JPH0452373B2 - - Google Patents
Info
- Publication number
- JPH0452373B2 JPH0452373B2 JP57190616A JP19061682A JPH0452373B2 JP H0452373 B2 JPH0452373 B2 JP H0452373B2 JP 57190616 A JP57190616 A JP 57190616A JP 19061682 A JP19061682 A JP 19061682A JP H0452373 B2 JPH0452373 B2 JP H0452373B2
- Authority
- JP
- Japan
- Prior art keywords
- intake
- passage
- load
- cylinder
- low
- 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 - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B27/00—Use 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
- F02B27/005—Oscillating pipes with charging achieved by arrangement, dimensions or shapes of intakes pipes or chambers; Ram air pipes
- F02B27/006—Oscillating pipes with charging achieved by arrangement, dimensions or shapes of intakes pipes or chambers; Ram air pipes of intake runners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/10006—Air intakes; Induction systems characterised by the position of elements of the air intake system in direction of the air intake flow, i.e. between ambient air inlet and supply to the combustion chamber
- F02M35/10026—Plenum chambers
- F02M35/10045—Multiple plenum chambers; Plenum chambers having inner separation walls
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/104—Intake manifolds
- F02M35/108—Intake manifolds with primary and secondary intake passages
- F02M35/1085—Intake manifolds with primary and secondary intake passages the combustion chamber having multiple intake valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/104—Intake manifolds
- F02M35/112—Intake manifolds for engines with cylinders all in one line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/10—Air intakes; Induction systems
- F02M35/104—Intake manifolds
- F02M35/116—Intake manifolds for engines with cylinders in V-arrangement or arranged oppositely relative to the main shaft
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Characterised By The Charging Evacuation (AREA)
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は、エンジンの吸気装置に関し、特に低
負荷用と高負荷用との2系統の独立した吸気通路
を備えた多気筒エンジンにおいて吸気通路内に発
生する吸気圧力波を利用してエンジン高負荷高回
転時に過給効果を得るようにしたものに関する。DETAILED DESCRIPTION OF THE INVENTION (Industrial Application Field) The present invention relates to an intake system for an engine, and particularly to an intake passage in a multi-cylinder engine equipped with two independent intake passages, one for low load and one for high load. This relates to a device that uses intake pressure waves generated within the engine to obtain a supercharging effect when the engine is under high load and high rotation speed.
(従来の技術)
一般に、多気筒エンジンにおいて、各気筒へ独
立して開口する2系統の低負荷用吸気通路と高負
荷用吸気通路とを有する吸気通路を備え、該吸気
通路は、少なくとも低負荷用吸気通路を流れる吸
気量を変化させる1次弁と、高負荷用吸気通路を
流れる吸気量を変化させる2次弁とを有してお
り、エンジンの低負荷時には、上記1次弁のみを
開作動して通路面積の狭い低負荷用吸気通路のみ
から吸気を各気筒に供給することにより、吸気流
速を速めて燃焼安定性を向上させる一方、エンジ
ンの高負荷時には、上記2次弁をも開作動して高
負荷用吸気通路からも吸気の供給を行うことによ
り、充填効率を高めて出力向上を図るようにし
た、いわゆるデユアルインダクシヨン方式の吸気
システムはよく知られている。(Prior Art) Generally, a multi-cylinder engine is provided with an intake passage having two systems, a low-load intake passage and a high-load intake passage, which open independently to each cylinder, and the intake passage has at least a low-load intake passage. It has a primary valve that changes the amount of intake air flowing through the intake passage for normal use, and a secondary valve that changes the amount of intake air that flows through the intake passage for high loads.When the engine is under low load, only the primary valve is opened. By supplying intake air to each cylinder only from the low-load intake passage, which has a narrow passage area, it increases the intake flow rate and improves combustion stability.At the same time, when the engine is under high load, the secondary valve is also opened. A so-called dual-induction type intake system is well known, in which intake air is supplied from a high-load intake passage as well, thereby increasing filling efficiency and increasing output.
ところで、従来、エンジンの充填効率向上、出
力向上を図るべく吸気通路に過給機を設けて吸気
を過給する技術はよく知られているが、過給機装
備のため、構造が大がかりとなるとともにコスト
アツプとなる嫌いがあつた。 By the way, the technology of supercharging the intake air by installing a supercharger in the intake passage in order to improve the filling efficiency and output of the engine is well known, but since it is equipped with a supercharger, the structure is large-scale. At the same time, there was a dislike of increasing costs.
また、従来、エンジンの吸気通路内に発生する
吸気圧力波により過給効果を得る技術として、実
公昭45−2321号公報に開示されているように、単
一気筒エンジンにおいて、吸気管を寸法の異なる
2本の通路に分け、かつそれぞれ別の吸気ポート
を有し、エンジン高回転時は2本の吸気通路を用
い、低回転時には閉塞位置の遅い方の吸気通路を
閉止し吸気を早目に閉塞することにより、吸気管
の寸法やエンジン回転数の関数である吸気の最大
圧力時点での吸気の閉塞による過給作用を利用し
て広範囲のエンジン回転域に亘つて好適な充填効
率を得るようにしたものが提案されている。 In addition, as disclosed in Japanese Utility Model Publication No. 45-2321, a technique for obtaining a supercharging effect using intake pressure waves generated in the intake passage of an engine has conventionally been used in a single-cylinder engine to reduce the size of the intake pipe. Divided into two different passages, each with a separate intake port, the two intake passages are used when the engine is running at high speeds, and at low engine speeds, the intake passage that is at the later closing position is closed, allowing for early intake. By occluding the intake air, it is possible to obtain suitable charging efficiency over a wide range of engine speeds by utilizing the supercharging effect caused by the occlusion of the intake air at the maximum pressure of the intake air, which is a function of the intake pipe dimensions and engine speed. It has been proposed that
(発明が解決しようとする課題)
しかし、このものは、単一気筒のエンジンに対
するものであつて、吸気通路内に発生する吸気圧
力波をどのように利用するのか、その構成、作用
が定かでなく、直ちに実用に供し得ないものであ
つた。(Problem to be solved by the invention) However, this device is for a single-cylinder engine, and its structure and operation are unclear, such as how to utilize the intake pressure waves generated in the intake passage. Therefore, it could not be put into practical use immediately.
そこで、本発明者等は、エンジンの吸気特性を
検討するに、
(i) 吸気ポート開口時には燃焼室の残留排気ガス
の圧力によつて吸気が圧縮され、吸気通路内の
吸気ポート部分に圧縮波が発生しており、この
開口時圧縮波は、近年の市販車では騒音低減や
排気ガス浄化のためにエンジン排圧が高くなつ
ていることから特に強く発生すること、
(ii) 吸気ポート閉口時には吸気の慣性により吸気
が圧縮されて吸気通路内の吸気ポート部分に圧
縮波が発生すること、
(iii) 吸気ポートの吸気開始により吸気通路内に膨
張波が発生すること、
を知見した。 Therefore, when examining the intake characteristics of the engine, the present inventors found that (i) When the intake port is opened, the intake air is compressed by the pressure of the residual exhaust gas in the combustion chamber, and a compression wave is generated at the intake port part in the intake passage. This compression wave is generated particularly strongly when the intake port is closed because the engine exhaust pressure has been increased in recent commercial vehicles to reduce noise and purify exhaust gas. (ii) When the intake port is closed, We found that the inertia of the intake air compresses the intake air, generating compression waves in the intake port portion of the intake passage, and (iii) that the start of intake at the intake port generates expansion waves in the intake passage.
このことから、本発明は、上記の如き2系統の
独立した吸気通路を備えた多気筒エンジンにおい
て、一つの気筒での上記(i)の開口時圧縮波を他気
筒の特に吸気の吹き返しが生じる吸気行程終期に
作用せしめれば効果的に過給効果が得られること
(以下、排気干渉効果という)、一つの気筒での上
記(ii)の閉口時圧縮波を他気筒の同じく吸気行程終
期に作用せしめれば効果的に過給効果が得られる
こと(以下、吸気慣性効果という)及び各気筒で
の上記(iii)の膨張波を圧縮波に反転して該各気筒の
同じく吸気行程終期に作用せしめれば効果的に過
給効果が得られること(以下、吸気個有脈動効果
という)に着目し、上記気筒間干渉効果(排気干
渉効果及び吸気慣性効果)及び各気筒の吸気個有
脈動効果を利用することによつてエンジンの充填
効率向上を意図するものである。 Therefore, in a multi-cylinder engine equipped with two independent intake passages as described above, the present invention is capable of converting the compression wave (i) in one cylinder upon opening into other cylinders, in particular, causing intake air to blow back. If the supercharging effect is applied at the end of the intake stroke, the supercharging effect can be effectively obtained (hereinafter referred to as the exhaust interference effect). If activated, a supercharging effect can be effectively obtained (hereinafter referred to as intake inertia effect), and the expansion wave in (iii) above in each cylinder is reversed into a compression wave, which is also applied at the end of the intake stroke of each cylinder. Focusing on the fact that the supercharging effect can be effectively obtained if the supercharging effect is activated (hereinafter referred to as the intake individual pulsation effect), we have focused on the above-mentioned inter-cylinder interference effect (exhaust interference effect and intake inertia effect) and the intake individual pulsation of each cylinder. By utilizing this effect, it is intended to improve engine filling efficiency.
