air increases, and the output is reduced. was there.

本発明は、吸気マニホールドの小型化を図るためにチ
ャンバーを内燃機関に近づけた場合において、各分岐吸
気管路における吸気流れ抵抗が増大することをその湾曲
部における形態によって防止できるようにすることを技
術的課題とするものである。
The present invention provides a configuration in which, when the chamber is brought close to the internal combustion engine in order to reduce the size of the intake manifold, the intake flow resistance in each branch intake pipe can be prevented from increasing by the shape of the curved portion. It is a technical issue.

〔課題を解決するための手段〕[Means for solving the problem]

この技術的課題を達成するため本発明は、 「気筒列の方向に延びるチャンバーと、各気筒における
吸気ポートとの間を、各気筒の各々について独立する分
岐吸気管路にて接続し、この各分岐吸気管路のうち前記
吸気ポートに接続する部分を略直線状に延びる横向き管
部に、前記チャンバーに接続する部分を略直線状に延び
る立上り管部に、その間の部分を上向きに直角よりも大
きい角度に湾曲した湾曲管部に構成して成る吸気マニホ
ールドにおいて、 前記各分岐吸気管路における湾曲管部を、チャンバー
への立上り管部に繋がる上流側湾曲管部と、吸気ポート
への横向き管部に繋がる下流側湾曲管部とで構成して、
前記下流側湾曲管部における湾曲半径を、前記上流側湾
曲管部における湾曲半径よりも大きくする。」 と言う構成にした。
In order to achieve this technical object, the present invention provides a method of connecting a chamber extending in the direction of a cylinder row and an intake port of each cylinder with a branch intake pipe independent of each cylinder. In the branch intake pipe, a portion connected to the intake port is connected to a substantially straight laterally extending pipe portion, a portion connected to the chamber is connected to a substantially straight rising pipe portion, and a portion therebetween is upwardly bent at a right angle. In the intake manifold constituted by a curved pipe section curved at a large angle, the curved pipe section in each of the branch intake pipes is connected to an upstream curved pipe section connected to a rising pipe section to a chamber, and a lateral pipe to an intake port. And a downstream curved tube section connected to the section,
The radius of curvature of the downstream curved tube is made larger than the radius of curvature of the upstream curved tube. "

〔実施例〕〔Example〕

以下、本発明の実施例を図面について説明するに、図
において符号1は、第1気筒A1、第2気筒A2、第3気筒
A3及び第4気筒A4を備えた四気筒内燃機関を示し、該内
燃機関1のシリンダヘッド2における長手側面2aには、
前記各気筒A1,A2,A3,A4における吸気ポート3,4,5,6が開
口している。
Hereinafter, an embodiment of the present invention will be described with reference to the drawings. In the drawings, reference numeral 1 denotes a first cylinder A1, a second cylinder A2, and a third cylinder.
4 shows a four-cylinder internal combustion engine having an A3 and a fourth cylinder A4, and a longitudinal side surface 2a of a cylinder head 2 of the internal combustion engine 1 includes:
The intake ports 3, 4, 5, and 6 in each of the cylinders A1, A2, A3, and A4 are open.

符号7は、前記内燃機関1に対する慣性過給式の吸気
マニホールドを示し、該吸気マニホールド7は、前記内
燃機関1の側方に気筒列の方向に延びるように配設した
チャンバー8の、該チャンバー8と前記各吸気ポート3,
4,5,6との間を各々別々に接続する四本の分岐吸気管路
9,10,11,12とから成り、前記チャンバー8は、内燃機関
1に近付けた部位に位置する一方、前記各分岐吸気管路
9,10,11,12は、側面視において略L字状に湾曲してい
る。
Reference numeral 7 denotes an inertia-supercharged intake manifold for the internal combustion engine 1, and the intake manifold 7 is one of the chambers 8 arranged to extend in the direction of a cylinder row beside the internal combustion engine 1. 8 and the respective intake ports 3,
Four branch intake lines that connect separately between 4, 5, and 6
The chamber 8 is located at a position close to the internal combustion engine 1 while each of the branch intake pipes
9, 10, 11, and 12 are curved in a substantially L-shape in a side view.

