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JPH0247571B2 - - Google Patents
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JPH0247571B2 - - Google Patents

Info

Publication number
JPH0247571B2
JPH0247571B2 JP58202045A JP20204583A JPH0247571B2 JP H0247571 B2 JPH0247571 B2 JP H0247571B2 JP 58202045 A JP58202045 A JP 58202045A JP 20204583 A JP20204583 A JP 20204583A JP H0247571 B2 JPH0247571 B2 JP H0247571B2
Authority
JP
Japan
Prior art keywords
intake passage
intake
combustion chamber
main
auxiliary
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP58202045A
Other languages
Japanese (ja)
Other versions
JPS6093119A (en
Inventor
Koichi Hatamura
Koji Asaumi
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
    • 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
    • F02B31/00Modifying induction systems for imparting a rotation to the charge in the cylinder
    • F02B31/08Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air inlets
    • F02B31/085Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air inlets having two inlet valves
    • 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
    • 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

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

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、殊に一つの燃
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つた形式のエンジン
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, particularly 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 has come to be selectively used depending on 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を設け、
それら吸気ポートを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
56−44419号公報に開示されたエンジンでは、シ
リンダヘツドに形成された2個の吸気ポートのそ
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通路に接続されている。そし
て、一方の分岐吸気通路には開閉弁が、主吸気通
路には絞り弁がそれぞれ設けられており、この絞
り弁と開閉弁とは連動して、絞り弁が一定開度を
越えて開かれたとき開閉弁が開かれるようになつ
ている。すなわち、一方の分岐吸気通路は、エン
ジンの低負荷運転時には開閉弁により閉じられて
いるため、吸気は他方の分岐吸気通路のみから比
較的高い流速で供給され、高負荷運転時には吸気
は両方の分岐吸気通路から供給されて高い充填量
を確保することができる。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
時に十分な吸気充填量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
ど小さく形成されておらず、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領域で
は、吸気流速を十分に高めることができない。ま
た、吸気ポートの形状は、高負荷運転時の高充填
量確保のために、吸気流を燃焼室の軸線方向にほ
ぼ沿つて導入するようになつており、このこと
は、分岐吸気通路の断面積をあまり小さくできな
いことと相まつて、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している。
(Prior art) Multiple intake ports are provided in the combustion chamber of the engine,
It is known to selectively use these intake ports depending on the engine load. For example,
In the engine disclosed in Japanese Patent No. 56-44419, a branch intake passage is connected to each of two intake ports formed in the cylinder head, and the branch intake passages are connected to a common main intake passage. 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 prevent the throttle valve from opening beyond a certain degree. The on-off valve is designed to open when the In other words, one branch intake passage is closed by an on-off valve when the engine is operating at low load, so intake air is supplied at a relatively high flow rate only from the other branch intake passage, and during high load operation, intake air is supplied from both branches. It is supplied from the intake passage and can ensure a high filling amount. However, since the engine intake system described in this publication is intended to ensure a sufficient amount of intake air during high-load operation, the cross-sectional area of each branch intake passage is not formed so small. First, even if only one branch intake passage is used during low-load operation, the intake flow rate cannot be sufficiently increased in an operating region where the load is very small, such as during idling. In addition, the shape of the intake port is designed to introduce the intake air flow almost along the axial direction of the combustion chamber in order to ensure a high filling amount during high-load operation. Coupled with the fact that the area cannot be made very small, this makes it difficult to form a strong swirl inside the combustion chamber during low load operation.

特開昭55−25511号公報には、2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
吸気ポートに断面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まれる高速
吸気流により燃焼室の中央付近、特に点火栓の近
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。しかし、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
通路がその効果を発揮するが、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
のみでは十分な吸気量を確保できなくなるので、
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通路が僅
かでも開かれると、補助吸気通路からの吸気流の
流速は急激に低下し、燃焼室内の乱流が弱められ
る。したがつて、この吸気装置は、エンジン負荷
がアイドリング状態より僅かに高くなつた領域か
ら中負荷領域にわたつて満足できるほど安定した
燃焼状態を与えることはできない。
Japanese Patent Laid-Open No. 55-25511 discloses that in an engine intake system having two intake ports, an auxiliary intake passage with a small cross-sectional area is opened in each intake port, and a thin air passage is opened from this auxiliary intake passage during low-load operation. Techniques have been disclosed for providing high-velocity intake air flow. The engine intake system described in this publication uses a high-speed intake air flow blown into the combustion chamber during low-load operation to form intense turbulence near the center of the combustion chamber, especially near the ignition plug, thereby scavenging air around the ignition plug. The aim is to promote stable combustion by increasing the flame propagation speed. However, with this intake system, although the auxiliary intake passage is effective in operating conditions where the engine load is very low, such as idling, in operating areas where the engine load increases even slightly, the auxiliary intake passage alone is insufficient. Since the amount of intake air cannot be secured,
It becomes necessary to open a branch intake passage that is continuous with each intake port. When the branch intake passage is opened even slightly in this way, 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 region where the engine load is slightly higher than the idling 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
開口させて高負荷運転時に吸気の高充填量を確保
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
ールを形成でき、それによつて良好な燃焼状態を
得ることができるようにすることを目的とする。
(Objective of the Invention) The present invention provides an intake system in which a plurality of intake ports are opened in one combustion chamber to ensure a high filling amount of intake air during high-load operation, over a relatively wide range of low-load operation. It is an object of the present invention to form a strong swirl in a combustion chamber throughout the combustion chamber, thereby making it possible to obtain a good combustion state.