すなわち、本発明の目的は、上記の如き2系統
の吸気通路を備えた多気筒エンジンの吸気系を、
高出力を要するエンジン高負荷高回転時に少なく
とも一方の吸気系統において上記の如く一つの気
筒の吸気ポートに特に強く生じる開口時圧縮波を
吸気行程終期にある他気筒に有効に伝播させて気
筒間干渉としての排気干渉効果により効果的に過
給効果を得るように設定するとともに、各気筒の
吸気系に膨張波を圧縮波に反転する拡大室を設け
て、双方の吸気系統において同じ高回転域で上記
吸気個有脈動効果による過給効果をも併せ得るよ
うにすることにより、過給機等を用いることなく
既存の吸気系の僅かな設計変更による簡単な構成
でもつてエンジン高負荷高回転時の充填効率を高
めて出力向上を有効に図らんとするものである。 That is, an object of the present invention is to provide an intake system for a multi-cylinder engine having two intake passages as described above.
During high-load, high-speed engines that require high output, the opening compression wave that occurs particularly strongly at the intake port of one cylinder as described above in at least one intake system is effectively propagated to other cylinders at the end of the intake stroke, resulting in inter-cylinder interference. In addition to setting it to effectively obtain a supercharging effect by using the exhaust interference effect as By making it possible to obtain the supercharging effect due to the above-mentioned intake air pulsation effect, it is possible to operate the engine at high loads and high speeds with a simple configuration by making slight design changes to the existing intake system without using a supercharger etc. This aims to effectively improve output by increasing filling efficiency.
(課題を解決するための手段)
この目的を達成するため、本発明の解決手段
は、各気筒毎に互いに独立した低負荷用吸気通路
と高負荷用吸気通路とを有するとともに該各気筒
の低負荷用吸気通路と高負荷用吸気通路とを各気
筒の燃焼室に吸気ポートを介して開口させた吸気
通路を備え、該吸気通路は、少なくとも上記低負
荷用吸気通路を流れる吸気量を変化させる1次弁
と、上記高負荷用吸気通路を流れる吸気量を変化
させる2次弁とを有するエンジンの吸気装置を前
提とする。そして、上記1次弁及び2次弁の下流
において上記各気筒の低負荷用吸気通路同士及び
高負荷用吸気通路同士を連通するそれぞれ各吸気
通路の最小通路断面積以上の通路断面積の連通路
を有する拡大室を設ける。上記連通路を介しての
各気筒間の低負荷用吸気通路及び高負荷用吸気通
路の通路長さを、少なくとも一方が5000〜
7000rpmのエンジン高回転時、一つの気筒の吸気
ポートの開口時に生じる圧縮波が吸気行程終期に
ある他の気筒の吸気ポートに伝播して過給を行う
ように設定する。また、上記拡大室から各気筒の
吸気ポートに至る上記低負荷用吸気通路及び高負
荷用吸気通路の通路長さlP,lSを、双方が5000〜
7000rpmのエンジンの高回転時、各気筒の吸気ポ
ートの吸気開始により生じる膨張波を上記拡大室
で反転して反射した圧縮波の2次脈動波が該各気
筒の吸気行程終期の吸気ポートに伝播して過給を
行うように、下記式
lP=(θP−θ2)×(60/360N)
×(1/4)×a
lS=(θS−θ2)×(60/360N)
×(1/4)×a
(ここで、θP及びθSは各吸気ポートの開口期
間、θ2は各吸気ポートの開口から膨張波が実質的
に発生するまでの期間と効果的に過給を行うため
に該膨張波を反転した圧縮波の2次脈動波が伝播
される各吸気ポートの閉口直前の時期から閉口ま
での期間とを合算した無効期間、Nはエンジン回
転数、aは圧力波の伝播速度である)により設定
したものとする。(Means for Solving the Problem) In order to achieve this object, the solving means of the present invention has a low-load intake passage and a high-load intake passage independent of each other for each cylinder, and a low-load intake passage for each cylinder. An intake passage is provided in which a load intake passage and a high load intake passage are opened to the combustion chamber of each cylinder via an intake port, and the intake passage changes at least the amount of intake air flowing through the low load intake passage. The present invention is based on an engine intake system having a primary valve and a secondary valve that changes the amount of intake air flowing through the high-load intake passage. and a communication passage having a passage cross-sectional area equal to or greater than the minimum passage cross-sectional area of each intake passage, which communicates the low-load intake passages and the high-load intake passages of each cylinder downstream of the primary valve and the secondary valve. Provide an expansion room with a The passage length of the low-load intake passage and the high-load intake passage between each cylinder via the above-mentioned communication passage is set to 5000 to 5000 for at least one of them.
When the engine rotates at a high speed of 7,000 rpm, the compression wave generated when the intake port of one cylinder opens will propagate to the intake ports of other cylinders at the end of the intake stroke to perform supercharging. In addition, the passage lengths l P and l S of the low load intake passage and the high load intake passage from the enlarged chamber to the intake port of each cylinder are both 5000~
When the engine rotates at a high speed of 7000 rpm, the expansion wave generated by the start of intake at the intake port of each cylinder is reversed and reflected in the expansion chamber, and the secondary pulsating wave of the compression wave propagates to the intake port of each cylinder at the end of the intake stroke. The following formula l P = (θ P - θ 2 ) x (60/360N) x (1/4) x a l S = (θ S - θ 2 ) x (60/360N) ) × (1/4) × a (where θ P and θ S are the opening periods of each intake port, and θ 2 is the period from the opening of each intake port until the expansion wave is substantially generated) N is the engine rotational speed, a is the propagation velocity of the pressure wave).
(作用)
これにより、本発明では、高出力を要する5000
〜7000rpmのエンジン高回転時には、2次弁の開
動作により低負荷用吸気通路と共に高負荷用吸気
通路も開かれて、各気筒に対し、各高負荷用吸気
通路からも各低負荷用吸気通路とは独立して吸気
の供給が行われる。その際、低負荷用及び高負荷
用の少なくとも一方の吸気系統において、一方の
気筒の吸気ポートの開口時に該吸気ポート付近に
発生した開口時圧縮波は、連通路を経て、吸気行
程終期にある他気筒の吸気ポートに伝播される。
その結果、この開口時圧縮波により、吸気が吸気
行程終期にある他気筒の吸気ポートより燃焼室内
へ押し込まれて過給が行われることになる(排気
干渉効果)。(Function) As a result, in the present invention, the 5000
At high engine speeds of ~7000rpm, the opening operation of the secondary valve opens both the low-load intake passage and the high-load intake passage. Intake air is supplied independently of the At this time, in at least one of the low-load and high-load intake systems, when the intake port of one cylinder is opened, the opening compression wave generated near the intake port passes through the communication path and is generated at the end of the intake stroke. It is propagated to the intake ports of other cylinders.
As a result, this opening compression wave forces intake air into the combustion chamber from the intake ports of other cylinders at the end of the intake stroke, resulting in supercharging (exhaust interference effect).
それと同時に、各気筒の低負荷用及び高負荷用
吸気通路の双方において、低負荷用及び高負荷用
吸気ポートからの吸気開始により低負荷用及び高
負荷用吸気通路内に発生した膨張波は、拡大室で
反転して反射した圧縮波の2次動脈波として該各
気筒の吸気行程終期の各吸気ポートに伝播されて
同じく過給が行われる(吸気個有脈動効果)。 At the same time, in both the low-load and high-load intake passages of each cylinder, expansion waves generated in the low-load and high-load intake passages due to the start of intake from the low-load and high-load intake ports, A secondary arterial wave of the compression wave that is reversed and reflected in the expansion chamber is propagated to each intake port at the end of the intake stroke of each cylinder, and supercharging is also performed (intake-specific pulsation effect).
その場合、上記各連通路は、それぞれ1次弁及
び2次弁下流に位置し、しかも該各連通路の通路
断面積をそれぞれの各吸気通路の最小通路断面積
以上としたので、上記各弁によつて圧力波が減衰
されることがなく、しかも各連通路自身の通路断
面積の拡大による圧力波減衰はあるものの、通路
断面積の縮小(絞り)による圧力波減衰と比較し
て減衰割合は少なく、よつて上記排気干渉効果を
有効に発揮できる。また、上記拡大室は、1次弁
及び2次弁の下流に位置するので、同様に吸気個
有脈動効果を有効に発揮できる。 In that case, each of the communication passages is located downstream of the primary valve and the secondary valve, respectively, and the passage cross-sectional area of each communication passage is set to be greater than or equal to the minimum passage cross-sectional area of each intake passage. Although there is pressure wave attenuation due to the expansion of the passage cross-sectional area of each communication passage itself, the attenuation rate is lower than the pressure wave attenuation due to the reduction of the passage cross-sectional area (throttling). Therefore, the above-mentioned exhaust interference effect can be effectively exhibited. Furthermore, since the enlarged chamber is located downstream of the primary valve and the secondary valve, it can similarly effectively exert the unique intake pulsation effect.
ここにおいて、上記排気干渉効果及び吸気個有
脈動効果を得るエンジン高回転時としての5000〜
7000rpmの限定は、一般に最高出力及び最高速度
がこの範囲に設定されていることから、エンジン
の高負荷高回転領域であつて高出力を要し、充填
効率向上、出力向上に有効な領域であることによ
る。 Here, 5000 ~
The limit of 7000 rpm is generally set in this range for maximum output and maximum speed, so it is a high load, high rotation area of the engine that requires high output, and is an effective area for improving charging efficiency and output. It depends.
また、上記低負荷用吸気通路と高負荷用吸気通
路とを1次弁及び2次弁の下流において独立にす
る理由は、各気筒の低負荷用及び高負荷用吸気通
路でそれぞれ発生した圧力波が他方に分散した
り、相互に干渉し合つて弱まるのを防止するため
であり、特に低負荷用吸気通路と高負荷用吸気通
路とはデユアルインダクシヨン吸気システムでの
要求の違いから吸気ポートの開閉タイミングや長
さが異なり、一方の圧力波が他方によつて減衰さ
せられることになるからである。 Furthermore, the reason why the low-load intake passage and the high-load intake passage are made independent downstream of the primary and secondary valves is that the pressure waves generated in the low-load and high-load intake passages of each cylinder are This is to prevent the intake passage from dispersing to the other or from weakening due to interference with each other.In particular, due to the difference in requirements between the low-load intake passage and the high-load intake passage in a dual induction intake system, the intake port This is because the opening/closing timing and length are different, and one pressure wave is attenuated by the other.
