JPS6035115A - Laminar charging engine - Google Patents

Laminar charging engine

Info

Publication number
JPS6035115A
JPS6035115A JP58144265A JP14426583A JPS6035115A JP S6035115 A JPS6035115 A JP S6035115A JP 58144265 A JP58144265 A JP 58144265A JP 14426583 A JP14426583 A JP 14426583A JP S6035115 A JPS6035115 A JP S6035115A
Authority
JP
Japan
Prior art keywords
fuel
air
injection valve
engine
fuel injection
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP58144265A
Other languages
Japanese (ja)
Other versions
JPH0478813B2 (en
Inventor
Hiroyuki Oda
博之 小田
Masakimi Kono
河野 誠公
Haruo Okimoto
沖本 晴男
Shinichi Tamura
伸一 田村
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 JP58144265A priority Critical patent/JPS6035115A/en
Publication of JPS6035115A publication Critical patent/JPS6035115A/en
Publication of JPH0478813B2 publication Critical patent/JPH0478813B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10209Fluid connections to the air intake system; their arrangement of pipes, valves or the like
    • F02M35/10216Fuel injectors; Fuel pipes or rails; Fuel pumps or pressure regulators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B17/00Engines characterised by means for effecting stratification of charge in cylinders
    • F02B17/005Engines characterised by means for effecting stratification of charge in cylinders having direct injection in the combustion chamber
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/24Cylinder heads
    • F02F1/42Shape or arrangement of intake or exhaust channels in cylinder heads
    • F02F1/4214Shape or arrangement of intake or exhaust channels in cylinder heads specially adapted for four or more valves per cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/104Intake manifolds
    • F02M35/108Intake manifolds with primary and secondary intake passages
    • F02M35/1085Intake manifolds with primary and secondary intake passages the combustion chamber having multiple intake valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/104Intake manifolds
    • F02M35/112Intake manifolds for engines with cylinders all in one line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
    • 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
    • F02B75/12Other methods of operation
    • F02B2075/125Direct injection in the combustion chamber for spark ignition engines, i.e. not in pre-combustion chamber
    • 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
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M23/00Apparatus for adding secondary air to fuel-air mixture
    • F02M2023/008Apparatus for adding secondary air to fuel-air mixture by injecting compressed air directly into the combustion chamber

Abstract

PURPOSE:To accelerate atomization and evaporation and improve ignition performance by jetting-out fuel into a spark plug at a prescribed time in the course ranging from the latter half of intake cycle to compression cycle and mixing the air into the jetted-out fuel in the latter half of fuel injection. CONSTITUTION:In an engine in which the primary and the secondary intake ports 13 and 14 and an exhaust port 15 which are opened to the combustion chamber 7 of each cylinder are opened and closed by the primary and the secondary side intake valves 16 and 17 and an exhaust valve 18, a spark plug 20 is installed nearly at the center in the combustion chamber 7, and a fuel injection valve 21 is installed so that the jetted-out fuel is directed towards the spark plug 20. An air injection valve 22 is installed closely to the fuel injection valve 21 so that air is jetted-out in the direction in which interference with jetted-out fuel is generated. In low loaded state, the fuel injection valve 21 is controlled so that fuel is jetted-out at a prescribed time in the course ranging from the latter half of intake cycle to compression cycle, and the air injection valve 22 is controlled so that air is jetted-out in the latter half of the fuel injection period.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、燃料をエンジンの点火プラグに向けて送る層
状給気エンジンに関するものである。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a stratified air charge engine that directs fuel towards a spark plug of the engine.

−1− 一〇。-1- Ten.

(従来技術) 従来σ) 般的(7火花JjJ大H5−エンジン(ガソ
リンエンジン)では、スロワ1−ルバルブによって吸入
空気f1を調節し、か゛)、吸入空気ωに応じた吊の燃
料を供給して空気と均一に沢合さt!、燃焼室内で点火
プラグにJ:り着火ざぜるようにしている。
(Prior art) Conventional σ) In a general (7-spark JjJ large H5-engine (gasoline engine)), the intake air f1 is adjusted by a throat valve, and the amount of fuel corresponding to the intake air ω is supplied. The air is evenly distributed! The spark plug is ignited in the combustion chamber.

このJ:うなエンジンにおいて出力および燃費を向上す
る1段としては、例えば実開昭54−56006号公報
にみられるにうに、圧縮行程で燃焼室内に圧縮空気を供
給して旋回流を助長させ、燃焼速度を高めるようにした
ものなどが知られている。
As a first stage for improving output and fuel efficiency in this J: Eel engine, as shown in Utility Model Application Publication No. 54-56006, for example, compressed air is supplied into the combustion chamber during the compression stroke to promote swirling flow. Some are known that increase the combustion rate.

