JPS58200026A - Helical suction port - Google Patents

Helical suction port

Info

Publication number
JPS58200026A
JPS58200026A JP57080858A JP8085882A JPS58200026A JP S58200026 A JPS58200026 A JP S58200026A JP 57080858 A JP57080858 A JP 57080858A JP 8085882 A JP8085882 A JP 8085882A JP S58200026 A JPS58200026 A JP S58200026A
Authority
JP
Japan
Prior art keywords
passage
valve
wall surface
groove
branch
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
JP57080858A
Other languages
Japanese (ja)
Other versions
JPS6238528B2 (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 JP57080858A priority Critical patent/JPS58200026A/en
Publication of JPS58200026A publication Critical patent/JPS58200026A/en
Publication of JPS6238528B2 publication Critical patent/JPS6238528B2/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)

Abstract

PURPOSE:To prevent an accumulation of impurities such as gum material and leakage of air-fuel mixture from occurring and to expedite vaporization of liquid fuel accumulated in a groove, by a method wherein the groove is formed on a wall surface of the bottom of a suction port and a cooling water duct is provided in the vicinity of the groove. CONSTITUTION:When a space between the lower end of a valve plug 31 and a bottom wall surface 21 is blocked completely the valve plug 31 is sticked on the wall surface 21 of the bottom of a titled port by accumulating impurities, such as a gaseous material to be contained in air-fuel mixture on a lower end part of the valve plug 31 as air-fuel mixture collides against the valve plug 31 at the time of a low speed load operation of an engine. To prevent an above-stated matter from occurring a hollowed groove 36 is formed on the wall surface 21 of the bottom of the titled port and a labyrinth seal is formed by the tip part of the valve plug 31 and the hollowed groove 36. But, as liquid fuel becomes accumulative in the groove 36 vaporization of the liquid fuel is expedited by providing a cooling water duct close to the groove 36.

Description

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

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′!&続されかつほぼま
っ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t−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? ト
渦巻部の渦巻鼾端部に連通する分岐路金シリンダへ、ド
内に形成し、分岐路内に開閉弁金膜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型吸気ポ
ートが不出願人によシ既に提案されている。このヘリカ
ル型吸気ポートで#i機関高速高負荷違転時にヘリカル
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鉤巻部内に送
シ込まれるために吸入空気の流路断11111&が増大
し、斯くして充填効率を向上することができる。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、しかも分岐路全
入口m路部に隣接して形成しなければならないために人
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
^い充填効率t−得るのが困難となっている。史に、ヘ
リカル型吸気ポートはそれ自体の形状が伽帷であり、し
かも入口通路部から完全に独立した分牡路金併設した場
合には吸気ポートの全体構造が惨めて複雑となるのでこ
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り困難である。 ゛ 本発明は機関iSIS高速荷運転時に高い充填効率を得
ることができると共に4造の容易な新規形状を有するヘ
リカル型秋気ポート金提供することにある。
A helical intake port usually has a spiral part formed around the intake valve, and a spiral part tangential to this spiral part. & an inlet passageway which is connected and extends 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. To solve this problem, a helical intake port is branched from the inlet passage. A helical type opening/closing valve is formed inside the metal cylinder, which communicates with the end of the spiral part of the spiral part, and the opening/closing valve is covered with gold film inside the branching passage so that the opening/closing valve opens during high-speed, high-load operation of the engine. An intake port has already been proposed by the applicant. With this helical type intake port, part of the intake air sent into the helical type intake port inlet passage when #i engine is at high speed and under high load is sent into the helical type intake port hooked part through the branch passage. The flow path cutoff 11111& of the intake air increases, thus improving the filling efficiency. 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. This limits the cross-sectional area of the artificial passageway, making it difficult to obtain a sufficiently satisfactory filling efficiency. Historically, the helical type intake port itself has a typical shape, and if a branch pipe that is completely independent from the inlet passage is attached, the overall structure of the intake port becomes extremely complicated. It is quite difficult to form a helical intake port with a branching path in a cylinder head. The object of the present invention is to provide a helical type air port which can obtain high filling efficiency during engine iSIS high-speed loading operation and has a novel shape that is easy to construct.

