JPS5859334A - Knocking suppressing device for internal-combustion engine - Google Patents
Knocking suppressing device for internal-combustion engineInfo
- Publication number
- JPS5859334A JPS5859334A JP56157788A JP15778881A JPS5859334A JP S5859334 A JPS5859334 A JP S5859334A JP 56157788 A JP56157788 A JP 56157788A JP 15778881 A JP15778881 A JP 15778881A JP S5859334 A JPS5859334 A JP S5859334A
- Authority
- JP
- Japan
- Prior art keywords
- fuel ratio
- air
- knocking
- ignition timing
- control
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
- F02P5/00—Advancing or retarding ignition; Control therefor
- F02P5/04—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions
- F02P5/145—Advancing 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
- F02P5/15—Digital data processing
- F02P5/152—Digital data processing dependent on pinking
- F02P5/1528—Digital data processing dependent on pinking for turbocompressed engine
-
- 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)
- Signal Processing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of The Air-Fuel Ratio Of Carburetors (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Abstract
Description
【発明の詳細な説明】
零発8Aは、火花点火式の内燃機関における)・ソ十シ
ジを抑制制御する装flK関するものである。DETAILED DESCRIPTION OF THE INVENTION The zero engine 8A relates to a system flK for suppressing and controlling the internal combustion engine of a spark ignition type internal combustion engine.
火花点火式の内部機関においで高出力と低燃料消費率と
を得るには、点火時期を機関の全運転域にわたって常に
f&適点火時期(MBT )4C制御するのが望ましい
が、MBTは機関の高負荷、低回転埴では、ノ・9十シ
ジ限界の点火時期より進角側に存在する場合があるので
、この領域においてノッ、?−シクが発生すると七にな
り、特に機関の圧縮比を高くするとノツキングが発生す
る領域が増大することになる。In order to obtain high output and low fuel consumption in a spark-ignition internal engine, it is desirable to always control the ignition timing by f & appropriate ignition timing (MBT) 4C over the entire operating range of the engine. In high-load, low-speed engines, the ignition timing may be on the advanced side of the 90-degree limit, so in this region, the ignition timing may be advanced. - When knocking occurs, it becomes 7. In particular, when the compression ratio of the engine is increased, the area where knocking occurs increases.
そこで最近の一部の内燃機関においては、機関にノ・ソ
+シクセンサーを設け、ノ・ソ士シジが発生すればこれ
妊応じて点火時期を適宜遅角し、ノ・す十ンクがなくな
れば元の点火時期に戻すようにしたhわゆるノックフィ
ードバックシステムの点火時期制御を行なうことにより
、ノツキングを抑制することが行なわれている。しかし
、このよう九機関における実際の点火時期をノツキング
に応じてノツキングが削5減する所まで遅角させること
は、可成り遅角りなければならないから、点火時期の遅
角処゛理によるノ1シ+、クジ抑制時において、機関の
出力か急激に低すするのである。Therefore, some of the recent internal combustion engines are equipped with a fuel pump sensor, and when fuel leakage occurs, the ignition timing is retarded appropriately to eliminate fuel leakage. Knocking has been suppressed by controlling the ignition timing using a so-called knock feedback system, which returns the ignition timing to the original ignition timing. However, in order to retard the actual ignition timing in these nine engines to the point where knocking is reduced by 55%, the ignition timing must be retarded considerably. 1+, when the engine is suppressed, the engine's output drops suddenly.
これに対し先行技術として特開昭55−43206号公
報は5.ノ・″!+−シジと吸気混合気の空燃比とは一
定の相関関係をもち、空燃比を濃くするとノ・ン+yり
が発生し難くなる事実に鑑み、ノッ+ンタが発生すると
これに応じて空燃比を一時的に濃くすることによシ、機
関の出力タウンを伴うこ、となくノツ士ングを抑制する
ことを提案しているか1、空燃比によるノッ十シジの抑
制に際しては、ノ・ソ士ンタに対する応答性が遅い点に
問題があるばかりか、ノ・ソ十ンジの程度により著しく
空燃比を濃くしなければならないから、点火栓にかぶり
を生じたり或いは燃費が悪化する点に問題かあった。On the other hand, as a prior art, Japanese Patent Application Laid-open No. 55-43206 discloses 5. There is a certain correlation between the air-fuel ratio of the intake air-fuel mixture and the air-fuel ratio of the intake air-fuel mixture, and considering the fact that the richer the air-fuel ratio, the less likely it is that the air-fuel ratio will occur. Accordingly, it is proposed to temporarily increase the air-fuel ratio to suppress the engine's engine output loss, without causing the engine's output to decrease. Not only is there a problem in that the response to engine failure is slow, but the air-fuel ratio must be significantly enriched depending on the degree of engine failure, which may cause fogging of the ignition plug or worsen fuel efficiency. There was a problem.
