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JP2552284B2 - Engine intake system - Google Patents
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JP2552284B2 - Engine intake system - Google Patents

Engine intake system

Info

Publication number
JP2552284B2
JP2552284B2 JP62103951A JP10395187A JP2552284B2 JP 2552284 B2 JP2552284 B2 JP 2552284B2 JP 62103951 A JP62103951 A JP 62103951A JP 10395187 A JP10395187 A JP 10395187A JP 2552284 B2 JP2552284 B2 JP 2552284B2
Authority
JP
Japan
Prior art keywords
intake
cylinder
passage
pressure wave
intake air
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.)
Expired - Fee Related
Application number
JP62103951A
Other languages
Japanese (ja)
Other versions
JPS63268918A (en
Inventor
光夫 人見
昭則 山下
敏彦 服部
泰浩 楪
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 JP62103951A priority Critical patent/JP2552284B2/en
Publication of JPS63268918A publication Critical patent/JPS63268918A/en
Application granted granted Critical
Publication of JP2552284B2 publication Critical patent/JP2552284B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は動的効果によって吸気の充填効率を高めるよ
うにしたエンジンの吸気装置に関するものである。
Description: TECHNICAL FIELD The present invention relates to an intake system for an engine, which enhances intake charging efficiency by a dynamic effect.

(従来技術) 従来から、吸気の動的効果によって充填効率を高める
ようにしたエンジンの吸気装置は種々知られている。例
えば、特開昭59−565号公報に見られるように、V型エ
ンジンにおいて、ブランチ部に相当する湾曲した個々の
吸気通路と、この個々の吸気通路に連通した拡大室に相
当する空間とを有する吸気マニホールドを配置すること
により、慣性過給効果をもたせ、充填効率を高めるよう
にしたものがある。また、この公報に示されるもので
は、吸気系をV型エンジンの両バンク間にレイアウト
し、全体の小型化を図っている。
(Prior Art) Conventionally, various engine intake devices have been known in which the charging efficiency is enhanced by the dynamic effect of intake air. For example, as seen in JP-A-59-565, in a V-type engine, a curved individual intake passage corresponding to a branch portion and a space corresponding to an expansion chamber communicating with the individual intake passage are provided. Some of them have an intake manifold to have an inertia supercharging effect to improve the charging efficiency. In addition, in the one disclosed in this publication, the intake system is laid out between both banks of the V-type engine to reduce the overall size.

ところで、動的効果を利用するものとしては、上記慣
性効果の他に共鳴効果により充填効率を高める手法があ
り、例えば、特開昭61−241418号公報に見られるよう
に、多気筒エンジンにおいて、吸気通路に、吸気順序が
隣合わない2つの気筒群の吸気ポートにそれぞれ連通さ
れる2つのサージタンクを設けるとともに、この両サー
ジタンクを上流側及び下流側でそれぞれ連通した環状通
路を形成し、共鳴過給を行なわせるようにしたものがあ
る。
By the way, as a method of utilizing the dynamic effect, there is a method of increasing the charging efficiency by the resonance effect in addition to the inertia effect, for example, as seen in JP-A-61-241418, in a multi-cylinder engine, The intake passage is provided with two surge tanks that communicate with the intake ports of two cylinder groups whose intake orders are not adjacent to each other, and an annular passage that connects these surge tanks with each other on the upstream side and the downstream side is formed. Some have been designed to perform resonance supercharging.

(発明が解決しようとする課題) この種の吸気装置においては、できるだけ圧力液の減
衰を避けることによって動的効果を高めることが望まれ
るが、このような圧力波の減衰という点で課題が残され
ていた。すなわち、例えば上記の特開昭61−241418号公
報に示されるような装置では、2つの気筒群の吸気ポー
トにそれぞれ連通される2つの通路(サージタンク)が
上流側及び下流側でそれぞれ連通されるとともに、上流
側の連通部分が吸気の流通経路を兼ねているため、この
上流側の連通部分を含めた環状通路全体にわたり圧力波
を伝播させて動的効果をもたせようとする場合、吸気流
により圧力波が減衰されて動的効果に悪影響を及ぼす可
能性がある。
(Problems to be Solved by the Invention) In this type of intake device, it is desirable to enhance the dynamic effect by avoiding the attenuation of the pressure liquid as much as possible, but there is a problem in such attenuation of the pressure wave. It had been. That is, for example, in the device as disclosed in Japanese Patent Laid-Open No. 61-241418, two passages (surge tanks) that communicate with the intake ports of the two cylinder groups are communicated with each other on the upstream side and the downstream side, respectively. In addition, since the upstream side communication part also serves as the intake flow path, when trying to propagate the pressure wave over the entire annular passage including this upstream side communication part to give a dynamic effect, May dampen the pressure wave and adversely affect the dynamic effects.

