JPH01280632A - Intake system for engine - Google Patents

Intake system for engine

Info

Publication number
JPH01280632A
JPH01280632A JP10941288A JP10941288A JPH01280632A JP H01280632 A JPH01280632 A JP H01280632A JP 10941288 A JP10941288 A JP 10941288A JP 10941288 A JP10941288 A JP 10941288A JP H01280632 A JPH01280632 A JP H01280632A
Authority
JP
Japan
Prior art keywords
intake
resonance
engine
passage
rotation speed
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
JP10941288A
Other languages
Japanese (ja)
Other versions
JP2771175B2 (en
Inventor
Mitsuo Hitomi
光夫 人見
Akinori Yamashita
山下 昭則
Toshihiko Hattori
服部 敏彦
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 JP63109412A priority Critical patent/JP2771175B2/en
Publication of JPH01280632A publication Critical patent/JPH01280632A/en
Application granted granted Critical
Publication of JP2771175B2 publication Critical patent/JP2771175B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は共鳴効果によって吸気の充填効率を高めるよう
にLノだエンジンの吸気装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION (Industrial Field of Application) The present invention relates to an intake system for an L-noise engine that improves the filling efficiency of intake air through a resonance effect.

(従来の技術) 従来から、吸気の動的効果によって充填効蜜を高めるよ
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、特公昭60−14169号公報に示された装置では
、多気筒丁4ンジンにおいて、吸気系を吸気順序が連続
しない気筒間」を同一・グループとする2つのグループ
に分け、この2つのグループの吸気系をそれぞれ、気筒
別の独立吸気通路(吸気ン二ボールドブランチ)の上流
端が接続された容積大の集合部と、この集合部から上流
に延びる共鳴通路とを備えて構成するととらに、上記集
合部に、−1−記名グループの吸気系相ムンを連通遮断
可能とする切替装置を設け、各共鳴通路の上流端を1流
側集合室に接続している。イし一〇、上記切替装置が上
記各グループ相与をm1IiLだ状態にあるどきは、土
浦側集合窄で反則される吸気圧力波によって下ンジンの
低速域で゛過給作用が盲られるよう【こ、上記ト流側集
合゛全と各吸気ボー1〜どの間の吸気系による固有振動
数を設定しておくとと6に、」:記切替装置が「記名吸
気通路を連通する状態となったどきは、化較的高速域で
上記独立吸気通路による慣性過給効果く各気筒毎に独立
吸気通路の土浦端で反射されるj]−力波が吸入終期に
作用することにJ:る過給効果)が得られるように、独
立吸気通路の艮ざ等を設定している。
(Prior Art) Various engine intake devices have been known in which the filling efficiency is enhanced by the dynamic effect of intake air. For example, in the device disclosed in Japanese Patent Publication No. 60-14169, in a multi-cylinder four-engine engine, the intake system is divided into two groups in which the cylinders in which the intake order is not consecutive are the same group. Each of the intake systems is configured to include a large-volume gathering section to which the upstream ends of independent intake passages (intake two bold branches) for each cylinder are connected, and a resonant passage extending upstream from the gathering section. , A switching device is provided in the collecting section to enable communication and disconnection of the intake system phase of the -1-registered group, and the upstream end of each resonance passage is connected to the first flow side collecting chamber. 10. When the switching device is in the state where the above-mentioned groups are mutually equal to m1IiL, the intake pressure wave that is counteracted by the Tsuchiura side condensation will blind the supercharging effect in the low speed range of the lower engine. If we set the natural frequency of the intake system between the above-mentioned flow-side set ``all'' and each intake bow 1 to 6, the switching device will be in the state of communicating the named intake passage. The reason for this is that in a relatively high speed range, the inertial supercharging effect of the above-mentioned independent intake passage causes a force wave to be reflected at the Tsuchiura end of the independent intake passage for each cylinder and acts at the end of intake. The shape of the independent intake passage is designed to achieve a supercharging effect (supercharging effect).

〔発明が解決しようどする課題) 十配吸気装h′のJ、うに高速域での過給作用を気筒別
の独立吸気通路による慣性効果によっで得るようにJる
場合は、高速域とはいえども実用回転数域内で慣性効果
を持たせる必要があり、従って、十記独ft吸気通路に
j、る慣+11同調回転数が]ンシンの許容最高回転数
より【、1、低くなるように、独\°l吸気通路をある
稈庶艮く形成づる必要がある。1しかし、F記独\シ吸
気通路は各気筒毎にそれぞれ設けられるので、この各独
立吸気通路をそれぞれ長く形成すると、吸気系を−」ン
バク;・化することが困ガとなる。
[Problem to be solved by the invention] When the ten-distribution intake system h' is used to obtain supercharging action in the high-speed range by the inertial effect of the independent intake passages for each cylinder, the high-speed range and However, it is necessary to have an inertial effect within the practical rotational speed range, so the tuned rotational speed in the intake passage should be [, 1, 1, lower than the maximum allowable rotational speed for]. Therefore, it is necessary to form the intake passage in a certain way. However, since an intake passage is provided for each cylinder, if each independent intake passage is formed to be long, it becomes difficult to make the intake system compact.