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

第1図並ひに第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l内で往復動するピストン、
3はシリンダブロック1上に固締されたシリンダヘッド
、4Fiピストン2とシリンダヘッド3間に形成された
燃焼室、5Fi吸気弁、6はシリンダへ、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b!i、逼れた排気ポート、′9は燃
焼室4内に配置された点火栓、1oは吸気弁5のステム
5a’i東内するステムガイドを夫々示す。第1図並び
にm2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が一体成形もれ、この隔壁
12によって渦巻部Bと、この渦巻部BK接縁状に接続
され九入口通路部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#′i人口通路部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
図かられがるようにこの隔壁12の根元部の巾LFi人
口迩路部Aからステムガイド10に近づくにつれて徐々
IL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111513t−有し、更
に隔壁12は第2図においてこの先端1IS13から反
時計回りにステムガイド101で砥びる絹l5i1i壁
面14mと・先端913から時制■りにステムガイド1
01で延びる第211t+Ii面14bとを有する。第
1狽1j橡面14mは先鵡部13からステムガイド10
の側力を通って渦%部Bのllllk面15の近傍まで
延びて渦巻部1ill壁如15との間に狭窄部16を形
成する。次いで第1側壁曲14mは渦巻部1411壁血
15から徐々に間隔を隔てるように彎曲しつつステムガ
イド10まで延ひる。−ツバ第2側壁(3)14bは先
端部13からステムガイド101で#1ばまっすぐに姑
ひる。
Referring to FIG. 1 and FIG. 2, 1 is a cylinder block, 2 is a piston that reciprocates within the cylinder block l,
3 is a cylinder head fixed on the cylinder block 1, 4Fi combustion chamber formed between piston 2 and cylinder head 3, 5Fi intake valve, 6 is helical intake port formed in cylinder 3, 7 is an exhaust valve, 8 is a type b in the cylinder head 3! i, a closed exhaust port, '9, a spark plug disposed in the combustion chamber 4, and 1o, a stem guide extending eastward into the stem 5a'i of the intake valve 5, respectively. As shown in FIG. 1 and FIG. A helical intake port 6 consisting of nine connected inlet passage sections A is formed. The partition wall 12#'i extends from inside the artificial passageway section A to around the stem guide 10 of the intake valve 5.
As shown in the figure, the width LFi of the root portion of this partition wall 12 gradually becomes wider as it approaches the stem guide 10 from the artificial feed path section A. The partition wall 12 is the inlet opening 6a of the intake port 6.
The partition wall 12 has a tip 111513t located on the side closest to the tip 1IS13 in FIG. 1
211t+Ii surface 14b extending at 01. The 1st section 1j 14m is from the tip section 13 to the stem guide 10.
The side force of the vortex portion B extends to the vicinity of the llllk surface 15 of the vortex portion B, and a narrow portion 16 is formed between the vortex portion 1ill wall 15 and the vortex portion B. Next, the first side wall curve 14m extends to the stem guide 10 while curving so as to be gradually spaced apart from the spiral portion 1411 and the wall blood 15. - The brim second side wall (3) 14b is extended straight from the tip 13 by the stem guide 101.

第1図から第9図を参照すると、人口fikt部Aの側
壁面17.18は#よは垂直配置され、−万人1適路m
Aの土壁[11119は渦巻部Bに向1yで皆々に下降
する。人口通、路部Aの側−面17rよ礒壱1bB17
)llil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の土壁面20に滑ら力・に接続
される。渦巻部Bの上壁面20は渦巻sBと人口通路部
Aの接続部から狭窄部16に向iて下降しつつ徐々に巾
を狭め・次いで狭窄部16t−通過すると徐々に巾を広
ける。−万、入口通路部6の下壁向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
水平金なしており、1111I壁面17に隣接する底壁
面部分21jLFi第8図に示すように渦巻NSBに近
づくに従って隆起して傾斜[10を形成する。この傾I
P+底壁面部分21mの傾斜角は渦巻sBK近づくにつ
れて徐々に大きくなる。
Referring to FIGS. 1 to 9, the side wall surface 17.18 of the population fikt part A is vertically arranged,
The earthen wall of A [11119 descends toward the spiral part B in the direction 1y. Population street, side 17r of road section A, Isoichi 1bB17
)llil wall surface 15 and is smoothly connected to the inlet passage section A.
The upper wall surface 19 of the spiral portion B is connected to the earth wall surface 20 of the spiral portion B by a sliding force. The upper wall surface 20 of the spiral portion B gradually narrows in width as it descends from the connection between the spiral sB and the artificial passageway portion A toward the narrowing portion 16, and then gradually widens as it passes through the narrowing portion 16t. As shown in FIG. 5, the lower wall direction 21 of the inlet passage section 6 is almost horizontal in its entirety in the vicinity of the inlet opening 6a, and the bottom wall surface portion 21jLFi 8th adjacent to the 1111I wall surface 17 As shown in the figure, as it approaches the spiral NSB, it rises and forms an inclination [10]. This slope I
The inclination angle of the P+ bottom wall surface portion 21m gradually increases as it approaches the spiral sBK.