(発明の構成) 上記目的を達成するため、本発明は次の構成を
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2つの吸気ポートと、
前記2つ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燃焼室に
対しほぼ円周方向に向くように前記吸気ポートの
一方に接続される補助吸気通路とを有し、前記2
つの吸気ポートは前記主吸気通路の中心線に関し
両側に配置され、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
側と反対側に偏つて配置されたことを特徴とす
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
吸気通路の下側を通り吸気ポートに開口するの
で、吸気流は比較的浅い角度で、すなわち燃焼室
の軸線に対し直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つた位置で該燃
焼室に送り込まれることになり、燃焼室の軸線ま
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. That is, the engine intake device according to the present invention includes two intake ports opening into the combustion chamber;
a branch intake passage connected to each of the two intake ports, a main intake passage connected to the upstream side of the branch intake passage, and an on-off valve provided in the main intake passage and opened during high-load operation; an auxiliary intake passage that branches from the main intake passage through an opening provided in the main intake passage on an upstream side of the on-off valve and is connected to one of the intake ports so as to face approximately circumferentially with respect to the combustion chamber; and the above 2
The two intake ports are arranged on both sides of the center line of the main intake passage, and the opening where the auxiliary intake passage branches from the main intake passage has its center located at the center of the one intake port with respect to the center of the main intake passage. It is characterized by being biased toward the opposite side. According to this configuration of the present invention, in a low-load operating region where the on-off valve is closed, intake air is supplied only from the auxiliary intake passage. Since the auxiliary intake passage passes under the branch intake passage and opens into the intake port, the intake air flow is directed toward the combustion chamber at a relatively shallow angle, that is, at an angle close to perpendicular to the axis of the combustion chamber. The intake air flow is sent into the combustion chamber from only one intake port at a position offset laterally with respect to the axis of the combustion chamber, forming a strong swirl around the axis of the combustion chamber.

