JPH0240859B2 - - Google Patents
Info
- Publication number
- JPH0240859B2 JPH0240859B2 JP56118955A JP11895581A JPH0240859B2 JP H0240859 B2 JPH0240859 B2 JP H0240859B2 JP 56118955 A JP56118955 A JP 56118955A JP 11895581 A JP11895581 A JP 11895581A JP H0240859 B2 JPH0240859 B2 JP H0240859B2
- Authority
- JP
- Japan
- Prior art keywords
- cylinder
- engine
- fuel
- ignition
- dead center
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/30—Controlling fuel injection
- F02D41/32—Controlling fuel injection of the low pressure type
- F02D41/34—Controlling fuel injection of the low pressure type with means for controlling injection timing or duration
- F02D41/345—Controlling injection timing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine management systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Description
【発明の詳細な説明】
本発明は少気筒エンジンに適した燃料噴射制御
方法に関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a fuel injection control method suitable for small cylinder engines.
吸気管内に燃料を噴射する燃料噴射装置は、一
般に、燃料噴射量の制御系統を簡素化するため毎
回転同時方法、例えば6気筒エンジンではエンジ
ンの1回転で全気筒の燃焼に必要な量の半分が噴
射され、次の1回転で残りの半分が噴射される方
法が実施されており、噴射時期は点火信号の分周
波に同期させる方式、同じく6気筒エンジンの場
合でみると、第1図Aに示すように、エンジンの
一回転に3パルスある点火信号を1/3分周して噴
射時期信号とする方式が多くとられている。4気
筒エンジンの場合でも同様にエンジンの1回転に
2パルスある点火信号を1/2分周して噴射時期信
号を得るので、容易に毎回転同時噴射を行なうこ
とができる。 Generally speaking, fuel injection devices that inject fuel into the intake pipe use a method that simplifies the control system for the amount of fuel injected at the same time every revolution. For example, in a six-cylinder engine, one revolution of the engine injects half of the amount required for combustion in all cylinders. is injected, and the remaining half is injected in the next revolution, and the injection timing is synchronized with the frequency division of the ignition signal. As shown in Figure 2, a method is often adopted in which the frequency of the ignition signal, which has three pulses per engine revolution, is divided by 1/3 and used as the injection timing signal. In the case of a four-cylinder engine, the injection timing signal is similarly obtained by dividing the frequency of the ignition signal, which has two pulses per engine revolution, by 1/2, so that simultaneous injection can be easily performed at every revolution.
ところが3気筒エンジンの場合は第1図Bに示
すように、点火信号はエンジンの1回転ごとに2
パルスと1パルスを交互に繰り返しているので、
6気筒エンジンや4気筒エンジンのように点火信
号の分周波に同期させて噴射時期信号を得、1回
転に1回燃料噴射をすることができず、2回転に
3パルスある点火信号を1/3分周し2回転に1回
燃料噴射を行なうことになる。つまり、3気筒エ
ンジンではエンジンの2回転に1回3気筒分の燃
料を全量噴射することになる。 However, in the case of a three-cylinder engine, as shown in Figure 1B, the ignition signal changes twice every revolution of the engine.
Since pulses and 1 pulse are repeated alternately,
Unlike 6-cylinder engines and 4-cylinder engines, the injection timing signal is synchronized with the divided wave of the ignition signal, and it is not possible to inject fuel once per revolution, so the ignition signal has 3 pulses per 2 revolutions. The frequency is divided into 3 and fuel injection is performed once every 2 revolutions. In other words, in a three-cylinder engine, the entire amount of fuel for three cylinders is injected once every two rotations of the engine.
このため、3気筒エンジンでは1回当りの噴射
量が多くなり、噴射時期に各気筒が吸入、圧縮、
爆発、排気のいずれの行程にあるか、特に吸入弁
が開いているか否かで、吸入条件が大きく異な
り、3気筒間の燃料分配が不安定であつた。その
ため、過吸収により空燃比が増大し、未燃炭化水
素(HC)の増加をまねていた。 For this reason, in a three-cylinder engine, the amount of injection per injection is large, and each cylinder has suction, compression, and
Intake conditions varied greatly depending on whether the engine was in the explosion or exhaust stroke, especially whether the intake valve was open or not, and fuel distribution among the three cylinders was unstable. Therefore, the air-fuel ratio increased due to overabsorption, mimicking an increase in unburned hydrocarbons (HC).
