JPS62101824A - Intake passage for engine - Google Patents

Intake passage for engine

Info

Publication number
JPS62101824A
JPS62101824A JP60243176A JP24317685A JPS62101824A JP S62101824 A JPS62101824 A JP S62101824A JP 60243176 A JP60243176 A JP 60243176A JP 24317685 A JP24317685 A JP 24317685A JP S62101824 A JPS62101824 A JP S62101824A
Authority
JP
Japan
Prior art keywords
intake
passages
intake passage
cylindrical body
passage
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
JP60243176A
Other languages
Japanese (ja)
Other versions
JPH0665848B2 (en
Inventor
Mitsuo Hitomi
光夫 人見
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 JP60243176A priority Critical patent/JPH0665848B2/en
Publication of JPS62101824A publication Critical patent/JPS62101824A/en
Publication of JPH0665848B2 publication Critical patent/JPH0665848B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02B27/0226Use 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
    • F02B27/0247Plenum chambers; Resonance chambers or resonance pipes
    • F02B27/0263Plenum chambers; Resonance chambers or resonance pipes the plenum chamber and at least one of the intake ducts having a common wall, and the intake ducts wrap partially around the plenum chamber, i.e. snail-type
    • 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
    • F02B27/0221Resonance charging combined with oscillating pipe 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
    • F02B27/0268Valves
    • F02B27/0284Rotary slide valves
    • 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
    • F02B27/0294Actuators or controllers therefor; Diagnosis; Calibration
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

PURPOSE:To obtain a favorable inertial effect of intake air over wide operating areas by forming the middle part of each of independent intake passages leading from each of cylinders to a common intake passage, into a cylinder arc shaped curved part, rotatably inserting a cylindrical body through each of said curved parts which are on one axis, and making the length of a pressure wave transmitting passage variable. CONSTITUTION:An intake manifold 2 installed on the side wall 1S of the cylinder head 1 of an engine E, consists of independent intake passages 5 which are connected to the intake ports 4 of cylinders 3 and a common intake passage 6 which is connected to the upper courses of these passages 5... to distribute intake air. The upper course side of each of the independent intake passages 5... is formed into a circular arc shaped curved part 7 having a relatively large curvature radius, and a rotary body 8 having a relatively small diameter is rotatably provided in the center part of the carved part 7 of each of the passages 5..., so as to pass through the whole curved parts 7.... This rotary body 8 has openings 10 which are connected to each of the passages 5... and is rotated driven by a motor 13 controlled by a control circuit 15, according to the output of a rotation number sensor 16.

Description

【発明の詳細な説明】 [産業上の利用分野] 本発明は、エンジンの吸気通路の構造、とりわけ、各気
筒に至る独立吸気通路の圧力波伝播長さを変化させるこ
とかできるエンジンの吸気通路構造に関するものである
Detailed Description of the Invention [Industrial Application Field] The present invention relates to an engine intake passageway structure, in particular an engine intake passageway that can change the pressure wave propagation length of an independent intake passageway leading to each cylinder. It's about structure.

一般に、吸気の際に発生する負圧波を容積部で正圧波に
反転させ、この正圧波により、充填効率の向上を図るよ
うにした、いわゆる吸気慣性効果を利用して、エンジン
の出力向上を図るようにしたエンジンの吸気通路構造は
よく知られている。
In general, the negative pressure wave that occurs during intake is reversed into a positive pressure wave in the volume part, and this positive pressure wave is used to improve the filling efficiency. This takes advantage of the so-called intake inertia effect, which aims to improve engine output. Such an engine intake passage structure is well known.

ところで、この種の吸気慣性効果を得るに必要な圧力波
伝播通路長さは、エンジン回転数によって変化すること
から、広い運転範囲にわたって吸気慣性効果を得るため
には、圧力波伝播通路長さをエンジン回転数に応じて変
化させてやる必要がある。
By the way, the length of the pressure wave propagation passage necessary to obtain this type of intake inertia effect varies depending on the engine speed, so in order to obtain the intake inertia effect over a wide operating range, the length of the pressure wave propagation passage must be increased. It is necessary to change it according to the engine speed.

