JPH0819851B2 - Multi-cylinder engine intake system - Google Patents
Multi-cylinder engine intake systemInfo
- Publication number
- JPH0819851B2 JPH0819851B2 JP10277487A JP10277487A JPH0819851B2 JP H0819851 B2 JPH0819851 B2 JP H0819851B2 JP 10277487 A JP10277487 A JP 10277487A JP 10277487 A JP10277487 A JP 10277487A JP H0819851 B2 JPH0819851 B2 JP H0819851B2
- Authority
- JP
- Japan
- Prior art keywords
- surge tank
- intake
- valve
- pressure wave
- valves
- 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
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- Characterised By The Charging Evacuation (AREA)
Description
【発明の詳細な説明】 [産業上の利用分野] 本発明は吸気通路にサージタンクを介設した多気筒エ
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 device for a multi-cylinder engine in which a surge tank is provided in an intake passage.
[従来技術] 多気筒エンジンにおいて、吸気系の慣性効果あるいは
共鳴効果を利用して圧力波過給を行ない充填効率を向上
させたものはよく知られている。[Prior Art] It is well known that in a multi-cylinder engine, pressure wave supercharging is performed by utilizing the inertial effect or resonance effect of the intake system to improve the charging efficiency.
ここにおいて、慣性効果による圧力波過給とは、各気
筒の独立吸気通路の上流部に容積部を設け、各気筒の吸
気弁開弁時に吸気ポートに発生する負の圧力波を吸気ポ
ートと容積部との間の独立吸気通路内を往復伝播させ、
その際容積部で負の圧力波が正の圧力波に反転する現象
を利用して、この正の圧力波によって吸気を燃焼室に押
し込めるものであって、この効果は、独立吸気通路の管
長による制約上比較的高回転時に高くなるという特性を
有する。Here, the pressure wave supercharging due to the inertia effect means that a volume portion is provided in the upstream portion of the independent intake passage of each cylinder, and the negative pressure wave generated in the intake port when the intake valve of each cylinder is opened causes Reciprocating in the independent intake passage between the
At this time, the phenomenon in which the negative pressure wave is inverted into the positive pressure wave in the volume portion is used to push the intake air into the combustion chamber by this positive pressure wave, and this effect depends on the pipe length of the independent intake passage. Due to restrictions, it has the characteristic of becoming higher at relatively high rotation speeds.
一方、共鳴効果による圧力波過給とは、点火時期が連
続しない気筒で構成される気筒群を形成し、これに属す
る各気筒の独立吸気通路を上流部で1つの共通吸気通路
に集合させて、この共通吸気通路の所定の位置に容積部
を設け、各気筒と容積部との間を往復伝播する各気筒毎
の圧力波を共鳴させ、これによって各単独気筒毎に発生
する圧力振動より大きな振幅を有し、かつ、容積部と吸
気通路の寸法によって決定される固有振動数を有する定
常圧力波を発生させ、これによってより大きな過給効果
が得られるようにしたものであり、この場合圧力波の伝
播経路長さは前記の慣性効果の場合より長くなる関係
上、比較的低回転域においてその効果を発揮するという
特性を有する。On the other hand, the pressure wave supercharging due to the resonance effect means that a cylinder group composed of cylinders whose ignition timings are not continuous is formed, and the independent intake passages of the cylinders belonging to this cylinder are gathered in one common intake passage in the upstream portion. , A volume portion is provided at a predetermined position of this common intake passage, and a pressure wave of each cylinder that propagates back and forth between each cylinder and the volume portion is resonated, and is larger than the pressure vibration generated in each individual cylinder. A steady pressure wave having an amplitude and a natural frequency determined by the dimensions of the volume and the intake passage is generated so that a larger supercharging effect can be obtained. Since the wave propagation path length is longer than in the case of the inertial effect described above, it has a characteristic that the effect is exhibited in a relatively low rotation range.