本発明の目的は、3気筒間の燃料分配を安定さ
せ燃焼バランスを良好にすることにより、滑らか
なエンジン回転状態を得るとともに、排出ガス
(HC)の特性を改善できる燃料噴射制御方法を
提供することにある。 An object of the present invention is to provide a fuel injection control method that can stabilize fuel distribution among three cylinders and improve combustion balance, thereby achieving smooth engine rotation and improving exhaust gas (HC) characteristics. There is a particular thing.
前記目的を達成するために本発明による第1の
燃料噴射制御方法は、ポイント式の点火装置を有
し、エンジンの回転に同期してその2回転で3回
点火信号を発生し点火を行なうエンジンの燃料噴
射制御方法において、第1気筒の点火時期より所
定時間遅延させ第1気筒の点火時期に吸入行程に
ある第3気筒のクランク角度が下死点前40度から
下死点後60度の範囲内で各気筒に燃料を同時噴射
するように構成されている。 In order to achieve the above object, a first fuel injection control method according to the present invention provides an engine that has a point type ignition device and generates an ignition signal three times in two rotations in synchronization with the rotation of the engine to ignite the engine. In the fuel injection control method, the ignition timing of the first cylinder is delayed by a predetermined period of time, and the crank angle of the third cylinder, which is in the intake stroke, is changed from 40 degrees before bottom dead center to 60 degrees after bottom dead center. It is configured to simultaneously inject fuel into each cylinder within a range.
本発明による第2の燃料噴射方法は、ポイント
式の点火装置を有し、エンジンの回転に同期して
その2回転で3回点火信号を発生し点火を行なう
エンジンの燃料噴射制御方法において、前記エン
ジンがアイドリングまたは減速の状態にあること
を検出して、第1気筒の点火時期より所定時間遅
延させ第1気筒の点火時期に吸入行程にある第3
気筒のクランク角度が下死点前40度から下死点後
60度の範囲内で各気筒に燃料を同時噴射するよう
にし、それ以外の状態では第1気筒の点火時期に
同期して各気筒に燃料を同時噴射するように構成
されている。 A second fuel injection method according to the present invention is a fuel injection control method for an engine that has a point-type ignition device and generates an ignition signal three times in two rotations in synchronization with the rotation of the engine to perform ignition. It detects that the engine is idling or decelerating, and delays the ignition timing of the first cylinder by a predetermined period of time so that the ignition timing of the third cylinder, which is in the intake stroke, is delayed by a predetermined period of time from the ignition timing of the first cylinder.
Cylinder crank angle changes from 40 degrees before bottom dead center to after bottom dead center
Fuel is injected simultaneously into each cylinder within a range of 60 degrees, and in other conditions, fuel is injected simultaneously into each cylinder in synchronization with the ignition timing of the first cylinder.
前記構成によれば本発明の目的は完全に達成で
きる。 According to the above structure, the object of the present invention can be completely achieved.
以下図面等を参照して従来例と比較しながら本
発明をさらに詳しく説明する。 The present invention will be described in more detail below with reference to the drawings and in comparison with conventional examples.
