JPS60132023A - Air intake mechanism for multicylinder engine - Google Patents

Air intake mechanism for multicylinder engine

Info

Publication number
JPS60132023A
JPS60132023A JP58242698A JP24269883A JPS60132023A JP S60132023 A JPS60132023 A JP S60132023A JP 58242698 A JP58242698 A JP 58242698A JP 24269883 A JP24269883 A JP 24269883A JP S60132023 A JPS60132023 A JP S60132023A
Authority
JP
Japan
Prior art keywords
intake
surge tank
engine
air
cylinder
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.)
Pending
Application number
JP58242698A
Other languages
Japanese (ja)
Inventor
Kazuhiko Ueda
和彦 上田
Junzo Sasaki
潤三 佐々木
Mitsuo Hitomi
光夫 人見
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mazda Motor Corp
Original Assignee
Mazda Motor Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mazda Motor Corp filed Critical Mazda Motor Corp
Priority to JP58242698A priority Critical patent/JPS60132023A/en
Priority to US06/683,836 priority patent/US4619226A/en
Priority to DE3446377A priority patent/DE3446377C2/en
Publication of JPS60132023A publication Critical patent/JPS60132023A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B27/00Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
    • F02B27/02Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means
    • F02B27/0226Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means characterised by the means generating the charging effect
    • F02B27/0247Plenum chambers; Resonance chambers or resonance pipes
    • F02B27/0257Rotatable plenum chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B27/00Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
    • F02B27/02Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means
    • F02B27/0205Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means characterised by the charging effect
    • F02B27/0215Oscillating pipe charging, i.e. variable intake pipe length charging
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B27/00Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
    • F02B27/02Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means
    • F02B27/0226Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues the systems having variable, i.e. adjustable, cross-sectional areas, chambers of variable volume, or like variable means characterised by the means generating the charging effect
    • F02B27/0247Plenum chambers; Resonance chambers or resonance pipes
    • F02B27/0263Plenum chambers; Resonance chambers or resonance pipes the plenum chamber and at least one of the intake ducts having a common wall, and the intake ducts wrap partially around the plenum chamber, i.e. snail-type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B2075/1804Number of cylinders
    • F02B2075/1816Number of cylinders four
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/20Multi-cylinder engines with cylinders all in one line
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

PURPOSE:To enable the length of an air intake passage to be varied over a wide range by partitioning a surge tank into an inner space and extended parts and rotating a rotary partition member, which connects both parts through a connecting port. CONSTITUTION:Air sucked in from an air cleaner is introduced into a surge tank 6 through an air flow meter and a throttle valve. Then, the air is sucked into each cylinder 9 through each branch passage 10 and intake port 8. When the number of revolution of an engine 1 is low, the connecting part between the inner space 16 and each of the extension parts 13 of the surge tank 6 is positioned at B. When the number of revolution is increased causing a rotary partition member 15 to rotate in the direction of (a), the connecting part is also rotated in the direction of (a), being positioned at B' at the highest condition.

Description

【発明の詳細な説明】 −1− (産業上の利用分野〉 本発明は多気筒エンジンの吸気装置、特にす−ジタンク
から各気筒に夫々独立した吸気通路が設けられ、且つ各
吸気通路の長さが可変とされた吸気装置に関する。
Detailed Description of the Invention -1- (Industrial Application Field) The present invention relates to an intake system for a multi-cylinder engine, in particular an air intake system in which an independent intake passage is provided from a gas tank to each cylinder, and the length of each intake passage is This invention relates to an intake device whose height is variable.

