JPH0480231B2 - - Google Patents

Info

Publication number
JPH0480231B2
JPH0480231B2 JP59068408A JP6840884A JPH0480231B2 JP H0480231 B2 JPH0480231 B2 JP H0480231B2 JP 59068408 A JP59068408 A JP 59068408A JP 6840884 A JP6840884 A JP 6840884A JP H0480231 B2 JPH0480231 B2 JP H0480231B2
Authority
JP
Japan
Prior art keywords
intake passage
valve
intake
passage
downstream
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
JP59068408A
Other languages
Japanese (ja)
Other versions
JPS60212665A (en
Inventor
Katsumi Okazaki
Toshio Nishikawa
Toshimasu Tanaka
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 JP59068408A priority Critical patent/JPS60212665A/en
Publication of JPS60212665A publication Critical patent/JPS60212665A/en
Publication of JPH0480231B2 publication Critical patent/JPH0480231B2/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
    • F02B31/08Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air inlets
    • 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
    • F02B2275/18DOHC [Double overhead camshaft]
    • 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)

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、燃焼室に連通する2つの吸気通路を
備えるとともに、その1つの吸気通路には、該通
路を開閉する開閉弁を備えた燃料噴射式エンジン
に関する。
Detailed Description of the Invention (Industrial Field of Application) The present invention is provided with two intake passages communicating with a combustion chamber, and one of the intake passages is equipped with an on-off valve for opening and closing the passage. Regarding injection type engines.

(従来技術) 燃料噴射弁を備え、複数の吸気通路を燃焼室に
連通させた吸気構造を有するエンジンは公知であ
る。例えば特開昭54−39721号公報に記載された
構造は、燃焼室に通じる低負荷用吸気通路、及び
その上方に形成された高負荷用吸気通路を備える
とともに、さらに、高負荷用吸気通路には低負荷
時に該通路を閉じる開閉弁を備えている。そし
て、燃料噴射弁は、高負荷用吸気通路の開閉弁下
流に、噴射燃料が開閉弁の開閉動作に干渉しない
ように配置される。この構造では、開閉弁が閉じ
ると高負荷用吸気通路を流通うる吸気の流速が低
下するので、燃料の霧化が不十分になる。この問
題を避けるために、燃料噴射弁を低負荷用吸気通
路に配置するようにすると、低負荷用吸気通路は
燃焼室に対して、比較的浅い角度を成すように、
すなわち、ほぼ水平方向に向けられているので、
燃料の噴射方向を燃料室に向けることが難しくな
る。また、低負荷用吸気通路の吸気流は高負荷時
でもそれ程強くならないので、高負荷時における
霧化の効率が低下するという問題がある。また、
実開昭55−4355号公報に記載された構造では、1
つの吸気ポートに通じる低負荷用及び高負荷用吸
気通路を備えており、燃料噴射弁を、該低負荷用
及び高負荷用吸気通路の合流点付近に燃料噴射が
行なわれるように構成して、低負荷時から高負荷
時にわたつて吸気流中に燃料を噴射して霧化の促
進を図つている。しかし、この構造では、燃料が
噴射される位置が燃焼室に極めて近くなるので、
吸気の十分な混合を達成することができない。
(Prior Art) Engines are known that have an intake structure including a fuel injection valve and a plurality of intake passages communicating with a combustion chamber. For example, the structure described in Japanese Patent Application Laid-Open No. 54-39721 includes a low-load intake passage leading to the combustion chamber and a high-load intake passage formed above the low-load intake passage. is equipped with an on-off valve that closes the passage when the load is low. The fuel injection valve is arranged downstream of the on-off valve in the high-load intake passage so that the injected fuel does not interfere with the opening/closing operation of the on-off valve. In this structure, when the on-off valve closes, the flow velocity of the intake air that can flow through the high-load intake passage decreases, resulting in insufficient atomization of the fuel. To avoid this problem, the fuel injection valve is placed in the low-load intake passage, so that the low-load intake passage forms a relatively shallow angle with the combustion chamber.
That is, it is oriented almost horizontally, so
It becomes difficult to direct the fuel injection direction to the fuel chamber. Furthermore, since the intake air flow in the low-load intake passage does not become very strong even under high loads, there is a problem in that the efficiency of atomization during high loads decreases. Also,
In the structure described in Utility Model Application Publication No. 55-4355, 1
a low-load intake passage and a high-load intake passage communicating with two intake ports, the fuel injection valve is configured so that fuel injection is performed near the confluence of the low-load intake passage and the high-load intake passage, Fuel is injected into the intake air flow from low to high loads to promote atomization. However, with this structure, the fuel is injected very close to the combustion chamber, so
Not being able to achieve sufficient mixing of the intake air.

