JP2002364472A - Intake device for internal combustion engine - Google Patents

Intake device for internal combustion engine

Info

Publication number
JP2002364472A
JP2002364472A JP2002147071A JP2002147071A JP2002364472A JP 2002364472 A JP2002364472 A JP 2002364472A JP 2002147071 A JP2002147071 A JP 2002147071A JP 2002147071 A JP2002147071 A JP 2002147071A JP 2002364472 A JP2002364472 A JP 2002364472A
Authority
JP
Japan
Prior art keywords
intake
valve
internal combustion
combustion engine
intake pipe
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
JP2002147071A
Other languages
Japanese (ja)
Other versions
JP3786050B2 (en
Inventor
Minoru Osuga
大須賀  稔
Junichi Yamaguchi
純一 山口
Ryoichi Komuro
亮一 古室
Masayoshi Momono
正吉 桃野
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.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP2002147071A priority Critical patent/JP3786050B2/en
Publication of JP2002364472A publication Critical patent/JP2002364472A/en
Application granted granted Critical
Publication of JP3786050B2 publication Critical patent/JP3786050B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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

PROBLEM TO BE SOLVED: To simplify a structure of an intake passage in a device for generating a turning flow in an combustion chamber of an engine. SOLUTION: The air passing through a throttle valve 1 diverges at a collector part 3 and is led to an independent intake pipe 4. Then, the air passes an intake valve 5 and is sucked into a cylinder 6. An auxiliary pipe 7 is provided in the independent intake pipe 4, and two intake passages 8 are provided for bypassing it. The intake passage 8 is formed to be in a straight passage between the collector part 3 and a nozzle part of a fuel injection valve 10. The auxiliary valve 7 is opened usually. When performing lean combustion or when it is required to improve combustion such as at idling or at a low temperature, the auxiliary valve 7 is closed and the intake air is supplied to the cylinder 6 from the intake passage 8. Thus, the structure of the bypass intake passage for generating the turning flow in the combustion chamber can be simplified.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】エンジンの燃焼室に空気,燃
料を供給する吸気装置の構成に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a structure of an intake device for supplying air and fuel to a combustion chamber of an engine.

【0002】[0002]

【従来の技術】従来の吸気管においては、燃焼の効率を
高めるために機関の特定の運転状態で燃焼室内に旋回流
を積極的に発生させる試みがなされている。具体的には
吸気主通路に補助弁と補助弁をバイパスするバイパス通
路を設け、この補助弁を機関の特定の運転状態で閉じ
て、バイパス通路から燃焼室内に入る空気が燃焼室の入
口に対して特定の偏った位置から入るようにすることで
燃焼室内に旋回流を形成している。
2. Description of the Related Art In a conventional intake pipe, an attempt has been made to positively generate a swirling flow in a combustion chamber in a specific operating state of an engine in order to increase the efficiency of combustion. Specifically, an auxiliary valve and a bypass passage that bypasses the auxiliary valve are provided in the intake main passage, and the auxiliary valve is closed in a specific operation state of the engine, so that air entering the combustion chamber from the bypass passage flows to the inlet of the combustion chamber. As a result, a swirling flow is formed in the combustion chamber by entering from a specific biased position.

【0003】[0003]

【発明が解決しようとする課題】然るに従来の装置で
は、このバイパス通路が成形し難いという問題があっ
た。
However, the conventional apparatus has a problem that it is difficult to form the bypass passage.

【0004】本発明の目的は、燃焼室内に旋回流を発生
させるための分割通路,補助弁,バイパス通路の配置構
成を工夫して成形しやすい構成とすることを目的とす
る。
SUMMARY OF THE INVENTION It is an object of the present invention to improve the arrangement of a divided passage, an auxiliary valve, and a bypass passage for generating a swirling flow in a combustion chamber so that the structure can be easily formed.

【0005】[0005]

【課題を解決するための手段】上記目的は、コレクタと
エンジンヘッドとの間に位置する独立吸気管に、リーン
燃焼時やアイドルや低温時に閉じる補助弁と、燃料噴射
弁と、補助弁をバイパスしてコレクタと燃料噴射弁の噴
射口の両側とを結ぶ真直ぐな通路で構成することによっ
て達成される。
SUMMARY OF THE INVENTION An object of the present invention is to provide an independent intake pipe located between a collector and an engine head, the auxiliary valve being closed at the time of lean combustion, idling or low temperature, the fuel injection valve, and the auxiliary valve being bypassed. This is achieved by forming a straight passage connecting the collector and both sides of the injection port of the fuel injection valve.

【0006】好適には、独立吸気管内に設置された2個
の吸気通路の上流側開口部と下流側開口部との間の距離
が、独立吸気管の上流側開口部と下流側開口部との間の
距離に略等しくする。
Preferably, the distance between the upstream opening and the downstream opening of the two intake passages installed in the independent intake pipe is equal to the distance between the upstream opening and the downstream opening of the independent intake pipe. About equal to the distance between

【0007】また好適には、2個の吸気通路から噴出す
る空気の流れと、燃料噴射弁から噴出する燃料の流れと
が略並行に構成する。
[0007] Preferably, the flow of air ejected from the two intake passages and the flow of fuel ejected from the fuel injection valve are substantially parallel to each other.

