JPS6263129A - Suction device for engine - Google Patents

Suction device for engine

Info

Publication number
JPS6263129A
JPS6263129A JP60205786A JP20578685A JPS6263129A JP S6263129 A JPS6263129 A JP S6263129A JP 60205786 A JP60205786 A JP 60205786A JP 20578685 A JP20578685 A JP 20578685A JP S6263129 A JPS6263129 A JP S6263129A
Authority
JP
Japan
Prior art keywords
valve
intake
opening
shutter
accelerator pedal
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
JP60205786A
Other languages
Japanese (ja)
Inventor
Hiroyuki Oda
博之 小田
Akio Nagao
長尾 彰士
Masanori Misumi
三角 正法
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 JP60205786A priority Critical patent/JPS6263129A/en
Priority to US06/907,996 priority patent/US4714063A/en
Priority to DE19863631474 priority patent/DE3631474A1/en
Publication of JPS6263129A publication Critical patent/JPS6263129A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/32Controlling fuel injection of the low pressure type
    • F02D41/34Controlling fuel injection of the low pressure type with means for controlling injection timing or duration
    • F02D41/345Controlling injection timing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/08Modifying distribution valve timing for charging purposes
    • F02B29/083Cyclically operated valves disposed upstream of the cylinder intake valve, controlled by external means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B31/00Modifying induction systems for imparting a rotation to the charge in the cylinder
    • F02B31/08Modifying induction systems for imparting a rotation to the charge in the cylinder having multiple air inlets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/0002Controlling intake air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D9/00Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/02Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits concerning induction conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/20SOHC [Single overhead camshaft]
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/32Miller cycle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D9/00Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/02Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits concerning induction conduits
    • F02D2009/0201Arrangements; Control features; Details thereof
    • F02D2009/0279Throttle valve control for intake system with two parallel air flow paths, each controlled by a throttle, e.g. a resilient flap disposed on a throttle
    • 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
    • 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
    • Y02T10/40Engine management systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)
  • Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)

Abstract

PURPOSE:To secure a smooth increment characteristic in engine output, by controlling each valve for opening or closing with the specified process according to the opening of an accelerator pedal, in case of a device which installs a shutter valve in a suction passage and a rotary valve in a bypass passage bypassing the said shutter valve, respectively. CONSTITUTION:In case of a suction valve which installs a shutter valve each to a suction passage 10a to be connected to a suction port 3 of each cylinder side by side, and also installs a rotary valve 18 in the bypass passage 15a installed so as to bypass the shutter valve 11a side by side, this rotary valve 18 is controlled by a rotary valve controlling device 35 inclusive of a planetary gear mechanism 23 to be interlocked with a cam shaft 25. That is to say, valve close timing is delayed to some extent according to an increase in the opening of an accelerator pedal, and valve open timing is controlled so as to be almost overlapped with the valve open timing of a suction valve 5. In addition, the shutter valve 11a is controlled so as to increase its valve opening more than the specified pedal opening by degrees according to an increase of the pedal opening by a shutter valve controlling device 40.

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、特に低負荷域での
燃焼性の向上とボンピングロスの低減とを図るようにし
たものの改良に関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an engine intake system, and particularly to an improvement in the intake system for improving combustibility and reducing pumping loss in a low load range.

(従来の技術) 従来より、この種のエンジンの吸気IIIとして、例え
ば特開昭58−23245号公報に開示されるように、
アクセルペダル開度が所定開度以上で開くシャッタバル
ブを吸気通路に配置するとともに、該シャッタバルブを
バイパスする小径のバイパス通路に、カム軸の回転に対
して1/2の回転数比で回転するロータリバルブを配置
し、アクセルペダル開度が所定開度未満の低負荷域では
上記シャッタバルブの閉作動により吸気通路を閉じてバ
イパス通路のみから吸気を供給することにより、吸気の
流速を速め吸気のスワールを生成させて、燃焼性を向上
させると共に、上記ロータリバルブを吸気行程の途中で
閉じることにより、ポンピングロスを低減し、燃費性能
の向上を図るようにしたものが知られている。そして、
上記のものでは、低負荷域からアクセルペダルを所定開
面以上に踏込んだ高負荷時には、シャッタバルブが開作
動して吸気通路が聞くことにより、バイパス通路と共に
この吸気通路からも吸気が供給されて、出力の向上が図
られる。
(Prior Art) Conventionally, as an intake III for this type of engine, for example, as disclosed in Japanese Patent Application Laid-Open No. 58-23245,
A shutter valve that opens when the accelerator pedal opening is equal to or greater than a predetermined opening is arranged in the intake passage, and a small-diameter bypass passage that bypasses the shutter valve rotates at a rotation speed ratio of 1/2 to the rotation of the camshaft. A rotary valve is installed, and in a low load range where the accelerator pedal opening is less than a predetermined opening, the shutter valve is closed to close the intake passage and supply intake air only from the bypass passage, increasing the flow rate of intake air and increasing the intake air flow rate. It is known to generate swirl to improve combustibility, and to reduce pumping loss and improve fuel efficiency by closing the rotary valve in the middle of the intake stroke. and,
In the above model, when the accelerator pedal is depressed from a low load range to a high load, the shutter valve opens and the intake passage is exposed, and intake air is supplied from this intake passage as well as the bypass passage. As a result, output can be improved.

