JPS60162017A - Intake device for engine - Google Patents

Intake device for engine

Info

Publication number
JPS60162017A
JPS60162017A JP59016823A JP1682384A JPS60162017A JP S60162017 A JPS60162017 A JP S60162017A JP 59016823 A JP59016823 A JP 59016823A JP 1682384 A JP1682384 A JP 1682384A JP S60162017 A JPS60162017 A JP S60162017A
Authority
JP
Japan
Prior art keywords
intake
passage
intake passage
auxiliary
load
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
JP59016823A
Other languages
Japanese (ja)
Other versions
JPH0330697B2 (en
Inventor
Sadashichi Yoshioka
吉岡 定七
Noboru Hashimoto
昇 橋本
Hiroyuki Oda
博之 小田
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 JP59016823A priority Critical patent/JPS60162017A/en
Publication of JPS60162017A publication Critical patent/JPS60162017A/en
Publication of JPH0330697B2 publication Critical patent/JPH0330697B2/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
    • F02B31/085Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air inlets having two inlet 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Characterised By The Charging Evacuation (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

PURPOSE:To prevent the shock of the changeover from the low-load run of an engine to its high-load run, by curving the second-intake-port-side wall of an auxiliary intake passage, from a second intake port toward a first intake port, to maintain the swirling performance of the engine in its low-load run. CONSTITUTION:The upstream opening 13a of an auxiliary intake passage 13 is located at the bottom of an intake passage 8 upstream to a shutoff valve 12, while the downstream opening 13b of the passage 13 is located upstream to the downstream end 9a of a partition wall 9. The auxiliary intake passage 13 is slowly curved across a center line l. The second-intake-port-side wall 13c of the auxiliary intake passage 13 is curved from a second intake port 5 toward a first intake port 4. The upstream opening 13a of the auxiliary intake passage 13 is provided at a common passage portion, in which the intake passage 8 is not ramified, to have a large open area. The cross-sectional area of the passage 13 is thus enlarged to prevent the shock of the changeover from the low-load run of an engine to its high-load run.

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、特に2ポート等の複数
の吸気ポートをエンジンの燃焼室に開口させるとともに
、各吸気ポートに対してこれを開閉する吸気弁を配置し
た型式の吸気装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention is directed to an engine intake system, in particular, to open a plurality of intake ports such as two ports into a combustion chamber of the engine, and to open the same to each intake port. This invention relates to a type of intake device equipped with an intake valve that opens and closes.

(従来技術) 従来より、レシプロエンノンにおいで、各燃焼室に則し
て、はぼ均等な開口面積を有する2つの吸気ポートを開
口させて大ぎな開口面積を確保するとともに、シリング
へンド内に形成する吸気通路を各吸気ポートに燃焼室の
軸方向に沿った大角度で接続して吸気を燃焼室にストレ
ートに流入させることにより、エンジ゛ンの充填効率を
最大限向上させ、エンジンの高出力化を図ったエンン゛
ンの吸気構造はよく知られている。
(Prior art) Conventionally, in a reciprocating engine, two intake ports with approximately equal opening areas are opened in accordance with each combustion chamber to ensure a large opening area, and a The intake passage formed at The intake structure of engines designed to increase output is well known.

かかる2ポ一ト型式の吸気構造は、高負荷運転時の高出
力化を図るという点で有利であるが、その反面、吸気量
の少ない低負荷運転時には、吸気流速が弱まり、燃焼性
か低下し燃費の面でも、エミッションの面でも不利とな
る欠点がある。
Such a two-point intake structure is advantageous in that it can achieve high output during high-load operation, but on the other hand, during low-load operation with a small amount of intake air, the intake flow velocity weakens and combustibility deteriorates. However, it has disadvantages in terms of fuel efficiency and emissions.

