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JPS6035143A - Engine - Google Patents

Engine

Info

Publication number
JPS6035143A
JPS6035143A JP58144267A JP14426783A JPS6035143A JP S6035143 A JPS6035143 A JP S6035143A JP 58144267 A JP58144267 A JP 58144267A JP 14426783 A JP14426783 A JP 14426783A JP S6035143 A JPS6035143 A JP S6035143A
Authority
JP
Japan
Prior art keywords
air
engine
valve
injection valve
fuel
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
JP58144267A
Other languages
Japanese (ja)
Inventor
Haruo Okimoto
沖本 晴男
Takashige Tokushima
徳島 孝成
Shinichi Tamura
伸一 田村
Masakimi Kono
河野 誠公
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 JP58144267A priority Critical patent/JPS6035143A/en
Publication of JPS6035143A publication Critical patent/JPS6035143A/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
    • F02D41/02Circuit arrangements for generating control signals
    • F02D41/04Introducing corrections for particular operating conditions
    • F02D41/06Introducing corrections for particular operating conditions for engine starting or warming up
    • F02D41/062Introducing corrections for particular operating conditions for engine starting or warming up for starting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D35/00Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
    • F02D35/0015Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for using exhaust gas sensors
    • F02D35/0023Controlling air supply
    • F02D35/0038Controlling air supply by means of air pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

PURPOSE:To enhance the starting characteristic of an engine having an air injection valve in its combustion chamber by stopping supply of compressed air from an air pump to said air injection valve while the engine is under starting procedure, and thereby preventing excessive supply of the air at the time of starting. CONSTITUTION:In an engine, in which a primary, a secondary suction port 13, 14 and an exhaust port 15 opening at the combustion chamber 7 of each cylinder are opened and closed by a primary, a secondary suction valve and an exhaust valve, respectively, and in which an ignition plug 20, fuel injection valve 21 and air injection valve 22 are arranged in each combustion chamber 7, a control unit 40 is provided, wherein the outputs of an accelerator opening sensor 51, crank angle sensor 52 and start sensor 53 are entered. When it is judged that the starting is completed, an electro-magnetic clutch 35 to transmit the power of engine to an air pump 30 is turned off to stop supply of the air to air injection valve 22. The appropriate actuator 12a is also controlled so as to shut a suction throttle valve 12 in the suction passage 2 to a specific degree of opening.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、燃焼室に空気を供給する空気噴射弁とこの空
気噴射弁に加圧空気を供給する空気ポンプとを備えたエ
ンジンに関するものである。
Detailed Description of the Invention (Field of Industrial Application) The present invention relates to an engine equipped with an air injection valve that supplies air to a combustion chamber and an air pump that supplies pressurized air to the air injection valve. be.

(従来技術) 従来から、秤々の目的で、燃焼室に空気を供給するため
の空気噴射弁を設けたエンジンがある。
(Prior Art) Conventionally, there has been an engine provided with an air injection valve for supplying air to a combustion chamber for the purpose of weighing.

例えば実開昭54−56006号公報に示された− 1
 − エンジンでII2、燃焼速仰を高めて出力の増加、祐薄
燃焼を可能にすることを目的として、燃焼室に鳴流口を
聞1]2キせた空気噴射弁を設置ノ、これを空気ポンプ
(コンプレッサ)に接続し、かつ、圧縮行程時に空気噴
射弁を聞くようにしている。
For example, the method shown in Japanese Utility Model Application Publication No. 54-56006-1
- In the engine, an air injection valve with a narrow air flow opening was installed in the combustion chamber in order to increase the combustion speed, increase output, and enable smooth combustion. It is connected to an air pump (compressor) and listens to the air injection valve during the compression stroke.

ところで、エンジン始動時には、吸気量、空燃比等の要
求値が通常の運転状態と界なるが、従来、空気噴射弁を
設警づだ場合の蛤i1+時の制御については着目されて
いなかった。
By the way, when the engine is started, the required values for the intake air amount, air-fuel ratio, etc. are different from the normal operating state, but conventionally, no attention has been paid to the control at the time of clam i1+ when the air injection valve is activated.

(発明の目的) 本発明はこれらの事情に鑑み、使用目的に応じて必要時
に空気噴射弁から燃焼室に空気を供給づることができる
ように()ながら、エンジン始動時に空気が過剰供給さ
れることを避(Jて始動時を向上げることを目的とする
ものである。
(Purpose of the Invention) In view of these circumstances, the present invention is designed to supply air from an air injection valve to a combustion chamber when necessary depending on the purpose of use, while preventing excessive supply of air when starting an engine. The purpose is to avoid this and improve the startup time.