(発明が解決しようとする問題点) ところで、上記の如ぎシャッタバルブおよびロータリバ
ルブを備えたエンジンの吸気装置において、所定アクセ
ルペダル開度でシャッタバルブを開く場合、低負荷時に
はロータリバルブの吸気行程途中での閉弁によるいわゆ
るミラーサイクルによってポンピングロスの低減が図ら
れているものの、アクセルペダルの踏込によりアクセル
ペダル開度が所定開度に達してシャッタバルブが開かれ
ると、吸気通路からの吸気の供給により吸気終了タイミ
ングが吸気行程途中から通常の吸気行程終了時に急変し
て、ミラーサイクルから通常のサイクル(オツトーサイ
クル)に急激に切換わるため、トルクショックを生じ、
エンジン出力のスムーズな増大特性が1!7られないと
いう欠点が生じる。
(Problems to be Solved by the Invention) By the way, in an engine intake system equipped with a shutter valve and a rotary valve as described above, when opening the shutter valve at a predetermined opening degree of the accelerator pedal, the intake stroke of the rotary valve at low load. Pumping losses are reduced by the so-called mirror cycle, which is achieved by closing the valve midway, but when the accelerator pedal opening reaches a predetermined opening and the shutter valve is opened, the amount of intake air from the intake passage is reduced. Due to the supply, the intake end timing suddenly changes from the middle of the intake stroke to the end of the normal intake stroke, causing a sudden switch from the Miller cycle to the normal cycle (Otto cycle), causing torque shock.
This has the disadvantage that the engine output cannot be smoothly increased.

本発明は斯かる点に鑑みてなされたものであり、その目
的は、ロータリバルブの閉弁時期を可変制御し、シャッ
タバルブが開作動し始める所定アクセルペダル間度時に
は、ロークリバルブの閉弁時期を吸気行程終了時に一致
するよう吸気終了タイミングを移行させておくことによ
り、その後のシャッタバルブの開弁動作に伴うミラーサ
イクルからオート−サイクルへの切換えをスムーズに行
って、エンジンのトルクショックの発生を防止して、エ
ンジン出力のスムーズな増大特性を得ることにある。
The present invention has been made in view of the above, and its purpose is to variably control the closing timing of the rotary valve, and to control the closing timing of the rotary valve at a predetermined accelerator pedal distance when the shutter valve starts to open. By shifting the intake end timing so that it coincides with the end of the intake stroke, the subsequent switching from the mirror cycle to the auto cycle due to the opening of the shutter valve can be performed smoothly, and the occurrence of torque shock in the engine can be prevented. The objective is to prevent this problem and obtain a smooth increase characteristic of engine output.

(問題点を解決するための手段) 上記の目的を達成するため、本発明の解決手段は、吸気
通路に該吸気通路を開閉するシャッタバルブを配置する
と共に、該シャッタバルブをバイパスするバイパス通路
に該バイパス通路を開閉するロータリバルブを配置し、
低負荷域で上記シトツタバルブを閉じると共に上記ロー
タリバルブを吸気行程の途中で閉じるようにしたエンジ
ンの吸気装置を前提とする。そして、上記ロータリバル
ブの閉弁時期をアクセルペダル開度の増大に応じて遅ら
せ、所定アクセルペダル開度でロータリバルブの開弁期
間を吸気弁の開弁期間にほぼオーバラップさせるロータ
リバルブ制御手段と、上記シャッタバルブの開度を上記
所定アクセルペダル開度より漸次アクセルペダル開度の
増大に応じて増大させるシャッタバルブ制御手段とを備
える構成としたものである。
(Means for Solving the Problems) In order to achieve the above object, the solving means of the present invention includes disposing a shutter valve in the intake passage for opening and closing the intake passage, and providing a bypass passage for bypassing the shutter valve. A rotary valve is arranged to open and close the bypass passage,
The present invention is based on an engine intake system in which the above-mentioned stub valve is closed in a low load range, and the above-mentioned rotary valve is closed during the intake stroke. and rotary valve control means for delaying the closing timing of the rotary valve in accordance with an increase in the accelerator pedal opening, and causing the opening period of the rotary valve to substantially overlap the opening period of the intake valve at a predetermined accelerator pedal opening. and shutter valve control means for increasing the opening degree of the shutter valve from the predetermined accelerator pedal opening degree gradually in response to an increase in the accelerator pedal opening degree.

(作用) 以上の構成により、本発明では、所定アクセルペダル開
度未満の低負荷域では、シャッタバルブは開状態にあっ
てバイパス通路のみから吸気が供給されるので、吸気流
速が早くなり、吸気スワールが生成されて燃焼性が向上
すると共に、ロータリバルブが吸気行程途中で閉じてミ
ラーサイクルになるので、ボンピングロスが効果的に低
減されて燃費性能の向上が図られる。
(Function) With the above configuration, in the present invention, in the low load range below the predetermined accelerator pedal opening, the shutter valve is in the open state and intake air is supplied only from the bypass passage, so the intake air flow rate becomes faster and the intake air Swirl is generated to improve combustion performance, and since the rotary valve closes during the intake stroke to create a Miller cycle, pumping loss is effectively reduced and fuel efficiency is improved.

