JPS6045779A - Ignition timing controller for internal-combustion engine - Google Patents

Ignition timing controller for internal-combustion engine

Info

Publication number
JPS6045779A
JPS6045779A JP15160283A JP15160283A JPS6045779A JP S6045779 A JPS6045779 A JP S6045779A JP 15160283 A JP15160283 A JP 15160283A JP 15160283 A JP15160283 A JP 15160283A JP S6045779 A JPS6045779 A JP S6045779A
Authority
JP
Japan
Prior art keywords
ignition timing
speed
advance
maximum output
output
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
JP15160283A
Other languages
Japanese (ja)
Other versions
JPS6252137B2 (en
Inventor
Yuzuru Nanba
難波 譲
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.)
Suzuki Motor Corp
Original Assignee
Suzuki 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 Suzuki Motor Corp filed Critical Suzuki Motor Corp
Priority to JP15160283A priority Critical patent/JPS6045779A/en
Publication of JPS6045779A publication Critical patent/JPS6045779A/en
Publication of JPS6252137B2 publication Critical patent/JPS6252137B2/ja
Granted legal-status Critical Current

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  • Electrical Control Of Ignition Timing (AREA)

Abstract

PURPOSE:To reduce a combustion noise without sacrificing a rate of fuel consumption and power characteristics, by delaying the ignition timing of an engine in time of high engine speed. CONSTITUTION:Ignition timing by means of a centrifugal timer is set to the delay control side from optimum ignition timing so as to cause an output drop from a maximum output point to be within the range of 4% at maximum output engine speed in full load, while the said delay control value is gradually decreased at the side of lower speed than the said maximum output engine speed, making it congruous with the optimum ignition timing, and the said delay control value is gradually increased (decreasing the advance value) at the side of higher speed than the said maximum output engine speed. Thus, at the maximum output engine speed that is pretty high speed, the advance control is held down to the extent that a slight output drop is brought about, and in case of superhigh speed being more than that, further the advance control is held down to some extent, that is, there is seen a fair output drop but this must be considered as an inevitable consequence. A suchlike superhigh speed part is not remotest chance of practical use and, what is more, this disadvantage has such a reverse effect as prevention against overrotation so that it may be tolerable enough in view of practicality.

Description

【発明の詳細な説明】 〔発明の技術分野] この発明は内燃機関の点火時期制御装置の改良に係り、
特に、内燃機関の出力低下を最小限に抑えて騒音低下を
図るように点火時期を設定した遠心進角装置を備えた内
燃機関の点火時期制御装置に関する。
[Detailed Description of the Invention] [Technical Field of the Invention] The present invention relates to an improvement of an ignition timing control device for an internal combustion engine,
In particular, the present invention relates to an ignition timing control device for an internal combustion engine equipped with a centrifugal advance device that sets the ignition timing so as to minimize a decrease in the output of the internal combustion engine and reduce noise.

[発明の技術的背景] 従来、ガソリン機関等では、最良の出力性能燃費を得る
ために、機関の回転速度や負荷に応じて最適点火時期に
点火するように点火時期制御装置が設けられている。
[Technical Background of the Invention] Conventionally, gasoline engines and the like have been provided with an ignition timing control device to ignite at the optimum ignition timing according to the engine rotation speed and load in order to obtain the best output performance and fuel efficiency. .

点火時期制御装置のうち、回転速度によって点火時期を
制御する遠心進角装置は、おもりが回転の遠心力によっ
て開く現象を利用して、その変位をカム機構によってタ
イミングレバーに伝達し、回転速度に応じた進角を与え
ている。この進角は全負荷における各回転速度で最大出
力となる点火時期、すなわち最適点火時期となるように
決定されている。
Among ignition timing control devices, a centrifugal advance device that controls ignition timing based on rotational speed utilizes the phenomenon in which a weight opens due to the centrifugal force of rotation, transmits the displacement to the timing lever using a cam mechanism, and adjusts the rotational speed. The lead angle is given accordingly. This advance angle is determined to be the ignition timing that produces the maximum output at each rotational speed under full load, that is, the optimum ignition timing.