かかる欠点を解消するため、低負荷用吸気通路とシャッ
ターバルブを介設した高負荷用吸気通路とを」1記2つ
の吸気ポートに夫々接続し、エンジンの低負荷運転時に
は、シャッターバルブを閉じて、低負荷用吸気通路のみ
から吸気を行なうようにしたものか′知られている(例
えば、特開昭56−44419号公報参照)。
In order to eliminate this drawback, a low-load intake passage and a high-load intake passage with a shutter valve interposed are connected to the two intake ports in 1. When the engine is operating at low load, the shutter valve is closed. It is known that air is taken only from the low-load intake passage (for example, see Japanese Patent Laid-Open No. 56-44419).

しかしなから、かかる科策は低負荷対策として必らずし
も有効ではない。即ち、もともと高出力化のため2つの
吸気ポートの開口面積を最大限確保するようにしたもの
であるため、1つの吸気ボートのみを使用するとしても
吸気量が少ない極低負荷運転時には、開口面積が依然大
きすぎて吸気流速を有効に向上させることがでとず、燃
焼性の向上に不可欠なスワールを有効に形成できない。
However, such measures are not necessarily effective as low-load countermeasures. In other words, the opening area of the two intake ports was originally designed to be maximized in order to achieve high output, so even if only one intake port is used, during extremely low load operation where the amount of intake air is small, the opening area will be reduced. is still too large to effectively improve the intake air flow velocity, making it impossible to effectively form the swirl that is essential for improving combustibility.

かかる不具合は、特開昭56−146 (11S号公報
に開示された如く、低負荷用吸気通路の通路面積を絞れ
ば、それで解消しうるように思えるが、その場合には、
高負荷用吸気通路の通路面積を余程大トくシなければ高
出力化という本来の目的を達成することがで外す、実際
に通路面積を大きくすると低負荷用吸気通路の通路面積
とのアンバランスが大きくなって、低負荷用吸気通路を
開く低負荷から高負荷への切替えに際して所謂切替ショ
ックを生じ、また、高負荷時には、吸気抵抗の少ない高
負荷用吸気通路に吸気が集中して、実質的には高出力化
を達成するのに有効な吸気通路面積を確保できないとい
う矛盾がある。さらに、高出力化を図る目的から吸気通
路のボート接続部は前述したように、燃焼室の軸方向に
沿った方向に形成されているため、吸気流速を早めるこ
とによって燃焼室内に流速の早い流れが生成されたとし
ても燃焼室の周方向に沿った有効なスワールとして生J
!!、されない。このため、この吸気の流れは圧縮行程
において早期に減衰されてしまうといった問題がある。
It seems that this problem can be solved by narrowing down the passage area of the low-load intake passage, as disclosed in Japanese Patent Application Laid-open No. 11S (1986-146), but in that case,
If you do not increase the passage area of the high-load intake passage too much, you will be able to achieve the original purpose of increasing output, but if you actually increase the passage area, the difference between the passage area of the low-load intake passage and The balance becomes large, causing a so-called switching shock when switching from low load to high load, which opens the low-load intake passage, and at high loads, intake air concentrates in the high-load intake passage where there is less intake resistance. In reality, there is a contradiction in that an effective intake passage area cannot be secured to achieve high output. Furthermore, for the purpose of achieving high output, the boat connection part of the intake passage is formed along the axial direction of the combustion chamber, as described above, so that by increasing the intake air velocity, a high-velocity flow flows inside the combustion chamber. Even if J is generated as an effective swirl along the circumferential direction of the combustion chamber,
! ! , not done. Therefore, there is a problem in that the intake air flow is attenuated early in the compression stroke.