ところで、このような共鳴効果による圧力波過給シス
テムにおいては、2つの気筒群間の吸気系内の圧力波の
位相が互いに逆であることに着目して、2つの気筒群の
夫々の共通吸気通路を連通する連通部を設け、連通部内
の圧力が、両気筒群の圧力波の相互の干渉作用により均
一に保たれるという現象を利用して、該連通部に容積部
と同様の作用を行なわせ、吸気系の簡素化を図ったもの
が提案されている。(例えば、実開昭56−120315号公
報、実開昭58−175121号公報参照)。By the way, in such a pressure wave supercharging system by the resonance effect, attention is paid to the fact that the phases of the pressure waves in the intake system between the two cylinder groups are opposite to each other. By providing a communicating portion that communicates the passages, and utilizing the phenomenon that the pressure in the communicating portion is uniformly maintained by the mutual interference action of the pressure waves of both cylinder groups, the communicating portion has the same function as the volume portion. It has been proposed to make the intake system simpler. (See, for example, Japanese Utility Model Publication No. 56-120315 and Japanese Utility Model Publication No. 58-175121).
そして、前記したような2つの圧力波過給の特性に着
目して、エンジンの所定の低回転域では共鳴効果による
圧力波過給を行ない、一方、所定の高回転域では慣性効
果による圧力波過給を行なうようにして、全回転域での
過給効果を向上させるようにしたものが提案されてい
る。そして、その手法の1つとして、例えば、第5図に
示すように、吸気系統に所定の容積を有するサージタン
ク31を介設し、サージタンク31の長手方向に延びる両側
面に、夫々、点火順序が連続しない気筒で構成される気
筒群の独立吸気通路32を接続し、サージタンク31の中央
部に独立吸気通路32の配列方向に伸長する連通部33を設
けるとともに、サージタンク31内の2つの気筒群に夫々
接続された、2つの空間部34,35を連通または遮断する
開閉弁36を設け、低回転時には開閉弁36を閉じて連通路
33を圧力反転部とする共鳴効果による圧力波過給を行な
い、一方、高回転時には開閉弁36を開いてサージタンク
31を単一の容積部として作用させ、慣性効果による圧力
波過給を行なうようにしたものが提案されている(例え
ば、特願昭60−183530号参照)。Focusing on the two characteristics of pressure wave supercharging as described above, pressure wave supercharging is performed by the resonance effect in a predetermined low rotation range of the engine, while pressure waves are generated by the inertia effect in a predetermined high rotation range. It has been proposed that supercharging is performed to improve the supercharging effect in the entire rotation range. As one of the methods, for example, as shown in FIG. 5, a surge tank 31 having a predetermined volume is provided in the intake system, and both side surfaces extending in the longitudinal direction of the surge tank 31 are respectively ignited. The independent intake passages 32 of the cylinder group composed of cylinders which are not consecutive are connected to each other, and the communication portion 33 extending in the arrangement direction of the independent intake passages 32 is provided at the center of the surge tank 31. An on-off valve 36 that connects or disconnects the two space portions 34 and 35, which are respectively connected to one cylinder group, is provided, and when the engine speed is low, the on-off valve 36 is closed to establish a communication passage.
The pressure wave is supercharged by the resonance effect with 33 as the pressure reversal part, while the open / close valve 36 is opened at high speed to surge tank.
It has been proposed that 31 acts as a single volume to perform pressure wave supercharging by the inertial effect (see, for example, Japanese Patent Application No. 60-183530).
しかし、この従来のものにおいては、開閉弁が開かれ
ても、サージタンク内の両気筒群側の空間部は、互い
に、開閉弁を設けた部分の狭い連通部を介して連通する
だけなので、サージタンクは十分な容積を有する容積部
として完全には作用せず、高回転時における慣性効果の
効率が低下するといった問題があった。However, in this conventional one, even if the on-off valve is opened, the space portions on both cylinder group sides in the surge tank communicate with each other only through the narrow communication portion of the portion provided with the on-off valve. The surge tank does not completely function as a volume portion having a sufficient volume, and there is a problem in that the efficiency of the inertia effect at the time of high rotation decreases.