また、上記の、J:うに吸気系を2つのグルー1に分【
プた場合、上記独立吸気通路によるti!1竹効果のは
かに、グループ別の独立吸気通路の集合部とその上流側
で連通づる通路部分も含めた共鳴系での圧力波の」を振
による共鳴効果も期待゛Cきるが、独ft吸気通路が長
く形成されていると、高速域で共鳴効果を持たせるため
には気筒間の連通部分の長さが極端に短くなって吸気系
を2グループに分LJたことの効果がうすれ、かつ、独
立吸気通路の固有振動数に支配されて共鳴系の固有振り
J数が充分に高められない。これらの理由もあって、従
来公知のものでは、とくに]−ンシンのム′1容最高回
転数付近で有効に共鳴効果が得られるようにしたしのが
なかった、。
In addition, above J: Separate the sea urchin intake system into two glues 1 [
ti! due to the above-mentioned independent intake passage. In addition to the bamboo effect, we can also expect a resonance effect due to the vibration of pressure waves in the resonant system that includes the collective part of the independent intake passages of each group and the passage part that communicates with them on the upstream side. ft. If the intake passage is formed long, the length of the communication part between the cylinders will be extremely short in order to have a resonance effect in the high-speed range, and the effect of dividing the intake system into two groups will be weakened. , and the natural oscillation J number of the resonance system cannot be sufficiently increased because it is dominated by the natural frequency of the independent intake passage. For these reasons, none of the conventionally known motors has been able to effectively obtain a resonance effect, particularly near the maximum rotational speed of the engine.

本発明は一上記の小情tこ1’L Jt、気筒別の独立
吸気通路を短くし′C吸気系を」ンバク1〜化しつつ、
とくに二Iンジンの許容最高回転数イζ1近の高速域で
共鳴効果によりTンジン出力を高めることができる]−
ンジンの吸気装置を提供覆るものて゛ある。
The present invention addresses the above-mentioned details by shortening the independent intake passages for each cylinder and converting the intake system into one.
In particular, the T engine output can be increased due to the resonance effect in the high speed range near the maximum allowable rotation speed of the 2 I engine.
There is something that covers the engine's intake system.

〔課題を解決するlζめのf段〕[1ζth f stage to solve the problem]

本発明は上記のような目的を達成するため、エンジンの
吸気系を吸気順序か連続しない気筒間」を同一グループ
どする複数のグループに分りで、気筒別の独立吸気通路
を各グループ毎に各々集合させ、上記各グループの独0
吸気通路および集合部と各集合部に連なる通路部分とで
各グループに対する共鳴系を構成するとどしに、上記独
立吸気通路を、この通路による慣ゼ[同調回転数がエン
ジンの許容最高回転数より高くなるように設定し、かつ
、上記共鳴系を、その最り、(1経路による共鳴同調回
転数Nrがエンジンの許’fl IR高回転数N ma
xに対し−( 0、7Nmax <N r < 1 、2Nmaxどな
るように設定したしの(−ある。
In order to achieve the above object, the present invention divides the intake system of an engine into a plurality of groups in which cylinders that are not consecutive in the intake order are grouped into the same group, and creates independent intake passages for each cylinder in each group. Gather each group above and
The intake passage, the collecting part, and the passage part connected to each collecting part form a resonance system for each group. IR high rotation speed Nma
For x, -(0, 7Nmax <N r < 1, 2Nmax is set as (-).

〔作用〕[Effect]

上記構成にJ:ると、独立吸気通路による慣性同調回転
数を上記設定どすることによって独立吸気通路が充分に
’)、F5 < ’、にり、よノこ、この設定により独
立吸気通路の慣性効果には頼らない、J:うにする−方
、共鳴系の上記共鳴同調回転数Nrをl−記設定とする
ことにより、後に詳述するように1ンシンの許容最高回
転数N max付近の高速域でイj効に共鳴過給作用が
得られる。
With the above configuration, by setting the inertia synchronized rotation speed of the independent intake passage as described above, the independent intake passage becomes sufficient. In order not to rely on inertial effects, by setting the resonance tuning rotation speed Nr of the resonant system as described below, as will be detailed later, the maximum allowable rotation speed N max of one engine can be achieved. Resonant supercharging effect can be obtained in the high speed range.

〔実施例〕〔Example〕

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、この図において、V型エ
ンジンの一1ノのバンク1には1番、2番、3番の3つ
の気筒3a、3b、3cが設(プられ、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。上記各気筒3a〜3tにはそれぞれ吸
気ボート4a−4fおよび排気ポー1−(図示省略)が
配設され、これらボートが図外の吸気弁おJ:びυ1気
弁によってそれぞれ所定のタイミングで開閉される。上
記各気筒3a〜3tの吸気順序(点火順序)は、1番気
筒3a−)4香気B 3 d −> 2番気筒3b−〉
5番気筒3e→3番気筒3cmνθ番気M3fの順どな
っている。
FIG. 1 shows an embodiment in which the device of the present invention is applied to a V-type six-cylinder engine. Three cylinders 3a, 3b, 3c are installed (pulled), and the other bank 2
Three cylinders 3d, 3e, and 3f, numbered 4, 5, and 6, are provided. Each of the cylinders 3a to 3t is provided with an intake boat 4a to 4f and an exhaust port 1- (not shown), and these boats are opened and closed at predetermined timings by intake valves and υ1 valves (not shown). be done. The intake order (ignition order) of each of the cylinders 3a to 3t is as follows: No. 1 cylinder 3a-)4 aroma B3d->No. 2 cylinder 3b->
The order is from No. 5 cylinder 3e to No. 3 cylinder 3cmvθ to No. M3f.