また、アクセルペダル開度の増大時、上記低負荷域では
ロータリバルブの閉弁時期が漸次遅れることにより吸入
空気量が次第に増大するとともに、その後、所定アクセ
ルペダル聞痕に至ると、ロークリバルブの開弁期間が吸
気弁の開弁期間にほぼオーバラップして吸気終了タイミ
ングが吸気行程終了時に移行し、この時点でシトツタバ
ルブが開作動し始めるので、ミラーサイクルからオツト
ーサイクルへの切換えがスムーズに行われて、吸気通路
からも吸気が供給されて吸入空気量が増大し、その結果
、トルクショックなくエンジン出力がスムーズに増大す
ることになる。
In addition, when the accelerator pedal opening increases, the intake air amount gradually increases due to the gradual delay in the closing timing of the rotary valve in the above-mentioned low load range, and then, when the accelerator pedal reaches a predetermined level, the rotary valve opens. The period almost overlaps with the intake valve opening period, and the intake end timing shifts to the end of the intake stroke, and at this point the Shitotsuta valve begins to open, so the switch from the Miller cycle to the Otto cycle is performed smoothly. As a result, intake air is also supplied from the intake passage, increasing the amount of intake air, and as a result, the engine output increases smoothly without torque shock.

(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図および第2図は4気筒4サイクルエンジンの吸気
装置に適用した実施例を示す。同図において、1は第1
〜第4気筒18〜1dを有するエンジン、2はエンジン
1の各気筒1a〜1(1に形成される燃焼室であって、
該6燃焼室2には吸気ボート3と排気ポート4とが開口
されていて、吸気ボート3の燃焼室2への開口部には吸
気弁5が、排気ボート4の燃焼室2への開口部には排気
弁6が各々配設されている。
FIG. 1 and FIG. 2 show an embodiment applied to an intake system for a four-cylinder, four-cycle engine. In the same figure, 1 is the first
-An engine having fourth cylinders 18 to 1d, 2 is a combustion chamber formed in each cylinder 1a to 1 (1) of the engine 1,
An intake boat 3 and an exhaust port 4 are opened in the six combustion chambers 2, an intake valve 5 is located at the opening of the intake boat 3 to the combustion chamber 2, and an intake valve 5 is located at the opening of the exhaust boat 4 to the combustion chamber 2. An exhaust valve 6 is disposed at each of the exhaust valves 6.

また、10a〜10dは一端が大気に連通し他端が吸気
ボート3を介して各燃焼室2に開口してエンジン1の各
気筒1a〜1dに吸気を供給する吸気通路であって、該
各吸気通路10a〜10dの吸気ボート3近1労には、
各吸気通路10a〜10dを開閉するシャッタバルブI
la〜11dが配置されていて、該各シャッタバルブ1
1a〜11dは、気筒列方向に配置した弁軸12に一連
に連動可能に連結されており、スプリング14によって
閉方向に付勢されている。また、各吸気通路10a〜1
0dのシtツタパルプ11a 〜11d直下流には、そ
れぞれ燃料を噴射供給する燃料噴射弁13が配設されて
いる。
Reference numerals 10a to 10d are intake passages whose one end communicates with the atmosphere and whose other end opens into each combustion chamber 2 via an intake boat 3 to supply intake air to each cylinder 1a to 1d of the engine 1; In the intake boats 3 and 1 of the intake passages 10a to 10d,
Shutter valve I that opens and closes each intake passage 10a to 10d
la to 11d are arranged, and each shutter valve 1
1a to 11d are serially connected to a valve shaft 12 disposed in the direction of the cylinder row, and are biased in the closing direction by a spring 14. In addition, each intake passage 10a to 1
Immediately downstream of the shita pulp 11a to 11d of 0d, fuel injection valves 13 for injecting and supplying fuel are respectively disposed.

上記各吸気通路108〜10dには、各々吸気通路10
a〜10dのシャッタバルブ118〜11d上流側と吸
気ボート3とをシャッタバルブ118〜11dをバイパ
スして連通ずる第1ないし第4のバイパス通路158〜
15dが設けられている。該各バイパス通路158〜1
5dはその通路断面積が吸気通路108〜10dよりも
小に設定され、且つその下流端間口部が燃焼室2の周方
向に向って開口していて、吸入空気をバイパス通路15
a〜15dを通して燃焼室2に吸入させることにより、
燃焼室2内に周方向に沿って旋回する吸気スワールを生
成させるようになされている。
Each of the above-mentioned intake passages 108 to 10d includes an intake passage 10
The first to fourth bypass passages 158 to 158 communicate the upstream side of the shutter valves 118 to 11d of a to 10d and the intake boat 3 by bypassing the shutter valves 118 to 11d.
15d is provided. Each bypass passage 158-1
5d has a passage cross-sectional area smaller than that of the intake passages 108 to 10d, and its downstream end opening opens toward the circumferential direction of the combustion chamber 2, directing intake air to the bypass passage 15.
By inhaling into the combustion chamber 2 through a to 15d,
An intake swirl is generated in the combustion chamber 2 along the circumferential direction.