[発明の目的] 本発明は上記従来の問題点に鑑みてなされたものであ
って、吸気系統にサージタンクを設けて、慣性効果によ
る圧力波過給と共鳴効果による圧力波過給の両方を行な
うようにした多気筒エンジンにおいて、エンジンの全回
転域において、高い過給効率が得られ、エンジンの出力
が向上する多気筒エンジンの吸気装置を提供することを
目的とする。[Object of the Invention] The present invention has been made in view of the above conventional problems, and a surge tank is provided in the intake system to perform both pressure wave supercharging due to the inertia effect and pressure wave supercharging due to the resonance effect. It is an object of the present invention to provide an intake system for a multi-cylinder engine in which high supercharging efficiency is obtained and engine output is improved in the entire rotation range of the engine in the multi-cylinder engine.
[発明の構成] 本発明は上記の目的を達するため、吸気通路に所定の
容積を有するサージタンクを介設した多気筒エンジンの
吸気装置において、サージタンクの長手方向に延びる各
側面壁に、夫々、点火順序が互いに連続しない気筒同士
の独立吸気通路を接続する一方、サージタンク内に上記
長手方向と交差する方向に所定間隔を保って、サージタ
ンクの長手方向に伸長する複数の開閉弁を設け、該複数
の開閉弁が閉じられたときには相隣合う開閉弁間に一方
の側面壁側の空間と他方の側面壁側の空間とを連通させ
る連通路を形成し、上記複数の開閉弁が開かれたときに
は十分なサージタンク容量を得るように上記開閉弁を配
設したことを特徴とする多気筒エンジンの吸気装置を提
供する。In order to achieve the above object, the present invention has an intake device for a multi-cylinder engine in which a surge tank having a predetermined volume is provided in an intake passage, and each side wall extending in the longitudinal direction of the surge tank is provided with a side wall. While connecting the independent intake passages of the cylinders whose ignition orders are not continuous to each other, a plurality of on-off valves extending in the longitudinal direction of the surge tank are provided in the surge tank at predetermined intervals in a direction intersecting the longitudinal direction. When the plurality of on-off valves are closed, a communication passage is formed between adjacent ones of the on-off valves to connect the space on one side wall side and the space on the other side wall side, and the plurality of on-off valves are opened. Provided is an intake system for a multi-cylinder engine, characterized in that the on-off valve is arranged so as to obtain a sufficient surge tank capacity when it is opened.
[発明の効果] 本発明によれば、所定の低回転域で各開閉弁を閉じれ
ば、サージタンク内の相隣合う開閉弁間に、サージタン
クの長手方向にほぼその全長にわたって伸長する連通路
が形成され、この連通路が十分な長さを有する共鳴効果
の共鳴管及び圧力反転部として機能するので、限られた
スペースを利用したコンパクトな構造で高い共鳴効果を
得ることができる。[Effect of the Invention] According to the present invention, if each on-off valve is closed in a predetermined low rotation range, a communication passage extending between the adjacent on-off valves in the surge tank over substantially the entire length thereof in the longitudinal direction of the surge tank. Is formed, and this communication passage functions as a resonance tube having a resonance effect having a sufficient length and a pressure reversal portion, so that a high resonance effect can be obtained with a compact structure utilizing a limited space.
他方、所定の高回転域で各開閉弁を開けば、サージタ
ンクの長手方向と交差する方向には実質的に吸気の流れ
ないしは圧力波の伝播を遮るものはなく、サージタンク
を十分な容積を有する単一の容積部として機能させるこ
とができる。この場合、各独立吸気通路を上流に向かっ
て伝播してきた負の圧力波が、サージタンクでほぼ完全
に圧力を反転させられて強い正圧波として各気筒に戻る
ので、効果的な慣性効果により充填効率すなわちエンジ
ン出力が高められる。On the other hand, if each on-off valve is opened in a predetermined high rotation range, there is no substantial obstruction to the flow of intake air or the propagation of pressure waves in the direction intersecting the longitudinal direction of the surge tank, and the surge tank has a sufficient volume. It can function as a single volume with. In this case, the negative pressure wave propagating upstream in each independent intake passage is almost completely pressure-reversed in the surge tank and returns to each cylinder as a strong positive pressure wave. Efficiency or engine power is increased.
[実施例] 以下、本発明の実施例を具体的に説明する。[Examples] Examples of the present invention will be specifically described below.
