JPS6093119A - Suction device of engine - Google Patents

Suction device of engine

Info

Publication number
JPS6093119A
JPS6093119A JP58202045A JP20204583A JPS6093119A JP S6093119 A JPS6093119 A JP S6093119A JP 58202045 A JP58202045 A JP 58202045A JP 20204583 A JP20204583 A JP 20204583A JP S6093119 A JPS6093119 A JP S6093119A
Authority
JP
Japan
Prior art keywords
intake
intake air
intake passage
opening
passage
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
JP58202045A
Other languages
Japanese (ja)
Other versions
JPH0247571B2 (en
Inventor
Koichi Hatamura
耕一 畑村
Koji Asaumi
皓二 浅海
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.)
Mazda Motor Corp
Original Assignee
Mazda Motor Corp
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 Mazda Motor Corp filed Critical Mazda Motor Corp
Priority to JP58202045A priority Critical patent/JPS6093119A/en
Priority to EP84111361A priority patent/EP0137393B1/en
Priority to DE8484111361T priority patent/DE3475419D1/en
Publication of JPS6093119A publication Critical patent/JPS6093119A/en
Priority to US06/815,287 priority patent/US4625687A/en
Publication of JPH0247571B2 publication Critical patent/JPH0247571B2/ja
Granted legal-status Critical Current

Links

Classifications

    • 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
    • F02B31/06Movable means, e.g. butterfly valves
    • F02B31/08Movable means, e.g. butterfly valves having multiple air inlets, i.e. having main and auxiliary intake passages
    • F02B31/085Movable means, e.g. butterfly valves having multiple air inlets, i.e. having main and auxiliary intake passages having two inlet valves
    • 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
    • F02F1/4214Shape or arrangement of intake or exhaust channels in cylinder heads specially adapted for four or more valves per cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
    • 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
    • F02B2031/006Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air intake valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/20SOHC [Single overhead camshaft]
    • 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
    • F02F2001/244Arrangement of valve stems in cylinder heads
    • F02F2001/245Arrangement of valve stems in cylinder heads the valve stems being orientated at an angle with the cylinder 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

Abstract

PURPOSE:To produce a strong swirl in a combustion chamber over a relatively wide range of a low load running area by locating the center of the opening of an auxiliary intake air path branching from a main intake air path, in a position deviating in the direction opposite to the position where the other intake air port is located, from the center of the main intake air path. CONSTITUTION:In a low load running area where a closing valve 18 is closed, all the intake air passing through a main intake air path 11 is led from an opening 19 to an auxiliary intake air path 20, and is fed to a combustion chamber 4 from an opening 21 through the first intake air port 5, thus, a strong swirl is formed. With increasing the engine load, a closing valve 18 also begins to open when a throttle valve opens beyond its specified value. In the running area where the opening of the closing valve 18 is relatively small, since the auxiliary intake air path 20 opens only the first intake air port 5 and the opening 19 is located in a position deviating toward the second intake air port 6, the quantity of intake air supplied to the combustion chamber 4 through the first intake air port 5 becomes larger than the quantity of intake air passing through the second intake air port 6. Thus, a certain degree of swirl can be formed even in the area where the load is increased.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、エンジンの吸気装置、殊九一つの燃焼室に複
数の吸気ポートが開口し、そのうちの少くとも一つの吸
気ポートがエンジン負荷に応じて選択的に使用されるよ
うになった形式のエンジンの吸気装置に関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an engine intake system, especially an engine in which a plurality of intake ports are opened in one combustion chamber, and at least one of the intake ports is connected to an engine load. The present invention relates to an engine intake system of a type that is selectively used according to the type of engine.

(従来技術) エンジンの燃焼室に複数の吸気ポート全般け、それら吸
気ポー)?エンジン負荷に応じて選択的に使用すること
は公知である。たとえば、特開昭S乙−4tlI4!、
ity号公報に開示されたエンジンでは、シリンダヘッ
ドに形成されたコイ1^1の暖気νJ9−トのそれぞれ
に分岐吸気通路が接続され、この分岐吸気通路は共通の
主吸気)I!I略に接続されている。
(Prior art) Is there a plurality of intake ports in the engine combustion chamber? It is known to use them selectively depending on the engine load. For example, Tokukai Showa S Otsu-4tlI4! ,
In the engine disclosed in the ity publication, a branch intake passage is connected to each of the warm air νJ9-to of the coil 1^1 formed in the cylinder head, and this branch intake passage is connected to a common main intake) I! It is connected to I.

