JPS60198330A - Intake device for engine - Google Patents

Intake device for engine

Info

Publication number
JPS60198330A
JPS60198330A JP59054105A JP5410584A JPS60198330A JP S60198330 A JPS60198330 A JP S60198330A JP 59054105 A JP59054105 A JP 59054105A JP 5410584 A JP5410584 A JP 5410584A JP S60198330 A JPS60198330 A JP S60198330A
Authority
JP
Japan
Prior art keywords
intake
passage
intake passage
auxiliary
port
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.)
Pending
Application number
JP59054105A
Other languages
Japanese (ja)
Inventor
Teruhisa Murakami
村上 照久
Yukio Kajiwara
梶原 幸生
Takashi Kadota
門田 隆
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 JP59054105A priority Critical patent/JPS60198330A/en
Publication of JPS60198330A publication Critical patent/JPS60198330A/en
Pending 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
    • 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
    • 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 achieve swirl of desired of desired strength under wide operational range and to improve the combustion performance by providing an auxiliary intake path branched from an intake path in the upstream of a gate valve while/ communicated to one intake port and enlarging the diameter of the intake port communicated with said path. CONSTITUTION:Plural intake ports 5, 6 are opened to a combustion chamber 4 while a gate valve 18 to be closed under low load operation is arranged in main intake path 11 communicatable through branch intake paths 15, 16 with respective intake port 5, 6. An opening 19 is formed through the bottom of main intake path 11 in the upstream of the gate valve 18 while an auxiliary intake path 20 is extended from said opening 19 to the underside of main intake path 11 and coupled through an opening 21 to first intake port 5. The diameter of the first intake port 5 is made larger than that of the second intake port 6 thereby the auxiliary intake path 20 to be coupled with the first intake port 5 is enlarged.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、エンジンの燃焼室に吸気を導入する複俄の吸
気ボートを備え、該各々の吸気ボートに接続される吸気
通路がそれぞれ設けられ、さらにいずれか一つの吸気ボ
ートに接続された補助吸気通路を備えたエンジンの吸気
装置に関する。
Detailed Description of the Invention (Industrial Application Field) The present invention comprises multiple intake boats for introducing intake air into the combustion chamber of an engine, and an intake passage connected to each intake boat. The present invention further relates to an engine intake system including an auxiliary intake passage connected to any one of the intake boats.

(従来技術) エンジンの高出力化を図るためには、吸気の通路面積を
拡大し充填効率を向上させることが必要となるが一つの
吸気ボートによシ大きな通路面積を確保するようにする
と、吸気弁の慣性重量が大きくなって追従性が悪化する
こと、燃焼室構造の強度上の不利が生じること等の理由
から2つの吸気ボートから吸気を導入するようにして高
出力化を図るエンジンの吸気構造が従来から知られてい
る。
(Prior art) In order to increase the output of an engine, it is necessary to expand the intake passage area and improve the filling efficiency, but if one intake boat has a large passage area, For reasons such as the inertial weight of the intake valve becoming large and the follow-up performance becoming worse, and the strength of the combustion chamber structure being disadvantageous, it is recommended that the engine be designed to increase output by introducing intake air from two intake boats. Air intake structures have been known for some time.

このような2ボート型の吸気装置は、高負荷運転時にお
いて多量の吸気を導入して高出力を得ることができると
いう利点があるが、吸気前が少い低負荷運転時では吸気
流速が低下して1着火性が悪化し、燃焼性が低下すると
いう問題が生じる。
Such a two-boat type intake system has the advantage of being able to introduce a large amount of intake air and obtain high output during high-load operation, but during low-load operation with less air intake, the intake flow rate decreases. This causes problems such as deterioration of ignitability and deterioration of combustibility.

このような不利を解消するため低負荷運転時においては
、吸気流速を高めるとともに吸気のスワールを形成する
ようにして低負荷時の燃焼性を改善することが知られて
いる。例えば、特開昭56−44419号公報には、燃
焼室に開口する2つの吸気ポートとこれらのボートに1
つの吸気通路から分岐した2つの吸気通路をそれぞれ接
続し、該分岐吸気通路の一方に高負荷時に開くシャッタ
ーパルプを設けた吸気装置の1.iI造が開示されてい
る。
In order to eliminate such disadvantages, it is known to improve the combustibility during low load operation by increasing the intake air flow velocity and forming an intake air swirl during low load operation. For example, Japanese Patent Application Laid-open No. 56-44419 discloses two intake ports opening into the combustion chamber and one port on these boats.
1. An intake system in which two intake passages branched from one intake passage are connected to each other, and one of the branched intake passages is provided with a shutter pulp that opens at high load. An iI construction is disclosed.