(本発明の目的) 従つて、本発明の目的は、二つの吸気通路及び
開閉弁を備えたエンジンにおいて低負荷から高負
荷にわたる広い運転領域で、良好な燃料の気化、
霧化、混合状態を与えることができるとともに、
低負荷運転領域において、スワールの生成を促進
することができる燃料噴射式エンジンを提供する
ことである。
(Objective of the present invention) Therefore, the object of the present invention is to provide good fuel vaporization and good fuel vaporization over a wide operating range from low load to high load in an engine equipped with two intake passages and on-off valves.
In addition to being able to provide atomization and mixing conditions,
An object of the present invention is to provide a fuel injection engine capable of promoting the generation of swirl in a low load operating region.

(本発明の構成) 本発明は、上記目的を達成するため以下のよう
に構成される。すなわち、本発明にかかる燃料噴
射式エンジンは、燃焼室に吸気を供給する主吸気
通路と、該主吸気通路内に設けられるスロツトル
弁と、前記主吸気通路内のスロツトル弁よりも下
流側に設けられ低負荷運転領域で閉じ、高負荷運
転領域で開くように制御される開閉弁と、一端が
該開閉弁の上流側かつスロツトル弁下流の主吸気
通路に開口するとともに、他端が該開閉弁の下流
の前記燃焼室近傍に開口する補助吸気通路と、前
記開閉弁の直下流の前記主吸気通路内にその先端
部が臨むように設けられた燃料噴射弁と、を備え
た燃料噴射式エンジンにおいて、一端が前記開閉
弁の上流側でかつスロツトル弁の下流の主吸気通
路に開口するとともに他端が前記燃料噴射弁の先
端部近傍に向けて開口するエアブリード通路を設
け、前記補助吸気通路の前記燃焼室近傍に開口す
る他端がシリンダ径に対して接線方向でかつほぼ
水平方向に開口する、ことを特徴とする。上記エ
アブリード通路からのエアは開閉弁が閉のときす
わなち、負荷が比較的低いときは、スロツトル弁
下流の吸気通路内の吸気圧の範囲内で、噴射燃料
に向けて噴出する。これによつて、低負荷時の燃
料の霧化及び混合が促進される。
(Configuration of the present invention) In order to achieve the above object, the present invention is configured as follows. That is, the fuel injection engine according to the present invention has a main intake passage that supplies intake air to a combustion chamber, a throttle valve provided in the main intake passage, and a throttle valve provided downstream of the throttle valve in the main intake passage. an on-off valve that is controlled to close in a low-load operating range and open in a high-load operating range; one end of the on-off valve opens into the main intake passage upstream of the on-off valve and downstream of the throttle valve; and the other end of the on-off valve A fuel injection type engine comprising: an auxiliary intake passage that opens near the combustion chamber downstream of the valve; and a fuel injection valve provided such that its tip faces into the main intake passage immediately downstream of the on-off valve. An air bleed passage is provided, one end of which opens into the main intake passage upstream of the on-off valve and downstream of the throttle valve, and the other end of which opens near the tip of the fuel injection valve; The other end opening near the combustion chamber is tangential to the cylinder diameter and opening substantially horizontally. When the on-off valve is closed, that is, when the load is relatively low, the air from the air bleed passage is injected toward the injected fuel within the range of the intake pressure in the intake passage downstream of the throttle valve. This facilitates fuel atomization and mixing at low loads.

