JPH02112646A - Misfire detector for multicylinder internal combustion engine - Google Patents
Misfire detector for multicylinder internal combustion engineInfo
- Publication number
- JPH02112646A JPH02112646A JP26497888A JP26497888A JPH02112646A JP H02112646 A JPH02112646 A JP H02112646A JP 26497888 A JP26497888 A JP 26497888A JP 26497888 A JP26497888 A JP 26497888A JP H02112646 A JPH02112646 A JP H02112646A
- Authority
- JP
- Japan
- Prior art keywords
- cylinder
- detected
- internal combustion
- combustion engine
- detecting
- 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
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 21
- 230000002159 abnormal effect Effects 0.000 claims abstract description 14
- 238000001514 detection method Methods 0.000 claims description 12
- 238000000034 method Methods 0.000 description 14
- 230000005856 abnormality Effects 0.000 description 12
- 238000010586 diagram Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 239000000498 cooling water Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 description 2
- 238000004880 explosion Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Landscapes
- Combined Controls Of Internal Combustion Engines (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は多気筒内燃機関において、正常に点火が行われ
ない(失火)気筒を自動的に検出する多〔従来の技術〕
従来のこの種のものとしては、多気筒内燃機関の1回転
につき複数の角度位置を検出する単位信号発生手段によ
り検出した角度位置間隔から各角度位置間における瞬時
回転数を検出し、そのうちから各気筒の最小値と最大値
との少なくとも一方を判別して、それらの各気筒間の変
動分から失火気筒を検出するものが知られている(例え
ば、特開昭61−258955号公報、特開昭62−1
180.31号公報)。[Detailed Description of the Invention] [Field of Industrial Application] The present invention is a multi-cylinder internal combustion engine that automatically detects a cylinder in which ignition does not occur normally (misfire). In this method, the instantaneous rotational speed between each angular position is detected from the angular position interval detected by a unit signal generating means that detects multiple angular positions per rotation of a multi-cylinder internal combustion engine, and the minimum value of each cylinder is determined from among the angular position intervals. It is known that a misfiring cylinder is detected by determining at least one of the maximum value and the maximum value, and detecting a misfiring cylinder based on the variation between each cylinder.
180.31).
ところが、上述した従来のものでは、各気筒の瞬時回転
数の最小値と最大値との少なくとも一方を判別するため
に、各角度位置間で絶えず瞬時回転数の変動分を演算し
なければならないので、演算負荷が大きくなり、実用的
でないという問題がある。However, in the conventional system described above, in order to determine at least one of the minimum and maximum values of the instantaneous rotational speed of each cylinder, it is necessary to constantly calculate the variation in the instantaneous rotational speed between each angular position. , there is a problem that the calculation load becomes large and it is not practical.
また、演算負荷を低減するために、各気筒の上死点間の
角度間隔から各気筒の平均回転数を検出し、この平均回
転数の変化分より異常気筒を検出することも考えられる
が、各気筒の上死点間の幅の広い角度間隔の平均回転数
を検出することになるので、失火した気筒と失火しない
気筒との回転数の変動分が少なくなり、正確に失火気筒
を判別することができないという問題がある。In addition, in order to reduce the calculation load, it is possible to detect the average rotational speed of each cylinder from the angular interval between the top dead center of each cylinder, and detect abnormal cylinders from the change in this average rotational speed. Since the average rotational speed in a wide angular interval between the top dead center of each cylinder is detected, the variation in rotational speed between a cylinder that misfires and a cylinder that does not misfire is reduced, making it possible to accurately identify the cylinder that misfires. The problem is that I can't.
そこで、本発明は演算負荷を大きくすることなく、正確
に失火気筒を検出することを目的とするものである。Therefore, an object of the present invention is to accurately detect a misfiring cylinder without increasing the calculation load.