本発明は上記の事情に鑑み、有効に吸気の動的効果を
発揮させることができ、とくに、強い圧力波が得られて
大きな動的効果をもたせることができるエンジンの吸気
装置を提供するものである。
In view of the above circumstances, the present invention provides an intake system for an engine, which can effectively exhibit the dynamic effect of intake air, and in particular, can obtain a large dynamic effect by obtaining a strong pressure wave. is there.

(課題を解決するための手段) 本発明の装置は、多気筒エンジンを吸気順序が連続し
ない気筒を同一グループとする第1,第2の2つの気筒グ
ループに分け、各気筒の吸気ポートに通じる吸気通路
に、第1気筒グループの各気筒へ吸気を供給する第1吸
気供給通路と、第2気筒グループの各気筒へ吸気を供給
する第2吸気供給通路と、この両吸気供給通路を両側に
おいてそれぞれ連通する両側連通部分とからなる環状通
路を設けたエンジンの吸気装置であって、各気筒へ吸気
を導入するための主吸気通路を、上記第1吸気供給通路
における第1気筒グループの両端気筒に対応する吸気ポ
ート接続部の間と第2吸気供給通路における第2気筒グ
ループの両端気筒に対応する吸気ポート接続部の間とに
それぞれ開口するように接続したものである。
(Means for Solving the Problem) According to the device of the present invention, a multi-cylinder engine is divided into two cylinder groups, a first cylinder and a second cylinder, in which cylinders whose intake order is not continuous are grouped, and the cylinders are connected to an intake port of each cylinder. A first intake supply passage for supplying intake air to each cylinder of the first cylinder group, a second intake supply passage for supplying intake air to each cylinder of the second cylinder group, and both intake supply passages on both sides of the intake passage. An intake system for an engine, which is provided with an annular passage formed by communicating both sides communicating with each other, wherein a main intake passage for introducing intake air into each cylinder is provided with cylinders at both ends of a first cylinder group in the first intake supply passage. Are connected so as to open between the intake port connecting portions corresponding to the above and the intake port connecting portions corresponding to both end cylinders of the second cylinder group in the second intake supply passage.

(作用) この構成によると、上記の各グループ毎に、吸気ポー
ト付近に吸気行程終期に正圧となる圧力波が生じ、この
圧力波が上記環状通路をほぼ一周して同一気筒グループ
の吸気ポートに作用することにより動的効果が得られ
る。そして、圧力波の伝播経路となる環状通路両側の連
通部分が、吸気の供給を行なう主吸気通路から独立して
形成され、主吸気通路からの吸気流が上記両連通部分を
通らずに上記両吸気供給通路中に導入されるため、吸気
流により圧力波が減衰されることが抑制される。
(Operation) According to this configuration, a pressure wave that becomes a positive pressure at the end of the intake stroke is generated in the vicinity of the intake port for each of the above groups, and the pressure wave makes a full circle around the annular passage and the intake ports of the same cylinder group. A dynamic effect is obtained by acting on. Then, the communicating portions on both sides of the annular passage, which are the propagation paths of the pressure wave, are formed independently of the main intake passage that supplies the intake air, and the intake flow from the main intake passage does not pass through both the communicating portions. Since it is introduced into the intake air supply passage, the pressure wave is suppressed from being attenuated by the intake air flow.