ところで、少なくともエンジン低f”[時には、点火プ
ラグ付近に着火可能な空燃比の混合気が存在すれば、燃
焼室内の他の部分cbいて燃料が希薄であっても充分に
燃焼は可能であり、エンジンを作動させることができる
。このような点に着目し、大幅な燃費の向上を図る手段
として、特開昭49−62807号公報に示されるJ:
うに、点火時期に対応した所定時期に燃料を点火プラグ
に向けて噴射させるようにした、いわゆる肋状給気エン
ジー 2 = ;− ンが知られている。このエンジンによると、点火プラグ
付近に所要の空燃比を与える燃料が供給される限E)、
希薄燃焼が可能どなるとと1)に、空気が過剰に供給さ
れても差Iノ支えないので低負荷時にス[1ツ1−ルバ
ルブの聞磨を大きクシ、また(、1スロツ[−ルバルブ
を省略することができ、これにより低角荷時のボンピン
グロスを低減Jることができる。その結果、大幅な燃費
の向」二が可能となる。
By the way, if there is an air-fuel mixture with an ignitable air-fuel ratio near the spark plug, sufficient combustion is possible even if the fuel is lean in other parts of the combustion chamber. The engine can be operated. Focusing on this point, as a means to significantly improve fuel efficiency, J:
A so-called rib air supply engine is known that injects fuel toward a spark plug at a predetermined timing corresponding to the ignition timing. According to this engine, there is a limit E) in which fuel is supplied near the spark plug to provide the required air-fuel ratio.
1) If lean combustion is possible, even if excessive air is supplied, there will be no difference, so at low loads, it is recommended to use a large comb to polish the 1-throttle valve. This makes it possible to reduce the pumping loss during low angle loads.As a result, it is possible to significantly improve fuel efficiency.

このように点火プラグに向Cづて燃111が噴射される
層状給気エンジンでは、低負荷時に、着火性の向、1−
のため、効率良く上記燃料の霧化、気化を促進づること
が要求されている。とくにこの場合、噴射期間のうちの
遅い時期に噴射される燃1’lはど点火時期までに霧化
が行われにくく、一方、早い時期に噴射される燃料は点
火時期までに拡散し易いという点も考慮して、不必要に
燃料が拡散しない状態で上記要求を満足させることが望
ましい。
In a stratified air charge engine in which fuel 111 is injected toward the spark plug in this way, at low load, the direction of ignition is 1-
Therefore, it is required to efficiently promote atomization and vaporization of the fuel. In particular, in this case, fuel injected late in the injection period is difficult to atomize by the ignition timing, while fuel injected early is likely to diffuse by the ignition timing. Taking this into consideration, it is desirable to satisfy the above requirements without unnecessary fuel diffusion.

(発明の目的) 本発明はこのにうな事情に鑑み、少イTくとも低負荷時
に所定のタイミングで燃料を点火プラグに−3− 向け[噴mするJ、うに1)た層状給気エンジンにおい
−C1」−記燃料を積極的に霧化、気化し、しかも、噴
射期間前゛1′に口fj川さJする燃r1が不必要に拡
散してリーン化するという事態も避(J1着火竹を向上
することを目的と16bのである。
(Object of the Invention) In view of these circumstances, the present invention provides a stratified air supply engine that directs fuel to the spark plug at a predetermined timing at least when the load is low. By actively atomizing and vaporizing the fuel described in "Odor - C1", it is also possible to avoid the situation where the fuel R1, which flows into the mouth before the injection period, is unnecessarily diffused and becomes lean (J1 16b with the purpose of improving the ignition of bamboo.

(発明の構成) 本発明の層状給気Yンジンは、エンジンの点火プラグに
向t−1で配置された燃料噴射弁ど、該燃1111’l
射弁からの噴口・1燃r1と干渉する方向に空気を噴射
づる空気噴射弁と、エンジンの負荷状態を検出Jる負荷
検出手段と、−Lンジンのクランク角を検出するクラン
ク角検出手段と、燃″P1制御手段と、空気制御手段と
を備えている。−[記燃料制御手段は、上記口前検出手
段とクランク角検出−1段どの出力を受【プ、エンジン
但負荷時、吸気行程後半から圧縮行稈の所定の時期に燃
料を噴I)lツるように上記燃F1噴射弁を制御し、ま
た、空気制御手段は、燃料噴射期間の後半に空気を噴射
するように空気噴射弁を制御1゛る構成と1ノでいる。
(Structure of the Invention) The stratified air supply Y engine of the present invention includes a fuel injection valve disposed in the direction t-1 to the spark plug of the engine, and the fuel 1111'l
An air injection valve that injects air in a direction that interferes with the nozzle port 1 fuel r1 from the injection valve, load detection means that detects the load state of the engine, and crank angle detection means that detects the crank angle of the -L engine. , a fuel P1 control means, and an air control means. The fuel F1 injector is controlled so that fuel is injected at a predetermined time in the compression culm from the latter half of the stroke, and the air control means controls the air so that the air is injected in the latter half of the fuel injection period. The configuration is one in which the injection valve is controlled.