[背景技術の問題点コ ところが、近時、燃費向上のためガソリン機関等におい
ても高圧縮比(具体的には9.0以上)に設計される傾
向にあるが、シリンダ内で混合気が点火され燃焼すると
き、高圧縮比のためガス温度が高く、燃焼速度が早く、
シリンダ内最高圧力が高くなるなめ燃焼にともなう騒音
が大きくなる。
[Problems with the background technology] However, recently, there is a tendency for gasoline engines to be designed with high compression ratios (specifically, 9.0 or higher) in order to improve fuel efficiency. When it burns, the gas temperature is high due to the high compression ratio, and the combustion speed is fast.
The noise associated with slant combustion increases as the maximum pressure inside the cylinder increases.

前述の最適点火時期に点火するよう点火制御装置を設定
することと、圧縮比を大きくすることを併用すれば、出
力増大、燃費向上となるが、特にシリンダ内最高圧力は
大きくなり、燃焼騒音が増加し、特に高速回転時に甚し
く、実用上支障を生じることとなる。
Setting the ignition control device to ignite at the optimal ignition timing mentioned above and increasing the compression ratio will increase output and improve fuel efficiency, but the maximum pressure in the cylinder will increase and combustion noise will increase. This is especially serious at high speed rotation, and causes practical problems.

このrJJBばシリンダブロックにアルミニウム合金を
採用した機関では鉄より弾性係数が低いため騒音が大き
く一層深刻な問題である。
This rJJB engine uses an aluminum alloy for its cylinder block, which has a lower elastic modulus than steel, which makes the problem louder and more serious.

また一般に、進角量が大きい場合はピストン上死点では
既に燃焼がかなり進行して高温となっているためシリン
ダ内最高圧力が高くなり、燃焼騒音が大きくなる。
Generally, when the amount of advance is large, combustion has already progressed considerably at the top dead center of the piston and the temperature has reached a high temperature, so the maximum pressure inside the cylinder increases and combustion noise increases.

進角量の決定は、全負荷特番回転速度における最適点火
時期(最高出力点)をほぼ通るように設定した遠心進角
装置と、市街地走行時に多用する中低速で中低負荷域に
おける最適点火時期をほぼ通るように設定した真空進角
装置とを合算併用して進角が決定されるが、このように
すると高回転で中低負荷の場合高回転、高負圧のため遠
心進角も真空進角も最大となり合算進角量が最大となり
、前述の理由で燃焼騒音が特に大となる。
The amount of advance is determined by a centrifugal advance device that is set to almost pass through the optimum ignition timing (maximum output point) at full load special rotation speed, and by a centrifugal advance device that is set to almost pass through the optimum ignition timing (maximum output point) at full load special rotation speed, and the optimum ignition timing at medium and low load ranges at medium and low speeds that are often used when driving in urban areas. The advance angle is determined by combining the vacuum advance angle device, which is set to almost pass through the The advance angle also becomes maximum, the total advance angle amount becomes maximum, and the combustion noise becomes particularly large for the above-mentioned reason.

このように従来の遠心進角装置と真空進角装置との組合
せによる進角装置では実用燃費向上と騒音低下とは両立
させることができない。
As described above, the conventional advance angle device that is a combination of a centrifugal advance device and a vacuum advance device cannot achieve both practical fuel efficiency improvement and noise reduction.

進角制御に電子制御を導入して進角量を自由に決定でき
るようにすれば、この欠点はある程度解決できるが、現
在のところ電子制御進角装置は複雑であり高価である。
This drawback can be solved to some extent by introducing electronic control into the advance angle control so that the amount of advance angle can be determined freely, but at present, electronically controlled advance angle devices are complicated and expensive.

