JPS5843584B2 - Ignition timing control device - Google Patents

Ignition timing control device

Info

Publication number
JPS5843584B2
JPS5843584B2 JP54012793A JP1279379A JPS5843584B2 JP S5843584 B2 JPS5843584 B2 JP S5843584B2 JP 54012793 A JP54012793 A JP 54012793A JP 1279379 A JP1279379 A JP 1279379A JP S5843584 B2 JPS5843584 B2 JP S5843584B2
Authority
JP
Japan
Prior art keywords
ignition timing
difference
ignition
limit
value
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
Application number
JP54012793A
Other languages
Japanese (ja)
Other versions
JPS55107070A (en
Inventor
憲二 池浦
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP54012793A priority Critical patent/JPS5843584B2/en
Publication of JPS55107070A publication Critical patent/JPS55107070A/en
Publication of JPS5843584B2 publication Critical patent/JPS5843584B2/en
Expired legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P5/00Advancing or retarding ignition; Control therefor
    • F02P5/04Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions
    • F02P5/145Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using electrical means
    • F02P5/15Digital data processing
    • F02P5/1502Digital data processing using one central computing unit
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/40Engine management systems

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  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Signal Processing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Electrical Control Of Ignition Timing (AREA)

Description

【発明の詳細な説明】 本発明は内燃機関の点火時期制御装置に関し、特に運転
状態急変時の運転性、安定性を向上させた点火時期制御
装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an ignition timing control device for an internal combustion engine, and more particularly to an ignition timing control device that improves drivability and stability during sudden changes in operating conditions.

最近、マイクロコンピュータ等の演算装置を用い、機関
の回転速度や負荷等の機関運転変数に基づいて点火時期
(進角値又は遅角値)を算出する電子式点火時期制御装
置が開発されている。
Recently, electronic ignition timing control devices have been developed that use arithmetic devices such as microcomputers to calculate ignition timing (advanced or retarded) based on engine operating variables such as engine speed and load. .

上記の電子式点火時期制御装置は、従来の遠心進角装置
や真空進角装置のごとき機械式進角装置に比して、点火
時期の制御巾を大きくすることが出来、また機関の運転
状態に最も適した点火時期を容易に設定することが出来
るという特徴がある。
The above-mentioned electronic ignition timing control device can widen the control range of the ignition timing compared to conventional mechanical advance devices such as centrifugal advance devices and vacuum advance devices. It is characterized by the ability to easily set the most suitable ignition timing.

しかし電子式点火時期制御装置においては、点火時期を
機関運転状態から演算によって算出するため、運転状態
が変化したとき点火時期が不連続に急変することがある
However, in the electronic ignition timing control device, the ignition timing is calculated based on the engine operating state, so when the operating state changes, the ignition timing may suddenly change discontinuously.

特に、運転状態をいくつかの種類に分け、各種類ごとに
点火時期を記憶したテーブルをもち、運転状態に応じて
それらのテーブルから点火時期を読み出す方式、例えば
(リフクランキング中は温度テーブルによって冷却水温
に対応して点火時期を設定、(2)アイドルスイッチが
オンのときには回転速度に応じて点火時期を設定、(3
)通常運転時は回転速度と負荷(吸入負圧、吸入空気流
量又は噴射パルス巾から検出)とに対応してテーブルに
記憶されている値を読み出して点火時期を設定、という
方式においては、上記の(す、 (2) 、 (3)の
状態が切換わるときに該当するテーブルも切換わるため
点火時期が不連続に急変するおそれがある。
In particular, there is a method that divides operating conditions into several types, has a table that stores the ignition timing for each type, and reads out the ignition timing from those tables according to the operating condition. Set the ignition timing according to the cooling water temperature, (2) set the ignition timing according to the rotation speed when the idle switch is on, (3)
) During normal operation, the ignition timing is set by reading values stored in a table corresponding to the rotation speed and load (detected from suction negative pressure, intake air flow rate, or injection pulse width). When the states of (2) and (3) change, the corresponding table also changes, so there is a risk that the ignition timing may suddenly change discontinuously.