第2図は噴射時期と各気筒の吸入弁開時期を示
す図である。第2図において縦軸の1、3、2は
それぞれ第1気筒、第3気筒、第2気筒であり点
火順序を示しており、横軸はクランク角度を示
し、Tは上死点、Bは下死点である。点火時期S
は各気筒の上死点前10度であり、従来の燃料噴射
時期は点火信号を1/3分周させて第1気筒の点火
に同期して噴射していた。第1気筒の点火に同期
させて噴射すると(第2図Iの時点)各気筒の吸
入弁は、第1気筒は燃焼行程中で閉、第3気筒は
吸入行程中で開、第2気筒は排気行程中で閉の状
態にあり、3気筒間の吸入条件の差が大きいこと
がわかる。このうち、第3気筒は燃料噴射時期に
吸入弁が開いているので、第3気筒のピストンが
下死点付近まで下降した時点で燃料を噴射すれ
ば、吸入弁は開いていても吸入作用は弱まつてい
るので、他の2つの気筒の吸入条件に近づくこと
がわかる(第2図Jの時点)。 FIG. 2 is a diagram showing the injection timing and the intake valve opening timing of each cylinder. In Fig. 2, 1, 3, and 2 on the vertical axis are the first cylinder, third cylinder, and second cylinder, respectively, and indicate the ignition order, the horizontal axis indicates the crank angle, T is the top dead center, and B is the top dead center. It is bottom dead center. Ignition timing S
is 10 degrees before the top dead center of each cylinder, and the conventional fuel injection timing was to divide the ignition signal by 1/3 and inject in synchronization with the ignition of the first cylinder. When the injection is synchronized with the ignition of the first cylinder (at the point I in Fig. 2), the intake valves of each cylinder are closed during the combustion stroke for the first cylinder, open during the intake stroke for the third cylinder, and open for the second cylinder during the intake stroke. It is in a closed state during the exhaust stroke, and it can be seen that there is a large difference in the intake conditions among the three cylinders. Of these, the intake valve of the 3rd cylinder is open at the time of fuel injection, so if fuel is injected when the piston of the 3rd cylinder descends to near the bottom dead center, there will be no suction action even if the intake valve is open. It can be seen that the suction conditions have weakened, approaching the intake conditions of the other two cylinders (at the time of J in FIG. 2).
さらに本件発明者等は、噴射時期の遅延と排出
HC濃度との関係を実験により求め、第3図のよ
うな結果を得た。第3図において、横軸はクラン
ク角度、縦軸は排出HC濃度を示している。ここ
では、一番問題になる第3気筒における排出HC
濃度を示しているが、点火同期噴射から下死点前
40度くらいまではHC濃度が高く燃焼状態が不安
定であり、それ以降下死点後60度くらいまでは安
定した燃焼をしていることがわかる。つまり3気
筒エンジンの場合、燃料噴射時期を吸入行程の気
筒、ここでは第3気筒、のクランク角度が下死点
前40度から下死点後60度の範囲にすれば、各気筒
の吸入配分が安定し、燃焼バランスが良好にな
り、それに伴い排ガス特性を改善されることがわ
かつた。 In addition, the inventors of the present invention are concerned with delaying injection timing and evacuation.
The relationship with HC concentration was determined through experiments, and the results shown in Figure 3 were obtained. In FIG. 3, the horizontal axis shows the crank angle, and the vertical axis shows the discharged HC concentration. Here, we will focus on the exhaust HC in the third cylinder, which is the most problematic.
Although the concentration is shown, it is before bottom dead center from ignition synchronized injection.
It can be seen that up to about 40 degrees, the HC concentration is high and the combustion state is unstable, and after that, combustion is stable until about 60 degrees after bottom dead center. In other words, in the case of a 3-cylinder engine, if the crank angle of the cylinder on the intake stroke, here the 3rd cylinder, is in the range of 40 degrees before bottom dead center to 60 degrees after bottom dead center, the intake distribution for each cylinder can be adjusted. It was found that the fuel consumption was stabilized, the combustion balance was improved, and the exhaust gas characteristics were improved accordingly.
次に第4図を参照しながら本発明の構成を説明
する。第4図は本発明による第1の方法を実施す
る燃料噴射制御装置の実施例を示すブロツク図で
ある。エンジンの2回転に3回点火信号の発生す
る点火装置1の点火信号2を分周回路3で1/3分
周し、分周信号4は、第1気筒の点火時期に吸入
行程にある第3気筒のクランク角度を下死点前40
度から下死点後60度の範囲内で遅延させる遅延回
路5を介して得られる噴射時期発生信号6により
インジエクタ7から燃料を噴射させるように構成
されている。ここでは遅延回路5は分周回路3の
後に挿入したが分周回路3の前に設けることも可
能である。 Next, the configuration of the present invention will be explained with reference to FIG. FIG. 4 is a block diagram showing an embodiment of a fuel injection control device implementing the first method according to the present invention. The frequency of the ignition signal 2 of the ignition device 1, which generates an ignition signal three times every two revolutions of the engine, is divided by 1/3 by the frequency dividing circuit 3. 3 cylinder crank angle 40 before bottom dead center
The fuel is injected from the injector 7 in response to an injection timing generation signal 6 obtained via a delay circuit 5 which delays the injection timing within a range of 60 degrees after the bottom dead center. Here, the delay circuit 5 is inserted after the frequency divider circuit 3, but it can also be provided before the frequency divider circuit 3.