(従 来 技 術) 一般にエンジンにおいては、吸気の充填効率を高めて出
力の向上を図るためには所謂吸気慣性効果を(11用す
ることが有効であるが、この吸気慣性効果は吸気通路の
長さとエンジンの回転数との関係に依存し、該効果が@
も効果的に得られる吸気通路の良さがエンジン回転数の
上昇に従って短くなるという関係にある。そこで、例え
ば実開昭56−2023号公報や実開昭57−2262
9号公報に開示されているように、吸気通路の長さを可
変とし、その長さをエンジン回転数に応じて変化さぼる
ことにより、低速から高速までの広い範囲で吸気慣性効
果を利用できるようにした吸気装置が提案されている。
(Prior art) In general, in engines, it is effective to use the so-called intake inertia effect (11) in order to increase intake air filling efficiency and improve output. The effect depends on the relationship between length and engine speed.
There is also a relationship in which the quality of the intake passage that can be effectively obtained becomes shorter as the engine speed increases. Therefore, for example, Utility Model Application Publication No. 56-2023 and Utility Model Application No. 57-2262
As disclosed in Publication No. 9, by making the length of the intake passage variable and changing the length according to the engine speed, it is possible to utilize the intake inertia effect over a wide range from low speeds to high speeds. An intake device has been proposed.

しかし、これらの公報に開示された吸気装置tよ、−2
− いずれも固定管に嵌合された可動管を直線方向にスライ
ドさせることによって吸気通路の長さを変化させる構成
であるため、該長さを所要の範囲で変化させるためには
装置Nが大型化し、特に当該エンジンを自動車に搭載J
る場合に大ぎなスペースを必要とする欠点がある。また
、多気筒エンジンの場合は、各気筒毎に独立した吸気通
路を設け、その夫々について長さを可変としなければな
らないから、」上記の如ぎ構成によると部品点数が著し
く多くなり、且つ駆動機構が複雑化することになる。
However, the intake device disclosed in these publications is -2
- In both cases, the length of the intake passage is changed by sliding a movable pipe fitted to a fixed pipe in a linear direction, so the device N is large in order to change the length within the required range. In particular, the engine will be installed in a car.
The disadvantage is that it requires a large amount of space when used. Furthermore, in the case of a multi-cylinder engine, an independent intake passage must be provided for each cylinder, and the length of each passage must be made variable. The mechanism becomes complicated.

(発 明 の 目 的) 本発明は、吸気通路の長さを可変とした吸気装置につい
ての上記のような問題に対処するもので、装置の全体が
コンバク1〜に構成され、且つ多気筒エンジン用として
部品点数が少なく、また駆動機構が簡素な吸気装置を実
現することを目的とする。
(Object of the Invention) The present invention is intended to solve the above-mentioned problems regarding an intake system in which the length of the intake passage is variable. The purpose of this invention is to realize an intake device with a small number of parts and a simple drive mechanism.

ところで、本願出願人は先の特許出願(特願昭58−4
8344号)で上記のような目的を達成するエンジンの
吸気通路に関する発明を出願したー 3 − が、本願発明はこの先願発明を更に改良するもので、吸
気通路の良さが可変の多気筒エンジンの吸気装置として
、吸気がスムーズに流れ、しかもエンジンの全高が高く
4〒らない吸気装置の実現を目的とする。
By the way, the applicant of this application has filed an earlier patent application (Japanese Patent Application No. 1986-4)
No. 8344), he filed an application for an invention related to an engine intake passage that achieves the above-mentioned object - 3 - However, the present invention is a further improvement of this earlier invention, and is a multi-cylinder engine with variable intake passage quality. The purpose of the present invention is to realize an intake system in which intake air flows smoothly and the total height of the engine is not high.

(発 明 の 構 成) 本発明に係る多気筒エンジンの吸気装置は上記目的達成
のため次のように構成される。
(Structure of the Invention) In order to achieve the above object, the intake system for a multi-cylinder engine according to the present invention is structured as follows.