上記燃料噴射弁および空気噴射弁は、上記要件を満足す
る限り、−4= 燃焼室に設けておいてもよい()、燃焼室’ytt傍の
吸気ボートにnQ tづておいてもよい。
As long as the above requirements are satisfied, the fuel injection valve and air injection valve may be provided in the combustion chamber () or may be provided in an intake boat near the combustion chamber.

(実施例) 第1図は本発明を4気筒4ザイクルエンジンに適用した
場合の一実施例を概略的に示1ノ、第2図はこのJ−ン
ジンの燃焼室部分とその近傍部の具体的構造を示す。こ
れらの図において、1番よエンジン本体、21よ吸気管
3および吸気マニホールド4からなる吸気通路、5は吸
気通路2の1−流部に設置ノられたエアクリーナ、6は
排気マニホールドである。図に示す実施例では、エンジ
ン本体1の各気筒の燃焼室7に対してそれぞれ一次吸気
通路8と二次吸気通路9どが吸気マニホールド4に設け
られ、上記二次吸気通路9には、この通路9の開度を調
節するスワール調節弁10が設けられている。このスワ
ール調節弁10の作動は、後述する制御ユニツ1〜/I
−0により、アクチュエータ11を介して制御されるよ
うにしている。
(Embodiment) Fig. 1 schematically shows an embodiment in which the present invention is applied to a 4-cylinder 4-cycle engine. It shows the structure of In these figures, 1 is the engine body, 21 is an intake passage consisting of an intake pipe 3 and an intake manifold 4, 5 is an air cleaner installed in the 1st flow part of the intake passage 2, and 6 is an exhaust manifold. In the embodiment shown in the figure, a primary intake passage 8 and a secondary intake passage 9 are provided in the intake manifold 4 for each combustion chamber 7 of each cylinder of the engine body 1, and the secondary intake passage 9 is provided with a primary intake passage 8 and a secondary intake passage 9, respectively. A swirl control valve 10 is provided to adjust the opening degree of the passage 9. The operation of this swirl control valve 10 is controlled by control units 1 to /I, which will be described later.
-0, it is controlled via the actuator 11.

各気筒の燃焼室7には、−次吸気通路8に連通づる一次
吸気ボート13と、二次吸気通路9に連−5− 通りる二次吸気ボーI・14ど、排気ポー1−15とが
間口し、これらのボー+−13,14,15の開口部に
、図外の動弁機構によってぞれぞれ所定のタイミングで
開閉作動される一次側吸気弁1G、二次側吸気弁17お
J−び排気弁18が装備されている。また、燃焼室7内
には、点火プラグ20が設けられるとともに、燃I′!
I@躬弁21および空気噴射弁22が配置されている。
The combustion chamber 7 of each cylinder includes a primary intake port 13 communicating with the secondary intake passage 8, a secondary intake port I/14 communicating with the secondary intake passage 9, and an exhaust port 1-15. The openings of these bows +-13, 14, and 15 are provided with a primary intake valve 1G and a secondary intake valve 17, which are respectively opened and closed at predetermined timings by a valve mechanism (not shown). It is equipped with an exhaust valve 18. Further, a spark plug 20 is provided in the combustion chamber 7, and a spark plug 20 is provided inside the combustion chamber 7.
An I@man valve 21 and an air injection valve 22 are arranged.

上記燃料噴射弁21は点火プラグ20に向(プて設【)
られている。また、空気噴射弁22は、燃料噴射弁21
に近接して配置され、かつ、燃r1噴射弁21からの噴
射燃料と干渉する方向に空気を噴射させるような配置に
設けられている。なお、第1図では作図の便宜上、右端
の気筒に対してのみ燃料噴射弁21および空気噴射弁2
2の配置を明らかにしたが、他の気筒にも同様にそれぞ
れ燃料噴射弁21および空気噴射弁22が配置されてい
る。
The fuel injector 21 is directed toward the spark plug 20.
It is being Further, the air injection valve 22 is connected to the fuel injection valve 21.
The fuel injector 21 is disposed close to the fuel injector 21, and is arranged so as to inject air in a direction that interferes with the fuel injected from the fuel r1 injection valve 21. In addition, in FIG. 1, for convenience of drawing, only the fuel injection valve 21 and the air injection valve 2 are shown for the rightmost cylinder.
Although the arrangement of No. 2 has been made clear, fuel injection valves 21 and air injection valves 22 are similarly arranged in the other cylinders, respectively.

