JPS58200030A - Helical suction port - Google Patents

Helical suction port

Info

Publication number
JPS58200030A
JPS58200030A JP57082409A JP8240982A JPS58200030A JP S58200030 A JPS58200030 A JP S58200030A JP 57082409 A JP57082409 A JP 57082409A JP 8240982 A JP8240982 A JP 8240982A JP S58200030 A JPS58200030 A JP S58200030A
Authority
JP
Japan
Prior art keywords
valve
inlet passage
passage
wall surface
intake
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
JP57082409A
Other languages
Japanese (ja)
Other versions
JPS6238530B2 (en
Inventor
Hisashige Onishi
大西 寿成
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.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
Toyota Jidosha 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 Toyota Motor Corp, Toyota Jidosha Kogyo KK filed Critical Toyota Motor Corp
Priority to JP57082409A priority Critical patent/JPS58200030A/en
Publication of JPS58200030A publication Critical patent/JPS58200030A/en
Publication of JPS6238530B2 publication Critical patent/JPS6238530B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/24Cylinder heads
    • F02F1/42Shape or arrangement of intake or exhaust channels in cylinder heads
    • F02F1/4228Helically-shaped channels 
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B31/00Modifying induction systems for imparting a rotation to the charge in the cylinder
    • F02B31/04Modifying induction systems for imparting a rotation to the charge in the cylinder by means within the induction channel, e.g. deflectors
    • F02B31/042Modifying induction systems for imparting a rotation to the charge in the cylinder by means within the induction channel, e.g. deflectors induction channel having a helical shape around the intake valve axis
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 本発明はヘリカルm吸気ポートに関する。[Detailed description of the invention] The present invention relates to a helical m-intake port.

ヘリカル型吸気ポートは通常吸気弁脚りに形成された渦
巻部と、この渦巻部に接線状に接続されかつほぼまっす
ぐに蝙びる入口通路部とによシ構成される。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
形状になっ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/−)入
口通路部から分岐されてヘリカル屋吸気ポート渦巻部の
渦巻終端部に連通ずる分岐路をシリンダヘッド内に形成
し、分岐路内に開閉弁を設けて機関高速高負荷運転時に
開閉弁を開弁するようにしたヘリカル製吸気4−トが本
出願人より既に提案されている。このヘリカル型吸気ポ
ートで紘機関高速高負荷運転時にヘリカル型吸気ポート
入口通路部内に送り込まれた吸入空気の一部が分岐路を
介してヘリカル型吸気ポート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、斯くして充填効率
を向上することかできる。
A helical intake port usually consists of a spiral formed in the intake valve leg 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 when the engine is operating at low speed and low load 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, a branch path is formed in the cylinder head that branches from the helical intake/-) inlet passage and communicates with the spiral end of the helical intake port spiral section, and a branch path that opens and closes within the branch path. The applicant has already proposed a helical intake 4-way valve that is provided with a valve to open the on-off valve during high-speed, high-load engine operation. With this helical-type intake port, during high-speed, high-load operation of the Hiro engine, part of the intake air sent into the helical-type intake port inlet passage is sent into the helical-type intake port volute via the branch passage, so the intake air flow is reduced. The cross-sectional area of the path can be increased, thus improving the filling efficiency.

しかしながらこのヘリカル型吸気ポートでは分岐路が入
口通路部から完全に独立した筒状の通路として形成され
ているので分岐路の流れ抵抗が比較的大きく、しかも分
岐路を入口通路部に隣接して形成しなければならないた
めに入口通路部の断面積が制限を受けるので十分に満足
のいく高い充填効率を得るのが困難となっている。更に
、ヘリカル型吸気ポートはそれ自体の形状が複雑であり
、しかも入口通路部から完全に独立した分岐路を併設し
た場合には吸気ポートの全体構造が極めて複雑と表るの
でこのような分岐路を具えたヘリカル型吸気ポートをシ
リンダヘッド内に形成するのはかなシ困離である。
However, in this helical intake port, the branch passage is formed as a cylindrical passage completely independent from the inlet passage, so the flow resistance of the branch passage is relatively large, and the branch passage is formed adjacent to the inlet passage. This limits the cross-sectional area of the inlet passage, making it difficult to obtain a sufficiently high filling efficiency. Furthermore, the helical intake port itself has a complicated shape, and if a branch passage that is completely independent from the inlet passage is provided, the overall structure of the intake port will be extremely complicated. It is difficult to form a helical intake port with a helical type in the cylinder head.