このエンジンの吸気系は吸気順序が連続しない気筒間t
を同一グループどする2つのグループに分【ノられ、つ
まり上記吸気順序に、J:ると、一方のバンク2の各気
筒3 a・〜・330は!7いに吸気順序が連続せヂ、
他方のバンク2の各気筒3d〜3fb亙いに吸気類1%
が連続しないの−(、吸気系が−hのバンク1側のグル
ー/(第1グループ)と他方のバンク2側のグループ(
第2グループ)とに分(プられている。そして、第1グ
ループの各吸気ボート4a−4Cにそれぞれ接続された
気筒別の各独立吸気通路5a〜5Cおよび第2グループ
の各吸気ボー1〜4d〜41−にそれぞれ接続された気
筒別の各独立吸気通路5d〜5fは、各グループ毎に各
々集合され、つまり、独立吸気通路5a〜5Cの各上流
端が第1グループ側の集合部6に接続されるとともに、
独11吸気通路5 d〜5[の各土浦端が第2グループ
側の集合部7に接続されている。このグループ別の集合
部6,7の各−・端側には、上流側連通部分を構成する
通路8.9が接続され、この各通路8.9は上流端側で
互いに連通されて、この連通箇所に共通吸気通路10が
接続されている1、まIこ、上記集合部6,7の各他端
側には、下流側連通路11が接続されている。J記共通
吸気通路10には、上流側か1う順に1アクリ−+ 1
2. l’771]−メータ13+ll;cLヒス1:
1ツhル弁14が配設されCいる。
The intake system of this engine has t between cylinders where the intake order is not consecutive.
are divided into two groups that are the same group, that is, according to the above intake order, then each cylinder 3a...330 of one bank 2 is! 7. Inhalation order is consecutive,
1% intake for each cylinder 3d to 3fb of the other bank 2
are not consecutive - (, the intake system is -h's bank 1 side glue / (1st group) and the other bank 2 side group (
Each of the independent intake passages 5a to 5C for each cylinder connected to each intake boat 4a to 4C of the first group and each intake boat 1 to 1 of the second group The independent intake passages 5d to 5f for each cylinder connected to the respective cylinders 4d to 41- are collected in each group, that is, the upstream ends of the independent intake passages 5a to 5C are connected to the collecting part 6 on the first group side. In addition to being connected to
Each Tsuchiura end of the intake passages 5 d to 5 is connected to the collecting portion 7 on the second group side. A passage 8.9 constituting an upstream communication part is connected to each end of the grouped gathering parts 6, 7, and the passages 8.9 are communicated with each other at the upstream end. A downstream communication passage 11 is connected to the other end of each of the gathering parts 6 and 7, to which the common intake passage 10 is connected. In the J common intake passage 10, 1acry + 1 in the order of upstream or 1
2. l'771] - meter 13 + ll; cL hiss 1:
A one-way valve 14 is provided.

この実施例では、各グループにおりる独立吸気通路5a
 〜5c、5d 〜51’お、」;び集合部6.7と各
集合部6,7間の連通部分を構成する通路8゜9.1;
流側連通路11により共鳴系が構成される。
In this embodiment, independent intake passages 5a leading to each group
~5c, 5d ~51'o,''; and a passage 8°9.1 that constitutes a communication portion between the gathering portion 6.7 and each gathering portion 6,7;
The flow side communication path 11 constitutes a resonance system.

この共鳴系において、上記通路8.9により構成される
上流側連通部分とl;流側連通路11とは同等の長さに
形成しておいてもよいが、例えば小流側連通路11の長
さを知くするというにうに両側連通部分の長さを異なら
せ一〇おいてもよい。さらに図に示すに・)に、ト流側
連通路11に1ニンジン回転数に応じて開閉される開閉
弁15を設けてJ3き、口の開閉弁15によってF流側
連通路11が閉じられたとさと聞かれたときとC゛共鳴
系の共鳴固有振動数が変化するJ:うにしておいてbよ
い。
In this resonance system, the upstream communication passage 11 constituted by the passage 8.9 and the upstream communication passage 11 may be formed to have the same length; In order to know the length, the lengths of the communicating portions on both sides may be made different by 10. Furthermore, as shown in the figure, an on-off valve 15 that opens and closes according to the number of rotations of one carrot is provided in the flow-side communication passage 11, and the on-off valve 15 at the mouth closes the communication passage F. When asked, the resonant natural frequency of the resonant system changes.

また、十配集合部6.7は、通路8.9と同じ断面積の
パイプにより形成しておいてらよいが、図に示すように
断面積を大きくしである程度の容量を槓たせ−Cおいて
も、共鳴効果は得られる。
Additionally, the ten-way gathering portion 6.7 may be formed of a pipe having the same cross-sectional area as the passage 8.9, but as shown in the figure, the cross-sectional area may be increased to provide a certain amount of capacity. However, you can still get the resonance effect.

この吸気装置におりる」二記名独Xア吸気通路5a〜5
rは、その慣f[同調回転数Niがエンジンの許容最高
回転数(エンジンの信頼性零の而から許容される最高回
転数)NIllaXに対してNi>Nmax   ・・
・・・・■ となるように充分短く形成されている。また、共鳴系の
最短経路による共鳴同調回転数Nrがエンジンの庄′(
容最高回転数N maXに対して0、 7NnlaX 
<N r < 1 、 2Nmax  +++++・■
と4Tるように、共鳴系を構成する部分の長さ、容量等
が設定されている。
Intake passages 5a to 5 enter this intake device.
r is the habitus [tuned rotation speed Ni is the maximum allowable engine speed (maximum allowable engine speed since engine reliability is zero) NIllaX, Ni>Nmax...
It is formed sufficiently short so that...■. In addition, the resonance tuning speed Nr due to the shortest path of the resonance system is
0, 7NnlaX for maximum rotational speed NmaX
<N r < 1, 2Nmax ++++++・■
The length, capacity, etc. of the parts that make up the resonance system are set so that 4T.