(発明の構成) ′本発明は、エンジン燃焼室に空気を供給するための空
気噴射弁と、該空気噴q・l弁へ加圧空気を供給する空
気ポンプとを備えた]]ンジンにおいて、エンジンの始
動を検出する始動センサーと、該始動−2− センサの出力を受けて始動時に上記空気ポンプからの加
圧空気の供給を停止する制御手段とを設Gづたものであ
る。上記空気噴射弁は、燃焼室内に配置してもよいし、
燃焼室近傍の吸気ボー1−に配置してもよい。
(Structure of the Invention) The present invention provides an engine equipped with an air injection valve for supplying air to an engine combustion chamber and an air pump for supplying pressurized air to the air injection q/l valve. The engine is equipped with a start sensor that detects the start of the engine, and a control means that receives the output of the start-2 sensor and stops the supply of pressurized air from the air pump at the time of start. The air injection valve may be placed inside the combustion chamber, or
It may be placed in the intake bow 1- near the combustion chamber.

(実施例) 図では本発明を適用づ−るエンジンの例と1ノで、燃料
をエンジンの点火プラグに向けて噴61−jるようにし
たいわゆる層状給気エンジンで、がっ、噴射燃料の霧化
、気化を促進するため空気噴射弁を燃焼室内に設けたエ
ンジンを示す。この層状給気エンジンは、燃費向上のた
め、少なくども低角荷時に、燃料を主に点火プラグ付近
に供給して着火、燃焼させるようにしたものである。
(Example) The figure shows an example of an engine to which the present invention is applied. This shows an engine equipped with an air injection valve inside the combustion chamber to promote atomization and vaporization. In order to improve fuel efficiency, this stratified air charge engine is designed to supply fuel mainly to the vicinity of the spark plug for ignition and combustion, at least during low angle loads.

第1図はこのよう<kエンジンの全体構造の一実施例を
示し、第2図は燃焼室部分とその近傍部の具体的1f4
造を示しCおり、これらの図において、1はエンジン本
体、2は吸気管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の上流部に設GJられたエアク
リーナ、6は排気マニー 3 − ホールドである。吸気マニホールド4には、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V
#18と二次吸気通路9とが設【Jられ、上記二次吸気
通路9には、この通路9の開度を調節1゛るスワール調
節弁10が設()られている。このスワール調節弁10
の作動は、後述する制御ユニッ1へ/IOにより、アク
チユエータ11を介して制御される、J、うにしている
。また、上記吸気管3には、始8時にのみ所定量だけ閉
じられる吸気絞り弁12が設(ツられている。この吸気
絞り弁12b1制御ニアニット40にJ:す、アクチユ
エータ12aを介して制御されるようにしている。なお
、この実施例の層状給気エンジンでは、後述でるJ:う
に低負荷時(始動時を除く)には空気が過剰に供給され
て−b差し支えないので、一般のエンジンに設けられて
いるスロットルバルブ(アクセルペダルに連動づる絞り
弁)は省略されており、」−記吸気絞り弁12はチョー
ク弁に相当づ゛るものである5、 各気筒の燃焼室7には、−次吸気通路8に連通−4= する−次吸気ポート13と、二次吸気通路9に連通ずる
二次吸気ボー1−14と、排気ボート15とが間口し、
これらのボート13.1/1.15の開口部に、図外の
動弁機構によってイ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16、二次側吸気弁17および排気
弁18が装備されている1、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、燃料噴射弁21お
よび空気噴射弁22が配設されている。上記燃料噴射弁
21は、低負荷時に層状給気を行うことができるように
、点火プラグ20に向けて設(プられている。
Fig. 1 shows an example of the overall structure of such a <k engine, and Fig. 2 shows a specific 1f4 of the combustion chamber and its vicinity.
In these figures, 1 is the engine body, 2 is an intake passage consisting of an intake pipe 3 and an intake manifold 4, 5 is an air cleaner installed in the upstream part of the intake passage 2, and 6 is an exhaust manifold. − It is a hold. The intake manifold 4 has a primary intake vent V for each combustion chamber 7 of each cylinder of the engine body 1.
#18 and a secondary intake passage 9 are provided, and the secondary intake passage 9 is provided with a swirl control valve 10 for adjusting the opening degree of the passage 9. This swirl control valve 10
The operation of the control unit 1 is controlled via an actuator 11 by an I/O to a control unit 1, which will be described later. Further, the intake pipe 3 is provided with an intake throttle valve 12 that is closed by a predetermined amount only at 8 o'clock in the morning. In addition, in the stratified air supply engine of this embodiment, there is no problem with excessive air being supplied at low load (excluding startup), as described below. The throttle valve (throttle valve linked to the accelerator pedal) installed in the engine is omitted, and the intake throttle valve 12 is equivalent to a choke valve5. , - the secondary intake port 13 communicating with the secondary intake passage 8, the secondary intake bow 1-14 communicating with the secondary intake passage 9, and the exhaust boat 15,
At the openings of these boats 13.1/1.15, there are a primary intake valve 16, a secondary intake valve 17, and an exhaust valve 18, which are respectively opened and closed at predetermined timing by a valve mechanism (not shown). In addition, a spark plug 20 is provided in the combustion chamber 7, and a fuel injection valve 21 and an air injection valve 22 are also provided. The fuel injection valve 21 is arranged toward the spark plug 20 so that stratified air supply can be performed during low load.