即ち、吸気系の途中にサージタンクが備えられ、且つ該
サージタンクから各気筒に夫々独立した吸気通路が設け
られた吸気装置において、上記サージタンクの周壁部に
各吸気通路の延長部を夫々独立させて上下方向に形成す
ると共に、この延長部の上方部に各吸気通路の上流端を
夫々接続し、且つサージタンク内には、その内部空間と
」:記名延長部とを画成すると共にその両者を連通さゼ
る連通口を有する画成回動部材を設ける。イして、該回
動部材を駆動機構によってエンジンの運転状態に応じて
回動させることにJ:す、上記吸気通路延長部とサージ
タンク内部空間との連通位置を変化−4− させで、す゛−ジタンク下流の吸気通路の長さを変化さ
せるように構成する。
That is, in an intake system in which a surge tank is provided in the middle of the intake system, and independent intake passages are provided from the surge tank to each cylinder, the extended portions of each intake passage are provided independently on the peripheral wall of the surge tank. The upstream end of each intake passage is connected to the upper part of this extension, and the surge tank defines an internal space and an extension part thereof. A defining rotating member having a communication port that communicates the two is provided. and the rotating member is rotated by a drive mechanism according to the operating state of the engine, and the communication position between the intake passage extension and the internal space of the surge tank is changed, The length of the intake passage downstream of the stirrer tank is configured to vary.

このような構成によれば、画成回動部材の回動によって
各気筒に夫々通じる複数の吸気通路の長さが変化するの
で、装置全体の大型化や部品点数の増大、更には駆動機
構の複雑化等を来たすことなく、各吸気通路の長さを広
範囲に変化させることが可能となる。特に、上記サージ
タンクの周壁部に設けられる各延長部がその上方部にお
いて各吸気通路に接続されるから、該延長部を含む吸気
通路がエンジン全高を高くすることなく且つ吸気がスム
ーズに流れるように構成されることになる。
According to such a configuration, the lengths of the plurality of intake passages leading to each cylinder are changed by the rotation of the defining rotating member, resulting in an increase in the size of the entire device, an increase in the number of parts, and furthermore, in the drive mechanism. It becomes possible to vary the length of each intake passage over a wide range without causing complications. In particular, since the extensions provided on the peripheral wall of the surge tank are connected to the intake passages at their upper parts, the intake passages including the extensions do not increase the overall height of the engine and the intake air flows smoothly. It will be composed of

(実 施 例) 以下、本発明の実施例を図面に基づいて説明する。(Example) Embodiments of the present invention will be described below based on the drawings.

第1図に示すにうに、エンジン1の一側部に設(プられ
た吸気装置2は、エアクリーナ3からエア70−メータ
4及びスロワ1〜ル弁5を介して空気が導入されるサー
ジタンク6と、該サージタンク6から分岐されて、該タ
ンク内の空気をシリンダー 5 − ヘッド7における各吸気ボート8・・・8を介して各気
筒9・・・9に吸入させる複数の分岐管10・・・10
とを有し、これらにより上記エアクリーナ3から複数の
気筒9・・・9に至る吸気系が構成されている。
As shown in FIG. 1, an intake device 2 installed on one side of the engine 1 is a surge tank into which air is introduced from an air cleaner 3 through an air 70-meter 4 and a thrower 1 through a valve 5. 6, and a plurality of branch pipes 10 branched from the surge tank 6 and sucking air in the tank into each cylinder 9...9 via each intake boat 8...8 in the cylinder 5-head 7. ...10
These constitute an intake system extending from the air cleaner 3 to the plurality of cylinders 9...9.