第1図と第2図とは、本発明の実施例を示すサージタ
ンクまわりの吸気装置の一部断面平面図と一部断面立面
図とである。FIG. 1 and FIG. 2 are a partial sectional plan view and a partial sectional elevation view of an intake device around a surge tank showing an embodiment of the present invention.
これらの図に示すように、6気筒レシプロエンジン
(図示せず)の上方に配設された、細長の中空略直方体
状のサージタンク1の長手方向に延びる2つの側面壁2
p,2qの中で、第1側面壁2pには、サージタンク1の吸気
流入側端部1s(以下、前端部1sという)側から他方の側
端部1t(以下、後端部1tという)に向って順に、点火順
序が連続しない第1,第3,第5気筒(図示していないが、
以下これらを第1気筒群という)と夫々連通する第1,第
3,第5独立吸気通路3a,3c,3e(以下、第1独立吸気通路
群3pという)が接続され、一方、第2側面壁2qには、前
端部1s側から後端部1t側に向って順に、点火順序が連続
しない第2,第4,第6気筒(図示していないが、以下これ
らを第2気筒群という)と連通する第2,第4,第6独立吸
気通路3b,3d,3f(以下、第2独立吸気通路群3qという)
が接続されている。As shown in these drawings, two side walls 2 extending in the longitudinal direction of a long and slender hollow surge tank 1 disposed in the upper portion of a 6-cylinder reciprocating engine (not shown).
Of the p and 2q, the first side wall 2p has a side end 1t (hereinafter referred to as a rear end 1t) from the intake inflow side end 1s (hereinafter referred to as a front end 1s) side of the surge tank 1 to the other side end 1t. In the order of, the first, third, and fifth cylinders whose ignition order is not continuous (not shown,
Hereinafter, these are referred to as the first cylinder group)
The third and fifth independent intake passages 3a, 3c, 3e (hereinafter referred to as the first independent intake passage group 3p) are connected, while the second side wall 2q extends from the front end 1s side toward the rear end 1t side. The second, fourth, and sixth independent intake passages 3b, 3d communicating with the second, fourth, and sixth cylinders (not shown, but hereinafter referred to as the second cylinder group) whose ignition order is not continuous. , 3f (hereinafter referred to as the second independent intake passage group 3q)
Is connected.
そして、サージタンク1内の空間部には、長手方向と
直交する方向(以下、横断方向という)について中寄り
となる位置において、サージタンク1の後面壁2tを貫通
して、サージタンク1の長手方向にその全長の大部分に
渡って伸長する第1弁軸5に取付けられた第1開閉弁6
と、第1弁軸5に対してこれより第2側面壁2q側に所定
の間隔を保ち、かつサージタンク1の後面壁2tを貫通
し、さらにサージタンク1の上面壁2uと底面壁2wとに結
合された後部仕切壁7の一部をその長手方向に貫通し
て、サージタンク1の長手方向にその全長の大部分に渡
って伸長する第2弁軸8に取付けられた第2開閉弁9と
が設けられている。なお、この後部仕切壁7はその前側
終端部7hより前方には形成されていないので、この部分
ではサージタンク1内の空間部は仕切られないようにな
っている。The surge tank 1 extends through the rear wall 2t of the surge tank 1 at a position closer to the center in the direction orthogonal to the longitudinal direction (hereinafter referred to as the transverse direction) in the space inside the surge tank 1. A first on-off valve 6 mounted on a first valve shaft 5 extending in the direction of most of its entire length.
With respect to the first valve shaft 5, the second side wall 2q side is kept at a predetermined distance from the first valve shaft 5, and the rear wall 2t of the surge tank 1 is penetrated. Further, the top wall 2u and the bottom wall 2w of the surge tank 1 A second on-off valve attached to a second valve shaft 8 that penetrates a part of the rear partition wall 7 connected to the longitudinal direction thereof and extends in the longitudinal direction of the surge tank 1 over most of its entire length. 9 and are provided. Since the rear partition wall 7 is not formed in front of the front end portion 7h, the space inside the surge tank 1 is not partitioned at this portion.