このよう41設定を、第2図に示J吸気系のモデルを参
照しつ−)説明する。独立吸気通路5a〜5fの艮ざを
ρ、この通路の断面積を1−(第2図参照)、シリンダ
容積をvm、?A速をa、クランク角で表わしIこ聞弁
明間をOとすると、独立吸気通路5a〜5[のtell
う同調回転数N1および同右振動数νは次の■、(4)
式のJ、う’;l 1.’にる。
The 41 setting will be explained with reference to the model of the J intake system shown in FIG. The size of the independent intake passages 5a to 5f is ρ, the cross-sectional area of this passage is 1- (see Fig. 2), and the cylinder volume is vm. If A speed is expressed by a, crank angle is expressed, and I is expressed by O, then the independent intake passages 5a to 5 [tell
The tuning rotation speed N1 and the tuning frequency ν are as follows (■), (4)
Formula J, u';l 1. 'Niru.

N1=−0・ ν/6   ・・・・・・■v= (a
/2π)Eワ聞〒丁四■ ・・・・・・0120式は、
慣性の同調条f1が (60/Ni )・(θ/360)=1/νとなること
から求められる。
N1=-0・ν/6 ・・・・・・■v= (a
/2π)Ewa 〒cho4■ ・・・・・・0120 type is,
It is obtained from the fact that the inertial tuning line f1 is (60/Ni)·(θ/360)=1/ν.

従って、独立吸気通路58〜5fを充分に短く形成して
おくことにより、」−20,0式から求められる慣性同
調回転数N1か、+Vj (20式の条件を14足する
程度に高くなる。
Therefore, by forming the independent intake passages 58 to 5f sufficiently short, the inertia tuning rotational speed N1 determined from the -20,0 formula can be increased to +Vj (14 times the condition of the 20 formula).

また、第2図に示1)だモデルによると各グループの独
立吸気通路5 a−5G (5d 〜5 ’l’ )お
J、び集合部6(7)とその間の連通部分とを含めた部
分く破線で囲った部分)で構成される」L鳴系の共鳴同
調回転数N r d−3J:び共鳴固有振動数νrは、
次のqD、0式のJ、うになる。
In addition, according to the model 1) shown in Fig. 2, the independent intake passages 5a-5G (5d to 5'l') and J of each group, as well as the convergence part 6 (7) and the communication part between them, are included. The resonant tuning rotational speed N r d-3J: and the resonant natural frequency νr of the L ringing system are
The next qD, J of the 0 formula, becomes.

Nr −(120/m)Xνr  ・・・・・・■vr
 −(a/4)X (1/ (Vr/F−+ l−−N
’)))・・・・・■ m:1グループの気筒数 a:音速 Vr:1グループの独立吸気通路と集合部(第2図中の
斜線部分)の容部 1:二集合部間の連通部分の平均断面積[−二十記連通
部分の中点」、C′の長さ1〕:上記連通部分の平均直
径(管端補正)つまり、共鳴系の等価長が近似的に(V
r /F+L+1つ)となり、かつ、上記連通部分の中
点では圧力波の11−負が反転して反射されると考えら
れるので圧力波の2往復分が1周期と相当することから
、共鳴固有振動数vrが近似的に120式で求められる
。また、各グルー1毎にエンジンの2回転で1グループ
の気筒数m fご(J吸気を行なう関係で、1秒当り吸
入回数と固イ9振動数vrとが−・致するときの回転数
である共鳴同調回転数Nrは上記0式で求められる。
Nr − (120/m)Xνr ・・・・・・■vr
-(a/4)X (1/ (Vr/F-+ l--N
')))...■ m: Number of cylinders in 1 group a: Sound velocity Vr: Capacity between independent intake passages in 1 group and the collecting part (shaded area in Figure 2) 1: Between the two collecting parts Average cross-sectional area of the communicating part [-20 midpoint of the communicating part'', length C' 1]: Average diameter of the communicating part (tube end correction), that is, the equivalent length of the resonant system is approximately (V
r/F+L+1), and since it is thought that the 11-negative part of the pressure wave is inverted and reflected at the midpoint of the above-mentioned communication part, two round trips of the pressure wave correspond to one cycle, so the resonance characteristic The vibration frequency vr can be approximately determined by formula 120. In addition, for each glue 1, the number of cylinders in one group m f is determined by two revolutions of the engine. The resonance tuning rotation speed Nr is determined by the above equation 0.

このように、上記容量Vr、十記平均断面積ト、」二記
長さ1−および上記平均直径1つ等の共鳴系の諸元によ
り共鳴同調回転数Nrか定まる。そこで、jt鳴系の最
りク経路ににる場合の共鳴同調回転数Nrが前記0式の
範囲とイfるJ、う(ご共鳴系の諸元が設定され、例え
ば第1図に示した構造においT CAL、共鳴系を構成
する各独立吸気通路58〜5「、集合部6,7、通路8
,9、手法側連通路11等の諸元がL記のように設定さ
れる。
In this way, the resonance tuning rotation speed Nr is determined by the specifications of the resonance system, such as the capacitance Vr, the average cross-sectional area, the length 1-, and the average diameter. Therefore, if the resonant tuning rotation speed Nr when the jt ringing system is on the highest path is within the range of the above equation 0, then the specifications of the resonant system are set, for example as shown in Fig. In the structure, each independent intake passage 58 to 5', convergence part 6, 7, passage 8 constituting a resonance system
, 9, the specifications of the method side communication path 11, etc. are set as shown in L.