このエアの噴出はスロツトル弁の下流の圧力に
よつて行われるのでスロツトル開度に応じたエア
ブリードを行うことができる。したがつて低負荷
状態において、不当に過剰の空気導入を起こす心
配ははい。また、開閉弁が大きく開かれる比較的
高負荷運転域では、主吸気通路を流通する吸気流
が強力であるので、噴射燃料がこの吸気流と接触
することにより霧化が促進される。さらに、前記
補助吸気通路の燃焼室近傍に開口する他端は、シ
リンダ径に対して接線方向でかつほぼ水平方向に
開口するように設けられており、このため、補助
吸気通路より吸気が燃焼室に供給される低負荷運
転領域において、スワールの生成を促進すること
が可能になる。本発明を適用することができる吸
気構造は、必ずしも複数の吸気ポートを備えてい
る必要はなく、一つの吸気ポートに通じる2つの
吸気通路を有する形式のものでも良い。
Since this air is ejected by the pressure downstream of the throttle valve, air bleed can be performed in accordance with the throttle opening. Therefore, there is no need to worry about unduly introducing excessive air under low load conditions. Furthermore, in a relatively high-load operating range where the on-off valve is wide open, the intake air flow flowing through the main intake passage is strong, so that the injected fuel comes into contact with this intake air flow, thereby promoting atomization. Furthermore, the other end of the auxiliary intake passage that opens near the combustion chamber is provided so as to open tangentially to the cylinder diameter and in a substantially horizontal direction. It becomes possible to promote the generation of swirl in the low-load operation region where the fuel is supplied to the fuel. An intake structure to which the present invention can be applied does not necessarily have to include a plurality of intake ports, and may have two intake passages leading to one intake port.

開閉弁下流側への吸気導入手段としては、該弁
の上流側と、下流側の吸気通路を連通するエアブ
リード通路を設けることが挙げられる。さらに、
スロツトル弁上流側と開閉弁下流側の吸気通路と
を連通するエアブリード通路を形成するようにし
てもよい。そして、この後者のようにすると吸気
を常時噴射燃料に向けて供給することができる。
As a means for introducing intake air to the downstream side of the on-off valve, it is possible to provide an air bleed passage that communicates the upstream side of the valve with the intake passage on the downstream side. moreover,
An air bleed passage may be formed that communicates the intake passage on the upstream side of the throttle valve and the intake passage on the downstream side of the on-off valve. If this latter method is used, intake air can be constantly supplied toward the injected fuel.

(実施例) 第1図および第2図を参照すると、エンジンE
はシリンダポア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。
(Example) Referring to FIGS. 1 and 2, engine E
is a cylinder block 1 having a cylinder pore 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内にはスロツ
トル弁12が配置されている。第1図に示すよう
に、主吸気通路は、途中にサージタンク24を備
え、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及び第2吸
気ポート5,6に通じる第1、第2分岐通路1
5,16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の上流側に燃料噴射弁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
計算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12に連動さ
れて該絞り弁に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。
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 includes a surge tank 24 in the middle, extends into the cylinder head 2, and extends approximately along the cylinder center line l in the width direction of the cylinder block in the vicinity of the intake ports 5 and 6. First and second branch passages 1 are separated by a partition wall 14 formed as follows and communicate with first and second intake ports 5 and 6, respectively.
5 and 16. The 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 fuel injection valve 23 is arranged upstream of the partition wall 14, and fuel calculated based on a signal corresponding to engine operating conditions is supplied to the combustion chamber 4. An on-off valve 18 is provided within the main intake passage 11 .
The opening/closing valve 18 is, for example, linked to the throttle valve 12 so that it is closed in a low-load operating region where the throttle valve has a relatively small opening, and is opened when the throttle valve 12 is opened beyond a predetermined opening. configured.

