JPS60150471A - Suction device for internal-combustion engine - Google Patents

Suction device for internal-combustion engine

Info

Publication number
JPS60150471A
JPS60150471A JP59007752A JP775284A JPS60150471A JP S60150471 A JPS60150471 A JP S60150471A JP 59007752 A JP59007752 A JP 59007752A JP 775284 A JP775284 A JP 775284A JP S60150471 A JPS60150471 A JP S60150471A
Authority
JP
Japan
Prior art keywords
intake
primary
passage
engine
suction
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
JP59007752A
Other languages
Japanese (ja)
Inventor
Yoshiaki Hidaka
義明 日高
Kiyoshi Ishii
清 石井
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.)
Honda Motor Co Ltd
Original Assignee
Honda Motor Co 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 Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Priority to JP59007752A priority Critical patent/JPS60150471A/en
Publication of JPS60150471A publication Critical patent/JPS60150471A/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
    • F02B27/00Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
    • F02B27/02Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means
    • F02B27/0205Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means characterised by the charging effect
    • F02B27/0215Oscillating pipe charging, i.e. variable intake pipe length charging
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B27/00Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
    • F02B27/02Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means
    • F02B27/0226Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means characterised by the means generating the charging effect
    • F02B27/0289Intake runners having multiple intake valves per cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/22Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • 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)

Abstract

PURPOSE:To bring a suction inertial effect into full action as well as to improve both combustion and charging efficiencies in a low load operation range of an engine, by connecting a primary suction passage and a secondary suction passage being reversed with each other to a suction port, while forming the primary suction passage into being long in its pipe length. CONSTITUTION:At a low load operation range of an engine, a shutter valve 33 is closed and suction air flows from a suction distributor chamber 22 to a primary suction passage 20, while part of it flows into a secondary suction passage 21 at the more downstream than the shutter valve 33 by way of a bypass passage 32, firnally flowing in a combustion chamber 9. Likewise, at a high load operation range of the engine, the shutter valve 33 is opened whereby the suction air flows into the combustion chamber 9 from both these primary and secondary suction passages 20 and 21.

Description

【発明の詳細な説明】 本発明は充填効率、燃焼効率を高めて出力性能を大幅に
向上させた内燃機関の吸気装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an intake system for an internal combustion engine that has improved charging efficiency and combustion efficiency to significantly improve output performance.

一般に内燃機関にお−・ては、機関の全負荷運転域、就
中その低負荷運転域での充填効率、燃焼効率を高めるこ
とが機関性能の向上に大きく寄与することが知られてい
る。そこで従来では、燃焼室に吸気弁で開閉される2つ
の吸気ボートを開口し、それらの吸気ボートに吸気通路
をそれぞれ連通させ、それらの通路の一方もしくは両方
にンヤノタバルブを設け、それらのシャッタバルブを開
閉制御して機関の低、高負荷運転域での充填効率、燃焼
効率を高めるようにした技術手段が種々提案されている
が、それらは何れも所期の効果が十分に達成できなかっ
たり、またコスト高になったりして必らずしも満足のい
くものではなかった。
In general, in internal combustion engines, it is known that increasing the charging efficiency and combustion efficiency in the engine's full load operating range, especially in its low load operating range, greatly contributes to improving engine performance. Conventionally, therefore, two intake boats that are opened and closed by intake valves are opened in the combustion chamber, intake passages are communicated with each of the intake boats, a Nyanota valve is provided in one or both of these passages, and the shutter valves are connected to the combustion chamber. Various technical means have been proposed to increase the charging efficiency and combustion efficiency in the low and high load operating ranges of the engine by controlling opening and closing, but none of them have been able to sufficiently achieve the desired effect. Furthermore, the cost was high and the results were not always satisfactory.

本発明は上記実情にかんがみてなされたもので、機関の
運転域、特にその低負荷運転域での充填効率、および燃
焼効率を大幅に高め、もって出力性能を著しく向−ヒさ
せるようにした構造簡栄な内燃機関の吸気製品を提供す
ることを目的とするものである。
The present invention has been made in view of the above-mentioned circumstances, and has a structure that significantly increases the charging efficiency and combustion efficiency in the operating range of the engine, especially in the low-load operating range, thereby significantly improving the output performance. The purpose is to provide a simple and convenient intake product for internal combustion engines.