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II+噴射弁21からの噴射燃料と干
渉づる方向に空気を噴射するように所定の向きに設けら
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J:び空気噴射弁22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。
Further, the air injection valve 22 is disposed close to the fuel injection valve 21 and is oriented in a predetermined direction so as to inject air in a direction that interferes with the fuel injected from the fuel injection valve 21. In addition, for convenience of drawing, in FIG. 1, the arrangement of the fuel injection valve 21 and the air injection valve 22 is shown only for the rightmost cylinder, but the arrangement of the fuel injection valve 21 and the air injection valve 22 is shown for the other cylinders as well. An injection valve 22 is arranged.

上記燃料噴射弁21は燃料噴射ポンプ23に接= 5 
− 続されている。この燃料噴射ポンプ23はタイミングベ
ル1−24おJ:びプーリ25.26を介してエンジン
のクランク軸27により駆動され、名気筒の燃料噴射弁
21にそれぞれ燃r1を供給して噴射さIるJ:うに]
ノ、かつ、その噴口・1開始時期おJ、び噴fJJ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
構造となっている。また、空気噴q4弁22は電気的に
開閉可能な構造とし、空気ポンプ30から空気りIF−
バ29を介しで圧縮空気が空気噴射弁22に供給される
ようにしている。
The fuel injection valve 21 is in contact with the fuel injection pump 23 = 5
− Continued. This fuel injection pump 23 is driven by the crankshaft 27 of the engine via timing bells 1-24 and pulleys 25 and 26, and supplies fuel r1 to the fuel injection valves 21 of the famous cylinders for injection. J: Sea urchin]
Moreover, the structure is such that the start timing of the nozzle 1 and the end timing of the nozzle fJJ can be adjusted in accordance with electrical control signals. In addition, the air jet q4 valve 22 has a structure that can be electrically opened and closed, and air is supplied from the air pump 30 to the air IF-
Compressed air is supplied to the air injection valve 22 via a bar 29.

この空気ポンプ30は、ベル1〜31およびプーリ32
.33を介して上記クランク軸27にJ:り駆動される
ようにし、かつ、プーリ32ど空気ポンプ30のポンプ
軸34との間に電磁クラッチ35を介在させることによ
り、該電磁クラップ35が切られたときは空気ポンプ3
0の駆動が停止ざ11゜るようにしている。36は空気
ポンプ30への空気導入用通路37に設GJられたチェ
ックバルブ、38は空気リリーフ用通路39に設置−J
られたリリーフ弁である。
This air pump 30 includes bells 1 to 31 and a pulley 32.
.. 33, and by interposing an electromagnetic clutch 35 between the pulley 32 and the pump shaft 34 of the air pump 30, the electromagnetic clamp 35 is disconnected. When the air pump 3
The drive of 0 is made to stop at an angle of 11 degrees. 36 is a check valve installed in the air introduction passage 37 to the air pump 30, and 38 is a check valve installed in the air relief passage 39.
It is a relief valve that has been installed.