そうかといって、流速をで外るだけ高めようとして、低
負荷用吸気通路を絞りすぎれば、それだけ賄いうる負荷
範囲か制限され、比較的低い負荷域でシャッターバルブ
を開いて高負荷用吸気通路からも吸気を供給する必要が
生ずる。その場合、2つの吸気ポートは、燃焼室の水平
方向中心線に関して対向的に形成されているため、低負
荷用吸気ボートから吸入される吸気流と高負荷用吸気ボ
ートから吸入される吸気流とが衝突して、スワールが消
滅されないまでもますます弱められてしまい、スワール
による良好な燃焼性を確保し難い欠点かある。
On the other hand, if you try to increase the flow velocity and restrict the low-load intake passage too much, the load range that can be covered will be limited. It is also necessary to supply intake air from the In that case, the two intake ports are formed opposite to each other with respect to the horizontal center line of the combustion chamber, so that the intake air flow taken in from the low-load intake boat and the intake flow taken in from the high-load intake boat are different. If the swirls collide with each other, the swirl is further weakened, if not eliminated, making it difficult to ensure good combustibility due to the swirl.

以1ユのように、低負荷用吸気通路およびこれに接続さ
れる吸気ポートを絞ることは、高出力化を図る目的とは
相客れも・いのみならず、種々の新たな不具合を招来す
る。
As shown in Figure 1 above, narrowing down the low-load intake passage and the intake port connected to it not only contradicts the purpose of achieving high output, but also causes various new problems. do.

本出願人は、エンジンの高出力化をねらった2吸気ポ一
ト方式を実質的に変更することなしに、エンジンの低負
荷運転時において燃焼室内に燃焼性の向」二を図るのに
有効なスワールを生成することかでトる吸気構造を備え
たエンジンの吸気装置を特願昭58−176776号に
おいて既に提案している。
The present applicant has discovered that the two-intake point system, which aims to increase engine output, is effective in improving combustibility within the combustion chamber during low-load operation of the engine without substantially changing the two-intake point system. Japanese Patent Application No. 58-176,776 has already proposed an engine intake system having an intake structure that generates a swirl.

この提案にかかる発明は、複数の吸気ポー)をエンジン
の燃焼室にそれぞれ開口させ、各吸気ポートを吸気弁で
開閉するようにしたエンジンの吸気装置において、複数
の吸気ポートに接続される吸気通路内に開閉弁を配設し
て、この開閉弁を低負荷運転時には閉じ高負荷運転時に
は開くようにエンジンの運転状態に応じて上記吸気通路
の通路面積を増減制御する一力、上記開閉弁よりも」−
流の吸気通路の底部から分岐し、上記吸気ボートのいず
れか一つに接続され、通路面積力佳記吸気通路に比べて
小さい補助吸気通路を設けたことを基本的な特徴として
いる。
The proposed invention relates to an intake system for an engine in which a plurality of intake ports are respectively opened into combustion chambers of an engine, and each intake port is opened and closed by an intake valve. An on-off valve is disposed inside the engine, and the on-off valve is closed during low-load operation and opened during high-load operation. Mo”-
The basic feature is that an auxiliary intake passage is provided, which branches off from the bottom of the air intake passage, is connected to any one of the intake boats, and is smaller in area than the intake passage.

即ち、この発明においては、開閉弁か閉しられるエンノ
ンの低負荷運転時、吸気は専ら吸気通路の底部側に形成
された補助吸気通路からこの通路が接続された吸気ポー
トを介して早い流速でエンジンの燃焼室に供給される。
That is, in this invention, during low-load operation of the Ennon when the on-off valve is closed, intake air flows exclusively from the auxiliary intake passage formed at the bottom of the intake passage through the intake port to which this passage is connected at a high flow rate. Supplied to the combustion chamber of the engine.

その場合、補助吸気通路は、吸気通路の底部11111
に形成されていることか呟シリンダヘッドとシリンダブ
ロックとの合せ面に則して必然的に浅い角度をなし、燃
焼室内に流入した吸気は、燃焼室の周方向に旋回するス
ワールを生成することかでS、また、開閉弁か開かれる
エンジンの高負荷運転時には、複数の吸気ポートから充
填効率よく吸気が吸入され、本来の高出力を保証するこ
とができるのである。
In that case, the auxiliary intake passage is located at the bottom 11111 of the intake passage.
This naturally forms a shallow angle in line with the mating surfaces of the cylinder head and cylinder block, and the intake air flowing into the combustion chamber generates a swirl that swirls in the circumferential direction of the combustion chamber. Furthermore, during high-load operation of the engine when the on-off valve is opened, intake air is drawn in from a plurality of intake ports with high filling efficiency, and the original high output can be guaranteed.