そのため、本発明は第1図に示すごとく、多気筒内燃機
関の1回転につき複数の角度位置を検出する単位信号発
生手段と、この単位信号発生手段により検出した角度位
置間隔から各気筒の特定の回転位置の瞬時回転数を検出
する回転数検出手段と、この回転数検出手段により検出
した各気筒の特定の回転位置の瞬時回転数の変動分から
異常気筒を検出する異常気筒検出手段とを備える多気筒
内燃機関用失火検出装置を提供するものである。Therefore, as shown in FIG. 1, the present invention includes a unit signal generating means for detecting a plurality of angular positions per rotation of a multi-cylinder internal combustion engine, and a specific angular position interval detected by the unit signal generating means for detecting a specific position of each cylinder. A multi-purpose cylinder comprising a rotation speed detection means for detecting an instantaneous rotation speed at a rotation position, and an abnormal cylinder detection means for detecting an abnormal cylinder based on the variation in the instantaneous rotation speed at a specific rotation position of each cylinder detected by the rotation speed detection means. A misfire detection device for a cylinder internal combustion engine is provided.
これにより、単位信号発生手段により多気筒内燃機関の
1回転につき複数の角度位置を検出し、この単位信号発
生手段により検出した角度位置間隔から回転数検出手段
により各気筒の特定の回転位置の瞬時回転数を検出し、
この回転数検出手段により検出した各気筒の特定の回転
位置の瞬時回転数の変動分から異常気筒検出手段により
異常気筒を検出する。As a result, the unit signal generating means detects a plurality of angular positions per rotation of the multi-cylinder internal combustion engine, and the rotational speed detecting means detects the instantaneous timing of a specific rotational position of each cylinder based on the angular position interval detected by the unit signal generating means. Detects the rotation speed,
An abnormal cylinder is detected by the abnormal cylinder detection means based on the variation in the instantaneous rotation speed at a specific rotational position of each cylinder detected by the rotation speed detection means.
本発明による多気筒内燃機関の失火気筒検出装置は前記
目的達成のために第2図に示すような構成をとる。クラ
ンク軸の1回転につき複数の単位信号パルスを発生する
単位信号発生手段1と、エンジンの2回転で1回転する
カム軸の1回転につき1個の基準信号のパルスを発生す
る基準信号発生手段2と、特定のクランク期間のパルス
周期を計測し、その結果に基づいて失火判別する失火気
筒判別手段を含むマイクロコンピュータ3とから成り立
っている。またマイクロコンピュータ3は公知のごとく
、基準信号、単位信号以外にその他のセンサ4からの吸
気状態、冷却水温等のエンジンパラメータを入力して、
点火時期や燃料噴射量を演算して、その結果に基づきイ
グナイタ5やインジェクタ6を駆動する。単位信号発生
手段1は細かい程精度が向上するが、必要以上に細かく
設定する必要はなく、最低限点火周期を4等分する分解
能があれば良い。つまり6気筒内燃機関ならば30°C
A信号、4気筒内燃機関ならば45°CA信号以上の分
解能があれば十分である。The misfiring cylinder detection device for a multi-cylinder internal combustion engine according to the present invention has a configuration as shown in FIG. 2 in order to achieve the above object. A unit signal generating means 1 that generates a plurality of unit signal pulses per revolution of the crankshaft, and a reference signal generating means 2 that generates one reference signal pulse per revolution of the camshaft, which rotates once every two revolutions of the engine. and a microcomputer 3 including misfiring cylinder discriminating means for measuring the pulse period of a specific crank period and discriminating misfire based on the result. In addition, as is well known, the microcomputer 3 inputs engine parameters such as the intake air condition and cooling water temperature from the sensor 4 in addition to the reference signal and the unit signal.
The ignition timing and fuel injection amount are calculated, and the igniter 5 and injector 6 are driven based on the results. The precision of the unit signal generating means 1 improves as it becomes finer, but there is no need to set it more finely than necessary, and it is sufficient that it has at least the resolution to divide the ignition period into four equal parts. In other words, 30°C for a 6-cylinder internal combustion engine.
If the A signal is a 4-cylinder internal combustion engine, a resolution of 45° CA signal or higher is sufficient.
