JPH0143473Y2 - - Google Patents

Info

Publication number
JPH0143473Y2
JPH0143473Y2 JP6504283U JP6504283U JPH0143473Y2 JP H0143473 Y2 JPH0143473 Y2 JP H0143473Y2 JP 6504283 U JP6504283 U JP 6504283U JP 6504283 U JP6504283 U JP 6504283U JP H0143473 Y2 JPH0143473 Y2 JP H0143473Y2
Authority
JP
Japan
Prior art keywords
spiral
rotary valve
connecting rod
wall surface
valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP6504283U
Other languages
Japanese (ja)
Other versions
JPS59170633U (en
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 filed Critical
Priority to JP6504283U priority Critical patent/JPS59170633U/en
Publication of JPS59170633U publication Critical patent/JPS59170633U/en
Application granted granted Critical
Publication of JPH0143473Y2 publication Critical patent/JPH0143473Y2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)

Description

【考案の詳細な説明】 産業上の利用分野 本考案は内燃機関の吸気制御装置に関する。[Detailed explanation of the idea] Industrial applications The present invention relates to an intake control device for an internal combustion engine.

従来技術 ヘリカル型吸気ポートは通常吸気弁周りに形成
された渦巻部と、この渦巻部に接線状に接続され
かつほぼまつすぐに延びる入口通路部とにより構
成される。このようなヘリカル型吸気ポートを用
いて吸入空気量の少ない機関低速低負荷運転時に
機関燃焼室内に強力な旋回流を発生せしめようと
すると吸気ポート形状が流れ抵抗の大きな形状に
なつてしまうので吸入空気量の多い機関高速高負
荷運転時に充填効率が低下するという問題を生ず
る。このような問題を解決するためにヘリカル型
吸気ポート入口通路部から分岐されてヘリカル型
吸気ポート渦巻部の渦巻終端部に連通する分岐路
をシリンダヘツド内に形成し、分岐路内に夫々ロ
ータリ弁を設けると共に各ロータリ弁の弁軸に取
付けられたアームを共通の連結ロツドにより互に
連結し、この連結ロツドをアクチユエータにより
作動させることによつて機関高速高負荷運転時に
各ロータリ弁を同時に開弁せしめるようにした吸
気制御装置が例えば特開昭57−176320号公報に記
載されているように既に本出願人により提案され
ている。この吸気制御装置を具えた内燃機関では
機関高速高負荷運転時に吸気ポートの入口通路部
内に送り込まれた混合気の一部が分岐路を介して
吸気ポートの渦巻部内に送り込まれるために吸入
空気の流路断面積が増大し、斯くして高い充填効
率を得ることができる。
BACKGROUND OF THE INVENTION A helical intake port typically consists of a spiral formed around an intake valve and an inlet passageway tangentially connected to the spiral and extending substantially straight. If you try to use such a helical intake port to generate a strong swirling flow in the combustion chamber of the engine during low-speed, low-load engine operation with a small amount of intake air, the shape of the intake port will have a large flow resistance. A problem arises in that the filling efficiency decreases when the engine is operated at high speed and under high load with a large amount of air. In order to solve this problem, branch passages are formed in the cylinder head that branch from the helical intake port inlet passage and communicate with the spiral end of the helical intake port spiral part, and a rotary valve is installed in each branch passage. At the same time, the arms attached to the valve stems of each rotary valve are connected to each other by a common connecting rod, and by actuating this connecting rod with an actuator, each rotary valve can be opened at the same time during engine high-speed, high-load operation. An intake air control device designed to reduce the amount of air is already proposed by the present applicant, as described in, for example, Japanese Patent Laid-Open No. 176320/1983. In an internal combustion engine equipped with this intake control device, when the engine is operated at high speed and under high load, a portion of the air-fuel mixture sent into the inlet passage of the intake port is sent into the volute of the intake port via a branch passage. The cross-sectional area of the flow path is increased, thus high filling efficiency can be obtained.

この内燃機関では各気筒の吸気ポートの渦巻部
の渦巻方向が全て同じであり、従つて各ロータリ
弁の弁軸に取付けられたアームの先端部を一本の
共通連結ロツドにより互に連結することによつて
各ロータリ弁を同時に開閉制御することができ
る。しかしながら場合によつては各気筒の吸気ポ
ートをそれらの渦巻部の渦巻方向が互に反対向き
となるように配置しなければならない場合があ
り、このような場合にはロータリ弁の回動すべき
方向が互に逆向きとなるためにもはや一本の共通
連結ロツドを各アームの先端部に単に枢着するこ
とによつてはロータリ弁を同時に制御することは
困難である。
In this internal combustion engine, the spiral direction of the spiral portion of each cylinder's intake port is the same, and therefore the tips of the arms attached to the valve shaft of each rotary valve are interconnected by one common connecting rod. Each rotary valve can be controlled to open and close at the same time. However, in some cases, it may be necessary to arrange the intake ports of each cylinder so that the spiral directions of their spiral parts are opposite to each other, and in such cases, the rotary valve should be rotated. Since the directions are opposite to each other, it is no longer possible to control the rotary valves simultaneously by simply pivoting one common connecting rod to the tip of each arm.