本発明によれば、011記目的達成のため、シリンダヘ
ッドに形成される燃焼室に、その中心部を挾んで相対向
する2つの吸気ボートを開口し、それらの吸気ボートに
、互いに逆向きのプライマリ吸気通路と、セカンダリ吸
気通路をそれぞれ接続し、前1:1シブライマリ吸気d
路は、前記シリンダヘッドを迂回させてその管長を長く
形成したことを特徴としている。
According to the present invention, in order to achieve the object No. 011, two intake boats facing each other are opened in the combustion chamber formed in the cylinder head, and two intake boats are opened in opposite directions with the center of the combustion chamber in between. Connect the primary intake passage and the secondary intake passage respectively, and connect the front 1:1 primary intake d
The pipe is characterized by having a long pipe length by detouring the cylinder head.

以1・、r)”、’ 4〜3図により本発明をV型内燃
機関に実施した場合の第1実施例について説明する。
Hereinafter, a first embodiment in which the present invention is applied to a V-type internal combustion engine will be described with reference to FIGS. 4 to 3.

第1図において、V型に配置される左、右側エンジンブ
ロックI) l 、 Brは、何れも同一の構造を備え
ているが、左側エンジンブロックB tば、一対の吸気
弁1..12の軸線に沿い、また右側エンジンブロック
/J rは、排気弁2と点火プラグ3の軸線に沿ってそ
れぞれ縦断して示される。左。
In FIG. 1, the left and right engine blocks I) and Br, which are arranged in a V-shape, have the same structure, but the left engine block Bt has a pair of intake valves 1. .. 12, and the right engine block /Jr is shown longitudinally along the axes of the exhaust valve 2 and spark plug 3, respectively. left.

右側エンジンブロックBl 、 B rは何れも7リン
ダブロツク4にガスケット6を介してシリンダヘッド5
を重合結着して構成される。各シリンダブロック4のシ
リンダ8内には、ピストン7が摺動自在に嵌合され、各
7リンタ゛ヘツ)5には、ピストン7の頂面と対向して
燃焼室9が形成される。
Both the right engine blocks Bl and Br are connected to the cylinder head 5 via a gasket 6 to the 7 cylinder block 4.
It is composed by polymerizing and bonding. A piston 7 is slidably fitted into the cylinder 8 of each cylinder block 4, and a combustion chamber 9 is formed in each cylinder block 5 so as to face the top surface of the piston 7.

燃焼室9の外周縁には、環状の案内壁10が垂設これ5
この案内壁10はシリンダ8の」−線内周に形成した環
状溝11に嵌入されて、ピストン7の−1−1死点位1
6での上縁外周を案内する。各燃焼室9には、第2図に
示すように、該室9の中心部を挾んでシリンダヘッド5
に形成した2つの吸気ボー1−12..122の内端が
開口され、一方の吸気ボー1・12.の外端は、シリン
ダヘッド5の外側面に開口され、他方の吸気ボート12
2の外端はシリンダヘッド5の内11111面に開口さ
れる。2つの吸気ボー 1・12..122は、シリン
ダヘッド5に」二1;に摺動自在に支J’4sされる2
つの吸気弁1..12によってそれぞれ開閉され、それ
らの吸気弁1,112は、シリンダヘッド5」二のカム
室14に設けられる従来公知の吸気側動弁機構15Vc
よって所定のタイミングを以て開閉作動される。また第
2図に示すように燃焼室9には、前記2つのボー1・1
2、.122間において、シリンダヘッド5に形成され
る1つの471気ボート16の内端が開口され。
An annular guide wall 10 is vertically disposed on the outer peripheral edge of the combustion chamber 9.
This guide wall 10 is fitted into an annular groove 11 formed on the inner periphery of the cylinder 8 in the -1-1 dead center position of the piston 7.
Guide the outer circumference of the upper edge at step 6. In each combustion chamber 9, as shown in FIG.
Two intake bows 1-12. .. 122 is opened, and one of the intake bows 1, 12. The outer end of the cylinder head 5 is opened at the outer surface of the cylinder head 5 and the other intake boat 12
The outer end of 2 is opened to the inner 11111 surface of the cylinder head 5. Two intake bows 1.12. .. 122 is slidably supported on the cylinder head 5.
Two intake valves1. .. 12, and these intake valves 1 and 112 are operated by a conventionally known intake side valve operating mechanism 15Vc provided in the cam chamber 14 of the cylinder head 5''.
Therefore, the opening and closing operations are performed at predetermined timing. Furthermore, as shown in FIG. 2, the combustion chamber 9 includes the two bows 1 and 1.
2. Between 122 and 122, the inner end of one 471 air boat 16 formed in the cylinder head 5 is opened.