次に各信号の位相であるが第3図に示す6気筒内燃機関
の瞬時回転数と内燃機関の°CAの関係から明らかなよ
うに、第3図(a)の実線で示すごとく瞬時回転数は各
気筒の上死点(TDC)近辺で最も落ち込み、燃焼によ
り加速されて次の気筒の上死点で再び落ち込むという周
期性を存している。Next, regarding the phase of each signal, as is clear from the relationship between the instantaneous rotational speed of the 6-cylinder internal combustion engine and °CA of the internal combustion engine shown in Figure 3, the instantaneous rotational speed is as shown by the solid line in Figure 3(a). has a periodicity in which it drops the most near the top dead center (TDC) of each cylinder, is accelerated by combustion, and then drops again at the top dead center of the next cylinder.
ここである特定気筒に異常が発生して正常な燃焼が行な
われないと、第3図(a)の破線で示すごとく加速され
ずに次の気筒の上死点まで回転速度が下降し続ける。そ
こで、燃焼結果が最も顕著に表われる上死点付近の瞬時
回転数を計測するために、上記単位信号の位相を第3図
(C)または(d)のように設定するのが最適と言える
(パルス信号が30°C°A周期でその立ち上がりを有
効エツジとして矢印の範囲を周期計測する場合)。If an abnormality occurs in a particular cylinder and normal combustion is not performed, the rotational speed continues to decrease to the top dead center of the next cylinder without being accelerated, as shown by the broken line in FIG. 3(a). Therefore, in order to measure the instantaneous rotation speed near top dead center, where the combustion result is most noticeable, it is best to set the phase of the unit signal as shown in Figure 3 (C) or (d). (When the pulse signal has a period of 30°C°A and its rising edge is used as an effective edge to measure the period in the range indicated by the arrow).
以下に本発明にかかわる主要な処理であるマイクロコン
ピュータ3による異常気筒検出処理について第4図のフ
ローチャートを用いて詳しく説明する。第4図における
iは気筒数カウンタのカウント値であるが、これは爆発
行程にある気筒の番号を表わし、本実施例では6気筒で
あるので、0〜5の数値が用いられる。又、C(i)は
各々の気筒の異常検出回数をカウントする気筒別異常回
数カウンタのカウント値であり、本実施例ではB回(例
えば4回)以上連続して異常有りと判定された時、その
気筒が異常であるとして、該当気筒の判定結果フラッグ
H(i)に1を立てるようになっている。Cは単位信号
をカウントする単位信号カウンタのカウント値であり、
本実施例では6気筒内燃機関で30°CA信号となるよ
うに1〜24の数値が用いである。Below, the abnormal cylinder detection process by the microcomputer 3, which is the main process related to the present invention, will be explained in detail using the flowchart shown in FIG. In FIG. 4, i is the count value of the cylinder number counter, which represents the number of the cylinder in the explosion stroke, and since there are six cylinders in this embodiment, a numerical value from 0 to 5 is used. Further, C(i) is the count value of a cylinder-specific abnormality counter that counts the number of times an abnormality is detected in each cylinder. , the cylinder is determined to be abnormal, and the determination result flag H(i) of the cylinder is set to 1. C is the count value of a unit signal counter that counts unit signals,
In this embodiment, numerical values from 1 to 24 are used to obtain a 30° CA signal in a 6-cylinder internal combustion engine.
そして、各カウンタのカウント値c、 c(i)、
iはエンジン始動のためにキースイッチをONするこ
とにより初期化され、第4図のフローチャートは単位信
号(NE信号)が立ち上がるごとに実行される。Then, the count value c of each counter, c(i),
i is initialized by turning on the key switch to start the engine, and the flowchart in FIG. 4 is executed every time the unit signal (NE signal) rises.