本発明は機関開運高負荷運転時に高い充填効率を得るこ
とができると共に製造の容易な新規形状を有するヘリカ
ル型吸気ポートを提供することにある。
SUMMARY OF THE INVENTION The present invention provides a helical intake port that is capable of achieving high filling efficiency during high-load operation of an engine and has a new shape that is easy to manufacture.

以下、添付図面を参照して本発明の詳細な説明する。Hereinafter, the present invention will be described in detail with reference to the accompanying drawings.

第1図並びに第2図を参照すると、1はシリンダブロッ
ク、2はシリンダブロック1内で往復動するピストン、
3はシリンダプロツク1上に固締され九シリンダヘッド
、4はピストン2とシリンダヘッド3間に形成された燃
焼室、5は吸気弁、6はシリンダヘッド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
ッド3内に形成された排気ポート、9は燃焼m4内に配
置された点火栓、10は吸気弁5のステム5at−案内
するステムガイドを夫々示す。第1図並びに@2図に示
されるように吸気ポート6の下壁面11上には下方に突
出する隔1i12が一体成形され、この隔壁12によっ
て渦巻部Bと、この渦巻部BK接線状に接続され九人口
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9、第2図かられかるよ
うにこの隔壁120根元部の巾りは入口通路部Aからス
テムガイド1oに近づくにつれて徐々に広くなる。隔壁
12は吸気ボート60入口開口6aに最も近い側に位置
する先端1iB13を有し、更に隔壁12は第2図にお
いてこの先端部13がら反時計回りにステムガイド10
1で延びる第1側壁面141と、先端部13がら時計回
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 flA’m1li]14 mは先端部1
3がらステムガイド10の側方を通って渦巻部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14mは渦巻部側
壁面15から徐々に間隔を隔てるように彎曲しりつステ
ムがイド1oまで延びる。一方、第2側壁面14bは先
端部13がらステムガイド10までほぼまっすぐに延び
る。この第2側壁血14b上には吸気弁ステム5aの軸
線周りに部分円筒状の凹溝14cが形成され、この凹*
 l 4 eの上端部にステムガイド1oの下端部が嵌
着される。ステムガイド10Fi円筒状をなしておシ、
従って第2図に示されるようにステムガイド1oは第2
側壁11i14bがら渦巻部B内に突出する。
Referring to FIG. 1 and FIG. 2, 1 is a cylinder block, 2 is a piston that reciprocates within the cylinder block 1,
3 is a cylinder head fixed on the cylinder block 1; 4 is a combustion chamber formed between the piston 2 and the cylinder head 3; 5 is an intake valve; 6 is a helical intake port formed within the cylinder head 3. , 7 is an exhaust valve, 8 is an exhaust port formed in the cylinder head 3, 9 is a spark plug disposed in the combustion chamber m4, and 10 is a stem guide for guiding the stem 5at of the intake valve 5. As shown in Fig. 1 and Fig. 2, a partition 1i12 projecting downward is integrally molded on the lower wall surface 11 of the intake port 6, and this partition 12 connects the spiral portion B to the spiral portion BK in a tangential manner. A helical intake port 6 consisting of nine artificial passages A is formed. This partition wall 12 extends from inside the inlet passage section A to around the stem guide 10 of the intake valve 5.As can be seen from FIG. It gradually becomes wider as it approaches. The bulkhead 12 has a tip 1iB13 located on the side closest to the inlet opening 6a of the intake boat 60, and the bulkhead 12 further extends counterclockwise from this tip 13 to the stem guide 10 in FIG.
1, and a second side wall surface 14b extending clockwise from the distal end portion 13 to the stem guide 10. 1st flA'm1li] 14 m is the tip 1
3 to the vicinity of the side wall surface 15 of the spiral portion B through the side of the stem guide 10 to form a narrow portion 16 between the spiral portion B and the side wall surface 15 of the spiral portion B. Next, the curved stem of the first side wall surface 14m is gradually spaced apart from the spiral portion side wall surface 15 and extends to the id 1o. On the other hand, the second side wall surface 14b extends substantially straight from the distal end portion 13 to the stem guide 10. A partially cylindrical groove 14c is formed on the second side wall 14b around the axis of the intake valve stem 5a, and this groove *
The lower end of the stem guide 1o is fitted into the upper end of l4e. Stem guide 10Fi has a cylindrical shape,
Therefore, as shown in FIG.
The side walls 11i14b protrude into the spiral portion B.