一部・隔壁12の第1側壁向14mはわずかげかり傾斜
した下向きのOI糾自からなり、第21111皺Ik1
4bはほぼ垂直をなす。隔!!12の底徽餉122/f
i先端部13からステムガイド10に向うに従って入口
通路s6の上壁mxxとの間隔が次第に大きくなるよう
に入口通路sAから渦巻部Bに向けてわ−rかばかり彎
曲しつつ下降する。隔皺12の底壁面22上には第4図
のハツチングで不す領域に底壁面22から1万に突出す
るりプ23が形成され、このリプ23の底面および底壁
面22はわずかばかり彎曲した傾斜面を形成する。
Part of the first side wall 14m of the partition wall 12 consists of a slightly inclined downward OI groove, and the 21111st wrinkle Ik1
4b is almost vertical. Separation! ! 12 bottoms 122/f
The entrance passage s6 curves downward from the entrance passage sA toward the spiral portion B so that the distance between the entrance passage s6 and the upper wall mxx gradually increases from the tip end 13 toward the stem guide 10. A lip 23 is formed on the bottom wall surface 22 of the partition wrinkle 12 in the area not marked by hatching in FIG. Form an inclined surface.

−万、シリンダヘッド3内には渦巻部Bの渦巻終端部C
と入口通路部Aと全連通する分肢w524が形成され、
この分岐路24の入口部にロータリ9f25が配置され
る。この分岐路24は隔壁12によって入口通路部Aか
ら分離逼れて↓−リ、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の土壁1126は
はは一様な1IJk壱゛シ、渦巻終錫都Cに向けて保々
に1降して渦巻部Bの土壁面20に滑らかに接続される
。隔壁12の第2111壁面14bに?j面する分岐路
24のll1l壁向27はほぼ毒血tなし、史にこの餉
憾面27は#1ぼ入口通路部Aの匈壁圓18の姑長上に
位置する。なお、第1図かられかるように隔壁12上に
形成されたリプ23はロータリ弁25の近傍から吸気弁
5に向けて蝿ひている。
- 10,000, inside the cylinder head 3 there is a spiral end portion C of the spiral portion B.
A branch w524 is formed that fully communicates with the entrance passage section A,
A rotary 9f25 is arranged at the entrance of this branch path 24. This branch passage 24 is separated from the entrance passage A by the partition wall 12, and the entire lower space of the branch passage 24 communicates with the entrance passage A. The earthen wall 1126 of the branching path 24 has a uniform slope of 1IJk, gradually descending towards the end of the spiral C, and is smoothly connected to the earthen wall surface 20 of the spiral portion B. On the 2111th wall surface 14b of the partition wall 12? There is almost no poisonous blood on the ll1l wall side 27 of the branching path 24 facing J. Historically, this grudge side 27 is located on the top of the wall wall 18 of #1 entrance passage section A. As can be seen from FIG. 1, the lip 23 formed on the partition wall 12 extends from the vicinity of the rotary valve 25 toward the intake valve 5.