−〇 − 51、た、40は各fili if−り御のための制御
コニツ[−であり、例えば第3図に示すにうにマイクロ
コンビコータを用いた制御部41おJ:び各種変換%:
42〜4/Iを含んでいる。上記制御部41には、通常
運転I)の給気制御のため、ア//けル1;IIαセン
サ51からA 、/ D変換器’12を介して与えられ
るアイ7【ごル開度信同ど、クランイノ角1!ン(15
2からF/V(周波数−電圧)変換器43お1:びA 
、/ D変換器44を介してI−iλら4′Iる丁−ン
ジン回転数信円と、クランイノ角センη°52からのク
ランク角信弓とが入力さ11でいる。さらに、Jンジン
始仙時の制御のため、運転開始時や1シスト時などに始
動操作が行われたときこれを検出覆る始動[ン4)53
からの始動信号がインタラブ1〜(割り込み(li号)
として上記制御部41に入力されている。上記制御部4
1は、通常運転時には、エンジン回転数とアクセル開度
とで法定される0荷状態に応じ、燃料噴射ポンプ23の
作動おにび空気噴射弁22の開閉作動を制御Nるととも
に、前記スワール調節弁10のアクチュエータ11を制
御している。ざら−7− にこの間胛部41は、始動時に空気ポンプ30からの加
圧空気の供給を停止する制御手段としての間OLを有し
、後に詳述覆るように、始動ロン4ノ゛53からの信号
に応じ、前記電磁クラッチ35を制on−y−るどどし
に、吸気絞り弁12のアクグー:IT−ウ12aの制御
おJ:び始動用燃料制御を行うようにしでいる。
-〇- 51, 40 are control units for controlling each fili-if-reference, for example, a control unit 41 using a micro combi coater as shown in FIG. 3 and various conversion percentages:
Contains 42-4/I. The control section 41 receives an A//KEL 1; II α sensor 51 via an A/D converter '12 for air supply control during normal operation I). Similarly, Clan Ino Kaku 1! (15)
2 to F/V (frequency-voltage) converter 43 and 1: and A
, /D converter 44, the engine rotational speed signal from I-iλ et al. Furthermore, in order to control the start of the engine, when a starting operation is performed at the start of operation or during one shift, this is detected and reversed.
The start signal from
It is input to the control section 41 as follows. The control section 4
1, during normal operation, controls the operation of the fuel injection pump 23 and the opening/closing operation of the air injection valve 22 according to the legal zero load state based on the engine speed and the accelerator opening, and also controls the swirl adjustment. The actuator 11 of the valve 10 is controlled. In addition, the intermediate section 41 has an intermediate OL as a control means for stopping the supply of pressurized air from the air pump 30 at the time of startup, and as will be described in detail later, the intermediate section 41 has a In response to the signal, the electromagnetic clutch 35 is turned on to control the IT-U 12a of the intake throttle valve 12 and to control the starting fuel.

上記制御部41内には、予め種々の運転状態にお番プる
燃料と空気の各噴射開始時期おJ:び各噴射終了時期が
データマツプとして配憶され、例えば第4図に示すよう
な特性で上記各時期が制御されるように上記マツプが作
成されCいる。ずな4つら、第4図において、FsおJ
ζび「eはイれぞれ燃料の噴射開始時期および噴射終了
時期、A S ;J3よびAeはそれぞれ空気の噴射開
始時期おにび噴射終了時+111を示し、■は点火時期
を示づ。この図のように、低負荷領域では層状給気を行
うように圧縮行稈後平で燃料おにび空気が噴mされ、こ
れらの噴射終了時期Fe、Aeが点火時期■に(Jぼ一
致するようにしている。イして、燃オニIおよび空気の
−〇 − 噴1(fiは噴射1町間に依存するので、負荷に応じた
適当な噴用邑が得られるように、燃料および空気の噴射
開始Rtl[lFs、Asが設定されている。燃料噴射
量が増加される高負荷時には、層状給気の必要が/、、
 、/、、むしろ空気利用率を高めて出力を向上させる
には燃料を分散ざぜた状態で着火する方が望81ニジい
ため、負荷がある稈磨高くなると燃IIおよび空気の噴
射時1■を望め、高負荷領域では吸気行稈のが1里に燃
r1が噴射されるようにしている。
In the control unit 41, the injection start timings and injection end timings of fuel and air corresponding to various operating conditions are stored in advance as a data map, and the characteristics as shown in FIG. 4 are stored in advance. The above map is created so that each of the above periods is controlled. Four Zuna, in Figure 4, Fs O J
ζ and "e indicate the fuel injection start time and injection end time, respectively, A S ;J3 and Ae indicate the air injection start time and injection end time +111, respectively, and ■ indicates the ignition timing. As shown in this figure, in the low load region, fuel and air are injected at the back of the compressor culm to perform stratified air supply, and these injection end timings Fe and Ae coincide with the ignition timing (J). Then, the fuel and air injection 1 (fi depends on the injection 1 interval, so the fuel and air are Air injection start Rtl [lFs, As is set. At high load when the fuel injection amount is increased, stratified air supply is required.
,/, Rather, in order to increase the air utilization rate and improve the output, it is better to ignite the fuel in a dispersed state, so when the load is high on the culm, it is necessary to In the high load range, fuel is injected at one point in the intake culm.