【0008】さらに好適には、2個の吸気通路から噴出
する空気の流れと、燃料噴射弁から噴出する燃料の流れ
とが、内燃機関の吸気弁の表面上で衝突するよう構成す
る。
[0008] More preferably, the flow of air ejected from the two intake passages and the flow of fuel ejected from the fuel injection valve collide on the surface of the intake valve of the internal combustion engine.

【0009】また好適には、2個の吸気通路の上流側開
口部が、2個の吸気通路の下流側開口部が開口する前記
独立吸気管が接続された前記コレクタ内に開口するよう
構成する。
[0009] Preferably, the upstream openings of the two intake passages are opened in the collector connected to the independent intake pipe in which the downstream openings of the two intake passages are opened. .

【0010】さらに好適には、補助弁の開度を前記内燃
機関の運転状態によって変化させるよう構成する。
[0010] More preferably, the opening degree of the auxiliary valve is changed according to the operating state of the internal combustion engine.

【0011】またさらに好適には、補助弁をバイパスす
る2個の吸気通路は、独立吸気管を形成する吸気通路壁
面を貫通する真直ぐな通路で構成される。
Still more preferably, the two intake passages bypassing the auxiliary valve are constituted by straight passages penetrating the intake passage wall forming an independent intake pipe.

【0012】[0012]

【発明の実施の形態】図1,図2に本発明の第一実施例
を示す。絞り弁1を通過した吸気は上部コレクタ2を通
過したあと、左右に仕切られたコレクタ3a,3bに別
れる。さらに、これらのコレクタから独立吸気管4に分
岐されて、吸気弁5を通過しシリンダ6に吸入される。
ここで、シリンダ内に旋回流を作るために補助弁7とこ
れをバイパスした吸気通路8を設けている。通常は補助
弁7は開いているが、リーン燃焼をする場合や、アイド
ルや低温時のように燃焼を改善したい場合は、補助弁7
を閉じて、吸気を吸気通路8の方からシリンダ6内に供
給する。このようにすると、図1に一点鎖線で示した方
向に、指向性のある空気流を吸気弁5のある位置に供給
すると、独立吸気管4内に偏流ができ、シリンダ6内に
旋回流9が形成される。燃料は燃料噴射弁10から供給
される。図1ではV型のエンジンへの適用例を示してい
るが、直列エンジンにも適用できる。
1 and 2 show a first embodiment of the present invention. After passing through the throttle valve 1, the intake air passes through the upper collector 2, and is separated into left and right partitioned collectors 3a and 3b. Further, the air is branched from these collectors into an independent intake pipe 4, passes through an intake valve 5, and is sucked into a cylinder 6.
Here, an auxiliary valve 7 and an intake passage 8 bypassing the auxiliary valve 7 are provided in order to generate a swirling flow in the cylinder. Normally, the auxiliary valve 7 is open. However, when performing lean combustion, or when it is desired to improve combustion such as at idle or low temperature, the auxiliary valve 7 is opened.
Is closed, and the intake air is supplied into the cylinder 6 from the intake passage 8. In this manner, when a directional air flow is supplied to the position where the intake valve 5 is provided in the direction indicated by the one-dot chain line in FIG. Is formed. Fuel is supplied from a fuel injection valve 10. Although FIG. 1 shows an example of application to a V-type engine, the invention can also be applied to an in-line engine.

【0013】図2に図1で示した空気流と燃料噴霧の方
向を示す。図2に示した(イ)の点線の右側が吸気管2
0で左側がエンジンヘッド15である。補助弁7をバイ
パスした吸気通路8から吸気を供給しシリンダ6内に旋
回流9を形成する。ここで、燃料噴射弁は図示されてい
ないが、吸気通路8から噴出する空気流12の方向を燃
料噴霧11の方向に一致させ、空気流12と燃料噴霧1
1は吸気弁5に至るまで交差することがないように構成
する。このように構成することにより、燃料噴霧11が
高速の空気流12により偏向されることなく、吸気弁5
を直撃する。もし、燃料噴霧11に高速気流が衝突する
ように構成されていると、吸気管の壁面15に燃料噴霧
11が衝突し液膜が形成され燃焼が悪化する。このよう
に空気流12と燃料噴霧11の方向をほぼ平行にするこ
とにより燃料噴霧11性状を悪化することなく、シリン
ダ6内に旋回流を形成できる。吸気通路8の出口13は
境界(イ)に開口しており、ヘッド側には突き出ていな
い。また、ヘッド側には吸気通路8から噴き出る空気流
12を邪魔しないように、切欠き14が形成されてい
る。図2のように、燃料噴射弁と吸気通路8の出口の位
置はほぼ同じ高さになっている。この実施例では、空気
流12は吸気弁5の開いた場合の隙間を狙っており、燃
料噴霧11は吸気弁5上を狙って噴射される。このよう
な構成により、エンジンからの未燃焼炭化水素の排出量
を低減し、リーン状態での燃焼を安定化することができ
る。
FIG. 2 shows the directions of the air flow and the fuel spray shown in FIG. The right side of the dotted line (a) shown in FIG.
At 0, the engine head 15 is on the left side. The intake air is supplied from an intake passage 8 bypassing the auxiliary valve 7 to form a swirling flow 9 in the cylinder 6. Here, although the fuel injection valve is not shown, the direction of the air flow 12 ejected from the intake passage 8 is made to coincide with the direction of the fuel spray 11 so that the air flow 12 and the fuel
1 is configured so as not to cross up to the intake valve 5. With this configuration, the fuel spray 11 is not deflected by the high-speed airflow 12 and the intake valve 5
Directly hit. If the fuel spray 11 is configured to collide with the high-speed airflow, the fuel spray 11 collides with the wall surface 15 of the intake pipe, a liquid film is formed, and combustion deteriorates. By thus making the direction of the air flow 12 and the direction of the fuel spray 11 substantially parallel, a swirling flow can be formed in the cylinder 6 without deteriorating the properties of the fuel spray 11. The outlet 13 of the intake passage 8 opens at the boundary (a) and does not protrude toward the head. Further, a cutout 14 is formed on the head side so as not to obstruct the airflow 12 ejected from the intake passage 8. As shown in FIG. 2, the positions of the fuel injection valve and the outlet of the intake passage 8 are substantially at the same height. In this embodiment, the air flow 12 is aimed at the gap when the intake valve 5 is open, and the fuel spray 11 is injected over the intake valve 5. With such a configuration, the amount of unburned hydrocarbons emitted from the engine can be reduced, and the combustion in the lean state can be stabilized.