点火時期が急変すると、機関の発生トルクが急変するの
で運転性が悪化し、またドウエル角が不安定になるため
点火コイルへの通電時間が長すぎたり短かすぎたりして
、例えば長すぎるとパワートランジスタが破損したり、
短かすぎると点火エネルギーが不足し、甚しい場合には
失火やバツクファイヤを生ずるおそれもある。
If the ignition timing suddenly changes, the torque generated by the engine will change suddenly, resulting in poor drivability, and the dwell angle will become unstable, causing the ignition coil to be energized for too long or too short. The power transistor is damaged or
If it is too short, ignition energy will be insufficient, and in severe cases, there is a risk of misfire or backfire.

本発明は上記の問題に鑑みてなされたものであり、直前
回(以下単に前回と記す)の点火の際に使用された点火
時期を記憶しておき、今回の算出値と比較し、その差が
所定の運転変数に応じて変化する制限範囲外である場合
は、差が制限範囲内になるように制限した値を点火時期
とすることによって、点火時期の急変を防止すると共に
、安定性を損なわない範囲で出来るだけ速やかに点火時
期を変化させるようにすることにより、機関の運転性と
安定性を向上させた点火時期制御装置を提供することを
目的とする。
The present invention has been made in view of the above problem, and it stores the ignition timing used in the previous ignition (hereinafter simply referred to as the previous time), compares it with the current calculated value, and calculates the difference. If the difference is outside the limit range that varies according to predetermined operating variables, the ignition timing is set to a value that is limited so that the difference is within the limit range, thereby preventing sudden changes in the ignition timing and improving stability. An object of the present invention is to provide an ignition timing control device that improves the drivability and stability of an engine by changing the ignition timing as quickly as possible without impairing the ignition timing.

以下図面に基づいて本発明の詳細な説明する。The present invention will be described in detail below based on the drawings.

第5図は本発明の全体の構成を示す図である。FIG. 5 is a diagram showing the overall configuration of the present invention.

第5図において、30は回転速度、負荷等の機関の各種
運転変数を検出するセンサ群であり、例えば後記第1図
の7〜12に相当する。
In FIG. 5, numeral 30 is a sensor group for detecting various operating variables of the engine, such as rotational speed and load, and corresponds to, for example, 7 to 12 in FIG. 1, which will be described later.

31は上記のセンサ群の出力に応じて機関の運転状態に
適合した点火時期を演算する演算手段である。
Reference numeral 31 denotes calculation means for calculating the ignition timing suitable for the operating condition of the engine in accordance with the outputs of the above-mentioned sensor group.

なお演算手段31は、機関回転に同期するか又は一定時
間毎に周期的に点火時期を算出する。
Note that the calculation means 31 calculates the ignition timing in synchronization with the engine rotation or periodically at fixed time intervals.

また32は、回転速度、負荷、機関温度及びバッテリ電
圧のうちの少なくとも一つの運転変数を検出する検出手
段である。
Further, 32 is a detection means for detecting at least one operating variable among rotational speed, load, engine temperature, and battery voltage.

なおこの検出手段32は、検出すべき運転変数がセンサ
群30と共通のときは、センサ群30の出力を共用する
ことによって省略することが出来る。
Note that this detection means 32 can be omitted by sharing the output of the sensor group 30 when the operating variable to be detected is common to the sensor group 30.

また33は、検出手段32で検出した運転変数に応じて
制限範囲を算出する制限範囲算出手段である。
Reference numeral 33 denotes a limit range calculation means for calculating a limit range according to the operating variables detected by the detection means 32.

上記の制限範囲は、前回の点火時期と今回の点火時期と
の差の許容巾を定めるものであり、前回より今回が進角
する場合の限度を上限、遅角する場合の限度を下限とす
る。
The above limit range defines the allowable range for the difference between the previous ignition timing and the current ignition timing, with the upper limit being the limit when the current ignition timing is advanced compared to the previous time, and the lower limit being the limit when the current ignition timing is retarded. .

また記憶手段34は、前回の点火の際に使用された点火
時期を記憶して出力する。
Furthermore, the storage means 34 stores and outputs the ignition timing used during the previous ignition.

また差算出手段35は、記憶手段34から与えられる前
回の点火時期と、演算手段31で算出された今回の点火
時期との差を算出する。
Further, the difference calculation means 35 calculates the difference between the previous ignition timing given from the storage means 34 and the current ignition timing calculated by the calculation means 31.