考案の目的 本考案は各気筒の吸気ポートの渦巻部の渦巻方
向が異なる場合において全ロータリ弁を同時に開
閉制御することのできる構造の簡単な吸気制御装
置を提供することにある。
Purpose of the invention The object of the invention is to provide an intake control device with a simple structure that can open and close all rotary valves simultaneously when the spiral directions of the spiral portions of the intake ports of each cylinder are different.

考案の構成 本考案の構成は、吸気弁周りに形成された渦巻
部と、渦巻部に接線状に接続されかつほぼまつす
ぐに延びる入口通路部と、入口通路部から分岐さ
れて渦巻部の渦巻終端部に連通する分岐路とによ
り構成されたヘリカル型吸気ポートを具備し、分
岐路内に分岐路の開閉制御をするロータリ弁を配
置すると共にロータリ弁の弁軸に取付けたアーム
の先端部をアクチユエータに連結し、少なくとも
一対の気筒の渦巻部の渦巻方向が互に逆向きであ
る内燃機関において、一対の気筒に設けられたロ
ータリ弁のアームが各ロータリ弁を結ぶ線に関し
て互に反対向きに延びるように配置され、アクチ
ユエータに連結された連結ロツドをロータリ弁を
結ぶ線に沿つてロータリ弁の上方に配置し、連結
ロツドと直角方向に延びる長穴を形成した突出片
をロータリ弁の上方において連結ロツドからアー
ムと同一方向に突き出してアームの先端部に取付
けられたピンを長穴内に嵌着し、連結ロツドに向
けてピンを押圧するばね部材を連結ロツドに取付
けたことにある。
Structure of the invention The structure of the invention consists of a spiral part formed around the intake valve, an inlet passage part connected tangentially to the spiral part and extending almost straight, and a spiral part branched from the inlet passage part. It is equipped with a helical intake port consisting of a branch passage that communicates with the terminal end, and a rotary valve that controls the opening and closing of the branch passage is placed in the branch passage, and the tip of an arm attached to the valve shaft of the rotary valve is installed in the branch passage. In an internal combustion engine connected to an actuator and in which the spiral directions of the spiral parts of at least a pair of cylinders are opposite to each other, the arms of the rotary valves provided in the pair of cylinders are connected to the rotary valves in opposite directions with respect to a line connecting each rotary valve. A connecting rod connected to the actuator is placed above the rotary valve along a line connecting the rotary valves, and a protruding piece having a long hole extending perpendicularly to the connecting rod is placed above the rotary valve. A pin that protrudes from the connecting rod in the same direction as the arm and is attached to the tip of the arm is fitted into an elongated hole, and a spring member that presses the pin toward the connecting rod is attached to the connecting rod.

実施例 第1図および第2図を参照すると、1はシリン
ダブロツク、2はシリンダブロツク1内で往復運
動するピストン、3はシリンダブロツク1上に固
締されたシリンダヘツド、4はピストン2とシリ
ンダヘツド3間に形成された燃焼室、5は吸気
弁、6はシリンダヘツド3内に形成されたヘリカ
ル型吸気ポート、7は排気弁、8はシリンダヘツ
ド3内に形成された排気ポート、9は燃焼室4内
に配置された点火栓、10は吸気弁5のステム5
aを案内するステムガイドを夫々示す。第1図並
びに第2図に示されるように吸気ポート6の上壁
面11上には下方に突出する隔壁12が一体形成
され、この隔壁12によつて渦巻部Bと、この渦
巻部Bに接線状に接続された入口通路部Aからな
るヘリカル型吸気ポート6が形成される。この隔
壁12は入口通路部A内から吸気弁5のステムガ
イド10の周囲まで延びており、第2図からわか
るようにこの隔壁12の根元部の巾Lは入口通路
部Aからステムガイド10に近づくにつれて徐々
に広くなる。隔壁12は吸気ポート6の入口開口
6aに最も近い側に位置する先端部13を有し、
更に隔壁12は第2図においてこの先端部13か
ら反時計回りにステムガイド10まで延びる第1
側壁面14aと、先端部13から時計回りにステ
ムガイド10まで延びる第2側壁面14bとを有
する。第1側壁面14aは先端部13からステム
ガイド10の側方を通つて渦巻部Bの側壁面15
の近傍まで延びて渦巻部側壁面15との間に狭窄
部16を形成する。次いで第1側壁面14aは渦
巻部側壁面15から徐々に間隔を隔てるように弯
曲しつつステムガイド10まで延びる。一方、第
2側壁面14bは先端部13からステムガイド1
0までほぼまつすぐに延びる。
Embodiment Referring to FIGS. 1 and 2, 1 is a cylinder block, 2 is a piston reciprocating within the cylinder block 1, 3 is a cylinder head fixed on the cylinder block 1, and 4 is a piston 2 and a cylinder. A combustion chamber is formed between the heads 3, 5 is an intake valve, 6 is a helical intake port formed in the cylinder head 3, 7 is an exhaust valve, 8 is an exhaust port formed in the cylinder head 3, and 9 is a helical intake port formed in the cylinder head 3. A spark plug placed in the combustion chamber 4; 10 is a stem 5 of an intake valve 5;
The stem guides guiding a are shown respectively. As shown in FIGS. 1 and 2, a partition wall 12 projecting downward is integrally formed on the upper wall surface 11 of the intake port 6, and this partition wall 12 forms a spiral portion B and a tangent line to the spiral portion B. A helical intake port 6 is formed of inlet passages A connected in a shape. This partition wall 12 extends from inside the inlet passage part A to around the stem guide 10 of the intake valve 5, and as can be seen from FIG. It gradually becomes wider as you approach. The partition wall 12 has a tip 13 located on the side closest to the inlet opening 6a of the intake port 6,
Further, the partition wall 12 has a first section extending counterclockwise from the distal end 13 to the stem guide 10 in FIG.
It has a side wall surface 14a and a second side wall surface 14b extending clockwise from the distal end portion 13 to the stem guide 10. The first side wall surface 14a passes from the distal end portion 13 to the side of the stem guide 10 to the side wall surface 15 of the spiral portion B.
The constricted portion 16 is formed between the spiral portion side wall surface 15 and the spiral portion side wall surface 15 . Next, the first side wall surface 14a extends to the stem guide 10 while being curved so as to be gradually spaced apart from the spiral portion side wall surface 15. On the other hand, the second side wall surface 14b extends from the tip 13 to the stem guide 1.
It increases almost immediately to 0.