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i部Bに向けて徐々に下降する。入口通路
sh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
2oに滑らかに接続される。渦巻部Bの上壁面2o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16を通過す
ると徐々に巾を広げる。一方、入口通路部6の下壁面2
1Fi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シ、側壁面17に隣接
する底壁面部分21mは第8図に示すように渦巻部Bに
近づくに従って隆起して傾斜面を形成する。この傾斜底
壁面部分21m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 side wall surfaces 17,18 of the inlet passage section A are substantially vertically arranged, while the upper wall surface 19 of the inlet passage section A gradually descends towards the vortex i section B. The side wall surface 17 of the inlet passage sh is smoothly connected to the side wall surface 15 of the spiral part B, and the upper wall surface 19 of the inlet passage part A is smoothly connected to the upper wall surface 2o of the spiral part B. The upper wall surface 2o of the spiral portion B gradually narrows in width while descending from the connecting portion between the spiral portion B and the inlet passage portion A toward the narrowed portion 16, and then gradually widens after passing through the narrowed portion 16. On the other hand, the lower wall surface 2 of the inlet passage section 6
1Fi As shown in FIG. 5, the entire area near the inlet opening 6a is almost horizontal, and the bottom wall surface portion 21m adjacent to the side wall surface 17 is curved as it approaches the spiral portion B as shown in FIG. It rises to form an inclined surface. The angle of inclination of this inclined bottom wall surface portion 21m gradually increases as it approaches the spiral portion B.

一方、隔壁12の第1側壁面14畠はわずかばかり傾斜
した下向きの傾斜面がらなシ、第211141面14b
はほぼ垂直をなす。隔壁12の底壁面22は先端部13
からスデムガイド10に向うに従って入口通路部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1に向けてわずかばかり彎曲しつつ下降す
る。隔壁12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プ23が形
成され、このりゾ23の底面および底壁面22はわずか
げかシ彎曲した傾斜面を形成する。
On the other hand, the first side wall surface 14 of the partition wall 12 has a slightly inclined downward slope, and the 211141st surface 14b
is almost vertical. The bottom wall surface 22 of the partition wall 12 has a tip end 13
It descends from the inlet passage A toward the spiral part 1 while slightly curving so that the distance from the upper wall surface 11 of the inlet passage A gradually increases as it moves toward the Sudem guide 10. A lip 23 is formed on the bottom wall surface 22 of the partition wall 12 in the region indicated by hatching in FIG. 4, and projects downward from the bottom wall surface 22. form a surface.

一方、シリンダヘッド3内には渦巻部Bの一巻終端部C
と入口通路部Aとを連通ずる分岐路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。
On the other hand, inside the cylinder head 3, there is an end portion C of one turn of the spiral portion B.
A branch passage 24 is formed which communicates the inlet passage A with the inlet passage A, and a rotary valve 25 is disposed at the entrance of the branch passage 24.