また、この特性図に示さないが、エンジンの始動時には
、上記低f′J荷領域と比べて燃料の噴射時期を甲める
とともに、ある程度燃料噴OA組を増量するように設定
されている。
Further, although not shown in this characteristic diagram, when the engine is started, the fuel injection timing is set earlier than in the above-mentioned low f'J load region, and the amount of the fuel injection OA group is increased to some extent.

さらに上記制御部41内には、予め種々の負荷状態にお
けるスワールB1節弁100開度がデータマツプとして
記憶され、低負荷時に前記スワール調節弁10を閉じ、
で1荷が高くなるとイれに応じた開度にスワール調節弁
10を開くように、上記マツプが作成されている。
Further, in the control section 41, the opening degrees of the swirl B1 control valve 100 under various load conditions are stored in advance as a data map, and the swirl control valve 10 is closed when the load is low.
The above map is created so that when the load becomes high, the swirl control valve 10 is opened to an opening degree corresponding to the drop.

上記制御ユニツ1へ/IOにJ:って実行される制御−
9− を70−ヂャ−1−で示寸ど第5図おJ:び第6図のj
;うになる。
Control executed by J: to the above control unit 1/IO
9- is shown in 70-dia-1- as shown in Figure 5 and J: and Figure 6.
; become angry.

エンジンの始動時以外は第5図に示1メインルーヂンに
よる制御が行われ、先ず負荷状態を決定りるアクセル間
mAどJンジン回転数Rの名検出信号が入力され(ステ
ップ×1 )、この信号に基づき、予め前記の第4図に
示す特性をうえるように設定されたマツプから、その鮎
のf1荷状態に応じた燃料ど空気の6噴Q・1聞始肋1
1As、Fsおよび各噴射終了時期Ae、 Feが演算
される〈ステップX2 、 X3 )。次に、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
噴射開始時期Δs、「sに達りるのを持ってから、燃F
lおよび空気の噴口・jを開始する制御が行われる(ス
テップ×4〜Xs )。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が上記噛!J1終
了時明△e、Feに達す−るのを持ってから、燃料およ
び空気の噴射を終了でる制御が行われる(ステップX7
 =X9 )。ざらに、十記アクセル開度Aとエンジン
回転数Rとに応じて、前記スワ−10− −ル調節升10の聞1!J、(S弁聞麻)Soが部枠さ
れ、この開度Soをjgえる制御信号が前記アクチコ工
−タ11に出力される(ステップX1a、Xη)1.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−(いる、1 このような制御にJ、れば、低角荷時には、圧縮h P
i! 1G ’l’ 17) r9i定I+51111
 ニ燃1’l I’CI ’)l jt 21 h’ 
ラH’、i ’9(7ラグ20に向+1で燃INlが噴
射されることにJ:す、−1−に点火lラグイζ1)1
1に燃料が存右1ろ状態で点火が行われ、少ない燃料で
も4火、燃焼が可能となる。この1易合、低i″I荷時
はあまり高出力が曹求されず、かつ既にエンジンが作動
している状態にあるので、上記の層状給気にJこる燃焼
によってt)Tンジン作動に支障はなく、また、この場
合に一次吸気通路8がら空気が過剰に吸気されて−b差
し支えないのでボンピングロスも低減される。そして、
空気1I11射弁22からは唱用燃料に向けて空気が噴
射されることにより、噴射燃料の霧化、気化が促進され
、名犬性および燃焼性が向」ニされる。
Except when the engine is started, control is performed according to the main routine shown in Fig. 5. First, a detection signal of engine rotation speed R such as mA between accelerators and engine speed R, which determines the load condition, is input (step x 1). Based on the signal, 6 injections of fuel and air, Q.
1As, Fs and each injection end timing Ae, Fe are calculated (steps X2, X3). Next, while repeatedly inputting the detection signal of the crank angle θ, after the crank angle θ reaches the injection start timing Δs, s, the fuel
Control is performed to start l and air nozzle j (steps x4 to xs). Subsequently, while repeatedly inputting the detection signal of the crank angle θ, the crank angle θ reaches the above value! After reaching light Δe and Fe at the end of J1, control is performed to end fuel and air injection (step X7).
=X9). Roughly, depending on the accelerator opening A and the engine speed R, the swirl adjustment scale 10 is adjusted according to the 10 degrees of the accelerator opening A and the engine speed R. J, (S valve position) So is set, and a control signal for controlling the opening So is output to the actuator 11 (steps X1a, Xη)1. After that, return to step x1 and repeat the above flow.
i! 1G 'l' 17) r9i constant I+51111
21'l I'CI')l jt 21 h'
La H', i '9 (7 lag 20 to be injected with fuel INl at +1 J:su, -1- to ignition l lag ζ 1) 1
Ignition is performed when fuel is present in the first place, making it possible to burn four flames even with a small amount of fuel. In this case, when the load is low, not much high output is produced and the engine is already in operation, so the stratified air charge combustion causes the T engine to operate. There is no problem, and in this case, there is no problem with excessive intake of air from the primary intake passage 8, so the pumping loss is also reduced.
Air is injected from the air 1I11 injection valve 22 toward the injected fuel, thereby promoting atomization and vaporization of the injected fuel, thereby improving its performance and combustibility.