第1図から第9図を参照すると、入口通路部A
の側壁面17,18はほぼ垂直配置され、一方、
入口通路部Aの上壁面19は渦巻部Bに向けて
徐々に下降する。入口通路部Aの側壁面17は渦
巻部Bの側壁面15に滑らかに接続され、入口通
路部Aの上壁面19は渦巻部Bの上壁面20に滑
らかに接続される。渦巻部Bの上壁面20は滑巻
部Bと入口通路部Aの接続部から狭窄部16に向
けて下隣しつつ徐々に巾を狭め、次いで狭窄部1
6を通過すると徐々に巾を広げる。一方、入口通
路部Aの下壁面21は第5図に示すように入口開
口6aの近傍においてはその全体がほぼ水平をな
しており、側壁面17に隣接する底壁面部分21
aは第8図に示すように渦巻部Bに近づくに従つ
て隆起して傾斜面を形成する。この傾斜底壁面部
分21aの傾斜角は渦巻部Bに近づくに従つて隆
起して傾斜面を形成する。この傾斜底壁面部分2
1aの傾斜角は渦巻部Bに近づくにつれて徐々に
大きくなる。
Referring to FIGS. 1 to 9, the inlet passage section A
The side wall surfaces 17, 18 of are arranged substantially vertically, while
The upper wall surface 19 of the inlet passage section A gradually descends toward the spiral section B. The side wall surface 17 of the inlet passage section A is smoothly connected to the side wall surface 15 of the spiral section B, and the upper wall surface 19 of the entrance passage section A is smoothly connected to the upper wall surface 20 of the spiral section B. The upper wall surface 20 of the spiral part B gradually narrows in width from the connecting part of the sliding part B and the inlet passage part A toward the narrowing part 16 while adjoining the narrowing part 16.
After passing 6, the width gradually increases. On the other hand, as shown in FIG.
As shown in FIG. 8, as it approaches the spiral portion B, the portion a is raised to form an inclined surface. The angle of inclination of this inclined bottom wall surface portion 21a rises as it approaches the spiral portion B, forming an inclined surface. This inclined bottom wall part 2
The inclination angle of 1a gradually increases as it approaches the spiral portion B.

一方、隔壁12の第1側壁面14aはわずかば
かり傾斜した下向きの傾斜面からなり、第2側壁
面14bはほぼ垂直をなす。隔壁12の底壁面2
2は先端部13からステムガイド10に向かうに
従つて入口通路部Aの上壁面11との間隔が次第
に大きくなるように入口通路部Aから渦巻部Bに
向けてわずかばかり弯曲しつつ下降する。隔壁1
2の底壁面22上には第4図のハツチングで示す
領域に底壁面22から下方に突出するリブ23が
形成され、このリブ23の底面および底壁面22
はわずかばかり弯曲した傾斜面を形成する。
On the other hand, the first side wall surface 14a of the partition wall 12 is a slightly downwardly inclined surface, and the second side wall surface 14b is substantially vertical. Bottom wall surface 2 of partition wall 12
2 descends from the inlet passage A toward the spiral part B while being slightly curved so that the distance from the upper wall surface 11 of the inlet passage A gradually increases as it goes from the tip 13 to the stem guide 10. Bulkhead 1
A rib 23 protruding downward from the bottom wall surface 22 is formed on the bottom wall surface 22 of No. 2 in the area indicated by hatching in FIG.
forms a slightly curved slope.