前述の特開昭55−25511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、強い乱流は燃焼室固壁に沿つて発生し、中
央付近には発生しにくくなるため、点火栓を中央
付近に置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、2個の吸気ポートの
それぞれに小径の補助吸気通路を開口させ、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
乱流を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置と異り、比較的巾
をもつた高速逆気流を燃焼室の軸心に対して偏つ
た方向に吹き込むことにより、燃焼室内に強いス
ワールを発生させるものである。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
に対し偏つて配置され、その偏りの方向は、該補
助吸気通路が接続される吸気ポートの偏り方向と
は反対である。したがつて、補助吸気通路からの
吸気流の吹き出し口を燃焼室の周方向に向けて形
成し、スワールの発生傾向を強めるようにして
も、補助吸気通路に極端な曲りをつける必要がな
くなり、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 intake system described in the above-mentioned Japanese Patent Application Laid-Open No. 55-25511 has a configuration that generates swirl within the combustion chamber, and strong turbulence occurs along the solid walls of the combustion chamber and is less likely to occur near the center. Therefore, based on the recognition that good combustion cannot be maintained in an engine with the spark plug placed near the center, a small diameter auxiliary intake passage is opened in each of the two intake ports, and a thin By blowing a high-speed flow symmetrically into the combustion chamber, the aim is to create intense turbulence near the center of the combustion chamber. Unlike such known intake devices, the present invention generates a strong swirl inside the combustion chamber by blowing a relatively wide high-speed reverse airflow in a direction biased to the axis of the combustion chamber. It is. In particular, in the present invention, the opening of the portion where the auxiliary intake port branches from the main intake passage is arranged with its center offset from the center of the main intake passage, and the direction of the deviation is in the direction of the opening where the auxiliary intake passage is connected. This is opposite to the direction of deflection of the intake port. Therefore, even if the outlet of the intake air from the auxiliary intake passage is formed to face the circumferential direction of the combustion chamber to increase the tendency for swirl to occur, there is no need to make an extreme bend in 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
補助吸気通路が、主吸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吸気通路および補
助吸気通路の下側を通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、低負荷運転時の比
較的少い吸気流によつ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、主吸気通路の中心に対
し、該補助吸気通路の接続された吸気ポートとは
反対側に偏つて配置されるので、補助吸気通路と
吸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りをつける必要がなく、
吸気抵抗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。また、補助吸気通路が上述
のように偏つた位置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、複数の
吸気ポートを通る吸気流の流量が不均等になり、
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 branches from the bottom of the main intake passage, the auxiliary intake passage is located below the main intake passage and the auxiliary intake passage. Since this auxiliary intake passage is connected to one of the intake ports, it is possible to create a strong swirl inside the combustion chamber even with a relatively small intake air flow during low-load operation. can be formed and ensure combustion stability. Furthermore, the center of the opening of the part where the auxiliary intake passage branches off from the main intake passage is located on the opposite side of the center of the main intake passage from the intake port to which the auxiliary intake passage is connected. , even if the direction of the connection between the auxiliary intake passage and the intake port is oriented in the circumferential direction of the combustion chamber so that swirl is more likely to be formed,
There is no need to make extreme bends in the auxiliary intake passage,
It becomes possible to form an ideal auxiliary intake passage with low intake resistance. In addition, since the auxiliary intake passage branches off from the main intake passage at an uneven position as described above, the flow rate of the intake air passing through the multiple intake ports becomes uneven in the load region where the on-off valve begins to open.
As a result, it can be expected that a certain amount of swirl will be generated.

(実施例の説明) 第1図および第2図を参照すると、エンジンE
はシリンダボア1aを有するシリンダブロツク1
と該シリンダブロツク1の上部に取付けられたシ
リンダヘツド2を有し、シリンダボア1a内には
ピストン3が軸方向往復動自在に配置されて、シ
リンダボア1a内に燃焼室4を形成する。シリン
ダヘツド2には第1および第2吸気ポート5,6
と排気ポート7が形成され、第1、第2吸気ポー
ト5,6にはそれぞれ吸気弁8が、排気ポート7
には排気弁9が取付けられる。第1図を参照する
と、第1、第2吸気ポート5,6はほぼ同径で、
シリンダブロツク1の巾方向のシリンダ中心線l
に関してほぼ対称に配置され、排気ポート7はシ
リンダブロツク1の長手方向中心線mをはさんで
第2吸気ポート6と対向する位置に配置されてい
る。
(Description of Examples) Referring to FIGS. 1 and 2, engine E
is a cylinder block 1 having a cylinder bore 1a.
The engine has a cylinder head 2 attached to the upper part of the cylinder block 1, and a piston 3 is disposed within the cylinder bore 1a so as to be able to reciprocate in the axial direction, thereby forming a combustion chamber 4 within the cylinder bore 1a. The cylinder head 2 has first and second intake ports 5, 6.
and an exhaust port 7 are formed, an intake valve 8 is formed in the first and second intake ports 5 and 6, and an exhaust port 7 is formed in the first and second intake ports 5 and 6, respectively.
An exhaust valve 9 is attached to the. Referring to FIG. 1, the first and second intake ports 5 and 6 have approximately the same diameter;
Cylinder center line l in the width direction of cylinder block 1
The exhaust port 7 is arranged at a position facing the second intake port 6 across the longitudinal centerline m of the cylinder block 1.