まず、ステップ90で基準信号(G信号)があるか否か
が判断され、基準信号があるときにはステップ91に進
んで単位信号カウンタCを0にリセットした後ス゛テッ
プ92へ進み、基準信号がないときには直接ステップ9
2へ進む。ステ・ンプ92では単位信号カウンタのカウ
ント値Cを1つ増やす。次のステップ93では各気筒の
上死点付近の特定の角度位置を検出するため、単位信号
カウンタのカウント値Cを4で割算したときの余りが1
か否かを判断し、余りが1でないときには上死点付近の
特定位置でないので、ステップ94に進んで、カウント
値Cが24か否かを判断し、カウント値Cが24のとき
にはステップ95へ進んでカウント値CをOにリセット
した後、リターンし、カウント値Cが24以外のときに
はそのままリターンする。また、ステップ93において
、(C÷4)の余りが1であると判断すると、上死点付
近の特定の角度位置であると判断して、ステップ100
へ進む。このステップ100では今回の単位角度信号の
割込時刻と、その1つ前の単位角度信号の割込時刻との
差より第3図(C)または(d)の矢印で示す特定クラ
ンクタイミングにおけるエンジン回転数(瞬時回転数)
を演算して、NE、。、とする。次にステップ101に
おいて1点火前の同演算値NE、、、との差ΔNEを演
算する。ステップ102においてΔNBを所定(iiA
(ここで、A〉Oで、例えば2Orpm)と比較し、A
よりも大きく回転数が落ち込んだ場合はステップ103
に進み該当気筒の異常発生回数を数える気筒別異常回数
カウンタのカウント値C(i)を1つ増やす。それ以外
のときはステップ104に進んで該当気筒の気筒別異常
回数カウンタのカウンタ値c (Dをクリアする。次の
ステップ105では連続何回同一の気筒の異常発生が続
いたかを判別する項で、本実施例の場合はB回(例えば
4回)以上連続した場合にステップ106へ進んで該当
気筒の異常判別フラッグH(i)に1を立てるようにな
っている。ステップ107〜109は気筒のインデック
スを周期的に変化させるためのものである。また、ステ
ップ110は次回のステップ101の演算のために該当
気筒のNF、0−aを更新するためのものである。First, in step 90, it is determined whether or not there is a reference signal (G signal). If there is a reference signal, the process proceeds to step 91, and after resetting the unit signal counter C to 0, the process proceeds to step 92. If there is no reference signal, the process proceeds to step 92. Direct step 9
Proceed to 2. Step 92 increments the count value C of the unit signal counter by one. In the next step 93, in order to detect a specific angular position near the top dead center of each cylinder, the remainder when the count value C of the unit signal counter is divided by 4 is 1.
If the remainder is not 1, the specific position is not near the top dead center, so the process proceeds to step 94, and it is determined whether the count value C is 24. If the count value C is 24, the process proceeds to step 95. After proceeding and resetting the count value C to O, the process returns, and if the count value C is other than 24, the process returns directly. Further, in step 93, if it is determined that the remainder of (C÷4) is 1, it is determined that the position is a specific angular position near the top dead center, and step 100 is performed.
Proceed to. In this step 100, the engine at a specific crank timing shown by the arrow in FIG. Rotation speed (instantaneous rotation speed)
Compute NE. , and so on. Next, in step 101, the difference ΔNE from the same calculated value NE, . . . one ignition before is calculated. In step 102, ΔNB is predetermined (iiA
(Here, A>O, for example, 2Orpm),
If the rotation speed drops more than , step 103
Then, the count value C(i) of the cylinder-by-cylinder abnormality counter, which counts the number of abnormality occurrences in the relevant cylinder, is increased by one. Otherwise, the process advances to step 104 and clears the counter value c (D) of the cylinder-specific abnormality counter for the cylinder in question. In the next step 105, a step is performed to determine how many consecutive abnormalities have occurred in the same cylinder. , in the case of this embodiment, if the abnormality determination flag H(i) of the relevant cylinder is set to 1 if it occurs B times or more (for example, 4 times) or more consecutively, the process proceeds to step 106 and sets 1 to the abnormality determination flag H(i) of the relevant cylinder.Steps 107 to 109 Step 110 is for updating the NF, 0-a of the relevant cylinder for the next calculation in step 101.
これによって、比較的簡単なソフト構成にて、失火気筒
を判別して記憶することができる。そして、異常判定フ
ラグH(i)を読み出すことによってどの気筒が失火し
ているのかを知ることができる。As a result, a misfiring cylinder can be determined and stored using a relatively simple software configuration. Then, by reading out the abnormality determination flag H(i), it is possible to know which cylinder is misfiring.