第10図にボされるようにロータリ升25Fi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, it is composed of a rotary box 25Fi rotary valve holder 28 and a valve shaft 29 rotatably supported within the rotary valve holder 28, and this rotary valve holder 28 is bored in the cylinder head 3. 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
上11面26から底壁面21まで延びる・−万、弁軸2
9の上WAs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m33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が故地まれる
。更にロータリ弁ホルダ28の上端部にはシール部材3
5が嵌層され、このシール部材35によって弁軸29の
シール作用が行なわれる。−万、第1図、第3図および
第7図に示されるように弁体31の下端部に対面する抵
Ii面21上には円錐状の凹$36が形成場れ一弁体3
1Q、下端部が凹溝36の壁面か、わずかな間隔□隔−
C−cm擲、6内、挿入内、81・れる。挺に、第1図
に示すように凹#I36近傍のシリンダヘッド3内には
冷却水通路37が形&場れ、この冷却水通路37Fi薄
肉壁38t−隔てて分岐路24に沿って姑びる。
A thin plate-shaped valve body 31 is integrally formed at the lower end of the valve shaft 29, and as shown in FIG. Valve stem 2
An arm 32 is fixed to the upper WAs of 9. Further, a ring m33 is formed on the outer peripheral surface of the valve shaft 29, and an E-shaped positioning ring 34 is disposed within this ring groove 33. Furthermore, a sealing member 3 is provided at the upper end of the rotary valve holder 28.
5 is fitted over the valve shaft 29, and this sealing member 35 performs a sealing action on the valve shaft 29. - As shown in FIGS. 1, 3, and 7, a conical recess 36 is formed on the resistor surface 21 facing the lower end of the valve body 31.
1Q, the lower end is the wall of the groove 36, or there is a slight interval □ -
C-cm pumping, 6 inside, insertion inside, 81. As shown in FIG. 1, a cooling water passage 37 is formed in the cylinder head 3 near the recess #I36, and the cooling water passage 37 is separated from the thin wall 38t by the cooling water passage 37 along the branch passage 24. .

第11図を参照すると、ロータリ弁25の上4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fii
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FIt40Fiダイアフラム41によって大気から隔
離された負圧室44’を有し、この負圧室44内にダイ
アフラム押圧用圧縮はね45が挿入される。シリンダへ
、ド3にru 1次側気化器46mと2次側気化器46
bからなるコン・ゼウンド型気化器46を具えた吸気マ
ニホノ1ド47が取付けられ、負圧室44は負圧尋′#
48金介して吸気マニホルド47内に連結逼れる。この
負圧導管48内には負圧室44から吸気マニホルド47
内に向けてのみ派通hJ能な逆止弁49か挿入逼れる。
Referring to FIG. 11, the tip of the arm 32 fixed to the upper four parts of the rotary valve 25 is equipped with a negative pressure diaphragm.
It is connected via a connecting rod 43 to a control rod 42 fixed to a diaphragm 41 of 40. It has a negative pressure chamber 44' isolated from the atmosphere by a negative pressure diaphragm device FIt40Fi diaphragm 41, and a compression spring 45 for pressing the diaphragm is inserted into this negative pressure chamber 44. To the cylinder, ru to Do 3 Primary side carburetor 46m and secondary side carburetor 46
An intake manifold 47 equipped with a compound carburetor 46 consisting of a negative pressure chamber 44 is installed, and a negative pressure chamber 44 is
It is connected to the intake manifold 47 through 48-karat gold. In this negative pressure conduit 48, an intake manifold 47 is connected from the negative pressure chamber 44.
The check valve 49, which can only flow inward, is inserted.

更に、負圧室44は大気導管50並びに大気開放制御弁
51t−介して大気に連通する。
Further, the negative pressure chamber 44 communicates with the atmosphere via an atmospheric conduit 50 and an atmospheric release control valve 51t.

この大気開放制御弁51Fiダイアフラム52によって
隔成された負圧蔓53と大気圧室54とt南し、更に大
気圧室54に隣接して弁室55を有する。この弁室55
は一部では大気導管50を介して負圧室44内に連通し
、他方では弁ボート56並びにエアフィルタ57t−介
して大気に連通ずる。
The atmospheric release control valve 51Fi has a negative pressure valve 53 and an atmospheric pressure chamber 54 separated by the diaphragm 52 to the south, and further has a valve chamber 55 adjacent to the atmospheric pressure chamber 54. This valve chamber 55
communicates in part with the negative pressure chamber 44 via an atmospheric conduit 50 and, on the other hand, with the atmosphere via a valve boat 56 and an air filter 57t.

弁室55内には弁ポート56の、開閉制御をする弁体5
8が設けられ、この弁体58は弁ロツド59會介してダ
イアフラム52に連結される。負圧i53内にはダイア
フラム押圧用圧縮はね60が挿入され、史に負圧室53
1i負圧導管61t−介して1次個気化器46mのペン
チ、9部62に連結逼れる。
Inside the valve chamber 55 is a valve element 5 that controls opening and closing of a valve port 56.
8 is provided, the valve body 58 being connected to the diaphragm 52 via a valve rod 59. A compression spring 60 for pressing the diaphragm is inserted into the negative pressure i53, and the negative pressure chamber 53 is
1i negative pressure conduit 61t is connected to the pliers 9 part 62 of the primary vaporizer 46m.