上記燃料噴射弁21は燃料噴射ポンプ23に接続されて
いる。この燃II+噴射ポンプ23はタイミングベルト
24およびプーリ25,26を介【ノて− 6 − エンジンのクランク軸27ににり駆動され、各気筒の燃
君噴111)1弁21にそれぞれ燃料を供給して噴射さ
1!るJ:うにし、かつ、その噴射開始n、′I!!1
11および噴射終了時期を電気的な制御信号に応じて調
節することができる構造どなっている。また、空気噴射
弁22は空気リザーバ2つを介して空気ポンプ30に接
続され、この空気ポンプ30は、ベルト31およびプー
リ32,33を介して」口開クランクnil+ 27に
より駆動されるJ:うにしている。図では、エンジン始
動時に空気リザーバ2つ内の圧力上背を促進するため、
空気リザーバ29と空気ポンプ30との間に空気リター
ン通路34をm (jlこの空気リターン通路3/1に
、エンジン始動時に開閉作動されるリサイクルバルブ3
5が設けられている。36は空気ポンプ30への空気う
9人用通路37に設けられたチェックバルブ、38は空
気リリーフ用通路39に段(Jられたリリーフ弁である
The fuel injection valve 21 is connected to a fuel injection pump 23. This fuel injection pump 23 is driven by the crankshaft 27 of the engine via a timing belt 24 and pulleys 25, 26, and supplies fuel to the fuel injection 111) 1 valve 21 of each cylinder. Then jet 1! RuJ: Sea urchin and its injection start n,'I! ! 1
11 and the injection end timing can be adjusted according to an electrical control signal. The air injection valve 22 is also connected to an air pump 30 via two air reservoirs, and the air pump 30 is driven by an open crank 27 via a belt 31 and pulleys 32, 33. I have to. In the figure, to promote pressure build-up in the two air reservoirs when starting the engine,
An air return passage 34 is provided between the air reservoir 29 and the air pump 30 (jl) In this air return passage 3/1, there is a recycle valve 3 that is opened and closed when the engine is started.
5 is provided. 36 is a check valve provided in the air passage 37 for air to the air pump 30, and 38 is a relief valve installed in the air relief passage 39.

また、40は各種制御のための制御コニットであり、例
えば第3図に示Jようにマイクロコンビ−7− ュータを用い1.:制御部41および各種変換器/12
〜46を含んでいる。上記制御部41にIj1アクUル
間匪セン与51からΔ/l)変換器42を介してアクセ
ル開度信号が入力されるとともに、クランク角セン)J
52からF/V (固彼数−電圧)変換器43およびΔ
/D変換器44を介してエンジン回転数伏目が入力され
、このアクセル開度とエンジン回転数とで負荷状態が検
出されるようにし、また、′lランク角レしリ52から
クランク角信号が入力されている。ざI)に、実施例で
はスモーク発生時にイれに応じた空気噴射時期の制御を
行うように、スモークセンサ53からの検出信号も△/
D変換器45を介して制御部/11に入力されている。
Further, 40 is a control unit for various controls, for example, as shown in FIG. :Control unit 41 and various converters/12
Contains ~46. An accelerator opening signal is inputted to the control section 41 from the Ij1 axle angle sensor 51 via the Δ/l) converter 42, and the crank angle sensor) J
52 to F/V (Fixed Frequency-Voltage) converter 43 and Δ
The engine rotational speed foreshadowing is inputted via the /D converter 44, and the load condition is detected based on this accelerator opening degree and the engine rotational speed. It has been entered. (I) In the embodiment, the detection signal from the smoke sensor 53 is also adjusted to
The signal is input to the control unit/11 via the D converter 45.

また、後述する始動時の制御のため、前記空気リリ゛−
バ29内の圧力を検出覆る圧力センリ54からA/[1
変換器46を介して与えられる圧力信号ど、スタードレ
ン4J−55から与えられる一インタラブ[へ〈割り込
み信号)としてのスター1〜信号も上記制御部41に入
力されている1、上記制御部41は、燃わ1噴射弁21
からの燃料噴射を制御−8− する燃r1制御手段どしての機能と、空気噴射弁22か
らの空気噴射を制御11づる空気制御手段としての機能
とを有し、心接には燃料噴射ポンプ23の作りjおよび
空気噴射弁22の開閉作動を制御している。また、11
11記スワ一ル調節弁10のアクチコ工−タ11おJ:
び前記リサイクルバルブ35も」−記制御部/11によ
って制御している。
In addition, for control at the time of starting which will be described later, the air release is
The pressure sensor 54 detects the pressure inside the bar 29.
The pressure signal given through the converter 46 and the star 1 signal given from the star drain 4J-55 as an interrupt signal are also input to the control section 41. burns 1 injector 21
It has a function as a fuel r1 control means to control fuel injection from the air injection valve 22, and an air control means to control air injection from the air injection valve 22, and has a function as an air control means to control air injection from the air injection valve 22. It controls the construction of the pump 23 and the opening/closing operation of the air injection valve 22. Also, 11
Actuator 11 of 11 Swirl control valve 10:
The recycle valve 35 is also controlled by the control section 11.