この分岐路24は隔壁12によって入口通路部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9:・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2
7はほぼ垂直をなし、更にこの1IllWk向27はほ
ぼ入口通路部人の側壁面18の延長上に位置する。なお
、第1図かられかるように隔壁12上に形成されたりプ
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。
This branch passage 24 is separated from the inlet passage part A by the partition wall 12, and the entire lower space of the branch passage 24 communicates with the inlet passage part A. The upper wall surface 9:26 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
Side wall surface 2 of branch path 24 facing second side wall surface 14b of No. 2
7 is approximately vertical, and furthermore, this 1IllWk direction 27 is located approximately on an extension of the side wall surface 18 of the entrance passage. As can be seen from FIG. 1, the pipe 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はシリンダヘッド3に穿設されたねじ孔
30内に螺着される。
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.

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31は分岐路24の
土壁面26から底壁面21f、で延びる。一方、弁軸2
9の上端部に、はアーム32が固定される。ま九、弁軸
29の外周面上にはリング#133が形成され、このり
フグ溝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によって弁軸29
の      □1シール作用が行なわれる。
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, this valve body 31 extends from the soil wall surface 26 of the branch passage 24 to the bottom wall surface 21f. On the other hand, valve stem 2
An arm 32 is fixed to the upper end of 9. Finally, a ring #133 is formed on the outer peripheral surface of the valve shaft 29, and an E-shaped positioning ring 34 is fitted into the puffer groove 33. Further, a sealing member 35 is fitted to the upper end of the rotary valve holder 28, and this sealing member 35 allows the valve shaft 29 to be
□1 sealing action is performed.

第11図を参照すると、ロータリ弁25の上端部に固着
されたアーム32の先端部は負圧ダイアフラム装置40
のダイアフラム41に固着された制御ロッド42に連結
ロッド43を介して連結される。負圧ダイアフラム装置
4041ダイアフラム41によって大気から隔離された
負圧室44′Jk有し、この負圧室44内にダイアワラ
ム押圧用圧縮ばね45が挿入される。シリンダヘッド3
には1次側気化器46mと2次側気化器46bからなる
コンパウンド型気化器46を具えた吸気マニホルド47
が堰付けられ、負圧′1A44は負圧導管48を介して
吸気マニホルド47内に連結される。この負圧導管48
内には負圧室44から吸気マニホルド47内に向けての
み流通可能な逆止弁49が挿入される。更に、負圧室4
4は大気導$50並びに大気開放制御弁51を介して大
気に連通ずる。
Referring to FIG. 11, the tip of the arm 32 fixed to the upper end of the rotary valve 25 is connected to a negative pressure diaphragm device 40.
It is connected via a connecting rod 43 to a control rod 42 fixed to a diaphragm 41 of. Negative pressure diaphragm device 4041 has a negative pressure chamber 44'Jk isolated from the atmosphere by the diaphragm 41, and a compression spring 45 for pressing the diaphragm is inserted into this negative pressure chamber 44. cylinder head 3
The intake manifold 47 is equipped with a compound type carburetor 46 consisting of a primary side carburetor 46m and a secondary side carburetor 46b.
is dammed, and the negative pressure '1A44 is connected into the intake manifold 47 via the negative pressure conduit 48. This negative pressure conduit 48
A check valve 49 that allows flow only from the negative pressure chamber 44 into the intake manifold 47 is inserted therein. Furthermore, negative pressure chamber 4
4 communicates with the atmosphere via an atmosphere conduit $50 and an atmosphere release control valve 51.

この大気開放制御弁51はダイアフラム52によって隔
成された負圧室53と大気圧蔓54とを有し、更に大気
圧室54に隣接して弁室55を有する。この弁室55は
一方では大気導管50を介して負圧室44内に連通し、
他方では弁/ −) 56並びにエアフィルタ57を介
して大気に連通ずる。
The atmospheric release control valve 51 has a negative pressure chamber 53 and an atmospheric pressure valve 54 separated by a diaphragm 52, and further has a valve chamber 55 adjacent to the atmospheric pressure chamber 54. This valve chamber 55 communicates with the negative pressure chamber 44 via an atmospheric conduit 50 on the one hand;
On the other hand, it communicates with the atmosphere via a valve (/-) 56 and an air filter 57.