気化器46は通常用いられる気化器であって1次側スロ
ットル弁63か所定洲度以上開弁したときに2次側スロ
ットル弁64が開弁じ、1次側スロットル弁63が全開
すれは2次側スロットル弁64も全開する。1次側気化
器46mのペンチュ1Js62に発生する負圧は機関シ
リンダ内に供給逼れる吸入空気量が増大するほど大きく
なシ、従ってベンチュリ部62に発生する負圧が所定負
圧よりも大きくなったときに、即ち機関^速高負荷運転
時に大気開放制御弁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が弁ボー
ト56を開弁して負圧ダイアフラム装@40の負圧室4
4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のはね力によシ1万に移動し、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。−
万1次側スロットル弁63の一度が小さいときにはペン
チ、すs62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は圧縮はね60のばね力に
より左方に移動し、弁体58が弁ポート56′t−閉鎖
する。更にこのように1次餉スロ、トル弁63の開度が
小さいときには吸気マニホルド47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
圧が負圧ダイアフラム装置140の其圧室44内の負圧
よりも大きくなると−弁じ、吸気□マーホルト47内の
負圧が負圧室44内の負圧よりも小さくなると鉤」弁す
るので大気開放制御弁51が開弁している限り負圧室4
4内の負圧は吸気マニホルド47内に発生した最大負圧
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が回動せしめられて分岐路24が閉鎖される
。従って機関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
運転時であっても機−回転数が低い場合、運びに機関回
転数が高くても低負向運転が行なわれている場合にはペ
ンチ、り部62に発生する負圧が小さなために大気−放
迩断弁51は閉鎖され続けている。従ってこのような低
速為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。
The carburetor 46 is a commonly used carburetor, and when the primary throttle valve 63 is opened to a predetermined degree or more, the secondary throttle valve 64 is opened, and when the primary throttle valve 63 is fully opened, the secondary throttle valve 64 is opened. The side throttle valve 64 is also fully opened. The negative pressure generated in the pentuary 1Js62 of the primary side carburetor 46m increases as the amount of intake air supplied to the engine cylinder increases. Therefore, the negative pressure generated in the venturi portion 62 becomes larger than the predetermined negative pressure. When the engine is operated at high speed and under high load, 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 boat 56 and creates negative pressure. Negative pressure chamber 4 of diaphragm @40
4 to the atmosphere. At this time, the diaphragm 41 is moved 10,000 degrees 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. −
If the degree of rotation of the primary throttle valve 63 is small, the negative pressure generated in the pliers 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't. 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 47. When the negative pressure in the intake manifold 47 becomes larger than the negative pressure in the pressure chamber 44 of the negative pressure diaphragm device 140, the check valve 49 closes and the negative pressure in the intake manifold 47 becomes negative in the negative pressure chamber 44. When the pressure becomes smaller than the pressure, the valve opens, so as long as the atmospheric release control valve 51 is open, the negative pressure chamber 4
The negative pressure within the intake manifold 47 is maintained at the maximum negative pressure developed within the intake manifold 47. When negative pressure is applied within the negative pressure chamber 44, the diaphragm 41 rises against the compression spring 45, and as a result, the rotary valve 25 is rotated and the branch passage 24 is closed. Therefore, when the engine is operating at low speed and low load, the rotary valve 25 closes the branch passage 24. Furthermore, if the machine rotation speed is low even during high load operation, or if the engine rotation speed is high but low negative operation is being performed, the negative pressure generated in the pliers and the rim 62 will be reduced. Because of the small size, the atmosphere-discharge valve 51 continues to be closed. Therefore, during such low-speed, low-load operation and high-speed, low-load operation, the negative pressure chamber 44
Since the negative pressure inside is maintained at the maximum negative pressure mentioned above, the branch passage 24 is closed by the rotary valve 25.