この4ノ1気ボー 1−16の外端はシリンダヘッド5
の外側面に開]ヨされる。Jul気ボート16はシリン
ダヘッド5に摺動自在に支持される排気弁2によって開
閉され、該4Vl’気弁2も、シリンダヘッド5上のカ
ム室14に設けられる従来公知の排気側動弁機構18に
よって所定のタイミングを以て開閉作動される。
The outer end of this 4-1 air cylinder 1-16 is the cylinder head 5.
opened on the outside surface of the body. The Jul air boat 16 is opened and closed by an exhaust valve 2 slidably supported by the cylinder head 5, and the 4Vl' air valve 2 is also a conventionally known exhaust side valve operating mechanism provided in the cam chamber 14 on the cylinder head 5. 18, it is opened and closed at predetermined timing.

また燃焼室9の中央部には、点火プラグ3が螺着される
Further, a spark plug 3 is screwed into the center of the combustion chamber 9.

左、右側エンジンブロックI) l 、 IJ r c
)各一方の吸気ボート121の外端には、プライマリ吸
気通路20が連通接続され、プライマリ吸気通路20ば
、シリンダヘッド5の上方を迂回して断面C字状に彎曲
形成され、両エンジンブロックBl 、 IJ r間の
V字状空間Sの中央部までのびていて、その管長が長く
形成される。また左、右側エンジンブロックBl 、B
rの各他方の吸気ボー1−122には、セカンダリ吸気
通路21が連通接続され、各セカンダリ吸気通路21は
直接V字状空間Sの中央部までのびて炉(形成されてい
る。
Left and right engine blocks I) l, IJ r c
) A primary intake passage 20 is connected to the outer end of each intake boat 121, and the primary intake passage 20 bypasses above the cylinder head 5 and is curved to have a C-shaped cross section. , IJ r, and extends to the center of the V-shaped space S between them, forming a long tube. Also left and right engine blocks Bl, B
Secondary intake passages 21 are connected to the other intake bows 1-122 of r, and each secondary intake passage 21 extends directly to the center of the V-shaped space S (formed in a furnace).

左、右の、プライマリ吸気通路20.20およびセカン
ダリ吸気通路21.21は、V字状空間Sの中央部にお
いて集合されて吸気分配室22に連通され、この吸気分
配室22は吸気主通路23に連通され、該主通路23は
図示しないエアクリ−すを介して大気に連通される。前
記吸気分配室22の人[」には、絞り弁24が開閉自在
に設けられ5吸気主通路23より吸気分配室22内に流
入した吸気は前記絞り弁24を通過したのち、左。
The left and right primary intake passages 20.20 and secondary intake passages 21.21 are gathered at the center of the V-shaped space S and communicated with an intake distribution chamber 22, and this intake distribution chamber 22 is connected to the main intake passage 23. The main passage 23 is communicated with the atmosphere via an air cleaner (not shown). A throttle valve 24 is provided in the air intake distribution chamber 22 so as to be openable and closable, and the intake air flowing into the air intake distribution chamber 22 from the main air intake passage 23 passes through the throttle valve 24 and then is directed to the left.

右のプライマリおよびセカンダリ吸気通路20゜20.
21.21に分流される。
Right primary and secondary intake passages 20°20.
21.21 will be diverted.

プライマリ吸気通路20とセカンダリ吸気通路21の、
各集合部25には燃t1噴射弁26が設けられる。
of the primary intake passage 20 and the secondary intake passage 21,
Each gathering portion 25 is provided with a fuel t1 injection valve 26 .

前記排気ボート16の外端には、排気通路27が連通さ
れ、この排気通路21は、排気マフラAfを介して大気
に連通される。
An exhaust passage 27 is communicated with the outer end of the exhaust boat 16, and this exhaust passage 21 is communicated with the atmosphere via an exhaust muffler Af.