一方、高負荷時には、燃料噴射量が増量される− 11
 − どと1)に、吸気行程の前半に燃料が哨削され、31゜
た、スワール調節弁10が聞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v1が燃焼室7内に充分拡散されてから点火が行われ
る。
On the other hand, when the load is high, the amount of fuel injection is increased.
- In 1), the fuel is extracted in the first half of the intake stroke, and the swirl control valve 10 is activated at 31 degrees, and the swirl in the combustion chamber 7 is increased by the intake air from the secondary intake passage 9.
Ignition is performed after the fuel v1 is sufficiently diffused within the combustion chamber 7.

また、9h動時には第6図に示す割込みルーチンにj、
る制御が行われる。この制御は前8d始動1?ンサ53
からの信号によって開始され、先ず前記電磁クラップ3
5をOFFと1ノ(ステップY+ )、次に予め設定さ
れた胎動用の燃料+1fi161時期おJ−び燃r1噴
射帛をも−)−(燃籾噴用を行い(ステップY2)、さ
らに吸気絞り弁12を所定間度開じるようにそのアクチ
1■−夕12aを制御りる(ステップY3 )。そして
、胎動が終了したか否かを判別しくステップY4)、始
動が終了1ノーる:1.では上記のステップY1〜Y3
を繰返し、始O1が終了すれば電磁クラッチ35をON
とするとどしに吸気絞り弁12を間きくステップYs、
Ye)、−’Pの後第5図のメインルーチンに戻される
ようにしている。
Also, when operating for 9 hours, the interrupt routine shown in FIG.
control is performed. Is this control before 8d start 1? Nsa 53
is started by a signal from the electromagnetic clap 3.
5 to OFF and 1 no (step Y+), then preset fuel for fetal movement +1fi161 timing and fuel r1 injection fabric-)-(fuel for paddy injection (step Y2), and then intake The actuator 12a is controlled to open the throttle valve 12 for a predetermined period of time (step Y3).Then, it is determined whether the fetal movement has ended or not (step Y4), and the start is completed. :1. Now, step Y1 to Y3 above.
Repeat this, and when the first O1 is completed, turn on the electromagnetic clutch 35.
Step Ys, which closes the intake throttle valve 12 as soon as possible.
After Ye) and -'P, the process returns to the main routine shown in FIG.

= 12 − この制御により、始f’JJ +11が向上される。つ
まり、エンジンの始動が完了するまでは、温度−に胃を
促進りる等のため、ある秤度燃料を増囲覆るとともに燃
焼室7内全体に燃F1を拡散させた状態で燃焼さヒる方
が好ましいため、燃f++噴射時1!0を望め、層状給
気は行わないようにしている。そしてこの場合、空気が
過剰に供給されると始動時の適正空燃比が得られなくな
るので、吸気絞り弁12を小開度に閉じて吸入空気量を
減少させるとともに、前記電磁クラッチ35をOFFと
することにより空気ボン130を停止させ、燃焼室7へ
の加圧空気の供給を停止させており、こうして始動性を
向上しているのである。
= 12 - This control improves the initial f'JJ +11. In other words, until the start of the engine is completed, a certain amount of fuel is surrounded and covered, and the fuel F1 is spread throughout the combustion chamber 7 and burned in order to promote the stomach temperature to -. Since this is more preferable, a fuel f++ of 1!0 can be expected during injection, and stratified air supply is not performed. In this case, if too much air is supplied, it will not be possible to obtain an appropriate air-fuel ratio at startup, so the intake throttle valve 12 is closed to a small opening to reduce the amount of intake air, and the electromagnetic clutch 35 is turned off. By doing so, the air cylinder 130 is stopped and the supply of pressurized air to the combustion chamber 7 is stopped, thereby improving startability.