【0014】図3,図4は第二実施例であり、吸気通路
8の構成を示す。図3では燃料噴射弁10の先端部に吸
気通路8の出口13が開口している。その状態を(ロ)
の矢印の方向から見た図を図4に示す。ここでは吸気通
路8を燃料噴射弁10の両サイドに設けている。つま
り、ひとつのシリンダ当り2個の吸気通路8が設けられ
ている。このため、吸気通路8の出口部13は2か所と
なる。21は燃料噴射弁10からの燃料噴霧11が噴出
するために設けられた開口部である。この出口13はこ
の開口部21の両側に設けられることになる。図3では
V型エンジンの例を示したが、図2に示した様に直列エ
ンジンの場合も同様に適用できる。このように本発明
は、直列エンジン,水平対向エンジン,V型エンジンな
どすべてのエンジンに適応できる。
FIGS. 3 and 4 show a second embodiment, and show the structure of the intake passage 8. FIG. In FIG. 3, an outlet 13 of the intake passage 8 is opened at the tip of the fuel injection valve 10. (B)
FIG. 4 is a diagram viewed from the direction of the arrow of FIG. Here, the intake passage 8 is provided on both sides of the fuel injection valve 10. That is, two intake passages 8 are provided for each cylinder. Therefore, there are two outlet portions 13 of the intake passage 8. Reference numeral 21 denotes an opening provided for ejecting the fuel spray 11 from the fuel injection valve 10. The outlets 13 are provided on both sides of the opening 21. FIG. 3 shows an example of a V-type engine, but the present invention can be similarly applied to a serial engine as shown in FIG. As described above, the present invention can be applied to all engines such as an in-line engine, a horizontally opposed engine, and a V-type engine.

【0015】図5は第三実施例であり、V型エンジンで
の実施例を示す。補助弁7をバイパスした吸気通路8の
上流側の開口部22がコレクタ3bに開口しているが、
V型エンジンの場合は、コレクタ3a,3bの二つに隔
壁23で別れている。この場合、独立吸気管4での圧力
変動で吸気慣性過給が生じ、シリンダ6内に空気が充填
される。しかし、吸気通路8が図1に示したように、独
立吸気管4に対応していない別のバンクのコレクタ3a
に開口していたのでは、独立吸気管4内の圧力波が別バ
ンクのコレクタ3aに逃げてしまい慣性過給効果が減少
してしまう。そこで、図5に示すように、独立吸気管4
に設けられた吸気通路8の開口部22は、その独立吸気
管4に対応したコレクタ3bに開口するようにした。こ
の場合、圧力波は吸気通路8内と独立吸気管4内を同じ
ように伝搬するので、慣性過給効果は減少しない。ま
た、この圧力波の伝搬が時間的に同じになるように、通
路の両端の開口部間の距離(A〜B)と、それに対応す
る独立吸気管4での距離(A〜B)を同じにする必要が
ある。同じにすると、両者の圧力波のピーク時間が一致
するので、効果が大きくなる。
FIG. 5 shows a third embodiment, in which a V-type engine is used. An opening 22 on the upstream side of the intake passage 8 that bypasses the auxiliary valve 7 is open to the collector 3b.
In the case of the V-type engine, the collector is divided into two of the collectors 3a and 3b by a partition wall 23. In this case, pressure fluctuations in the independent intake pipe 4 cause intake inertia supercharging, and the cylinder 6 is filled with air. However, as shown in FIG. 1, the intake passage 8 does not correspond to the independent intake pipe 4, and the collector 3a of another bank is not provided.
, The pressure wave in the independent intake pipe 4 escapes to the collector 3a of another bank, and the inertia supercharging effect is reduced. Therefore, as shown in FIG.
The opening 22 of the intake passage 8 provided at the opening 3 is opened to the collector 3 b corresponding to the independent intake pipe 4. In this case, since the pressure wave propagates in the intake passage 8 and the independent intake pipe 4 in the same manner, the inertia supercharging effect does not decrease. In addition, the distance (A to B) between the openings at both ends of the passage and the corresponding distance (A to B) in the independent intake pipe 4 are the same so that the propagation of the pressure wave becomes the same in time. Need to be If they are the same, the peak time of both pressure waves coincide with each other, so that the effect is increased.