弁′M55内には弁ポート56の開閉制御をする弁体5
Bが設けられ、この弁体58は弁ロッド59を介してダ
イアフラム52に連結される。負圧室53内にはダイア
フラム押圧用圧mはね60が挿入され、史に負圧室53
は負圧導管61を介して1次側気化器46mのベンチ、
り部62に連結される。
Inside the valve 'M55 is a valve body 5 that controls the opening and closing of the valve port 56.
A valve body 58 is connected to the diaphragm 52 via a valve rod 59. A pressure spring 60 for pressing the diaphragm is inserted into the negative pressure chamber 53, and the pressure spring 60 is inserted into the negative pressure chamber 53.
is the bench of the primary side vaporizer 46m via the negative pressure conduit 61,
62.

気化器46は通常用いられる気化器であって1久側スロ
ツトル弁63か所定開度以上開弁したときに2久側スロ
ツトル弁64が開弁し、1次側スロットル升63が全開
すれば2久側スロツトル弁64も全開する。1次側気化
器461のベンチュリ部62に発生する負圧は機関シリ
ンダ内に供給される吸入空気量が増大するほど大きくな
り、従ってベンチ、1Js62に発生する負圧が所定員
圧よりも大金くなったときに、即ち機関高速高負荷運b
twに大気開放制御弁51のダイアフラム52が圧縮ば
ね60に抗して右方に移動し、その結果弁体58が弁ポ
ート56を開弁して負圧ダイアフラム装置40の負圧室
44を大気に開放する。このときダイアフラム41は圧
縮ばね45のばね力により下方に移動し、その結果ロー
タリ弁25が回転せしめられて分岐路24を全開する。
The carburetor 46 is a normally used carburetor, and when the first throttle valve 63 opens a predetermined opening degree or more, the second throttle valve 64 opens, and if the primary throttle valve 63 fully opens, the second throttle valve 64 opens. The far side throttle valve 64 is also fully opened. The negative pressure generated in the venturi section 62 of the primary side carburetor 461 increases as the amount of intake air supplied into the engine cylinder increases. In other words, when the engine is operating at high speed and high load, b
tw, the diaphragm 52 of the atmospheric release control valve 51 moves to the right against the compression spring 60, and as a result, the valve body 58 opens the valve port 56, opening the negative pressure chamber 44 of the negative pressure diaphragm device 40 to the atmosphere. open to At this time, the diaphragm 41 is moved downward by the spring force of the compression spring 45, and as a result, the rotary valve 25 is rotated and the branch passage 24 is fully opened.