(実施例) 第1図は本発明の装置をV型6気筒エンジンに適用し
た場合の一実施例を示しており、V型エンジンの一方の
バンク1には、1番、2番、3番の3つの気筒3a,3b,3c
が設けられ、他方のバンク2には、4番、5番、6番の
3つの気筒3d,3e,3fが設けられている。各気筒の点火順
序(吸気順序)は、例えば、1番気筒3a→4番気筒3d→
2番気筒3b→5番気筒3e→3番気筒3c→6番気筒3fとさ
れて、一方のバンク1における各気筒3a〜3cが吸気順序
の連続しない第1気筒グループを構成し、他方のバンク
2における各気筒3d〜3fが吸気順序の連続しない第2気
筒グループを構成している。各気筒3a〜3fにはそれぞれ
吸気ポート4a〜4fおよび排気ポート5a〜5fが配設されて
おり、これら吸気ポート4a〜4fおよび排気ポート5a〜5f
は、図外の吸気弁および排気弁によってそれぞれ所定の
タイミングで開閉される。
(Embodiment) FIG. 1 shows an embodiment in which the apparatus of the present invention is applied to a V-type 6-cylinder engine. Three cylinders 3a, 3b, 3c
The other bank 2 is provided with three cylinders 3d, 3e, 3f of No. 4, No. 5, and No. 6. The ignition order (intake order) of each cylinder is, for example, the first cylinder 3a → the fourth cylinder 3d →
No. 2 cylinder 3b → No. 5 cylinder 3e → No. 3 cylinder 3c → No. 6 cylinder 3f, and each cylinder 3a to 3c in one bank 1 constitutes the first cylinder group in which the intake order is not continuous, and the other bank Each of the cylinders 3d to 3f in No. 2 constitutes a second cylinder group in which the intake order is not continuous. Intake ports 4a to 4f and exhaust ports 5a to 5f are provided in the cylinders 3a to 3f, respectively, and the intake ports 4a to 4f and the exhaust ports 5a to 5f are arranged.
Are opened and closed at predetermined timings by an intake valve and an exhaust valve (not shown).

上記各気筒の吸気ポート4a〜4fは、拡大室を有しない
共鳴用の環状通路6に接続されている。この環状通路6
は、第1気筒グループの各吸気ポート4a〜4cに短い枝管
7a〜7cを介して通じる第1吸気供給通路6aと、第2気筒
グループの各吸気ポート4d〜4fに短い枝管7d〜7fを介し
て通じる第2吸気供給通路6bとが、それぞれ両側に延び
て両端部で互いに連なることにより、環状に形成されて
いる。つまりこの環状通路6は、両側においてそれぞ
れ、第1気筒グループの各吸気ポート4a〜4cに通じる部
分と第2気筒グループの各吸気ポート4d〜4fに通じる部
分とを連通する連通部分6c,6dを有しており、両気筒グ
ループ間で圧力波が互いに弱め合うような干渉が生じな
いように、上記各連通部分6c,6dの長さは同一気筒グル
ープの隣接する気筒の吸気ポート間の長さよりも充分に
大きく形成されている。
The intake ports 4a to 4f of each cylinder are connected to a resonance annular passage 6 having no expansion chamber. This circular passage 6
Is a short branch pipe for each intake port 4a-4c of the first cylinder group.
A first intake air supply passage 6a communicating via 7a to 7c and a second intake air supply passage 6b communicating to each of the intake ports 4d to 4f of the second cylinder group via short branch pipes 7d to 7f extend on both sides. And both ends are connected to each other to form an annular shape. In other words, the annular passage 6 has, on both sides, communication portions 6c and 6d that communicate with the portions communicating with the intake ports 4a to 4c of the first cylinder group and the portions communicating with the intake ports 4d to 4f of the second cylinder group, respectively. The length of each of the communication portions 6c and 6d is longer than the length between the intake ports of the adjacent cylinders of the same cylinder group so that the pressure waves between the cylinder groups do not interfere with each other so as to weaken each other. Is also large enough.

また、8は吸気を供給するための主吸気通路で、この
主吸気通路8は、エアクリーナ9を介して吸気を導入す
る共通吸気通路8aと、この共通吸気通路8aから二又に分
岐した分岐吸気通路8b,8cとで構成されており、主吸気
通路8中には、吸気量を検出するエアフローメータ10お
よびアクセス操作に応じて吸気量を調整するスロットル
弁11が配設されている。
Reference numeral 8 denotes a main intake passage for supplying intake air. The main intake passage 8 includes a common intake passage 8a for introducing intake air through an air cleaner 9 and a branch intake air branched from the common intake passage 8a. The main intake passage 8 is provided with an air flow meter 10 for detecting the intake air amount and a throttle valve 11 for adjusting the intake air amount according to an access operation.