【0016】図6,図7は第四実施例であり、図6は上
方から見た吸気管の構成を、図7は図6の縦断面を示
す。燃料噴射弁10の両側に設けられた吸気通路8a,
8bからの空気流12は、燃料噴射弁10からの燃料噴
霧11を挟むように構成される。さらに、燃料噴霧11
は吸気弁5上の空気流12の当たる位置より内側に当た
るようにする。このようにすると、燃料噴霧11が吸気
弁5の外側に分散することなく、中心に集められる。つ
まり、空気流12がエアカーテンのような効果を示し、
燃料噴霧11の分散を防止する。シリンダ5に流入した
燃料噴霧25は点火プラグ24付近に集中し、供給空燃
比をリーンに設定した場合でも点火プラグ24の周りは
リッチになるので、失火することなく安定した燃焼が可
能となる。
FIGS. 6 and 7 show a fourth embodiment. FIG. 6 shows the structure of the intake pipe viewed from above, and FIG. 7 shows a longitudinal section of FIG. The intake passages 8a provided on both sides of the fuel injection valve 10,
The air flow 12 from 8b is configured to sandwich the fuel spray 11 from the fuel injection valve 10. Further, the fuel spray 11
Is made to hit inside the position where the air flow 12 on the intake valve 5 hits. In this way, the fuel spray 11 is collected at the center without dispersing outside the intake valve 5. That is, the airflow 12 exhibits an effect like an air curtain,
Dispersion of the fuel spray 11 is prevented. The fuel spray 25 flowing into the cylinder 5 concentrates in the vicinity of the spark plug 24 and becomes rich around the spark plug 24 even when the supply air-fuel ratio is set to lean, so that stable combustion can be performed without misfiring.

【0017】また、図2のように燃料噴射弁10と吸気
通路8の位置を同じ高さにするとエンジンヘッドに切欠
き14を設ける加工が必要となるが、図6のように独立
吸気管27側の燃料噴射弁10の下流に吸気通路8を設
けることにより、エンジンヘッド26を加工しなくても
吸気通路8を形成することができる。
When the position of the fuel injection valve 10 and the position of the intake passage 8 are set to the same height as shown in FIG. 2, it is necessary to provide a cutout 14 in the engine head, but as shown in FIG. By providing the intake passage 8 downstream of the fuel injection valve 10 on the side, the intake passage 8 can be formed without processing the engine head 26.

【0018】図8,図9は第五実施例であり、シリンダ
6内に旋回流を形成するための別の手段の実施例を示
す。独立吸気管4内に補助弁29を設けて、空気流に偏
流を与える方法である。この場合、図9に示すように補
助弁29の一部を切り欠くことにより空気流に偏流を与
えるようにする。この切り欠き部28a,28bの形状
を、燃料噴射弁10の噴射口の両側に位置するようにし
た。このようにすることにより、図6に示したように、
空気流で燃料噴射弁10からの燃料噴霧を挟むようにな
るので、燃料噴霧はシリンダの中心に集中するようにな
る。
FIGS. 8 and 9 show a fifth embodiment, which is another embodiment of another means for forming a swirling flow in the cylinder 6. FIG. This is a method in which an auxiliary valve 29 is provided in the independent intake pipe 4 to give a drift to the air flow. In this case, as shown in FIG. 9, a part of the auxiliary valve 29 is cut out to give a deviated air flow. The shapes of the notches 28a and 28b are located on both sides of the injection port of the fuel injection valve 10. By doing so, as shown in FIG.
Since the fuel spray from the fuel injection valve 10 is sandwiched by the airflow, the fuel spray is concentrated at the center of the cylinder.

【0019】一般に自動車では、吸気の量,燃料の量,
空燃比の量等をマイクロコンピュータを使用して制御し
ている。本発明でも空燃比,補助弁7,29の開度をマ
ップ状にメモリ素子に書き込み、制御値を読み出してい
る。図10に空燃比のマップの一例を、図11に補助弁
開度のマップの一例を示す。これらのマップは縦軸がエ
ンジン回転数Ne、横軸が燃料噴射量TPになってい
る。図10の例はリーン燃焼エンジンの制御用の設定目
標空燃比のマップであり、運転状態によって目標空燃比
が異なっている。また、図11は、補助弁7,29の開
度の設定値のマップであり、数値が大きい方が開度が小
さい。つまり、数値が大きい方が吸気通路8を流れる空
気量が多い。このように運転状態によってこの補助弁
7,29の開度を変えることにより、最適な旋回流を得
ることができ、各運転状態で最適な空燃比を得ることが
できる。
Generally, in an automobile, the amount of intake air, the amount of fuel,
The air-fuel ratio and the like are controlled using a microcomputer. In the present invention as well, the air-fuel ratio and the degree of opening of the auxiliary valves 7 and 29 are written into the memory element in a map form, and the control values are read. FIG. 10 shows an example of an air-fuel ratio map, and FIG. 11 shows an example of an auxiliary valve opening degree map. In these maps, the vertical axis represents the engine speed Ne, and the horizontal axis represents the fuel injection amount TP. The example of FIG. 10 is a map of the set target air-fuel ratio for controlling the lean combustion engine, and the target air-fuel ratio differs depending on the operation state. FIG. 11 is a map of the set values of the opening degrees of the auxiliary valves 7 and 29. The larger the numerical value, the smaller the opening degree. That is, the larger the numerical value, the larger the amount of air flowing through the intake passage 8. By changing the opening degree of the auxiliary valves 7 and 29 depending on the operation state, an optimum swirl flow can be obtained, and an optimum air-fuel ratio can be obtained in each operation state.

