JPH0143472Y2 - - Google Patents
Info
- Publication number
- JPH0143472Y2 JPH0143472Y2 JP6504183U JP6504183U JPH0143472Y2 JP H0143472 Y2 JPH0143472 Y2 JP H0143472Y2 JP 6504183 U JP6504183 U JP 6504183U JP 6504183 U JP6504183 U JP 6504183U JP H0143472 Y2 JPH0143472 Y2 JP H0143472Y2
- Authority
- JP
- Japan
- Prior art keywords
- connecting rod
- spiral
- wall surface
- valve
- rotary
- 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
Links
- 238000002485 combustion reaction Methods 0.000 claims description 15
- 239000000203 mixture Substances 0.000 description 12
- 238000005192 partition Methods 0.000 description 11
- 239000000446 fuel Substances 0.000 description 6
- 238000013459 approach Methods 0.000 description 4
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000012447 hatching Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
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
閉制御することが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。OBJECT OF THE INVENTION The object of the present 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部とによ
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、ロータ
リ弁を結ぶ線の両側に互にほぼ平行に延びる第1
連結ロツドと第2連結ロツドを配置し、第1連結
ロツドの中間部を一方のアームの先端部に枢着す
ると共に第2連結ロツドの一端部を他方のアーム
の先端部に枢着し、更に第1連結ロツドの一端部
をアクチユエータに連結し、第1連結ロツドの他
端部をピンと長穴からなる遊合連結機構を介して
第2連結ロツドの他端部に連結したことにある。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 part 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 the 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 first line extending substantially parallel to each other on both sides of a line connecting the rotary valves;
arranging a connecting rod and a second connecting rod, pivotally connecting an intermediate portion of the first connecting rod to the tip of one arm, and pivotally connecting one end of the second connecting rod to the tip of the other arm; One end of the first connecting rod is connected to the actuator, and the other end of the first connecting rod is connected to the other end of the second connecting rod via a loose connecting mechanism consisting of a pin and an elongated hole.
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5a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1
1上には下方に突出する隔壁12が一体成形さ
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6
a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10
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 formed between the heads 3, 5 an intake valve,
6 is a helical intake port formed in the cylinder head 3, 7 is an exhaust valve, and 8 is a cylinder head 3.
Reference numeral 9 indicates an ignition plug disposed within the combustion chamber 4, and reference numeral 10 indicates a stem guide for guiding the stem 5a of the intake valve 5. As shown in FIGS. 1 and 2, the upper wall surface 1 of the intake port 6
A partition wall 12 projecting downward is integrally molded on the top of the helical intake port 6, which consists of a spiral portion B and an inlet passage portion A tangentially connected to the spiral portion B. be done. 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 is the inlet opening 6 of the intake port 6.
The partition wall 12 further includes a first side wall surface 14a extending counterclockwise from the tip 13 to the stem guide 10 in FIG. 2, and a first side wall surface 14a extending clockwise from the tip 13 in FIG. and a second side wall surface 14b extending to the stem guide 10. The first side wall surface 14a extends from the distal end portion 13 through the side of the stem guide 10 to the vicinity of the side wall surface 15 of the spiral portion B, and forms a narrow portion 16 between the first side wall surface 14a 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
The side wall surface 14b extends from the tip 13 to the stem guide 10.
It extends almost immediately.
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は渦巻
部Bと入口通路部Aの接続部から狭窄部16に向
けて下降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 while descending from the connection part between the spiral part B and the inlet passage part A toward the narrowing part 16, and then gradually narrows in width.
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, it rises to form an inclined surface. The angle of inclination of this inclined bottom wall surface portion 21a 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
終端部Cと入口通路部Aとを連結する分岐路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, in the cylinder head 3 there is a branch passage 24 connecting the spiral end C of the spiral portion B and the inlet passage A.
is formed, and a rotary valve 25 is disposed at the inlet of this branch passage 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弁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35
が嵌着され、このシール部材35によつて弁軸2
9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 rotary valve holder valve 28 is bored into the cylinder head 3. It is screwed into the provided 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 35 is provided at the upper end of the rotary valve holder 28.
is fitted, and the valve shaft 2 is fitted by this seal member 35.
9 sealing action is performed.