上述したように吸入空気蓋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
のどき、入口通路部A内に送り込まれた混合気の一部は
土壁i1i[i19.20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に憤突して入口
通路gAの側壁面17の万へ向きを変えた懐に@巻部B
の一壁面15に沿って進む。−11述したように土壁i
&I19.20の+ijは狭窄部16に近づくに従って
次第に狭くなるために上壁面19.20に沿って流れる
混合気の流路は次第に狭ばまシ、斯くして上に!!に面
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似kjtm 14 mは
渦巻部Bのl114壁ij[i15の近傍まで蝙ひてい
るので土壁面19.20に沿って進む混合気流は渦巻部
Bの1411壁面15上に押しやられ、次いでl1ll
壁面15に沿って進むためにa巻MB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−)吸
気弁5とその弁肢間に形成でれる間陣を通って燃焼室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
。このように機@低速低負向運転時には弁体31に混合
気が衝突するので弁体31の下端部と底壁th121間
金完全間過完全た場合には混合気中に冨まれるガム負等
の不純@か弁体31の下gtA部に堆積して弁体31が
底壁面21に固着するという問題を生ずる。このような
間Mk回避するために弁体31の下勉部と底壁面21間
に間隙を設けているがこの間隙を単fc設けただけでは
この間1Ijt通って混合気が漏洩するために渦II!
1部B内に発生する旋回流が刺められてしまう。
As described above, the rotary valve 25 closes the branch passage 24 when the engine is operated at low speed and under low load when there are few intake air caps. At this point, part of the air-fuel mixture sent into the inlet passage section A advances along the earthen wall i1i [i19.20, and part of the remaining air-fuel mixture crashes into the rotary valve 25. At the end of the side wall surface 17 of the entrance passage gA
Proceed along one wall 15 of . −11 As mentioned above, earthen wall i
+ij of &I19.20 gradually narrows as it approaches the narrowed part 16, so the flow path of the air-fuel mixture flowing along the upper wall surface 19.20 gradually narrows, thus upward! ! The air mixture flow along planes 19° and 20 gradually increases in speed. Furthermore,
As mentioned above, the first quasi kjtm 14 m of the partition wall 12 extends to the vicinity of the l114 wall ij[i15 of the spiral part B, so the mixed air flow that advances along the soil wall surface 19.20 is caused by the 1411 wall surface 15 of the spiral part B. pushed up and then l1ll
In order to proceed along the wall surface 15, a strong swirling flow is generated within the volume a MB. The mixture then swirls and passes through the gap formed between the intake valve 5 and its valve limbs into the combustion chamber 4.
and generates a strong swirling flow within the combustion chamber 4. In this way, when the engine is running at low speed and in the negative direction, the air-fuel mixture collides with the valve element 31, so if the gap between the lower end of the valve element 31 and the bottom wall TH121 is completely over, the gum accumulated in the air-fuel mixture will be removed. Such impurities accumulate on the lower gtA portion of the valve body 31, causing a problem that the valve body 31 is stuck to the bottom wall surface 21. In order to avoid Mk during such a period, a gap is provided between the lower part of the valve body 31 and the bottom wall surface 21, but if this gap is only provided with a single fc, the air-fuel mixture will pass through 1Ijt during this time and leak, resulting in a vortex II. !
The swirling flow generated in part 1B will be stung.

そこで本発明では底壁面2.1上に凹$36t″形成し
て弁体31の先端部と凹溝36によシラピリンスシール
を構成してガム質勢の不純物が堆積するのを阻止しつつ
混合気の漏洩t−阻止するようにしている。しかしなが
らこのように底壁面21上に凹溝36が形成されるとこ
の凹溝36内に液状燃料が溜ってしまうという間組が生
ずる。ところが本発明では凹#36に近接して冷却水通
路37が設けられているために凹$36内に溜った液状
燃料の気化が冷却水によって促進できる仁とになる。
Therefore, in the present invention, a concave portion 36t'' is formed on the bottom wall surface 2.1, and a seal is formed between the tip of the valve body 31 and the concave groove 36 to prevent gum-like impurities from accumulating. However, when the groove 36 is formed on the bottom wall surface 21 in this way, a problem arises in which liquid fuel accumulates in the groove 36. In the invention, since the cooling water passage 37 is provided adjacent to the recess #36, the vaporization of the liquid fuel accumulated in the recess #36 can be promoted by the cooling water.