上記分岐吸気通路8b,8cの各下流端は、上記第1吸気
供給通路6aにおける第1気筒グループの両端気筒の吸気
ポート4a,4cの対する接続部の間と、第2吸気供給通路
における第2気筒グループの両端気筒の吸気ポート4d,4
fに対する接続部の間とに、それぞれ開口するように接
続されている。従って、環状通路6の両側連通部分6c,6
dは主吸気通路8から独立し、つまり、主吸気通路8か
ら送られる吸気が上記両連通部分6c,6dを通らずに各気
筒に供給されるように、環状通路6および主吸気通路8
が形成されている。なお、望ましくは、環状通路6の半
周分の通路長さL1と、主吸気通路8の両分岐吸気通路8
a,8bにわたっての通路長さL2とが、ほぼ等しくなるよう
に形成しておく。
The respective downstream ends of the branch intake passages 8b, 8c are provided between the connection portions of the intake ports 4a, 4c of the cylinders at both ends of the first cylinder group in the first intake supply passage 6a and the second intake supply passage 2a. Intake ports 4d, 4 on both ends of the cylinder group
It is connected so as to open between the connection parts for f. Therefore, the communicating portions 6c, 6 on both sides of the annular passage 6 are
d is independent of the main intake passage 8, that is, so that the intake air sent from the main intake passage 8 is supplied to each cylinder without passing through both the communication portions 6c, 6d.
Are formed. Desirably, the passage length L 1 corresponding to a half circumference of the annular passage 6 and the bifurcated intake passages 8 of the main intake passage 8 are provided.
The passage length L 2 across a and 8b is formed to be substantially equal.

この実施例の装置による場合の作用を、第2図を参照
して説明する。
The operation of the apparatus of this embodiment will be described with reference to FIG.

吸気順序が連続しない同一気筒グループの各吸気ポー
ト付近、例えば第1気筒グループの各吸気ポート4a〜4c
付近には、第1気筒グループの各気筒の作動によりそれ
ぞれの吸気行程途中で負圧となって吸気行程終期に正圧
となる基本的圧力振動(第2図の線A)が生じる。この
吸気ポート付近に生じた圧力波は、両側に分かれてそれ
ぞれ環状通路6を周回するように伝播し、環状通路6を
ほぼ一周して同一気筒グループの他の気筒の吸気ポート
に作用する。この場合、環状通路6は拡大室を有しない
ので、圧力波は反転することなく伝播される。
Near each intake port of the same cylinder group in which the intake order is not continuous, for example, each intake port 4a to 4c of the first cylinder group
In the vicinity, a basic pressure oscillation (line A in FIG. 2) is generated by the operation of each cylinder of the first cylinder group, which becomes a negative pressure in the middle of each intake stroke and becomes a positive pressure at the end of the intake stroke. The pressure wave generated in the vicinity of the intake port propagates so as to be divided into both sides and circulate around the annular passage 6, respectively, and makes a round of the annular passage 6 to act on the intake ports of other cylinders in the same cylinder group. In this case, since the annular passage 6 has no expansion chamber, the pressure wave propagates without inversion.

そして、圧力波が環状通路6をほぼ一周する時間と上
記の基本的圧力振動の周期τとが一致する状態となった
とき、すなわち環状通路6全体の長さL(枝管の容積な
ども考慮した等価管長)と上記周期τとの関係が τ=L/a …… a:音速 となったときは、第2図に矢印で示すように1番気筒3a
に生じて環状通路6を伝播した圧力波が2番気筒3bに生
じた圧力波と重なり、同様にして2番気筒3bから伝播し
た圧力波が3番気筒3cに生じる圧力波と重なり、3番気
筒3cから伝播した圧力波が1番気筒3aに生じる圧力波と
重なる。こうして、第1気筒グループの気筒相互間で圧
力波が共振して第2図に線Bで示すように圧力振動が強
められ、同様に第2気筒グループの気筒相互間でも共振
が生じて圧力振動が強められる。このような共鳴効果に
より、各気筒の充填効率が高められることとなる。
Then, when the time period during which the pressure wave travels around the annular passage 6 and the period τ of the above-mentioned basic pressure oscillation match, that is, the entire length L of the annular passage 6 (the volume of the branch pipe, etc. is also taken into consideration). When the relation between the equivalent pipe length) and the period τ becomes τ = L / a ...... a: speed of sound, as shown by the arrow in Fig. 2, the first cylinder 3a
Pressure wave that has propagated through the annular passage 6 and that overlaps with the pressure wave that has occurred in the second cylinder 3b, and the pressure wave that has similarly propagated from the second cylinder 3b has overlapped with the pressure wave that has occurred in the third cylinder 3c. The pressure wave propagating from the cylinder 3c overlaps with the pressure wave generated in the first cylinder 3a. In this way, the pressure waves resonate between the cylinders of the first cylinder group, and the pressure vibration is intensified as indicated by the line B in FIG. Is strengthened. Due to such a resonance effect, the charging efficiency of each cylinder is improved.