そして、上記各バイパス通路158〜15dの途中には
、気筒列方向に配置せしめた円筒部材16内にスリーブ
17を介して回転可能に配置した1つのロータリバルブ
18が共通して介設されている。該ロータリバルブ18
は中空体のもので構成され、且つその第1気筒1a側の
端部は後述する遊星歯車機構23のサンギヤ31の回転
111d131aを嵌入せしめて)l塞され、またその
第4気筒1d側の端部は閉塞部材19で閉塞されて、内
部に袋形状の吸気供給用通路20が形成されているとと
もに、各バイパス通路15a〜15dに対向する外周部
には、対応する気vR1a〜1dの吸気行程に対応する
角度範囲で吸気弁5の開弁期間に相当する部分が周方向
に切欠かれて開口18aが形成されており、該ロータリ
バルブ18の回転に伴いその外周部の各開口18aが該
ロータリバルブ18下流側のバイパス通路15a〜15
dに連通した開弁時には、吸気弁5の開閉状態に応じて
吸気を各バイパス通路15a〜15dを通して燃焼室2
に供給可能にしている。
In the middle of each of the bypass passages 158 to 15d, a single rotary valve 18 rotatably disposed within a cylindrical member 16 disposed in the cylinder row direction via a sleeve 17 is interposed in common. . The rotary valve 18
is made of a hollow body, and its end on the first cylinder 1a side is closed by fitting the rotation 111d131a of the sun gear 31 of the planetary gear mechanism 23, which will be described later, and its end on the fourth cylinder 1d side is closed. The section is closed with a closing member 19, and a bag-shaped intake air supply passage 20 is formed inside, and the outer periphery facing each bypass passage 15a to 15d is provided with an intake stroke of the corresponding air vR1a to 1d. An opening 18a is formed by cutting out a portion corresponding to the opening period of the intake valve 5 in the circumferential direction in an angular range corresponding to the rotation of the rotary valve 18. Bypass passages 15a to 15 on the downstream side of the valve 18
When the valve is opened and communicated with
We are making it possible to supply.

また、上記ロータリパルプ18の第1気[1a側の端部
には、遊星歯車機構23を介して該ロータリバルブ18
回転駆動用の大径のプーリ24が接続され、該プーリ2
4には、燃焼室2上方に気筒列方向に配置せしめたカム
軸25の端部に設けた小径のプーリ26との間でベルト
27が巻掛けられており、カム軸25の回転によりロー
タリパルプ18を回転駆動するようになされている。上
記遊星歯車機構23は、上記大径のブー924に同軸に
連結されたリングギヤ28と、該リングギヤ28に噛合
しキャリア29で相互に連結された3個の遊星ギヤ30
と、該各遊星ギヤ30に噛合するサンギヤ31とから成
り、該31)2星歯車機構23の変速比は、カム軸25
に対するロータリパルプ18の回転数の比が「1」にな
るように予め設定されている。また、上記ロータリバル
ブ18の各開口18aは、遊星歯車機構23の遊星ギヤ
30が各々図示の初期位置にあるアクセルペダルの非踏
込時において、各バイパス通路15a〜15dをそれぞ
れその吸気行程途中の所定時期で閉じるよう予め位置付
けられている。さらに、上記遊星歯車機構23のキャリ
ア2つはワイヤ一部材32を介してアクセルペダル(図
示せず)に接続されていて、アクセルペダルの踏込操作
によりキャリア29が第2図時計方向に回転して、リン
グギヤ28とサンギヤ31との相対位置をずらすことに
より、ロータリバルブ18の各間口18aの位置を第2
図時計方向に漸次回転変位させて、第3図に示すように
ロータリパルプ18の閉弁時期をアクセルペダル開度の
増大に応じて次第に遅らせ、所定アクセルペダル開度O
Aでその閉弁時期を吸気行程終了時に一致させてロータ
リバルブ18の開弁期間を吸気弁5の開弁期間にほぼオ
ーバラップさせるようにしたロータリバルブ制御手段3
5を構成している。
Further, the rotary valve 18 is connected to the end of the rotary pulp 18 on the first air [1a side] via a planetary gear mechanism 23.
A large diameter pulley 24 for rotational driving is connected, and the pulley 2
4, a belt 27 is wound around a small diameter pulley 26 provided at the end of a camshaft 25 arranged above the combustion chamber 2 in the direction of the cylinder row, and the rotation of the camshaft 25 causes rotary pulp 18 to rotate. The planetary gear mechanism 23 includes a ring gear 28 coaxially connected to the large-diameter boob 924, and three planetary gears 30 meshing with the ring gear 28 and interconnected by a carrier 29.
and a sun gear 31 that meshes with each of the planetary gears 30, and the gear ratio of the two-star gear mechanism 23 is
The ratio of the rotation speed of the rotary pulp 18 to the rotation speed of the rotary pulp 18 is set in advance to be "1". Further, each opening 18a of the rotary valve 18 opens each bypass passage 15a to 15d to a predetermined position in the middle of its intake stroke when the accelerator pedal is not depressed and the planetary gear 30 of the planetary gear mechanism 23 is at the initial position shown. It is pre-positioned to close at a certain time. Further, the two carriers of the planetary gear mechanism 23 are connected to an accelerator pedal (not shown) via a wire member 32, and when the accelerator pedal is depressed, the carrier 29 rotates clockwise in FIG. , by shifting the relative positions of the ring gear 28 and the sun gear 31, the position of each opening 18a of the rotary valve 18 is changed to a second position.
The valve closing timing of the rotary pulp 18 is gradually delayed as the accelerator pedal opening increases to a predetermined accelerator pedal opening as shown in FIG.
A rotary valve control means 3 whose valve closing timing coincides with the end of the intake stroke so that the valve opening period of the rotary valve 18 almost overlaps with the valve opening period of the intake valve 5.
5.