このため、例えば、特開昭59−188027号公報に
は、サージタンクと各気筒の吸気通路との連通位置を変
化させる回転ドラムを設けたエンジンの吸気通路構造が
抛案されている。
For this reason, for example, Japanese Patent Laid-Open No. 59-188027 proposes an engine intake passage structure including a rotating drum that changes the communication position between the surge tank and the intake passage of each cylinder.

この回転ドラムは、サージタンクとして必要な容積を有
する必要があるため大容量のものが必要となり、また、
連通部で吸気流が急激に曲げられるため吸気抵抗が増大
するといった問題もあった。
This rotating drum needs to have the necessary volume as a surge tank, so it needs to have a large capacity.
There was also a problem in that the intake air flow was sharply bent at the communication portion, resulting in increased intake resistance.

「発明の目的] 本発明の目的は、圧力波伝播通路長さを可変とすること
ができ、容積的にはきわめてコンパクトで、しかも吸気
抵抗の増大をもたらすことのない構造を有するエンジン
の吸気通路を提供することである。
[Object of the Invention] An object of the present invention is to provide an engine intake passage which has a structure in which the length of the pressure wave propagation passage can be made variable, is extremely compact in terms of volume, and does not cause an increase in intake resistance. The goal is to provide the following.

[発明の構成] このため、本発明は、各気筒もしくは点火順序が連続し
ない気筒群の吸気通路集合部に至る独立吸気通路の途中
に円弧状の湾曲部を形成し、同一軸上の各湾曲部にわた
って円筒状の筒体を回転自在に貫挿し、かつ筒体には、
軸に平行な線上に位置する連通開口を各湾曲部ごとに設
けて、各独立吸気通路を筒体を介して連通させるととも
に、筒体の回転によって、独立吸気通路の圧力波伝播通
路長さを変化させるようにしたことを特徴とする。
[Structure of the Invention] For this reason, the present invention forms an arc-shaped curved portion in the middle of an independent intake passage leading to the intake passage gathering portion of each cylinder or a group of cylinders in which the firing order is not consecutive, and each curved portion on the same axis A cylindrical body is rotatably inserted through the cylinder, and the cylinder has a
A communication opening located on a line parallel to the axis is provided for each curved portion to communicate each independent intake passage through the cylinder, and the pressure wave propagation path length of the independent intake passage can be changed by rotating the cylinder. It is characterized by being made to change.

[発明の効果] 本発明によれば、吸気通路自体は湾曲部に沿って施れる
ため吸気抵抗−は増大することがなく、また、筒体は全
ての吸気通路を連通しているため、筒体それ自体の容積
を大きくとる必要がなく、湾曲部を貫通するようにその
中心部にコンパクトに組込むことができ、圧力波伝播通
路長さを可変とするコンパクトな吸気通路構造を実現す
ることができる。
[Effects of the Invention] According to the present invention, since the intake passage itself is formed along the curved part, the intake resistance does not increase, and since the cylindrical body communicates all the intake passages, the cylindrical body There is no need to increase the volume of the body itself, and it can be compactly incorporated into the center of the curved part so as to pass through it, making it possible to realize a compact intake passage structure with variable pressure wave propagation passage length. can.

[実施例コ 以下、本発明の実施例を添付の図面を参照して具体的に
説明する。
[Embodiments] Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings.

第1図および第2図に示すように、エンジンEのシリン
ダヘッドlの側壁Isに取付ける吸気マニホールド2は
、各気筒3の吸気ボート4に連通ずる独立吸気通路5と
、これら独立吸気通路5゜5、・・・の上流に連通して
、吸気を分配する共通吸気通路6とを備えている。
As shown in FIGS. 1 and 2, the intake manifold 2 attached to the side wall Is of the cylinder head 1 of the engine E has independent intake passages 5 communicating with the intake boats 4 of each cylinder 3, and these independent intake passages 5°. 5, . . . and a common intake passage 6 for distributing intake air.