前記吸気主通路23と排気通路27には、それらに跨っ
て従来公知のターボチャージャ1゛が設けられる。すな
わら前記排気通路27の途中には、排気エネルギによっ
て回転駆動される抽気タービン28が介装され、また前
記吸気主通路23の途中には、前記排気タービン28に
よって駆動されるコノプレツザ29が介装される。
A conventionally known turbocharger 1' is provided across the main intake passage 23 and the exhaust passage 27. That is, a bleed air turbine 28 that is rotationally driven by exhaust energy is interposed in the exhaust passage 27, and a conoprezer 29 that is driven by the exhaust turbine 28 is interposed in the air intake main passage 23. equipped.

次に本発明の第1実施例の作用につし・て説明する。Next, the operation of the first embodiment of the present invention will be explained.

いま機関の運転により、吸気主通路23に導入された吸
気は、吸気分配室22内において絞り弁24によりその
流量が制御され、燃料噴射弁26からの噴射燃料と混合
し、混合気となって左、右のプライマリおよびセカンダ
リ吸気通路20,20゜21.21に分流される。プラ
イマリ吸気通路20内を流れる吸気は、長い道程を通っ
て一方の吸気ボート121より燃焼室9内に導入され、
またセカンダリ吸気路21を流れる吸気は旬い道程を通
つて他方の吸気ボート122より燃焼室9内に導入され
る。而してプライマリ吸気通路20とセカンダリ吸気通
路21を流れる吸気は互いに反対方向より燃焼室9へ向
い、しかも2つの吸気ボート12、.122の燃焼室9
側開一端は、該燃焼室9の中心部を挾んで相対向される
ので、2つの吸気ボー 1−12. 、122より燃焼
室9内に入った吸気は、第2図矢部a 、 bに示すよ
うに燃焼室90周I:、(に沿−〕て流れ、燃焼室9内
に強力なスワールを生起さljる。
When the engine is currently operating, the intake air introduced into the main intake passage 23 has its flow rate controlled by the throttle valve 24 in the intake air distribution chamber 22, mixes with the fuel injected from the fuel injection valve 26, and becomes an air-fuel mixture. The air is divided into left and right primary and secondary intake passages 20, 20° 21.21. The intake air flowing through the primary intake passage 20 is introduced into the combustion chamber 9 from one intake boat 121 through a long path.
In addition, the intake air flowing through the secondary intake passage 21 is introduced into the combustion chamber 9 from the other intake boat 122 through a short path. Thus, the intake air flowing through the primary intake passage 20 and the secondary intake passage 21 is directed toward the combustion chamber 9 from opposite directions, and the two intake boats 12, . 122 combustion chambers 9
The side open ends are opposed to each other across the center of the combustion chamber 9, so that the two intake bows 1-12. , 122 into the combustion chamber 9 flows along the 90th circumference of the combustion chamber I:, as shown by arrows a and b in FIG. ljru.

とこ7)で機関の低負荷運転域では、長い管長をイJ4
るプライマリ吸気通路20が良9イな吸気慣性効果を発
揮1−2で究明効率が高められ、また比較的流:1:、
の少/[い混合気はl’+i+述のように2つの吸気ボ
ー l□ 121 + 122 ヲ、1lT1ツー(燃
焼”4i9内に強力なスIハルを発生させ点火ジンク3
の火花点火による混合気の燃焼を良9rに(2゛(その
燃焼性が改善される。また機関が高負荷運転域に移行す
れば、プライマリおよびセカンダリ吸気通路20.21
からの流量の多い導入空気はターボチャージャ7゛によ
り過給されて勢(・よく燃焼室9内に流入し、その際前
述の混合気のスワール化と相俟って機関の充填効率およ
び燃焼効率が高められる。
In 7), in the low load operating range of the engine, the long pipe length is
The primary intake passage 20 exhibits a good intake inertia effect, and the investigation efficiency is increased in 1-2, and the flow rate is relatively high.
A small/[low air-fuel mixture is l' + i + two intake bows as described above.
The combustion of the air-fuel mixture by spark ignition is improved by 9r (2゛).In addition, when the engine moves to a high load operating range, the primary and secondary intake passages 20.21
The introduced air with a large flow rate is supercharged by the turbocharger 7 and flows into the combustion chamber 9, and at this time, together with the aforementioned swirling of the air-fuel mixture, the charging efficiency and combustion efficiency of the engine are improved. is enhanced.