一方1次側スロットル弁63の開度が小さいときにはベ
ンチュリ部62に発生する負圧が小さなために大気開放
制御弁51のダイアフラム52は圧縮ばね60のばね力
により左方に移動し、弁体58が弁ポート56を閉鎖す
る。更にこのように1次側スロットル弁63の開度が小
さいときには吸気マニホルy47内には大きな負圧が発
生している。逆止弁49は吸気マニホルド47内の負圧
が負圧ダイアプラム装置40の負圧室44内の負圧より
も大きくなると開弁し、吸気マニホルド47内の負圧が
負圧室44内の負圧よりも小さくなると閉弁するので大
気開放制御弁51が閉弁している限り負え室、4内。貝
柱吸気:“”q=$k )−4□4発生した最大負圧に
維持される。負圧室44内に負圧が加わるとダイアフラ
ム41は圧縮ばね45に抗して上昇し、その結果ロータ
リ弁25が回動せ低速低負荷運転時にはロータリ弁25
によって分岐路24が閉鎖されることになる。なお、高
負荷運転時でToりても機関回転数が低い場合、並びに
機関回転数が高くても低負荷運転が行なわれている場合
にはベンチ、!JW62に発生する負圧が小さなために
大気開放遮断弁51は閉鎖され続けている。従ってこの
ような低速高負荷運転時並びに高速低負荷運転時には負
圧室44内の負圧が前述の最大負圧に維持されているの
でロータリ弁25によって分岐路24が閉鎖されている
On the other hand, when the opening degree of the primary throttle valve 63 is small, the negative pressure generated in the venturi section 62 is small, so the diaphragm 52 of the atmospheric release control valve 51 moves to the left by the spring force of the compression spring 60, and the valve body 58 closes valve port 56. Furthermore, when the opening degree of the primary throttle valve 63 is small as described above, a large negative pressure is generated within the intake manifold y47. The check valve 49 opens when the negative pressure in the intake manifold 47 becomes larger than the negative pressure in the negative pressure chamber 44 of the negative pressure diaphragm device 40, and the negative pressure in the intake manifold 47 becomes larger than the negative pressure in the negative pressure chamber 44. The valve closes when the pressure becomes smaller than the pressure, so as long as the atmospheric release control valve 51 is closed, the pressure inside the load chamber 4 is maintained. Scallop intake: “”q=$k )−4□4 is maintained at the maximum negative pressure generated. When negative pressure is applied to the negative pressure chamber 44, the diaphragm 41 rises against the compression spring 45, and as a result, the rotary valve 25 rotates.
Therefore, the branch road 24 is closed. In addition, if the engine speed is low even if the engine speed is turned on during high load operation, or if the engine speed is high but low load operation is being performed, the bench, ! Since the negative pressure generated in the JW 62 is small, the atmospheric release shutoff valve 51 continues to be closed. Therefore, during such low-speed, high-load operation and high-speed, low-load operation, the negative pressure in the negative pressure chamber 44 is maintained at the aforementioned maximum negative pressure, so the branch passage 24 is closed by the rotary valve 25.

上述したように吸入空気量が少ない機関低速低負荷運転
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に沿って進み、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の方へ向きを変え先後に渦巻部Bの1Il
i壁面15に沿って進む。前述したように上壁面19.
20の巾は狭窄部16に近づくに従って次第に狭くなる
ために土壁面19.20に沿って流れる混合気の流路は
次第に狭はまり、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1
2の第1IIllI1面14m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19.20に沿って進
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me面15に沿っ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って燃焼
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 described above, the rotary valve 25 closes the branch passage 24 when the engine is operated at low speed and under low load with a small amount of intake air. At this time, part of the air-fuel mixture sent into the inlet passage section A advances along the upper wall surface 19,20, and part of the remaining air-fuel mixture collides with the rotary valve 25 and passes through the inlet passage. Part A
1Il of the spiral part B after changing the direction toward the side wall surface 17 of
i Proceed along the wall surface 15. As mentioned above, the upper wall surface 19.
The width of 20 gradually narrows as it approaches the narrowed part 16, so the flow path of the mixture flowing along the soil wall surface 19.20 gradually narrows, and thus the speed of the mixture flow along the upper wall surface 19.20 gradually increases. be done. Furthermore, as mentioned above, the partition wall 1
2, the first IIIllI1 surface 14m is the side wall surface 15 of the spiral portion B.
Since the mixture flow extends close to the upper wall surface 19,20, it is pushed onto the side wall surface 15 of the swirl section B, and then proceeds along the me surface 15, so there is a strong swirl inside the swirl section B. A flow is generated. 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[12の第1側壁面14mと入口通路部
Aの側壁面17間に流入し、次いで渦巻部Bの上様面2
0に沿って旋回しつつ流れる混合気流であ)、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に沿っ
て渦巻部B内に流入する混合気流である。
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 is opened, so that the air-fuel mixture sent into the inlet passage A is roughly divided into three flows. That is,
The first flow flows between the first side wall surface 14m of the partition [12] and the side wall surface 17 of the inlet passage section A, and then flows into the upper surface 2 of the spiral section B.
0), 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 mixed air flow that flows into the swirl part B through the branch passage 24, and the third flow is a mixed air flow that flows along the bottom wall surface 21 of the inlet passage part A. This is a mixed air flow that flows into the swirl portion B along the .