」ニ記制御部41内には、予め種々の運転状態にd3 
G−Jる燃料と空気の各噴射開始時期および各噴射終了
時期がデータマツプとして記憶され、このマツプにより
、少なくとも低負荷時には吸気行程後半ないし圧縮行程
で燃料を噴射するとともに、燃r1噴射明間の後半に空
気を噴OA′!l’るように設定されている。例えば第
4図に示すJ:うな特性で上記時期が制御されるにうに
上記マツプが作成されている。ずなわら、第4図におい
て、l”sおよびFeはイれぞれ燃lp1の噴射開始時
期および噴射終了時期、AsおにびAeはそれぞれ空気
の噴射開始時期おJ:び噴射終了時期を示し、■は点火
時期を示す。この図のにうに、低負荷領域では圧縮行程
−9− 後半で燃¥N1が噴r1・1され、子の噴04終了時明
FO。
” (d) In the control unit 41, d3 is set to various operating states in advance.
The injection start timing and injection end timing of G-J fuel and air are stored as a data map, and this map allows fuel to be injected in the latter half of the intake stroke or compression stroke at least when the load is low, and to inject fuel between the first and second injections. OA' blowing air in the second half! It is set so that For example, the above map is created so that the above timing is controlled by the J: Una characteristic shown in FIG. In Fig. 4, l"s and Fe respectively represent the injection start time and injection end time of fuel lp1, and As and Ae represent the injection start time and J: and injection end time of air, respectively. As shown in this figure, in the low load region, fuel N1 is injected in the second half of the compression stroke -9-, and the fuel is injected FO at the end of the secondary injection 04.

Aeが点火時期■にほぼ一致するにうにしている。Ae is made to almost match the ignition timing (■).

そして、噴射Mは噴射期間に依存づるので、負荷に応じ
lζ適当な燃お1噴射量が得られるように、燃料終了時
期「e8基i1[にして燃料噴射開始時期「Sが設定さ
れている。また、少なくともこの低角荷時において、空
気の噴射開始時期△Sは燃料の噴射開始時期「Sよりも
遅ら1±、両者の噴射終了時期「e、八〇は一致さく!
ている。高負荷時の制御については本発明で限定しない
が、燃料噴@量が増加される高負荷前には、層状給気の
必要がなく、むしろ空気利用率を高めて出力を向上させ
るには燃r1を分散させた状態で着火する方が望ましい
。このため、図示の特性では負荷がある程度高くなるど
燃料おJ:び空気の噴射時l!l′lを早め、高負荷領
域で【j、吸気行程の前半に燃料が噴射されるようにし
ている。なお、この図において二点鎖線AS′は、スモ
ーク発生時の空気の噴射開始時期を示し、このにうにス
モーク発生時には空気の噴射開始時期が早められるよう
にし、この特性を与え−10− るだめの補正係数も予めマツプに記憶さ!N−(いる。
Since the injection M depends on the injection period, the fuel end time "e8 and i1" and the fuel injection start time "S" are set so that an appropriate fuel injection amount can be obtained depending on the load. Also, at least at this low angle load, the air injection start time △S is 1± later than the fuel injection start time "S", and both injection end times "e" and "80" match!
ing. Control during high loads is not limited by the present invention, but stratified air supply is not necessary before high loads when the amount of fuel injection is increased, and rather, it is necessary to increase the air utilization rate and improve the output. It is preferable to ignite with r1 dispersed. For this reason, with the characteristics shown in the figure, even when the load is high to some extent, when fuel and air are injected, l! l'l is advanced so that fuel is injected in the first half of the intake stroke in the high load region. In this figure, the dashed-double line AS' indicates the timing of the start of air injection when smoke is generated. The correction coefficients are also stored in the map in advance! N-(There is.

さらに上記制御部41内には、予め種々の負荷状態にお
【)るスワール調節弁10の開度がデークマップとして
記憶され、低負荷時に前記スワール調節か10を閉じ、
負荷が高くイTるど−てれに応じた開度にスワール調節
弁10を聞くように、上記マツプが作成されている。
Further, in the control section 41, the opening degree of the swirl control valve 10 under various load conditions is stored in advance as a disk map, and the swirl control valve 10 is closed when the load is low.
The above map is created so that the swirl control valve 10 is adjusted to an opening degree corresponding to a high load and an electric current.

上記制御ユニツ1へ40によって実行される制御をフロ
ーヂャ−1へで示すと第5図おにび第6図のようになる
The control executed by the control unit 1 by the flowchart 1 is shown in FIG. 5 and FIG. 6.

第5図に示すメインルーチンにおいては、先ず負荷状態
を決定するアクセル間IAとTンジン回転数Rの各検出
信号が入力され(ステップX1)、この信号に基づき、
予め前記の第4図に示す特性を与えるJ:うに設定され
たマツプから、イの時の負荷状態に応じた燃料と空気の
各噴射開始時期As、Fsおよび各噴射終了り期△e、
 Feが演算される(ステップ、X2 、 X3 )。
In the main routine shown in FIG. 5, first, detection signals of accelerator distance IA and T engine rotation speed R, which determine the load condition, are input (step X1), and based on these signals,
From the map set in J: which gives the characteristics shown in FIG. 4 in advance, each injection start timing As, Fs and each injection end time Δe,
Fe is calculated (steps X2, X3).