(実施例)
以下、本発明の実施例を図面に基づいて詳細に
説明する。(Example) Hereinafter, an example of the present invention will be described in detail based on the drawings.
第1図及び第2図はデユアルインダクシヨンタ
イプの4バルブ式2気筒4サイクルエンジンに本
発明を適用した基本構造例としての第1実施例を
示す。同図において、1A及び1Bは第1気筒及
び第2気筒であり、2は各気筒1A,1Bにおい
てシリンダ3とピストン4とで形成された燃焼室
である。 FIGS. 1 and 2 show a first embodiment as a basic structural example in which the present invention is applied to a dual induction type four-valve two-cylinder four-cycle engine. In the figure, 1A and 1B are a first cylinder and a second cylinder, and 2 is a combustion chamber formed by a cylinder 3 and a piston 4 in each cylinder 1A, 1B.
5は一端がエアクリーナ6を介して大気に開口
して各気筒1A,1Bに吸気を供給するための主
吸気通路であつて、該主吸気通路5には吸入空気
量を検出するエアフローメータ7が配設されてい
る。上記主吸気通路5はエアフローメータ7下流
において隔壁8によつて主低負荷用吸気通路9と
主高負荷用吸気通路10とに仕切られている。該
主低負荷用吸気通路9には、エンジン負荷の増大
に応じて開作動し所定負荷以上になると全開とな
つてエンジン低負荷時主低負荷用吸気通路9を流
れる吸気量を変化させる1次弁11が配設されて
いる。また、上記主高負荷用吸気通路10には、
エンジン負荷が所定負荷以上になると開作動して
エンジン高負荷時主高負荷用吸気通路10を流れ
る吸気量を変化させる2次弁12が配設されてい
る。さらに、上記主低負荷用吸気通路9は、1次
弁11下流において同形状寸法の第1及び第2低
負荷用吸気通路9a,9bに分岐されたのち各々
低負荷用吸気ポート13,13を介して各気筒1
A,1Bの燃焼室2,2に連通している。また、
上記主高負荷用吸気通路10は、2次弁12下流
において同形状寸法の第1及び第2高負荷用吸気
通路10a,10bに分岐されたのち各々高負荷
用吸気ポート14,14を介して各気筒1A,1
Bの燃焼室2,2に連通している。よつて、各気
筒1A,1Bに対して、低負荷用吸気通路9a,
9bと高負荷用吸気通路10a,10bとは1次
弁11及び2次弁12の下流において各々独立し
て燃焼室2に開口するように構成されている。 Reference numeral 5 denotes a main intake passage whose one end opens to the atmosphere via an air cleaner 6 to supply intake air to each cylinder 1A, 1B, and the main intake passage 5 is equipped with an air flow meter 7 for detecting the amount of intake air. It is arranged. The main intake passage 5 is partitioned downstream of the air flow meter 7 by a partition 8 into a main low-load intake passage 9 and a main high-load intake passage 10. The main low-load intake passage 9 has a primary valve that opens as the engine load increases, and when the load exceeds a predetermined load, opens fully to change the amount of intake air flowing through the main low-load intake passage 9 when the engine load is low. A valve 11 is provided. In addition, in the main high-load intake passage 10,
A secondary valve 12 is provided that opens when the engine load exceeds a predetermined load and changes the amount of intake air flowing through the main high-load intake passage 10 when the engine is under high load. Further, the main low-load intake passage 9 is branched downstream of the primary valve 11 into first and second low-load intake passages 9a and 9b having the same shape and dimensions, and then connected to low-load intake ports 13 and 13, respectively. Through each cylinder 1
It communicates with the combustion chambers 2, 2 of A and 1B. Also,
The main high-load intake passage 10 is branched into first and second high-load intake passages 10a and 10b having the same shape and dimensions downstream of the secondary valve 12, and then connected through high-load intake ports 14 and 14, respectively. Each cylinder 1A, 1
It communicates with the combustion chambers 2, 2 of B. Therefore, for each cylinder 1A, 1B, low load intake passage 9a,
9b and the high-load intake passages 10a and 10b are configured to open into the combustion chamber 2 independently at the downstream of the primary valve 11 and the secondary valve 12.
上記各高負荷用吸気通路10a,10bの最小
通路断面積ASは各低負荷用吸気通路9a,9b
の最小通路断面積APよりも大きく設定されてお
り(AS>AP)、高負荷用吸気通路10a,10b
による圧力波の伝播をその減衰を小さくして有効
に行い得るようにしている。 The minimum passage cross-sectional area A S of each of the above-mentioned high-load intake passages 10a, 10b is the respective low-load intake passage 9a, 9b.
The minimum passage cross-sectional area A P is set larger than the minimum passage cross-sectional area A P (A S > A P ), and the high-load intake passages 10a and 10b
This makes it possible to effectively propagate pressure waves by reducing their attenuation.
また、上記各低負荷用吸気通路9a,9b(当
然後述の連通路18より下流に位置する)の下流
端部にはそれぞれ上記エアフローメータ7の出力
に基づく吸入空気量に応じて燃料噴射量が制御さ
れる電磁弁式の燃料噴射ノズル15,15が配設
されており、燃料の良好な応答性を確保するよう
にしている。 Further, at the downstream end of each of the low-load intake passages 9a and 9b (of course located downstream of the communication passage 18 described later), a fuel injection amount is determined according to the intake air amount based on the output of the air flow meter 7. Controlled electromagnetic valve type fuel injection nozzles 15, 15 are provided to ensure good fuel response.
そして、上記主高負荷用吸気通路10の分岐部
は、2次弁12下流に位置していて、第1及び第
2高負荷用吸気通路10a,10b同志を連通す
る連通路16を有する拡大室17によつて構成さ
れている。上記連通路16の通路断面積ACSは、
圧力波をその減衰を小さくして有効に伝達するよ
うに各高負荷用吸気通路10a,10bの最小通
路断面積ASよりも大きく設定されている(ACS≧
AS)。 The branch part of the main high-load intake passage 10 is located downstream of the secondary valve 12, and is an enlarged chamber having a communication passage 16 that communicates the first and second high-load intake passages 10a and 10b. 17. The passage cross-sectional area A CS of the communication passage 16 is:
The minimum passage cross-sectional area of each high-load intake passage 10a, 10b is set to be larger than the minimum passage cross-sectional area A S (A CS ≧
A S ).
また、上記主低負荷用吸気通路9の分岐部は、
1次弁11下流に位置していて、第1及び第2低
負荷用吸気通路9a,9b同志を連通する連通路
18を有する拡大室19によつて構成されてい
る。上記連通路18の通路断面積ACPは、同じく
圧力波をその減衰を小さくして伝達するように各
低負荷用吸気通路9a,9bの最小通路断面積
APより大きく設定されている(ACP>AP)。 Further, the branch part of the main low-load intake passage 9 is
It is located downstream of the primary valve 11 and is constituted by an enlarged chamber 19 having a communication passage 18 that communicates the first and second low-load intake passages 9a and 9b. The passage cross-sectional area A CP of the communication passage 18 is the minimum passage cross-sectional area of each low-load intake passage 9a, 9b so as to similarly transmit pressure waves with reduced attenuation.
It is set larger than A P (A CP > A P ).
また、上記各拡大室17,19の容積はそれぞ
れエンジン排気量の0.5〜2.0倍に設定されてい
る。これは、0.5倍未満では膨張波と圧縮波間の
反転効果が得られず、一方、2.0倍を超えると圧
力波が拡散してしまい気筒間干渉効果が著しく低
下することによるものである。また、上記各拡大
室17,19は、エンジンの加速運転時又は減速
運転時等の過渡運転時での吸入空気のサージタン
クとして機能し、燃料の良好な応答性を確保する
ものである。 Further, the volume of each of the enlarged chambers 17 and 19 is set to be 0.5 to 2.0 times the engine displacement. This is because if it is less than 0.5 times, no reversal effect between expansion waves and compression waves can be obtained, whereas if it exceeds 2.0 times, the pressure waves will be diffused and the inter-cylinder interference effect will be significantly reduced. Further, each of the enlarged chambers 17 and 19 functions as a surge tank for intake air during transient operation such as acceleration or deceleration of the engine, thereby ensuring good fuel response.
すなわち、上記1次弁11及び2次弁12の下
流に、各気筒1A,1Bの低負荷用吸気通路9a
と9b及び高負荷用吸気通路10aと10bがそ
れぞれ集合する大きな容積(上記所定の容積)を
有する拡大室19及び17を備えているため、1
次弁11と2次弁12が低開度の時は拡大室19
と17の双方に、もしくは2次弁12のみが低開
度の拡大室17にそれぞれ吸気負圧が生成し蓄え
られている。また、1次弁11と2次弁12が高
開度の時は拡大室19と17の双方に、もしくは
1次弁12のみが高開度の時は拡大室19にそれ
ぞれ大気圧に近い吸気圧力が生成し蓄えられてい
る。したがつて、加速運転時においては、上記弁
(1次弁11及び2次弁12の少なくとも一方)
の開度が急増して開弁する際、それまで上記拡大
室(拡大室19と17の少なくとも一方)に蓄え
られていた吸気負圧により該拡大室上流の吸気通
路の吸気流速を逸速く速め、エアフローメータ7
の応答性を高めることで、逸速い燃料増量(燃料
の応答性)が確保できる。また、減速運転時にお
いては、上記弁の開度が急減して閉弁する際、そ
れまで上記拡大室に蓄えられていた大気圧に近い
吸気圧力により該拡大室上流の吸気通路の吸気流
速を逸速く低下させ、エアフローメータ7の応答
性を高めることで、逸速い燃料減量(燃料の応答
性)が確保できる。 That is, downstream of the primary valve 11 and secondary valve 12, there is a low-load intake passage 9a for each cylinder 1A, 1B.
and 9b and high-load intake passages 10a and 10b, respectively, are provided with enlarged chambers 19 and 17 having large volumes (the above-mentioned predetermined volumes).