第3A図に示すように左、右のプライマリ吸気通路20
,20およびセカンダリ吸気通路21゜21は、相互に
集合させずに互いに並列して別々に連通させてもよく、
この場合には、左、右の。
As shown in FIG. 3A, the left and right primary intake passages 20
, 20 and the secondary intake passages 21 and 21 may be arranged in parallel with each other and communicated with each other separately, without being assembled together.
In this case, left, right.

プライマリ吸気通路20.20およびセカンダリ吸気通
路21.21の各連通部30.31にそれぞれプライマ
リおよびセカンダリ絞り弁24σ。
Primary and secondary throttle valves 24σ are provided in each communication portion 30.31 of the primary intake passage 20.20 and the secondary intake passage 21.21, respectively.

24bが設けられ、それらの連通部30°、31は吸気
主通路23に連通される。而して前記プライマリおよび
セカンダリ絞り弁24et、24bは連動して開閉し、
あるいは別々に開閉制御するようにしでもよい。
24b are provided, and their communicating portions 30° and 31 communicate with the main intake passage 23. The primary and secondary throttle valves 24et and 24b are opened and closed in conjunction with each other,
Alternatively, opening and closing may be controlled separately.

第4へ6図には、本発明の第2実施例が示される。A second embodiment of the invention is shown in FIGS. 4-6.

この第2実施例では、各プライマリ吸気通路20および
セカンダリ吸気通路21間を、バイパス通路32を以て
連通さぜ、そのバイパス通路32よりも上流側の各セカ
ンダリ吸気通路21にシャツタブF33を設け5さらに
Ail記燃刺噴射弁26の代わりにプライマリ吸気通路
20に連なる吸気ボート121に燃粉1噴射弁26αを
設けたものであって、その他の構成は、前記第1実施例
と同じである。
In this second embodiment, each primary intake passage 20 and the secondary intake passage 21 are communicated with each other through a bypass passage 32, and a shirt tab F33 is provided in each secondary intake passage 21 on the upstream side of the bypass passage 32. A fuel powder 1 injection valve 26α is provided in an intake boat 121 connected to the primary intake passage 20 in place of the memorizing injection valve 26, and the other configurations are the same as in the first embodiment.

而してこの第2実施例では、機関の低負荷運転域にある
とき、ツヤツタ弁33は閉弁され、吸気は吸気分配室2
2よりプライマリ吸気通路20へと流れ、その一部はバ
イパス通路32を通ってツヤツタ弁33よりも下流側の
セカンダリ吸気通路21へと流れる。したがって吸気の
大部分はプライマリ吸気通路20を通って燃料噴射弁2
6(Zかもの噴射燃料とともに燃焼室9へ流入し、さら
に僅かな吸気がセカンダリ吸気通路21を通って燃焼室
9へと流入して該燃焼室9内に混合気の強力なスワール
を生起させることができ、しかもバイパス通路32から
セカンダリ吸気通路21を通って燃焼室9へ流入する吸
気により、プライマリ吸気通路20から燃焼室9へ流入
した混合気の、セカンダリ吸気通路21への逆流が阻止
される。また燃焼室9へ流入する吸気の大部分は、管長
の長いプライマリ吸気通路20を通るので、良好な吸気
慣性効果が得られ充填効率が高められる。
In this second embodiment, when the engine is in the low-load operating range, the gloss valve 33 is closed and the intake air flows through the intake air distribution chamber 2.
2 to the primary intake passage 20 , and a part of it flows through the bypass passage 32 to the secondary intake passage 21 downstream of the gloss valve 33 . Therefore, most of the intake air passes through the primary intake passage 20 to the fuel injection valve 2.
6 (Z) The fuel flows into the combustion chamber 9 together with the injected fuel, and a small amount of intake air flows into the combustion chamber 9 through the secondary intake passage 21, creating a strong swirl of the air-fuel mixture within the combustion chamber 9. Moreover, the intake air flowing from the bypass passage 32 into the combustion chamber 9 through the secondary intake passage 21 prevents the air-fuel mixture that has flowed into the combustion chamber 9 from the primary intake passage 20 from flowing back into the secondary intake passage 21. Furthermore, since most of the intake air flowing into the combustion chamber 9 passes through the primary intake passage 20, which has a long pipe length, a good intake inertia effect is obtained and charging efficiency is increased.