加えて、遊星歯車機構23の3個の遊星ギV30のうち
上方に位置するものには、シャッタバルブ11a〜11
dの弁軸12方向に延びる第1リンク36および、該第
1リンク36の端部に形成した長手方向の切欠き孔37
に係合する係合ビン38を有する第2リンク39を介し
て上記シャッタバルブIia〜11dの弁軸12の端部
が連結されていて、上記第1リンク36の切欠き孔37
の長さは、アクセルペダル開度が110 II値から上
記所定アクセルペダル開a OAに達するまでに相当す
る長さに設定されている。よって、第3図に示すように
アクセルペダルの踏込時、その初期時には第1リンク3
6が第2図右方に移動するものの、第2リンク39の係
合ビン38が上記第1リンク36の切欠き孔37内を移
動してシャッタバルブIla〜11dは閉状態を維持す
る一方、所定アクセルペダル開度OAに達すると、第2
リンク39の係合ビン38が第1リンク36に係合して
シャッタバルブ11a〜11dの弁軸12が第2図時計
方向に回転して、各シャッタバルブ11a〜11dをア
クセルペダル171mの増大に応じて漸次増大させるよ
うにしたシャッタバルブ制御手段40を構成している。
In addition, the upper one of the three planetary gears V30 of the planetary gear mechanism 23 has shutter valves 11a to 11.
d, a first link 36 extending in the direction of the valve shaft 12, and a longitudinal notch hole 37 formed at the end of the first link 36.
The ends of the valve shafts 12 of the shutter valves Iia to 11d are connected via a second link 39 having an engagement pin 38 that engages with the notch hole 37 of the first link 36.
The length is set to a length corresponding to the time the accelerator pedal opening reaches from the 110 II value to the predetermined accelerator pedal opening aOA. Therefore, as shown in FIG. 3, when the accelerator pedal is depressed, the first link 3
6 moves to the right in FIG. 2, the engagement pin 38 of the second link 39 moves within the notch hole 37 of the first link 36, and the shutter valves Ila to 11d maintain the closed state, When the predetermined accelerator pedal opening degree OA is reached, the second
The engagement pin 38 of the link 39 engages with the first link 36, and the valve shafts 12 of the shutter valves 11a to 11d rotate clockwise in FIG. A shutter valve control means 40 is configured to gradually increase the number of shutter valves accordingly.

尚、第2図中、41は各燃料噴射弁13の噴口13aの
近傍にアシストエアを供給するためのアシストエア通路
であって、該アシストエア通路41の一端は吸気通路1
08〜10dの集合部上流に配置したエアクリーナ(図
示せず)に連通し、他端は燃料噴射弁13の先端部に被
冠されたキャップ42に設けた多数の小孔42a・・・
を介して該燃料噴射弁13の噴口13a近傍に連通して
おり、バイパス通路15a〜1.56のみから吸気を供
給する低負荷時、つまり燃料噴射弁13周りに吸気流れ
のない状態時には、燃料噴射弁13からの燃料を上記ア
シストエア通路41からのアシストエアにより微粒化し
て、燃焼室2内での混合気の燃焼を良好に行わせるよう
になされている。
In FIG. 2, reference numeral 41 indicates an assist air passage for supplying assist air to the vicinity of the injection port 13a of each fuel injection valve 13, and one end of the assist air passage 41 is connected to the intake passage 1.
The other end is connected to an air cleaner (not shown) disposed upstream of the collecting part of fuel injection valves 13, and has a large number of small holes 42a...
It communicates with the vicinity of the nozzle 13a of the fuel injection valve 13 through the bypass passages 15a to 1.56, and when the load is low, in which intake air is supplied only from the bypass passages 15a to 1.56, that is, when there is no intake air flow around the fuel injection valve 13, the fuel The fuel from the injection valve 13 is atomized by the assist air from the assist air passage 41, so that the air-fuel mixture within the combustion chamber 2 can be burnt efficiently.