次に制限手段36は、差算出手段35で算出した差が、
制限範囲算出手段33で算出した制限範囲内の場合は今
回の算出値をそのまま点火時期として出力し、また上記
の差が制限範囲の上限以上(進角側で制限以上)のとき
は差が上限になるように、下限以下(遅角側で制限以上
)の場合は差が下限になるように今回の算出値を制限し
た値を点火時期として出力する。
Next, the limiting means 36 determines that the difference calculated by the difference calculating means 35 is
If it is within the limit range calculated by the limit range calculation means 33, the current calculated value is output as is as the ignition timing, and if the above difference is greater than the upper limit of the limit range (more than the limit on the advance side), the difference is the upper limit. If the difference is below the lower limit (more than the limit on the retard side), a value obtained by limiting the current calculated value so that the difference becomes the lower limit is output as the ignition timing.

次に制御手段37は、制限手段36から与えられた点火
時期になったとき点火信号を出力し、それによって点火
装置38(後記第1図の13〜20に相当)が動作して
点火が行なわれる。
Next, the control means 37 outputs an ignition signal when the ignition timing given by the restriction means 36 is reached, whereby the ignition device 38 (corresponding to 13 to 20 in FIG. 1 described later) is operated to perform ignition. It will be done.

なお第5図において、30,31,37及び38の部分
は従来装置と同様であり、32〜36が本発明の特徴部
分である。
In FIG. 5, portions 30, 31, 37, and 38 are the same as those of the conventional device, and portions 32 to 36 are characteristic portions of the present invention.

次に実施例に基づいて本発明を説明する。Next, the present invention will be explained based on examples.

第1図は本発明の一実施例のブロック図である。FIG. 1 is a block diagram of one embodiment of the present invention.

第1図において、1は演算部であり、例えばマイクロコ
ンピュータで構成する。
In FIG. 1, numeral 1 denotes an arithmetic unit, which is composed of, for example, a microcomputer.

また7は機関回転速度に対応した信号s8を出力する回
転センサ、8は機関の吸入負圧に対応した信号S2を出
力する負圧センサ、9は機関冷却水温に対応した信号S
3を出力する温度センサ、10は機関のアイドリング状
態を検出してアイドル信号S4を出力するアイドルスイ
ッチである。
Further, 7 is a rotation sensor that outputs a signal s8 corresponding to the engine rotation speed, 8 is a negative pressure sensor that outputs a signal S2 that corresponds to the engine suction negative pressure, and 9 is a signal S that corresponds to the engine cooling water temperature.
10 is an idle switch that detects the idling state of the engine and outputs an idle signal S4.

また11はクランク角の基準角度(例えば120’)ご
とに基準角パルスS、を出力する基準角センサ、12は
クランク角の単位角度(例えば1°)ごとに単位角パル
スS6を出力する単位角センサである。
Reference numeral 11 is a reference angle sensor that outputs a reference angle pulse S for each reference angle of the crank angle (for example, 120'), and 12 is a unit angle sensor that outputs a unit angle pulse S6 for each unit angle of the crank angle (for example, 1°). It is a sensor.

演算部1において、演算装置2は、上記の各センサ7〜
10の各信号(必要に応じてこれ以外にも噴射パルス信
号、変速機の変速位置信号、車速信号等を用いてもよい
)を入力し、機関運転状態に対応した点火時期を演算に
よって算出するか、又は各運転状態の種類ごとに分けら
れて予め点火時期を記憶しているテーブル3〜5(例え
ばテーブル3は温度テーブル、テーブル4は回転速度テ
ーブル、テーブル5は回転速度及び負荷に対応したテー
ブル)から、そのときの運転状態に対応した値を読み出
すことにより、点火時期の基本値を設定する。
In the arithmetic section 1, the arithmetic device 2 includes each of the above-mentioned sensors 7 to
Each of the 10 signals (in addition to these, an injection pulse signal, a transmission shift position signal, a vehicle speed signal, etc. may be used as necessary) is input, and the ignition timing corresponding to the engine operating state is calculated by calculation. Alternatively, tables 3 to 5 store ignition timing in advance and are divided according to the type of each operating state (for example, table 3 is a temperature table, table 4 is a rotation speed table, and table 5 is a table corresponding to rotation speed and load). The basic value of the ignition timing is set by reading out the value corresponding to the operating state at that time from the table).