そして、一方の分岐吸気通路には開閉弁が、、主吸気通
路には絞シ弁がそれぞれ設けられておシ、この絞り弁と
開閉弁とは連動して、絞り弁が一犀開度を越えて開かれ
たとき開IJつ弁が開かf′1.るようになっている。
One of the branch intake passages is provided with an on-off valve, and the main intake passage is provided with a throttle valve.The throttle valve and the on-off valve work together to control the opening of the throttle valve at once. The open IJ valve opens when it is opened beyond f'1. It has become so.

すなわち、−力の分岐0&、シ1コ出路け、エンジンの
低負荷運転時には開閉弁により顯じられているため、吸
気は他方の分岐1汐気通路のみから比較的高い流速で供
給さノ1、酸1負荷運転時には吸気は両方の分岐吸気通
路から供給さねて高い充填量全確保することができる。
In other words, since the force branches 0 & 1 are controlled by on-off valves when the engine is operating at low load, intake air is supplied at a relatively high flow rate only from the other branch 1 air passage. During operation with one acid load, intake air is not supplied from both branch intake passages to ensure a high filling amount.

しかし、この公開公報に記載されたエンジンの吸気装置
は、高負荷運転時に十分々吸気充填ヤを確保することを
意図するものであるため、各分岐吸気通路の断面積はさ
ほど小さく形成官りておらず、低負荷運転時に一方の分
岐吸気通路のみを使用しても、アイドリング運転時のよ
うに負荷が非常に小さい運転動域では、吸気流速を十分
に高めることができカー。
However, since the engine intake system described in this publication is intended to ensure sufficient intake air filling during high-load operation, the cross-sectional area of each branch intake passage is not very small. Even if only one branch intake passage is used during low-load operation, the intake flow velocity can be sufficiently increased in operating ranges where the load is very small, such as during idling.

首穴、吸気デートの膨軟は、高負荷運転時の高充填量確
保のために、吸気流を燃焼岸の軸線カ同にほぼ沿って導
入するようになってお゛す、このことは、分岐吸気通路
の断面#をあ1り小さくできないことと相まって、低負
荷運転時に燃焼室内に強力なスワールを形成することを
困難にl、ている。
The expansion and softening of the neck hole and intake date allows the intake air flow to be introduced almost along the axis of the combustion bank in order to ensure a high filling amount during high-load operation. Coupled with the fact that the cross section of the branched intake passage cannot be made very small, this makes it difficult to form a strong swirl within the combustion chamber during low load operation.

特開昭33−.23!f; / 7号公報には、コ個の
吸気ポートを有するエンジンの吸気装置′において、各
々の吸気ポートに断i¥1′I積の小さな補助吸気通路
を開口させ、低負荷運転時にこの補助吸気通路から細い
高速吸気流を吹き込むようにする技術が開示されている
。この公報に記載されたエンジン吸気装置は、低負荷運
転時に燃焼室内に吹き込ブれる高速吸気流により燃焼室
の中央付近、製に点火栓の近傍に激しい乱流を形成させ
て、点火栓まわりの掃気を促進し、火焔伝播速度を高め
て、安定した燃焼を行なわせようとするものである。し
かt/ 、この吸気装置では、エンジン負荷が非常に小
さい運転状態、たとえばアイドリング運転時に補助吸気
通路がその効果全発揮するが、エンジン負荷が僅かでも
増大した運転領域では、この補助吸気通路のみでは十分
欧吸気蒙を確保できなくな之ので、各吸気ポートに連続
する分岐吸気通路を開く必要が生ずる。そして、このよ
うに分岐吸気油路が僅かでも開かれると、補助吸気通路
からの吸気流の流速は急徴に低下し、燃焼室内の乱流が
弱められる。したがって、この吸気装置は、エンジン負
荷がアイドリンク状態より僅かに直くなった領域から中
負荷領域にわたって満足できるほど安定した燃焼状態ケ
与えることはできない。
Unexamined Japanese Patent Publication No. 1973-. 23! f; / Publication No. 7 discloses that in an engine intake system having 7 intake ports, each intake port is opened with a small auxiliary intake passage with a cross section of i\1'I, and this auxiliary intake passage is used during low-load operation. A technique is disclosed in which a narrow high-speed intake air flow is blown from an intake passage. The engine intake system described in this publication uses the high-speed intake air that blows into the combustion chamber during low-load operation to form intense turbulence near the center of the combustion chamber and near the ignition plug. The aim is to promote stable combustion by promoting scavenging and increasing the flame propagation speed. However, in this intake system, the auxiliary intake passage exerts its full effect during operating conditions where the engine load is very low, such as idling, but in operating areas where the engine load increases even slightly, the auxiliary intake passage alone is insufficient. Since it is not possible to secure a sufficient amount of intake air, it becomes necessary to open a branch intake passage that is continuous with each intake port. When the branch intake oil passage is opened even slightly in this manner, the flow velocity of the intake air flow from the auxiliary intake passage decreases rapidly, and the turbulent flow within the combustion chamber is weakened. Therefore, this intake system cannot provide a satisfactorily stable combustion condition over a range from a region where the engine load is slightly above the idle state to a medium load region.