機関が低負荷から高負荷運転域に移行すれば、シャツタ
弁33が開弁してセカンダリ吸気通路21にも吸気が流
入して燃焼室9への吸気量が増量される。この場合前述
のように低負荷運転域において既にバイパス通路32か
らセカンダリ吸気通路21には、吸気の流れがあるので
低負荷から高負荷デ1!転域への吸気の増鼠切換が円f
it K行われる。
When the engine shifts from a low load to a high load operating range, the shatter valve 33 opens and intake air also flows into the secondary intake passage 21, increasing the amount of intake air into the combustion chamber 9. In this case, as mentioned above, there is already a flow of intake air from the bypass passage 32 to the secondary intake passage 21 in the low-load operating range, so the transition from low load to high load 1! The increase in intake air to the conversion area is circle f.
It K is done.

第2実施例の場合も左、右のプライマリ吸気通路20.
20とセカンダリ吸気通路21とを集合させることなく
各独立して並列させ、それらの連通1ll(にそれぞれ
プライマリセカンダリ絞り弁を設けるようにしてもよい
In the case of the second embodiment, the left and right primary intake passages 20.
20 and the secondary intake passage 21 may be arranged independently in parallel without being assembled, and a primary and secondary throttle valve may be provided in each of the communication lines 111.

以1・のJ、うに本発明によれば、燃焼室に、その中心
部を挾んで相対向する、2つの吸気ボー1・を1j旧」
し、それらの吸気ボー 1・に、互いに逆向ぎのプライ
マリ吸気通路とセカンダリ吸気通路をそれぞれ連j1.
11接続し、1)ij記プンイマリ吸気通路は、前記/
リンダヘッドを迂回させてその管長を長く形成したので
5ブソイ々IJ :ttiよびセカンタ゛り吸気通路を
通って燃焼室に流入した吸気は、七〇周壁に白って周方
向にか0して強力なスワールを形成することができると
ともにプライマリ吸気通路が高い吸気慣性効果を発揮し
て、特に機関の低負荷運転域における燃焼効率と充填効
率が高められ、全体として機関の出ノ月q:能を著しく
向上させることができる。
According to the present invention, there are two intake bows 1 in the combustion chamber that face each other across the center of the combustion chamber.
A primary intake passage and a secondary intake passage, which are opposite to each other, are connected to these intake bows 1 and 1, respectively.
11 connection, 1) the intake passage is connected to the above /
By bypassing the cylinder head and making the pipe length long, the intake air that flows into the combustion chamber through the 5-stroke IJ:tti and secondary intake passages is 70% white on the circumferential wall and 0. In addition to forming a strong swirl, the primary intake passage exhibits a high intake inertia effect, which improves combustion efficiency and charging efficiency, especially in the engine's low-load operating range, and improves engine performance as a whole. can be significantly improved.

尚、前記第1,2実施例のように機関にターボチャージ
ャを令j設すれば、’I? K機関の高負荷運転域にお
ける燃焼効率と充填効率が大幅に高められるので前記効
果が一層顕著となって高価で嵩の張るl) OII (
、’型動弁機構を採用しなくても機関の高出力化が達成
される。
Incidentally, if a turbocharger is installed in the engine as in the first and second embodiments, 'I? Since the combustion efficiency and charging efficiency in the high-load operating range of the K engine are greatly increased, the above effects become even more pronounced, which reduces the cost and bulk of the engine.
, high output of the engine can be achieved without adopting a 'type valve train.