なお、前記した実施例では単位信号発生手段1として2
4パルス/2rev (30°CA毎の信号)をあげ
たが、上死点をはさむ、もしくは十分近傍の(必ずしも
上死点近傍でなくてもよい)特定クランク角度の信号さ
えあれば事足りるので、第5図に示すごとく、各気筒の
上死点前15“CAと上死点後15°CAとのみに単位
信号を発生する信号発生手段でも良い。なお、エンジン
の減速運転時。In addition, in the embodiment described above, 2 units are used as the unit signal generating means 1.
I have given 4 pulses/2rev (signal every 30° CA), but all you need is a signal at a specific crank angle that is between or sufficiently close to top dead center (not necessarily near top dead center). As shown in FIG. 5, a signal generating means may be used that generates a unit signal only at 15° CA before top dead center and 15° CA after top dead center of each cylinder. Note that during deceleration operation of the engine.
冷間時等の外乱による誤判定を回避するために第4図に
おける異常検出の処理をエンジン条件に応じて実行する
(減速運転時や、エンジン冷却水温が低いときには異常
検出処理の実行を中止する)のも有効である。 また、
本発明によれば異常気筒を確実に検出できるので、点火
(点火コイル1次電圧)、及び燃料系(インジェクタ電
流)のモニタ信号との論理演算により異常の部位を特定
することも可能である。In order to avoid erroneous judgments due to disturbances such as when the engine is cold, the abnormality detection process shown in Figure 4 is executed according to the engine conditions (the execution of the abnormality detection process is stopped during deceleration operation or when the engine cooling water temperature is low). ) is also valid. Also,
According to the present invention, since an abnormal cylinder can be reliably detected, it is also possible to specify the abnormal part by logical operation with the ignition (ignition coil primary voltage) and fuel system (injector current) monitor signals.
また、第4図のフローチャートのうちステップ94.9
5は省略することもでき、逆にこのステップ94.95
を設けた場合にはステップ90〜92を省略し、場合に
よっては基準信号発生手段2も省略することもできる。Also, step 94.9 in the flowchart of FIG.
5 can be omitted; conversely, this step 94.95
In the case that steps 90 to 92 are provided, steps 90 to 92 may be omitted, and in some cases, the reference signal generating means 2 may also be omitted.
(発明の効果)
以上述べたように本発明においては、内燃機関の各気筒
の特定回転角度位置の瞬時回転数の変動分より失火気筒
を検出するから、演算負荷の増大を招くことなく、かつ
精度よく失火気筒を検出することができるという優れた
効果がある。(Effects of the Invention) As described above, in the present invention, a misfiring cylinder is detected based on the fluctuation in the instantaneous rotational speed at a specific rotational angle position of each cylinder of an internal combustion engine. This has the excellent effect of being able to detect misfiring cylinders with high accuracy.
第1図は本発明の特許請求の範囲対応図、第2図は本発
明装置の一実施例を示すブロック図、第3図は第2図図
示装置の作動説明に供する各部波形図、第4図は第2図
図示装置の作動説明に供するフローチャート、第5図は
本発明装置の他の実施例の説明に供する各部波形図であ
る。
1・・・単位信号発生手段、2・・・基準信号発生手段
、3・・・マイクロコンピュータ。FIG. 1 is a diagram corresponding to the claims of the present invention, FIG. 2 is a block diagram showing an embodiment of the device of the present invention, FIG. 3 is a waveform diagram of various parts for explaining the operation of the device shown in FIG. 2, and FIG. 2 is a flowchart for explaining the operation of the apparatus shown in FIG. 2, and FIG. 5 is a waveform diagram of various parts for explaining another embodiment of the apparatus of the present invention. DESCRIPTION OF SYMBOLS 1... Unit signal generation means, 2... Reference signal generation means, 3... Microcomputer.