一方、シリンダヘツド3内には渦巻部Bの渦巻
後端部Cと入口通路部Aとを連通する分岐路24
が形成され、この分岐路24の入口部にロータリ
弁25が配置される。この分岐路24は隔壁12
によつて入口通路部Aから分離されており、分岐
路24の下側空間全体が入口通路部Aに連通して
いる。分岐路24の上壁面26はほぼ一様な巾を
有し、渦巻終端部Cに向けて徐々に下降して渦巻
部Bの上壁面20に滑らかに接続される。隔壁1
2の第2側壁面14bに対面する分岐路24の側
壁面27はほぼ垂直をなし、更にこの側壁面27
はほぼ入口通路部Aの側壁面18の延長上に位置
する。なお、第1図からわかるように隔壁12上
に形成されたリブ23はロータリ弁25の近傍か
ら吸気弁5に向けて延びている。
On the other hand, a branch passage 24 is provided in the cylinder head 3 that communicates the spiral rear end C of the spiral section B with the inlet passage section A.
is formed, and a rotary valve 25 is disposed at the inlet of this branch path 24. This branch path 24 is connected to the partition wall 12
The branch passageway 24 is separated from the inlet passageway A by , and the entire lower space of the branch passage 24 communicates with the inlet passageway A. The upper wall surface 26 of the branch passage 24 has a substantially uniform width, gradually descends toward the spiral terminal end C, and is smoothly connected to the upper wall surface 20 of the spiral section B. Bulkhead 1
The side wall surface 27 of the branch path 24 facing the second side wall surface 14b of No. 2 is substantially perpendicular, and furthermore, this side wall surface 27
is located approximately on an extension of the side wall surface 18 of the inlet passage section A. As can be seen from FIG. 1, the rib 23 formed on the partition wall 12 extends from the vicinity of the rotary valve 25 toward the intake valve 5.

第10図に示されるようにロータリ弁25はロ
ータリ弁ホルダ28と、ロータリ弁ホルダ28内
において回転可能に支持された弁軸29とにより
構成され、このロータリ弁ホルダ28はシリンダ
ヘツド3に穿設されたねじ孔30内に螺着され
る。弁軸29の下端部には薄板状の弁体31が一
体形成され、第1図に示されるようにこの弁体3
1は分岐路24の上壁面26から底壁面21まで
延びる。一方、弁軸29の上端部にはアーム32
が固定される。また、弁軸29の外周面上にはリ
ング溝33が形成され、このリング溝33内には
E字型位置決めリング34が嵌め込まれる。更に
ロータリ弁ホルダ28の上端部にはシール部材3
5が嵌着され、このシール部材35によつて弁軸
29のシール作用が行われる。
As shown in FIG. 10, the rotary valve 25 is composed of a rotary valve holder 28 and a valve shaft 29 rotatably supported within the rotary valve holder 28. The screw hole 30 is screwed into the screw hole 30. A thin plate-shaped valve body 31 is integrally formed at the lower end of the valve shaft 29, and as shown in FIG.
1 extends from the top wall surface 26 of the branch path 24 to the bottom wall surface 21. On the other hand, an arm 32 is attached to the upper end of the valve shaft 29.
is fixed. Further, a ring groove 33 is formed on the outer peripheral surface of the valve shaft 29, and an E-shaped positioning ring 34 is fitted into the ring groove 33. Furthermore, a sealing member 3 is provided at the upper end of the rotary valve holder 28.
5 is fitted, and this sealing member 35 performs a sealing action on the valve shaft 29.