なお、第2図では、同一気筒グループにおいて生じる
圧力振動の1つの圧力波が次の圧力波に重なるように伝
播する基本的共振状態を示したが、圧力波が1つおきや
2つおきの圧力波に重なるように伝播するときにも共振
状態が得られ、従って、上記の基本的共振状態が得られ
るエンジン回転数の整数倍のエンジン回転数でも共振状
態が得られる。ただし、2つの気筒グループに分けると
各グループがほぼ逆位相の圧力波を発生するので、上記
一次の共振が得られる回転数の偶数倍のところでは両グ
ループの圧力波が互いに打消し合う作用をする。よっ
て、効果的なのは、上記一次の共振が得られる回転数の
奇数倍の回転数である。
Although FIG. 2 shows a basic resonance state in which one pressure wave of pressure oscillation occurring in the same cylinder group propagates so as to overlap with the next pressure wave, every other pressure wave or every other pressure wave is shown. A resonance state is obtained even when propagating so as to overlap with the pressure wave, and therefore a resonance state is obtained even at an engine speed that is an integral multiple of the engine speed at which the above-described basic resonance state is obtained. However, when divided into two cylinder groups, each group generates a pressure wave of almost opposite phase, so that the pressure waves of both groups cancel each other at an even multiple of the rotational speed at which the above-mentioned first-order resonance is obtained. To do. Therefore, what is effective is a rotational speed that is an odd multiple of the rotational speed at which the above-mentioned primary resonance is obtained.

このように上記環状通路6を周回する圧力波によって
共鳴効果をもたせるようにすると、高速域での充填効率
の向上に有利となる。
When the pressure wave circulating in the annular passage 6 is made to have a resonance effect in this way, it is advantageous for improving the filling efficiency in the high speed region.

つまり、仮に上記環状通路6を用いずに、例えば第1
気筒グループの各吸気ポートに通じる吸気通路と第2気
筒グループの各吸気ポートに通じる吸気通路との集合部
を圧力反転部として、反転圧力波により動的効果をもた
せようとする場合には、上記基本圧力振動の周期の1/2
に相当する時間に吸気ポートと上記集合部との間の通路
を圧力波が往復伝播する状態となったときに、上記集合
部で負圧から正圧に反転して反射された圧力波が自気筒
の吸気行程終期に作用して動的効果が得られることとな
り、このときの圧力振動の周期τと上記通路の長さL′
(等価管長)との関係は τ/2=2L′/a …… となる。そして、上記圧力振動の周期τが短くなる高速
域でこの関係を満足させようとすると、上記通路長さを
かなり短く設定する必要があるが、各気筒の吸気ポート
から通路集合部までの通路長さには、気筒相互の吸気ポ
ート間長さ分の較差があり、集合部までの通路長さを短
くする程、相対的に上記較差が大きくなるので、各気筒
に作用する圧力波のアンバランスが大きくなって、全体
的な充填効果を高めることは困難となる。
That is, if the annular passage 6 is not used, for example, the first passage
When a reversal pressure wave is used to exert a dynamic effect by using a pressure reversal portion as a collective portion of an intake passage communicating with each intake port of the cylinder group and an intake passage communicating with each intake port of the second cylinder group, 1/2 of basic pressure oscillation cycle
When the pressure wave reciprocally propagates in the passage between the intake port and the collecting portion at a time corresponding to, the pressure wave reflected by reversing from negative pressure to positive pressure in the collecting portion is automatically generated. A dynamic effect is obtained by acting at the end of the intake stroke of the cylinder. At this time, the period τ of pressure oscillation and the length L'of the passage are obtained.
The relationship with (equivalent pipe length) is τ / 2 = 2L '/ a .... Then, in order to satisfy this relationship in the high speed region where the cycle τ of the pressure oscillation becomes short, it is necessary to set the passage length to be considerably short, but the passage length from the intake port of each cylinder to the passage collecting portion is In addition, there is a difference in the length of the intake ports between the cylinders, and the shorter the passage length to the collecting section, the larger the difference becomes. Becomes larger and it becomes difficult to increase the overall filling effect.