(発明の目的) 本発明は、一つの燃焼室に複数の吸気ポートを開口略せ
て高負荷運転時に吸気の高充填1全確保できるようにし
た吸気装置において、低負荷運転領域の比較的広い範囲
にわたり燃焼室に強いスワールを形成てき、それによっ
て良好な燃焼状態を得ることができるようにすること全
目的とする。
(Objective of the Invention) The present invention provides an intake system that can omit opening a plurality of intake ports in one combustion chamber to ensure high intake air filling during high-load operation, over a relatively wide range of low-load operation. The overall purpose is to form a strong swirl in the combustion chamber over a period of time, thereby making it possible to obtain good combustion conditions.

(発明の構成) 上記目的を達成するため、本発明は次の構11+2を有
する。すなわち、本発明によるエンジンの吸気装置は、
燃焼室に開口する枚数の@気?−トと、前記4数の吸気
ポートのそれぞれに接続された分岐吸気通路と、前記分
岐吸気通路の上流側1に接続きれた主吸気通路と、前記
主吸気iJJ路内に設けられ高負荷運転時に開かれる開
閉弁と、前記開閉弁より上流側において前記主吸気通路
の底部に設けた開口により前記主吸気通路から分岐して
前記吸気ポートの一方に接続される補助吸気通路とケ有
し、前記補助脚り通路が主級気J〜路から分岐する前記
開口はその中心が前記主吸気通路の中心に対し前記一方
の吸気ポートの位置する(illと反対(ill1に偏
って配置されたこと全特徴とする。本発明のこの構成に
よれば、開閉弁が閉じられる低負荷運転領域では、吸気
は補助吸気通路のみから供給される。そして、補助吸気
通路は分岐吸気通路の下イ目11全通り吸気ポートに開
口するので、畷気流は比較的浅い角度で、すなわち燃焼
室の軸線に対し伯′角に近い角度で燃焼室に向けられる
とともに、その吸気流は一方の吸気ポートのみから燃焼
室の軸線に対し側方に偏った位置で該燃焼♀に送り込ま
れることKなシ、燃焼室の軸g!1わりに強い旋回流す
なわちスワールを形成する。
(Structure of the Invention) In order to achieve the above object, the present invention has the following structure 11+2. That is, the engine intake device according to the present invention has the following features:
@Ki of the number of sheets opening into the combustion chamber? - a branch intake passage connected to each of the four intake ports, a main intake passage connected to the upstream side 1 of the branch intake passage, and a main intake passage provided in the main intake iJJ passage for high-load operation. an on-off valve that opens when the on-off valve opens, and an auxiliary intake passage that branches from the main intake passage and connects to one of the intake ports through an opening provided at the bottom of the main intake passage upstream of the on-off valve; The center of the opening where the auxiliary leg passage branches from the main intake passage is located opposite to the one intake port (ill) with respect to the center of the main intake passage. According to this configuration of the present invention, in the low-load operation region where the on-off valve is closed, intake air is supplied only from the auxiliary intake passage. Since the entire intake port opens, the airflow is directed into the combustion chamber at a relatively shallow angle, that is, at an angle close to an angle with respect to the axis of the combustion chamber, and the intake airflow is directed toward the combustion chamber from only one intake port. Since it is not fed into the combustion chamber at a position that is deviated to the side with respect to the axis of the chamber, a strong turning flow, or swirl, is formed relative to the axis g of the combustion chamber.