【0020】図12に第六実施例を示す。図12は、二
つの吸気通路8が吸気弁5の内側を狙った場合で、シリ
ンダ6内に縦方向の旋回流を形成する。吸気通路8は独
立吸気管4の端に設けているので、主の空気流の邪魔に
ならない。吸気通路8の上流側の開口部30は、独立吸
気管4の上流のコレクタに開口している。
FIG. 12 shows a sixth embodiment. FIG. 12 shows a case where the two intake passages 8 aim inside the intake valve 5, and forms a vertical swirling flow in the cylinder 6. Since the intake passage 8 is provided at the end of the independent intake pipe 4, it does not obstruct the main airflow. The opening 30 on the upstream side of the intake passage 8 opens to a collector upstream of the independent intake pipe 4.

【0021】図13に第七実施例を示す。図13は、二
つの吸気通路8を並行に構成した例である。このように
すると、シリンダ6内で空気流が衝突することなく、縦
方向の旋回流が確実に形成される。
FIG. 13 shows a seventh embodiment. FIG. 13 is an example in which two intake passages 8 are configured in parallel. In this way, a vertical swirling flow is reliably formed without collision of the air flow in the cylinder 6.

【0022】図14は、第八実施例であり、吸気通路の
一方8aが吸気弁5aの内側を狙って燃料を噴射するよ
うに構成されており、もう一方の吸気通路8bは吸気弁
5bの外側を狙って燃料を噴射するように構成されてい
る。これによりシリンダ6内に横の旋回流を形成でき
る。また、吸気通路8a,8bを図の紙面に垂直な方向
に傾斜させることにより、斜めの旋回流をシリンダ6内
に形成することもできる。
FIG. 14 shows an eighth embodiment, in which one of the intake passages 8a is configured to inject fuel aiming at the inside of the intake valve 5a, and the other intake passage 8b is connected to the intake valve 5b. It is configured to inject fuel aiming at the outside. Thereby, a horizontal swirling flow can be formed in the cylinder 6. Further, an inclined swirling flow can be formed in the cylinder 6 by inclining the intake passages 8a and 8b in a direction perpendicular to the plane of the drawing.

【0023】図15は、第九実施例であり、吸気通路8
a,8bともそれぞれ吸気弁5a,5bの外側を狙って
燃料を噴射するように構成している。これによりシリン
ダ6内に二重の旋回流を形成できる。
FIG. 15 shows a ninth embodiment in which the intake passage 8
Both a and 8b are configured to inject fuel aiming outside the intake valves 5a and 5b, respectively. Thereby, a double swirling flow can be formed in the cylinder 6.

【0024】図16は、第十実施例であり、吸気通路8
aは吸気弁5bの外側、吸気通路8bは吸気弁5bの外
側を狙う燃料を噴射するようにした構成である。これ
は、シリンダ内に横または斜めの旋回流を形成するため
のものである。以上のように吸気通路8の方向を選定す
ることにより、シリンダ6内に所望の旋回流を形成でき
る。図17から図19は独立吸気管4を側方から見た例
で、独立吸気管4内に吸気に偏流を与える補助弁を用い
た場合の実施例を示す。図中の上方に補助弁の正面から
見た形状も示してある。
FIG. 16 shows a tenth embodiment in which the intake passage 8
“a” is configured to inject fuel aimed at the outside of the intake valve 5b and the intake passage 8b is configured to inject fuel aimed at the outside of the intake valve 5b. This is for forming a horizontal or oblique swirling flow in the cylinder. By selecting the direction of the intake passage 8 as described above, a desired swirling flow can be formed in the cylinder 6. FIGS. 17 to 19 show examples of the independent intake pipe 4 viewed from the side, and show an embodiment in which an auxiliary valve for giving a bias to intake air is used in the independent intake pipe 4. The shape seen from the front of the auxiliary valve is also shown in the upper part of the figure.

【0025】図17は、第十一実施例であり、補助弁4
0の下部が切り欠かれており、空気はこの切欠き41を
通って偏流される。しかし、この偏流された空気流は高
速なために、燃料噴射弁10からの燃料噴霧43は偏向
されて、壁面44に付着してしまう。そこで補助弁40
の上部に切欠き42を設け、燃料噴霧方向補正用の空気
流45を流し、燃料噴霧43が曲がるのを防止する。
FIG. 17 shows an eleventh embodiment in which the auxiliary valve 4 is used.
The lower part of 0 is notched and the air is deflected through this notch 41. However, due to the high speed of the deflected air flow, the fuel spray 43 from the fuel injection valve 10 is deflected and adheres to the wall surface 44. Therefore, the auxiliary valve 40
A notch 42 is provided in the upper part of the nozzle, and an air flow 45 for correcting the fuel spray direction flows to prevent the fuel spray 43 from bending.