上記サージタンク6及び各分岐管1O・・・1Oは、第
2,3図に示すように一体のケーシング11によって形
成され、該ケーシング11が」上記シリンダヘッド7の
一側面に固着されることにより各分岐管1O・・・1O
と各吸気ポート8・・・8とが接続されて、サージタン
ク6から各気筒9・・・9に至る略−直線状の吸気通路
12・・・12が夫々独立して形成されている。また、
サージタンク6の周壁部には上記各吸気通路12・・・
12の延長部13・・・13が設(プられている。この
延長部13・・・13は、ケーシング11の内面に立設
された仕切壁17I・・・14によって夫々独立させて
設けられ、第3図に示ずようにサージタンク6の上方部
において上記各吸気通路12・・・12の上流端に夫々
−直線状に接続されている。そして、該接続部△から上
下方向の面に沿って下巻き状に、即ちサージタンク6の
−〇 − 上方部から外側方部を経て下方に回り込み、更に内側方
から該タンク6の中央部に通じるように渦巻き状に形成
されている。
The surge tank 6 and each branch pipe 1O...1O are formed by an integral casing 11 as shown in FIGS. 2 and 3, and the casing 11 is fixed to one side of the cylinder head 7. Each branch pipe 1O...1O
and each intake port 8 . . . 8 are connected to form substantially linear intake passages 12 . . . 12 extending from the surge tank 6 to each cylinder 9 . Also,
The above-mentioned intake passages 12 are provided on the peripheral wall of the surge tank 6.
12 extension parts 13...13 are provided (pulled).These extension parts 13...13 are provided independently by partition walls 17I...14 erected on the inner surface of the casing 11. , are connected linearly to the upstream ends of the intake passages 12 . . . 12 in the upper part of the surge tank 6, respectively, as shown in FIG. In other words, it is formed in a spiral shape so as to extend downwardly from the upper part of the surge tank 6 through the outer part and then to the center part of the tank 6 from the inner side.

一方、サージタンク6の中央部には、周壁部における上
記各延長部13・・・13とその内側の空間とを画成J
る中空円筒状の画成回動部vJ15が備えられている。
On the other hand, in the central part of the surge tank 6, the above-mentioned extension parts 13...13 in the peripheral wall part and a space inside thereof are defined.
A hollow cylindrical defining rotating portion vJ15 is provided.

この回動部材15は第2図に示すJ:うに一端が間口さ
れ、内部空間16が該間口部17及びサージタンク6の
入口部18を介してスロワ1〜ル弁5が設けられた吸気
系の上流部に連通されていると共に、該端部において軸
受19を介してケーシング11に軸支され、また他端部
がケーシング11にボルト20・・・20により固着さ
れたサイドカバー21に軸受22を介して軸支されて、
サージタンク6内で回動自在とされている。
This rotating member 15 is connected to an intake system in which one end of the rotating member 15 is opened as shown in FIG. A bearing 22 is connected to the side cover 21, which is connected to the upstream part of the side cover 21, and is pivotally supported by the casing 11 via a bearing 19 at the end thereof, and the other end is fixed to the casing 11 by bolts 20...20. is pivoted through the
It is rotatable within the surge tank 6.

そして、該回動部材15にお()る上記各延長部13・
・・13と内部空間16とを画成する周面に複数の連通
口23・・・23が設(プられ、該連通口23・・・2
3によって内部空間16と各延長部13・・・13とが
夫々連通されている。
Each of the above-mentioned extension portions 13 and 13 attached to the rotating member 15 is
... 13 and the internal space 16, a plurality of communication ports 23...23 are provided (pulled) on the circumferential surface defining the inner space 16 and the communication ports 23...2.
3, the internal space 16 and each extension portion 13...13 are communicated with each other.

= 7 − また、第4図に示すようにこの画成回動部4,115を
回動さぜる駆動機構24がサージタンク6の一端部外側
に備えられているが、該駆動機構24は、上記サイドカ
バー21から外部に突出した回動部(215に一体の軸
部25に固着された入力歯車26と、該入力歯車26に
噛み合された円弧状歯車27と、この円弧状歯車27を
レバー28を介して駆動するダイヤフラム29とで構成
され、該ダイヤフラム29にエンジン1の排気通路(図
示せず)から排圧が導入されるようになっている。
= 7 - Furthermore, as shown in FIG. 4, a drive mechanism 24 for rotating the defining rotating parts 4, 115 is provided outside one end of the surge tank 6. , an input gear 26 fixed to a shaft part 25 integral with the rotating part (215) protruding from the side cover 21 to the outside, an arcuate gear 27 meshed with the input gear 26, and the arcuate gear 27. and a diaphragm 29 that is driven via a lever 28, and exhaust pressure is introduced into the diaphragm 29 from an exhaust passage (not shown) of the engine 1.