第1開閉弁6が第1図と第2図とにその状態を示すよ
うに閉弁されたときには、該第1開閉弁6と、上面壁2u
と底面壁2wとに結合された前部仕切壁11とは、協同して
サージタンク1内の空間部を第1開閉弁6にかからない
第1連通部12を除いて横断方向に仕切っている。なお、
この前部仕切壁11はその後側終端部11hより後方には形
成されていないので、この部分ではサージタンク1内の
空間部は仕切らないようになっている。これらと第1側
面壁2pとの間には第1独立吸気通路群3pと直接連通する
とともに、吸気が供給される第1共通吸気通路13と連通
する第1室14が画成されている。また、同様に第2開閉
弁9が閉弁されたときには、該第2開閉弁9と後部仕切
壁7とは、協同してサージタンク1内の空間部を第2開
閉弁9にかからない第2連通部15を除いて横断方向に仕
切っており、これらと第2側面壁2qとの間には第2独立
吸気通路群3qと直接連通するとともに、吸気が供給され
る第2共通吸気通路16と連通する第2室17が画成されて
いる。When the first on-off valve 6 is closed as shown in FIGS. 1 and 2, the first on-off valve 6 and the upper wall 2u
And a front partition wall 11 connected to the bottom wall 2w cooperate with each other to partition the space in the surge tank 1 in the transverse direction except for the first communication portion 12 that does not cover the first opening / closing valve 6. In addition,
Since the front partition wall 11 is not formed behind the rear end portion 11h, the space inside the surge tank 1 is not partitioned at this portion. A first chamber 14 that communicates directly with the first independent intake passage group 3p and also communicates with the first common intake passage 13 to which intake air is supplied is defined between these and the first side wall 2p. Similarly, when the second opening / closing valve 9 is closed, the second opening / closing valve 9 and the rear partition wall 7 cooperate with each other so that the space inside the surge tank 1 is not covered by the second opening / closing valve 9. It is partitioned in the transverse direction except the communication portion 15, and the second side wall 2q is directly communicated with the second independent intake passage group 3q, and the second common intake passage 16 is supplied with intake air. A second chamber 17 that communicates is defined.
そして、第1開閉弁6と第2開閉弁9とが閉弁されて
いるときには、これらの間に画成される空間部は、第1
連通部12において第1室14と連通し、かつ第2連通部15
において第2室17と連通して、サージタンク1の長手方
向に細長く伸長する連通路18を形成するようになってい
る。When the first on-off valve 6 and the second on-off valve 9 are closed, the space defined between them is the first
The communication part 12 communicates with the first chamber 14 and the second communication part 15
In the above, a communication passage 18 is formed which communicates with the second chamber 17 and which is elongated in the longitudinal direction of the surge tank 1.
一方、第1開閉弁6と第2開閉弁9とが開弁されたと
きには、サージタンク1内の空間部を横断方向に遮るも
のは実質的にはそれ程面積の大きくない後部仕切壁7と
前部仕切壁11のみとなり、サージタンク1内の空間部は
実質的にサージタンク1の全容積を有する単一な容積部
を形成するようになっている。On the other hand, when the first opening / closing valve 6 and the second opening / closing valve 9 are opened, the one that intercepts the space in the surge tank 1 in the transverse direction is substantially the same in area as the rear partition wall 7 and the front partition wall. Only the partition wall 11 is provided, and the space within the surge tank 1 forms a single volume having substantially the entire volume of the surge tank 1.
上記第1開閉弁6と第2開閉弁9とは、リンク機構21
を介してアクチュエータ22によって同一タイミングで開
閉されるようになっている。ところが、第1開閉弁6と
第2開閉弁9とがともに開弁されると、第3図に示すよ
うに、これらが互いに干渉し合うので、これを防止する
ために、第1弁軸5と第2弁軸8の取付け位置は上下方
向に第1,第2開閉弁6,9の厚さに相当する長さdだけオ
フセットをもたせて設定している。The first opening / closing valve 6 and the second opening / closing valve 9 have a link mechanism 21.
The actuator 22 is opened and closed at the same timing via the. However, when both the first opening / closing valve 6 and the second opening / closing valve 9 are opened, as shown in FIG. 3, they interfere with each other. The mounting position of the second valve shaft 8 is set in the vertical direction with an offset of a length d corresponding to the thickness of the first and second on-off valves 6 and 9.
以下、本実施例の作用について説明する。 The operation of this embodiment will be described below.