次に、メモリ6に記憶されている前回の点火の際に使用
された点火時期と今回の基本値とを比較し、前回の値と
今回の基本値との差が規定の制限範囲内であれば、上記
の基本値をそのまま今回の点火時期とし、また上記の差
が制限範囲外である場合には、制限範囲に限定した値を
今回の点火時期として決定する。
Next, the ignition timing used in the previous ignition stored in the memory 6 is compared with the current basic value, and if the difference between the previous value and the current basic value is within the specified limit range. For example, the above basic value is used as the current ignition timing, and if the above difference is outside the limited range, a value limited to the limited range is determined as the current ignition timing.

そして基準角センサ11から基準角パルスS5が与えら
れた時点から、上記の決定された点火時期に対応した数
だけ単位角センサ12の単位角パルスS6が与えられた
時点に点火信号S7を出力する。
Then, from the time when the reference angle pulse S5 is given from the reference angle sensor 11, the ignition signal S7 is outputted at the time when the unit angle pulse S6 of the unit angle sensor 12 is given as many as the number corresponding to the determined ignition timing. .

この点火信号S7によって点火コイル13の一次回路を
断続し、発生した高圧電流を配電器14を介して点火プ
ラグ15〜20へ送る。
This ignition signal S7 interrupts the primary circuit of the ignition coil 13, and sends the generated high voltage current to the spark plugs 15 to 20 via the power distributor 14.

次に、第2図は本発明の演算過程を示すフローチャート
であり、毎回の点火の毎に点火時期を算出する場合を示
す。
Next, FIG. 2 is a flowchart showing the calculation process of the present invention, and shows the case where the ignition timing is calculated for each ignition.

まず、P□において前記の各信号S□〜S4に基づいて
点火時期を計算(計算値FADV)する。
First, at P□, the ignition timing is calculated (calculated value FADV) based on the above-mentioned signals S□ to S4.

次にP2において、制限範囲すなわち前記と今回の点火
時期の差の許容巾の上限値Lu (前回より今回の方が
進角する場合の限度)と下限値L/(前回より今回の方
が遅角する場合の限度)とを算出する。
Next, in P2, the limit range, that is, the upper limit value Lu (limit when the current ignition timing is more advanced than the previous one) of the allowable range of the difference between the above and the current ignition timing, and the lower limit value L/(the limit when the current ignition timing is slower than the previous one) (limit when angular) is calculated.

この上限値Lu及び下限値Llの値は、回転速度、負荷
、機関温度、バッテリ電圧等の機関運転変数に応じて運
転性や安定性を損なわない範囲の値に設定する。
The upper limit value Lu and lower limit value Ll are set within a range that does not impair driveability or stability, depending on engine operating variables such as rotational speed, load, engine temperature, and battery voltage.

(Lu及びLlの設定方法については詳細後述)。(Details on how to set Lu and Ll will be described later).

次にP3において、計算値FADVと前回の言醇値PA
DVとの差X(X=FADV−PADV)を求め、差X
が制限範囲内(L/<X<Lu)にある場合はそのまま
P6へ、差Xが上限値以上(Lu≦X)の場合にはP、
へ、差Xが下限値以下(X≦−L7)の場合にはP4へ
、それぞれ送る。
Next, in P3, the calculated value FADV and the previous pronunciation value PA
Find the difference X (X = FADV - PADV) with DV, and calculate the difference X
If is within the limit range (L/<X<Lu), go directly to P6, if the difference X is greater than the upper limit (Lu≦X), go to P6,
and, if the difference X is less than the lower limit (X≦−L7), the data is sent to P4.

P、においては、前回の値PADVに上限値Luを加え
た値を今回の値FADVとしてP6へ送り、またP4に
おいては、前回の値PADVから下限値Llを減じた値
をP6へ送る。
In P, the value obtained by adding the upper limit value Lu to the previous value PADV is sent to P6 as the current value FADV, and in P4, the value obtained by subtracting the lower limit value Ll from the previous value PADV is sent to P6.

次にP6において、今回の値FADVを前回の値PAD
Vと書き換えて記憶し、P7においてFADVを点火時
期として出力する。
Next, in P6, the current value FADV is converted to the previous value PAD.
It is rewritten as V and stored, and FADV is outputted as the ignition timing at P7.