すなわち、前記各分岐吸気管路9,10,11,12は、前記吸
気ポート3,4,5,6に接続する部分を略直線状にした横向
き管部Dと、前記チャンバー9の下面に接続する部分を
略直線状にした立上り管部Cと、この横向き管部Dと立
上り管部Cとの間を繋ぐ上向きの湾曲管部Bとによって
構成され、且つ、前記湾曲管部Bにおける湾曲角度は直
角よりも大きい角度に構成されている。
In other words, each of the branch intake pipes 9, 10, 11, 12 is connected to a laterally oriented pipe portion D having a substantially linear portion connected to the intake ports 3, 4, 5, 6 and a lower surface of the chamber 9. And a rising pipe section B connecting the rising pipe section C and the horizontal pipe section D, and a bending angle in the bending pipe section B. Are configured at an angle greater than a right angle.

そして、前記各分岐吸気管路9,10,11,12における湾曲
管部Bを、前記チャンバー8への立上がり管部Cに繋が
る上流側湾曲管部B1と、各吸気ポート3,4,5,6への横向
き管部Dに繋がる下流側湾曲管部B2とによって構成し、
前記下流側湾曲部B2における湾曲半径R2を、前記上流側
湾曲管部B1における湾曲半径R1よりも大きくすると言う
構成にする。
The curved pipe section B in each of the branch intake pipes 9, 10, 11, 12 is connected to an upstream curved pipe section B1 connected to a rising pipe section C to the chamber 8, and each of the intake ports 3, 4, 5,. 6 comprising a downstream curved tube portion B2 connected to the transverse tube portion D to 6,
The configuration is such that the bending radius R2 of the downstream bending portion B2 is larger than the bending radius R1 of the upstream bending tube portion B1.

なお、前記各分岐吸気管路9,10,11,12における立上り
管部Cは、チャンバー8に向かって断面積を次第に拡大
するように、換言すると、湾曲管部Bに向かって断面積
を次第に減少するように構成されている。
The rising pipe section C in each of the branch intake pipes 9, 10, 11, 12 gradually increases in cross-sectional area toward the chamber 8, in other words, gradually increases in cross-sectional area toward the curved pipe section B. It is configured to decrease.

この慣性過給式の吸気マニホールド7における各分岐
吸気管路9,10,11,12には、所定の長さ寸法が必要である
から、チャンバー8を、内燃機関1に近付けた状態で、
各分岐吸気管路9,10,11,12に所定の長さ寸法を確保する
には、各分岐吸気管路9,10,11,12の湾曲管部Bにおける
湾曲角度を直角よりも大きくすると共に、この湾曲管部
Bにおける湾曲半径Rを、第2図に二点鎖線Eで示すと
共に、第3図に示すように、比較的に小さいものにしな
ければならないから、各分岐吸気管路9,10,11,12内にお
ける吸気流れ抵抗が大きくなり、慣性過給の効果が減少
することになる。
Each branch intake pipe 9, 10, 11, 12 in the inertia supercharged intake manifold 7 needs a predetermined length dimension, so that the chamber 8 is placed close to the internal combustion engine 1,
In order to secure a predetermined length dimension in each of the branch intake pipes 9, 10, 11, and 12, the bending angle of each of the branch intake pipes 9, 10, 11, and 12 in the curved pipe portion B is made larger than a right angle. At the same time, the bending radius R in the bending pipe portion B must be relatively small as shown by a two-dot chain line E in FIG. 2 and shown in FIG. , 10, 11, and 12, the flow resistance of the intake air increases, and the effect of inertia supercharging decreases.