[発明の目的] そこで、この発明の目的は、燃費、動力性能を犠牲にす
ることなく、実用上特に問題となる高速回転時の燃焼騒
音を低下させようとするものである。
[Object of the Invention] Therefore, an object of the present invention is to reduce combustion noise during high-speed rotation, which is a particular problem in practical use, without sacrificing fuel efficiency or power performance.

[発明の構成] この目的を達成するために、−この発明は、内燃機関の
点火時期制御装置において、遠心進角装置による点火時
期を、全負荷最大出力回転速度において最大出力点から
の出力低下が4%以内となるように最適点火時期から遅
角側に設定し、前記最大出力回転速度より低速回転側で
は前記遅角量を漸次減少させて最適点火時期に一致させ
、前記最大出力回転速度より高速回転側では前記遅角量
を漸次増加(進角量を漸減)させるように設定した遠心
角装置を備えたことを特徴とする。
[Structure of the Invention] In order to achieve this object, the present invention provides an ignition timing control device for an internal combustion engine in which the ignition timing is controlled by a centrifugal advance device to reduce the output from the maximum output point at full load maximum output rotation speed. The ignition timing is set to the retard side from the optimum ignition timing so that The present invention is characterized in that it includes a centrifugal angle device that is set to gradually increase the retard amount (gradually decrease the advance amount) on the higher speed rotation side.

[発明の実施例] 以下図面に基づいて、この発明の詳細な説明する。第1
図は従来の真空進角装置と遠心進角装置を設けた配電器
の進角の分布を機関回転速度と出力(負荷)を横・縦軸
として表わした例である。
[Embodiments of the Invention] The present invention will be described in detail below based on the drawings. 1st
The figure is an example of the advance angle distribution of a power distributor equipped with a conventional vacuum advance angle device and a centrifugal advance angle device, with engine rotational speed and output (load) expressed as horizontal and vertical axes.

この場合、遠心進角については、第2図に示すように機
関を全負荷で運転した場合の各回転速度における最高出
力点を通る線、すなわち第2図の鎖線で示す線、に成る
よう進角量を決定している。
In this case, the centrifugal advance angle should be advanced so that the line passes through the maximum output point at each rotational speed when the engine is operated at full load, as shown in Figure 2, that is, the line shown by the chain line in Figure 2. The amount of angle is determined.

第1図の実線は全負荷出力であり、この線上の進角は第
2図の鎖線で決定する進角とするが、実際の運転状態で
ある部分負荷の場合は真空進角装置が作動して、第1図
に示すようにこれより進角が増加する。
The solid line in Figure 1 is the full load output, and the advance angle on this line is determined by the chain line in Figure 2. However, in the case of partial load, which is the actual operating condition, the vacuum advance angle device operates. As shown in FIG. 1, the advance angle increases from this point.

第1図のBで示す区域は市街地走行時のような中・低速
かつ中・低負荷の区域であり、遠心進角装置はあまり作
動しないが、燃費向上のため真空進角装置を作動させて
適当な進角となるように設定しであるが、第1図へで示
す高速区域では、遠心進角装置も真空進角装置も最大に
作動して大きな進角となり、シリンダ内のガス温度の上
昇のため、燃焼速度が早くなることもあって、前述のと
おり最高圧力が増加するので、燃焼騒音が著しく増加す
る。
The area indicated by B in Figure 1 is an area of medium to low speed and medium to low load, such as when driving in a city, and the centrifugal advance device does not operate much, but the vacuum advance device is activated to improve fuel efficiency. The advance angle is set to an appropriate value, but in the high-speed region shown in Figure 1, both the centrifugal advance device and the vacuum advance device operate to their maximum, resulting in a large advance angle, which causes the gas temperature in the cylinder to drop. Due to the increase in combustion rate, the combustion speed becomes faster, and as mentioned above, the maximum pressure increases, resulting in a significant increase in combustion noise.