上記の5TARTからENDまでの演算は、機関回転に
同期して毎回の点火毎(4サイクル6気筒機関の場合は
クランク角120°毎)に繰返し行なう。
The calculations from 5TART to END described above are repeated for each ignition (every 120 degrees of crank angle in the case of a 4-cycle, 6-cylinder engine) in synchronization with the engine rotation.

次に、第3図は本発明の他の演算過程を示すフローチャ
ートであり、点火時期の計算を機関回転に同期せずに(
例えば一定周期で)行なう場合を示す。
Next, FIG. 3 is a flowchart showing another calculation process of the present invention, in which the ignition timing calculation is not synchronized with the engine rotation (
For example, this example shows a case where the process is performed at a fixed period.

第3図のフローチャートは、第2図のフローチャートか
ら書き換え過程のP6を除いたものであり、書き換え過
程は別系統のP8によって回転と同期して行なう。
The flowchart of FIG. 3 is the flowchart of FIG. 2 with P6 of the rewriting process removed, and the rewriting process is performed in synchronization with the rotation by P8 of a separate system.

すなわち第3図においては、点火時期の計算は回転と同
期せずに、例えば一定周期のクロック信号に同期して行
なうが、前回の値と今回の値との書き換えのみは回転に
同期して点火時期毎(例えば120°毎)に行なうよう
に構成している。
In other words, in Fig. 3, the ignition timing is calculated not in synchronization with the rotation, but in synchronization with, for example, a clock signal of a constant cycle, but only the rewriting of the previous value and the current value is performed in synchronization with the rotation. The configuration is such that it is performed every period (for example, every 120 degrees).

次に、上限値Lu及び下限値Llについて説明する。Next, the upper limit value Lu and the lower limit value Ll will be explained.

第4図は基準角信号Aと点火コイルの一次電流Bとの関
係図であり、上死点TDCの60°前に基準角信号M、
、 M2. M3・・・・・・が出力され、その時点
で今回の点火と次回の通電とをセットする場合を例示す
る。
Fig. 4 is a diagram showing the relationship between the reference angle signal A and the primary current B of the ignition coil.
, M2. A case will be exemplified in which the current ignition and the next energization are set at that point when M3... is output.

まず第4図イは、正常動作の例であり、点火進角がBT
DC40’ (上死点前40°)、ドウエル角(通電角
)が40°で一定の場合を示す。
First, Fig. 4A is an example of normal operation, and the ignition advance angle is BT.
The case where DC40' (40° before top dead center) and dwell angle (energization angle) are constant at 40° are shown.

第4図イから判るように、基準角信号M0がbえられた
時点で今回の点火時期Tnと次回の通電時期TN2(M
2の20°前)とをセットする。
As can be seen from Fig. 4A, when the reference angle signal M0 is obtained, the current ignition timing Tn and the next energization timing TN2 (M
20° before 2).

次に第4図口は、点火進角が急変したため通電が不可能
になる場合の例であり、点火進角BTDC1O°、ドウ
エル角20°の状態から点火進角BTDC40°、ドウ
エル角30°の状態に急変する場合を示す。
Next, Figure 4 shows an example where energization becomes impossible due to a sudden change in the ignition advance angle. Indicates a sudden change in condition.

この場合には、基準角信号M3が与えられた時点で今回
の点火時期TF3と次回の通電時期TN4とをセットし
、基準角信号風が与えられた時点で次回の点火時期TF
4と次々回の通電時期TN。
In this case, the current ignition timing TF3 and the next energization timing TN4 are set when the reference angle signal M3 is given, and the next ignition timing TF is set when the reference angle signal M3 is given.
4 and the next energization timing TN.

をセットするが、基準角信号風から点火進角及びドウエ
ル角が急変するので、次回の通電時期TN4より次回の
点火時期TF4の方が先になづてしまい、点火が不可能
になる。
However, since the ignition advance angle and dwell angle suddenly change from the reference angle signal wind, the next ignition timing TF4 will be earlier than the next energization timing TN4, making ignition impossible.

したがって点火時期の変化範囲の上限(紅u及び下限値
L/を一定値に設定する場合には、少なくとも上記のご
とき点火不能を生じない範囲、すなわち通電時期が点火
時期より必ず早くなる範囲に設定すれば良い。
Therefore, when setting the upper limit (red u) and lower limit L/ of the ignition timing change range to a constant value, set it at least within a range that does not cause ignition failure as described above, that is, a range where the energization timing is always earlier than the ignition timing. Just do it.