この装置においては、低負荷運転時にはシャッターパル
プが閉じているので、吸気は、シャッターパルプの設け
られていない他方の分岐吸気通路からのみ導入される。
In this device, since the shutter pulp is closed during low load operation, intake air is introduced only from the other branch intake passage where the shutter pulp is not provided.

この装置では、これによって吸気の流速低下を防止して
、吸気のスワールを生成するようにしている。
In this device, this prevents a decrease in the flow velocity of intake air and generates a swirl of intake air.

しかし、この装置は、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、吸気通路は
吸気流を燃焼室の軸線方向に導入するようになっておシ
、このため低負荷時に一方の吸気ポートから吸気を導入
しても燃焼室内で強力なスワールを形成することは困難
である。また、この公開された装置では2つの吸気ポー
トの大きさに差異がないため、負荷が増大した場合には
However, since this device is intended to ensure sufficient intake air charging during high-load operation, the intake passage introduces the intake air flow in the axial direction of the combustion chamber. Even if intake air is introduced from one intake port during low load, it is difficult to form a strong swirl within the combustion chamber. Also, in this disclosed device, there is no difference in the size of the two intake ports, so if the load increases.

吸気量を確保するため比較的早期にシャツターノ(ルゾ
を開いて2つの吸気ポートから吸気を導入しなければな
らない。しかし、2つの吸気ポートを開くと吸気のスワ
ール生成力は急速に弱まって燃焼性の悪化をもたらすこ
ととなり、従ってこの装置では広い負荷運転領域にわた
る良好な燃焼性を確保することができない。
In order to secure the amount of intake air, it is necessary to open the Shattano (Luso) relatively early and introduce intake air from the two intake ports.However, when the two intake ports are opened, the swirl-generating force of the intake air quickly weakens and combustion Therefore, this device cannot ensure good combustibility over a wide load operating range.

(本発明の目的) 本発明の目的は、低負荷領域から中負荷領域にわたる広
い負荷運転領域において所望の強さの吸気スワールを形
成し、良好な燃焼性を確保することができる補助吸気通
路を備えたエンジンの吸気装置を提供することである。
(Objective of the present invention) An object of the present invention is to provide an auxiliary intake passage that can form an intake swirl of desired strength and ensure good combustibility in a wide load operation range from low load to medium load. It is an object of the present invention to provide an intake system for an engine equipped with the following.

(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、本発明の吸気装置は燃焼室に開口する複
数の吸気ポートと、曲名吸気ボートに連通ずる吸気通路
と、該吸気通路に設けられ低負荷運転時には閉方向に高
負荷運転時には開方向に制御されて吸気通路の通路面積
を増減させる開閉弁とを備えるとともに、上記開閉弁よ
シも上流の吸気通路の底部から分岐して上記吸気ポート
のいずれか一つに連通ずる補助吸気−通路を備えている
(Configuration of the present invention) In order to achieve the above object, the present invention is configured as follows. That is, the intake device of the present invention has a plurality of intake ports that open into the combustion chamber, an intake passage that communicates with the intake port, and an intake passage that is provided in the intake passage and is controlled in the closed direction during low-load operation and in the open direction during high-load operation. and an on-off valve that increases or decreases the passage area of the intake passage, and the on-off valve also includes an auxiliary intake passage that branches from the bottom of the upstream intake passage and communicates with one of the intake ports. ing.

そして、この補助吸気通路が連通ずる吸気ポートのポー
ト径は他の吸気ポートのボート径よ勺も大きくなってお
)、これによって上記補助吸気通路の通路面積は比較的
大きなものになっている。補助吸気通路は好ましくは、
該補助吸気通路が連通し通路面積が前記吸気通路の通路
面積よりも小さい吸気ポートの反対側に偏った位置から
分岐している。そして開閉弁が閉じられる運転領域では
、吸気は補助吸気通路からのみ供給される。この場合・
補助吸気通路は分岐吸気通路の下側を2[8ル吸気ボー
トに開口するので、吸気流は比較的浅い角度で、すなわ
ち燃焼室の両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った位置で該燃焼室に送シ
込まれることになシ、燃焼室の軸線まわシに強い旋回流
すなわちスワールを形成する。
The port diameter of the intake port with which this auxiliary intake passage communicates is larger than the port diameter of the other intake ports, so that the passage area of the auxiliary intake passage is relatively large. The auxiliary intake passage is preferably
The auxiliary intake passage branches off from a position opposite to the intake port where the passage area is smaller than the passage area of the intake passage. In an operating range where the on-off valve is closed, intake air is supplied only from the auxiliary intake passage. in this case·
Since the auxiliary intake passage opens the lower side of the branched intake passage into a 2[8] intake boat, the intake air flow is directed into the combustion chamber at a relatively shallow angle, that is, at an angle close to perpendicular to both lines of the combustion chamber. , the intake air flow is sent into the combustion chamber from only one intake port at a position that is biased to the side with respect to the axis of the combustion chamber, creating a strong swirl flow around the axis of the combustion chamber. Form.