そこで本発明者達は、先に特願昭55−41007号に
おいて、点火時期のノックフィードパtリク制御により
点火時期をノ・ソ士シクに応じて遅角することに加えて
、これと同時に又は相前後して吸気系に燃料を追加供給
することにょシ、点火時期の遅角量を、燃料供給の増量
による効果分だけ少なくする一方、燃料供給の増量によ
って点火時期の遅角に基づく機関出力の低下分を補償し
て、出力のタウン及び応答性遅れを伴うことなく、ノ・
シ士ンジを抑制することを提案したが、このものは、吸
気系へ、の燃料供給系に、ノ・す+シジによる燃料増量
手段を別途に設けなければならないので、その構、造が
複雑化するのであった。Therefore, the present inventors previously proposed in Japanese Patent Application No. 55-41007 that in addition to retarding the ignition timing according to the ignition timing by knock-feed control of the ignition timing, at the same time Alternatively, if additional fuel is supplied to the intake system in succession, the amount of retardation of the ignition timing is reduced by the effect of the increased amount of fuel supply, while the engine is based on retardation of the ignition timing by increasing the amount of fuel supply. Compensates for the decrease in output and eliminates output town and response delay.
We have proposed suppressing the fuel flow, but this method requires a separate means for increasing the amount of fuel by adding pressure to the fuel supply system to the intake system, so its structure is complicated. It was to become.
本発明は、最近の内燃機関においては排気ガス中のNO
X、’Co及びHCの三元有害成分を同時に浄イ「する
目的で、排気系に排気センサーを設け、該排気センサー
に応じて吸気混谷気の空燃比を調節することにより、排
気系の空燃比が略理論空燃比になるようにフィードバッ
ク制御するいわゆる空燃比フィードバックシステムか付
帯されていることKi!み、この空燃比フィードバック
システムと前記のノックフィードバラクシステムとを組
み合せ・ノツ十シクピシサーがノ・シ+シタを検出すれ
ば点火時期を遅角する一方、これと同時又は相前後して
、空燃比フィードバックシステムをその排気センサーに
優先して吸気系の垂燃比かリッチものであり、このよう
に空燃比のりツ予化を空燃比フイードバシクシステムを
利用して行なうことにより、本発明者達による先−にお
ける構造複雑化の問題を解消できると共K、空燃比フィ
ードパ゛ツクシステムにおける吸気系空燃比の理論空燃
比設定及び高圧縮比化が可能になり燃料消費量を低減す
ることができる。The present invention aims to reduce the amount of NO in exhaust gas in modern internal combustion engines.
In order to simultaneously purify the ternary harmful components of It is important to note that it is equipped with a so-called air-fuel ratio feedback system that performs feedback control so that the air-fuel ratio becomes approximately the stoichiometric air-fuel ratio, and by combining this air-fuel ratio feedback system and the above-mentioned knock feed barak system.・If the ignition timing is detected, the ignition timing is retarded, and at the same time or around the same time, the air-fuel ratio feedback system is prioritized over the exhaust sensor to increase the intake system's normal fuel ratio. By using an air-fuel ratio feed pump system to pre-register the air-fuel ratio, the inventors believe that the problem of complicating the structure described above can be solved. It becomes possible to set the system air-fuel ratio to the stoichiometric air-fuel ratio and increase the compression ratio, thereby reducing fuel consumption.
以F本発明を気化器式内燃機関に適用した場合の実施例
について説明すると、図において(1)は各気筒に点火
栓(2)を有する多気筒内燃機関で、その−側面にはエ
アクリーナ(3)及び気イヒ器(4)を有する吸気マニ
ホールド(5)が、他側面には三元触媒(61内蔵の排
気浄化装置1 (7)を有する排気マニホールド(8)
が各々取付いている。(9)は点火時期制徊装+rtの
一例であるダイストリピユータ、Oυは点−火コイル、
(lりはバ′リテリー、収はイクニツショシスイ・ソチ
を各々示し、前記ダイストリしユータ【9)は、点火コ
イル(1すに対する断続器部−と各点火栓(2)に対す
る配電FMSf14)とからなシ、また、ディストリF
:l−タ(9)1・こは図示しない従来公知の真空式進
角機構と辿心弐進角機構とが備えられ、点火時期を機関
の負荷及び回転数に対して所定の進角特性に基いて制−
御するように構成されている。Hereinafter, an embodiment in which the present invention is applied to a carburetor internal combustion engine will be described. In the figure, (1) is a multi-cylinder internal combustion engine that has a spark plug (2) in each cylinder, and an air cleaner (2) is installed on the side of the engine. The intake manifold (5) has an exhaust gas purification device 1 (7) with a built-in three-way catalyst (61) on the other side.
are installed on each. (9) is a die repeater which is an example of an ignition timing control device +rt, Oυ is an ignition-fire coil,
(L indicates the battery, and the figure indicates the ignition system. Karanashi, also DistriF
: L-tor (9) 1. This is equipped with a conventionally known vacuum type advance mechanism (not shown) and a reciprocating center advance mechanism (not shown), which adjusts the ignition timing to a predetermined advance characteristic with respect to the engine load and rotation speed. Based on -
It is configured to be controlled.