When the next valve 11 and the secondary valve 12 are at a low opening, the expansion chamber 19
Intake negative pressure is generated and stored in the enlarged chamber 17 in which both the valve 17 and the secondary valve 12 or only the secondary valve 12 has a low opening. In addition, when the primary valve 11 and the secondary valve 12 are at a high opening, intake air close to atmospheric pressure is supplied to both the expansion chambers 19 and 17, or when only the primary valve 12 is at a high opening, the expansion chamber 19 is filled with air near atmospheric pressure. Pressure is generated and stored. Therefore, during acceleration operation, the above-mentioned valve (at least one of the primary valve 11 and the secondary valve 12)
When the valve opening rapidly increases and the valve opens, the negative intake pressure that had been stored in the expansion chamber (at least one of the expansion chambers 19 and 17) rapidly increases the intake flow velocity in the intake passage upstream of the expansion chamber. , air flow meter 7
By increasing the responsiveness of the engine, a rapid fuel increase (fuel responsiveness) can be ensured. In addition, during deceleration operation, when the opening of the valve suddenly decreases and the valve closes, the intake flow velocity in the intake passage upstream of the expansion chamber is reduced by the intake pressure close to atmospheric pressure that had been stored in the expansion chamber until then. By quickly reducing the amount of fuel and increasing the responsiveness of the air flow meter 7, a rapid fuel loss (fuel responsiveness) can be ensured.
さらに、上記各高負荷用吸気ポート14には該
高負荷用吸気ポート14を開閉する高負荷用吸気
弁20が設けられ、また図示していないが各低負
荷用吸気ポート13には該低負荷用吸気ポート1
3を開閉する低負荷用吸気弁が設けられている。
尚、各気筒1A,1Bにおいて、21及び22は
それぞれ一端が大気に開口し他端が排気ポート2
3,24を介して各気筒1A,1Bの燃焼室2に
開口して燃焼室2からの排気ガスを排出する第1
及び第2排気通路であつて、上記各排気ポート2
3,24には該排気ポート23,24を開閉する
排気弁25,25が設けられている。また、図示
していないが、上記各気筒1A,1Bの各排気通
路21,21,22,22の下流集合部には排気
ガス浄化用の触媒装置等が介設されていて、排圧
が高くなつている。 Furthermore, each of the high-load intake ports 14 is provided with a high-load intake valve 20 that opens and closes the high-load intake port 14, and although not shown, each of the low-load intake ports 13 is provided with a high-load intake valve 20 for opening and closing the high-load intake port 14. Intake port 1
A low-load intake valve that opens and closes 3 is provided.
In each cylinder 1A, 1B, one end of 21 and 22 opens to the atmosphere, and the other end opens to the exhaust port 2.
3, 24 to open into the combustion chamber 2 of each cylinder 1A, 1B to discharge exhaust gas from the combustion chamber 2.
and a second exhaust passage, each of the above exhaust ports 2
3 and 24 are provided with exhaust valves 25 and 25 that open and close the exhaust ports 23 and 24, respectively. Although not shown, a catalyst device for purifying exhaust gas is installed at the downstream collecting portion of each exhaust passage 21, 21, 22, 22 of each cylinder 1A, 1B, and the exhaust pressure is high. It's summery.
また、上記高負荷用吸気弁20の開弁時期(高
負荷用吸気ポート14の開口時期)は低負荷用吸
気弁(図示せず)の開弁時期(低負荷用吸気ポー
ト13の開口時期)より以早に設定されており、
高負荷用吸気通路10a,10bにおいて開口時
圧縮波を強く発生させるようにしている。また、
両者の閉弁時期はほぼ同時期に設定されている。 Furthermore, the opening timing of the high-load intake valve 20 (the opening timing of the high-load intake port 14) is the opening timing of the low-load intake valve (not shown) (the opening timing of the low-load intake port 13). It was set earlier than
A strong compression wave is generated in the high-load intake passages 10a and 10b when they are opened. Also,
Both valve closing timings are set at approximately the same time.
加えて、上記連通路16を介しての両気筒1
A,1B間の高負荷用吸気通路10a,10bの
通路長さLS(つまり高負荷用吸気ポート14,1
4間の連通長さ)は、連通路16の通路長さlCS
と該連通路16下流の第1、第2高負荷用吸気通
路10a,10bの各通路長さlS,lSとを加算し
たもの(LS=lCS+2lS)である。また、上記連通
路18を介しての両気筒1A,1B間の低負荷用
吸気通路9a,9bの通路長さLP(つまり低負荷
用吸気ポート13,13間の連通長さ)は、同様
に、連通路18の通路長さlCPと該連通路18下
流の第1、第2低負荷用吸気通路9a,9bの各
通路長さlP,lPとを加算したもの(LP=lCP+2lP)
である。そして、上記各通路長さLS、LPは、
5000〜7000rpmの回転域で両気筒1A,1Bで排
気干渉効果を得る場合には、
LS(P)={(720/Z)+θS(P)
−θO}×(60/360N)×a …()
の式より求められた値に設定される。尚、上記
()式において、Zは気筒数でZ=2であり、
720/Zは気筒間の位相差を示す。θS(P)は各吸気
弁の開弁期間である。また、θOは各吸気弁の開弁
(吸気ポートの開口)から開口時圧縮波が実質的
に発生するまでの期間と効果的に過給を行うため
に該開口時圧縮波が伝播される各吸気弁の閉弁
(吸気ポート閉口)直前の時期から閉弁までの期
間とを合算した無効期間で、開弁特性等によつて
異なるが約10〜50゜である。よつて{(720/Z)+
θS(P)−θO}は一方の気筒での開口時圧縮波の発生
から吸気行程終期にある他方の気筒への伝播まで
に要するクランクシヤフトの回転角度を表わす。
またNはエンジン回転数でN=5000〜7000rpmで
あり、60/360Nは1゜回転するに要する時間(秒)
を表わす。また、aは圧力波の伝播速度で、20℃
でa=343m/sである。 In addition, both cylinders 1 via the communication passage 16
Passage length L S of high load intake passages 10a and 10b between A and 1B (that is, high load intake ports 14 and 1
4) is the passage length of the communication passage 16 l CS
and the respective passage lengths l S and l S of the first and second high-load intake passages 10a and 10b downstream of the communication passage 16 ( L S = l CS +2l S ). Furthermore, the passage length L P of the low-load intake passages 9a and 9b between the cylinders 1A and 1B via the communication passage 18 (that is, the communication length between the low-load intake ports 13 and 13) is the same. is the sum of the passage length l CP of the communication passage 18 and the passage lengths l P and l P of the first and second low-load intake passages 9a and 9b downstream of the communication passage 18 ( L P = l CP + 2l P )
It is. The above passage lengths L S and L P are as follows:
When obtaining exhaust interference effect in both cylinders 1A and 1B in the rotation range of 5000 to 7000 rpm, L S (P) = {(720/Z) + θ S (P) −θ O }×(60/360N)× a...Set to the value determined from the formula (). In addition, in the above formula (), Z is the number of cylinders and Z=2,
720/Z indicates the phase difference between cylinders. θ S (P) is the opening period of each intake valve. In addition, θ O is the period from the opening of each intake valve (opening of the intake port) until the compression wave at the time of opening is substantially generated, and the period during which the compression wave at the time of opening is propagated in order to effectively perform supercharging. The invalid period is the sum of the period from the time just before each intake valve closes (intake port closes) until the valve closes, and varies depending on the valve opening characteristics, etc., but is about 10 to 50 degrees. Yotsute {(720/Z)+
θ S (P)−θ O } represents the rotation angle of the crankshaft required from generation of an opening compression wave in one cylinder to propagation to the other cylinder at the end of the intake stroke.
Also, N is the engine rotation speed, N = 5000 to 7000 rpm, and 60/360N is the time (seconds) required to rotate 1°.
represents. Also, a is the propagation speed of the pressure wave, which is 20℃
So a=343m/s.
また、上記各通路長さLS,LPは、5000〜
7000rpmの回転域で両気筒1A,1B間で吸気慣
性効果を得る場合には、
LS(P)={(720/Z)−θ1}
×(60/360N)×a …()
の式から求められた値に設定される。尚、上記
()式において、θ1は各吸気弁の閉弁(吸気ポ
ート閉口)から閉口時圧縮波が実質的に発生する
までの期間と効果的に過給を行うために該閉口時
圧縮波が伝播される各吸気弁の閉弁直前の時期か
ら閉弁までの期間とを合算した無効期間で同じく
約10〜50゜であり、{(720/Z)−θ1}は一方の気
筒での閉口時圧縮波の発生から吸気行程終期の他
方の気筒への伝播までに要するクランクシヤフト
の回転角度を表わす。その他は上記()式の場
合と同じである。 In addition, each of the above passage lengths L S and L P are 5000~
When obtaining the intake inertia effect between both cylinders 1A and 1B in the rotation range of 7000 rpm, the formula L S (P) = {(720/Z) - θ 1 } × (60/360N) × a ... () is set to the value calculated from. In the above equation (), θ 1 is the period from the closing of each intake valve (intake port closing) until the compression wave at closing is substantially generated, and the compression wave at closing to perform effective supercharging. The invalid period, which is the sum of the period from just before closing to the closing of each intake valve during which the waves are propagated, is also about 10 to 50 degrees, and {(720/Z) − θ 1 } is the same for one cylinder. It represents the rotation angle of the crankshaft required from the generation of the compression wave at closing to the propagation to the other cylinder at the end of the intake stroke. The rest is the same as in the case of formula () above.