エンジン回転数Nが第4図に示すような所定回転数N0
より小さい低回転域では、アクチュエータ22によって第
1,第2開閉弁6,9がともに閉じられる。このとき、本願
従来例において詳しく説明したように、第1気筒群3pと
第2気筒群3qとは夫々、連通路18を両気筒分3p,3qの吸
気系統の夫々の圧力波の相互干渉による均圧部すなわ
ち、圧力波反転部とする共鳴効果によって圧力波過給が
行なわれる。このような共鳴効果による圧力波過給が行
なわれた場合のエンジンの出力(トルク)の特性は第4
図中の曲線G1のようになり、N0より小さい所定の回転数
で極大となり、これより高回転側では回転数の増加に伴
って急激に低下している。The engine speed N is a predetermined speed N 0 as shown in FIG.
In the smaller low speed range, actuator 22
Both the first and second on-off valves 6 and 9 are closed. At this time, as described in detail in the prior art example of the present application, the first cylinder group 3p and the second cylinder group 3q respectively have the communication passage 18 through the mutual interference of the pressure waves of the intake systems of both cylinders 3p and 3q. Pressure wave supercharging is performed by the resonance effect of the pressure equalizing portion, that is, the pressure wave inverting portion. The characteristic of the output (torque) of the engine when the pressure wave supercharging due to the resonance effect is performed is the fourth characteristic.
It becomes like a curve G 1 in the figure, and reaches a maximum at a predetermined rotation speed smaller than N 0 , and on the higher rotation side than this, it sharply decreases as the rotation speed increases.
そこで、エンジン回転数NがN0以上の高回転域では、
アクチュエータ22によって第1,第2開閉弁6,9がともに
開かれ、高回転域で効果を発揮する慣性効果による圧力
波過給が行なわれる。このとき、サージタンク1内の空
間部は前記したように実質的に単一の容積部となるの
で、本願従来技術で説明したように、各気筒では、夫
々、サージタンク1内の空間部を容積部とする慣性効果
による圧力波過給が行なわれる。このような、慣性効果
による圧力波過給が行なわれた場合のエンジン出力の特
性は第4図中の曲線G3のようになり、N0より大きい所定
の回転数で極大となる。本案では、サージタンク1内の
空間部が十分な容積を有する容積部となり、各独立吸気
通路から伝播される負の圧力波をほぼ完全に正の圧力波
に反転させるので、過給効果が高まり、例えば、第4図
中の曲線G2で示すような従来のものより大幅にエンジン
出力が向上する。Therefore, in the high speed range where the engine speed N is N 0 or more,
The actuator 22 opens both the first and second on-off valves 6 and 9 to perform pressure wave supercharging by the inertial effect that is effective in a high rotation range. At this time, since the space inside the surge tank 1 is substantially a single volume as described above, the space inside the surge tank 1 is different in each cylinder as described in the related art. Pressure wave supercharging is performed by the inertial effect of the volume. The characteristic of the engine output when the pressure wave supercharging by the inertial effect is performed is as shown by a curve G 3 in FIG. 4, and becomes maximum at a predetermined rotation speed higher than N 0 . In the present proposal, the space inside the surge tank 1 becomes a volume having a sufficient volume, and the negative pressure wave propagating from each independent intake passage is almost completely inverted to the positive pressure wave, so that the supercharging effect is enhanced. For example, the engine output is significantly improved as compared with the conventional one as shown by the curve G 2 in FIG.
このようにして、本案ではサージタンク内の開閉弁の
開閉により低回転域では共鳴効果により、高回転域では
慣性効果により強力な圧力波過給が行なわれるので、コ
ンパクトな構成で全回転域においてエンジン出力を向上
させることができる。In this way, according to the present invention, by opening and closing the on-off valve in the surge tank, strong pressure wave supercharging is performed by the resonance effect in the low rotation range and the inertial effect in the high rotation range. The engine output can be improved.
なお、本実施例ではサージタンク内に開閉弁を2つ設
けているが、開閉弁の数をこれより増やして連通路を複
数とした場合でも、本実施例と同様の作用・効果が得ら
れるのはもちろんである。In this embodiment, two on-off valves are provided in the surge tank. However, even if the number of on-off valves is increased to make a plurality of communication passages, the same action and effect as in this embodiment can be obtained. Of course.