【0026】図18は、第十二実施例であり、独立吸気
管4に隔壁46を設け、その上部に補助弁47を設け
る。この隔壁46の下部を吸気偏流用の高速空気流が流
れ、燃料噴霧43には吸気弁5の近傍で衝突するので燃
料噴霧43が偏向されることはない。
FIG. 18 shows a twelfth embodiment in which a partition wall 46 is provided in the independent intake pipe 4 and an auxiliary valve 47 is provided above the partition wall. The high-speed airflow for the intake air drift flows under the partition wall 46 and collides with the fuel spray 43 near the intake valve 5, so that the fuel spray 43 is not deflected.

【0027】図19は、第十三実施例であり、補助弁4
8の下部49に燃料噴射弁10からの燃料噴霧43を衝
突させて微粒化させる構造になっている。このように、
燃料が微粒化されていると、たとえ偏向されても独立吸
気管4内の壁面に付着することなく吸気と一緒に燃焼室
内に流入する。
FIG. 19 shows a thirteenth embodiment in which the auxiliary valve 4
The fuel spray 43 from the fuel injection valve 10 collides with the lower portion 49 of the nozzle 8 to atomize it. in this way,
If the fuel is atomized, even if it is deflected, the fuel flows into the combustion chamber together with the intake air without adhering to the wall surface in the independent intake pipe 4.

【0028】図20から図22は独立吸気管4を側方か
ら見た例で、独立吸気管4内に補助弁を設けた場合の別
の実施例を示す。
FIGS. 20 to 22 show another embodiment in which an auxiliary valve is provided in the independent intake pipe 4 when the independent intake pipe 4 is viewed from the side.

【0029】図20は、第十四実施例であり、補助弁5
0の一部を切り欠いて吸気に偏流を与える。さらに、こ
の偏流した高速の空気流に対し、燃料噴霧43と反対側
に吸気通路51から、高速の空気流52を供給する。こ
の高速の空気流52により燃料噴霧43が偏向されるの
が防止できる。この高速の空気流52は絞り弁または補
助弁50をバイパスした通路によって得ることができ
る。
FIG. 20 shows a fourteenth embodiment in which the auxiliary valve 5 is used.
A part of 0 is cut out to give a drift to the intake air. Further, a high-speed airflow 52 is supplied to the deflected high-speed airflow from the intake passage 51 on the side opposite to the fuel spray 43. The high-speed air flow 52 can prevent the fuel spray 43 from being deflected. This high velocity air flow 52 can be obtained by a passage bypassing the throttle valve or auxiliary valve 50.

【0030】図21は、第十五実施例であり、独立吸気
管4に隔壁54を設け、その下部に補助弁53を設け、
上部を空気流55が流れるように構成した。この時の空
気流55は吸気弁5の近傍で燃料噴霧43と衝突するた
めに、燃料噴霧43は偏向されることはない。
FIG. 21 shows a fifteenth embodiment in which a partition wall 54 is provided in the independent intake pipe 4, and an auxiliary valve 53 is provided below the partition wall 54.
The upper part was configured so that the air flow 55 flows. At this time, since the air flow 55 collides with the fuel spray 43 near the intake valve 5, the fuel spray 43 is not deflected.

【0031】図22は、第十六実施例であり、補助弁5
6に燃料噴霧43の通過位置に対応した位置に切欠き5
7を設けた。この切欠き57を燃料噴霧43と高速の偏
流用空気流とが一緒に通過するために、燃料噴霧43は
偏向されることなく空気流と同じ方向に飛翔する。この
空気流と燃料噴霧43の飛翔方向を吸気弁5の所望の位
置に設定することにより、シリンダ内に旋回流を形成し
つつ、良好な混合気分布を得ることができる。
FIG. 22 shows a sixteenth embodiment in which the auxiliary valve 5 is used.
6 has a notch at a position corresponding to the passing position of the fuel spray 43.
7 was provided. Since the fuel spray 43 and the high-speed drift air flow pass through the notch 57 together, the fuel spray 43 flies in the same direction as the air flow without being deflected. By setting the flight direction of the air flow and the fuel spray 43 to a desired position of the intake valve 5, it is possible to obtain a good air-fuel mixture distribution while forming a swirl flow in the cylinder.

【0032】なお、図17,図19,図20,図22で
は補助弁の切欠き部を下部に設けた構成を示したが、補
助弁の上部に切欠きを設けた構成にしても良い。また、
図17では、切欠きを上部に設け、燃料噴霧偏向防止用
の空気流を作るための切欠きを下部に設けても良い。図
19では、補助弁の切欠きを上部に設けて、その上端に
燃料噴霧を衝突させ微粒化するようにしても良い。図2
0では、切欠きを上部に設け、燃料噴霧補正用の空気流
を作る通路を下部から供給しても良い。さらに、図22
では、切欠きを補助弁の上部に設けても良い。さらに、
図17から図22の例では、燃料噴射弁からの燃料噴霧
が二方向の場合を示したが、一方向の燃料噴霧の場合
も、同様の構成として同様の効果を得ることができる。
Although FIGS. 17, 19, 20, and 22 show the configuration in which the notch portion of the auxiliary valve is provided in the lower portion, a configuration in which a notch is provided in the upper portion of the auxiliary valve may be used. Also,
In FIG. 17, a notch may be provided in the upper part, and a notch for creating an airflow for preventing fuel spray deflection may be provided in the lower part. In FIG. 19, the notch of the auxiliary valve may be provided at the upper part, and the fuel spray may collide with the upper end to atomize. FIG.
In the case of 0, a notch may be provided in the upper portion, and a passage for creating an air flow for fuel spray correction may be supplied from the lower portion. Further, FIG.
Then, a notch may be provided in the upper part of the auxiliary valve. further,
17 to 22 show the case where the fuel spray from the fuel injection valve is in two directions, but in the case of one-way fuel spray, the same effect can be obtained with a similar configuration.