ここで、上記排圧はエンジンの高回転時には高く、低回
転時には低くなるから、エンジン回転数の一ト昇に従っ
て上記円弧状歯車27及び入力歯車26が夫々図示の位
置からa方向に回動し、これに伴って回動部材15も第
3図に示すa方向に回動する。
Here, since the exhaust pressure is high when the engine rotates at high speeds and becomes low when the engine speeds are low, the arcuate gear 27 and the input gear 26 rotate in the direction a from the illustrated positions as the engine speed increases. Accordingly, the rotating member 15 also rotates in the direction a shown in FIG.

尚、この実施例においては、第2図に示でようにサージ
タンク6におLlる中央に位置する2つの延長部13.
13問に予備空間30が設けられていると共に、該空間
3Oと回動部材15の内部空−8− 間16とが連通口31によって連通されている。
In this embodiment, as shown in FIG. 2, there are two centrally located extensions 13.
A spare space 30 is provided in the 13 spaces, and the space 3O and the internal space 16 of the rotating member 15 are communicated through a communication port 31.

この空間30は、例えば排気ガスを還流する場合に該ガ
スを各気筒9・・・9に均等に還流するために、或いは
各種の制御用どして安定した吸気負圧を取出すため等に
用いられる。また、第3図に示すように各分岐管1O・
・・1Oの上方に燃料噴射ノズル32・・・32が取付
けられ、燃料供給管33によって供給される燃わ1を該
ノズル32・・・32によって各吸気通路12・・・1
2内に夫々噴射するようになっている。更に、ケーシン
グ11と回動部材15とは、サイドカバー21を取外し
た状態で回動部材15を挿入することにより容易に組立
てることができるように構成されている。
This space 30 is used, for example, to uniformly recirculate exhaust gas to each cylinder 9...9 when recirculating exhaust gas, or to obtain stable intake negative pressure for various control purposes. It will be done. In addition, as shown in Fig. 3, each branch pipe 1O.
. . 32 are installed above 1O, and the fuel 1 supplied through the fuel supply pipe 33 is injected into each intake passage 12 .
It is designed to inject into each of the 2 parts. Furthermore, the casing 11 and the rotating member 15 are configured so that they can be easily assembled by inserting the rotating member 15 with the side cover 21 removed.

上記の構成にJ:れば、エンジン1の運転時に第1図に
示すエアクリーナ3から吸入された空気はエアフローメ
ータ4及びスロワ1〜ル弁5を経てサージタンク6に導
入され、更に各分岐通路1O・・・1O及び吸気ポート
8・・・8を経て各気筒9・・・9に吸入されるのであ
るが、上記サージタンク6内においては、空気は該タン
ク6の入口部18から画一 9 − 成回動部材15の内部空間16に導入されるど共に、該
部材15の周面に形成された連通口23・・・23から
各延長部13・・・13に分配されて流入する。ぞして
、各延長部13・・・13を渦巻き状に通過した後、上
記分岐管10・・・10と吸気ポート8・・・8とでな
る吸気通路12・・・12を経て各気筒9・・・9に至
るのである。その場合に、上記各延長部13・・・13
ば仕切壁14・・・14によって独立して設けられてい
るから、空気は連通口23・・・23カ)ら延長部13
・・・13への連通部B(第3図参照)でサージタンク
6内の大容積の内部空間16から分岐されることになり
、該連通部Bから上記延長部13・・・13と吸気通路
12・・・12との接続部Aを軽て各気筒9・・・9に
至るまで夫々独立した通路を通過することになる。
With the above configuration, when the engine 1 is operating, the air taken in from the air cleaner 3 shown in FIG. 1O... 1O and intake ports 8... 9 - Introduced into the internal space 16 of the rotating member 15, and distributed to each extension portion 13...13 from the communication ports 23...23 formed on the circumferential surface of the member 15. . After passing through each extension part 13...13 in a spiral shape, each cylinder passes through the intake passage 12...12 consisting of the branch pipe 10...10 and the intake port 8...8. This leads to 9...9. In that case, each of the above extension parts 13...13
Since they are provided independently by the partition walls 14...14, air flows from the communication ports 23...23) to the extension portion 13.
. . 13 is branched from the large volume internal space 16 in the surge tank 6 at the communication portion B (see Fig. 3), and from the communication portion B to the extension portions 13 . . . 13 and the intake air. The connecting portions A with the passages 12...12 are passed through independent passages until reaching each cylinder 9...9.