00は機関(1)に取付くノッ十シジtシサー〇〇から
の芦号に基いて°)ツ十シタの有無を判別する回路で、
該ノック判別lND$061はノ・ν中シタの判断をす
れば、前記ダイストリピユータ(9)における断続器0
濁ど点火コイルωの→次側とをつなぐ回路中に設けた点
火時期遅延回路(171に)・すi:7り信号を発する
。点火時期遅延回MOカはこれにノtソ+シジ信号が入
ると、前記ディストリビュータ(9)による点火時期を
適宜角度0だけ遅角し、ノッ辛シク信号がなくなれば元
の点火時期に戻すようになっている。00 is a circuit that determines the presence or absence of the switch based on the number from the switch installed on the engine (1).
If the knock determination lND$061 is determined to be in the middle, the interrupter 0 in the die repeater (9)
The ignition timing delay circuit (171) provided in the circuit connecting the ignition coil ω to the next side emits a signal. When the ignition timing retardation MO switch receives a notch signal, the ignition timing by the distributor (9) is appropriately retarded by an angle of 0, and when the noisy signal disappears, the ignition timing is returned to the original ignition timing. It has become.
前記気イヒ器におけるメイン系燃料供給通路用及びスロ
ー果燃料供給通路一やうちいずれか一方又は両方には、
通路類を介してエアクリーナ(3)等の大気連通箇所に
関する空燃比フィードパ・シフ制御用の補助エアブリー
ド1IT1221が接続され、両補助エアナリード12
11 !22 Fi、アクチ゛ユI−夕のにおける針弁
e141 @ Kてアナ0り的市開−される。Either or both of the main system fuel supply passage and the slow fuel supply passage in the above-mentioned ignition device,
An auxiliary air bleed 1IT1221 for air-fuel ratio feed/shift control for air communication points such as the air cleaner (3) is connected through passages, and both auxiliary air bleed leads 12
11! 22 Fi, the needle valve e141 in the evening of Actuary I-K will be opened on the market.
割は排気ガス中の02、C01COhl(C又はNOx
の濃度を検出する排気セシサー、Q71II′i該排気
センサー2(i)からの信号を入力とする空燃比フィー
ドパ・ツク制御回路を各々示し、この制御回路けは排気
センサー四回の出力と制御目標値とを比較し、これに応
じて+111記アク子ユエータ■を作動するもので、例
えば、排気tシサー(イ)がO2濃度を検出するもので
ある場合において、仁れによって検出したOf濃度が理
論空燃比のときの0諺濃度を越えているとき、空燃比は
理論空燃比よりリーンであるから、アク子ユエータ(ハ
)によって両補助エアづリードホードe2+112Aの
開口面積を減少して吸気系の空燃比を濃くし、また、検
出したO!濃度が理論空燃比のときのO2濃度に達して
いないとき、空燃比は理論′!P燃比よりリッチである
から、アク予ユエータ囚に両補助エアブリードボート@
t+(22の開口面積を増大して吸気系の空燃比を薄く
するようにして、排気セシサー箇所の空燃比を略理論空
燃比罠つイードパ・ツク制御するようになっている。The percentage is 02, C01COhl (C or NOx) in the exhaust gas.
The exhaust sensor that detects the concentration of This function compares the value with When the stoichiometric air-fuel ratio exceeds 0 concentration, the air-fuel ratio is leaner than the stoichiometric air-fuel ratio, so the actuator (c) reduces the opening area of both auxiliary air lead hoards e2+112A and improves the intake system. The air-fuel ratio was enriched, and the detected O! When the O2 concentration has not reached the stoichiometric air-fuel ratio, the air-fuel ratio is stoichiometric! Since it is richer than the P fuel ratio, both auxiliary air bleed boat @
By increasing the opening area of t+(22) and reducing the air-fuel ratio of the intake system, the air-fuel ratio at the exhaust processor is controlled to be approximately at the stoichiometric air-fuel ratio.