さらに、スモーク信号Sに応じた補正係数Saがマツプ
からめられ、先にめられた空気の噴!)j開始時期As
に−11− 上記補正係数Saが乗算される(ステップX4゜X5 
)。この場合、第7図に示すようにスモークが少ないh
に補正体lI4!S aを1と1ノ、スモークが増加す
ると補正係数Saが減少するように設定しておく。次に
、クランク角Oの検出信号を繰返1ノ入力しつつイアラ
ンク角θが上記哨用開始時期As。
Furthermore, a correction coefficient Sa corresponding to the smoke signal S is set from the map, and the preset air jet! )j start time As
-11- is multiplied by the above correction coefficient Sa (steps X4°X5
). In this case, as shown in Figure 7, there is less smoke.
Correction body lI4! Sa is set to 1 and 1 so that as the smoke increases, the correction coefficient Sa decreases. Next, while repeatedly inputting the detection signal of the crank angle O, the ear rank angle θ is determined at the above-mentioned patrol start time As.

Fsに達!するのを持ってから、燃r1および空気の噴
射を開始する制御が行われる(ステップ×6〜Xa )
。引続いて、クランク角θの検出信号を繰返し入力しつ
つクランク角θが上記噴射終了時期Ae、Feに達する
のを持ってから、燃料および空気の噴q4を終了づる制
御が行われる(ステップ×9〜×11)。さらに、上記
アクセル開度Aとエンジン回転数Rとに応じて、前記ス
ワール調節弁10の開度(S弁開度)Soが演算され、
この開度Soを与える制御信号が前記アクチュエータ1
1に出力される(スフツブX+o、X1+)。その後ス
テップ×1に戻り、以上のフローが繰返されるようにし
ている。
Reached Fs! After that, control is performed to start the injection of fuel r1 and air (steps x6 to Xa).
. Subsequently, the detection signal of the crank angle θ is repeatedly input, and after the crank angle θ reaches the injection end timings Ae and Fe, control is performed to end the fuel and air injection q4 (step 9-×11). Furthermore, the opening degree (S valve opening degree) So of the swirl control valve 10 is calculated according to the accelerator opening degree A and the engine rotation speed R,
The control signal that provides this opening degree So is the actuator 1
1 (Sfutub X+o, X1+). Thereafter, the process returns to step x1 and the above flow is repeated.

このような制御により、低負荷時には、圧縮行−12− 程後半の所定時期に燃r1噴射弁21から点火プラグ2
0に向けて燃料が噴射され、主に点火プラグ付近に燃料
が供給されて燃焼室7の他の部分では燃料が希薄な状態
で点火が行われる。従って、少ない燃v1でも着火、燃
焼が可能どなってエンジンを作動させることができると
ともに、−次吸気通路8から燃焼室7に空気が過剰に供
給されても差し支えないので、ポンピングロスが低減さ
れる。
Through such control, when the load is low, the spark plug 2 is discharged from the fuel r1 injector 21 at a predetermined time in the latter half of the compression stroke.
Fuel is injected towards zero, the fuel is mainly supplied near the spark plug, and ignition is performed in other parts of the combustion chamber 7 with fuel being lean. Therefore, it is possible to ignite and burn the engine even with a small amount of fuel v1, and the engine can be operated.Also, since there is no problem even if excessive air is supplied from the secondary intake passage 8 to the combustion chamber 7, pumping loss is reduced. Ru.

そして、この場合に第4図に承りような特性で空気が噴
射されることにJ:す、噴射燃料が拡散しすぎない程度
で適切に霧化、気化が行われる。つまり、点火時点にお
いては、燃料噴射期間の甲い時期に噴射された燃r1は
と拡散し、近い時期に噴射された燃料はど本来的に霧化
、気化が行われにくい。従って、燃料が拡散しすぎて点
火プラグ20付近がリーン化するということのないよう
に、燃料噴rJJ期間め前半は空気の噴射を停+L L
、燃料噴射期間後半は噴射空気により燃料の霧化、気化
を2進するようにしている。ただし、スモークが発生す
るときは点火プラグ20付近が過濃であるた−13− 00 め、空気噴01時期を早めて燃料の拡散度を調整lノで
いる。
In this case, the air is injected with the characteristics shown in FIG. 4, and the injected fuel is appropriately atomized and vaporized to the extent that it does not spread too much. In other words, at the time of ignition, the fuel r1 injected at the first period of the fuel injection period is diffused, and the fuel injected at the near timing is inherently difficult to atomize or vaporize. Therefore, to prevent the fuel from spreading too much and causing the area near the spark plug 20 to become lean, air injection is stopped during the first half of the fuel injection period.
In the second half of the fuel injection period, the injection air is used to perform binary atomization and vaporization of the fuel. However, when smoke occurs, the area near the spark plug 20 is too rich, so the air injection timing is advanced to adjust the degree of fuel diffusion.