史に・この冷却水通路37は分岐路24に沿って延びて
いるために底壁面21上を流れる液状燃料の気化も促進
される仁とになる。
Historically, since this cooling water passage 37 extends along the branch passage 24, the vaporization of the liquid fuel flowing on the bottom wall surface 21 is also promoted.

一部、吸入空気量が多い機関^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地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111411壁面14mと入
口通路部Aの1411壁面17間に流入し、次いで渦巻
部Aの上壁面20に沿っ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’に介して渦巻部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sB内に流入する混合気流であ
る。
The rotary valve 25 is partially opened during high-speed, high-load operation of the engine with a large amount of intake air, so the air-fuel mixture sent into the inlet passageway A is roughly divided into three streams. That is,
The first flow is a mixed air flow that flows between the 111411 wall surface 14m of the partition wall 12 and the 1411 wall surface 17 of the inlet passage section A, and then flows while swirling along the upper wall surface 20 of the swirl section A. 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 swirl portion sB along the bottom wall surface 21 of the inlet passage portion A.

分岐路24の流れ抵抗はM11411壁1i 14 a
とI[e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 M11411 wall 1i 14 a
and I[e, compared to the flow resistance between the surfaces 17, and therefore the second mixed air flow is larger than the first mixed air flow.

更に、渦巻部B内′1kk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
。このように流れ抵抗の小石な分肢路24からの混合気
流が増大し、更にmll混気気流流れ方向が下向きに偏
向されるので尚い光会。
Further, the flow direction of the first air mixture flowing while rotating by 1kk in the spiral portion B is deflected downward by the second air mixture,
In this way, the swirling force of the first air mixture flow is weakened. In this way, the flow resistance of the mixture air flow from the small branch passage 24 increases, and the flow direction of the mixture air flow is further deflected downward, so that there is still light flow.

礪効率が得られることにな□る。tた、前述したように
隔l121の底壁面は下向きの傾斜面から彫成されてい
るので第3の混合気riL#′iこの91糾向に東向さ
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。
This results in greater efficiency. In addition, as mentioned above, since the bottom wall surface of the partition l121 is carved from a downwardly inclined surface, the third air-fuel mixture riL#'i is directed eastward in this 91 direction, and the flow direction is deflected downward. As a result, even higher filling efficiency can be obtained.

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の上壁面上に隔壁12を一体成形すればよいのでヘリ
カル型吸気ポー)1−容易に製造することができる。
Further, the helical type intake port according to the present invention can be easily manufactured because the partition wall 12 may be integrally formed on the upper wall surface of the intake port 6.

以上述べたように本発明によれば機関低速低負衝運1時
には分岐路管遮断して多量の混合気を渦巻部の土壁面に
沿って流すことにより強力な旋回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1−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るので商
い充填効率を得ることができる。また、熱気ポート抵壁
面上に凹#1會形成してこの凹溝とロータリ弁の弁体下
m部間でラビリンスシールt−構成することによりガム
質等の不純物の堆積を阻止しつつ混合気の漏洩を阻止で
き、史に凹溝近傍に冷却水通路を設けることによって凹
溝内に漏った液状燃料の気化を促進することができる。
As described above, according to the present invention, when the engine is running at low speed and low impact, the branch pipe is shut off and a large amount of air-fuel mixture flows along the soil wall surface of the volute part, thereby generating a strong swirling flow inside the combustion chamber. be able to. On the other hand, when the engine is operated at high speed and under high load, by opening the branch passage, the mixed air-fuel mixture is sent into the volute through the branch passage with low flow resistance, so that a higher filling efficiency can be obtained. In addition, by forming a concave #1 on the hot air port resistor wall surface and forming a labyrinth seal between this concave groove and the lower part of the valve body of the rotary valve, it is possible to prevent the accumulation of impurities such as gum and to maintain the air-fuel mixture. Furthermore, by providing a cooling water passage near the groove, vaporization of the liquid fuel leaked into the groove can be promoted.