然して、エンジン1の回転数が低く、第4図に示す駆動
機構2/Iのダイヤフラム29に導入される排圧が低い
場合は、上記画成回動部材15は第3図に示す位置にあ
って、サージタンク6の内部空間16と各延長部13・
・・13との連通部Bも図= 10 = 示の位置にあるが、この状態からエンジン回転数が−F
昇して上記ダイ髪7フラム2つに導入される排圧が上昇
すると、駆動機構24における歯車27゜26を介して
回動部材15がa方向に回動されることにより、該連通
部Bもa方向に移動して、エンジン回転数が最高の状態
では例えば符号B′で示す位置に来る。つまり、エンジ
ン回転数の変化によって延長部13・・・13が上記位
置B、B’間で伸縮し、該延長部13・・・13と上記
吸気通路12・・・12とでなるサージタンク下流の独
立した通路長ざが変化することになる。これにより、上
記長さを各エンジン回転数に対して常に最適の長さとな
るように変化させれば、低回転数から高回転数までの広
いエンジン運転領域で吸気慣性効果を効果的に利用する
ことができることになる。
However, when the rotation speed of the engine 1 is low and the exhaust pressure introduced into the diaphragm 29 of the drive mechanism 2/I shown in FIG. 4 is low, the defining rotating member 15 is in the position shown in FIG. 3. The internal space 16 of the surge tank 6 and each extension part 13.
...The communication part B with 13 is also in the position shown in Figure 10, but from this state the engine speed is -F
When the exhaust pressure introduced into the two dye hair 7 flams increases, the rotary member 15 is rotated in the direction a via the gears 27 and 26 in the drive mechanism 24, so that the communication portion B The motor also moves in the direction a, and reaches the position indicated by the symbol B', for example, when the engine speed is at its highest. In other words, the extensions 13...13 expand and contract between the positions B and B' due to changes in engine speed, and the surge tank downstream of the extensions 13...13 and the intake passages 12...12 The length of the independent passages will change. As a result, if the above length is always changed to the optimum length for each engine speed, the intake inertia effect can be effectively utilized in a wide engine operating range from low to high speeds. You will be able to do that.

ところで、−]二記の梠或によれば、渦巻き状の延長部
13・・・13の長さを画成回動部材15の回動によっ
て変化させる構成であるから、吸気装置2の全体を大型
化することなく、該延長部13・・・13の長さを大き
な範囲(位置B、B’ 間の寸法)−11− で変化さけることができ、また一つの回動部材15を駆
動するだ(プで複数の延長部13・・・13の長ざを一
斉に変化させることができるから、駆動機構24や装置
の全体を少ない部品で簡素に構成することができるので
ある。
By the way, according to the second paragraph, since the length of the spiral extensions 13...13 is changed by the rotation of the defining rotation member 15, the entire intake device 2 can be changed. The length of the extension parts 13...13 can be varied within a large range (dimension between positions B and B') without increasing the size, and one rotating member 15 can be driven. Since the lengths of the plurality of extension parts 13 . . . 13 can be changed all at once by pressing the button, the drive mechanism 24 and the entire device can be simply constructed with fewer parts.