ところで、各分岐吸気管路9,10,11,12の湾曲管部Bに
おける吸気流れ抵抗は、管路内における吸気の流速に比
例して増大すると共に、湾曲角度に比例し、且つ、湾曲
半径に反比例するものであるが、前記各分岐吸気管路9,
10,11,12内における吸気の流れは、圧縮性気体が圧力が
低い方向に向かって断熱膨張しながら流れるものとみな
すことができて、各分岐吸気管路9,10,11,12内における
吸気の流速は、チャンバー8に近い部分が最も遅くて、
この部分から各吸気ポート3,4,5,6に向かって次第に断
熱膨張によって加速されるものであるから、吸気の流速
度により湾曲管部のうち下流側湾曲管部における吸気流
れ抵抗の方が、湾曲部のうち上流側湾曲管部における吸
気流れ抵抗よりも大きい傾向を呈する。
By the way, the intake flow resistance in the curved pipe portion B of each of the branch intake pipes 9, 10, 11, 12 increases in proportion to the flow velocity of the intake air in the pipes, is proportional to the bending angle, and has a bending radius. Is inversely proportional to each of the branch intake pipes 9,
The flow of the intake air in 10, 11, 12 can be regarded as a flow in which the compressible gas flows while adiabatically expanding in the direction of lower pressure, and the flow of the intake air in each branch intake pipe 9, 10, 11, 12 The flow rate of the intake air is the slowest in the part near the chamber 8,
From this part, the air is gradually accelerated by adiabatic expansion toward each of the intake ports 3, 4, 5, and 6, so that the intake flow resistance in the downstream curved pipe portion of the curved pipe portion is higher due to the flow velocity of the intake air. In addition, there is a tendency that the intake flow resistance in the upstream curved pipe portion of the curved portion is larger than the intake flow resistance.

本発明者は、この点に着目して、前記のように、各分
岐吸気管路9,10,11,12における湾曲管部Bを、チャンバ
ー8への立上り管部Cに繋がる上流側湾曲管部B1と、各
吸気ポート3,4,5,6への横向き管部Dに繋がる下流側湾
曲管部B2とによって構成し、前記下流側湾曲管部B2にお
ける湾曲半径R2を、前記上流側湾曲管部B1における半径
よりも大きくすることにしたのである。
The inventor pays attention to this point, and as described above, connects the curved pipe section B in each of the branch intake pipes 9, 10, 11, 12 to the upstream curved pipe connecting the rising pipe section C to the chamber 8. B1 and a downstream curved pipe section B2 connected to a lateral pipe section D to each of the intake ports 3, 4, 5, and 6, and a bending radius R2 of the downstream curved pipe section B2 is defined by the upstream curved section. It was decided to make it larger than the radius of the tube section B1.

すなわち、各分岐吸気管路9,10,11,12の湾曲管部Bの
うち下流側湾曲管部B2内における吸気の流速は、前記湾
曲管部Bのうち上流側湾曲管部B1内における吸気の流速
よりも早いから、この吸気流速の早い下流側湾曲管部B2
における大きい湾曲半径R2にすることで、吸気流れ抵抗
の増大を確実に防止できるのである。
In other words, the flow velocity of the intake air in the downstream curved pipe section B2 of the curved pipe sections B of the branch intake pipes 9, 10, 11, 12 is the intake flow rate in the upstream curved pipe section B1 of the curved pipe section B. Is lower than the flow velocity of the downstream curved pipe section B2 where the intake flow velocity is high.
By setting the large curvature radius R2 at, it is possible to reliably prevent the intake flow resistance from increasing.

〔発明の効果〕〔The invention's effect〕

従って、本発明によると、各分岐吸気管路における吸
気の流れ抵抗を、各分岐吸気管路に所定の流さ寸法を確
保した状態で、低減することができるから、慣性過給式
の吸気マニホールドを大型することなく、吸気流れ抵抗
による出力の低下を確実に防止できる効果を有する。
Therefore, according to the present invention, the flow resistance of intake air in each branch intake pipe can be reduced in a state where a predetermined flow size is secured in each branch intake pipe, so that an inertia supercharged intake manifold is provided. This has the effect of reliably preventing a reduction in output due to intake flow resistance without increasing the size.