次に、上限値Lu及び下限値Lllを運転変数に応じて
変化させる場合を説明する。
Next, a case will be described in which the upper limit value Lu and the lower limit value Lll are changed in accordance with the operating variables.

点火コイルの通電時間は要求点火エネルギーによって変
化する。
The energization time of the ignition coil varies depending on the required ignition energy.

すなわち、アイドリング時のように燃焼が不安定なため
に要求エネルギーが大きな領域では、通電時間を長くす
る必要がある。
That is, in a region where the required energy is large due to unstable combustion, such as during idling, it is necessary to lengthen the energization time.

しかし回転速度が低いので、通電時間としては長くても
ドウエル角としては小さな値になる。
However, since the rotational speed is low, even if the energization time is long, the dwell angle will be a small value.

したがってこの様な条件で点火進角が大きく変化すると
、通電時間の変化が大きく、そのため失火するおそれが
大きくなる。
Therefore, if the ignition advance angle changes significantly under such conditions, the energization time will change greatly, which increases the risk of misfire.

一方、回転速度が大きい場合は、ドウエル角は犬でも通
電時間としては短くなる。
On the other hand, when the rotational speed is high, the dwell angle becomes short as the current application time even for dogs.

したがって点火進角がかなり変化しても、ドウエル角が
元来太きいため、通電時間の変化としては小さくなる。
Therefore, even if the ignition advance angle changes considerably, the dwell angle is originally large, so the change in the energization time will be small.

上記のように、点火進角の変化中は、ドウエル角と密接
な関係をもち、また要求されるドウエル角は各運転変数
に応じて定まるので、点火進角の変化の許容巾すなわち
制限範囲を運転変数に応じて定めれば、失火するおそれ
なしに最も速やかに点火進角を変化させることが出来る
As mentioned above, while the ignition advance angle is changing, there is a close relationship with the dwell angle, and the required dwell angle is determined according to each operating variable. If it is determined according to the operating variables, the ignition advance angle can be changed most quickly without fear of misfire.

なおドウエル角に影響を及ぼすのは、主として回転速度
、負荷、機関温度及びバッテリ電圧であるから、これら
の運転変数に基づいて制限範囲の上限11 L u、下
限値Llを設定してやれば、効率良く点火進角の制御を
行なうことが出来る。
Note that the dwell angle is mainly influenced by the rotational speed, load, engine temperature, and battery voltage, so if the upper limit L and lower limit of the limit range are set based on these operating variables, the dwell angle can be efficiently It is possible to control the ignition advance angle.

なお上記の説明から判るように点火進角の変化の制限に
ついて述べたことは、そのままドウエル角の変化につい
ても適用出来ることは明らかである。
As can be seen from the above explanation, it is clear that what has been said regarding the restriction on changes in the ignition advance angle can also be applied to changes in the dwell angle.

以上説明したごとく本発明によれば、運転状態が変化し
たときに点火時期が不連続に急変するおそれがなくなり
、そのため発生トルクの変化が滑らかになるので運転性
、安定性が向上し、またドウエル角が不安定になること
もないので失火を生ずるおそれもなく、しかも失火する
おそれなしに最も速やかに点火時期を変化させることが
出来るという効果がある。
As explained above, according to the present invention, there is no fear that the ignition timing will suddenly change discontinuously when the operating condition changes, and therefore the change in generated torque becomes smooth, improving drivability and stability. Since the angle does not become unstable, there is no risk of misfire, and the ignition timing can be changed most quickly without the risk of misfire.

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

第1図は本発明の一実施例のブロック図、第2図及び第
3図は本発明の演算過程を示すフローチャート、第4図
は基準角信号と点火コイルの一次電流との関係図、第5
図は本発明の全体の構成を示す図である。 符号の説明、1・・・・・・演算部、2・・・・・・演
算装置、3〜5・・・・・・テーブル、6・・・・・・
メモリ、7・・・・・・回転センサ、8・・・・・・負
圧センサ、9・・・・・・温度センサ、10・・・・・
・アイドルスイッチ、11・・・・・・基準角センサ、
12・・・・・・単位角センサ、13・・・・・・点火
コイル、14・・・・・・配電器、15〜20・・・・
・・点火プラグ。
FIG. 1 is a block diagram of an embodiment of the present invention, FIGS. 2 and 3 are flowcharts showing the calculation process of the present invention, FIG. 4 is a relationship diagram between the reference angle signal and the primary current of the ignition coil, and FIG. 5
The figure is a diagram showing the overall configuration of the present invention. Explanation of symbols, 1... Arithmetic unit, 2... Arithmetic device, 3 to 5... Table, 6...
Memory, 7...Rotation sensor, 8...Negative pressure sensor, 9...Temperature sensor, 10...
・Idle switch, 11...Reference angle sensor,
12...Unit angle sensor, 13...Ignition coil, 14...Distributor, 15-20...
...Spark plug.