第11図を参照すると、内燃機関は直列配置さ
れた4つの気筒、即ち1番気筒1,2番気筒、
3番気筒および4番気筒を有し、各気筒の吸
気ポート6は夫々対応する吸気ホニホルド枝管4
0a,40b,40c,40dに連結される。第
11図からわかるようにこの実施例では1番気筒
と3番気筒の渦巻部Bの渦巻方向が2番気筒
と4番気筒の渦巻部Bの渦巻方向と逆向きに
なつており、従つて1番気筒と3番気筒のロ
ータリ弁25の回動すべき方向と2番気筒と4
番気筒のロータリ弁25の回動すべき方向は逆
向きになる。各気筒のロータリ弁25は一直線上
に配置され、1番気筒と3番気筒のロータリ
弁25のアーム32は全ロータリ弁25の回転軸
線を結ぶ線に関して2番気筒と4番気筒のロ
ータリ弁25のアーム32と反対側に延びてい
る。各ロータリ弁25の上方には各ロータリ弁2
5を結ぶ線に沿つて延びる連結ロツド41が配置
され、この連結ロツド41の一端部はアクチユエ
ータ42の制御ロツド43に連結される。アクチ
ユエータ42はダイアフラム44によつて分離さ
れた負圧室45と大気圧室46を有し、ダイアフ
ラム44には制御ロツド43が固着される。負圧
室45内にはダイアフラム押圧用圧縮ばね47が
挿入され、この負圧室45は絞り48および負圧
導管49を介して吸気マニホルド枝管40aに連
結される。一方、第11図および第12図に示す
ように各ロータリ弁25の上方において連結ロツ
ド41に突出片50が一体形成され、これらの各
突出片50は対応するロータリ弁25のアーム3
2と同一方向に突出する。各突出片50は連結ロ
ツド41に対して直角方向に延びる長穴51を有
し、この長穴51内にアーム32の先端部に取付
けられたピン52が嵌着される。このピン52は
第10図および第13図に示されるように基部5
2aと、基部52aよりは径の小さな大径部52
bと、大径部52bよりも径の小さな小径部52
cと、拡大頭部52dからなり、長穴51内には
大径部52bが長穴51の軸線方向に摺動可能に
嵌合せしめられる。一方、各突出片50に対して
夫々板ばね部材53が設けられ、各板ばね部材5
3の一端部はリベツト54によつて連結ロツド4
1に固定される。一方、各板ばね部材53の自由
先端部55は円弧状に形成され、この円弧状先端
部55がピン52の小径部52cと係合する。従
つて各ピン52は板ばね部材53によつて常時連
結ロツド41に向けて押圧され、その結果各ピン
52は長穴51の一側内壁面上に押付けられるの
でピン52が長穴51内でガタつくのを阻止する
ことができる。
Referring to FIG. 11, the internal combustion engine has four cylinders arranged in series, namely, the first cylinder, the second cylinder,
It has a No. 3 cylinder and a No. 4 cylinder, and the intake port 6 of each cylinder is connected to the corresponding intake Honifold branch pipe 4.
0a, 40b, 40c, and 40d. As can be seen from FIG. 11, in this embodiment, the spiral direction of the spiral portion B of the No. 1 and No. 3 cylinders is opposite to the spiral direction of the spiral portion B of the No. 2 and No. 4 cylinders. The direction in which the rotary valves 25 of the 1st and 3rd cylinders should rotate and the 2nd and 4th cylinders
The rotary valve 25 of the numbered cylinder should rotate in the opposite direction. The rotary valves 25 of each cylinder are arranged in a straight line, and the arms 32 of the rotary valves 25 of the first and third cylinders are connected to the rotary valves 25 of the second and fourth cylinders with respect to the line connecting the rotation axes of all the rotary valves 25. The arm 32 extends on the opposite side. Each rotary valve 2 is provided above each rotary valve 25.
A connecting rod 41 is disposed extending along a line connecting the actuators 5 to 5, and one end of the connecting rod 41 is connected to a control rod 43 of an actuator 42. The actuator 42 has a negative pressure chamber 45 and an atmospheric pressure chamber 46 separated by a diaphragm 44, to which a control rod 43 is secured. A compression spring 47 for pressing the diaphragm is inserted into the negative pressure chamber 45, and the negative pressure chamber 45 is connected to the intake manifold branch pipe 40a via a throttle 48 and a negative pressure conduit 49. On the other hand, as shown in FIGS. 11 and 12, a protruding piece 50 is integrally formed on the connecting rod 41 above each rotary valve 25, and each of these protruding pieces 50 connects to the arm 3 of the corresponding rotary valve 25.
Projects in the same direction as 2. Each projecting piece 50 has an elongated hole 51 extending perpendicularly to the connecting rod 41, into which a pin 52 attached to the tip of the arm 32 is fitted. This pin 52 is attached to the base 5 as shown in FIGS. 10 and 13.
2a, and a large diameter portion 52 having a smaller diameter than the base portion 52a.
b, and a small diameter portion 52 having a smaller diameter than the large diameter portion 52b.
c and an enlarged head 52d, and a large diameter portion 52b is fitted into the elongated hole 51 so as to be slidable in the axial direction of the elongated hole 51. On the other hand, a leaf spring member 53 is provided for each protruding piece 50, and each leaf spring member 5
One end of 3 is connected to the connecting rod 4 by a rivet 54.
Fixed to 1. On the other hand, the free tip portion 55 of each leaf spring member 53 is formed in an arc shape, and this arcuate tip portion 55 engages with the small diameter portion 52c of the pin 52. Therefore, each pin 52 is constantly pressed toward the connecting rod 41 by the leaf spring member 53, and as a result, each pin 52 is pressed onto the inner wall surface of one side of the elongated hole 51, so that the pin 52 is not pushed inside the elongated hole 51. It can prevent rattling.