これに対し、前述のように拡大室を有しない環状通路
6を用いると、前記式が成立するときに共鳴効果が得
られ、この式と式とを比べると、圧力振動の周期τ
が同じであれば、環状通路6全体の等価管長Lは前記
式による場合の等価管長L′の4倍となり、高速域で
も、気筒毎の圧力波伝播経路の較差が相対的に小さいの
で、各気筒に作用する圧力波のアンバランスが小さくな
る。従って、高速域でも、各気筒にほぼ均等に圧力波を
作用させて、有効に各気筒の充填効率を高めることがで
きる。
On the other hand, when the annular passage 6 having no expansion chamber is used as described above, the resonance effect is obtained when the above equation is satisfied. When this equation is compared with the equation, the period τ of pressure oscillation is
Is the same, the equivalent pipe length L of the entire annular passage 6 is four times the equivalent pipe length L ′ in the case of the above expression, and the difference in the pressure wave propagation paths for each cylinder is relatively small even in the high speed region. The imbalance of the pressure wave acting on the cylinder is reduced. Therefore, even in the high speed range, the pressure wave can be applied to each cylinder almost uniformly, and the filling efficiency of each cylinder can be effectively increased.

また、とくにこの吸気装置によると、主吸気通路8を
通って導入される吸気は、主吸気通路8の分岐吸気通路
8b,8cから直接的に各吸気ポートに供給され、環状通路
6の両側連通部分6c,6dでは空気の流動自体が少ないの
で、環状通路6を伝播する圧力波が吸気流により減衰さ
れることが抑制される。その上、上記両側連通部分6c,6
dは、吸気導入量確保等のための制約をうけることな
く、通路径、容量、長さ等を圧力波の伝播に適するよう
に設定できるので、これによっても圧力波の強化が可能
となる。
Further, particularly according to this intake device, the intake air introduced through the main intake passage 8 is the branch intake passage of the main intake passage 8.
8b, 8c is directly supplied to each intake port, and the air flow itself is small in both side communicating portions 6c, 6d of the annular passage 6, so that the pressure wave propagating in the annular passage 6 may be attenuated by the intake flow. Suppressed. In addition, the above-mentioned communication parts 6c, 6 on both sides
Since the passage diameter, volume, length, etc. can be set to be suitable for the propagation of the pressure wave without any restriction for securing the intake air intake amount, etc., the pressure wave can also be strengthened by this.

なお、環状通路6を伝播する圧力波の一部は主吸気通
路8の上記分岐吸気通路8b,8cにも伝わり、この両分岐
吸気通路8b,8cと環状通路6とによっても圧力波の循環
経路が構成されるので、前述のように、環状通路6の略
半周の長さL1と上記両分岐吸気通路8b,8cにわたる長さL
2とをほぼ等しくしておけば、これらの間でも共振が生
じてより一層圧力波が強化されることとなる。
A part of the pressure wave propagating in the annular passage 6 is also transmitted to the branch intake passages 8b, 8c of the main intake passage 8, and the circulation path of the pressure wave is also formed by the branch intake passages 8b, 8c and the annular passage 6. Therefore, as described above, the length L 1 of the substantially half circumference of the annular passage 6 and the length L extending over both of the branch intake passages 8b and 8c are as described above.
If 2 and 2 are made almost equal, resonance will occur between them and the pressure wave will be further strengthened.

本発明装置の具体的構造は上記実施例に限定されず、
種々変更可能であり、その数例を第3図、第4図に示
す。
The specific structure of the device of the present invention is not limited to the above embodiment,
Various changes are possible, and some examples are shown in FIGS. 3 and 4.