第1図に明瞭に示すように、各独立吸気通路5の上流側
は、吸気が大きな吸気抵抗を伴うことなしに流下しうる
ような比較的大きな曲率半径を有する円弧状の湾曲部7
として形成し、この湾曲部7の上流端は、共通吸気通路
6に設けた連通口6aとなめらかに接続し、下流端は、
独立吸気通路5の直線部と接線方向になめらかに接続し
て、吸気の流れを極力スムーズなものとする。
As clearly shown in FIG. 1, the upstream side of each independent intake passage 5 has an arcuate curved portion 7 having a relatively large radius of curvature so that the intake air can flow down without encountering large intake resistance.
The upstream end of this curved portion 7 is smoothly connected to the communication port 6a provided in the common intake passage 6, and the downstream end is formed as follows.
The intake air flow is made as smooth as possible by smoothly connecting with the straight part of the independent intake passage 5 in the tangential direction.

そして、上記各独立吸気通路5の湾曲部7の中心部には
、全ての湾曲部7,7.・・・を貫通するように、比較
的小径の円筒体8を回転自在に軸受体9で軸承する。こ
の円筒体8の各湾曲部7に該当する位置には、同一位相
で連通開口IOを開設している。
At the center of the curved portion 7 of each independent intake passage 5, all the curved portions 7, 7. A relatively small-diameter cylindrical body 8 is rotatably supported by a bearing body 9 so as to penetrate through the cylindrical body 8. Communication openings IO are opened in the same phase at positions corresponding to each curved portion 7 of this cylindrical body 8.

この円筒体8は、それ自体のボリュームが小さくても、
全ての独立吸気通路5.5.・・・に夫々連通開口lO
を介して連通しているため、これらを合わせたボリュー
ムは十分大きなものとなり、圧力波を反転させることが
できる容積部を構成する。
Even if this cylindrical body 8 has a small volume,
All independent intake passages 5.5. . . . Each communication opening lO
Because they are in communication through the , their combined volume is sufficiently large and constitutes a volume that can invert pressure waves.

また、吸気自体は共通吸気通路6から独立吸気通路5に
流れるため、連通開口lOは実際の吸気の出入りには関
与せず、圧力の変動分だけを吸収して、圧力波の反射点
となる。
In addition, since the intake air itself flows from the common intake passage 6 to the independent intake passage 5, the communication opening 1O does not participate in the actual intake and exit of intake air, but absorbs only the pressure fluctuations and serves as a reflection point for pressure waves. .

上記円筒体8の一端は、軸として外方に延長して形成し
、軸部には被駆動ギヤ12を取付けている。この被駆動
ギヤ12には、モータ13の出力軸に取付けた駆動ギヤ
14を噛合わせて、円筒体8を軸廻りに回動させるよう
にしている。上記のモータ13は、制御回路15によっ
てその駆動を制御するようにし、制御回路15は回転数
センチ16から入力されるエンジン回転数に応じてモー
タ13に駆動パルスを送り、この駆動パルスを受けてモ
ータ13は円筒体8の回動位相、より具体的には連通開
口10の回動位置を設定する。
One end of the cylindrical body 8 is formed to extend outward as a shaft, and a driven gear 12 is attached to the shaft. A driving gear 14 attached to the output shaft of a motor 13 is meshed with the driven gear 12 to rotate the cylindrical body 8 around the axis. The drive of the motor 13 is controlled by a control circuit 15, and the control circuit 15 sends a drive pulse to the motor 13 according to the engine rotation speed input from the rotation speed centimeter 16, and receives this drive pulse. The motor 13 sets the rotational phase of the cylindrical body 8, more specifically, the rotational position of the communication opening 10.

この連通開口10を回動させることは、前述したように
円筒体8が圧力波を反転させるボリュームを有すること
から、圧力波伝播通路長さを変化させることを意味する
Rotating the communication opening 10 means changing the length of the pressure wave propagation path since the cylindrical body 8 has a volume that reverses pressure waves as described above.