第7図および第8図は別の実施例を示す。この実施例に
示Jエンジンも層状給気エンジンであるが、燃料噴射弁
21′おJ:び空気噴射弁22が一次吸気ボート13に
設けられている。この場合も、燃料1171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r1と干渉する方向に空気をlIN
%射するように配置されて−13− いる。;1、たこの実施例において燃刺噴r1・1弁2
′1′は、空気噴射弁22ど同様に、制御コニツ1−4
0によ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r1噴射弁21′は、通常のガソリンエ
ンジンに用いられているJ:うな燃料1rl口・1ポン
プ(図示省略)に接続しておt′jばにい。
7 and 8 show another embodiment. The J engine shown in this embodiment is also a stratified air charge engine, but the fuel injection valve 21' and the air injection valve 22 are provided in the primary intake boat 13. In this case as well, the fuel 1171 injection valve 21'
is arranged toward the spark plug 20 in the combustion chamber 7, and the air injection valve 22 injects air in a direction that interferes with the injected fuel r1.
-13- It is arranged so that it radiates %. ;1. In the embodiment of the octopus, fuel injection r1.1 valve 2
'1', like the air injection valve 22, is the control unit 1-4.
In this case, the fuel r1 injection valve 21' is connected to a fuel 1rl port/1 pump (not shown) used in a normal gasoline engine. Please leave it to me.

このJ:うに上記各噴射弁21’ 、22を吸気ポー 
1−13に股(プる場合、吸気弁16が閉じるまでに燃
料を噴射させる必要があるので、第9図に示すように、
低負荷領域では吸気行程の終期に燃料おj;び空気が1
@射されるようにそれぞれの噴04間始開始As、FS
および噴射終了時1111 F e 、△eが設定され
ているが、その他の構成は第1の実施例と同様である。
This J: Sea urchin connects each of the above injection valves 21' and 22 to the intake port.
1-13, it is necessary to inject fuel before the intake valve 16 closes, so as shown in Fig. 9,
In the low load region, at the end of the intake stroke, the fuel and air are
@Start As, FS of each jet 04 to be injected
and 1111 F e at the end of injection, Δe are set, but the other configurations are the same as in the first embodiment.

なお、図に示す実施例では、エンジンの始動時に前記電
磁クラッチ35をOFFと(〕て空気ポンプ30の作動
を停由さ「るようにしでいるが、エンジン始動時にも空
気ポンプ30ば作動させながら加圧空気の全量をリリー
フ用通路39に流J゛ように制御してもよい。また、本
発明が適用される− 14 − エンジンは層状給気エンジンに限定されず、例えば燃焼
室に渦流を生じさせて燃焼速度を高めるため空気噴射弁
および空気ポンプを設けたエンジンに適用してもよ(、
この場合でも始動時の加圧空気の供給を停止lりること
は始Wh 個の向上に0効である。
In the embodiment shown in the figure, the electromagnetic clutch 35 is turned OFF () to stop the operation of the air pump 30 when the engine is started, but the air pump 30 is also operated when the engine is started. However, the entire amount of pressurized air may be controlled so as to flow into the relief passage 39.Furthermore, the engine to which the present invention is applied is not limited to a stratified air supply engine; It may also be applied to engines equipped with air injection valves and air pumps to increase the combustion rate.
Even in this case, stopping the supply of pressurized air at startup has no effect on improving the starting speed.

(発明の効!!り 以上のように本発明は、燃焼室に加圧空気を供給づる空
気噴q4弁および空気ポンプを設けたエンジンにおいて
、エンジンの始動時に加圧空気の供給を停止するように
しているため、始動時に過剰に空気が供給されることを
防止して始動性を向上することができるものである。
(Effects of the Invention!!) As described above, the present invention provides a method for stopping the supply of pressurized air when starting the engine in an engine equipped with an air injection Q4 valve and an air pump that supply pressurized air to the combustion chamber. This prevents excessive air from being supplied during startup and improves startup performance.