そして、例えば上記実施例の場合には、通路面
積が大きくて圧力波を有効に伝播できる高負荷用
吸気通路10a,10b間で過給効果の大きい排
気干渉効果を得るように、その通路長さLSを上記
()式により求められる値に設定している。ま
た低負荷用吸気通路9a,9b間で吸気慣性効果
を得るようにその通路長さLPを上記()式に
より求められる値に設定している。 For example, in the case of the above embodiment, the length of the passage is set so as to obtain an exhaust interference effect with a large supercharging effect between the high-load intake passages 10a and 10b, which have a large passage area and can effectively propagate pressure waves. L S is set to the value determined by the above equation (). Further, in order to obtain an intake inertia effect between the low-load intake passages 9a and 9b, the passage length L P is set to a value determined by the above equation ().
さらに、上記各高負荷用吸気通路10a,10
bの通路長さlS及び各低負荷用吸気通路9a,9
bの通路長さlP、つまり各吸気通路の拡大室1
7,19への開口端面から燃焼室2への開口(各
吸気ポート13,14)までの通路長さlS,lPは
共に、5000〜7000rpmの回転域で2次の吸気個有
脈動効果を得るように、
lS(P)=(θS(P)−θ2)
×(60/360N)×(1/4)×a …()
の式から求められた値に設定されている。尚、上
記()式において、θ2は各吸気弁の開弁による
各吸気ポート開口から膨張波が実質的に発生する
までの期間と効果的に過給を行うために該膨張波
を反転した圧縮波の2次脈動波が伝播される吸気
弁の閉弁(吸気ポート閉口)直前の時期から閉弁
までの期間とを合算した無効期間で約60〜100゜程
度であり、よつて(θS(P)−θ2)は膨張波発生から
圧縮波の2次脈動波伝播までに要するクランクシ
ヤフトの回転角度を表わす。また、1/4は2次脈
動が2往復する行程の逆数を表わす。その他は上
記()式の場合と同じである。 Furthermore, each of the high-load intake passages 10a, 10
Passage length l S and each low load intake passage 9a, 9
The passage length l P of b, that is, the enlarged chamber 1 of each intake passage
The passage lengths l S and l P from the opening end face to the combustion chamber 2 (each intake port 13, 14) are both due to the second-order intake individual pulsation effect in the rotation range of 5000 to 7000 rpm. In order to obtain . In the above equation (), θ2 is the period from the opening of each intake port due to the opening of each intake valve until the expansion wave is substantially generated, and the period when the expansion wave is reversed in order to effectively perform supercharging. The ineffective period, which is the sum of the period from just before the intake valve closes (intake port closes) until the valve closes, during which the secondary pulsating wave of the compression wave is propagated, is about 60 to 100 degrees, and therefore (θ S (P)-θ 2 ) represents the rotation angle of the crankshaft required from the generation of the expansion wave to the propagation of the secondary pulsating wave of the compression wave. Moreover, 1/4 represents the reciprocal of the stroke in which the secondary pulsation makes two reciprocations. The rest is the same as in the case of formula () above.
尚、ここで、吸気個有脈動効果を得るに当つて
2次脈動を用いる理由は、1次脈動は上記効果が
大である反面、通路長さlS,lPが長くなりすぎ、
2次脈動の場合に対して2倍の長さとなるので車
載性が悪く、また吸気抵抗を増加させる傾向があ
る。一方、3次脈動は通路長さlS,lPが2次脈動
に対して2/3の長さに短くなる反面、2次脈動に
対して上記効果が約15〜25%程度低下し、また吸
気抵抗がさほど変わらない。このことから、通路
長さlS,lPを可及的に短くしながら吸気個有脈動
効果を有効に発揮させるためである。 Here, the reason why secondary pulsation is used to obtain the intake-specific pulsation effect is that while primary pulsation has the above-mentioned effect, the passage lengths l S and l P become too long.
Since the length is twice as long as that in the case of secondary pulsation, it is not easy to install on a vehicle and tends to increase intake resistance. On the other hand, in the case of tertiary pulsation, the path lengths l S and l P become 2/3 shorter than those of secondary pulsation, but on the other hand, the above-mentioned effect decreases by about 15 to 25% with respect to secondary pulsation. Also, the intake resistance does not change much. For this reason, the purpose is to effectively exhibit the intake-specific pulsation effect while making the passage lengths l S and l P as short as possible.
尚、上記()〜()式では、圧力波の伝播
に対する吸入空気の流れの影響を無視している。
これは、流速が音速に比べて小さく、吸気通路の
長さにほとんど変化をもたらさないためである。 Note that in the above equations () to (), the influence of the flow of intake air on the propagation of pressure waves is ignored.
This is because the flow velocity is smaller than the speed of sound and causes almost no change in the length of the intake passage.
次に、上記第1実施例の作用について第3図に
より説明するに、高出力を要する5000〜7000rpm
のエンジン高回転時には、2次弁12の開作動に
より主低負荷用吸気通路9と共に主高負荷用吸気
通路10も開かれて、各気筒1A,1Bに対し、
各高負荷用吸気通路10a,10bからも各低負
荷用吸気通路9a,9bとは独立して吸気の供給
が行われる。その際、一方の気筒例えば第2気筒
1Bの高負荷用吸気弁20の開弁による高負荷用
吸気ポート14開口時に第2高負荷用吸気通路1
0bの高負荷用吸気ポート14付近に発生した開
口時圧縮波は、両気筒1A,1B間の高負荷用吸
気通路10a,10bの通路長さLSを5000〜
7000rpmのエンジン高回転時を基準として上記
()式により求められる値に設定したことによ
り、第2高負荷用吸気通路10b→連通路16→
第1高負荷用吸気通路10aを経て、吸気行程終
期にある第1気筒1Aの高負荷用吸気ポート14
に伝播される。その結果、この開口時圧縮波によ
り、吸気が吸気行程終期にある第1気筒1Aの高
負荷用吸気ポート14より燃焼室2内へ押し込ま
れて過給が行われることになる(排気干渉効果)。 Next, the operation of the first embodiment will be explained with reference to FIG. 3.
When the engine is running at high speed, the secondary valve 12 is opened to open the main high-load intake passage 10 as well as the main low-load intake passage 9, and the main high-load intake passage 10 is opened for each cylinder 1A, 1B.
Intake air is supplied from each high-load intake passage 10a, 10b independently from each low-load intake passage 9a, 9b. At that time, when the high-load intake port 14 of one cylinder, for example, the high-load intake valve 20 of the second cylinder 1B is opened, the second high-load intake passage 1 is opened.
The opening compression wave generated near the high-load intake port 14 of 0b increases the passage length L S of the high-load intake passages 10a and 10b between both cylinders 1A and 1B by 5000~
By setting the value determined by the above formula () based on the engine high speed of 7000 rpm, the second high-load intake passage 10b → communication passage 16 →
After passing through the first high-load intake passage 10a, the high-load intake port 14 of the first cylinder 1A at the end of the intake stroke
is propagated to. As a result, this opening compression wave forces the intake air into the combustion chamber 2 from the high-load intake port 14 of the first cylinder 1A at the end of the intake stroke, resulting in supercharging (exhaust interference effect). .
それと同時に、第2気筒1Bの吸気行程終期に
おいて低負荷用吸気弁の閉弁による低負荷用吸気
ポート13閉口時に第2低負荷用吸気通路9bの
低負荷用吸気ポート13付近に発生した閉口時圧
縮波は、両気筒1A,1B間の低負荷用吸気通路
9a,9bの通路長さLPを5000〜7000rpmのエン
ジン高回転時を基準として上記()式により求
められる値に設定したことにより、第2低負荷用
吸気通路9b→連通路18→第1低負荷用吸気通
路9aを経て、同じく上記吸気行程終期にある第
1気筒1Aの低負荷用吸気ポート13に伝播され
て過給が行われる(吸気慣性効果)。 さらに同
時に、第1気筒1Aにおいて、低負荷用吸気弁及
び高負荷用吸気弁20の開弁後、低負荷用及び高
負荷用吸気ポート13,14からの吸気開始によ
り第1低負荷用及び高負荷用吸気通路9a,10
a内に発生した膨張波はそれぞれ、該各吸気通路
9a,10aの通路長さlP,lSを共に5000〜
7000rpmのエンジン高回転時を基準として上記
()式により求められる値に設定したことによ
り、各吸気通路9a,10a→各拡大室17,1
9(圧縮波に反転して反射)→各吸気通路9a,
10a→燃焼室2(膨張波に反転して反射)→各
吸気通路9a,10a→各拡大室17,19(圧
縮波に反転して反射)→各吸気通路9a,10a
を経て、圧縮波の2次脈動波として該第1気筒1
Aの吸気行程終期の各吸気ポート13,14に伝
播されて同じく過給が行われる(吸気個有脈動効
果)。 At the same time, when the low-load intake port 13 is closed due to the closing of the low-load intake valve at the end of the intake stroke of the second cylinder 1B, a closing occurs near the low-load intake port 13 of the second low-load intake passage 9b. The compression wave is generated by setting the passage length L P of the low-load intake passages 9a and 9b between both cylinders 1A and 1B to a value determined by the above formula () with reference to the high engine speed of 5000 to 7000 rpm. , through the second low-load intake passage 9b → the communication passage 18 → the first low-load intake passage 9a, and is propagated to the low-load intake port 13 of the first cylinder 1A, which is also at the end of the intake stroke, and supercharging is carried out. (inhalation inertia effect). Furthermore, at the same time, in the first cylinder 1A, after the low-load intake valve and the high-load intake valve 20 are opened, intake is started from the low-load and high-load intake ports 13 and 14, and the first low-load and high-load intake valves are opened. Load intake passages 9a, 10
The expansion waves generated in a respectively increase the passage lengths l P and l S of each intake passage 9a and 10a from 5000 to 5000.