【図面の簡単な説明】 第1図と第2図とは、夫々、本発明の実施例を示すサー
ジタンクまわりの吸気装置の一部断面平面図と一部断面
立面図とである。 第3図は、第2図のB−B線断面説明図である。 第4図は、本案にかかるエンジンの出力(トルク)のエ
ンジン回転数に対する特性を示す図である。 第5図は、内部に共鳴効果用均圧部として作用する連通
路を備えた従来のサージタンクを示す説明図である。 1……サージタンク、3a,3b,3c,3d,3e,3f……第1〜第
6独立吸気通路、6……第1開閉弁、9……第2開閉
弁、14……第1室、17……第2室、18……連通路。BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 and FIG. 2 are a partial sectional plan view and a partial sectional elevation view of an intake device around a surge tank showing an embodiment of the present invention, respectively. FIG. 3 is a cross-sectional explanatory view taken along the line BB of FIG. FIG. 4 is a diagram showing the characteristic of the output (torque) of the engine according to the present invention with respect to the engine speed. FIG. 5 is an explanatory view showing a conventional surge tank provided internally with a communication passage acting as a pressure equalizing portion for resonance effect. 1 ... surge tank, 3a, 3b, 3c, 3d, 3e, 3f ... first to sixth independent intake passages, 6 ... first opening / closing valve, 9 ... second opening / closing valve, 14 ... first chamber , 17 …… Second room, 18 …… Communication passage.
───────────────────────────────────────────────────── フロントページの続き (72)発明者 幸徳 正信 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62−41922(JP,A) 実公 平7−17783(JP,Y2) ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Masanori Kotoku, No. 3 Shinchi, Fuchu-cho, Aki-gun, Hiroshima Prefecture Mazda Co., Ltd. (56) References JP-A-62-41922 (JP, A) Jikkouhei 7- 17783 (JP, Y2)
Claims (1)
クを介設した多気筒エンジンの吸気装置において、 サージタンクの長手方向に延びる各側面壁に、夫々、点
火順序が互いに連続しない気筒同士の独立吸気通路を接
続する一方、 サージタンク内に上記長手方向と交差する方向に所定間
隔を保って、サージタンクの長手方向に伸長する複数の
開閉弁を設け、 該複数の開閉弁が閉じられたときには相隣合う開閉弁間
に一方の側面壁側の空間と他方の側面壁側の空間とを連
通させる連通路を形成し、上記複数の開閉弁が開かれた
ときには十分なサージタンク容量を得るように上記開閉
弁を配設したことを特徴とする多気筒エンジンの吸気装
置。1. An intake system for a multi-cylinder engine in which a surge tank having a predetermined volume is provided in an intake passage, and a side wall extending in the longitudinal direction of the surge tank is provided with cylinders whose ignition sequences are not continuous with each other. While connecting the independent intake passages, a plurality of on-off valves extending in the longitudinal direction of the surge tank are provided in the surge tank at a predetermined interval in a direction intersecting the longitudinal direction, and the on-off valves are closed. Occasionally, a communication passage that connects the space on one side wall side and the space on the other side wall side is formed between the adjacent open / close valves, and a sufficient surge tank capacity is obtained when the plurality of open / close valves are opened. An intake device for a multi-cylinder engine, in which the on-off valve is arranged as described above.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10277487A JPH0819851B2 (en) | 1987-04-23 | 1987-04-23 | Multi-cylinder engine intake system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10277487A JPH0819851B2 (en) | 1987-04-23 | 1987-04-23 | Multi-cylinder engine intake system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63266119A JPS63266119A (en) | 1988-11-02 |
| JPH0819851B2 true JPH0819851B2 (en) | 1996-02-28 |
Family
ID=14336503
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10277487A Expired - Fee Related JPH0819851B2 (en) | 1987-04-23 | 1987-04-23 | Multi-cylinder engine intake system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0819851B2 (en) |
-
1987
- 1987-04-23 JP JP10277487A patent/JPH0819851B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63266119A (en) | 1988-11-02 |
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