吸気系は、エアクリーナ10から延びる主吸気
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、シリンダヘツド2内に延びて、
吸気ポート5,6の近傍で、シリンダブロツク巾
方向のシリンダ中心線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、それぞれ第
1、第2吸気ポート5,6に通じる第1、第2分
岐通路15,16を構成している。排気ポート7
は、排気通路17に接続されて排気系を構成す
る。この排気系は普通の構成でよい。主吸気通路
11には、仕切壁14の上流側に燃焼噴射弁23
が配置され、エンジン運転条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に供給され
る。主吸気通路11内には、開閉弁18が設けら
れている。この開閉弁18は、たとえば絞り弁1
2に運転されて該絞り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が所定開
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
僅か上流側に開口19が形成され、この開口19
から主吸気通路11の下側を延びるように補助吸
気通路20が形成されている。補助吸気通路20
は、主吸気通路11の下側から第1分岐通路15
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、吸気ポート
5は、高負荷運転時の高充填量を確保するため
に、シリンダボア1aの軸線方向に近い角度で燃
焼室4に開口しており、図には示していないが、
第2吸気ポート6も同様な形状である。これに対
し、補助吸気通路20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に対し比較的浅角度で
向けられることになる。さらに、第1吸気ポート
5は、シリンダボア1aの中心線lに対し一方に
偏つ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4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
を発生する。
The intake system has a main intake passage 11 extending from an air cleaner 10, and 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.
In the vicinity of the intake ports 5 and 6, the first and second intake ports 5 and 6 are separated by a partition wall 14 formed substantially along the cylinder center line l in the width direction of the cylinder block, and communicate with the first and second intake ports 5 and 6, respectively. It constitutes second branch passages 15 and 16. Exhaust port 7
is connected to the exhaust passage 17 to constitute an exhaust system. This exhaust system may have a normal configuration. In the main intake passage 11, a combustion injection valve 23 is provided on the upstream side of the partition wall 14.
is arranged, and metered fuel is supplied to the combustion chamber 4 based on a signal corresponding to the engine operating conditions. An on-off valve 18 is provided within the main intake passage 11 . This on-off valve 18 is, for example, a throttle valve 1
2, the throttle valve 12 is closed in a low-load operating range where the opening degree of the throttle valve is relatively small, and is opened when the throttle valve 12 is opened beyond a predetermined opening degree. An opening 19 is formed at the bottom of the main intake passage 11 slightly upstream of the on-off valve 18.
An auxiliary intake passage 20 is formed to extend below the main intake passage 11 from the main intake passage 11 . Auxiliary intake passage 20
is from the bottom of the main intake passage 11 to the first branch passage 15.
The opening 21 passes through the lower side of the opening 21 and is connected to the first intake port 5 . As shown in Fig. 2, the intake port 5 opens into the combustion chamber 4 at an angle close to the axial direction of the cylinder bore 1a in order to ensure a high filling amount during high-load operation. No, but
The second intake port 6 also has a similar shape. On the other hand, since the auxiliary intake passage 20 opens to the first intake port 5 from below the main intake passage 11 and the first branch passage 15, it is oriented at a relatively shallow angle with respect to the combustion chamber 4. . Furthermore, since the first intake port 5 is arranged to be biased to one side with respect to the center line l of the cylinder bore 1a, the intake air jetted into the combustion chamber 4 at a shallow angle from the auxiliary intake passage 20 is directed within the combustion chamber 4. Generates a strong swirl in the horizontal plane.

このスワールを発生しやすくするためには、補
助吸気通路20の形状を、開口21の近傍でシリ
ンダボア1aの周壁に対しほぼ接線方向に向くよ
うに形成することが望ましい。このような形状に
するためには、補助吸気通路20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20は、主吸気通路11から分岐す
る部分の開口19が、その中心を主吸気通路11
の中心に対し第1吸気ポート5とは反対側すなわ
ち第2吸気ポート6の側に寄せて配置されている
ので、開口21の近傍でシリンダボア1aの周方
向に沿つ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 auxiliary intake passage 20 is formed so as to be oriented substantially tangentially to the peripheral wall of the cylinder bore 1a near the opening 21. In order to obtain such a shape, it is necessary to curve the auxiliary intake passage 20. However, as shown in Figure 1,
The auxiliary intake passage 20 has an opening 19 branching from the main intake passage 11 with its center pointing toward the main intake passage 11.
Since it is arranged on the side opposite to the first intake port 5, that is, on the side of the second intake port 6, with respect to the center of the , it is no longer necessary to give the auxiliary intake passage 20 an extreme bend, and as shown in FIG. 1, it is possible to form a relatively gentle flow path with little resistance.