本発明の上記構成によれば、補助吸気通路が連通ずる吸
気ポートの径は他の吸気ポートの径より大きくなってい
る。このため、補助吸気通路の断面積を不都合なく拡大
せしめることができるので負荷の増大に伴って吸気量が
増大しても、所望の吸気量を補助吸気通路からのみの吸
気供給によってまかなうことができる。すなわち、広い
負荷運転領域にわたって、補助吸気通路だけから有効に
スワールを形成しつつ所望の吸気量を確保、することが
できる。また、補助吸気通路が連通する吸気yg−トと
組合わされる吸気弁の開弁期間を他のものよル長く設定
すれば、さらに効率良く補助吸気通路の使用領域を拡大
せしめることができる。
According to the above configuration of the present invention, the diameter of the intake port with which the auxiliary intake passage communicates is larger than the diameters of the other intake ports. Therefore, the cross-sectional area of the auxiliary intake passage can be expanded without any inconvenience, so even if the amount of intake air increases as the load increases, the desired amount of intake air can be met by supplying air only from the auxiliary intake passage. . That is, a desired amount of intake air can be ensured while effectively forming a swirl only from the auxiliary intake passage over a wide load operating range. Further, by setting the opening period of the intake valve associated with the intake valve with which the auxiliary intake passage communicates to be longer than that of other intake valves, the usable area of the auxiliary intake passage can be expanded even more efficiently.

(本発明の効果) 本発明によ11ば、iつの燃焼室に両数の吸気ポ−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、上述のように低負荷運転
時から中負荷運転時にわたる広い運転領域において、所
望の強さのスワールを得ることができ、従って、この広
い範囲で安定した良好な燃焼件を得ることができる。
(Effects of the present invention) According to the present invention, there is provided an intake system in which both intake ports are opened in i combustion chambers to ensure a high filling amount of intake air during high-load operation. As such, a swirl of desired strength can be obtained in a wide operating range from low-load operation to medium-load operation, and therefore stable and good combustion conditions can be obtained in this wide range.

(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
ダデアlai有するシリンダブロック1と該シリンダブ
ロック1の上部に取付けられたシリンダヘッド2を有し
、シリンダが71a内にはピストン3が軸方同往復動自
在に配置されて、シリンダボ了1a内に燃焼室4を形成
する。シリンダヘッド2には第1および第2吸気ボート
5.6と排気ポート7が形成され、第1、第2吸気ボー
ト5.6Vc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吸
気ボート5は、第2吸気ボートよシも大径に形成されて
おり、シリンダブロック1の巾方向のシリンダ中心@ 
t VC関してはげ対称に配置され、排気ポート7はシ
リンダグロック1の長手方向中心線mをはさんで第2吸
気ボート6と対向する位置に配置されている。
(Description of an Embodiment) Referring to FIGS. 1 and 2, an engine E has a cylinder block 1 having a cylinder diameter and a cylinder head 2 attached to the upper part of the cylinder block 1. A piston 3 is arranged so as to be able to reciprocate in the axial direction, and forms a combustion chamber 4 within the cylinder body 1a. A first and second intake boat 5.6 and an exhaust port 7 are formed in the cylinder head 2. An intake valve 8 is attached to each of the first and second intake boats 5.6Vc, and an exhaust valve 9 is attached to the exhaust port 7. It will be done. Referring to FIG. 1, the first intake boat 5 is also formed to have a larger diameter than the second intake boat, and the cylinder center in the width direction of the cylinder block 1 @
The exhaust port 7 is arranged symmetrically with respect to tVC, and the exhaust port 7 is arranged at a position facing the second intake boat 6 across the longitudinal center line m of the cylinder glock 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内には絞シ弁12が配置にさ
れている。肩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方向のシリンダ中心軸tKはぼ沿
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吸気ボート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1
4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量された燃料が燃焼室
4に供給される。主吸気通路ll内には、開閉弁18が
設けられている。
The intake system includes a main intake passage 11 extending from the air cleaner 10.
A throttle valve 12 is disposed within the main intake passage 11. Shoulder 1 As shown in Figure 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 wall formed so that the cylinder center axis tK in the width direction of the cylinder block is approximately parallel to the main intake passage 11. 14, forming first and second branch passages 15.16 which communicate with the first and second intake boats 5.6, respectively. The exhaust port 7 is connected to the exhaust passage 17 to constitute an exhaust system. This exhaust system may have a normal configuration. The main intake passage 11 has a partition wall 1
A fuel injection valve 23 is disposed upstream of the combustion chamber 4, and fuel metered based on a signal corresponding to engine operating conditions is supplied to the combustion chamber 4. An on-off valve 18 is provided in the main intake passage ll.