したがって、この発明によれば、エンジンの高出力化と
いう2吸気ボ一ト方式本来の目的を何ら損なうことなし
に、低負荷運転時における燃焼性の向]−1さらには、
燃費性能およびエミッション性能の向−■−を図ること
ができるのであるが、なお改善の余地がある。
Therefore, according to the present invention, the combustibility during low-load operation can be improved without sacrificing the original purpose of the two-intake engine system, which is to increase engine output.
Although it is possible to improve fuel efficiency and emission performance, there is still room for improvement.

その一つば、前述した低負荷から高負荷への切替時に発
生しうる切替ショックの問題である。即ち、専ら補助吸
気通路が使用される低負荷領域から開閉弁が開かれる中
、高負荷域に移行する際には、多量の吸気が各吸気ボー
トから一時に燃焼室に流入するため、充填量が急増して
一種のトルクショックが発生するのである。
One of them is the above-mentioned problem of switching shock that may occur when switching from a low load to a high load. In other words, while the on-off valve is opened from the low-load region where the auxiliary intake passage is used exclusively, when moving to the high-load region, a large amount of intake air flows into the combustion chamber from each intake boat at once, so the charging amount decreases. increases rapidly, causing a kind of torque shock.

(発明の目的) 本発明の目的は、低負荷運転時のスワールを維持しつつ
、開閉弁を閉じた状態で賄いうる′低負荷領域を拡大し
、換言すれば、開閉弁の閉時と開時における吸気量ギヤ
ングを可能な限り小さくするように、閉時における吸気
量をある程度十分に確保することによって上記の如ト切
朴ショックを防止することである。
(Objective of the Invention) The object of the present invention is to expand the low load range that can be covered with the on-off valve closed while maintaining the swirl during low-load operation. The purpose is to prevent the above-mentioned cut-off shock by ensuring a sufficient amount of intake air when the valve is closed so as to minimize the amount of intake air when the valve is closed.

(発明の構成) このため、本発明は、燃焼室に開口する複数の吸気ボー
トと、下流において分岐される各分岐端が各吸気ボート
に夫々接続された吸気通路と、この吸気通路の分岐部よ
り上流に設けられ、低負荷時閉しられ高負荷時開かれる
開閉弁と、開閉弁より」−流の吸気通路から分岐し、下
流が吸気ボートのいずれか一つに接続される補助吸気通
路とを有するエンノンの吸気装置におい′ζ、上記補助
吸気通路の吸気ボート開口部を吸気通路の分岐部上流に
開口させるとともに、補助吸気通路の北方の吸気ボート
側の通路壁は、池方の吸気ボー1より補助吸気通路の開
1」する吸気ポート側へ傾斜むせて形成したものである
(Structure of the Invention) Therefore, the present invention provides a plurality of intake boats that open into a combustion chamber, an intake passage whose branch ends are connected to each intake boat and which are branched downstream, and a branch portion of the intake passage. An on-off valve that is provided further upstream and closes at low loads and opens at high loads, and an auxiliary intake passage that branches from the on-off intake passage and is connected to one of the intake boats downstream from the on-off valve. The intake boat opening of the auxiliary intake passage is opened upstream of the branch part of the intake passage, and the passage wall on the north side of the intake boat of the auxiliary intake passage is connected to the intake port of the auxiliary intake passage. It is formed so as to be inclined from the bow 1 toward the intake port side where the auxiliary intake passage is open 1''.