この燃焼騒音防止対策として、点火時期を遅らせた場合
を第3図、第4図に示す。第3図の遠心進角特性は従来
と同じとし、真空進角量を変えて、10モ一ド走行燃費
を測定した結果である。最適点火時期(MBT)より点
火時期を遅らせると騒音は低下するが燃費も低下する。
As a measure to prevent this combustion noise, the case where the ignition timing is delayed is shown in FIGS. 3 and 4. The centrifugal advance angle characteristic shown in FIG. 3 is the same as the conventional one, and the fuel efficiency during 10 mode driving was measured by changing the amount of vacuum advance angle. If the ignition timing is delayed from the optimum ignition timing (MBT), noise will be reduced, but fuel efficiency will also be reduced.

第4図は高速回軸持の遠心進角利用を変えた場合の出力
を示す。
Figure 4 shows the output when the use of the centrifugal advance angle of the high-speed rotation shaft is changed.

進角量を小さくすることによってやはり騒音は低下する
が出力も低下することがわかる。第5図は第4図に示し
た各進角の機関回転速度に対する遠心進角特性を示す。
It can be seen that by reducing the advance angle amount, the noise is reduced, but the output is also reduced. FIG. 5 shows the centrifugal advance angle characteristics with respect to the engine rotational speed for each advance angle shown in FIG.

次にこの発明の実施例を第6図乃至第9図に示す。第7
図は遠心進角特性を示す。低速で進角量、増速するに従
って進角は増加し、従来のものは破線で示すように約4
50ORPM以上では進角は一定(30度)となってい
る。この実施例では高速においては実線で示すように、
例えば4500RPMで28度(点1) 、5000P
PMで26度(点2) 、5500PPMで24度(点
3)というように、高速になるに従い進角量を減少させ
ている。
Next, embodiments of the present invention are shown in FIGS. 6 to 9. 7th
The figure shows the centrifugal advance characteristics. The amount of advance angle increases at low speeds, and as the speed increases, the amount of advance angle increases as the speed increases, and in the conventional model, the amount of advance angle is approximately 4 as shown by the broken line.
The advance angle is constant (30 degrees) above 50 ORPM. In this example, at high speed, as shown by the solid line,
For example, 28 degrees at 4500RPM (point 1), 5000P
The amount of advance angle is decreased as the speed increases, such as 26 degrees (point 2) for PM and 24 degrees (point 3) for 5500 PPM.

この遠心進角特性を決定する手順として、第8図に示す
全負荷時の点火時期−出力特性線図において、設計上の
最大出力回転速度(この例では5000PPM)におけ
る出力最高点に対する点火時期(この例では30度であ
り、この点より進角が増加しても減少しても出力は低下
する。)に対して出力低下があまり生じない点火時期ま
で遅らせた点2(この例では30度から4度遅らせて2
6度)を設定する。点火時期を遅らせると前述のように
出力が低下するが、綜合的な評価として、4%以内の出
力低下までは許容できるが、それ以上の出力低下では犠
牲が大き過ぎると判断される。
As a procedure for determining this centrifugal advance characteristic, in the ignition timing-output characteristic diagram at full load shown in Fig. 8, the ignition timing for the maximum output point at the designed maximum output rotation speed (5000 PPM in this example) In this example, the ignition timing is 30 degrees, and regardless of whether the advance angle increases or decreases from this point, the output will decrease.) In contrast to point 2, where the ignition timing is delayed until the ignition timing does not cause much decrease in output (30 degrees in this example). 4 degrees delayed from 2
6 degrees). If the ignition timing is delayed, the output decreases as described above, but as a comprehensive evaluation, it is determined that an output decrease of 4% or less is acceptable, but a greater output decrease would be too much of a sacrifice.

以上のようにして決定した点2 (5000RPMに対
して26度)に連続して低速(この例では45000P
PM)では前記設定点2より進角側に点1 (この例で
は28度)を設定し、高速(この例では5500PPM
)では点2より遅角側に点3 (この例では24度)を
設定する。
Continuously at point 2 determined as above (26 degrees for 5000 RPM), at a low speed (45000 P in this example)
PM), set point 1 (28 degrees in this example) on the advance side of set point 2, and
), set point 3 (24 degrees in this example) on the retard side of point 2.