【0033】[0033]

【発明の効果】本発明によれば、2個の吸気通路は一端
がコレクタに開口し、他端が独立吸気管の燃料噴射弁噴
口の両側に開口する真直ぐな通路で構成するので、吸気
通路の形成が容易である。
According to the present invention, the two intake passages are formed as straight passages having one end opening to the collector and the other end opening to both sides of the fuel injection valve nozzle of the independent intake pipe. Is easy to form.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明の第一実施例を示し、吸気系全体の構成
図。
FIG. 1 shows a first embodiment of the present invention, and is a configuration diagram of an entire intake system.

【図2】図1の吸気管の構成図。FIG. 2 is a configuration diagram of an intake pipe of FIG. 1;

【図3】本発明の第二実施例を示し、V型エンジンの吸
気通路の構成図。
FIG. 3 shows a second embodiment of the present invention and is a configuration diagram of an intake passage of a V-type engine.

【図4】図3の(ロ)矢視図。FIG. 4 is a view taken in the direction of the arrow (b) in FIG. 3;

【図5】本発明の第三実施例を示し、吸気系全体の構成
図。
FIG. 5 shows a third embodiment of the present invention, and is a configuration diagram of an entire intake system.

【図6】本発明の第四実施例を示し、上方から見た吸気
管の構成図。
FIG. 6 shows a fourth embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from above.

【図7】図6の縦断面図。FIG. 7 is a longitudinal sectional view of FIG. 6;

【図8】本発明の第五実施例を示し、吸気管の構成図。FIG. 8 shows a fifth embodiment of the present invention, and is a configuration diagram of an intake pipe.

【図9】補助弁の正面図。FIG. 9 is a front view of an auxiliary valve.

【図10】エンジン制御用の空燃比のマップ図。FIG. 10 is a map diagram of an air-fuel ratio for engine control.

【図11】エンジン制御用の補助弁開度のマップ図。FIG. 11 is a map diagram of an opening degree of an auxiliary valve for engine control.

【図12】本発明の第六実施例を示し、上方から見た吸
気管の構成図。
FIG. 12 shows a sixth embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from above.

【図13】本発明の第七実施例を示し、上方から見た吸
気管の構成図。
FIG. 13 shows a seventh embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from above.

【図14】本発明の第八実施例を示し、上方から見た吸
気管の構成図。
FIG. 14 shows an eighth embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from above.

【図15】本発明の第九実施例を示し、上方から見た吸
気管の構成図。
FIG. 15 shows a ninth embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from above.

【図16】本発明の第十実施例を示し、上方から見た吸
気管の構成図。
FIG. 16 is a view showing the configuration of an intake pipe viewed from above according to a tenth embodiment of the present invention.

【図17】本発明の第十一実施例を示し、側方から見た
吸気管の構成図。
FIG. 17 shows the eleventh embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from a side.

【図18】本発明の第十二実施例を示し、側方から見た
吸気管の構成図。
FIG. 18 shows a twelfth embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from a side.

【図19】本発明の第十三実施例を示し、側方から見た
吸気管の構成図。
FIG. 19 shows a thirteenth embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from a side.

【図20】本発明の第十四実施例を示し、側方から見た
吸気管の構成図。
FIG. 20 shows a fourteenth embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from the side.

【図21】本発明の第十五実施例を示し、側方から見た
吸気管の構成図。
FIG. 21 is a side view showing the configuration of an intake pipe according to a fifteenth embodiment of the present invention.

【図22】本発明の第十六実施例を示し、側方から見た
吸気管の構成図。
FIG. 22 shows the sixteenth embodiment of the present invention, and is a configuration diagram of an intake pipe viewed from a side.

【符号の説明】[Explanation of symbols]

1…絞り弁、3a,3b…コレクタ、4…独立吸気管、
5…吸気弁、6…シリンダ、7,29,40,47,4
8,50,53,56…補助弁、8,8a,8b…吸気
通路、9…旋回流、10…燃料噴射弁、11…燃料噴
霧、12…空気流。
1 ... Throttle valve, 3a, 3b ... Collector, 4 ... Independent intake pipe,
5 ... intake valve, 6 ... cylinder, 7, 29, 40, 47, 4
8, 50, 53, 56: auxiliary valve, 8, 8a, 8b: intake passage, 9: swirl flow, 10: fuel injection valve, 11: fuel spray, 12: air flow.