かかる設定により、補助吸気通路の吸気ボート開口部は
吸気通路が分岐する以前の共通の通路部に設けることか
できるので、大きな開口面積、特に幅方向寸法を確保す
ることかでと、ひいては補助吸気通路の通路断面積を大
きく確保することができ、補助吸気通路によって賄いう
る運転領域を拡大することができる。
With this setting, the intake boat opening of the auxiliary intake passage can be provided in the common passage before the intake passage branches, so it is possible to secure a large opening area, especially the width dimension, and the auxiliary intake A large cross-sectional area of the passage can be ensured, and the operating range that can be covered by the auxiliary intake passage can be expanded.

と同時に、上記のように、補助吸気通路をこの補助吸気
通路が開口される一方の吸気ポート側に傾斜して形成し
たので、補助吸気通路を流下して」二記一方の吸気ボー
トから燃焼室に流入する吸気流は燃焼室の周方向を指向
し、これによって強いスワールが燃焼室内に生成される
ことになる。
At the same time, as mentioned above, since the auxiliary intake passage is formed to be inclined toward the one intake port side where the auxiliary intake passage is opened, it flows down the auxiliary intake passage and from one intake boat to the combustion chamber. The intake air flow entering the combustion chamber is directed in the circumferential direction of the combustion chamber, thereby creating a strong swirl within the combustion chamber.

(発明の効果) したがって、本発明によれば、開閉弁を閉じた状態で賄
いうる負荷領域を、スワール性能を維持しつつ高負荷側
に拡大することができ、低負荷から高負荷へ移行する際
の所謂切替ショックを有効に防止することがでとる。
(Effects of the Invention) Therefore, according to the present invention, the load range that can be covered with the on-off valve closed can be expanded to the high load side while maintaining swirl performance, and the transition from low load to high load can be achieved. This makes it possible to effectively prevent the so-called switching shock at the time of switching.

(実施例) 以下、本発明の実施例についてより具体的に説明する。(Example) Examples of the present invention will be described in more detail below.

第1図に示すように、エンジンEの1つの気筒1の燃焼
室2には、エンジンEのシリンダブロックの幅方向中心
線でに関してほぼ対称に、はぼ同径の第1.第2の吸気
ボート4,5が開1]され、艮手方向中心線輪をはさん
で第1.第2吸気ボート4.5と対向する位置には、仙
気ポート6.7が開l]されている。
As shown in FIG. 1, in the combustion chamber 2 of one cylinder 1 of the engine E, there is a first cylinder 2 having approximately the same diameter, which is approximately symmetrical with respect to the center line in the width direction of the cylinder block of the engine E. The second intake boats 4, 5 are opened 1], and the first intake boat 4, 5 is opened 1], and the first intake boat 4, 5 is opened 1], and the first intake boat 4, 5 is opened 1]. An air port 6.7 is opened at a position facing the second air intake boat 4.5.