このJ、うな吸気装置によると、吸気系を吸気順序が連
続しない気筒同士を同一グルー1とづ°る2つのグルー
プにわけて共鳴系を構成していることにより、その各グ
ループにおいてそれぞれ、各気筒の作動により生じる圧
力波が独立吸気通路58〜5c、5d〜5fから集合部
6,7i15よび集合部6,7間の連通部分にわたって
伝播し、これらの共鳴系を構成づ−る部分に圧力振動が
生じる。そして、共鳴固有振動数νrが各グループ16
の吸入回数と合致づ−るとき、同一・グループの各気筒
に生じる1i力波が共振し、バカ振動が最も強められる
状態どなる。この状態となる共鳴同調回転数N「付近の
回転数域で共鳴効果による過給作用か得られ、エンジン
出力が高められる。
According to this J, Eel intake system, the resonance system is constructed by dividing the intake system into two groups in which cylinders whose intake order is not consecutive are assigned the same group 1. Pressure waves generated by cylinder operation propagate from the independent intake passages 58 to 5c, 5d to 5f to the collecting portions 6 and 7i15 and the communication portion between the collecting portions 6 and 7, and pressure is applied to the parts that constitute these resonance systems. Vibration occurs. Then, the resonance natural frequency νr is 16 for each group.
When the number of intakes matches the number of intakes, the 1i force wave generated in each cylinder of the same group resonates, and the state where the stupid vibration is strongest is reached. In this state, a supercharging effect due to the resonance effect is obtained in the rotation speed range near the resonance tuned rotation speed N, and the engine output is increased.

どくに、共鳴系の最短経路にJ、るJ(鳴同調回転数N
rをエンジンの許容最高回転数Nmaxに対して前記0
式の範囲に設定していることにより、上記許容最高回転
数Nmax(;j近の高速域で共鳴過給作用によりエン
ジン出力が高められる。このような効果を第33図にJ
、り説明する。
Dokuni, the shortest path of the resonance system is J, RuJ (sound tuning rotation speed N
r to the maximum allowable rotation speed Nmax of the engine.
By setting within the range of the formula, the engine output can be increased by resonance supercharging in the high speed range near the maximum allowable rotation speed Nmax (;j.
, I will explain.

第3図は、第1図に小したような構造において上記共鳴
同調回転数Nrを神々の(ll′1に設定した場合の1
〕ンジン出力トルクの特性(A1・〜A5)を、共pJ
4効果をイJしない揚台の狛↑(1(線B)と比較して
示す。この図において、線へ1は共鳴同調回転数Nrを
エンジンの九′1容最高回転数N maxとした場合の
特性ひあり、この場合は上記許容最高回転数N max
で゛土ンジン出力!−ルクかピークと41す、イの付近
の高速域で出力1−ルクが高められる。また、[0,7
Nmax<Nr <1.2Nmax lの範囲であれば
共鳴同調回転数N1・が上記許容最高回転数N max
がらずれた揚台(線△2 、 A3 )でも、」二記お
合最高回転数Nmax付近におい−C1エンジン出力ト
ルクかピークJ、りは低小づるものの共鳴効果を有しな
い場合より充分に高くなる。ところが、上記範囲にすb
低速側に人さく共鳴同調回転−’+3− 数Nrがずれるど、十記V1容最高回転数N旧+x(,
1近にお(〕る]ニンジン出力1〜ルクが共鳴効果を有
しない場合J、り低下して逆効果となり(線△4)、ま
た[記範囲よりも高速側に大きく」を鳴同調回転数N「
が”す゛れると、上記許容厄へ回転数Nmax以下では
エンジン出力1〜ルクか共鳴効果を右しない揚台どほど
lυど変りが1.rりなる(線△5)。従って、共鳴同
調回転数NrがP記範囲内となる。J:うに設定してお
くことにより、11容最高回転数Nm2+×付近の高速
域でエンジン出力1〜ルクが高められることとなる。
Figure 3 shows a structure similar to that shown in Figure 1 when the resonance tuning rotation speed Nr is set to the divine value (ll'1).
] Characteristics of engine output torque (A1・~A5), both pJ
4 effects are shown in comparison with ↑ (1 (line B)) of a lifting platform that does not have an impact. In this figure, line 1 is the resonance tuning rotation speed Nr, which is the engine's maximum rotation speed N max. In this case, the maximum allowable rotation speed N max
Soil engine output! The output power is increased by 1-lux in the high-speed range near the 41st and 41st peaks. Also, [0,7
If Nmax < Nr < 1.2Nmax l, the resonance tuning rotation speed N1 is the above-mentioned maximum allowable rotation speed N max
Even if the platform is shifted (lines △2, A3), the peak J of the C1 engine output torque near the maximum rotational speed Nmax is still low and small, but it is sufficiently higher than when there is no resonance effect. Become. However, within the above range
Resonant synchronized rotation on the low speed side -'+3- Although the number Nr is off, the maximum rotation speed N old + x (,
If the carrot output 1 to 1 near 1 does not have a resonance effect, J will decrease and have the opposite effect (line △4), and the resonance synchronized rotation will be [greater on the high speed side than the stated range]. Number N"
When the above-mentioned allowable rotation speed is below Nmax, the difference in engine output from 1 to 100 kW or lυ, which does not affect the resonance effect, becomes 1.r (line △5). Therefore, the resonance tuning speed Nr is within the range specified by P. By setting J: to 1, the engine output 1 to 1 torque is increased in the high speed range near the maximum rotational speed Nm2+x.