第5図は本発明による第2の方法を実施する燃
料噴射制御装置の実施例を示したブロツク図であ
る。前述したような3気筒間の混合気分配の誤差
が大きく表われるのはアイドリング時または減速
時等の軽気筒状態であることに着目し、アクセル
ペダルまたはスロツトルシヤフト部に設けられた
開度センサ8からの信号により、軽負荷状態であ
るか否かを判別回路9を分周回路3と遅延回路5
間に設け、軽負荷状態のときには遅延回路5を介
した噴射時期信号6によりインジエクタ7から燃
料を噴射させ、軽負荷状態でないときには分周信
号4を遅延回路5を通さず噴射時期信号として用
いインジエクタ7から燃料を噴射させるように構
成したものである。また、軽負荷状態の判別は吸
管内に設けられた負圧センサからの信号により判
別することも可能である。 FIG. 5 is a block diagram showing an embodiment of a fuel injection control device implementing the second method according to the present invention. Focusing on the fact that the above-mentioned error in the mixture distribution between the three cylinders is most apparent in light cylinder conditions such as when idling or decelerating, we developed an opening sensor installed on the accelerator pedal or throttle shaft. Based on the signal from 8, the circuit 9 determines whether or not it is in a light load state.
When the load is light, the injection timing signal 6 passed through the delay circuit 5 is used to inject fuel from the injector 7, and when the load is not light, the divided signal 4 is used as the injection timing signal without passing through the delay circuit 5. The structure is such that fuel is injected from 7. Further, the light load state can also be determined based on a signal from a negative pressure sensor provided in the suction pipe.
以上詳しく説明したように、本発明によれば、
燃料噴射時期を第3気筒のクランク角度が下死点
前40度から下死点後60度の範囲内に設定してある
ので、第3気筒の吸入弁が開いている間でも吸入
作用は弱まつており、他の2つの気筒の吸入条件
に近づき、各気筒の吸入配分が安定し燃焼バラン
スが良好となり、それに伴い排ガス特性も改善さ
れる。 As explained in detail above, according to the present invention,
Since the fuel injection timing is set within the range of the third cylinder's crank angle from 40 degrees before bottom dead center to 60 degrees after bottom dead center, the intake action is weak even when the third cylinder's intake valve is open. The intake conditions are close to those of the other two cylinders, the intake distribution in each cylinder is stabilized, the combustion balance is good, and the exhaust gas characteristics are also improved accordingly.
第1図は点火信号と燃料噴射時期を示した図で
あつて同図Aは6気筒エンジンの場合を同図Bは
3気筒エンジンの場合を示している、第2図は3
気筒エンジンの各行程と噴射時期を示した図、第
3図は噴射時期と排出HC濃度の関係を示すグラ
フ、第4図は本発明による第1の方法を実施する
燃料噴射制御装置の実施例を示したブロツク図、
第5図は第2の方法を実施する燃料噴射制御装置
の実施例を示したブロツク図である。
1……点火装置、2……点火信号、3……分周
回路、4……分周信号、5……遅延回路、6……
噴射時期発生信号、7……インジエクタ、8……
開度センサ、9……判別回路、T……上死点、B
……下死点。
Figure 1 shows the ignition signal and fuel injection timing. Figure A shows the case of a 6-cylinder engine, Figure B shows the case of a 3-cylinder engine, and Figure 2 shows the case of a 3-cylinder engine.
A diagram showing each cylinder engine stroke and injection timing, FIG. 3 is a graph showing the relationship between injection timing and exhaust HC concentration, and FIG. 4 is an embodiment of a fuel injection control device implementing the first method according to the present invention. A block diagram showing
FIG. 5 is a block diagram showing an embodiment of a fuel injection control device implementing the second method. DESCRIPTION OF SYMBOLS 1... Ignition device, 2... Ignition signal, 3... Frequency division circuit, 4... Frequency division signal, 5... Delay circuit, 6...
Injection timing generation signal, 7... Injector, 8...
Opening sensor, 9...Discrimination circuit, T...Top dead center, B
...Bottom dead center.