機関低負荷運転時には負圧室45内に大きな負
圧が発生するためにダイアフラム44は圧縮ばね
47に抗して負圧室45側に移動し、その結果1
番気筒および3番気筒のロータリ弁25が反
時計回りに回動し、同時に2番気筒および4番
気筒のロータリ弁25が時計回りに回動せしめ
られて各ロータリ弁25が対応する分岐路24を
閉鎖する。一方、機関高負荷運転時には負圧室4
5内の負圧が小さくなるためにダイアフラム44
は圧縮ばね47のばね力により大気圧室46側に
移動する。その結果、1番気筒および3番気筒
のロータリ弁25が時計回りに回動し、2番気
筒および4番気筒のロータリ弁25が反時計
回りに回動して各ロータリ弁25が対応する分岐
路24を全開する。なお、このようにロータリ弁
25が回動せしめられる間、各ピン52は板ばね
部材53により押圧されつつ長穴51内に摺動
し、各ピン52は円弧状の径路に沿つて移動する
ことがわかる。
During low engine load operation, a large negative pressure is generated in the negative pressure chamber 45, so the diaphragm 44 moves toward the negative pressure chamber 45 against the compression spring 47, and as a result, 1
The rotary valves 25 of the No. 2 and No. 3 cylinders are rotated counterclockwise, and at the same time, the rotary valves 25 of the No. 2 and No. 4 cylinders are rotated clockwise. will be closed. On the other hand, during high engine load operation, the negative pressure chamber 4
diaphragm 44 because the negative pressure inside 5 is reduced.
is moved toward the atmospheric pressure chamber 46 by the spring force of the compression spring 47. As a result, the rotary valves 25 of the first and third cylinders rotate clockwise, the rotary valves 25 of the second and fourth cylinders rotate counterclockwise, and each rotary valve 25 branches into a corresponding branch. Road 24 is fully opened. Note that while the rotary valve 25 is rotated in this manner, each pin 52 slides into the elongated hole 51 while being pressed by the leaf spring member 53, and each pin 52 moves along an arcuate path. I understand.

上述したように吸入空気量が少ない機関低負荷
運転時にはロータリ弁25が分岐路24を閉鎖し
ている。このとき、入口通路部A内に送り込まれ
た混合気の一部は上壁面19,20に沿つて進
み、残りの混合気のうちの一部の混合気はロータ
リ弁25に衝突して入口通路部Aの側壁面17の
方へ向きを変えた後に渦巻部Bの側壁面15に沿
つて進む。前述したように上壁面19,20の巾
は狭窄部16に近づくに従つて次第に狭くなるた
めに上壁面19,20に沿つて流れる混合気の流
路は次第に狭まり、斯くして上壁面19,20に
沿う混合気流は次第に増速される。更に、前述し
たように隔壁12の第1側壁面14aは渦巻部B
の側壁面15の近傍まで延びているので上壁面1
9,20に沿つて進む混合気流は渦巻部Bの側壁
面15上に押しやられ、次いで側壁面15に沿つ
て進むために渦巻部B内には強力な旋回流が発生
せしめられる。次いで混合気は旋回しつつ吸気弁
5とその弁座間に形成される間隙を通つて燃焼室
4内に流入して燃焼室4内に強力な旋回流を発生
せしめる。
As mentioned above, the rotary valve 25 closes the branch passage 24 when the engine is operating at low load with a small amount of intake air. At this time, part of the air-fuel mixture sent into the inlet passage A advances along the upper wall surfaces 19 and 20, and part of the remaining air-fuel mixture collides with the rotary valve 25 and flows into the inlet passage. After changing its direction toward the side wall surface 17 of section A, it proceeds along the side wall surface 15 of spiral section B. As described above, the widths of the upper wall surfaces 19 and 20 gradually become narrower as they approach the narrowed portion 16, so that the flow path for the air-fuel mixture flowing along the upper wall surfaces 19 and 20 gradually narrows. The air mixture flow along 20 is gradually accelerated. Further, as described above, the first side wall surface 14a of the partition wall 12 has the spiral portion B.
Since it extends to the vicinity of the side wall surface 15, the upper wall surface 1
The air mixture flowing along the spiral portions 9 and 20 is forced onto the side wall surface 15 of the spiral portion B, and then proceeds along the side wall surface 15, so that a strong swirling flow is generated within the spiral portion B. Next, the air-fuel mixture swirls and flows into the combustion chamber 4 through the gap formed between the intake valve 5 and its valve seat, generating a strong swirling flow within the combustion chamber 4.