前述の植開昭、t、!;−,23!; / 7号公報に
記載された吸気装置は、燃焼室内にスワールを発生させ
る構成では、強い乱流行燃焼室固壁に沿って発生し、中
央付近には発生しにくくなるため、点火栓を中央付近に
謝いたエンジンでは良好な燃焼が維持できない、との認
識に基づいて、a伽の吸気ポ−トのそれぞ名、に小径の
補助吸気通路を開口さゼ、それらの補助吸気通路から細
い高速流を燃焼室に対称に吹き込むことにより、燃焼室
中央付近に激しい乱流ゲ生じさせようとするものである
。本発明は、このような公知の吸気装Uとかlす、比較
的小?もった高速吸気流全燃焼室の細心に対して偏った
方向に吹き込むことにより、燃焼室内に強いスワールを
発生きせるものである。特に、本発明においては、補助
吸気ポートが主吸気通路から分岐する部分の開口が、そ
の中心を主吸気通路の中心に対し偏って自iffされ、
その偏りの方向け、該補助吸気通路が接続される吸気醪
−トの偏り方向とけ反対である。したがって、補助吸気
1ffJ路からの吸気流の吹き出しロケ燃焼室の周方向
に向けて形成し、スワールの発生傾向會強めるようにし
ても、補助吸気通路に極端な開力をつける必要がなくカ
リ、吸気抵抗の小さい補助吸気通路を形成することが可
能になる。
The aforementioned Akira Uekai, t,! ;-,23! / The intake system described in Publication No. 7 has a configuration that generates swirl in the combustion chamber, and strong turbulence occurs along the solid wall of the combustion chamber, and is less likely to occur near the center, so the ignition plug is placed in the center. Based on the recognition that it is not possible to maintain good combustion in the engine that was used in the vicinity, small-diameter auxiliary intake passages were opened in each of the intake ports of the a-ga, and from these auxiliary intake passages a thin By blowing a high-speed flow symmetrically into the combustion chamber, the aim is to create severe turbulence around the center of the combustion chamber. The present invention uses such a known intake system U, which is relatively small. A strong swirl is generated within the combustion chamber by blowing the high-speed intake air into the combustion chamber in a direction that is biased against the fine details of the entire combustion chamber. In particular, in the present invention, the opening of the portion where the auxiliary intake port branches from the main intake passage is self-aligned with its center offset from the center of the main intake passage,
The direction of the bias is opposite to the direction of bias of the intake mortar to which the auxiliary intake passage is connected. Therefore, even if the intake flow from the auxiliary intake 1ffJ passage is formed toward the circumferential direction of the combustion chamber to increase the tendency for swirl to occur, there is no need to apply extreme opening force to the auxiliary intake passage. It becomes possible to form an auxiliary intake passage with low intake resistance.

(発明の効果) 本発明によれば、低負荷運転領域で使用される補助吸気
通路≠・、千[捗気通路の底部から分岐しているので、
該補助吸気通路は主[F]気辿路および補助+4夕気通
路の下側を辿り吸気ポートに開口することになり、しか
もこの補助吸気通路は一方の吸気ポートに接続されてい
るので、低負荷:IW転時の比較的少い愕気浦によって
も燃焼室内に強いスワールを形成でき、燃焼の安定性を
確保できる。また、補助吸気通路が主吸気通路から分岐
する部分の開口は、その中心が、主+9j気通路の中心
に対し、該補助吸気通路の接続され、た吸気ポートとけ
反対側に偏って配置官ねるので、補助吸気通路と1及気
ポートとの接続部の方向を燃焼室の周方向に向けてスワ
ールが形成されやすいようにしても、補助吸気通路に極
端な曲力をつける必要か斤<、1hシ(利払の小さい理
想的な補助吸気通路を形成することが可能になる。才た
、補助吸気通路が上述のように偏った位Wで主吸気通路
から分岐しているので、開閉弁が開き始める負荷領域で
、4数の吸気ボート全曲る吸気流のωr、量が不均等に
なり、その結果ある程度のスワールを発生することも期
待できる。
(Effects of the Invention) According to the present invention, since the auxiliary intake passage used in the low-load operation region is branched from the bottom of the intake passage,
The auxiliary intake passage follows the lower side of the main [F] air passage and the auxiliary +4 evening air passage and opens into the intake port, and since this auxiliary intake passage is connected to one intake port, the low Load: Even with a relatively small amount of air pressure during IW rotation, a strong swirl can be formed in the combustion chamber, ensuring combustion stability. Furthermore, the center of the opening at the part where the auxiliary intake passage branches from the main intake passage is biased toward the center of the main +9j air passage and the opposite side of the intake port to which the auxiliary intake passage is connected. Therefore, even if the direction of the connection between the auxiliary intake passage and the first air port is oriented toward the circumferential direction of the combustion chamber to facilitate formation of swirl, it is not necessary to apply extreme bending force to the auxiliary intake passage. 1h (It is possible to form an ideal auxiliary intake passage with small interest payments.As the auxiliary intake passage branches off from the main intake passage at a biased point W as described above, the opening/closing valve In the load range where the intake airflow starts to open, the amount of intake airflow ωr that all four intake boats curve becomes uneven, and as a result, it can be expected that a certain amount of swirl will occur.