さらに、主吸気通路11には開閉弁18の僅か
に上流側に開口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吸気ポート5
に接続されている。また、主吸気通路11の開閉
弁18の上方には、エアブリード通路25が設け
られており、このエアブリード通路25の上流端
は、開口26により主吸気通路11の開閉弁18
よりも上流側の上部に連通している。第3図を併
せて参照すれば、開閉弁18の僅かに下流側の上
方には燃料噴射弁23が配置されており、そのノ
ズル先端部23aの周囲には、ソケツト27が嵌
合している。該ソケツト27は、外周に周囲溝2
7aを備えるとともにその溝27aには周方向に
隔置した複数の小穴27bが設けられている。そ
してエアブリード通路25の下流端はこの周囲溝
27aに連通している。従つて、エアブリード通
路25に導入されたエアは、この小穴27bから
ソケツト27の内側に向つて噴出し、これによつ
て噴射燃料の霧化が効率良く行なわれる。
Furthermore, an opening 19 is formed in the main intake passage 11 slightly upstream of the on-off valve 18, and an auxiliary intake passage 20 is formed extending below the main intake passage 11 from this opening 19. Auxiliary intake passage 20
is from the bottom of the main intake passage 11 to the first branch passage 15.
through the opening 21 of the first intake port 5.
It is connected to the. Further, an air bleed passage 25 is provided above the on-off valve 18 of the main intake passage 11, and the upstream end of this air bleed passage 25 is connected to the on-off valve 18 of the main intake passage 11 by an opening 26.
It is connected to the upper part on the upstream side. Referring also to FIG. 3, a fuel injection valve 23 is arranged slightly above the on-off valve 18 on the downstream side, and a socket 27 is fitted around the nozzle tip 23a. . The socket 27 has a peripheral groove 2 on its outer periphery.
7a, and the groove 27a is provided with a plurality of small holes 27b spaced apart in the circumferential direction. The downstream end of the air bleed passage 25 communicates with this peripheral groove 27a. Therefore, the air introduced into the air bleed passage 25 is blown out from the small hole 27b toward the inside of the socket 27, thereby efficiently atomizing the injected fuel.

第2図に示すように、第1、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に対し比較的浅い角度で向けられ
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。
As shown in FIG. 2, the first intake port 5 is
In order to ensure a high filling amount during high-load operation, the cylinder bore 1a opens into the combustion chamber 4 at an angle close to the axial direction.Although not shown in the figure, the second intake port 6 also has a similar shape. be. 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.

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。
As shown in FIG. 1, in this embodiment, 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. A spark plug 22 is attached to the portion. 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.

低負荷運転領域では、開閉弁18は閉又は開度
が小さい状態になつており、吸気は、主として補
助吸気通路20から燃焼室4に導入される。この
場合、燃料は主吸気通路11に向けて噴射される
が、一部の吸気は、エアーブリード通路25を通
じて、燃料噴射弁23から噴射される燃料に向け
て小穴27bから噴出し、燃料の霧化を促進す
る。このエアに噴出はスロツトル弁12の下流の
圧力によつて行われるのでスロツトル開度に応じ
たエアブリードを行うことができる。したがつて
低負荷状態において、不当に過剰の空気導入を起
こす心配はない。また、高負荷運転領域では、開
閉弁18は、開状態になつており、燃料は吸気流
の中に噴射され、これによつて、燃料の霧化が促
進される。
In the low-load operation region, the on-off valve 18 is closed or has a small opening, and intake air is mainly introduced into the combustion chamber 4 from the auxiliary intake passage 20. In this case, fuel is injected toward the main intake passage 11, but some intake air is injected from the small hole 27b through the air bleed passage 25 toward the fuel injected from the fuel injection valve 23, resulting in fuel mist. promote the development of Since this air is ejected by the pressure downstream of the throttle valve 12, air bleed can be performed in accordance with the throttle opening degree. Therefore, there is no need to worry about unduly introducing excessive air under low load conditions. Further, in a high-load operation region, the on-off valve 18 is in an open state, and fuel is injected into the intake air flow, thereby promoting atomization of the fuel.

(発明の効果) 本発明によれば、低負荷領域では、補助吸気通
路を介して、スワールを形成するように高速で吸
気を導入することができるとともに、エアブリー
ド通路からのエアにより、吸気の良好な霧化、気
化および混合状態を確保することができる。この
エアの噴出はスロツトル弁の下流の圧力によつて
行われるのでスロツトル開度に応じたエアブリー
ドを行うことができる。したがつて低負荷状態に
おいて、不当に過剰の空気導入を起こす心配はな
い。一方高負荷領域では、主吸気通路をを流通す
る吸気流により霧化が促進されるので、全運転領
域にわたつて良好な霧化、混合状態を得ることが
でき、燃費性能、走行性能を向上させることがで
きる。
(Effects of the Invention) According to the present invention, in a low load region, intake air can be introduced at high speed through the auxiliary intake passage to form a swirl, and the air from the air bleed passage can be used to reduce intake air. Good atomization, vaporization and mixing conditions can be ensured. Since this air is ejected by the pressure downstream of the throttle valve, air bleed can be performed in accordance with the throttle opening. Therefore, there is no need to worry about unduly introducing excessive air under low load conditions. On the other hand, in high-load regions, atomization is promoted by the intake air flowing through the main intake passage, making it possible to obtain good atomization and mixing conditions over the entire operating range, improving fuel efficiency and driving performance. can be done.