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.7 識別記号 FI テーマコート゛(参考) F02M 69/04 F02M 35/10 102R 69/00 350A 350W (72)発明者 古室 亮一 茨城県日立市大みか町七丁目1番1号 株 式会社日立製作所日立研究所内 (72)発明者 桃野 正吉 茨城県勝田市大字高場2520番地 株式会社 日立製作所自動車機器事業部内 Fターム(参考) 3G023 AA00 AA04 AA18 AB01 AC02 AD06 AF01 AG02 ──────────────────────────────────────────────────の Continued on the front page (51) Int.Cl. 7 Identification symbol FI Theme coat ゛ (Reference) F02M 69/04 F02M 35/10 102R 69/00 350A 350W (72) Inventor Ryoichi Furumuro Omika, Hitachi City, Ibaraki Prefecture 7-1-1, Cho, Hitachi, Ltd. Hitachi Research Laboratory, Ltd. (72) Inventor Masayoshi Momono 2520 Kataida, Ibaraki Pref. AD06 AF01 AG02

Claims (7)

【特許請求の範囲】[Claims] 【請求項1】内燃機関の燃焼室入口の吸気弁部に接続さ
れ、空気を内燃機関の燃焼室に導入する複数個の独立吸
気管、 当該独立吸気管に接続されるとともに導入された前記空
気を前記独立吸気管に分配するコレクタ、 前記独立吸気管の壁面に設置され燃料を供給する燃料噴
射弁、 前記独立吸気管に設けられ機関の特定の運転状態で閉じ
る補助弁、 一端が前記コレクタに開口され、前記補助弁をバイパス
して、その他端が前記燃料噴射弁の噴射口の両側で前記
独立吸気管通路部に開口される真直ぐな通路で形成され
た2個の吸気通路を備えた内燃機関の吸気装置。
A plurality of independent intake pipes connected to an intake valve at an inlet of a combustion chamber of the internal combustion engine for introducing air into the combustion chamber of the internal combustion engine; and the air connected to and introduced to the independent intake pipe. A fuel injection valve installed on a wall surface of the independent intake pipe to supply fuel, an auxiliary valve provided on the independent intake pipe and closed in a specific operation state of an engine, and one end provided to the collector. An internal combustion engine having two intake passages which are opened and bypass the auxiliary valve and are formed at the other end with straight passages open to the independent intake pipe passage portion on both sides of the injection port of the fuel injection valve. Engine intake device.
【請求項2】請求項1の記載において、前記独立吸気管
内に設置された前記2個の吸気通路の上流側開口部と下
流側開口部との間の距離が、前記独立吸気管の上流側開
口部と下流側開口部との間の距離に略等しい内燃機関の
吸気装置。
2. The independent intake pipe according to claim 1, wherein a distance between an upstream opening and a downstream opening of the two intake passages installed in the independent intake pipe is an upstream side of the independent intake pipe. An intake device for an internal combustion engine that is substantially equal to the distance between the opening and the downstream opening.
【請求項3】請求項1の記載において、前記2個の吸気
通路から噴出する空気の流れと、前記燃料噴射弁から噴
出する燃料の流れとが略並行である内燃機関の吸気装
置。
3. An intake system for an internal combustion engine according to claim 1, wherein the flow of air ejected from said two intake passages and the flow of fuel ejected from said fuel injection valve are substantially parallel.
【請求項4】請求項1の記載において、前記2個の吸気
通路から噴出する空気の流れと、前記燃料噴射弁から噴
出する燃料の流れとが、前記内燃機関の吸気弁の表面上
で衝突する内燃機関の吸気装置。
4. A flow according to claim 1, wherein a flow of air ejected from said two intake passages and a flow of fuel ejected from said fuel injection valve collide on a surface of an intake valve of said internal combustion engine. Intake device for an internal combustion engine.
【請求項5】請求項1の記載において、前記2個の吸気
通路の上流側開口部が、前記2個の吸気通路の下流側開
口部が開口する前記独立吸気管が接続された前記コレク
タ内に開口している内燃機関の吸気装置。
5. The collector according to claim 1, wherein an upstream opening of said two intake passages is open to a downstream opening of said two intake passages and said independent intake pipe is connected thereto. An intake device for an internal combustion engine that is open to the inside.
【請求項6】請求項1の記載において、前記補助弁の開
度を前記内燃機関の運転状態によって変化させる内燃機
関の吸気装置。
6. An intake device for an internal combustion engine according to claim 1, wherein an opening degree of said auxiliary valve is changed according to an operation state of said internal combustion engine.
【請求項7】請求項1の記載において、前記補助弁をバ
イパスする前記2個の吸気通路は前記独立吸気管を形成
する吸気通路壁面を貫通する真直ぐな通路である内燃機
関の吸気装置。
7. An intake system for an internal combustion engine according to claim 1, wherein said two intake passages bypassing said auxiliary valve are straight passages penetrating an intake passage wall forming said independent intake pipe.
JP2002147071A 2002-05-22 2002-05-22 Intake device for internal combustion engine Expired - Fee Related JP3786050B2 (en)

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Application Number Priority Date Filing Date Title
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Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2002147071A JP3786050B2 (en) 2002-05-22 2002-05-22 Intake device for internal combustion engine

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
JP09106294A Division JP3329935B2 (en) 1994-04-28 1994-04-28 Intake device for internal combustion engine

Publications (2)

Publication Number Publication Date
JP2002364472A true JP2002364472A (en) 2002-12-18
JP3786050B2 JP3786050B2 (en) 2006-06-14

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JPH0693866A (en) * 1992-09-11 1994-04-05 Suzuki Motor Corp Intake system for engine
JPH06108951A (en) * 1992-09-25 1994-04-19 Mitsubishi Motors Corp Intake port structure of stratified charge combustion type internal combustion engine

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