一方、吸入空気量が多い機関高速高負荷運転時
にはロータリ弁25が開弁するので入口通路部A
内に送り込まれた混合気は大別すると3つの流れ
に分流される。即ち、第1の流れは隔壁12の第
1側壁面14aと入口通路部Aの側壁面17間に
流入し、次いで渦巻部Bの上壁面20に沿つて旋
回しつつ流れる混合気流であり、第2の流れは分
岐路24を介して渦巻部B内に流入する混合気流
であり、第3の流れは入口通路部Aの底壁面21
に沿つて渦巻部B内に流入する混合気流である。
分岐路24の流れ抵抗は第1側壁面14aと側壁
面17間の流れ抵抗に比べて小さく、従つて第2
の混合気流の方が第1の混合気流よりも多くな
る。更に、渦巻部B内を旋回しつつ流れる第1混
合気流の流れ方向は第2混合気流によつて下向き
に偏向され、斯くして第1混合気流の旋回力が弱
められることになる。このように流れ抵抗の小さ
な分岐路24からの混合気流が増大し、更に第1
混合気流の流れ方向が下向きに偏向されので高い
充填効率が得られるようになる。また、前述した
ように隔壁21の底壁面は下向きの傾斜面から形
成されているので第3の混合気流はこの傾斜面に
案内されて流れ方向が下向きに偏向され、斯くし
て更に高い充填効率が得られることになる。
On the other hand, when the engine is operated at high speed and under high load with a large amount of intake air, the rotary valve 25 opens, so the inlet passage A
The air-fuel mixture sent into the tank is divided into three main streams. That is, the first flow is a mixed gas flow that flows between the first side wall surface 14a of the partition wall 12 and the side wall surface 17 of the inlet passage section A, and then flows while swirling along the upper wall surface 20 of the spiral section B. The second flow is a mixed air flow that flows into the swirl part B via the branch passage 24, and the third flow is a mixture flow that flows into the bottom wall surface 21 of the inlet passage part A.
This is a mixed air flow that flows into the spiral part B along .
The flow resistance of the branch path 24 is smaller than the flow resistance between the first side wall surface 14a and the side wall surface 17, and therefore
The number of mixed air flows is larger than that of the first mixed air flow. Further, the flow direction of the first air mixture flowing while swirling in the swirl portion B is deflected downward by the second air mixture, thus weakening the swirling force of the first air mixture. In this way, the mixed air flow from the branch passage 24 with low flow resistance increases, and furthermore, the first
Since the flow direction of the mixed gas flow is deflected downward, high filling efficiency can be obtained. Further, as mentioned above, since the bottom wall surface of the partition wall 21 is formed from a downwardly inclined surface, the third air mixture flow is guided by this inclined surface and the flow direction is deflected downward, thus achieving even higher filling efficiency. will be obtained.

考案の効果 各気筒における吸気ポートの渦巻部の渦巻方向
が互に逆向きになつている場合であつても1個の
連結ロツドを用いた簡単な構造によりロータリ弁
を逆向きに同時に回動せしめることができる。ま
た、ピンが板ばね部材によつて常時長穴の一側内
壁面上に押圧されているのでガタが生ずることは
なく、斯くしてロータリ弁を予め定められた開度
位置に正確に保持することができる。
Effect of the invention Even if the spiral directions of the spiral portions of the intake ports in each cylinder are opposite to each other, the rotary valves can be simultaneously rotated in opposite directions using a simple structure using one connecting rod. be able to. In addition, since the pin is constantly pressed against the inner wall surface of one side of the elongated hole by the leaf spring member, no looseness occurs, thus accurately holding the rotary valve at a predetermined opening position. be able to.