By setting the value determined by the above formula () based on the engine high speed of 7000 rpm, each intake passage 9a, 10a → each expansion chamber 17, 1
9 (reflected as a compression wave) → each intake passage 9a,
10a → Combustion chamber 2 (reflects as an expansion wave and reflects) → Each intake passage 9a, 10a → Each expansion chamber 17, 19 (reflects as a compression wave and reflects) → Each intake passage 9a, 10a
As a secondary pulsating wave of the compression wave, the first cylinder 1
The supercharging is also propagated to each intake port 13, 14 at the end of the intake stroke of A (intake individual pulsation effect).
また、同様に、第2気筒1Bにおいても、5000
〜7000rpmのエンジン高回転時、吸気行程終期で
の各吸気ポート13,14に対し、第1気筒1A
からの閉口時圧縮波及び開口時圧縮波と、第2気
筒1B自身の2次脈動圧縮波とが伝播されて過給
が行われる。 Similarly, in the second cylinder 1B, 5000
At high engine speed of ~7000rpm, the first cylinder 1A is applied to each intake port 13 and 14 at the end of the intake stroke.
The closing compression wave and the opening compression wave from the cylinder 1B and the secondary pulsating compression wave of the second cylinder 1B itself are propagated to perform supercharging.
したがつて、このように気筒1A,1B相互間
における気筒間干渉効果(高負荷用吸気系統での
排気干渉効果及び低負荷用吸気系統での吸気慣性
効果)による過給効果と、各気筒1A,1B自身
における低負荷用及び高負荷用吸気系統での吸気
個有脈動効果による過給効果との相乗作用によつ
て、第4図に示すようにエンジンの高負荷高回転
時(5000〜7000rpmの回転域)での充填効率が著
しく増大して出力を大巾に向上させることができ
る。尚、第4図では、各気筒1A,1Bの各吸気
通路9a,9b,10a,10bを各々独立させ
て6000rpmを基準として吸気個有脈動効果のみを
得た場合(破線で示す)に対し、これに加えて
6000rpmを基準にして気筒間干渉効果(排気干渉
効果及び吸気慣性効果)を得るようにした場合
(実線で示す)におけるエンジンの出力トルク特
性を示す。 Therefore, the supercharging effect due to the inter-cylinder interference effect between the cylinders 1A and 1B (the exhaust interference effect in the high-load intake system and the intake inertia effect in the low-load intake system), and the , 1B itself has a synergistic effect with the supercharging effect due to the unique intake pulsation effect in the low-load and high-load intake systems, as shown in Figure 4. The charging efficiency is significantly increased in the rotation range of In addition, in FIG. 4, compared to the case where each intake passage 9a, 9b, 10a, 10b of each cylinder 1A, 1B is made independent and only the intake individual pulsation effect is obtained based on 6000 rpm (indicated by a broken line), In addition to this
The output torque characteristics of the engine are shown when the inter-cylinder interference effect (exhaust interference effect and intake inertia effect) is obtained based on 6000 rpm (indicated by a solid line).
また、その場合、排気干渉効果及び吸気個有脈
動効果を得るための圧力波伝播経路である高負荷
用吸気通路10a,10bは、低負荷用吸気通路
9a,9bよりも通路断面積が大であることによ
り、圧力波の伝播の抵抗が小さく、特に過給効果
の大きい排気干渉効果を高負荷用吸気系統で有効
に発揮させることができる。 In that case, the high-load intake passages 10a, 10b, which are pressure wave propagation paths for obtaining the exhaust interference effect and the intake-specific pulsation effect, have a larger passage cross-sectional area than the low-load intake passages 9a, 9b. As a result, the resistance to the propagation of pressure waves is small, and the exhaust interference effect, which has a particularly large supercharging effect, can be effectively exerted in a high-load intake system.
また、上記連通路16,18は、それぞれ1次
弁11及び2次弁12下流に位置し、しかも該各
連通路16,18の通路断面積ACP,ACSを各吸
気通路9a,9b,10a,10bの最小通路断
面積AP,AS以上としたので、上記各弁11,1
2によつて圧力波が減衰されることがなく、しか
も各連通路16,18自身の通路断面積拡大によ
る圧力波減衰はあるものの、通路断面積縮小(絞
り)による圧力波減衰と比較して減衰割合は少な
く、よつて上記排気干渉効果及び吸気慣性効果を
有効に発揮できる。また、上記各拡大室17,1
9は、1次弁11及び2次弁12の下流に位置す
るので、同様に吸気個有脈動効果を有効に発揮で
きる。 Further, the communication passages 16 and 18 are located downstream of the primary valve 11 and the secondary valve 12, respectively, and the passage cross-sectional areas A CP and A CS of the communication passages 16 and 18 are the same as those of the intake passages 9a, 9b, and 18, respectively. Since the minimum passage cross-sectional area of valves 10a and 10b is set to be at least A P and A S , each of the above-mentioned valves 11 and 1
2, the pressure waves are not attenuated by the communication passages 16 and 18, and although there is pressure wave attenuation due to the expansion of the passage cross-sectional area of each communication passage 16, 18 itself, compared to the pressure wave attenuation due to the passage cross-sectional area reduction (throttle). The attenuation rate is small, so the exhaust interference effect and intake inertia effect described above can be effectively exerted. In addition, each of the expansion chambers 17, 1
Since the valve 9 is located downstream of the primary valve 11 and the secondary valve 12, it can similarly effectively exhibit the intake-specific pulsation effect.
さらに、上記高負荷用吸気ポート14の開口時
期を低負荷用吸気ポート13よりも以早としたこ
とにより、特に高負荷用吸気ポート14開口時の
開口時圧縮波を強く発生でき、排気干渉効果によ
る過給効果の向上により効果的である。 Furthermore, by opening the high-load intake port 14 earlier than the low-load intake port 13, a strong compression wave can be generated especially when the high-load intake port 14 opens, resulting in an exhaust interference effect. This is more effective due to improved supercharging effect.
また、燃料供給装置としての燃料噴射ノズル1
5は、連通路18下流の低負荷用吸気通路9a,
9bの下流端部(燃焼室2への開口部近傍)に設
けられているので、その吸気通路長さが長くなる
ことにより、連通路18(拡大室19)上流に配
置されたエアフローメータ7の加速及び減速運転
時における応答遅れに起因する燃料の応答性の悪
化(燃焼室2に導入される変化した空気量に対応
する燃料供給の応答遅れ)が生じることを防止し
て、良好な燃料応答性を確保できるとともに、全
運転域で吸気の供給を行い燃料の供給が可能な低
負荷用吸気通路9a,9bのみの設置で済み、燃
料供給装置の簡略化を図ることができる。 Also, a fuel injection nozzle 1 as a fuel supply device
5 is a low-load intake passage 9a downstream of the communication passage 18;
9b is provided at the downstream end (near the opening to the combustion chamber 2), the length of the intake passage becomes longer, so that the air flow meter 7 disposed upstream of the communication passage 18 (enlarged chamber 19) Good fuel response is achieved by preventing the deterioration of fuel response caused by response delays during acceleration and deceleration operations (response delay in fuel supply corresponding to the changed amount of air introduced into the combustion chamber 2). In addition, it is possible to simplify the fuel supply system by installing only the low-load intake passages 9a and 9b, which can supply intake air and fuel in all operating ranges.
また、上記排気干渉効果、吸気慣性効果及び吸
気個有脈動効果による過給効果は、連通路16,
18を有する各拡大室17,19の位置、並びに
該連通路16,18を介しての両気筒1A,1B
間の高負荷用吸気通路10a,10b及び低負荷
用吸気通路9a,9bの各通路長さLS,LP等を
上述の如く設定することによつて得られ、過給機
等を要さないので、既存の吸気系の僅かな設計変
更で済み、構造が極めて簡単なものであり、よつ
て容易にかつ安価に実施することができる。 In addition, the supercharging effect due to the exhaust interference effect, intake inertia effect, and intake unique pulsation effect is achieved by the communication passage 16,
18, and both cylinders 1A, 1B via the communication passages 16, 18.
This can be obtained by setting the lengths L S and L P of the high-load intake passages 10a, 10b and the low-load intake passages 9a, 9b between them as described above, and does not require a supercharger or the like. Therefore, only a slight design change to the existing intake system is required, and the structure is extremely simple, so it can be implemented easily and at low cost.
尚、本発明は上記実施例に限定されるものでは
なく、その他種々の変形例をも包含するものであ
る。例えば、上記実施例では各気筒1A,1Bに
おいて低負荷用及び高負荷用吸気通路9a,9
b,10a,10bを各々独立した低負荷用及び
高負荷世吸気ポート13,14を介して燃焼室2
に開口させたが、第5図に示す第2実施例のよう
に、単一の吸気ポート26を介して燃焼室2に開
口させるとともに、該吸気ポート26を単一の吸
気弁27で開閉するようにしてもよく、上記第1
実施例と同様の作用効果を奏することができる
(尚、第5図において上記第1実施例と同一の部
分については同一の符号を付してその説明を省略
する)。 It should be noted that the present invention is not limited to the above-mentioned embodiments, but also includes various other modifications. For example, in the above embodiment, in each cylinder 1A, 1B, the low load and high load intake passages 9a, 9
b, 10a, 10b are connected to the combustion chamber 2 through independent low-load and high-load intake ports 13, 14, respectively.