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、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マニホルド枝管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2番気筒の渦巻部Bの渦巻方向が3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2番気筒のロ
ータリ弁25の回動すべき方向と3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2番気筒のロータリ
弁25のアーム32は全ロータリ弁の回転軸線を
結ぶ線に関して3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。1
番気筒および2番気筒のアーム32の先端部
は第1連結ロツド41に枢着され、3番気筒お
よび4番気筒のアーム32の先端部は第2連結
ロツド42に枢着される。従つて第1連結ロツド
41と第2連結ロツド42は全ロータリ弁25を
結ぶ線の両側に互に平行をなして配置される。第
1連結ロツド41の一端部はリンク43を介して
アクチユエータ44の制御ロツド45に連結され
る。アクチユエータ44はダイアフラム46によ
つて分離された負圧室47と大気圧室48を有
し、ダイアフラム46には制御ロツド45が固着
される。負圧室47内にはダイアフラム押圧用圧
縮ばね49が挿入され、この負圧室47は絞り5
0および負圧導管51を介して吸気マニホルド枝
管40aに連結される。一方、第1連結ロツド4
1の他端部は遊合連結機構52を介して第2連結
ロツド42に連結される。第11図および第12
図に示すように第2連結ロツド42の端部には平
板部53が一体的に形成され、遊合連結機構52
は平板部53上に形成されかつ第2連結ロツド4
2に対して直角方向に延びる長穴54と、第1連
結ロツド41の端部に固着されかつ長穴54内に
嵌合するピン55とにより構成される。第12図
に示されるようにピン55は長穴54内に嵌合す
る小径部56を有し、ピン55の上端部にはワツ
シヤ57およびスナツプリング58が取付けられ
る。 Referring to FIG. 11, an internal combustion engine has four cylinders arranged in series, namely cylinder No. 1, cylinder No. 2,
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 manifold 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. 2 cylinders is opposite to the spiral direction of the spiral portion B of the No. 3 and No. 4 cylinders. The direction in which the rotary valves 25 of the 1st and 2nd cylinders should rotate and the 3rd 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 second cylinders are connected to the rotary valves 25 of the third and fourth cylinders with respect to the line connecting the rotation axes of all the rotary valves. It extends on the opposite side to the arm 32. 1
The distal ends of the arms 32 of the No. 3 and No. 2 cylinders are pivotally connected to a first connecting rod 41, and the distal ends of the arms 32 of the No. 3 and 4th cylinders are pivotally connected to a second connecting rod 42. Therefore, the first connecting rod 41 and the second connecting rod 42 are arranged parallel to each other on both sides of the line connecting all the rotary valves 25. One end of the first connecting rod 41 is connected to a control rod 45 of an actuator 44 via a link 43. The actuator 44 has a negative pressure chamber 47 and an atmospheric pressure chamber 48 separated by a diaphragm 46 to which a control rod 45 is secured. A compression spring 49 for pressing the diaphragm is inserted into the negative pressure chamber 47, and this negative pressure chamber 47 is connected to the throttle 5.
0 and a negative pressure conduit 51 to the intake manifold branch pipe 40a. On the other hand, the first connecting rod 4
1 is connected to the second connecting rod 42 via a loose connecting mechanism 52. Figures 11 and 12
As shown in the figure, a flat plate portion 53 is integrally formed at the end of the second connecting rod 42, and a loose connecting mechanism 52
is formed on the flat plate portion 53 and connected to the second connecting rod 4.
2, and a pin 55 fixed to the end of the first connecting rod 41 and fitted into the elongated hole 54. As shown in FIG. 12, the pin 55 has a small diameter portion 56 that fits into the elongated hole 54, and a washer 57 and a snap ring 58 are attached to the upper end of the pin 55.