したがって、上記実施例においては、シャッタバルブ1
1a〜11dが閉状態にある低負荷時には、吸気がバイ
パス通路15a〜15dのみから燃焼室2に供給される
ので、吸気流速が速くなると共に吸気にスワールが生成
されて燃焼性の向上が図られる。また、ロークリバルブ
18によって吸気終了タイミングが吸気行程の途中に設
定されるので、ボンピングロスが低減され、その結果、
燃費性能の向上が図られる。しかも、その際には、上記
吸気行程途中での吸気終了に伴い次の圧縮行程での有効
圧縮比が低下し、混合気の燃焼温度は低下する状況にな
るものの、吸気にスワールが生成されているので、燃焼
性は良好に確保される。
Therefore, in the above embodiment, the shutter valve 1
During low load when 1a to 11d are in the closed state, intake air is supplied to the combustion chamber 2 only from the bypass passages 15a to 15d, so that the intake air flow rate increases and a swirl is generated in the intake air to improve combustibility. . In addition, since the intake end timing is set in the middle of the intake stroke by the low revalve 18, the pumping loss is reduced, and as a result,
Improved fuel efficiency is achieved. Moreover, in this case, as the intake ends in the middle of the intake stroke, the effective compression ratio in the next compression stroke decreases, and although the combustion temperature of the mixture decreases, a swirl is generated in the intake. Therefore, good flammability is ensured.

また、アクセルペダルの踏込時には、アクセルペダル開
度の増大に応じてロークリバルブ18の開弁時期がロー
タリバルブ制御手段35によりばれ制御されて吸入空気
量が漸次増大し、その後、所定アクセルペダル開度〇へ
の時点でロータリバルブ18の閉弁時期が吸気行程終了
時に一致してロータリバルブ1Bの開弁期間が吸気弁5
の開弁期間にほぼオーバラップすると、この時点からシ
ャッタバルブ11a〜11dの開度がシャッタバルブ制
御手段40によりアクセルペダル開度の増大に応じて漸
次増大制御されるので、さらに吸入空気量が次第に増大
して、エンジン出力の向上が図られることになる。
Further, when the accelerator pedal is depressed, the opening timing of the low-return valve 18 is controlled by the rotary valve control means 35 in accordance with the increase in the accelerator pedal opening, and the intake air amount is gradually increased, and then the predetermined accelerator pedal opening is increased. At the point in time, the closing timing of the rotary valve 18 coincides with the end of the intake stroke, and the opening period of the rotary valve 1B coincides with the end of the intake stroke.
When the opening period of the shutter valves 11a to 11d almost overlaps, from this point on, the opening degrees of the shutter valves 11a to 11d are gradually increased by the shutter valve control means 40 in accordance with the increase in the opening degree of the accelerator pedal, so that the amount of intake air gradually increases. As a result, the engine output is improved.

その際、シャッタバルブ11a〜11dの開弁開始は、
所定アクセルペダル開度OAの位置でロータリバルブ1
8の開弁時期が吸気行程終了時に一致した時点で行われ
るので、いわゆるミラーサイクルからオツトーサイクル
への切換えがスムーズに行われてトルクショックを防止
することができ、よってエンジン出力のスムーズな増大
を確保することができる。
At that time, the start of opening of the shutter valves 11a to 11d is as follows.
Rotary valve 1 at the position of the predetermined accelerator pedal opening OA
Since the valve opening timing of 8 coincides with the end of the intake stroke, the switching from the so-called Miller cycle to the Otto cycle is performed smoothly and torque shock can be prevented, resulting in a smooth increase in engine output. can be ensured.

さらに、〇−タリバル718はカム軸25に対して1:
1で回転するので、従来の如くカム軸25に対して1/
2の回転数比で回転するものに比べて、ロータリバルブ
18の間弁明間中でのバイパス通路15a〜15dの有
効開口面積が増大して、吸入空気量の増大を図ることが
できる。しかも、上記カム軸25に対するロークリバル
ブ18の1:1の回転に伴い、ロータリバルブ18の各
開口18aの位置が所定気筒(例えば第1気筒1a)と
これより2行程遅れる気筒(第4気筒1d)との間で回
転角度で180°の位相差を生じた位置にあるので、所
定気筒(例えば第1気R9j1a ’)に対応する開口
18aがロータリバルブ18下流側の第1バイパス通路
15aに連通したときには、該第1気筒1aに対して2
行程遅れる第4気筒1dに対応する開口18aがロータ
リバルブ18上流側の第4バイパス通路15dに連通し
て、吸気が第4バイパス通路15dからロータリパル1
18内の吸気供給用通路20を介して第1バイパス通路
15aに供給されるので、他のパイピングを不要にして
構成の簡易化を図ることができる。
Furthermore, 〇-Taribal 718 is 1 for the camshaft 25:
Since it rotates at a rate of 1/1, the rotation rate is 1/1 with respect to the camshaft 25 as in the conventional case.
Compared to a rotary valve rotating at a rotational speed ratio of 2, the effective opening area of the bypass passages 15a to 15d during the opening period of the rotary valve 18 is increased, and the amount of intake air can be increased. Furthermore, due to the 1:1 rotation of the rotary valve 18 with respect to the camshaft 25, the positions of the openings 18a of the rotary valve 18 are different from the position of a predetermined cylinder (for example, the first cylinder 1a) and the cylinder two strokes later than this (the fourth cylinder 1d). Since the opening 18a corresponding to the predetermined cylinder (for example, the first air R9j1a') is located at a position where a phase difference of 180 degrees occurs in the rotation angle between the rotary valve 18 and the first bypass passage 15a on the downstream side of the rotary valve 18, Sometimes, 2 cylinders 1a and 2
The opening 18a corresponding to the fourth cylinder 1d whose stroke is delayed communicates with the fourth bypass passage 15d on the upstream side of the rotary valve 18, and the intake air flows from the fourth bypass passage 15d to the rotary valve 1.
Since the air is supplied to the first bypass passage 15a through the intake air supply passage 20 in the intake air supply passage 18, the structure can be simplified by eliminating the need for other piping.