However, as in the second embodiment shown in FIG. The above first
The same effects as in the embodiment can be achieved (in FIG. 5, the same parts as in the first embodiment are given the same reference numerals, and the explanation thereof will be omitted).
また、上記第1実施例では2気筒4サイクルエ
ンジンに適用した例を示したが、本発明はデユア
ルインダクシヨンタイプのその他各種多気筒エン
ジンに対しても適用できるのは勿論のことであ
る。例えば、その一例として第6図に4バルブ式
の4気筒4サイクルエンジンに適用した第3実施
例を示す(尚、第1実施例と同一の部分について
は同一の符号を付してその詳細な説明は省略す
る)。 Further, although the first embodiment described above shows an example in which the present invention is applied to a two-cylinder four-stroke engine, it goes without saying that the present invention can also be applied to various other multi-cylinder engines of the dual induction type. For example, as an example, FIG. 6 shows a third embodiment applied to a four-valve, four-cylinder, four-cycle engine (the same parts as in the first embodiment are denoted by the same reference numerals and detailed explanations are given below). (Explanation omitted).
本例の場合、各気筒1A〜1Dの高負荷用吸気
通路10a〜10dは2次弁12の下流において
拡大室17′の同一部分から分岐し該拡大室1
7′で形成される連通路16′によつて連通されて
いる。また各気筒1A〜1Dの低負荷用吸気通路
9a〜9dは1次弁11下流において拡大室1
9′の同一部分から分岐し該拡大室19′で形成さ
れる連通路18′によつて連通されている。第1、
第2、第3、第4気筒1A,1B,1C,1Dの
低負荷用吸気通路9a,9b,9c,9dは全て
等長に設定され、また第1、第2、第3、第4気
筒1A,1B,1C,1Dの高負荷用吸気通路1
0a,10b,10c,10dも全て等長に設定
され、必然的に1−3−4−2の点火順序におけ
る隣接気筒間のLS,LPが等しくなつている。ま
た、上記連通路16′,18′を介して気筒1A〜
1D間の高負荷用吸気通路10a〜10d及び低
負荷用吸気通路9a〜9dの通路長さLS,LPの
少なくとも一方は、排気干渉効果を得るためには
上記()式の右辺第1項(開口時圧縮波発生か
ら伝播までに要する回転角度)が異なり(第9図
参照)、
LS(P)=(θS(P)−180−θO)
×(60/360N)×a …(′)
により設定される。また吸気慣性効果を得る場合
には上記()式によりZ=4として設定され
る。また各吸気通路9a〜9d、10a〜10d
の通路長さlP,lSは共に2次の吸気個有脈動効果
を得るように上記()式により設定されてい
る。尚、3気筒4サイクルエンジンに対しても、
図示していないが2気筒の場合と同様であり、各
通路長さLS,LP,lP,lSを上記()〜()式
により設定すればよい。 In the case of this example, the high-load intake passages 10a to 10d of the cylinders 1A to 1D are branched from the same portion of the enlarged chamber 17' downstream of the secondary valve 12.
They are communicated by a communication path 16' formed by 7'. In addition, the low-load intake passages 9a to 9d of each cylinder 1A to 1D are connected to an enlarged chamber 1 downstream of the primary valve 11.
They are communicated by a communication passage 18' that branches from the same portion of the enlarged chamber 19'. First,
The low-load intake passages 9a, 9b, 9c, and 9d of the second, third, and fourth cylinders 1A, 1B, 1C, and 1D are all set to the same length. 1A, 1B, 1C, 1D high load intake passage 1
0a, 10b, 10c, and 10d are also all set to the same length, and L S and L P between adjacent cylinders in the 1-3-4-2 ignition order are necessarily equal. Further, the cylinders 1A to 1A are connected via the communication passages 16' and 18'.
In order to obtain the exhaust interference effect, at least one of the passage lengths L S and L P of the high load intake passages 10a to 10d and the low load intake passages 9a to 9d between 1D should be The term (rotation angle required from generation of compression wave to propagation during opening) is different (see Figure 9), L S (P) = (θ S (P) - 180 - θ O ) × (60/360N) × a ...(') is set. Further, when obtaining the intake inertia effect, Z=4 is set according to the above equation (). In addition, each intake passage 9a to 9d, 10a to 10d
The passage lengths l P and l S are both set according to the above equation ( ) so as to obtain a second-order intake-specific pulsation effect. Furthermore, for 3-cylinder 4-stroke engines,
Although not shown, it is the same as in the case of two cylinders, and each passage length L S , L P , l P , l S may be set using the above equations () to ().
さらに、排気干渉効果及び吸気慣性効果の気筒
間干渉の態様として、上記第1実施例(2気筒4
サイクルエンジン)では高負荷用吸気系統で排気
干渉効果を、低負荷用吸気系統で吸気慣性効果を
得るようにしたが、高負荷用及び低負荷用吸気系
統の少なくとも一方で排気干渉効果を得るように
設定すればよい。そして、その作用過程は、一般
の2気筒エンジンの場合、第7図に示すように、
既述と同様、排気干渉効果(実線矢印で示す)及
び吸気慣性効果(破線矢印で示す)は第1気筒か
ら第2気筒へ、第2気筒から第1気筒へと順次交
互に作用して行くのである。また、3気筒エンジ
ンの場合には、第8図に示すように、上記両効果
は、2気筒の場合と同様、第1気筒→第2気筒、
第2気筒→第3気筒、第3気筒→第1気筒へと順
次作用して行く。さらに、4気筒エンジンの場合
には、第9図に示すように、吸気慣性効果は、点
火順序通りに第1気筒→第3気筒、第3気筒→第
4気筒、第4気筒→第2気筒、第2気筒→第1気
筒へと順次作用して行き、排気干渉効果は、逆に
位相が180゜遅れた気筒から作用を受け、第3気筒
→第1気筒、第4気筒→第3気筒、第2気筒→第
4気筒、第1気筒→第2気筒、第3気筒→第1気
筒へと作用するのである。よつて、このように気
筒間干渉を行う気筒間の通路長さLS,LPの少な
くとも一方を排気干渉効果を得るように設定すれ
ばよい。 Furthermore, as a mode of inter-cylinder interference of the exhaust interference effect and the intake inertia effect, the first embodiment (two cylinders, four
cycle engine), the high-load intake system has an exhaust interference effect, and the low-load intake system has an intake inertia effect. You can set it to . In the case of a general two-cylinder engine, the working process is as shown in Fig. 7.
As described above, the exhaust interference effect (indicated by the solid line arrow) and the intake inertia effect (indicated by the dashed line arrow) act alternately from the first cylinder to the second cylinder and from the second cylinder to the first cylinder. It is. In addition, in the case of a three-cylinder engine, as shown in Fig. 8, both of the above effects can be achieved from the first cylinder to the second cylinder, as in the case of a two-cylinder engine.
It acts sequentially from the 2nd cylinder to the 3rd cylinder, and from the 3rd cylinder to the 1st cylinder. Furthermore, in the case of a four-cylinder engine, as shown in Figure 9, the intake inertia effect is caused by the firing order: 1st cylinder → 3rd cylinder, 3rd cylinder → 4th cylinder, 4th cylinder → 2nd cylinder. , the exhaust interference effect acts sequentially from the 2nd cylinder to the 1st cylinder, and conversely, the exhaust interference effect acts from the cylinder whose phase is delayed by 180 degrees, from the 3rd cylinder to the 1st cylinder, and from the 4th cylinder to the 3rd cylinder. , from the second cylinder to the fourth cylinder, from the first cylinder to the second cylinder, and from the third cylinder to the first cylinder. Therefore, at least one of the passage lengths L S and LP between the cylinders, which cause inter-cylinder interference in this way, may be set so as to obtain the exhaust interference effect.
また、上記実施例では、1次弁11を主低負荷
用吸気通路9内に設けた型式のものについて示し
たが、第1次弁11を、主低負荷用吸気通路9と
主高負荷用吸気通路10との分岐部上流の主吸気
通路5に設けた型式のものも採用可能である。 Further, in the above embodiment, the primary valve 11 is provided in the main low-load intake passage 9, but the primary valve 11 is provided in the main low-load intake passage 9 and the main high-load intake passage 9. A type provided in the main intake passage 5 upstream of the branching part with the intake passage 10 can also be adopted.
(発明の効果)
以上説明したように、本発明によれば、低負荷
用と高負荷用との2系統の独立した吸気通路を備
えた多気筒エンジンにおいて、5000〜7000rpmの
エンジン高回転時、高負荷用及び低負荷用の少な
くとも一方の吸気系統で気筒間の排気干渉効果に
よる過給効果を強力に得るとともに、各気筒自身
の高負荷用及び低負荷用の双方の吸気系統で吸気
個有脈動効果による過給効果を効果的に得るよう
にしたので、過給機等絵を要さずに既存の吸気系
の僅かな設計変更による簡単な構成でもつて、エ
ンジン高負荷高回転時の充填効率を高める出力向
上を有効に図ることができ、よつてエンジンの出
力向上対策の容易実施化及びコストダウン化に有
用なものである。(Effects of the Invention) As explained above, according to the present invention, in a multi-cylinder engine equipped with two independent intake passages for low load and high load, when the engine rotates at a high speed of 5000 to 7000 rpm, At least one of the high-load and low-load intake systems provides a strong supercharging effect due to the exhaust interference effect between cylinders, and each cylinder's own high-load and low-load intake systems provide unique intake characteristics. Since the supercharging effect due to the pulsation effect is effectively obtained, even a simple configuration consisting of a slight design change to the existing intake system can be used without the need for a supercharger or the like, and it is possible to easily charge the engine during high load and high rotation speeds. It is possible to effectively improve output to improve efficiency, and is therefore useful for easily implementing measures to improve engine output and reducing costs.