なお、第2図において、17は共通吸気通路6に介設さ
れたスロットル弁である。
Note that in FIG. 2, reference numeral 17 is a throttle valve provided in the common intake passage 6.

第3図は、第1図、第2図に示した吸気通路構造の等価
モデルを示すものである。
FIG. 3 shows an equivalent model of the intake passage structure shown in FIGS. 1 and 2. FIG.

この等価モデルに示すように、円筒体8の連通開口10
の位置を変化させることは、この円筒体8に相当する容
積部20を各独立吸気通路5.5゜・・・に対し、その
長手方向(通路方向)に平行移動することを示し、これ
によって、吸気ボート4から上記容積部20に至る通路
長、つまり圧力波伝播長さを変化させることができるの
である。
As shown in this equivalent model, the communication opening 10 of the cylindrical body 8
Changing the position of indicates that the volume portion 20 corresponding to the cylindrical body 8 is moved in parallel in the longitudinal direction (passage direction) with respect to each independent intake passage 5.5°. , it is possible to change the passage length from the intake boat 4 to the volume section 20, that is, the pressure wave propagation length.

よく知られているように、吸気慣性効果を得るに必要な
圧力波伝播長さは、圧力波発生周期を規定するエンジン
回転数に依存し、定性的には、低速側では長く、高速側
で短くなる。
As is well known, the pressure wave propagation length required to obtain the intake inertia effect depends on the engine speed, which determines the pressure wave generation period. Qualitatively, it is longer at low speeds and longer at high speeds. Becomes shorter.

したがって、第3図に実線(イ)で示す容積部20の位
置が低速側に有効な圧力波伝播通路長さに相当するもの
とすると、エンジン回転数が、低速から高速に上昇され
たときは、点線(ロ)で示す位置の方向に容積部20を
移動させる、つまり実際には、第1図に矢印Aで示す反
時計廻りに円筒体8を回動させるようにすればよい。
Therefore, assuming that the position of the volume portion 20 shown by the solid line (A) in FIG. 3 corresponds to the effective pressure wave propagation path length on the low speed side, when the engine speed is increased from low speed to high speed, , the volume portion 20 may be moved in the direction of the position indicated by the dotted line (B), that is, the cylindrical body 8 may be actually rotated counterclockwise as indicated by the arrow A in FIG.

なお、この回動制御は、必ずしもエンジン回転数の連続
関数として行なう必要はなく、エンジンの回転数を゛3
段階に区切り、段階ごとに円筒体8の回動位置を切換え
るようにしてもよい。
Note that this rotation control does not necessarily have to be performed as a continuous function of the engine speed;
It may be divided into stages and the rotational position of the cylindrical body 8 may be changed for each stage.

第4図には、6気筒エンジンの場合の実施例を示す。FIG. 4 shows an embodiment for a six-cylinder engine.

図示の如く、点火順序の連続しない左右のバンクの各気
筒に至る左、右の吸気マニホールドML。
As shown in the figure, the left and right intake manifolds ML lead to the cylinders of the left and right banks where the ignition order is not continuous.

MRは、夫々の集合部ML1.Mrtlから上流側に伸
びる各吸気通路21.22と、さらに上流の共通吸気通
路23との間を円弧状の湾曲部24゜25で連結する。
MR has each collection part ML1. Each intake passage 21, 22 extending upstream from Mrtl and a common intake passage 23 located further upstream are connected by arc-shaped curved portions 24 and 25.

この湾曲部24.25の軸心部には、円筒体26を回転
自在に貫挿し、この円筒体26を軸廻りで回動させるこ
とにより、円筒体26に設けた連通開口27の位置を変
化させ、両方の吸気通路24.25の連通長さを可変と
する。
A cylindrical body 26 is rotatably inserted into the axial center of this curved portion 24.25, and by rotating this cylindrical body 26 around the axis, the position of the communication opening 27 provided in the cylindrical body 26 is changed. The length of communication between both intake passages 24 and 25 is made variable.