(*施例の説明) 界7図および算2図を参照すると、エンジンEはシリン
ダが718?有するシリンダブロックlと該シリンダブ
ロック1の上部に増付けらねたシリンダヘッド2全治し
、シリンダボア】a内にはピストン8が軸方向性後動自
在に配置されて、シリンダボアla内に燃焼室4.’t
thffする。シリンダヘッド2には第1および第2吸
気Ft?−)5.(Sと排気ポート7が形成六ね、泥1
1第2吸気ポート5.6にはそれぞれ吻気弁8が、排気
yJ?−ドアには排気弁9が取付けらiする。第1図を
参照すると、第7、第2吸気ポート5.6けほぼ同径で
、シリンダブロックlの巾方向のシリンダ中心線)に関
してほぼ対称に配置され、排気ポート7はシリンダブロ
ックlの長手方向中心線mをけづんで餓2吸気ボート6
と対向する位置に配置されてい・ る。
(*Explanation of example) Referring to Figure 7 and Figure 2, engine E has cylinders 718? A cylinder block l having a cylinder block 1 and a cylinder head 2 added to the upper part of the cylinder block 1 have been completely repaired, and a piston 8 is disposed in the cylinder bore 1a so as to be able to move freely in the axial direction, and a combustion chamber 4 is formed in the cylinder bore 1a. .. 't
thff. The cylinder head 2 has first and second intake Ft? -)5. (S and exhaust port 7 form six, mud 1
1. The second intake port 5.6 has a nascent valve 8, respectively, and the exhaust yJ? - An exhaust valve 9 is attached to the door. Referring to FIG. 1, the seventh and second intake ports 5 and 6 have approximately the same diameter and are arranged approximately symmetrically with respect to the cylinder center line in the width direction of the cylinder block l, and the exhaust port 7 is located along the longitudinal axis of the cylinder block l. Staring 2 intake boat 6 with direction center line m
It is placed in a position facing the

吸気系は、エアクリーナlOから処びる主吸気通路11
を有し、該主吸気通路11内には絞り弁12が配置解さ
れている。第1図に示すように、主吸気通路11は、シ
リンダヘッド2内に延びて、吸気ポート5.6の近傍で
、シリンダブロック巾万同のシリンダ中心線lにほぼ沿
うように形成された仕切壁14により仕切られて、それ
ぞれ泥へ第2吸気ボート5.6に通じる第1.第2分岐
通路15.16ケ構成している。排気ポート7は、排気
細路17に接続されて排気系を構成する。この排気系F
i普通の構成でよい。主吸気通路11には、仕切壁14
の土泥側に燃料噴射弁28が配性され、エンジン運転φ
件に対応する信号に基づいて計量された燃料が燃焼室4
に供給きれる。主吸気通路11内には、開閉弁18が役
目られている。
The intake system includes a main intake passage 11 leading from the air cleaner lO.
A throttle valve 12 is disposed within the main intake passage 11. As shown in FIG. 1, the main intake passage 11 extends into the cylinder head 2, and is formed in the vicinity of the intake port 5.6 by a partition formed substantially along the cylinder center line l with the same cylinder block width. A first intake boat 5.6 is separated by a wall 14 and opens into a second intake boat 5.6, respectively. There are 15.16 second branch passages. The exhaust port 7 is connected to the exhaust narrow passage 17 to constitute an exhaust system. This exhaust system F
iA normal configuration is sufficient. The main intake passage 11 has a partition wall 14
A fuel injection valve 28 is arranged on the mud side of the engine, and the engine operation φ
The fuel metered based on the signal corresponding to the
can be supplied to. An on-off valve 18 serves within the main intake passage 11.

この開門弁18は、たとえば絞り弁12.に連F11さ
れて該絞多弁の開度が比較的小さい低負荷運転領域では
閉じられ、絞り弁12が所定一度を越えて開かれたとき
開かれるように構成される。主吸気通路11の底部には
、開閉弁18より僅か上#L側に開口19が形成され、
この−口19から主吸気通路11の下側を延びるように
補助吸気】山路20が形成されている。補助吸気通路2
0は、主吸気通路11の下(jullから第1分岐通路
J5の下側を通り、開口21により第1吸気口5に接続
されている。第2図に示すように、吸気永−ト5け、高
9荷逢転時の高光填量を命保するために、シリンダポア
1a17)IlIIl!糾方向に近い角1tで燃燐♀4
に開口しており、図には示していないが、第コ吸気ポー
ト6もド1様な形状である。こねに対し、補助吸気通路
2(1は主吸気通路11および第1分岐通路15の下側
・から第1吸気ポート5に開口しているので、燃焼室4
4に対し比較的浅角度で向けら引ることになる。さらに
、枦l吸気ポート5け、シリンダポアlaの中心線Jに
対し一方に偏って配置されてい、るので、補助吸気通路
20から浅い角度で燃焼室Φに噴出する吸気流は、燃焼
室4内で水平面内の強い旋回流すなわちスワール會発生
する。
This opening valve 18 is, for example, a throttle valve 12. In connection with F11, the throttle valve is closed in a low load operating range where the opening degree is relatively small, and is configured to be opened when the throttle valve 12 is opened more than a predetermined number of times. An opening 19 is formed at the bottom of the main intake passage 11 on the #L side slightly above the on-off valve 18.
An auxiliary intake mountain passage 20 is formed to extend below the main intake passage 11 from the opening 19. Auxiliary intake passage 2
0 passes under the main intake passage 11 (from the jull) below the first branch passage J5 and is connected to the first intake port 5 through the opening 21. As shown in FIG. In order to preserve the high light filling amount when the high 9 load is applied, the cylinder pore 1a17) IlIIl! Combustion phosphorus ♀4 at the corner 1t close to the direction of burning
Although not shown in the figure, the third intake port 6 also has a shape similar to that of the first. In contrast, since the auxiliary intake passage 2 (1 is open to the first intake port 5 from the lower side of the main intake passage 11 and the first branch passage 15), the combustion chamber 4
4, it will be pulled at a relatively shallow angle. Furthermore, the five intake ports are arranged biased to one side with respect to the center line J of the cylinder pore la, so that the intake air flowing from the auxiliary intake passage 20 into the combustion chamber Φ at a shallow angle is directed into the combustion chamber 4. , a strong swirling flow in the horizontal plane, ie, a swirl, occurs.