分岐路24の流れ抵抗は第1側壁面14mと側壁面17
間の流れ抵抗に比べて小さく、従って第2の混合気流の
方が第1の混合気流よりも多くなる。
The flow resistance of the branch path 24 is between the first side wall surface 14m and the side wall surface 17.
Therefore, the second mixed air flow is larger than the first mixed air flow.

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混合気流によっ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。ま
た、前述したようにステムガイド10が渦巻部B内に突
出しているために渦巻部Bの土壁面20近傍は流れ抵抗
が大きくなり、そ、の結果分岐路24から渦巻部B内に
流入する第2混合気流は下向きに偏向されるために第1
混合気流は一層下向きに偏向される。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、史にW
、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、斯くして更に尚い充填効率が得ら
れることになる。
Furthermore, 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. Furthermore, as described above, since the stem guide 10 protrudes into the spiral portion B, flow resistance increases near the soil wall surface 20 of the spiral portion B, and as a result, flow into the spiral portion B from the branch path 24 occurs. The second air mixture flow is deflected downward so that the first
The air mixture is deflected further downward. In this way, the mixed air flow from the branch passage 24 with low flow resistance increases, and the W
, 1. Since the flow direction of the mixed air 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 as a downwardly inclined surface, the third air mixture flow is guided by this inclined surface and the flow direction is deflected downward, thus further increasing the filling rate. Efficiency will be gained.

一方、前述したようにステムガイド10は輌巻部B内に
突出しているのでステムガイド10は餉巻部B内を旋回
する混合気流、および分岐m24から渦巻部B内に流入
する混合気流に[接さらされる。従ってステムガイド1
0が混合気流によって冷却されるために吸気弁ステム5
&の焼付塾を阻止できると共に混合気中の燃料の気化を
促進することができる。
On the other hand, as described above, since the stem guide 10 protrudes into the spiral part B, the stem guide 10 is connected to the air mixture swirling inside the winding part B and the air mixture flowing into the spiral part B from the branch m24. be exposed to Therefore, stem guide 1
0 is cooled by the air mixture flow so that the intake valve stem 5
It is possible to prevent the seizure of &, and also to promote the vaporization of the fuel in the air-fuel mixture.

また、本発明によるヘリカル型吸気ポートは吸気ポート
6の上檎圓上に隔壁12を一体成形すればよいのでヘリ
カル型吸気ポートを容易に製造することができる。
Further, in the helical type intake port according to the present invention, the partition wall 12 can be integrally formed on the upper circle of the intake port 6, so that the helical type intake port can be easily manufactured.

以上述べ友ように本発明によれば機関低速低負荷運転時
には分岐路を連断じて多量の混合気を祇巻部の上mtI
Dfcaって流すことによシ強力な旋回1、: 流を燃焼室内に発生せしめることができる。一方、機関
高速高負荷運転時には分岐路を開口することにより多量
の混合気が流れ、抵抗の小さな分岐路を介して渦巻部内
に送り込まれ、更にステムガイドによって混合気流が下
向きに偏向せしめられるために高い充填効率を得ること
ができる。
As described above, according to the present invention, when the engine is operating at low speed and low load, the branch passage is disconnected and a large amount of air-fuel mixture is delivered to the upper mtI of the Gimaki section.
By flowing Dfca, a strong swirling flow can be generated inside the combustion chamber. On the other hand, during engine high-speed, high-load operation, a large amount of air-fuel mixture flows by opening the branch passage, and is sent into the volute through the branch passage with low resistance, and the mixture flow is further deflected downward by the stem guide. High filling efficiency can be obtained.