また、第4図および第5図は本発明の他の実施例を示し
、上記実施例では、燃料噴射弁13を備えたエンジンに
対して適用したのに代え、気化器を備えたものに適用し
たものである。すなわち、吸気通路10’a〜10′d
の集合部上流側には気化器43が配置されているととも
に、該気化器43下方には、各気筒1a〜1dの各バイ
パス通路15’a〜15′dと連通ずる主バイパス通路
44が気筒列方向に配置されていて、気化器43からの
混合気を吸気通路10′a〜10’d集合部に供給する
とともに、主バイパス通路44を通して各バイパス通路
15′a〜15′dに供給するようになされており、他
の構成は上記実施例と同様である。よって、上記実施例
と同様に、低負荷域では速い吸気流速と吸気スワールに
より燃焼性の向上を図るとともに、ロータリバルブの吸
気行程途中での閉弁によりボンピングロスを低減しつつ
、アクセルペダル開度の増大時にはミラー、サイクルか
ら通常のオツトーサイクルへの切換えをスムーズに行い
得て、エンジン出力のスムーズな増大特性を得ることが
できる。
Further, FIGS. 4 and 5 show other embodiments of the present invention, and in the above embodiment, instead of being applied to an engine equipped with a fuel injection valve 13, it is applied to an engine equipped with a carburetor. This is what I did. That is, the intake passages 10'a to 10'd
A carburetor 43 is arranged on the upstream side of the gathering part of the cylinders, and below the carburetor 43, a main bypass passage 44 communicating with each bypass passage 15'a to 15'd of each cylinder 1a to 1d is arranged. They are arranged in the row direction, and supply the air-fuel mixture from the carburetor 43 to the intake passages 10'a to 10'd gathering portion, and also to the respective bypass passages 15'a to 15'd through the main bypass passage 44. The other configurations are the same as those in the above embodiment. Therefore, as in the above embodiment, in the low load range, combustion performance is improved by high intake flow velocity and intake swirl, and while reducing pumping loss by closing the rotary valve in the middle of the intake stroke, the accelerator pedal opening is reduced. When the engine power increases, the mirror cycle can be smoothly switched to the normal automatic cycle, and a smooth increase in engine output can be achieved.

尚、上記実施例では−、ロータリバルブ制御手段35お
よびシャッタバルブ制御手段40を、それぞれ遊星歯車
機構23を備えた機械式のもので構成したが、その他、
ロータリバルブ18およびシャッタバルブ11a〜11
dを各々アクセルペダル開度に応じて電気的に作動制御
するもので構成してもよい。
Incidentally, in the above embodiment, the rotary valve control means 35 and the shutter valve control means 40 are each constituted by a mechanical type equipped with a planetary gear mechanism 23, but other than that,
Rotary valve 18 and shutter valves 11a to 11
d may be electrically controlled depending on the degree of opening of the accelerator pedal.

(発明の効果) 以上説明したように、本発明のエンジンの吸気装置によ
れば、低負荷域ではバイパス通路のみからの吸気の供給
により吸気スワールを生成させて燃焼性の向上を図ると
ともに、ロータリバルブの吸気行程途中での開弁により
ボンピングロスの低減を図りつつ、アクセルペダルの踏
込時には、吸入空気量を上記ロータリバルブの閉弁時期
の遅れ制御およびこれに続くシャッタバルブ開度の増大
1IIII@により行い、上記シャッタバルブの開弁開
始時を、ロータリバルブの閉弁時期が吸気行程終了時に
一致する時点に設定して、いわゆるミラーサイクルから
オツトーサイクルへの切換えをスムーズに行うようにし
たので、トルクショックを防止してエンジン出力のスム
ーズな増大を確保することができ、エンジン性能の向上
を図ることができる。
(Effects of the Invention) As explained above, according to the engine intake system of the present invention, in a low load range, intake air is supplied only from the bypass passage to generate an intake swirl to improve combustibility. While reducing pumping loss by opening the valve during the intake stroke, when the accelerator pedal is depressed, the amount of intake air is controlled to delay the closing timing of the rotary valve, and the shutter valve opening is subsequently increased.1III@ The above-mentioned shutter valve opening time is set at the time when the rotary valve closing time coincides with the end of the intake stroke to smoothly switch from the so-called Miller cycle to the Otto cycle. , it is possible to prevent torque shock, ensure smooth increase in engine output, and improve engine performance.