このスワールを発生しやすくするためには、袖助労気通
路20の形状を、開口21の近傍でシリンダポアlaの
周壁に対しほぼ接続方向に同くように形成することが望
普しい。このような形状にするためには、補助吸気通路
2()を彎曲させることが必要になる。しかし、第1図
に示すように、補助吸気通路2()け、主吸気通路11
から分岐する部分の開口19が、その中心ケ主吸気通路
11の中心に対し第1吸気z −ト5とは反対側すなわ
ち第2吸気ボート0の佃1に寄ゼてIV f−さノ1て
いるので、開口2]の近傍でシリンダポア1aの周方向
に沿った形状とするばあいにも、該補助吸気通路20に
極端な曲りを与える必要がなくなり、第1図に示すよう
に比較的なだらかな流路抵抗の少ない形状とすることが
できる。
In order to facilitate the generation of this swirl, it is desirable that the shape of the sleeve assisting air passage 20 be formed in the vicinity of the opening 21 in substantially the same way as the circumferential wall of the cylinder pore la in the connecting direction. In order to obtain such a shape, it is necessary to curve the auxiliary intake passage 2(). However, as shown in FIG.
The opening 19 of the part branching from the main intake passage 11 is located on the side opposite to the first intake port 5 with respect to the center of the main intake passage 11; Therefore, even if the shape is shaped along the circumferential direction of the cylinder pore 1a in the vicinity of the opening 2, there is no need to give the auxiliary intake passage 20 an extreme bend, and as shown in FIG. The shape can be a gentle flow path with low resistance.

開閉弁18が閉じられる低餉荷領域では、主吸気コ…路
11を通る吸気はすべて開口18から補助11や気通路
20に導かれ、開口21から第1吸気ポート5を経て燃
焼室に送り込1れる。神助1汐気通路20け分岐通路1
5,16の各々に比し断面積が小さいので、吸気鍮の小
さい低負荷運転時にも比較的高い流速を保つことができ
る。さらに、補助吸気ilQ路20は81[述のように
比較的浅い角度でシリンダポアlaの円周方向に向Vj
られているので、該補助吸気通路20から燃焼室4 V
CC出出れる暖気流は、燃焼室4内で強いスワールを形
成する。第1図に示すように、本実施例においては、シ
リンダヘッド2の吸、排気?−トがJに成づれていない
部分、すなわぢシリンダブロックJの長生方向中心線m
を挾んでl)4/吸気ボート5と対向する部分に点火栓
22が取付けられている。したがって、点火栓22は、
補助吸気通路20からの吸気流が形成するスワールの旋
回軌跡上に位置するので、該点火栓22の近傍には確実
に新鮮な混合気が供給され、良好な着火性をもって燃焼
が行なわれる。
In the low-load region where the on-off valve 18 is closed, all the intake air passing through the main intake channel 11 is guided from the opening 18 to the auxiliary 11 and the air passage 20, and is sent from the opening 21 to the combustion chamber via the first intake port 5. Includes 1. Kamisuke 1 Shioki passage 20 branches branch passage 1
Since the cross-sectional area is smaller than those of Nos. 5 and 16, a relatively high flow rate can be maintained even during low-load operation with a small intake brass. Furthermore, the auxiliary intake ilQ passage 20 is 81 [as described above, directed at a relatively shallow angle in the circumferential direction of the cylinder pore
4 V from the auxiliary intake passage 20 to the combustion chamber.
The warm air flowing out of the CC forms a strong swirl within the combustion chamber 4. As shown in FIG. 1, in this embodiment, the cylinder head 2 has intake and exhaust air. - The part where the cylinder block J is not formed into a J shape, i.e. the center line m in the longitudinal direction of the cylinder block J.
An ignition plug 22 is attached to a portion facing the intake boat 5, sandwiching the l)4/ intake boat 5. Therefore, the ignition plug 22 is
Since it is located on the swirl trajectory formed by the intake air flow from the auxiliary intake passage 20, fresh air-fuel mixture is reliably supplied to the vicinity of the ignition plug 22, and combustion is performed with good ignitability.