このようにして決定した遠心進角特性を機関に適用した
場合、出力がどのようになるかを示すものが第6図であ
る。図において、点1は4500PPMにおいて進角2
8度であり、殆ど従来どおりの最高出力点となり、点2
は5000RPMにおいて進角26度で最高出力点の出
力により僅かな出力低下であり、点3は5500PPM
において進角24度でかなり出力が低下している。
FIG. 6 shows what the output will be when the centrifugal advance characteristic determined in this way is applied to the engine. In the figure, point 1 is at 4500 PPM with an advance angle of 2.
8 degrees, which is almost the same maximum output point as before, and point 2
At 5000RPM, the lead angle is 26 degrees, and there is a slight decrease in output due to the output at the highest output point, and point 3 is 5500PPM.
The output drops considerably at an advance angle of 24 degrees.

このように、この発明による実施例では、低速から中速
、高速になるまでは従来と同様に最高出力が得られる最
適点火時期に点火し、かなり高速である最高出力回転速
度では僅かな出力低下をきたす程度に進角を抑え、それ
以上の超高速ではさらに進角を抑え、かなりの出力低下
があるが止むを得ないとするものである。このような超
高速部分は実用上使用する機会は殆どなく、この不利は
後述のような過回転防止のような効果もあり、実用上充
分忍べるものであろう。
As described above, in the embodiment according to the present invention, from low speed to medium speed to high speed, the ignition is performed at the optimum ignition timing that provides the maximum output, as in the conventional case, and at the maximum output rotation speed, which is quite high, the output is slightly reduced. The advance angle is suppressed to such an extent that it causes a lag, and the advance angle is further suppressed at ultra-high speeds beyond that, resulting in a considerable drop in output, but this is unavoidable. Such an ultra-high-speed section has almost no chance of being used in practice, and this disadvantage can be easily tolerated in practice, as it also has effects such as over-speed prevention, which will be described later.

第9図は、この発明による遠心進角装置と従来の真空進
角装置とを組合せた実施例である。第1図と比較すれば
低・中速では従来と変らず、高速・中低負荷区域Aで進
角は例えば第1図では50度から第9図では44度に変
っていることがわかる。
FIG. 9 shows an embodiment in which the centrifugal advance device according to the present invention is combined with a conventional vacuum advance device. Comparing with FIG. 1, it can be seen that at low and medium speeds, there is no difference from the conventional one, but in high speed, medium and low load area A, the advance angle changes from, for example, 50 degrees in FIG. 1 to 44 degrees in FIG.

このように、この発明は実用範囲の燃費・性能を犠牲に
することなく、超高速区域の点火時期の進角を抑え、燃
焼騒音の低下を図ったものである。
In this way, the present invention aims to suppress the advance of the ignition timing in the ultra-high speed region and reduce combustion noise without sacrificing fuel efficiency and performance within the practical range.

この発明による第7図に示ずような遠心進角特性を得る
具体的機構としては、(a)機械式、(b)電気式、(
C)機械式+電気式の3通りが考えられる。
Specific mechanisms for obtaining the centrifugal advance characteristic as shown in FIG. 7 according to the present invention include (a) mechanical type, (b) electric type, (
C) Three types are possible: mechanical type + electric type.