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

第1〜4図は本発明の第1実施例を示すもので、第1図
は本発明を具備したV型内燃機関の要部縦断側面図、第
2図は、第1図11線に沿う部分、平面図、第3図は、
第1図111−用線に沿う部分断面図、第3A図は第1
実施例の一部の変型例で、第3図と同じ部分断面図、第
4〜6図は本発明の第2実施例を示すもので、第4図は
本発明を具備したV型内燃機関の要部縦断側面図、第5
図は、第4図V線に沿う部分平面図、第6図は、第4図
■−■線に沿う部分断面図である。 5・・・シリンダヘッド、9・・燃焼室、12. 、1
2□吸気ボート、20・・・プライマリ吸気通路、21
・・・セカンダリ吸気通路 特許出願人 本田技研工業株式会社 第3図 第2図 、5 第3A図 第5図 手続補正書(い、 昭和59イに4)427 L1 隻 特許庁長官殿 1、事件の表示 昭和59年 特 願第7752 号 2、発明の名称 内す然機関の吸気装置 3、補正をする者 事件との関係 特許出願人 名 称 (532)本田技研工業株式会社4、代 理 
人 〒105 1−1 所 束にζ都港区新橋四丁目4番5勺 第に/
ムラビル5補正命令の日刊 補正の内容 明細書第14貞第12行、 1−第1〜4図」 とあるを、 (−第1〜3図−」・・に訂正する。 以上
1 to 4 show a first embodiment of the present invention, FIG. 1 is a longitudinal sectional side view of the main part of a V-type internal combustion engine equipped with the present invention, and FIG. 2 is a view taken along the line 11 in FIG. 1. The part, plan view, and Figure 3 are as follows:
Figure 1 111 - Partial sectional view along service line, Figure 3A is
This is a partially modified example of the embodiment, the same partial sectional view as FIG. 3, and FIGS. 4 to 6 show a second embodiment of the present invention, and FIG. 4 shows a V-type internal combustion engine equipped with the present invention. Main part vertical side view, No. 5
The figure is a partial plan view taken along the line V in FIG. 4, and FIG. 6 is a partial sectional view taken along the line ■--■ in FIG. 4. 5... Cylinder head, 9... Combustion chamber, 12. ,1
2□Intake boat, 20...Primary intake passage, 21
...Secondary intake passage patent applicant Honda Motor Co., Ltd. Figure 3 Figure 2, 5 Figure 3A Figure 5 Procedural amendment (1984-4) 427 L1 Mr. Commissioner of the Japan Patent Office 1, Incident Indication of Patent Application No. 7752 of 1982 2, Intake device for Suzen engine within the name of the invention 3, Relationship with the case of the person making the amendment Name of patent applicant (532) Honda Motor Co., Ltd. 4, Agent
Person 〒105 1-1 Location 4-4-5 Shinbashi, Miyakominato-ku 2nd/
The statement “1-Figures 1 to 4” in the 14th line of the daily amendment statement of contents of the Murabiru 5 amendment order is corrected to (-Figures 1 to 3-”).

Claims (1)

【特許請求の範囲】[Claims] ノリングヘッドに形成される燃焼室に、その中心部を挾
んで相対向する、2つの吸気ボートを開1−Jシ、それ
らの吸気ボートに、互いに逆向きのプライマリ吸気通路
と、セカノグリ吸気通路をそれぞれ連通接続し、前記プ
ライマリ吸気通路は、前lit、 7 ’)ンダヘソド
を迂回させてその貿長を長く形成17たことをq!i徴
とする内燃機関の吸気装置。
In the combustion chamber formed in the noling head, open two intake boats that face each other across the center of the combustion chamber, and connect the primary intake passage and the secondary intake passage facing oppositely to each other to the intake boats. The primary intake passage is connected to each other, and the primary intake passage bypasses the front, 7', and 7' ends to form a longer length. An intake system for an internal combustion engine with characteristics i.
JP59007752A 1984-01-19 1984-01-19 Suction device for internal-combustion engine Pending JPS60150471A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59007752A JPS60150471A (en) 1984-01-19 1984-01-19 Suction device for internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59007752A JPS60150471A (en) 1984-01-19 1984-01-19 Suction device for internal-combustion engine

Publications (1)

Publication Number Publication Date
JPS60150471A true JPS60150471A (en) 1985-08-08

Family

ID=11674423

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59007752A Pending JPS60150471A (en) 1984-01-19 1984-01-19 Suction device for internal-combustion engine

Country Status (1)

Country Link
JP (1) JPS60150471A (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4727078U (en) * 1971-04-07 1972-11-27

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4727078U (en) * 1971-04-07 1972-11-27

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