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

第1図は第2図の−線に沿つてみた本考案
に係る内燃機関の側面断面図、第2図は第1図の
−線に沿つてみた平面断面図、第3図は本考
案によるヘリカル型吸気ポートの形状を図解的に
示す側面図、第4図はヘリカル型吸気ポートの形
状を図解的に示す平面図、第5図は第3図および
第4図の−線に沿つてみた断面図、第6図は
第3図および第4図の−線に沿つてみた断面
図、第7図は第3図および第4図の−線に沿
つてみた断面図、第8図は第3図および第4図の
−線に沿つてみた断面図、第9図は第3図お
よび第4図の−線に沿つてみた断面図、第1
0図はロータリ弁の側面断面図、第11図は内燃
機関の平面図、第12図は第11図の2番気筒お
よび3番気筒周りの拡大図、第13図はロータリ
弁のアームと連結ロツドの連結状態を示す斜視図
である。 4……燃焼室、6……ヘリカル型吸気ポート、
12……隔壁、24……分岐路、25……ロータ
リ弁、32……アーム、41……連結ロツド、4
2……アクチユエータ、50……突出片、51…
…長穴、52……ピン、53……板ばね部材。
Fig. 1 is a side sectional view of the internal combustion engine according to the present invention taken along the - line in Fig. 2, Fig. 2 is a plan sectional view taken along the - line in Fig. 1, and Fig. 3 is a sectional view according to the present invention taken along the - line in Fig. 2. FIG. 4 is a side view schematically showing the shape of the helical intake port, FIG. 4 is a plan view schematically showing the shape of the helical intake port, and FIG. 5 is a view taken along the - line in FIGS. 3 and 4. 6 is a sectional view taken along the - line in FIGS. 3 and 4, FIG. 7 is a sectional view taken along the - line in FIGS. 3 and 4, and FIG. 8 is a sectional view taken along the - line in FIGS. 3 and 4, FIG. 9 is a sectional view taken along the line - in FIGS. 3 and 4, and FIG.
Figure 0 is a side sectional view of the rotary valve, Figure 11 is a plan view of the internal combustion engine, Figure 12 is an enlarged view of the 2nd and 3rd cylinders in Figure 11, and Figure 13 is the rotary valve arm and connection. FIG. 3 is a perspective view showing the connected state of the rods. 4... Combustion chamber, 6... Helical intake port,
12... Bulkhead, 24... Branching path, 25... Rotary valve, 32... Arm, 41... Connection rod, 4
2... Actuator, 50... Projecting piece, 51...
...Elongated hole, 52...Pin, 53...Plate spring member.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 吸気弁周りに形成された渦巻部と、該渦巻部に
接線状に接続されかつほぼまつすぐに延びる入口
通路部と、該入口通路部から分岐されて該渦巻部
の渦巻終端部に連通する分岐路とにより構成され
たヘリカル型吸気ポートを具備し、該分岐路内に
分岐路の開閉制御をするロータリ弁を配置すると
共に該ロータリ弁の弁軸に取付けたアームの先端
部をアクチユエータに連結し、少なくとも一対の
気筒の該渦巻部の渦巻方向が互に逆向きである内
燃機関において、上記一対の気筒に設けられたロ
ータリ弁のアームが各ロータリ弁を結ぶ線に関し
て互に反対向きに延びるように配置され、上記ア
クチユエータに連結された連結ロツドを上記ロー
タリ弁を結ぶ線に沿つてロータリ弁の上方に配置
し、該連結ロツドと直角方向に延びる長穴を形成
した突出片をロータリ弁の上方において連結ロツ
ドからアームと同一方向に突き出してアームの先
端部に取付けられたピンを該長穴内に嵌着し、連
結ロツドに向けて該ピンを押圧するばね部材を連
結ロツドに取付けた内燃機関の吸気制御装置。
A spiral portion formed around the intake valve, an inlet passage portion connected tangentially to the spiral portion and extending almost straight, and a branch branching from the inlet passage portion and communicating with a spiral end portion of the spiral portion. A rotary valve for controlling the opening and closing of the branch passage is disposed within the branch passage, and the tip of an arm attached to the valve shaft of the rotary valve is connected to an actuator. In an internal combustion engine in which the spiral directions of the spiral portions of at least one pair of cylinders are opposite to each other, the arms of the rotary valves provided in the pair of cylinders extend in opposite directions with respect to a line connecting each rotary valve. A connecting rod connected to the actuator is placed above the rotary valve along a line connecting the rotary valves, and a protruding piece having a long hole extending perpendicularly to the connecting rod is placed above the rotary valve. An internal combustion engine in which a pin protruding from the connecting rod in the same direction as the arm and attached to the tip of the arm is fitted into the elongated hole, and a spring member is attached to the connecting rod to press the pin toward the connecting rod. Intake control device.
JP6504283U 1983-05-02 1983-05-02 Internal combustion engine intake control device Granted JPS59170633U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6504283U JPS59170633U (en) 1983-05-02 1983-05-02 Internal combustion engine intake control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6504283U JPS59170633U (en) 1983-05-02 1983-05-02 Internal combustion engine intake control device

Publications (2)

Publication Number Publication Date
JPS59170633U JPS59170633U (en) 1984-11-15
JPH0143473Y2 true JPH0143473Y2 (en) 1989-12-18

Family

ID=30195234

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6504283U Granted JPS59170633U (en) 1983-05-02 1983-05-02 Internal combustion engine intake control device

Country Status (1)

Country Link
JP (1) JPS59170633U (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0531234Y2 (en) * 1987-04-17 1993-08-11

Also Published As

Publication number Publication date
JPS59170633U (en) 1984-11-15

Similar Documents

Publication Publication Date Title
JPS6032009B2 (en) Helical intake port
JPS6023468Y2 (en) Flow path control device for helical intake port
JPS6238533B2 (en)
JPH0143473Y2 (en)
JPS6238537B2 (en)
JPH0143472Y2 (en)
JPS6236139B2 (en)
US4516544A (en) Helically-shaped intake port of an internal-combustion engine
JPS609378Y2 (en) Flow path control device for helical intake port
JPS6226589Y2 (en)
JPH032682Y2 (en)
JPH0133791Y2 (en)
JPS6231619Y2 (en)
JPS6239672B2 (en)
JPS6229624Y2 (en)
JPS6335166Y2 (en)
JPS6236138B2 (en)
JPS6021469Y2 (en) Helical intake port
JPS6321777Y2 (en)
JPH029070Y2 (en)
JPS6021470Y2 (en) Helical intake port
JPS6238534B2 (en)
JPS6229623Y2 (en)
JPH0244022Y2 (en)
JPS6236136B2 (en)