この開閉弁18は、たとえば絞シ弁12Vc連動されて
該絞シ弁の開度が比較的小さい低負荷運転領域では閉じ
られ、絞カ弁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よシ僅か上流側に開口19が形成され、この開
口19から主吸気通@11の下11411を延びるよう
に補助吸気通路2゜が形成されている。補助吸気通路2
oは、はぼ第1分岐通路の径に匹敵する通路中を有して
おり、主吸気通路11の下側から第1分岐通路工5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、シリンダ昶アlaの軸
線方向に近い角度で燃焼室4に開口しておシ、図には示
していないが、第2吸気ボート6も同様な形状である。
For example, this on-off valve 18 is linked to the throttle valve 12Vc, and is closed in a low-load operation region 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. It is configured as follows. An opening 19 is formed at the bottom of the main intake passage 11 slightly upstream of the on-off valve 18, and an auxiliary intake passage 2° is formed extending from this opening 19 to 11411 below the main intake passage @11. . Auxiliary intake passage 2
o has a passage approximately comparable in diameter to the first branch passage, passes from the lower side of the main intake passage 11 to the lower side of the first branch passage construction 5, and connects the first intake port 5 with the opening 21. It is connected to the. 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 a to ensure a high filling amount during high-load operation. Although not shown, the second intake boat 6 also has a similar shape.

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h5に開口し
ているので、燃焼室41C対し比幀的浅角度で向けられ
ることになる。さらに、第1吸気ボート5は、シリンダ
ボアlaの中心線tに対し一方に偏って配置されている
ので、補助吸気通路2o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O 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の近傍でシリンダポア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吸気ボート5とは反対側すなわち第2
吸気ボート6の側に寄せて配置されているので、開口2
1の近傍でシリンダボアla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に極端な曲シを与え
る必要がなく72−夛、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。
On the other hand, since the auxiliary intake passage 20 opens from the lower side of the main intake passage 11 and the first branch passage 15 to the first intake port h5, it is oriented at a relatively shallow angle with respect to the combustion chamber 41C. . Furthermore, since the first intake boat 5 is arranged to be biased to one side with respect to the center line t of the cylinder bore la, the intake air jetted into the combustion chamber 4 at a shallow angle from the auxiliary intake passage 2o is directed within the combustion chamber 4. Generates a strong swirl, that is, a strong swirl in the horizontal plane. In order to facilitate the generation of this swirl, the shape of the auxiliary intake passage 20 is formed so that it faces almost tangentially to the peripheral wall of the cylinder pore 1a near the opening 21. It is desirable to do so. In order to obtain such a shape, it is necessary to curve the auxiliary intake passage 20. However, as shown in FIG.
The side opposite to the first intake boat 5 with respect to the center of
Since it is placed closer to the intake boat 6, the opening 2
1, it is not necessary to give the auxiliary intake passage 20 an extreme curvature. A shape with less flow path resistance can be achieved.

開閉弁が閉じられる比校的負荷の低い運転領域では、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
焼室に送シ込まれる。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♂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
In an operating region with a low relative load in which the on-off valve is closed, all the intake air passing through the main intake passage 11 is guided from the opening 18 to the auxiliary intake passage, and is sent into the combustion chamber from the opening 21 through the first intake port 5. It will be done. Since the auxiliary intake passage 20 is oriented in the circumferential direction of the cylinder ♂a 1a at a relatively shallow angle as described above, the intake air jetted from the auxiliary intake passage 20 into the combustion chamber 4 is directed into the combustion chamber 4. to form a strong swirl.