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

第1図は第2図の11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型吸気
が一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wJ4図の■−■巌に沿ってみた断面図、第
6図は第3図および第4図の■−■縁に沿ってみたII
T面図、第7図は第3図および第4図の■−■紐に沿っ
てみた断面図、048図は第3図およびwJ4図の1−
■線に沿ってみfcIIT面図、第9図は第3図および
第4図のに−IXmに沿ってみた断1図、第10図はロ
ータリ弁の側面断面図、第11図はロータ゛り弁の駆動
制御I41装置11t−示す図である。 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
、36・・・凹溝、37・・・冷却水通路。 W/!、1図 !152図 第7図 第81!l 第101
FIG. 1 is a side sectional view of an internal combustion engine according to the present invention taken along line 11 in FIG. 2, FIG. 2 is a plan sectional view taken along line FIG. 4 is a side view schematically showing the shape of the helical intake port according to the invention, FIG. 4 is a plan view schematically showing the shape of the helical intake port, and FIG. A cross-sectional view taken along the rock, Figure 6 is II taken along the ■-■ edge of Figures 3 and 4.
T-side view, Figure 7 is a sectional view taken along the ■-■ string in Figures 3 and 4, and Figure 048 is 1- in Figures 3 and wJ4.
■FcIIT side view taken along the line, Figure 9 is a cross-sectional view taken along -IXm in Figures 3 and 4, Figure 10 is a side sectional view of the rotary valve, and Figure 11 is the rotary valve. It is a diagram showing a valve drive control I41 device 11t. 4... Combustion chamber, 6... Helical intake port, 12
... Partition wall, 24 ... Branch passage, 25 ... Rotary valve, 36 ... Concave groove, 37 ... Cooling water passage. W/! , Figure 1! 152 Figure 7 Figure 81! l No. 101

Claims (1)

【特許請求の範囲】[Claims] 吸気弁周りに形成された渦巻部と、該渦巻Sに接線状に
接続されかつほぼま9すぐに延びる入口通路部とによ多
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記渦巻部の摘巻終*部に連通する
分岐路金上記入口通路部に併設し、吸気ポート上壁面か
ら下方に突出しかつ入口通路部から吸気弁ステム周9ま
で組ひ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
口通路部に連通ずると共に駅入口造路部と分岐路との通
路壁全一体的に連結形成し、該分岐路内に分岐路上m向
から分岐路下壁面上まで組びる開閉弁t−設けて該開閉
弁により分肢路内を流れる吸入空気流tfilJ14L
、更に分岐路下壁面上に上記開閉弁O下趨部を受答する
凹溝を形成すると共に該凹溝に近接して冷却水通路を紋
りたへリカル型吸気ポート。
In a helical intake port that is configured with a spiral portion formed around the intake valve and an inlet passage portion that is tangentially connected to the spiral S and extends almost straight, the helical intake port is branched from the inlet passage portion. A branch passage communicating with the end of the winding * of the spiral part is attached to the inlet passage part, projects downward from the upper wall surface of the intake port, and is connected to the branch passage by a partition wall that is assembled from the inlet passage part to the circumference 9 of the intake valve stem. is separated from the entrance passage, and the entire lower space of the branch passage communicates with the entrance passage in the cross section, and the passage walls of the station entrance passageway and the branch passage are integrally connected. An on-off valve t installed in the branch path from the direction m of the branch road to the top of the lower wall surface of the branch path is provided, and the intake air flow tfilJ14L flows through the branch path by the on-off valve.
Further, a helical intake port is provided with a groove for receiving the lower end of the opening/closing valve O on the lower wall surface of the branch passage, and a cooling water passage is formed adjacent to the groove.
JP57080858A 1982-05-15 1982-05-15 Helical suction port Granted JPS58200026A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57080858A JPS58200026A (en) 1982-05-15 1982-05-15 Helical suction port

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57080858A JPS58200026A (en) 1982-05-15 1982-05-15 Helical suction port

Publications (2)

Publication Number Publication Date
JPS58200026A true JPS58200026A (en) 1983-11-21
JPS6238528B2 JPS6238528B2 (en) 1987-08-18

Family

ID=13730034

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57080858A Granted JPS58200026A (en) 1982-05-15 1982-05-15 Helical suction port

Country Status (1)

Country Link
JP (1) JPS58200026A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3318780A1 (en) * 1982-05-24 1983-12-22 Toyota Jidosha K.K., Toyota, Aichi SPIRAL SUCTION DEVICE FOR AN INTERNAL COMBUSTION ENGINE

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3318780A1 (en) * 1982-05-24 1983-12-22 Toyota Jidosha K.K., Toyota, Aichi SPIRAL SUCTION DEVICE FOR AN INTERNAL COMBUSTION ENGINE

Also Published As

Publication number Publication date
JPS6238528B2 (en) 1987-08-18

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