特に、上記各延長部13・・・13が下巻ぎ状とされて
各吸気通路12・・・12との接続部Aがサージタンク
6の上方部に設けられているから、第3図に示すように
斜め上方に傾斜している吸気ポート8・・・8に対して
吸気通路12・・・12〈分岐管1O・・・10)及び
延長部13・・・13を直線状に接続させても、サージ
タンク6の上端の位置が余り高くなることがなく、従っ
てエンジン1の全高を高くすることなく、しかも吸気が
スムーズに流れる通路を形成することができるのである
In particular, since each of the extension parts 13...13 is wound downward and the connection part A with each intake passage 12...12 is provided in the upper part of the surge tank 6, as shown in FIG. The intake passages 12...12 (branch pipes 1O...10) and extensions 13...13 are connected in a straight line to the intake ports 8...8 which are inclined diagonally upward as shown in FIG. Also, the position of the upper end of the surge tank 6 does not become too high, and therefore, the overall height of the engine 1 does not need to be increased, and a passage through which intake air flows smoothly can be formed.

更に、サージタンク6が吸気通路12・・・12の下方
に位置することに伴つ′″C該通路12・・・12の上
方にエンジン上端部より下方の範囲で広いスペースCが
確保されることになり、第3図に示すように該スペース
Cを利用して燃料噴射ノズル32− 12 − ・・・32を吸気通路12・・・12の上方に設置する
ことが可能どなる。つまり、一般に燃わ1噴射ノズルは
、組付()性或いは目詰まり防止等の点で吸気通路の−
F方に設置Jることが望ましいのである。
Furthermore, since the surge tank 6 is located below the intake passages 12...12, a wide space C is secured above the passages 12...12 in a range below the upper end of the engine. Therefore, it becomes possible to install the fuel injection nozzles 32-12-...32 above the intake passages 12...12 using the space C as shown in FIG. The fuel 1 injection nozzle is designed to be installed in the intake passage for ease of assembly and prevention of clogging.
It is desirable to install it on the F side.

尚、第5図に示すように画成回動部材15′にお(プる
連通口23′の下流側の縁部23a′を延長部13′に
滑らかに連続する形状とすれば、該回動部材115′ 
の内部空間16′から各延長部13′・・・13′への
空気の流出時における抵抗を小さくすることができ、ま
た同様の目的で第6図に示すように隣接づ−る連通口2
3’ 、23’間の仕切部231〕′の断面形状を内側
が丸味を有する形状としてもよい。
As shown in FIG. 5, if the downstream edge 23a' of the connecting port 23' is shaped to smoothly continue with the extension part 13', the rotating member 15' Moving member 115'
It is possible to reduce the resistance when air flows out from the internal space 16' to each extension part 13'...13', and for the same purpose, as shown in FIG.
The cross-sectional shape of the partition portion 231]' between 3' and 23' may be rounded on the inside.

(発 明 の 効 果) 以−にのように本発明によれば、吸気通路の長さを可変
とした多気筒エンジンの吸気装置において、上記吸気通
路の長さを広い範囲で変化させることができるど共に、
コンパクトで且つ簡素に構成され、しかもエンジン全高
を高くすることなく、吸気がスムーズに流れる吸気通路
を形成刃ることが−13− できるようになる。もって、この種の吸気通路の長さが
可変の吸気装置として、自動車用等のエンジンに適した
吸気装置が実用されることになる。
(Effects of the Invention) As described above, according to the present invention, in an intake system for a multi-cylinder engine in which the length of the intake passage is variable, the length of the intake passage can be varied over a wide range. Together as we can,
It is compact and simply configured, and it is possible to form an intake passage through which intake air flows smoothly without increasing the overall height of the engine. As a result, as this type of intake device with a variable length of the intake passage, an intake device suitable for automobile engines and the like will be put into practical use.