本例では、第1吸気ポート5が第2吸気ポート6よりも
大径になっており、これに伴い、第1吸気4ビート5に
接続される補助吸気通路20も大きく形成されている。
In this example, the first intake port 5 has a larger diameter than the second intake port 6, and accordingly, the auxiliary intake passage 20 connected to the first intake 4-beat 5 is also formed larger.

従って、ある程度負荷が増大して吸気量が増えても、補
助吸気通路20から送り込まれる吸気により全体の吸気
量を充足することができる。従って、比較的負荷が増大
した運転領域においても開閉弁18を開く必要がなく燃
・焼室内で吸気のスワールを存続させることができ、良
好な燃焼性を維持することができる。
Therefore, even if the load increases to some extent and the amount of intake air increases, the total amount of intake air can be satisfied by the intake air sent from the auxiliary intake passage 20. Therefore, even in an operating range where the load is relatively increased, there is no need to open the on-off valve 18, and the swirl of intake air can be maintained in the combustion chamber, and good combustibility can be maintained.

さらに、負荷が増大して、絞シ弁12が所定値を越えて
開かれると、開閉弁18も開き始める。
Further, when the load increases and the throttle valve 12 is opened beyond a predetermined value, the on-off valve 18 also begins to open.

開閉弁18の開度が比較的小さい運転領域では。In an operating range where the opening degree of the on-off valve 18 is relatively small.

吸気の一部は依然として補助吸気通路20を通って供給
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の側に偏っ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童が第2吸気ポ
ート6を通る量よりも多くなシ、その結果として、ある
程度のスワールをこのような負荷が増大した領域でも形
成することができる。
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 the position, the amount of intake air supplied to the combustion chamber 4 via the first intake port 5 is larger than the amount passing through the second intake port 6, and as a result, such a load causes a certain amount of swirl. Enlarged areas can also be formed.

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

第1図は本発明の一笑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・・・シリンダグロック、la・・・シリンダゼア、
2・・−シリンダヘッド、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。 第1図
FIG. 1 is a schematic plan view of an engine intake system showing one embodiment of the present invention, and FIG. 2 is a vertical sectional view of an engine embodying the present invention. 1... Cylinder Glock, la... Cylinder Zea,
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. Figure 1

Claims (1)

【特許請求の範囲】[Claims] 燃焼室に開口する複数の吸気ボートと、曲名吸気ポート
に連通ずる吸気通路と、該吸気通路に設けられ低負荷運
転時には閉方向に高負荷運転時には開方向に制御されて
吸気通路の通路面積を増減させる開閉弁とを備えたエン
ジンの吸気装置において、前記開閉弁よりも上流の吸気
通路から分岐して前記吸気ボートのいずれか一つに連通
し通路面積が前記吸気通路の通路面積よシも小さい補助
吸気通路が設けられるとともに、該補助吸気通路が連通
ずる吸気ボートの径をそれ以外の吸気ボートの径よシも
大きくすることにより前記補助吸気通路の通路面積を拡
大せしめたことを特徴とするエンジンの吸気装置。
A plurality of intake boats that open into the combustion chamber, an intake passage that communicates with the intake port, and an intake passage that is provided in the intake passage and are controlled in the closed direction during low load operation and in the open direction during high load operation to reduce the passage area of the intake passage. In an engine intake system equipped with an on-off valve that increases or decreases, the intake passage branches from an intake passage upstream of the on-off valve and communicates with one of the intake boats, and has a passage area that is larger than the passage area of the intake passage. A small auxiliary intake passage is provided, and the passage area of the auxiliary intake passage is expanded by making the diameter of the intake boat with which the auxiliary intake passage communicates larger than that of the other intake boats. engine intake system.
JP59054105A 1984-03-21 1984-03-21 Intake device for engine Pending JPS60198330A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59054105A JPS60198330A (en) 1984-03-21 1984-03-21 Intake device for engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59054105A JPS60198330A (en) 1984-03-21 1984-03-21 Intake device for engine

Publications (1)

Publication Number Publication Date
JPS60198330A true JPS60198330A (en) 1985-10-07

Family

ID=12961328

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59054105A Pending JPS60198330A (en) 1984-03-21 1984-03-21 Intake device for engine

Country Status (1)

Country Link
JP (1) JPS60198330A (en)

Citations (1)

* 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

Patent Citations (1)

* 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

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