【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、第3図は第2図のA部拡
大図、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、12……スロツト
ル弁、15,16……分岐吸気通路、18……開
閉弁、19……開口、20……補助吸気通路、2
5……エアブリード通路。
FIG. 1 is a schematic plan view of an engine intake system showing an embodiment of the present invention, FIG. 2 is a vertical sectional view of an engine embodying the present invention, and FIG. 3 is an enlarged view of part A in FIG. be. 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, 12...Throttle valve, 15, 16...Branch intake passage, 18...Opening/closing valve, 19... Opening, 20...Auxiliary intake passage, 2
5...Air bleed passage.

Claims (1)

【特許請求の範囲】 1 燃焼室4に吸気を供給する主吸気通路11
と、該主吸気通路11内に設けられるスロツトル
弁12と、前記主吸気通路11内のスロツトル弁
12よりも下流側に設けられ低負荷運転領域で閉
じ、高負荷運転領域で開くように制御される開閉
弁18と、一端が該開閉弁18の上流側かつスロ
ツトル弁12下流の主吸気通路11に開口すると
ともに、他端が該開閉弁の下流の前記燃焼室近傍
に開口する補助吸気通路20と、前記開閉弁18
の直下流の前記主吸気通路11内にその先端部が
臨むように設けられた燃料噴射弁23と、 を備えた燃料噴射式エンジンにおいて、 一端が前記開閉弁18の上流側でかつスロツト
ル弁12の下流の主吸気通路11に開口するとと
もに他端が前記燃料噴射弁23の先端部近傍に向
けて開口するエアブリード通路25を設け、 前記補助吸気通路20の前記燃焼室4近傍に開
口する他端がシリンダ径に対して接線方向でかつ
ほぼ水平方向に開口する、ことを特徴とする燃料
噴射式エンジン。
[Claims] 1. Main intake passage 11 that supplies intake air to the combustion chamber 4
, a throttle valve 12 provided in the main intake passage 11, and a throttle valve 12 provided downstream of the throttle valve 12 in the main intake passage 11, which is controlled to close in a low load operating region and open in a high load operating region. an on-off valve 18 with one end opening into the main intake passage 11 upstream of the on-off valve 18 and downstream of the throttle valve 12, and an auxiliary intake passage 20 with the other end opening downstream of the on-off valve near the combustion chamber. and the on-off valve 18
a fuel injection valve 23 provided such that its tip faces into the main intake passage 11 directly downstream of the throttle valve 12; An air bleed passage 25 is provided which opens into the main intake passage 11 downstream of the auxiliary intake passage 20 and whose other end opens towards the vicinity of the tip of the fuel injection valve 23, and which opens in the vicinity of the combustion chamber 4 of the auxiliary intake passage 20. A fuel injection engine characterized in that the end opens tangentially to the cylinder diameter and substantially horizontally.
JP59068408A 1984-04-05 1984-04-05 Fuel injection engine Granted JPS60212665A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59068408A JPS60212665A (en) 1984-04-05 1984-04-05 Fuel injection engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59068408A JPS60212665A (en) 1984-04-05 1984-04-05 Fuel injection engine

Publications (2)

Publication Number Publication Date
JPS60212665A JPS60212665A (en) 1985-10-24
JPH0480231B2 true JPH0480231B2 (en) 1992-12-18

Family

ID=13372819

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59068408A Granted JPS60212665A (en) 1984-04-05 1984-04-05 Fuel injection engine

Country Status (1)

Country Link
JP (1) JPS60212665A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1553288B1 (en) * 2002-10-18 2015-12-09 Yamaha Hatsudoki Kabushiki Kaisha Engine
JP4524617B2 (en) * 2004-12-03 2010-08-18 日産自動車株式会社 Intake control device and intake control method
JP7087510B2 (en) * 2018-03-20 2022-06-21 スズキ株式会社 Engine intake passage structure

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5554662A (en) * 1978-10-18 1980-04-22 Toyota Motor Corp Suction device for fuel injection type internal-combustion engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5554662A (en) * 1978-10-18 1980-04-22 Toyota Motor Corp Suction device for fuel injection type internal-combustion engine

Also Published As

Publication number Publication date
JPS60212665A (en) 1985-10-24

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