【図面の簡単な説明】 図面は本発明の実施例を示し、第1図は4気筒エンジン
の吸気装置に適用した場合の横断面図、第2図は第1図
のII−II線断面図、第3図は各々ロータリバルブお
よびシャッタパルプのアクセルペダル開度の増大に対す
る開度特性を示す図、第4図および第5図は他の実施例
を示し、第4図は第1図相当図、第5図は第2図相当図
である。 1・・・エンジン、2・・・燃焼!、5・・・吸気弁、
10a〜10d11o′a〜10′d・・・吸気通路、
11 a 〜11 d−・・シャッタバルブ、158〜
15d 。 15′a〜15′d・・・バイパス通路、18・・・ロ
ータリバルブ、18a・・・開口、20・・・吸気供給
用通路、23・・・遊星歯車機構、35・・・ロータリ
バルブ制御手段、37・・・切欠き孔、39・・・第2
リンク、40・・・シャッタバルブ制御手段、42・・
・主バイパス通路。 :Ij″jふ− 第1図 第5図
[BRIEF DESCRIPTION OF THE DRAWINGS] The drawings show an embodiment of the present invention, and FIG. 1 is a cross-sectional view when applied to an intake system of a four-cylinder engine, and FIG. 2 is a cross-sectional view taken along the line II-II in FIG. 1. , FIG. 3 is a diagram showing the opening characteristics of the rotary valve and the shutter pulp with respect to an increase in the accelerator pedal opening, respectively. FIGS. 4 and 5 show other embodiments, and FIG. 4 is a diagram corresponding to FIG. 1. , FIG. 5 is a diagram corresponding to FIG. 2. 1...engine, 2...combustion! , 5... Intake valve;
10a to 10d11o'a to 10'd...Intake passage,
11 a to 11 d--Shutter valve, 158-
15d. 15'a to 15'd... Bypass passage, 18... Rotary valve, 18a... Opening, 20... Intake supply passage, 23... Planetary gear mechanism, 35... Rotary valve control means, 37... notch hole, 39... second
Link, 40... Shutter valve control means, 42...
・Main bypass passage. :Ij″jfu- Figure 1 Figure 5

Claims (1)

【特許請求の範囲】[Claims] (1)吸気通路に配置され該吸気通路を開閉するシャッ
タバルブと、該シャッタバルブをバイパスするバイパス
通路に配置され該バイパス通路を開閉するロータリバル
ブとを有し、低負荷域で上記シャッタバルブを閉じると
共に上記ロータリバルブを吸気行程途中で閉じるように
したエンジンの吸気装置において、上記ロータリバルブ
の閉弁時期をアクセルペダル開度の増大に応じて遅らせ
、所定アクセルペダル開度でロータリバルブの開弁期間
を吸気弁の開弁期間にほぼオーバラップさせるロータリ
バルブ制御手段と、上記シャッタバルブの開度を上記所
定アクセルペダル開度より漸次アクセルペダル開度の増
大に応じて増大させるシャッタバルブ制御手段とを備え
たことを特徴とするエンジンの吸気装置。
(1) A shutter valve disposed in an intake passage to open and close the intake passage, and a rotary valve disposed in a bypass passage bypassing the shutter valve to open and close the bypass passage, and the shutter valve operates in a low load range. In this engine intake system, the rotary valve is closed in the middle of the intake stroke, and the rotary valve is delayed in accordance with an increase in accelerator pedal opening, and the rotary valve is opened at a predetermined accelerator pedal opening. rotary valve control means for causing a period to substantially overlap an opening period of the intake valve; and shutter valve control means for increasing the opening degree of the shutter valve from the predetermined accelerator pedal opening degree gradually in response to an increase in the accelerator pedal opening degree. An engine intake device characterized by comprising:
JP60205786A 1985-09-17 1985-09-17 Suction device for engine Pending JPS6263129A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP60205786A JPS6263129A (en) 1985-09-17 1985-09-17 Suction device for engine
US06/907,996 US4714063A (en) 1985-09-17 1986-09-16 Intake system for internal combustion engine
DE19863631474 DE3631474A1 (en) 1985-09-17 1986-09-16 INTAKE SYSTEM FOR AN INTERNAL COMBUSTION ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60205786A JPS6263129A (en) 1985-09-17 1985-09-17 Suction device for engine

Publications (1)

Publication Number Publication Date
JPS6263129A true JPS6263129A (en) 1987-03-19

Family

ID=16512649

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60205786A Pending JPS6263129A (en) 1985-09-17 1985-09-17 Suction device for engine

Country Status (1)

Country Link
JP (1) JPS6263129A (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57173526A (en) * 1981-04-20 1982-10-25 Mazda Motor Corp Intake device of engine

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57173526A (en) * 1981-04-20 1982-10-25 Mazda Motor Corp Intake device of engine

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