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

第1図及び第2図は本発明の実施例を示し、第1図は平
面図、第2図は第1図のII−II視断面図、第3図は第2
図と同じ箇所の断面図で従来のものを示す図である。 1……内燃機関、A1,A2,A3,A4……気筒、2……シリン
ダヘッド、3,4,5,6……吸気ポート、7……吸気マニホ
ールド、8……チャンバー、9,10,11,12……分岐吸気管
路、B……湾曲管部、B1……上流側湾曲管部、B2……下
流側湾曲管部、C……立上り部、D……横向き部。
1 and 2 show an embodiment of the present invention. FIG. 1 is a plan view, FIG. 2 is a sectional view taken along the line II-II of FIG. 1, and FIG.
It is a figure which shows the conventional thing in the sectional view of the same location as a figure. 1 ... internal combustion engine, A1, A2, A3, A4 ... cylinder, 2 ... cylinder head, 3, 4, 5, 6 ... intake port, 7 ... intake manifold, 8 ... chamber, 9, 10, 11, 12 ... branch intake pipe, B ... curved pipe section, B1 ... upstream curved pipe section, B2 ... downstream curved pipe section, C ... rising section, D ... sideways section.

───────────────────────────────────────────────────── フロントページの続き (58)調査した分野(Int.Cl.6,DB名) F02M 35/104 F02B 27/00──────────────────────────────────────────────────続 き Continued on front page (58) Field surveyed (Int. Cl. 6 , DB name) F02M 35/104 F02B 27/00

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】気筒列の方向に延びるチャンバーと、各気
筒における吸気ポートとの間を、各気筒の各々について
独立する分岐吸気管路にて接続し、この各分岐吸気管路
のうち前記吸気ポートに接続する部分を略直線状に延び
る横向き管部に、前記チャンバーに接続する部分を略直
線状に延びる立上り管部に、その間の部分を上向きに直
角よりも大きい角度に湾曲した湾曲管部に構成して成る
吸気マニホールドにおいて、 前記各分岐吸気管路における湾曲管部を、チャンバーへ
の立上り管部に繋がる上流側湾曲管部と、吸気ポートへ
の横向き管部に繋がる下流側湾曲管部とで構成して、前
記下流側湾曲管部における湾曲半径を、前記上流側湾曲
管部における湾曲半径よりも大きくしたことを特徴とす
る内燃機関における吸気マニホールド。
An independent branch intake pipe is connected to each of the cylinders between a chamber extending in the direction of the cylinder row and an intake port of each cylinder. A curved tube portion curved at an angle larger than a right angle, with a portion connected to the port being a substantially straight horizontal tube portion, a portion connected to the chamber being a substantially straight riser tube portion, and a portion therebetween being upwardly curved at an angle larger than a right angle. In the intake manifold, the curved pipe section in each of the branch intake pipes is connected to an upstream curved pipe section connected to a rising pipe section to a chamber, and a downstream curved pipe section connected to a horizontal pipe section to an intake port. Wherein the curvature radius of the downstream curved tube portion is larger than the curvature radius of the upstream curved tube portion.
JP16056990A 1990-06-18 1990-06-18 Intake manifold for internal combustion engine Expired - Fee Related JP2839657B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16056990A JP2839657B2 (en) 1990-06-18 1990-06-18 Intake manifold for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16056990A JP2839657B2 (en) 1990-06-18 1990-06-18 Intake manifold for internal combustion engine

Publications (2)

Publication Number Publication Date
JPH0450430A JPH0450430A (en) 1992-02-19
JP2839657B2 true JP2839657B2 (en) 1998-12-16

Family

ID=15717808

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16056990A Expired - Fee Related JP2839657B2 (en) 1990-06-18 1990-06-18 Intake manifold for internal combustion engine

Country Status (1)

Country Link
JP (1) JP2839657B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100339589C (en) * 2003-10-20 2007-09-26 三菱自动车工业株式会社 Intake manifold

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5855495B2 (en) * 2012-02-29 2016-02-09 愛三工業株式会社 Intake manifold

Cited By (1)

* Cited by examiner, † Cited by third party
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CN100339589C (en) * 2003-10-20 2007-09-26 三菱自动车工业株式会社 Intake manifold

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