(a)の機械式は最大進角位置に到達する回転数に到達
後それ以上の回転速度で作動するように設定したスプリ
ングを有する遅角ガバナーを使用すれば第7図の特性を
与えることができる。また他の方法として、ウェイトの
ピンが嵌入する窓孔の形状を、高速以上(この例では4
500RPM以上)でウェイトが開くとき遅角となるよ
うに窓孔の形状を形成しておいてもよいことは勿論であ
る。(b)の電気式については配電獄内で機関から得ら
れる点火信号が入力した場合、一定の遅れ時間”t”を
設けることにより、実際の2次側点火電圧を遅らせる様
に設定する。機関のクランク角が移動する時間は回転速
度の増加に逆比例して短くなる。したがって一定の遅れ
時間”t”を設けることにより回転速度が大きくなるほ
ど従来の進角からの遅角量は大きくなる。
The mechanical type (a) can provide the characteristics shown in Figure 7 by using a retard governor with a spring set to operate at a rotation speed higher than the rotation speed that reaches the maximum advance position. can. Another method is to change the shape of the window hole into which the pin of the weight fits to a higher speed (in this example, 4
Of course, the shape of the window hole may be formed so that when the weight opens at a speed of 500 RPM or more, the opening angle is delayed. Regarding the electric type (b), when an ignition signal obtained from the engine is input in the power distribution cell, a certain delay time "t" is provided so that the actual secondary side ignition voltage is delayed. The time it takes for the engine's crank angle to move becomes shorter in inverse proportion to the increase in rotational speed. Therefore, by providing a constant delay time "t", the amount of retardation from the conventional advance angle increases as the rotational speed increases.

(C)の機械式十電気式はCa>、(b)両方式を併用
する方式である。
The mechanical and electrical type (C) is a system that uses both Ca> and (b) types together.

[発明の効果] 以上説明したように、この発明によれば以下のような効
果を得ることができる。
[Effects of the Invention] As explained above, according to the present invention, the following effects can be obtained.

(1)燃費、動力性能を犠牲にすることなく、高速回転
時の点火時期を遅らせることにより、燃焼騒音の低減を
図ることができる。
(1) Combustion noise can be reduced by delaying the ignition timing during high speed rotation without sacrificing fuel efficiency or power performance.

特に、高圧縮比とした場合は一般に燃焼騒音が大きいも
のであるが、この発明による点火時期制御装置によれば
騒音低減の効果が著しい。
In particular, combustion noise is generally large when the compression ratio is high, but the ignition timing control device according to the present invention has a significant noise reduction effect.

また、アルミニウム合金シリンダブロックを使用した機
関でも騒音が大きいが、この発明の装置によれば騒音低
減の効果が著しい。
Further, although engines using aluminum alloy cylinder blocks also produce a lot of noise, the device of the present invention has a remarkable noise reduction effect.

(2)この発明によれば、高速回転においては回転速度
が大となるに従い進角は小となるので実用運転時の過回
転による機関の破壊を防止することができる。
(2) According to the present invention, in high-speed rotation, as the rotation speed increases, the advance angle becomes smaller, so that damage to the engine due to over-speed during practical operation can be prevented.

(3)この発明によれば設計最大出力回転数を明確に設
定できる。
(3) According to the present invention, the design maximum output rotation speed can be clearly set.