図面は本発明の実施例を示し、第1図及び第2
図は第1実施例を示す全体構成説明図及び同要部
概略図、第3図は第1実施例の吸気行程を示す説
明図、第4図は出力トルク特性を示す図、第5図
は第2実施例を示す要部概略図、第6図は第3実
施例を示す第1図相当図、第7図〜第9図はそれ
ぞれ2気筒、3気筒及び4気筒エンジンでの気筒
間干渉を示す説明図である。
1A〜1D…第1〜第4気筒、2…燃焼室、5
…主吸気通路、7…エアフローメータ、9…主低
負荷用吸気通路、9a〜9d…第1〜第4低負荷
用吸気通路、10…主高負荷用吸気通路、10a
〜10d…第1〜第4高負荷用吸気通路、11…
1次弁、12…2次弁、15…燃料噴射ノズル、
16,16′…連通路、17,17′…拡大室、1
8,18′…連通路、19,19′…拡大室。
The drawings show embodiments of the invention, FIGS. 1 and 2.
The figure is an explanatory diagram of the overall configuration and a schematic diagram of the main parts of the first embodiment, FIG. 3 is an explanatory diagram showing the intake stroke of the first embodiment, FIG. 4 is a diagram showing the output torque characteristics, and FIG. FIG. 6 is a schematic diagram of the main parts showing the second embodiment, FIG. 6 is a diagram equivalent to FIG. 1 showing the third embodiment, and FIGS. 7 to 9 are inter-cylinder interference in 2-cylinder, 3-cylinder, and 4-cylinder engines, respectively. FIG. 1A to 1D...1st to 4th cylinders, 2...Combustion chamber, 5
... Main intake passage, 7... Air flow meter, 9... Main low load intake passage, 9a to 9d... 1st to 4th low load intake passage, 10... Main high load intake passage, 10a
~10d...first to fourth high-load intake passages, 11...
Primary valve, 12... Secondary valve, 15... Fuel injection nozzle,
16, 16'...Communication path, 17, 17'...Enlargement chamber, 1
8, 18'...Communication path, 19, 19'...Enlargement chamber.
Claims (1)
と高負荷用吸気通路とを有するとともに該各気筒
の低負荷用吸気通路と高負荷用吸気通路とを各気
筒の燃焼室に吸気ポートを介して開口させた吸気
通路を備え、該吸気通路は、少なくとも上記低負
荷用吸気通路を流れる吸気量を変化させる1次弁
と、上記高負荷用吸気通路を流れる吸気量を変化
させる2次弁とを有するエンジンの吸気装置であ
つて、 上記1次弁及び2次弁の下流において上記各気
筒の低負荷用吸気通路同士及び高負荷用吸気通路
同士を連通するそれぞれ各吸気通路の最小通路断
面積以上の通路断面積の連通路を有する拡大室を
設け、 上記連通路を介しての各気筒間の低負荷用吸気
通路及び高負荷用吸気通路の通路長さを、少なく
とも一方が5000〜7000rpmのエンジンの高回転
時、一つの気筒の吸気ポートの開口時に生じる圧
縮波が吸気行程終期にある他の気筒の吸気ポート
に伝播して過給を行うように設定し、 上記拡大室から各気筒の吸気ポートに至る上記
低負荷用吸気通路及び高負荷用吸気通路の通路長
さlP,lSを、双方が5000〜7000rpmのエンジンの
高回転時、各気筒の吸気ポートの吸気開始により
生じる膨張波を上記拡大室で反転して反射した圧
縮波の2次脈動波が該各気筒の吸気行程終期の吸
気ポートに伝播して過給を行うように、下記式 lP =(θP−θ2)×(60/360N) ×(1/4)×a lS =(θS−θ2)×(60/360N) ×(1/4)×a (ここで、θP及びθSは各吸気ポートの開口期
間、θ2は各吸気ポートの開口から膨張波が実質的
に発生するまでの期間と該膨張波を反転した圧縮
波の2次脈動波が伝播される各吸気ポートの閉口
直前の時期から閉口までの期間とを合算した無効
期間、Nはエンジン回転数、aは圧力波の伝播速
度である) により設定したことを特徴とするエンジンの吸気
装置。 2 2気筒又は3気筒4サイクルエンジンにおい
て、上記連通路を介しての各気筒間の高負荷用吸
気通路の通路長さLS及び連通路を介しての各気筒
間の低負荷用吸気通路の通路長さLPの少なくと
も一方を、下記式 LS(P)={(720/Z)+θS(P) −θO}×(60/360N)×a (ここで、Zは気筒数、θS(P)は各吸気ポートの
開口期間、θOは各吸気ポートの開口から開口時圧
縮波が実質的に発生するまでの期間と効果的に過
給を行うために該開口時圧縮波が伝播される各吸
気ポートの閉口直前の時期から閉口までの期間と
を合算した無効期間、Nはエンジン回転数、aは
圧力波の伝播速度である) により設定した特許請求の範囲第1項記載のエン
ジンの吸気装置。 3 4気筒4サイクルエンジンにおいて、上記連
通路を介しての各気筒間の高負荷用吸気通路の通
路長さLS及び連通路を介しての各気筒間の低負荷
用吸気通路の通路長さLPの少なくとも一方を、
下記式 LS(P)=(θS(P)−180−θO) ×(60/360N)×a (ここで、θS(P)は各吸気ポートの開口期間、θO
は各吸気ポートの開口から開口時圧縮波が実質的
に発生するまでの期間と効果的に過給を行うため
に該開口時圧縮波が伝播される各吸気ポートの閉
口直前の時期から閉口までの期間とを合算した無
効期間、Nはエンジン回転数、aは圧力波の伝播
速度である)により設定した特許請求の範囲第1
項記載のエンジンの吸気装置。[Scope of Claims] 1. Each cylinder has an independent low-load intake passage and a high-load intake passage, and the low-load intake passage and high-load intake passage of each cylinder are connected to the combustion chamber of each cylinder. The chamber is provided with an intake passage opened through an intake port, and the intake passage includes at least a primary valve that changes the amount of intake air flowing through the low-load intake passage, and a primary valve that changes the amount of intake air that flows through the high-load intake passage. An intake system for an engine having a secondary valve that is changed, wherein the low-load intake passages and the high-load intake passages of each of the cylinders are connected downstream of the primary valve and the secondary valve, respectively. An enlarged chamber having a communication passage with a passage cross-sectional area larger than the minimum passage cross-sectional area of the passage is provided, and the passage length of the low-load intake passage and the high-load intake passage between each cylinder via the communication passage is at least When the engine is running at a high speed of 5,000 to 7,000 rpm, the compression wave generated when the intake port of one cylinder opens propagates to the intake port of the other cylinder at the end of the intake stroke to perform supercharging. The passage lengths l P and l S of the above-mentioned low-load intake passage and high-load intake passage from the expansion chamber to the intake port of each cylinder are determined when both are at high engine speed of 5000 to 7000 rpm. The following equation l = (θ P −θ 2 ) × (60/360N) × (1/4) × a l S = (θ S −θ 2 ) × (60/360N) × (1/4) × a (Here, θ P and θ S are the opening periods of each intake port, and θ 2 is the period from the opening of each intake port until the expansion wave is substantially generated, and the second pulsation wave of the compression wave, which is the inversion of the expansion wave, is propagated. (N is the engine rotational speed, and a is the propagation speed of pressure waves.) 2 In a 2-cylinder or 3-cylinder 4-cycle engine, the passage length L S of the high-load intake passage between each cylinder via the communication passage and the passage length L S of the low-load intake passage between each cylinder via the communication passage. At least one of the passage lengths L P can be calculated using the following formula L S (P) = {(720/Z) + θ S (P) −θ O } x (60/360 N) x a (where Z is the number of cylinders, θ S (P) is the opening period of each intake port, θ O is the period from the opening of each intake port until the opening compression wave is substantially generated, and the opening period of the opening compression wave for effective supercharging. (N is the engine rotational speed, and a is the propagation speed of the pressure wave.) Intake system for the engine described. 3 In a 4-cylinder 4-cycle engine, the passage length L S of the high-load intake passage between each cylinder via the communication passage and the passage length of the low-load intake passage between each cylinder via the communication passage. At least one of L P ,
The following formula L S (P) = (θ S (P) - 180 - θ O ) × (60/360N) × a (Here, θ S (P) is the opening period of each intake port, θ O
is the period from the opening of each intake port until the opening compression wave is substantially generated, and the period from just before closing of each intake port to the time when the opening compression wave is propagated in order to effectively perform supercharging. (N is the engine rotation speed, and a is the propagation speed of the pressure wave.)
Intake system for the engine described in Section 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57190616A JPS5979036A (en) | 1982-10-28 | 1982-10-28 | Intake apparatus for engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57190616A JPS5979036A (en) | 1982-10-28 | 1982-10-28 | Intake apparatus for engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5979036A JPS5979036A (en) | 1984-05-08 |
| JPH0452373B2 true JPH0452373B2 (en) | 1992-08-21 |
Family
ID=16261031
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP57190616A Granted JPS5979036A (en) | 1982-10-28 | 1982-10-28 | Intake apparatus for engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5979036A (en) |
-
1982
- 1982-10-28 JP JP57190616A patent/JPS5979036A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5979036A (en) | 1984-05-08 |
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