第3図に示す実施例では、環状通路6の通路長さを可
変としている。すなわち、環状通路6における両気筒グ
ループ間の片側の連通部分6cに、その途中を短絡する短
絡連通部6eが設けられ、この短絡連通部6eとこれを迂回
する部分との分岐箇所に、短絡連通部6eを閉じて迂回部
分を開く状態と短絡連通部6eを開いて迂回部分を閉じる
状態とに切替える切替弁12が設けられている。この構造
によると、短絡連通部6eを閉じた状態では環状通路6が
比較的長く、短絡連通部6eを開いた状態では環状通路6
の実質的な長さが短くなる。従って、図外の制御手段に
より、エンジン回転数に応じて上記切替弁12の開閉作動
を切替えることにより、異なる回転数域でそれぞれ共鳴
効果を高めることができる。
In the embodiment shown in FIG. 3, the passage length of the annular passage 6 is variable. That is, a short-circuit communication part 6e for short-circuiting the middle of the one-way communication part 6c between the two cylinder groups in the annular passage 6 is provided, and the short-circuit communication part 6e and the part bypassing the short-circuit communication part 6e are connected. A switching valve 12 for switching between a state in which the portion 6e is closed and the bypass portion is opened and a state in which the short-circuit communication portion 6e is opened and the bypass portion is closed are provided. According to this structure, the annular passage 6 is relatively long when the short-circuit communicating portion 6e is closed, and the annular passage 6 is opened when the short-circuit communicating portion 6e is opened.
The actual length of Therefore, the resonance effect can be enhanced in different rotational speed regions by switching the opening / closing operation of the switching valve 12 according to the engine rotational speed by the control means (not shown).

第4図は本発明を直列6気筒エンジンに適用した場合
の実施例を示している。この場合も、吸気順序が連続し
ない1番〜3番気筒3a〜3cを第1気筒グループ、吸気順
序が連続しない4番〜6番気筒3d〜3fを第2気筒グルー
プとし、第1気筒グループの各吸気ポート4a〜4cに通じ
る第1吸気供給通路6aと第2グループの各吸気ポート4d
〜4fに通じる第2吸気供給通路6bとがそれぞれ両側に延
出されてそれぞれの延出部分が互いに連なることによ
り、両気筒グループ間の両側にそれぞれ適当な長さの連
通部分6c,6dを有する環状通路6が構成されている。そ
してこの場合も、主吸気通路8の両分岐吸気通路8b,8c
の下流端が第1,第2吸気供給通路6a,6bにおける両端気
筒の吸気ポートに対する接続部の間の箇所に接続される
ことにより、環状通路6の両側連通部分6c,6dが主吸気
通路8から独立して形成されている。
FIG. 4 shows an embodiment in which the present invention is applied to an in-line 6-cylinder engine. Also in this case, the first to third cylinders 3a to 3c whose intake order is not continuous are the first cylinder group, and the fourth to sixth cylinders 3d to 3f whose intake order are not continuous are the second cylinder group, and the first cylinder group First intake supply passage 6a leading to each intake port 4a-4c and each intake port 4d of the second group
The second intake air supply passages 6b leading to 4f extend to both sides, and the extending portions connect to each other, so that the communicating portions 6c and 6d having appropriate lengths are provided on both sides between the two cylinder groups. An annular passage 6 is formed. Also in this case, both the branch intake passages 8b, 8c of the main intake passage 8 are also
Is connected to the downstream end of the first and second intake supply passages 6a, 6b between the connection portions for the intake ports of the cylinders at both ends, so that the both-side communication portions 6c, 6d of the annular passage 6 are connected to the main intake passage 8 It is formed independently from.

(発明の効果) 以上のように本発明は、吸気順序が連続しない気筒を
同一グループとする2つの気筒グループにそれぞれ吸気
を供給する第1,第2吸気供給通路と両側連通部分とから
なる環状通路を備え、この環状通路を伝播する圧力波に
より動的効果が得られるようにしているので、各気筒の
充填効率を高めることができる。とくに、吸気の供給を
行なう主吸気通路を、上記第1吸気供給通路における両
端気筒に対応する吸気ポート接続部の間と第2吸気供給
通路における両端気筒に対応する吸気ポート接続部の間
とにそれぞれ接続することにより、環状通路の両側連通
部分を主吸気通路から独立させているので、環状通路を
通る圧力波が吸気流により減衰されることを抑制し、こ
れによって圧力波を強め、動的効果をより一層高めるこ
とができるものである。
(Effects of the Invention) As described above, according to the present invention, an annular structure including first and second intake supply passages for supplying intake air to two cylinder groups in which the cylinders whose intake orders are not continuous belong to the same group and both side communicating portions are connected to each other. Since the passage is provided and the dynamic effect is obtained by the pressure wave propagating through the annular passage, the filling efficiency of each cylinder can be increased. In particular, the main intake passage for supplying intake air is provided between the intake port connecting portions corresponding to both cylinders in the first intake supply passage and between the intake port connecting portions corresponding to both cylinders in the second intake supply passage. By connecting each of them, the communicating parts on both sides of the annular passage are made independent from the main intake passage, so that the pressure wave passing through the annular passage is suppressed from being attenuated by the intake flow, thereby strengthening the pressure wave and dynamically The effect can be further enhanced.