第1.第2吸気ボート4,5に吸気を供給する吸気通路
8は、シリンダヘッド(第2図:)0参照)内において
徐々に分岐され、第1.第2吸気ボート4.5の手前で
は、上記幅方向中心線でにほぼ沿って突出するように形
成された仕切壁9によって二叉に分岐され、これら分岐
吸気通路10.11か、第1.第2吸気ボート4,5に
それぞれ接続されている。図示の如く、吸気通路8の上
流側にはシャッターバルブフ゛】2を介設している。5
二のシャンターバルブ12は具体的に図示しないが、周
知の開閉制御(幾構(例えば、スロットルバルブに連結
されるリンク機構)によりエンノンEの低負荷運転時に
は吸気通路8を閉じ、高負荷運転時には、負荷に応じて
開くようにその開閉が制御される。そして、吸気通路8
のシャッターバルブ12より」ニ流側には、吸気通路8
の中心線に関して、第1吸気ボート4側にかだ寄せて補
助吸気通路13の上流側聞口13aを吸気通路8の底壁
に開口させている。この補助吸気通路13は、分岐吸気
通路10゜】1を仕切る仕切壁9の先端9aよI)僅か
上流側に開「比だ、吸気ポート開口部としての下流側聞
D 1311を有している。下流側聞I11131)を
かかる位置に設定十乞ことにより、特に幅方向=J法を
十分に確保することかできる。そして、補助吸気通路1
3は」1記幅方向中心線Pを横切るようにゆるやかに湾
曲して、上流側開口13aと下l光側開D 1313と
を連通する。即ち、補助吸気通路1:(の第2吸気ボー
ト5側の通路壁13cは、第2吸気ボート5側より第1
吸気ボート、1側に向けて仲。
1st. The intake passage 8 that supplies intake air to the second intake boats 4 and 5 gradually branches within the cylinder head (see Figure 2: ) 0). In front of the second intake boat 4.5, the branched intake passage 10.11 is divided into two by a partition wall 9 formed to protrude substantially along the center line in the width direction. They are connected to second intake boats 4 and 5, respectively. As shown in the figure, a shutter valve 2 is provided on the upstream side of the intake passage 8. 5
Although the second shunter valve 12 is not specifically shown, it closes the intake passage 8 during low load operation of the Ennon E by a well-known opening/closing control (a link mechanism connected to a throttle valve, for example), and closes the intake passage 8 during high load operation. Sometimes, the opening and closing of the intake passage 8 is controlled to open according to the load.
On the second flow side from the shutter valve 12, there is an intake passage 8.
With respect to the center line, the upstream opening 13a of the auxiliary intake passage 13 is opened at the bottom wall of the intake passage 8 by leaning toward the first intake boat 4 side. This auxiliary intake passage 13 is opened slightly upstream from the tip 9a of the partition wall 9 that partitions the branched intake passage 10°1, and has a downstream side D1311 serving as an intake port opening. By setting the downstream side passageway I11131) at such a position, it is possible to sufficiently ensure the width direction = J direction.
3 is gently curved so as to cross the width direction center line P mentioned in 1, and communicates between the upstream side opening 13a and the lower light side opening D 1313. That is, the passage wall 13c on the second intake boat 5 side of the auxiliary intake passage 1:(
Intake boat, towards the 1st side.

斜するように湾曲されている。It is curved at an angle.

上記補助吸気通路13は、第2図により兵庫的に示すよ
うに、吸気通路8の底部を形成する底壁14に形成され
、その下流側聞口13bは」−記仕切壁9のに流側端部
9a、即ち分岐吸気通路10゜11の分岐点より僅か上
流に設定されている。このため、補助吸気通路13を流
下する吸気は、両方の分岐吸気通路1O,11に分配さ
れるIjf能性があるか、補助吸気通路13か第1吸気
ボート・・1側に向けて傾斜して形成されているので、
吸気には第1吸気ボート4に向かう指向性か1)えられ
、はぼ全量が第1吸気ボート・・1から燃焼室ン内にl
Aら人することとなる。そして、補助吸気通路13は、
第1吸気ボート4の直」貿fIぼ゛気筒1の軸方向に湾
曲されている分岐吸気通路1()に月し、シリンダ70
ンク31とシリングへ7ド3()との合せ面Cに月して
僅かな傾き角をなすように交差しており、したかって、
燃焼室2の周方向に指向した方向性を有するようになる
As shown in FIG. 2, the auxiliary intake passage 13 is formed in a bottom wall 14 forming the bottom of the intake passage 8, and its downstream opening 13b is on the downstream side of the partition wall 9. It is set slightly upstream from the end 9a, that is, the branch point of the branched intake passage 10°11. Therefore, the intake air flowing down the auxiliary intake passage 13 has an Ijf ability to be distributed to both the branch intake passages 1O, 11, or the auxiliary intake passage 13 is inclined toward the first intake boat 1 side. Because it is formed by
The intake air has a directivity toward the first intake boat 4 (1), and almost the entire amount flows from the first intake boat 1 into the combustion chamber.
A and others will be doing so. The auxiliary intake passage 13 is
The first intake boat 4 is directly connected to the branch intake passage 1 () which is curved in the axial direction of the cylinder 1, and the cylinder 70
It intersects at a slight angle of inclination to the mating surface C of Nk 31 and Schilling 7D 3 (), and therefore,
It has directionality oriented in the circumferential direction of the combustion chamber 2.