機関低負荷運転時には負圧室47内に大きな負
圧が発生するためにダイアフラム46は圧縮ばね
49に抗して負圧室47側に移動し、その結果1
番気筒と2番気筒のロータリ弁25が反時計
回りに回動せしめられてロータリ弁25が分岐路
24を閉鎖する。一方、このとき遊合連結機構5
2のピン55が長穴54内を摺動しつつ第2連結
ロツド42が第1連結ロツド41によつて引張ら
れるために3番気筒と4番気筒のロータリ弁
25は時計回りに回動せしめられ、その結果ロー
タリ弁25が分岐路24を閉鎖する。一方、機関
高負荷運転時には負圧室47内の負圧が小さくな
るためにダイアフラム46は圧縮ばね49のばね
力により大気圧室48側に移動する。その結果、
1番気筒と2番気筒のロータリ弁25が時計
回りに回動して対応する分岐路24が開口せしめ
られ、3番気筒と4番気筒のロータリ弁25
が反時計回りに回動して対応する分岐路24が開
口せしめられる。このように第1連結ロツド41
と第2連結ロツド42とを簡単な構造を有する遊
合連結機構52を介して互に連結することによつ
て1番気筒と2番気筒のロータリ弁25を3
番気筒と4番気筒のロータリ弁25と逆向き
に回動せしめることができる。 During low-load engine operation, large negative pressure is generated in the negative pressure chamber 47, so the diaphragm 46 moves toward the negative pressure chamber 47 against the compression spring 49, and as a result, 1
The rotary valves 25 of the No. 1 and No. 2 cylinders are rotated counterclockwise, and the rotary valves 25 close the branch passage 24. On the other hand, at this time, the loose connection mechanism 5
Since the second connecting rod 42 is pulled by the first connecting rod 41 while the second pin 55 slides in the elongated hole 54, the rotary valves 25 of the third and fourth cylinders are rotated clockwise. As a result, the rotary valve 25 closes the branch passage 24. On the other hand, when the engine is operated under high load, the negative pressure in the negative pressure chamber 47 decreases, so the diaphragm 46 moves toward the atmospheric pressure chamber 48 by the spring force of the compression spring 49. the result,
The rotary valves 25 of the first and second cylinders are rotated clockwise to open the corresponding branch passages 24, and the rotary valves 25 of the third and fourth cylinders are rotated clockwise.
is rotated counterclockwise to open the corresponding branch passage 24. In this way, the first connecting rod 41
By connecting the rotary valves 25 and the second connecting rod 42 to each other via a loose connecting mechanism 52 having a simple structure, the rotary valves 25 of the first and second cylinders can be connected to the third cylinder.
It can be rotated in the opposite direction to the rotary valves 25 of the No. 1 and No. 4 cylinders.
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 a 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の底壁剖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るので高
い充填効率が得られることになる。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 portion B via the branch passage 24, and the third flow is a mixed air flow that flows into the bottom wall section 21 of the inlet passage portion 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
アクチユエータと構造の簡単な遊合連結機構を用
いて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。Effects 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 rotated in opposite directions using a single actuator and a loose coupling mechanism with a simple structure. They can be rotated at the same time.
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XII−XII線に
沿つてみた断面図である。
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……第1連結ロツ
ド、42……第2連結ロツド、44……アクチユ
エータ、52……遊合連結機構。
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.
0 is a side sectional view of the rotary valve, FIG. 11 is a plan view of the internal combustion engine, and FIG. 12 is a sectional view taken along line XII-XII in FIG. 11. 4... Combustion chamber, 6... Helical intake port,
12... Bulkhead, 24... Branch path, 25... Rotary valve, 32... Arm, 41... First connecting rod, 42... Second connecting rod, 44... Actuator, 52... Loose connection mechanism .
Claims (1)
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
気筒の該過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、上記ロ
ータリ弁を結ぶ線の両側に互にほぼ平行に延びる
第1連結ロツドと第2連結ロツドを配置し、該第
1連結ロツドの中間部を一方のアームの先端部に
枢着すると共に該第2連結ロツドの一端部を他方
のアームの先端部に枢着し、更に第1連結ロツド
の一端部をアクチユエータに連結し、第1連結ロ
ツドの他端部をピンと長穴からなる遊合連結機構
を介して第2連結ロツドの他端部に連結した内燃
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 overwound 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 first connecting rod and a second connecting rod are arranged so as to extend substantially parallel to each other on both sides of the line connecting the rotary valves, and the intermediate portion of the first connecting rod is pivoted to the tip of one arm. At the same time, one end of the second connecting rod is pivotally connected to the tip of the other arm, one end of the first connecting rod is connected to the actuator, and the other end of the first connecting rod is inserted through the pin and the elongated hole. An intake control device for an internal combustion engine connected to the other end of the second connecting rod via a loose connecting mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6504183U JPS59170632U (en) | 1983-05-02 | 1983-05-02 | Internal combustion engine intake control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6504183U JPS59170632U (en) | 1983-05-02 | 1983-05-02 | Internal combustion engine intake control device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59170632U JPS59170632U (en) | 1984-11-15 |
| JPH0143472Y2 true JPH0143472Y2 (en) | 1989-12-18 |
Family
ID=30195233
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6504183U Granted JPS59170632U (en) | 1983-05-02 | 1983-05-02 | Internal combustion engine intake control device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59170632U (en) |
-
1983
- 1983-05-02 JP JP6504183U patent/JPS59170632U/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59170632U (en) | 1984-11-15 |
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