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

第1図は本発明の一実施例を示す吸気装置概略図、第2
図は吸気ポート付近の圧力振動を示す図、第3図および
第4図は各々別の実施例を示す吸気装置概略図である。 3a〜3c……第1気筒グループの各気筒、3d〜3f……第2
気筒グループの各気筒、4a〜4f……吸気ポート、6……
環状通路、6a,6b……吸気供給通路、6c,6d……環状通路
における両側連通部分、8……主吸気通路。
FIG. 1 is a schematic view of an intake device showing an embodiment of the present invention, and FIG.
FIG. 3 is a diagram showing pressure oscillation near the intake port, and FIGS. 3 and 4 are schematic diagrams of an intake device showing different embodiments. 3a to 3c: each cylinder of the first cylinder group, 3d to 3f: second
Each cylinder in the cylinder group, 4a to 4f ... intake port, 6 ...
Annular passages, 6a, 6b ... intake air supply passages, 6c, 6d ... communication parts on both sides of the annular passage, 8 ... main intake passages.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 楪 泰浩 広島県安芸郡府中町新地3番1号 マツ ダ株式会社内 (56)参考文献 特開 昭56−52522(JP,A) ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Yasuhiro Yuzuru 3-3 Shinchi, Fuchu-cho, Aki-gun, Hiroshima Prefecture Mazda Corporation (56) References JP-A-56-52522 (JP, A)

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】多気筒エンジンを吸気順序が連続しない気
筒を同一グループとする第1,第2の2つの気筒グループ
に分け、各気筒の吸気ポートに通じる吸気通路に、第1
気筒グループの各気筒へ吸気を供給する第1吸気供給通
路と、第2気筒グループの各気筒へ吸気を供給する第2
吸気供給通路と、この両吸気供給通路を両側においてそ
れぞれ連通する両側連通部分とからなる環状通路を設け
たエンジンの吸気装置であって、各気筒へ吸気を導入す
るための主吸気通路を、上記第1吸気供給通路における
第1気筒グループの両端気筒に対応する吸気ポート接続
部の間と第2吸気供給通路における第2気筒グループの
両端気筒に対応する吸気ポート接続部の間とにそれぞれ
開口するように接続したことを特徴とするエンジンの吸
気装置。
1. A multi-cylinder engine is divided into two cylinder groups, a first cylinder group and a second cylinder group, in which cylinders whose intake order is not continuous are the same group, and a first cylinder is provided in an intake passage leading to an intake port of each cylinder.
A first intake air supply passage for supplying intake air to each cylinder of the cylinder group, and a second intake air supply passage for supplying intake air to each cylinder of the second cylinder group
An intake device for an engine, which is provided with an annular passage formed of an intake air supply passage and both side communicating portions that communicate the intake air supply passage on both sides, wherein a main intake air passage for introducing intake air into each cylinder is Opening is made between the intake port connecting portions corresponding to both end cylinders of the first cylinder group in the first intake supply passage and between the intake port connecting portions corresponding to both end cylinders of the second cylinder group in the second intake supply passage. The intake system for the engine is characterized in that it is connected in this way.
JP62103951A 1987-04-27 1987-04-27 Engine intake system Expired - Fee Related JP2552284B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62103951A JP2552284B2 (en) 1987-04-27 1987-04-27 Engine intake system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62103951A JP2552284B2 (en) 1987-04-27 1987-04-27 Engine intake system

Publications (2)

Publication Number Publication Date
JPS63268918A JPS63268918A (en) 1988-11-07
JP2552284B2 true JP2552284B2 (en) 1996-11-06

Family

ID=14367724

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62103951A Expired - Fee Related JP2552284B2 (en) 1987-04-27 1987-04-27 Engine intake system

Country Status (1)

Country Link
JP (1) JP2552284B2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5652522A (en) * 1979-10-06 1981-05-11 Nissan Diesel Motor Co Ltd Air suction device for internal combustion engine

Also Published As

Publication number Publication date
JPS63268918A (en) 1988-11-07

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