1−記補助吸気通路13の上流側聞1−113 aより
僅か下;嘉には、吸気通路暮を開閉するシャッターパル
712を下流に向って斜め下向きに傾斜させて配設しさ
らにシャッターバルブ12より僅か下流の吸気通路8の
上壁16に予め設けた取(=1部16aには、燃料噴射
弁17を取伺けでいる。この場合、燃料噴射口18は、
シャンターパル712の回転軸121〕より僅か下流側
て゛かっ吸気通路8の中心線」二に位置するように設定
している。
1- Slightly below the upstream side of the auxiliary intake passage 13 1-113a; a shutter valve 712 for opening and closing the intake passage is provided so as to be inclined obliquely downward toward the downstream side, and the shutter valve 12 A fuel injection valve 17 can be inserted into a hole (=1 part 16a) previously provided on the upper wall 16 of the intake passage 8 located slightly downstream. In this case, the fuel injection port 18 is
It is set to be located slightly downstream of the rotating shaft 121 of the shunter pallet 712 and on the center line of the intake passage 8.

なお、第1吸気ボート4を開閉する吸気弁]5゜第2吸
気ボート5を開閉する吸気弁(図示せず)および仙気ボ
ート6、’7を開閉する抽気弁10(数カは図示せず)
は、周知のオーバーへ、ドカム(戊構20により、エン
ジ゛ンEの回転に同期したI91定のタイミングで夫々
開閉駆動される。
Note that the intake valve that opens and closes the first intake boat 4] 5. The intake valve that opens and closes the second intake boat 5 (not shown) and the bleed valve 10 that opens and closes the Senki boats 6 and '7 (the number is not shown). figure)
are driven to open and close by a well-known overdrive mechanism 20 at a fixed timing I91 synchronized with the rotation of the engine E.

また、第1図に示すように、点火プラグ21は、第1.
第2吸気ボー)11..5および抽気ボートし。
Further, as shown in FIG. 1, the spark plug 21 is connected to the first.
2nd intake bow) 11. .. 5 and bleed boat.

°7か設けられていない部分、より兵庫的には、jメに
焼室2の中心部分に設定する。
Set it in the center of the grilling chamber 2 in the part where it is not provided, more like Hyogo style.

]−記の補助吸気通路13の構成とすれは、補助吸気通
路13の通路面積を十分大トなものとすることか゛でき
るので、シャッターバルブ12を閉したままで賄いうる
負荷範囲を拡大でトるうえ、補助吸気通路13を流下す
る吸気は燃焼室2の周方向の指向性を有するので、その
拡大した負荷範囲内で良好な又ワールを維持することが
できることになる。
] - With the configuration of the auxiliary intake passage 13, the passage area of the auxiliary intake passage 13 can be made sufficiently large, so the load range that can be handled with the shutter valve 12 closed can be expanded. Moreover, since the intake air flowing down through the auxiliary intake passage 13 has directivity in the circumferential direction of the combustion chamber 2, a good whirl can be maintained within the expanded load range.

さらに、負荷範囲が高負荷側に拡大されるよっにシャッ
ターバルブ12の閉時の吸気量を確保できるため、シャ
7ターバルフ1ンか開かれる高負荷運転に移行されたと
しこも、シャッターバルブ12か開かれたときの吸気の
増加!’、i’1合は比較的小さくすることができ、所
謂切昔ションクを確実に防止することかてbる。
Furthermore, as the load range is expanded to the high load side, the amount of intake air when the shutter valve 12 is closed can be secured, so even if the shutter valve 12 is opened and shifted to high load operation, the shutter valve 12 Increased air intake when opened! ', i'1 can be made relatively small, thereby reliably preventing so-called cutting.