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

第1図は従来の遠心、真空併用進角装置の回転速度と出
力(負荷)に対する進角量を示すグラフ、第2図は全負
荷における各回転速度に対する点火時期の変化による出
力の変化とその最大点を示すグラフ、第3図は遠心進角
特性は同一とし、真空進角量を変化させた場合の10モ
ード燃費を測定した結果を示すグラフ、第4図は高速回
転時における遠心進角量を変化させた場合の出力の変化
を示すグラフ、第5図は第4図の場合の遠心進角特性を
示すグラフ、第6図は高速回転時における機関回転速度
に対する全負荷最大出力を遠心進角をパラメータとして
表したグラフ、第7図はこの発明による遠心進角特性(
実線)と従来の特性(点線)を示すグラフ、第8図は回
転速度をパラメータとして点火時期に対する最大出力を
表したグラフ、第9図はこの発明による遠心進角装置と
従来と同様な真空進角装置を設けた内燃機関の回転速度
と出力(負荷)に対する進角の分布を示すグラフである
。 第6図 回転&(RPM)− 第8図 7弘火吟M (BTDC) − 第7図 rj:J転数(PPM) − 第9図 □(RPM)−
Figure 1 is a graph showing the amount of advance with respect to rotational speed and output (load) of a conventional centrifugal/vacuum combination advance device. Figure 2 is a graph showing the change in output due to changes in ignition timing for each rotational speed at full load, and its A graph showing the maximum point, Figure 3 is a graph showing the results of measuring 10 mode fuel efficiency when the vacuum advance angle amount is changed with the same centrifugal advance angle characteristics, and Figure 4 is a graph showing the centrifugal advance angle at high speed rotation. Figure 5 is a graph showing the centrifugal advance characteristics in the case of Figure 4. Figure 6 is a graph showing the change in output when the amount is changed. Figure 6 is a graph showing the centrifugal advance angle characteristics in the case of Figure 4. A graph showing the advance angle as a parameter, Figure 7 shows the centrifugal advance angle characteristics (
Figure 8 is a graph showing the maximum output versus ignition timing using rotational speed as a parameter. Figure 9 is a graph showing the characteristics of the centrifugal advance device according to the present invention and the conventional vacuum advance device. 2 is a graph showing the distribution of advance angle with respect to rotational speed and output (load) of an internal combustion engine provided with an angle device. Fig. 6 Rotation & (RPM) - Fig. 8 7 Kokagin M (BTDC) - Fig. 7 rj: J rotation (PPM) - Fig. 9 □ (RPM) -

Claims (1)

【特許請求の範囲】 1、内燃機関の点火時期制御装置において、遠心進角装
置による点火時期を、全負荷最大出力回転速度において
は最大出力からの出力低下が4%以内となるように最適
点火時期から遅角側に設定し、前記最大出力回転速度よ
り低速回転側では前記遅角量を漸減させて最適点火時期
に一致させ、前記最大出力回転速度より高速回転側では
前記遅角量を漸増(進角量を漸減)させるように設定し
た遠心進角装置を備えたことを特徴とする内燃機関の点
火時期制御装置。 2、内燃機関の圧縮比が9.0以上である特許請求の範
囲第1項記載の点火時期制御装置。 3、内燃機関のシリンダブロックがアルミニウム合金製
である特許請求の範囲第1項記載の点火時期制御装置。
[Scope of Claims] 1. In an ignition timing control device for an internal combustion engine, the ignition timing by a centrifugal advance device is optimized so that the output decrease from the maximum output is within 4% at full load maximum output rotation speed. The ignition timing is set to the retard side from the timing, and the retard amount is gradually decreased to match the optimum ignition timing when the rotation speed is lower than the maximum output rotation speed, and the retard amount is gradually increased when the rotation speed is higher than the maximum output rotation speed. An ignition timing control device for an internal combustion engine, comprising a centrifugal advance device configured to gradually decrease the advance amount. 2. The ignition timing control device according to claim 1, wherein the compression ratio of the internal combustion engine is 9.0 or more. 3. The ignition timing control device according to claim 1, wherein the cylinder block of the internal combustion engine is made of an aluminum alloy.
JP15160283A 1983-08-22 1983-08-22 Ignition timing controller for internal-combustion engine Granted JPS6045779A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15160283A JPS6045779A (en) 1983-08-22 1983-08-22 Ignition timing controller for internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15160283A JPS6045779A (en) 1983-08-22 1983-08-22 Ignition timing controller for internal-combustion engine

Publications (2)

Publication Number Publication Date
JPS6045779A true JPS6045779A (en) 1985-03-12
JPS6252137B2 JPS6252137B2 (en) 1987-11-04

Family

ID=15522113

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15160283A Granted JPS6045779A (en) 1983-08-22 1983-08-22 Ignition timing controller for internal-combustion engine

Country Status (1)

Country Link
JP (1) JPS6045779A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03256848A (en) * 1990-03-06 1991-11-15 Minoru Suematsu Bulky article vacuum receiving bag
JPH06227551A (en) * 1991-04-15 1994-08-16 Nippon Seiki Kk Air drawing device

Also Published As

Publication number Publication date
JPS6252137B2 (en) 1987-11-04

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