一方、高負荷時には、燃r1噴射量が増量されるととも
に、吸気行程の前半に燃料が噴射され、また、スワール
調節弁10が開かれて二次吸気通路9からの吸気により
燃焼室7内のスワールが高められるため、燃料が燃焼室
7内に充分拡散されてから点火が行われることとなる。
On the other hand, when the load is high, the fuel r1 injection amount is increased, fuel is injected in the first half of the intake stroke, and the swirl control valve 10 is opened to cause the intake air from the secondary intake passage 9 to flow into the combustion chamber 7. Since the swirl is increased, ignition is performed after the fuel is sufficiently diffused within the combustion chamber 7.

また、第6図に示す割込みルーチンは、始動時の制御を
行うもので、前記スタートセンサ54がらの信号によっ
て開始され、まず前記圧力センサ53からの圧力信号が
入力され(ステップY1)、その圧力Pが設定値α以上
か否かが判別される〈ステップY2 )。上記圧力Pが
設定値α未満であれば、前記リサイクルバルブ35が開
閉作動を繰返すように制御され(ステップY3)、これ
によって前記空気リザーバ29内の圧力上昇が促進され
る。上記圧力Pが設定値α以上になると、前記リサイク
ルパル135が閉じられるとともに、始動用の燃料およ
び空気が噴射される(ステップ−14− Y4 )。イして、始動が終了したか否かが判別され(
ステップY5)、始動が終了すると前記の第5図に示1
Jメインルーチンに戻されるように【ノている。
The interrupt routine shown in FIG. 6 is for controlling the start, and is started by a signal from the start sensor 54. First, a pressure signal from the pressure sensor 53 is input (step Y1), and the pressure It is determined whether P is greater than or equal to the set value α (step Y2). If the pressure P is less than the set value α, the recycle valve 35 is controlled to repeatedly open and close (step Y3), thereby promoting a rise in the pressure in the air reservoir 29. When the pressure P exceeds the set value α, the recycle pulse 135 is closed and starting fuel and air are injected (step-14-Y4). It is determined whether the startup has been completed or not (
Step Y5), when the starting is completed, the 1 shown in FIG.
J It seems like you are being returned to the main routine.

第8図および第9図は本発明の別の実施例を示す。この
実施例では燃料噴射弁21′および空気噴射弁22が一
次吸気ボー1−13に設置′Jられ、この場合も、燃わ
1噴射弁21′は燃焼室7内の点火プラグ20に向けて
配置され、空気噴射弁22は噴射燃料と干渉する方向に
空気を噴射させるように配置されている。また、この実
施例において燃料噴射弁21′は、空気噴射弁22と同
様に制御ユニット/IOににって直接に開閉作動が制御
されるようにしてあり、この場合に燃料噴射弁21′は
、通常のガソリンエンジンに用いられでいるような燃料
噴射ポンプ(図示省略)に接続してお(1ばJ:い。
8 and 9 show another embodiment of the invention. In this embodiment, the fuel injection valve 21' and the air injection valve 22 are installed in the primary intake bow 1-13. The air injection valve 22 is arranged so as to inject air in a direction that interferes with the injected fuel. Further, in this embodiment, the opening and closing operation of the fuel injection valve 21' is directly controlled by the control unit/IO similarly to the air injection valve 22, and in this case, the fuel injection valve 21' is , is connected to a fuel injection pump (not shown) that is used in ordinary gasoline engines.

このように上記各噴射弁21’ 、22を吸気ボート1
3に設G」る場合、吸気弁16が閉じるまでに燃料を噴
OAさせる必要があるので、第10図に−15− 示づように、低負荷領域では吸気行程の終期に燃料おJ
:び空気が噴θJされるようにそれぞれの噴射開始時期
A S 、 F S il’3よび噴口1終了時III
 F e 、Δeが設定、されるが、イの他の構成は第
1の実施例と同様である。
In this way, each of the injection valves 21' and 22 is connected to the intake boat 1.
3, it is necessary to inject fuel before the intake valve 16 closes, so as shown in Fig. 10, the fuel is injected at the end of the intake stroke in the low load region.
: and the injection start timing A S , F S il'3 and the end of the nozzle 1 III so that the air is injected θJ.
F e and Δe are set, but the other configuration of A is the same as in the first embodiment.

(発明の効果) 1ヌ十のように本発明は、エンジン低角荷時に、吸気行
程後半から圧縮行程の所定の時期に燃料を点大プラグに
向けて噴射するととbに、燃r1噴射期間の後半に空気
を噴口4して噴射燃料に混入させるようにしているため
、いわゆる層状給気により燃費が向上されるとともに、
燃料の霧化、気化が促進され、かつ、不必要に燃料が拡
散しすぎることも防止されて着火性おJ:び燃焼性が格
段に向上されるものである。
(Effects of the Invention) As shown in item 1 and 10, the present invention provides that when the engine is under low angle load, fuel is injected toward the large point plug from the latter half of the intake stroke to a predetermined period of the compression stroke. Since the air is mixed into the injected fuel through the nozzle 4 in the latter half of the fuel injection, the so-called stratified air supply improves fuel efficiency.
Atomization and vaporization of the fuel are promoted, and unnecessary excessive diffusion of the fuel is also prevented, thereby significantly improving ignitability and combustibility.