Claims (1)
転に同期してその2回転で3回点火信号を発生し
点火を行なうエンジンの燃料噴射制御方法におい
て、第1気筒の点火時期より所定時間遅延させ第
1気筒の点火時期に吸入行程にある第3気筒のク
ランク角度が下死点前40度から下死点後60度の範
囲内で各気筒に燃料を同時噴射するように構成し
たことを特徴とする燃料噴射制御方法。 2 ポイント式の点火装置を有し、エンジンの回
転に同期してその2回転で3回点火信号を発生し
点火を行なうエンジンの燃料噴射制御方法におい
て、前記エンジンがアイドリングまたは減速の状
態にあることを検出して、第1気筒の点火時期よ
り所定時間遅延させ第1気筒の点火時期に吸入行
程にある第3気筒のクランク角度が下死点前40度
から下死点後60度の範囲内で各気筒に燃料を同時
噴射するようにし、それ以外の状態では第1気筒
の点火時期に同期して各気筒に燃料を同時噴射す
るように構成したことを特徴とする燃料噴射制御
方法。[Claims] In a fuel injection control method for an engine having a one-point ignition device and generating ignition signals three times in two rotations of the engine in synchronization with the rotation of the engine, The fuel is injected into each cylinder simultaneously when the crank angle of the third cylinder, which is on the intake stroke, is within the range of 40 degrees before bottom dead center to 60 degrees after bottom dead center when the ignition timing of the first cylinder is delayed by a predetermined period of time. A fuel injection control method characterized by comprising: 2. In a fuel injection control method for an engine that has a point-type ignition device and generates an ignition signal three times in two rotations of the engine in synchronization with the rotation of the engine to ignite, the engine is in an idling or decelerating state. is detected and delayed by a predetermined period of time from the ignition timing of the first cylinder so that the crank angle of the third cylinder in the intake stroke is within the range of 40 degrees before bottom dead center to 60 degrees after bottom dead center. 1. A fuel injection control method characterized in that fuel is simultaneously injected into each cylinder in other conditions, and fuel is simultaneously injected into each cylinder in synchronization with the ignition timing of the first cylinder in other conditions.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP56118955A JPS5820933A (en) | 1981-07-28 | 1981-07-28 | Fuel injection controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP56118955A JPS5820933A (en) | 1981-07-28 | 1981-07-28 | Fuel injection controller |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5820933A JPS5820933A (en) | 1983-02-07 |
| JPH0240859B2 true JPH0240859B2 (en) | 1990-09-13 |
Family
ID=14749398
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP56118955A Granted JPS5820933A (en) | 1981-07-28 | 1981-07-28 | Fuel injection controller |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5820933A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150219041A1 (en) * | 2014-02-06 | 2015-08-06 | Kubota Corporation | Engine |
| WO2021033425A1 (en) | 2019-08-22 | 2021-02-25 | 住友金属鉱山株式会社 | Optical film, sputtering target, and film formation method for optical film |
| WO2021106254A1 (en) | 2019-11-25 | 2021-06-03 | 住友金属鉱山株式会社 | Optical film, sputtering target and method for forming optical film |
| WO2022249591A1 (en) | 2021-05-25 | 2022-12-01 | 住友金属鉱山株式会社 | Sputtering target and method for forming cesium tungsten oxide film |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3045716A1 (en) * | 1980-12-04 | 1982-07-22 | Robert Bosch Gmbh, 7000 Stuttgart | SIGNALER FOR THE TRIGGERING OF IGNITION AND INJECTION PROCESSES IN A FOUR-STOCK COMBUSTION ENGINE |
-
1981
- 1981-07-28 JP JP56118955A patent/JPS5820933A/en active Granted
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150219041A1 (en) * | 2014-02-06 | 2015-08-06 | Kubota Corporation | Engine |
| US9784153B2 (en) * | 2014-02-06 | 2017-10-10 | Kubota Corporation | Engine |
| WO2021033425A1 (en) | 2019-08-22 | 2021-02-25 | 住友金属鉱山株式会社 | Optical film, sputtering target, and film formation method for optical film |
| WO2021106254A1 (en) | 2019-11-25 | 2021-06-03 | 住友金属鉱山株式会社 | Optical film, sputtering target and method for forming optical film |
| WO2022249591A1 (en) | 2021-05-25 | 2022-12-01 | 住友金属鉱山株式会社 | Sputtering target and method for forming cesium tungsten oxide film |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5820933A (en) | 1983-02-07 |
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