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

図面は本発明の実施例を示すもので、第1図は吸気装置
の全体を示す平面図、第2図は第1図■−IT線で切断
した拡大縦断側面図、第3図は第2図■−■線で切断し
た縦断正面図、第4図は駆動機構を示す背面図、第5図
は連通口周辺の他の実施例を示す要部縦断正面図、第6
図は同じく第5図Vl −Vl線で切断した要部横断平
面図である。 1・・・エンジン、2・・・吸気装置、6・・・サージ
タンク、9・・・気筒、12・・・吸気通路、13・・
・延長部、15・・・画成回動部材、16・・・内部空
間、23・・・連通口、24・・・駆動機構。 出願人 東洋工業株式会社 −14− 第5図 第6図 5b 1AC
The drawings show an embodiment of the present invention, and FIG. 1 is a plan view showing the entire intake system, FIG. Fig. 4 is a rear view showing the drive mechanism; Fig. 5 is a longitudinal sectional front view of main parts showing another embodiment around the communication port; Fig. 6 is a longitudinal sectional front view taken along the line
The figure is a cross-sectional plan view of the main part taken along the line Vl--Vl in Fig. 5. DESCRIPTION OF SYMBOLS 1... Engine, 2... Intake system, 6... Surge tank, 9... Cylinder, 12... Intake passage, 13...
- Extension portion, 15... Defining rotating member, 16... Internal space, 23... Communication port, 24... Drive mechanism. Applicant Toyo Kogyo Co., Ltd. -14- Figure 5 Figure 6 5b 1AC

Claims (1)

【特許請求の範囲】[Claims] (1) 吸気系の途中にり一−ジタンクを備え、該刀−
ジタンクから各気筒に夫々独立した吸気通路を設けた多
気筒エンジンの吸気装置であって、上記サージタンクの
周壁部に上記各吸気通路の延長部を夫々独立さ「て上下
方向に形成すると共に、各延長部の上方部に上記各吸気
通路の」−流端を夫々接続し、且つサージタンクの内部
空間と上記各延長部とを画成して両者を連通口により連
通させると共に延長部に沿って回動して上記連通口の位
置を変化させることにより1ノーージタンク下流の吸気
通路の長さを変化させる画成回動部材を設け、更に該画
成回動部材をエンジンの運転状態に応じて回動さ「る駆
動機構を備えたことを特徴とする多気筒エンジンの吸気
装置。
(1) A pilot tank is provided in the middle of the intake system, and the sword
An intake system for a multi-cylinder engine in which independent intake passages are provided from a surge tank to each cylinder, wherein extensions of each of the intake passages are formed independently in the vertical direction on a peripheral wall of the surge tank, and The flow ends of each of the above-mentioned intake passages are connected to the upper part of each extension, and the internal space of the surge tank and each of the above-mentioned extensions are defined so that they communicate with each other through a communication port, and the flow ends of each of the intake passages are connected to the upper part of each extension. A defining rotary member is provided that changes the length of the intake passage downstream of one nouge tank by rotating to change the position of the communication port, and the defining rotary member is rotated according to the operating state of the engine. An intake system for a multi-cylinder engine characterized by being equipped with a rotating drive mechanism.
JP58242698A 1983-12-21 1983-12-21 Air intake mechanism for multicylinder engine Pending JPS60132023A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP58242698A JPS60132023A (en) 1983-12-21 1983-12-21 Air intake mechanism for multicylinder engine
US06/683,836 US4619226A (en) 1983-12-21 1984-12-19 Intake device for internal combustion engine
DE3446377A DE3446377C2 (en) 1983-12-21 1984-12-19 Intake device for a piston internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58242698A JPS60132023A (en) 1983-12-21 1983-12-21 Air intake mechanism for multicylinder engine

Publications (1)

Publication Number Publication Date
JPS60132023A true JPS60132023A (en) 1985-07-13

Family

ID=17092910

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58242698A Pending JPS60132023A (en) 1983-12-21 1983-12-21 Air intake mechanism for multicylinder engine

Country Status (1)

Country Link
JP (1) JPS60132023A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62174528A (en) * 1986-01-27 1987-07-31 Hino Motors Ltd Intake manifold

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62174528A (en) * 1986-01-27 1987-07-31 Hino Motors Ltd Intake manifold

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