そして、シャ7ターバルフ1ンが開かれる高負荷連lk
では、第1.第2吸気ボート・・1,5から必要部分な
吸気が供給されζ、2ボ一1本米の高出力を保、111
する。
Then, the shutter valve is opened and the high load link is opened.
So, first. 2nd intake boat... Necessary intake air is supplied from 1 and 5, maintaining high output of ζ, 2 boats and 1 boat, 111
do.

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

第1図は本発明の天施例を示1エンノンの要部断面説明
図、第2図は第1図のII−II線方向の縦断面図であ
る。 2・・・燃焼室、 −・L、5・第1.第2吸気ボート
、し・・吸気通路、9・・・仕切壁、 H)、]]・・・分岐吸気通路、 12・・・シャッターバルブ、 13・・・補助吸気通路、 (13b・・・下流側聞り、13c・・・第2吸気ボー
ト側通路壁)、 14・・・底壁、 15・・・吸気弁。 特許出願人 東洋工業株式会社
FIG. 1 is an explanatory cross-sectional view of a main part of the top embodiment of the present invention, and FIG. 2 is a longitudinal cross-sectional view taken along the line II--II in FIG. 1. 2... Combustion chamber, - L, 5 1st. 2nd intake boat,...Intake passage, 9...Partition wall, H),]]...Branch intake passage, 12...Shutter valve, 13...Auxiliary intake passage, (13b... downstream side, 13c...second intake boat side passage wall), 14...bottom wall, 15...intake valve. Patent applicant: Toyo Kogyo Co., Ltd.

Claims (1)

【特許請求の範囲】[Claims] (1)それぞれ吸気弁により開閉される複数の吸気ボー
トを燃焼室に開口させるとともに、低負荷時閉じ高負荷
時開く開閉弁によって開閉され、該開閉弁下流で分岐さ
れ、各分岐端が上記吸気ポートにそれぞれ接続された吸
気通路と、上記開閉弁より上流の吸気通路から分岐し、
上記吸気ポートのいずれか一つに接続される補助吸気通
路とが設けられ、該補助吸気通路はその吸気ボート開口
部が吸気通路分岐点より上流に開口し、他方の吸気ボー
ト側の通路壁は、他方の吸気ポートより補助吸気通路の
開口する吸気ボート側へ傾斜して形成しすこことば特徴
とするエンジンの吸気装置。
(1) A plurality of intake boats each opened and closed by an intake valve are opened into the combustion chamber, and are opened and closed by an on-off valve that closes at low load and opens at high load, and are branched downstream of the on-off valve, and each branch end is connected to the intake boat An intake passage connected to each port and branched from an intake passage upstream of the above-mentioned on-off valve,
An auxiliary intake passage connected to any one of the intake ports is provided, and the auxiliary intake passage has an intake boat opening upstream of the intake passage branch point, and a passage wall on the other intake boat side. An intake system for an engine, characterized in that the intake port is inclined from the other intake port toward the intake boat side where the auxiliary intake passage opens.
JP59016823A 1984-01-31 1984-01-31 Intake device for engine Granted JPS60162017A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59016823A JPS60162017A (en) 1984-01-31 1984-01-31 Intake device for engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59016823A JPS60162017A (en) 1984-01-31 1984-01-31 Intake device for engine

Publications (2)

Publication Number Publication Date
JPS60162017A true JPS60162017A (en) 1985-08-23
JPH0330697B2 JPH0330697B2 (en) 1991-05-01

Family

ID=11926894

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59016823A Granted JPS60162017A (en) 1984-01-31 1984-01-31 Intake device for engine

Country Status (1)

Country Link
JP (1) JPS60162017A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2545946A (en) * 2015-09-18 2017-07-05 Maserati Spa An intake conduit

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2545946A (en) * 2015-09-18 2017-07-05 Maserati Spa An intake conduit
GB2545946B (en) * 2015-09-18 2021-03-10 Maserati Spa Intake conduit with variable geometry for an internal combustion engine

Also Published As

Publication number Publication date
JPH0330697B2 (en) 1991-05-01

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