エンジン負荷の増加に伴ない絞り弁12がPJrw値を
越えて開かれると、開閉弁18も開き始める。
When the throttle valve 12 is opened beyond the PJrw value as the engine load increases, the on-off valve 18 also begins to open.

開閉弁18の一度か比較的小さい運転領域で−、吸気の
一部は依然として補助吸気通路2()を辿って供給され
る。この状態では、補助吸気通路2゜が第1吸気ポート
5のみに開口していることと、補助吸気通路20が主吸
気通路11がら分岐する部分の開口19が第コ吸気ポー
ト6の側に偏って位置することから、第1吸気ポート5
ケ経て燃焼室Φに供給される吸気の齋が第2@気ボート
6を通る量よりも多くなり、その結果として、ある程V
のスワールを負荷が卑大した領域でも形成することがで
きる。
Once or in a relatively small operating range of the switching valve 18, a portion of the intake air is still supplied along the auxiliary intake channel 2(). In this state, the auxiliary intake passage 2° opens only to the first intake port 5, and the opening 19 where the auxiliary intake passage 20 branches from the main intake passage 11 is biased toward the first intake port 6. Since the first intake port 5 is located at
After that, the amount of intake air supplied to the combustion chamber Φ becomes larger than the amount passing through the second air boat 6, and as a result, the V
A swirl can be formed even in areas with heavy loads.

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

第1図は本発明の一実施例を示すエンジン吸気装置の概
略平面図、第1図は本発明を実施例したエンジンの垂直
断面図である。 J、・・・シリンダブロック、1a・・・シリンダポア
、2・・・シリンダヘッド、8・・・ピストン、4・・
・燃焼室、5.6・・・吸気z−1、?・・・排気−−
ト、11・・・主@勿通路、15、lfl・・・分岐吸
気】Ff]路、18・・・開閉弁、19・・・開口、2
0・・・補助吸気通路。 手続補正用 59.10.18 昭和 年 月 日 1、事件の表示 昭和58年特許願第2020/15号
2、発明の名称 エンジンの吸気装置 3、補正をする者 事件との関係 出願人 4、代理人 6、補正の対象 明細書の特許請求の範囲の樅1特許請
求の範囲 燃焼室に開口する複数の吸気ポートと、前記複数の吸気
ポートのそれぞれに接続された分岐吸気通路と、前記分
岐吸気通路の」−流側に接続された主吸気通路と、前記
主吸気通路内に設けられ高負荷運転時に開かれる開閉弁
と、前記開閉弁より上流側において前記主吸気通路に設
けた開口により前記主吸気通路から分岐して前記吸気ポ
ートの一方に接続される補助吸気通路とを有し、前記補
助吸気通路が主吸気通路から分岐する前記開口はその中
心が前記主吸気通路の中心に対し前記一方の吸気ポート
の位置する側と反対側に偏って配置されたことを特徴と
するエンジンの吸気装置。
FIG. 1 is a schematic plan view of an engine intake system showing an embodiment of the present invention, and FIG. 1 is a vertical sectional view of an engine embodying the present invention. J,... Cylinder block, 1a... Cylinder pore, 2... Cylinder head, 8... Piston, 4...
・Combustion chamber, 5.6...Intake z-1, ? ...Exhaust--
G, 11... Main@Normal passage, 15, lfl... Branch intake ]Ff] passage, 18... Opening/closing valve, 19... Opening, 2
0... Auxiliary intake passage. For procedural amendment 59.10.18 Showa year, month, day 1, Indication of case 1988 Patent Application No. 2020/15 2, Title of invention Engine intake device 3, Person making the amendment Relationship to the case Applicant 4, Agent 6, subject of amendment: Claims in the specification: Claim 1: A plurality of intake ports opening into a combustion chamber, a branch intake passage connected to each of the plurality of intake ports, and a branch intake passage connected to each of the plurality of intake ports; A main intake passage connected to the downstream side of the intake passage, an on-off valve provided in the main intake passage that opens during high-load operation, and an opening provided in the main intake passage upstream of the on-off valve. an auxiliary intake passage that branches from the main intake passage and is connected to one of the intake ports, and the opening where the auxiliary intake passage branches from the main intake passage has its center relative to the center of the main intake passage. An intake device for an engine, characterized in that it is disposed biased toward a side opposite to the side where the one intake port is located.