したがって、この場合にも、エンジンの回転数に応じて
連通長さを変化させることにより、広い運転範囲にわた
って有効な吸気慣性効果を得ることができ、高いエンジ
ン出力を保証することができる。
Therefore, in this case as well, by changing the communication length according to the engine speed, an effective intake inertia effect can be obtained over a wide operating range, and high engine output can be guaranteed.

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

第1図は本発明の実施例を示すエンジンの縦断面図、第
2図は同じく水平方向断面図、第3図は本発明の実施例
の原理的構成をモデル化して示す斜視説′明図、第4図
は6気筒エンジンについて本発明を適用した場合の全体
概略説明図である。 5.5.・・・・・・独立吸気通路、 6・・・共通吸
気通路、7・・・湾曲部、 8・・・円筒体、  10
・・・連通開口。 特 許 出 願 人   マツダ株式会社代 理 人 
弁理士 青白 葆 ほか2名第1図
Fig. 1 is a vertical sectional view of an engine showing an embodiment of the present invention, Fig. 2 is a horizontal sectional view thereof, and Fig. 3 is a perspective explanatory view modeling the basic configuration of an embodiment of the present invention. , FIG. 4 is an overall schematic explanatory diagram when the present invention is applied to a six-cylinder engine. 5.5. ...Independent intake passage, 6...Common intake passage, 7...Curved portion, 8...Cylindrical body, 10
...Communication opening. Patent applicant Mazda Motor Corporation agent
Patent attorneys Aohaku Ao and 2 others Figure 1

Claims (1)

【特許請求の範囲】[Claims] (1)各気筒もしくは点火順序が連続しない気筒群の吸
気通路集合部に至る独立吸気通路の途中に円弧状の湾曲
部を形成し、同一軸上の各湾曲部にわたって円筒状の筒
体を回転自在に貫挿し、かつ筒体には、軸に平行な線上
に位置する連通開口を各湾曲部ごとに設けて、各独立吸
気通路を筒体を介して連通させるとともに、筒体の回転
によって独立吸気通路の圧力波伝播通路長さを変化させ
るようにしたことを特徴とするエンジンの吸気通路。
(1) An arc-shaped curved part is formed in the middle of the independent intake passage leading to the intake passage gathering part of each cylinder or a group of cylinders in which the firing order is not consecutive, and the cylindrical body is rotated across each curved part on the same axis. The cylindrical body is provided with a communication opening located on a line parallel to the axis for each curved part so that each independent intake passage can be communicated through the cylindrical body, and can also be opened independently by rotation of the cylindrical body. An intake passage for an engine, characterized in that the length of a pressure wave propagation passage in the intake passage is varied.
JP60243176A 1985-10-29 1985-10-29 Engine intake passage Expired - Fee Related JPH0665848B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60243176A JPH0665848B2 (en) 1985-10-29 1985-10-29 Engine intake passage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60243176A JPH0665848B2 (en) 1985-10-29 1985-10-29 Engine intake passage

Publications (2)

Publication Number Publication Date
JPS62101824A true JPS62101824A (en) 1987-05-12
JPH0665848B2 JPH0665848B2 (en) 1994-08-24

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ID=17099947

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60243176A Expired - Fee Related JPH0665848B2 (en) 1985-10-29 1985-10-29 Engine intake passage

Country Status (1)

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JP (1) JPH0665848B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4110597A1 (en) * 1990-03-30 1991-10-02 Mazda Motor INLET SYSTEM FOR A MULTI-CYLINDER INTERNAL COMBUSTION ENGINE

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4110597A1 (en) * 1990-03-30 1991-10-02 Mazda Motor INLET SYSTEM FOR A MULTI-CYLINDER INTERNAL COMBUSTION ENGINE
DE4110597C2 (en) * 1990-03-30 2003-12-04 Mazda Motor Intake air intake system for a multi-cylinder internal combustion engine

Also Published As

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JPH0665848B2 (en) 1994-08-24

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