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

第1図は第2図の1−1線に沿ってみた本発明に係る内
燃機関の側面断面図、第2図は第1図の■−■線に沿っ
てみた平面断面図、第3図は本発明によるヘリカル製吸
気4−トの形状を図解的に示す11面図、第4図はヘリ
カル型吸気/−)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■−v線に沿ってみた断面図、
第6図は第3図および第4図のVt−Vt線に沿ってみ
た断面図、第7図は第3図および第4図の■−■線に沿
ってみた断面図、第8図は第3図および第4図の■−■
線に沿ってみた断面図、第9図は第3図および第4図の
■−X線に沿ってみた断面図、第10図はロータリ弁の
側面断面図、第11図はロータリ弁の駆動制御装置を示
す図である。 4・・・燃焼室、6・・・ヘリカル型吸気4−ト、10
・・・ステムガイド、12・・・隔壁、24・・・分岐
路、25・・・ロータリ弁。 第2図 第4図 第5図 第7!a 第91!1 Wp18図 第10図
1 is a side sectional view of an internal combustion engine according to the present invention taken along line 1-1 in FIG. 2, FIG. 2 is a sectional plan view taken along line 1--1 in FIG. 11 is a plan view schematically showing the shape of the helical air intake 4-t according to the present invention, FIG. 4 is a plan view schematically showing the shape of the helical air intake, and FIG. Cross-sectional view taken along the ■-v line in Figure 4,
Fig. 6 is a sectional view taken along the Vt-Vt 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 ■-■ in Figures 3 and 4
Figure 9 is a cross-sectional view taken along the -X line in Figures 3 and 4, Figure 10 is a side cross-sectional view of the rotary valve, and Figure 11 is the drive of the rotary valve. It is a figure showing a control device. 4... Combustion chamber, 6... Helical intake 4-to, 10
... Stem guide, 12... Bulkhead, 24... Branch passage, 25... Rotary valve. Figure 2 Figure 4 Figure 5 Figure 7! a 91!1 Wp18 Figure 10

Claims (1)

【特許請求の範囲】[Claims] 吸気弁周シ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っすぐに延びる入口通路部とによシ
構成されたヘリカル型吸気ポートにおいて、上記入口通
路部から分岐されて上配堝巻部の渦巻終端部に連通する
分岐路を上記入口通路部に併設し、吸気/−)土壁面か
ら下方に突出しかつ入口通路部から吸気弁ステム周りま
で延びる隔壁によって該分岐路が入口通路部から分離さ
れ、該分岐路の下側空間全体が横断面内において上記入
口通路部に連通すると共に該入口通路部と分岐路との通
路壁を一体的に連結形成し、該分岐路内に開閉弁を設け
て該開閉弁により分岐路内を流れる吸入空気流を制御し
、更に上記吸気弁を支持するステムガイドの一部を渦巻
部内に謹呈するようにしたヘリカル型吸気ポート。
In a helical intake port configured with a spiral part formed around the intake valve and an inlet passage part connected tangentially to the spiral part and extending almost straight, the intake port is branched from the inlet passage part. A branch passage communicating with the spiral terminal end of the upper winding part is provided in the above-mentioned inlet passage part, and the branch passage is connected by a partition wall that protrudes downward from the earth wall surface and extends from the inlet passage part to around the intake valve stem. It is separated from the inlet passage, the entire lower space of the branch passage communicates with the inlet passage in a cross section, and the passage walls of the inlet passage and the branch passage are integrally connected, and the branch passage is separated from the inlet passage. A helical-type intake port is provided with an on-off valve therein, the on-off valve controls the flow of intake air flowing through the branch passage, and a part of a stem guide supporting the intake valve is disposed within the spiral portion.
JP57082409A 1982-05-18 1982-05-18 Helical suction port Granted JPS58200030A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57082409A JPS58200030A (en) 1982-05-18 1982-05-18 Helical suction port

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57082409A JPS58200030A (en) 1982-05-18 1982-05-18 Helical suction port

Publications (2)

Publication Number Publication Date
JPS58200030A true JPS58200030A (en) 1983-11-21
JPS6238530B2 JPS6238530B2 (en) 1987-08-18

Family

ID=13773786

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57082409A Granted JPS58200030A (en) 1982-05-18 1982-05-18 Helical suction port

Country Status (1)

Country Link
JP (1) JPS58200030A (en)

Also Published As

Publication number Publication date
JPS6238530B2 (en) 1987-08-18

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