Claims (1)

【特許請求の範囲】[Claims] 燃焼室に開口する複数の吸気ポートと、前記検数の吸気
ポートのそれぞれに接続さ力た分岐吸気通路と、前記分
岐吸気通路の上流(illに接続さり、た主吸気通路と
、前記主吸気通路内に設けられ高負荷運転時に開かれる
開閉弁と、前記開閉弁より上流側において前記主吸気通
路の底部に設けた開口により前記主吸気通路から分岐し
て前記吸気2−トの一方に接続される補助吸気通路と分
有し、前記補助吸気通路が主吸気通路から分岐する前記
開口はその中心が前記主吸気通路の中心に対し81■記
一方の吸気ポートの位置する側と反対仙に偏って配置さ
れたこと′ft%徴とするエンジンの吸気装置。
a plurality of intake ports opening into the combustion chamber; a branch intake passage connected to each of the intake ports; a main intake passage connected upstream (ill) of the branch intake passage; An on-off valve provided in the passage and opened during high-load operation, and an opening provided at the bottom of the main intake passage on the upstream side of the on-off valve, branching from the main intake passage and connecting to one of the two intake passages. The opening from which the auxiliary intake passage branches from the main intake passage has its center located at 81. An engine intake system characterized by uneven placement.
JP58202045A 1983-09-24 1983-10-28 Suction device of engine Granted JPS6093119A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP58202045A JPS6093119A (en) 1983-10-28 1983-10-28 Suction device of engine
EP84111361A EP0137393B1 (en) 1983-09-24 1984-09-24 Intake arrangement for internal combustion engine
DE8484111361T DE3475419D1 (en) 1983-09-24 1984-09-24 Intake arrangement for internal combustion engine
US06/815,287 US4625687A (en) 1983-09-24 1985-12-27 Intake arrangement for internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58202045A JPS6093119A (en) 1983-10-28 1983-10-28 Suction device of engine

Publications (2)

Publication Number Publication Date
JPS6093119A true JPS6093119A (en) 1985-05-24
JPH0247571B2 JPH0247571B2 (en) 1990-10-22

Family

ID=16451010

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58202045A Granted JPS6093119A (en) 1983-09-24 1983-10-28 Suction device of engine

Country Status (1)

Country Link
JP (1) JPS6093119A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6282513A (en) * 1985-10-05 1987-04-16 Hitachi Electronics Eng Co Ltd Cleaning device for disk member

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5644418A (en) * 1979-09-20 1981-04-23 Honda Motor Co Ltd Device for improving combustion of mixture in four-cycle internal combustion engine
JPS58183818A (en) * 1982-04-21 1983-10-27 Mazda Motor Corp Suction device of engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5644418A (en) * 1979-09-20 1981-04-23 Honda Motor Co Ltd Device for improving combustion of mixture in four-cycle internal combustion engine
JPS58183818A (en) * 1982-04-21 1983-10-27 Mazda Motor Corp Suction device of engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6282513A (en) * 1985-10-05 1987-04-16 Hitachi Electronics Eng Co Ltd Cleaning device for disk member
JPH0572011B2 (en) * 1985-10-05 1993-10-08 Hitachi Electr Eng

Also Published As

Publication number Publication date
JPH0247571B2 (en) 1990-10-22

Similar Documents

Publication Publication Date Title
JPS6025604B2 (en) Intake control method for internal combustion engine
JPS58187519A (en) Intake device of engine
JPS6060009B2 (en) Intake system for multi-cylinder internal combustion engine
JP3329935B2 (en) Intake device for internal combustion engine
JPS6093119A (en) Suction device of engine
JP3386588B2 (en) Engine intake control device
US4464312A (en) Carburetor for internal combustion engines
JP2002221036A (en) Intake system for engine
JP2501556Y2 (en) Internal combustion engine intake system
JPS6062655A (en) Intake device of v-type engine
JPS6353375B2 (en)
GB2087479A (en) Ic engine mixture intake system
JPS6335167Y2 (en)
JPH021476Y2 (en)
JPS6093121A (en) Suction device of engine
JPS60101224A (en) Intake-air device in engine
JPS588230A (en) Suction device for multi-cylinder internal combustion engine
JPH0247572B2 (en)
JPS60198327A (en) Intake device for engine
JPS59147867A (en) Fuel injection type internal-combustion engine
JPS6027781Y2 (en) Internal combustion engine air supply system
JPS5862317A (en) Suction system of multicylinder internal-combustion engine
JPH0439413Y2 (en)
JPS597539Y2 (en) Double intake internal combustion engine
JPS5813080Y2 (en) engine intake system