この場合に、独立吸気通路58〜5tによる慣性同調回
転数Niを前記0式のように設定しでJ3くことにより
、この慣性同調回転数N1に支配されることなく共鳴同
調回転数N rを充分に高めることができ、かつ、この
ように独立吸気通路5a・〜51゛を知くJることによ
り、集合部6,7間の連通部分にある程度の長さを持l
こUつつ」を鳴同調回転数NrをF記範囲まで高めるこ
とができて、吸気系を2グループに分()たことの効架
が損われず、イ」効に高速j或での共鳴効果を持たせる
ことかできる1、 また、前述のように下流側連通路11(こ開閉弁15を
設(プてその開閉により共鳴固有振動数が変化するJ、
うにしでお(Jぽ、異(’Lる回転数域でそれぞれ共鳴
効果を持たせることができる。
In this case, by setting the inertia-tuned rotation speed Ni by the independent intake passages 58 to 5t as in the above equation 0, the resonance-tuned rotation speed Nr can be set without being controlled by the inertia-tuned rotation speed N1. By knowing the independent intake passages 5a to 51' in this way, it is possible to have a certain length in the communicating part between the gathering parts 6 and 7.
It is possible to increase the synchronized rotational speed Nr to the range specified by F, and the effectiveness of dividing the intake system into two groups is not impaired, and resonance at high speeds is effectively achieved. In addition, as mentioned above, the downstream side communication passage 11 (the on-off valve 15 is installed), and the resonant natural frequency changes depending on the opening and closing of the downstream communication passage 11.
It is possible to create resonance effects in different rotation speed ranges.

なお、本発明の装置の具体的椙造は上記実施例には限定
されず、種々変史1月能であって、その数例を第4図乃
↑第7図に示づ。
Note that the specific construction of the device of the present invention is not limited to the above-mentioned embodiments, but can be implemented in various ways, some examples of which are shown in FIGS. 4 to 7.

第4図に示づ一実施例では、V型6気筒Tンジンの一方
のバンク1側の各独9吸気通路58〜50および他方の
バンク2側の各独立吸気通路56〜51がそれぞれ集合
され、その各集合部16,17の一端側に接続され7ζ
通路18.19が1流端側て連通されてこの部分に供給
吸気通路10か接続されるとともに、F記通路18.1
9のJT流端側連通箇所J、リム土浦(こ、内通路18
.19を連通ずる連通部21が設置Jられている。この
連通部21には、エンジン回転数tこ応して開閉する開
閉弁22が設【ブられ−Cいる。また、上記通路18゜
−11)  〜 19の連通部21 、J:すF流側部分は断面積が大き
くされている。
In one embodiment shown in FIG. 4, nine intake passages 58 to 50 on one bank 1 side of a V-type six-cylinder T-engine and each independent intake passages 56 to 51 on the other bank 2 side are assembled together. , connected to one end side of each of the collecting parts 16 and 17, and 7ζ
The passage 18.19 is communicated with the first flow end side and the supply intake passage 10 is connected to this part, and the F passage 18.1
9 JT flow end side communication point J, rim Tsuchiura (inner passage 18
.. 19 is installed. This communication portion 21 is provided with an on-off valve 22 that opens and closes in response to the engine speed t. Further, the communication portions 21, J:F flow side portions of the passages 18°-11) to 19 have a large cross-sectional area.

口の実施例でも、各独立吸気通路5 a□ 51’ L
こよる慣性同調回転数Niを面記■式のように設定する
ととらに、連通部21庖通る最短経路による共鳴同調回
転数(開閉弁22が開かれた状態での共鳴同調回転数)
Nrを前記0式のJ、うに設定りることにより、第1図
に示した実施例と同様に高速域で共鳴過給作用が得られ
る。この場合、前記0式中の平均断面積Fが大きくなれ
ば共鳴固有振動数ν「が高くなるので、上記連通部21
より下流側の通路断面積を大きくしておくこと(こより
、集合部間の連通部分にある程度の長さを持たせて、吸
気系を2グループに分(ブたことの効果が損われないJ
、うにしつ゛つ、有効(こ高速域での共鳴効果を持たせ
ることができる。
In the embodiment of the mouth, each independent intake passage 5a□51'L
In addition to setting the inertia-tuned rotation speed Ni as shown in the formula (2), the resonance-tuned rotation speed (resonance-tuned rotation speed when the on-off valve 22 is open) due to the shortest path passing through the communication portion 21 is set.
By setting Nr to J in the above-mentioned formula 0, a resonant supercharging effect can be obtained in the high speed range, similar to the embodiment shown in FIG. In this case, as the average cross-sectional area F in the formula 0 increases, the resonance natural frequency ν' increases, so the communication portion 21
The cross-sectional area of the passage on the downstream side should be made larger (this allows the communication part between the gathering parts to have a certain length, and the intake system should be divided into two groups (J
, while still being effective (this allows for a resonance effect in the high-speed range).