Claims (1)

【特許請求の範囲】[Claims] 1 機関の各種運転変数に基づき機関回転に同期して又
は一定時間毎に周期的に点火時期を算出する電子式点火
時期制御装置において、直前回の点火の際に使用された
点火時期を記憶する記憶手段と、上記の直前回の点火時
期と今回算出された点火時期との差を算出する差算出手
段と、回転速度、負荷、機関温度及びバッテリ電圧のう
ちの少なくとも一つの運転変数を検出する検出手段と、
該検出手段で検出した運転変数に応じた制限範囲を算出
する制限範囲算出手段と、上記の差が上記制限範囲内で
ある場合は今回の算出値をそのまま点火時期とし、また
上記の差が制限範囲の上限以上のときは差が上限になる
ように、下限以下の場合は差が下限になるように制限し
た値を点火時期として出力する制限手段とを具備し、直
前回の点火時期と今回の点火時期との差を、上記検出手
段で検出した運転変数に応じて変化する制限範囲内に制
限したことを特徴とする点火時期制御装置。
1. In an electronic ignition timing control device that calculates ignition timing in synchronization with engine rotation or periodically at regular intervals based on various operating variables of the engine, the ignition timing used in the previous ignition is memorized. a storage means, a difference calculation means for calculating the difference between the previous ignition timing and the currently calculated ignition timing, and detecting at least one operating variable among rotational speed, load, engine temperature, and battery voltage. detection means;
A limit range calculation means that calculates a limit range according to the operating variable detected by the detection means, and if the above difference is within the above limit range, the current calculated value is used as the ignition timing, and the above difference is the limit range. It is equipped with a limiting means that outputs a limited value as the ignition timing so that the difference becomes the upper limit when it is above the upper limit of the range, and so that the difference becomes the lower limit when it is below the lower limit. An ignition timing control device characterized in that the difference between the ignition timing and the ignition timing of the ignition timing is limited to within a limit range that varies depending on the operating variable detected by the detection means.
JP54012793A 1979-02-08 1979-02-08 Ignition timing control device Expired JPS5843584B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP54012793A JPS5843584B2 (en) 1979-02-08 1979-02-08 Ignition timing control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP54012793A JPS5843584B2 (en) 1979-02-08 1979-02-08 Ignition timing control device

Publications (2)

Publication Number Publication Date
JPS55107070A JPS55107070A (en) 1980-08-16
JPS5843584B2 true JPS5843584B2 (en) 1983-09-28

Family

ID=11815265

Family Applications (1)

Application Number Title Priority Date Filing Date
JP54012793A Expired JPS5843584B2 (en) 1979-02-08 1979-02-08 Ignition timing control device

Country Status (1)

Country Link
JP (1) JPS5843584B2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58210366A (en) * 1982-05-31 1983-12-07 Toyota Motor Corp Spark advance control device in gasoline engine
JPS5929750A (en) * 1982-08-12 1984-02-17 Toyota Motor Corp Method of torque variation control in internal combustion engine
JPH0646025B2 (en) * 1982-12-24 1994-06-15 トヨタ自動車株式会社 Knotting control method for internal combustion engine
JP5675466B2 (en) * 2011-03-31 2015-02-25 三菱重工業株式会社 Pilot injection timing control method and apparatus when engine combustion diagnosis signal is abnormal

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5090826A (en) * 1973-12-12 1975-07-21
JPS51110139A (en) * 1975-02-06 1976-09-29 Bosch Gmbh Robert

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5090826A (en) * 1973-12-12 1975-07-21
JPS51110139A (en) * 1975-02-06 1976-09-29 Bosch Gmbh Robert

Also Published As

Publication number Publication date
JPS55107070A (en) 1980-08-16

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