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

第1図は本発明の一実施例を示す全体概略図、第2図は
その燃焼室部分およびその近傍部の拡大図、第3図は制
御系統のブロック図、第4図は燃料および空気の噴q」
時期の特性図、第5図および−16− 第6図は70−チト一ト、第7図はスモークに応じた空
気噴射開始時期補正係数の特性図、第8図は別の実施例
を示づ全体概略図、第9図はその第2図相当図、第10
図はこの実施例による場合の第4図相当図である。 20・・・点火プラグ、21.21’・・・燃料噴射弁
、22・・・空気l1lll射弁、40・・・制御]ニ
ラ1〜(制御手段)、51・・・アクセル開度センサ、
52・・・クランク角しンリー1゜ 特許出願人 東洋工業株式会社 −17− 第2図 第う図 第7図 第0図 第9図 第10図 賭
Fig. 1 is an overall schematic diagram showing an embodiment of the present invention, Fig. 2 is an enlarged view of the combustion chamber and its vicinity, Fig. 3 is a block diagram of the control system, and Fig. 4 is a diagram of the fuel and air flow. "Spout"
Characteristic diagrams of timing, Figures 5 and -16- Figure 6 shows 70 seconds, Figure 7 shows characteristics of air injection start timing correction coefficient according to smoke, and Figure 8 shows another example. Figure 9 is a diagram equivalent to Figure 2, Figure 10 is a schematic diagram of the whole.
The figure is a diagram corresponding to FIG. 4 in the case of this embodiment. 20... Spark plug, 21. 21'... Fuel injection valve, 22... Air l1llll injection valve, 40... Control] chive 1~ (control means), 51... Accelerator opening sensor,
52...Crank angle 1゜Patent applicant Toyo Kogyo Co., Ltd. -17- Figure 2 Figure 7 Figure 0 Figure 9 Figure 10

Claims (1)

【特許請求の範囲】[Claims] 1、エンジンの点火プラグに向けて配置された燃料噴射
弁と、該燃料噴射弁からの噴射燃料と干渉する方向に空
気を噴射する空気噴射弁と、エンジンの負荷状態を検出
する負荷検出手段と、エンジンのクランク角を検出する
クランク角検出手段と、上記負荷検出手段とクランク角
検出手段との出力を受け、エンジン低負荷時、吸気行程
後半から圧縮行程の所定の時期に燃料を噴射するように
上記燃料噴射弁を制御する燃料制御手段と、燃料噴射期
間の後半に空気を噴射するように空気噴射弁を制御する
空気制御手段とを設けたことを特徴とする層状給気エン
ジン。
1. A fuel injection valve disposed toward the spark plug of the engine, an air injection valve that injects air in a direction that interferes with the injected fuel from the fuel injection valve, and a load detection means that detects the load state of the engine. , a crank angle detecting means for detecting the crank angle of the engine, and receiving outputs from the load detecting means and the crank angle detecting means to inject fuel at a predetermined timing from the latter half of the intake stroke to the compression stroke when the engine is under low load. A stratified air supply engine comprising: a fuel control means for controlling the fuel injection valve; and an air control means for controlling the air injection valve so as to inject air in the latter half of a fuel injection period.
JP58144265A 1983-08-05 1983-08-05 Laminar charging engine Granted JPS6035115A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58144265A JPS6035115A (en) 1983-08-05 1983-08-05 Laminar charging engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58144265A JPS6035115A (en) 1983-08-05 1983-08-05 Laminar charging engine

Publications (2)

Publication Number Publication Date
JPS6035115A true JPS6035115A (en) 1985-02-22
JPH0478813B2 JPH0478813B2 (en) 1992-12-14

Family

ID=15358067

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58144265A Granted JPS6035115A (en) 1983-08-05 1983-08-05 Laminar charging engine

Country Status (1)

Country Link
JP (1) JPS6035115A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02136560A (en) * 1988-11-16 1990-05-25 Hitachi Ltd Fuel injection controller
JPH0742564A (en) * 1993-08-03 1995-02-10 Minoru Nakagawa Air feed forced combustion type engine
WO2017130526A1 (en) * 2016-01-29 2017-08-03 日立オートモティブシステムズ株式会社 Fuel injection valve control device

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111058938A (en) * 2019-12-27 2020-04-24 中国第一汽车股份有限公司 In-cylinder tumble flow disturbance system and automobile

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02136560A (en) * 1988-11-16 1990-05-25 Hitachi Ltd Fuel injection controller
JPH0742564A (en) * 1993-08-03 1995-02-10 Minoru Nakagawa Air feed forced combustion type engine
WO2017130526A1 (en) * 2016-01-29 2017-08-03 日立オートモティブシステムズ株式会社 Fuel injection valve control device

Also Published As

Publication number Publication date
JPH0478813B2 (en) 1992-12-14

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