第5)図はV型4気筒J−ンジンに適用した場合の実施
例を示す。この場合し、−hのバンク31の気筒33a
、33b同1、および他方のバンク32の気筒33c、
33d同tは、それぞれ吸気類序が連続しないので、吸
気系を一方のバンク31側のグループと他方のバンクご
32側のグループとに分+′lJ’c、各グループ毎に
独1ア吸気通路35a。
Figure 5) shows an embodiment in which the present invention is applied to a V-type 4-cylinder J-engine. In this case, -h cylinder 33a of bank 31
, 33b same 1, and cylinder 33c of the other bank 32,
In 33d and t, the intake system is not consecutive, so the intake system is divided into one bank 31 side group and the other bank 32 side group+'lJ'c, and 1A intake for each group. Passageway 35a.

35 bおよび35G、35dを集合させるとともに、
集合部36.37.通路38,39、共通吸気通路40
、下流側連通路41、開閉弁45等を第1図の実施例と
同様に構成している。あるいは、第2図の実施例と同様
(J共鳴系を構成し”(’ d3いてしよい。
While collecting 35 b, 35G, and 35d,
Gathering section 36.37. Passages 38, 39, common intake passage 40
, the downstream side communication passage 41, the on-off valve 45, etc. are constructed in the same manner as in the embodiment shown in FIG. Alternatively, a J resonance system may be configured as in the embodiment shown in FIG.

また、第6図に示づ実施例では、一方のバンク1側と他
方のバンク2側とに分けられた各グループIOの集合部
56.57にそれぞれ通路58,59が接続されて、そ
の」7流端側連通箇所に共通吸気通路60が接続される
とともに、上記各通路558.59の途中箇1ダ1から
それぞれ分岐しlζ通路状部分61 、62が設けられ
ている。この通路状部分61.62の先端は閉塞端とな
っている。
Furthermore, in the embodiment shown in FIG. 6, passages 58 and 59 are respectively connected to the gathering parts 56 and 57 of each group IO divided into one bank 1 side and the other bank 2 side. A common intake passage 60 is connected to the communication point on the flow end side of each of the passages 558 and 59, and passage-like portions 61 and 62 are provided which branch off from the midpoint of each of the passages 558 and 59, respectively. The ends of the passage-like portions 61, 62 are closed ends.

この実施例によると、上記通路状部分61.62が共鳴
系の−・部としてJt鳴固有振動数vl゛に関係゛りる
のて゛、この通路状部分6’l、62によっても共鳴同
調回転数Nrを調整できる。そしてこの場合も、前記■
、■式を満足するように独立吸気通路5 a−5) f
および共鳴系を設定しておくことに、J:す、許容最高
回転数Nn1ax付近の高速域で有効に共鳴過給作用が
得られる。
According to this embodiment, since the passage-like portions 61 and 62 are related to the natural frequency vl of the Jt sound as a part of the resonance system, the passage-like portions 6'l and 62 also contribute to the resonant tuning rotational speed. Nr can be adjusted. And in this case too, the above ■
, the independent intake passage 5 a-5) f so as to satisfy the formula
By setting up a resonance system, resonance supercharging can be effectively obtained in the high speed range near the maximum allowable rotation speed Nn1ax.

第7図は直列4気筒■ンシンに適用した場合を示づ1.
この場合は、吸気%l′l序が連続しない1番気筒73
aと4番気筒73dとが第1グループ、2番気筒73b
と3番気筒73Gとが第2グループとされ、これらのグ
ループ毎に、各独1′J吸気通路75a、75dおよび
75b、75Gがそれぞれ集合されて、その各集合部7
6.77に接続された通路78.79の上流端側連通箇
所に共通吸気通路80が接続されている3、そして、こ
の場合し前記の各種実施例に埠じて高速域で1し鳴過給
!I II+が得られるようなg pi系が構成され、
例えば、通路78.79からそれぞれ分岐した通路状部
分ε3コ、82が設置Jられる。この通路状部分81.
82は第6図の実施例のような右端状でもJ、いが、こ
の図の、J:うに通路状部分81.82をUいに連通さ
せて、連通部分に開閉弁83を設置づ、その開閉にJ、
って共鳴固有振動数が変えられるようにしておいてらよ
い。独立吸気通路73 a〜73fおJζび共鳴系が前
記■、■式を満足するように設定されることは他の実施
例と同様である。
Figure 7 shows the case where it is applied to an in-line four-cylinder engine.1.
In this case, the number 1 cylinder 73 whose intake %l'l order is not consecutive
a and the fourth cylinder 73d are in the first group, and the second cylinder 73b
and No. 3 cylinder 73G are set as a second group, and each of the 1'J intake passages 75a, 75d and 75b, 75G are collected in each group, and each collecting portion 7
A common intake passage 80 is connected to the upstream end communication point of the passage 78 and 79 connected to the passage 78 and 77. Salary! A g pi system is constructed such that I II+ is obtained,
For example, passage-like portions ε3 and 82 branching from the passages 78 and 79, respectively, are installed. This passage-like portion 81.
82 may have a right end shape like the embodiment shown in FIG. J to open and close it,
It would be better to make it possible to change the resonance natural frequency. As in the other embodiments, the independent intake passages 73a to 73f and the resonance system are set to satisfy equations (1) and (2) above.