Claims (1)
する単位信号発生手段と、この単位信号発生手段により
検出した角度位置間隔から各気筒の特定の回転位置の瞬
時回転数を検出する回転数検出手段と、この回転数検出
手段により検出した各気筒の特定の回転位置の瞬時回転
数の変動分から異常気筒を検出する異常気筒検出手段と
を備える多気筒内燃機関用失火検出装置。unit signal generating means for detecting a plurality of angular positions per rotation of a multi-cylinder internal combustion engine; and rotational speed detection for detecting the instantaneous rotational speed at a specific rotational position of each cylinder from the angular position interval detected by the unit signal generating means. A misfire detection device for a multi-cylinder internal combustion engine, comprising: a means for detecting an abnormal cylinder; and an abnormal cylinder detecting means for detecting an abnormal cylinder based on a variation in the instantaneous rotational speed at a specific rotational position of each cylinder detected by the rotational speed detecting means.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP26497888A JP2611387B2 (en) | 1988-10-20 | 1988-10-20 | Misfire detector for multi-cylinder heat engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP26497888A JP2611387B2 (en) | 1988-10-20 | 1988-10-20 | Misfire detector for multi-cylinder heat engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH02112646A true JPH02112646A (en) | 1990-04-25 |
JP2611387B2 JP2611387B2 (en) | 1997-05-21 |
Family
ID=17410859
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP26497888A Expired - Lifetime JP2611387B2 (en) | 1988-10-20 | 1988-10-20 | Misfire detector for multi-cylinder heat engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2611387B2 (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04128536A (en) * | 1990-09-18 | 1992-04-30 | Daihatsu Motor Co Ltd | Misfire detection method of internal combustion engine |
JPH0571409A (en) * | 1991-07-12 | 1993-03-23 | Honda Motor Co Ltd | Misfire detector for multiple cylinder internal combustion engine |
DE4324200A1 (en) * | 1992-07-21 | 1994-01-27 | Fuji Heavy Ind Ltd | Misfire detection method for an engine |
DE4334068A1 (en) * | 1992-10-08 | 1994-04-14 | Fuji Heavy Ind Ltd | Engine misfire detection method |
US5379634A (en) * | 1991-07-12 | 1995-01-10 | Honda Giken Kogyo Kabushiki Kaisha | Misfire-detecting system for internal combustion engines |
US5485374A (en) * | 1992-06-03 | 1996-01-16 | Hitachi, Ltd. | Combustion-conditon diagnostic system and method for a multicylinder engine |
US6061624A (en) * | 1993-11-29 | 2000-05-09 | Hitachi, Ltd. | Multi-cylinder engine combustion state diagnosis apparatus and method |
KR100405721B1 (en) * | 2001-09-17 | 2003-11-14 | 현대자동차주식회사 | Misfire detection controlling method of hybrid electronic vehicle |
-
1988
- 1988-10-20 JP JP26497888A patent/JP2611387B2/en not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04128536A (en) * | 1990-09-18 | 1992-04-30 | Daihatsu Motor Co Ltd | Misfire detection method of internal combustion engine |
JPH0571409A (en) * | 1991-07-12 | 1993-03-23 | Honda Motor Co Ltd | Misfire detector for multiple cylinder internal combustion engine |
US5379634A (en) * | 1991-07-12 | 1995-01-10 | Honda Giken Kogyo Kabushiki Kaisha | Misfire-detecting system for internal combustion engines |
US5485374A (en) * | 1992-06-03 | 1996-01-16 | Hitachi, Ltd. | Combustion-conditon diagnostic system and method for a multicylinder engine |
DE4324200A1 (en) * | 1992-07-21 | 1994-01-27 | Fuji Heavy Ind Ltd | Misfire detection method for an engine |
DE4324200C2 (en) * | 1992-07-21 | 1998-09-10 | Fuji Heavy Ind Ltd | Misfire detection method for an engine |
DE4334068A1 (en) * | 1992-10-08 | 1994-04-14 | Fuji Heavy Ind Ltd | Engine misfire detection method |
DE4334068C2 (en) * | 1992-10-08 | 1998-03-26 | Fuji Heavy Ind Ltd | Engine misfire detection method |
US6061624A (en) * | 1993-11-29 | 2000-05-09 | Hitachi, Ltd. | Multi-cylinder engine combustion state diagnosis apparatus and method |
KR100405721B1 (en) * | 2001-09-17 | 2003-11-14 | 현대자동차주식회사 | Misfire detection controlling method of hybrid electronic vehicle |
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JP2611387B2 (en) | 1997-05-21 |
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