開閉弁18が閉じられる低負荷領域では、主吸
気通路11を通る吸気はすべて開口18から補助
吸気通路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まれる。補助吸気通
路20は分岐通路15,16の各々に比し断面積
が小さいので、吸気量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
助吸気通路20は前述のように比較的浅い角度で
シリンダボア1aの円周方向に向けられているの
で、該補助吸気通路20から燃焼室4に噴出され
る吸気流は、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、
シリンダヘツド2の吸、排気ポートが形成されて
いない部分、すなわちシリンダブロツク1の長手
方向中心線mを挾んで第1吸気ポート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
つて、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、良好な着火性をもつて燃焼が行な
われる。
In a low load region where the on-off valve 18 is closed, all intake air passing through the main intake passage 11 is guided from the opening 18 to the auxiliary intake passage 20, and is sent from the opening 21 through the first intake port 5 into the combustion chamber. Since the auxiliary intake passage 20 has a smaller cross-sectional area than each of the branch passages 15 and 16, a relatively high flow rate can be maintained even during low-load operation with a small intake air amount. Furthermore, since the auxiliary intake passage 20 is oriented in the circumferential direction of the cylinder bore 1a at a relatively shallow angle as described above, the intake air flow injected from the auxiliary intake passage 20 into the combustion chamber 4 is directed within the combustion chamber 4. to form a strong swirl. As shown in FIG. 1, in this example,
An ignition plug 22 is attached to a portion of the cylinder head 2 where intake and exhaust ports are not formed, that is, a portion facing the first intake port 5 across the longitudinal centerline m of the cylinder block 1. Therefore, since the ignition plug 22 is located on the swirl locus 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, resulting in a good air-fuel mixture. Combustion occurs with ignitability.

エンジン負荷の増加に伴ない絞り弁12が所定
値を越えて開かれると、開閉弁18も開き始め
る。開閉弁18の開度が比較的小さい運転領域で
は、吸気の一部は依然として補助吸気通路20を
通つて供給される。この状態では、補助吸気通路
20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から分岐
する部分の開口19が第2吸気ポート6の側に偏
つて位置することから、第1吸気ポート5を経て
燃焼室4に供給される吸気の量が第2吸気ポート
6を通る量よりも多くなり、その結果として、あ
る程度のスワールを負荷が増大した領域でも形成
することができる。
When the throttle valve 12 is opened beyond a predetermined value as the engine load increases, the on-off valve 18 also begins to open. In an operating range where the opening degree of the on-off valve 18 is relatively small, a portion of the intake air is still supplied through the auxiliary intake passage 20. In this state, the auxiliary intake passage 20 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 second intake port 6. Because of this position, the amount of intake air supplied to the combustion chamber 4 via the first intake port 5 is greater than the amount passing through the second intake port 6, and as a result, a certain amount of swirl is generated even in areas where the load is increased. can be formed.

【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2図は本発明を実施例した
エンジンの垂直断面図である。 1…シリンダブロツク、1a…シリンダボア、
2…シリンダヘツド、3…ピストン、4…燃焼
室、5,6…吸気ポート、7…排気ポート、11
…主吸気通路、15,16…分岐吸気通路、18
…開閉弁、19…開口、20…補助吸気通路。
FIG. 1 is a schematic plan view of an engine intake system according to an embodiment of the present invention, and FIG. 2 is a vertical sectional view of an engine embodying the present invention. 1...Cylinder block, 1a...Cylinder bore,
2... Cylinder head, 3... Piston, 4... Combustion chamber, 5, 6... Intake port, 7... Exhaust port, 11
...Main intake passage, 15, 16...Branch intake passage, 18
...Opening/closing valve, 19...Opening, 20...Auxiliary intake passage.

Claims (1)

【特許請求の範囲】[Claims] 1 燃焼室に開口する2つの吸気ポートと、前記
2つ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燃焼室に対し
ほぼ円周方向に向くように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2つの
吸気ポートは前記主吸気通路の中心線に関し両側
に配置され、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
反対側に偏つて配置されたことを特徴とするエン
ジンの吸気通路。
1. Two intake ports opening into the combustion chamber, a branch intake passage connected to each of the two intake ports, a main intake passage connected to the upstream side of the branch intake passage, and a main intake passage within the main intake passage. an on-off valve that is provided and opens during high-load operation; and an opening provided in the main intake passage upstream of the on-off valve so that the main intake passage branches off from the main intake passage and faces approximately circumferentially with respect to the combustion chamber. an auxiliary intake passage connected to one of the intake ports, the two intake ports are arranged on both sides of the center line of the main intake passage, and the opening where the auxiliary intake passage branches from the main intake passage is 1. An intake passage for an engine, wherein the center of the main intake passage is offset to a side opposite to the side where the one intake port is located with respect to the center of the main intake passage.
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 JPS6093119A (en) 1985-05-24
JPH0247571B2 true 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)

Families Citing this family (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

Family Cites Families (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
JPS5936091B2 (en) * 1982-04-21 1984-09-01 マツダ株式会社 engine intake system

Also Published As

Publication number Publication date
JPS6093119A (en) 1985-05-24

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