〔発明の効果〕〔Effect of the invention〕

以上のように本発明は、吸気順序が連続しない気筒同士
を同一グループとする各グループ毎に気筒別の独立吸気
通路を各々集合ざして、これらと各集合部に連4【る通
路部分とで共鳴系を構成するとともに、−上記独立吸気
通路による慣性同調回転数N1J5よび上記共鳴系の最
短経路による共鳴同調回転数Nrをそれぞれエンジンの
n容最高回転数Nmaxに対して Ni>Nmax Q、7Nmax <Nr〆:l、 2Nmaxとなるよ
うに設定しているlこめ、気筒別の各独立吸気通路が充
分に知くなって吸気系を一コンパクト化りることがでさ
、かつ、]ンジンのSKI容同転数付近の高速域で右グ
Jに11、鳴効宋が1111〜)れて■ンジン出力を高
めることができるノ〕のである。
As described above, the present invention collects independent intake passages for each cylinder for each group in which cylinders whose intake order is not consecutive are grouped into the same group, and connects these and the passage portions connected to each collection part. A resonance system is configured, and - the inertial tuning rotation speed N1J5 due to the independent intake passage and the resonance tuning rotation speed Nr due to the shortest path of the resonance system are respectively Ni>Nmax Q, 7Nmax with respect to the maximum rotation speed Nmax of the engine. <Nr〆:l, 2Nmax is set so that the independent intake passages for each cylinder can be fully understood and the intake system can be made more compact, and the engine's In the high-speed range near the SKI rotary speed, the engine output can be increased by increasing the right gear J (11, Ningei Song (1111~)).

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

第1図は本発明の一実施例を示す吸気装置6概略図、第
2図は独立吸気通路おにび共鳴系の設定条件を説明する
ため吸気装置をモデル化して示す説明図、第33図は共
鳴同調回転数を種々変えた場合の1ニンジン出力トルク
の特性図、第4図乃至第7図【j、それぞれ別の実施例
を示す吸気装置概略図である。 3 a−3f 、 33 a 〜33 d、 73 a
 〜73 d・・・気筒、5a 〜りI’、35a〜3
5d、75a〜75d・・・独立吸気通路、6.7.1
6,17,36.37,56,57.76.77・・・
集合部、8.9.11.18.19.21.38,39
.41゜58.59,61,62,78.79.81.
82・・・集合部に連なる通路部分。
FIG. 1 is a schematic diagram of an intake device 6 showing an embodiment of the present invention, FIG. 2 is an explanatory diagram showing a model of the intake device to explain the setting conditions of the independent intake passage and resonance system, and FIG. 33 7A and 7B are characteristic diagrams of one carrot output torque when the resonance tuning rotational speed is variously changed, and FIGS. 4 to 7 [j] are schematic diagrams of intake devices showing different embodiments. 3 a-3f, 33 a to 33 d, 73 a
~73 d...Cylinder, 5a ~riI', 35a~3
5d, 75a to 75d...Independent intake passage, 6.7.1
6, 17, 36.37, 56, 57.76.77...
Gathering part, 8.9.11.18.19.21.38,39
.. 41°58.59, 61, 62, 78.79.81.
82...A passageway connected to the gathering area.

Claims (1)

【特許請求の範囲】 1、エンジンの吸気系を吸気順序が連続しない気筒同士
を同一グループとする複数のグループに分けて、気筒別
の独立吸気通路を各グループ毎に各々集合させ、上記各
グループの独立吸気通路および集合部と各集合部に連な
る通路部分とで各グループに対する共鳴系を構成すると
ともに、上記独立吸気通路を、この通路による慣性同調
回転数がエンジンの許容最高回転数より高くなるように
設定し、かつ、上記共鳴系を、その最短経路による共鳴
同調回転数Nrがエンジンの許容最高回転数Nmaxに
対して 0.7Nmax<Nr<1.2Nmax となるように設定したことを特徴とするエンジンの吸気
装置。
[Scope of Claims] 1. The intake system of the engine is divided into a plurality of groups in which cylinders whose intake order is not consecutive are grouped into the same group, and the independent intake passages for each cylinder are assembled in each group, and each of the above groups The independent intake passages and the collecting parts and the passage parts connected to each collecting part constitute a resonance system for each group, and the independent intake passages have an inertial tuned rotation speed that is higher than the maximum allowable rotation speed of the engine. and the resonance system is set so that the resonance tuning speed Nr of the shortest path satisfies 0.7Nmax<Nr<1.2Nmax with respect to the maximum allowable engine speed Nmax. The intake system of the engine.
JP63109412A 1988-05-02 1988-05-02 Engine intake system Expired - Fee Related JP2771175B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63109412A JP2771175B2 (en) 1988-05-02 1988-05-02 Engine intake system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63109412A JP2771175B2 (en) 1988-05-02 1988-05-02 Engine intake system

Publications (2)

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JPH01280632A true JPH01280632A (en) 1989-11-10
JP2771175B2 JP2771175B2 (en) 1998-07-02

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JP63109412A Expired - Fee Related JP2771175B2 (en) 1988-05-02 1988-05-02 Engine intake system

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Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57148024A (en) * 1981-03-11 1982-09-13 Hino Motors Ltd Intake and exhaust for diesel engine
JPS57153924A (en) * 1981-03-20 1982-09-22 Hino Motors Ltd Inertia supercharging intake manifold in internal combustion engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57148024A (en) * 1981-03-11 1982-09-13 Hino Motors Ltd Intake and exhaust for diesel engine
JPS57153924A (en) * 1981-03-20 1982-09-22 Hino Motors Ltd Inertia supercharging intake manifold in internal combustion engine

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