【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J5びその近傍部の拡大図、第3図は
制御系統のブ[1ツク図、第4図は燃料おJ:び空気の
哨q・1時期のrf性図、第5図および第6図(tフロ
ーヂャ−1〜、第7図は別の実施例を示J全体概略図、
第8図はイの第2図相当図、第一 15 − 9図【沫この実施例による場合の第4図相当図である。 7・・・燃焼室、22・・・空気噴射弁、30・・・空
気ポンプ、35・・・電磁クラッチ、40・・・制御ユ
ニツl− 。 1′!1許出願人 東洋工業株式会ネ1− 16 = 第 2 図 第 3 図 第 8 図 第9図 ム 貝荷
Fig. 1 is an overall schematic diagram showing one embodiment of the present invention, Fig. 2 is an enlarged view of the combustion chamber part, J5 and its vicinity, Fig. 3 is a block diagram of the control system, and Fig. 4 is a block diagram of the control system. RF characteristic diagram of fuel and air flow chart 1 period, Figures 5 and 6 (t flowchart 1 to 7, Figure 7 shows another example, J overall schematic diagram,
FIG. 8 is a diagram corresponding to FIG. 2 of A, and FIG. 15-9 is a diagram equivalent to FIG. 4 in the case of this embodiment. 7... Combustion chamber, 22... Air injection valve, 30... Air pump, 35... Electromagnetic clutch, 40... Control unit l-. 1′! 1 Applicant: Toyo Kogyo Co., Ltd. Ne1-16 = Figure 2 Figure 3 Figure 8 Figure 9 Mussel cargo

Claims (1)

【特許請求の範囲】[Claims] 1、エンジンの燃焼室に空気を供給りるための空気噴射
弁と、該空気噴射弁へ加圧空気を供給する空気ポンプと
を備えたエンジンにおいて、エンジンの始動を検出する
始動センサと、該始動センサの出力を受けて始動時に上
記空気ポンプからの加圧空気の供給を停止する制御手段
とを設Gjたことを特徴とするエンジン。
1. In an engine equipped with an air injection valve for supplying air to a combustion chamber of the engine and an air pump for supplying pressurized air to the air injection valve, a starting sensor for detecting engine starting; An engine characterized in that it is provided with a control means for receiving an output from a starting sensor and stopping the supply of pressurized air from the air pump at the time of starting.
JP58144267A 1983-08-05 1983-08-05 Engine Pending JPS6035143A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58144267A JPS6035143A (en) 1983-08-05 1983-08-05 Engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58144267A JPS6035143A (en) 1983-08-05 1983-08-05 Engine

Publications (1)

Publication Number Publication Date
JPS6035143A true JPS6035143A (en) 1985-02-22

Family

ID=15358110

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58144267A Pending JPS6035143A (en) 1983-08-05 1983-08-05 Engine

Country Status (1)

Country Link
JP (1) JPS6035143A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63143349A (en) * 1986-12-08 1988-06-15 Mazda Motor Corp Suction device for engine
WO1990000222A1 (en) * 1988-07-01 1990-01-11 Toyota Jidosha Kabushiki Kaisha Two-cycle internal combustion engine
US5239960A (en) * 1991-07-30 1993-08-31 Mazda Motor Corporation Engine induction system provided with a mechanical supercharger
WO2007124046A1 (en) * 2006-04-20 2007-11-01 Sturman Digital Systems, Llc Low emission high performance engines, multiple cylinder engines and operating methods
US7958864B2 (en) 2008-01-18 2011-06-14 Sturman Digital Systems, Llc Compression ignition engines and methods
JP2016176383A (en) * 2015-03-19 2016-10-06 本田技研工業株式会社 Cylinder injection type internal combustion engine

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5642731A (en) * 1979-09-14 1981-04-21 Gomma Antivibranti Applic Buffer for absorbing striking energy
JPS5746018A (en) * 1980-09-01 1982-03-16 Shuichi Kitamura Intake device for engine supplied with laminar mixture

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5642731A (en) * 1979-09-14 1981-04-21 Gomma Antivibranti Applic Buffer for absorbing striking energy
JPS5746018A (en) * 1980-09-01 1982-03-16 Shuichi Kitamura Intake device for engine supplied with laminar mixture

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63143349A (en) * 1986-12-08 1988-06-15 Mazda Motor Corp Suction device for engine
WO1990000222A1 (en) * 1988-07-01 1990-01-11 Toyota Jidosha Kabushiki Kaisha Two-cycle internal combustion engine
US5062395A (en) * 1988-07-01 1991-11-05 Toyota Jidosha Kabushiki Kaisha Two-stroke internal combustion engine
US5239960A (en) * 1991-07-30 1993-08-31 Mazda Motor Corporation Engine induction system provided with a mechanical supercharger
WO2007124046A1 (en) * 2006-04-20 2007-11-01 Sturman Digital Systems, Llc Low emission high performance engines, multiple cylinder engines and operating methods
US7958864B2 (en) 2008-01-18 2011-06-14 Sturman Digital Systems, Llc Compression ignition engines and methods
JP2016176383A (en) * 2015-03-19 2016-10-06 本田技研工業株式会社 Cylinder injection type internal combustion engine

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