史に前記空燃比フィードバック制御回路f)は、前記ノ
・シフ判別回路a@からの信号を入力とじ、機関にノウ
中ジグが発生すれば、その信号に基づき、排気セシサー
(至)からの信号に拘らず、前記アクチェータ(ハ)に
より両補助エアブリードa’ll翰の開口面積置、フッ
中ジグ発生前の伏動よりも適宜量だけ減少することによ
り、吸気系の空燃比を適宜値だけ濃くするようKなって
いる。The air-fuel ratio feedback control circuit f) inputs the signal from the shift discrimination circuit a@, and if a jig occurs in the engine, the air-fuel ratio feedback control circuit f) outputs a signal from the exhaust selector based on the signal. Regardless of the above, the actuator (c) reduces the opening area of both auxiliary air bleeds by an appropriate amount compared to the downward movement before the jig occurs, thereby adjusting the air-fuel ratio of the intake system by an appropriate value. K is set to make it darker.
すなわち、機関にノ・す十シタが発生すれば、点火時期
が適宜角度θだけ遅角制御される一方、吸気系の空燃比
が適宜値だi漉くなるから、ノッ十ジグ抑制されるので
あり、従来め点火時期の遅角のみによってノウ中ジグを
制御する場合に比較して、点火時期の遅角量を、空燃比
を濃くすることによる効果分だけ小さくできる一方、点
火時期を遅角したことKよる出力のタウシ分を、空燃比
の濃化によって補償することができる。から、出方タウ
ンを伴うことなくノウ中ジグを抑制することができ・る
のであり、また、先行技術としての特開昭55−+−4
3206号公報のように空燃比の濃化のみによってノ・
ソ中ジグを制御する場合(比較して、空燃比の1化値を
、点火時期の遅角による効果分1tけ小さくできるから
、点火栓のかぶり及び応答性更には燃費を向上できるの
である。In other words, when nozzle jig occurs in the engine, the ignition timing is retarded by an appropriate angle θ, and the air-fuel ratio in the intake system is increased by an appropriate value, so that nozzle jig is suppressed. Compared to the conventional case of controlling the ignition timing jig only by retarding the ignition timing, the amount of retardation of the ignition timing can be reduced by the effect of enriching the air-fuel ratio, while retarding the ignition timing. The increase in output due to K can be compensated for by enriching the air-fuel ratio. Therefore, it is possible to suppress the jig in the middle without causing the appearance town, and also, as a prior art,
As in Publication No. 3206, no.
When controlling a saw jig (by comparison, the unification value of the air-fuel ratio can be reduced by 1 ton due to the effect of retarding the ignition timing, so the fogging of the ignition plug and the responsiveness as well as fuel efficiency can be improved).
この場合、ノツキングに対する吸気系空燃比のl層化処
理は、ノウ中ジグに対する点火時期の遅角処理と同時に
行なうか、遅角処理の前又は後に行なっても良いか、ノ
ウ中ジグに対して先づ空燃比を濃イヒし、これで)・シ
キシジがなくなれば元の空燃比に戻し、まだノツキング
が消えないときには点火時期を遅角し、これによってノ
・ソ+ンジがなくなれば逆の順序で元に戻すようにした
り、或いは、ノツキングに対して先づ点火時期を遅角し
、これでノツキングがなくなれば元の点火時期に灰し、
まだノウ牛ンジが消えないときには空燃比を濃化し、こ
れによってノウ中ジグがなくなれば逆の順序で元に戻す
ようにしても良く、また、これら両方処理を機関のスロ
ットル開度又は吸気負圧等に関連し、高負荷域では点火
時期の遅角処理の力を先に、他の負荷域では点火時期の
遅角処理のみにするか両方を組み合せるようにすること
もできるのであり、ノ1ソキシクに対する遅角量はクラ
ンク角で2〜4が、空燃比の濃化値は理論空燃比に対し
、て数%〜20%が適当である。In this case, the l-stratification process of the intake system air-fuel ratio for knocking may be performed at the same time as the ignition timing retardation process for the nozzle jig, or may be performed before or after the ignition timing retardation process. First, the air-fuel ratio is enriched, and when the sparking disappears, the air-fuel ratio is returned to the original one, and if the knocking still does not disappear, the ignition timing is retarded, and if the sparking disappears, the reverse order is performed. Or, you can first retard the ignition timing to prevent knocking, and if the knocking disappears, the ignition timing will return to its original value.
If the air-fuel ratio still does not go away, the air-fuel ratio may be enriched, and if the air-fuel ratio disappears, the air-fuel ratio may be restored in the reverse order. In relation to this, it is possible to first retard the ignition timing in the high load range, and only retard the ignition timing in other load ranges, or to combine both. Appropriately, the amount of retardation per crank angle is 2 to 4 in terms of crank angle, and the enrichment value of the air-fuel ratio is several percent to 20% with respect to the stoichiometric air-fuel ratio.
なお、上記実施例は点火時期の制−に従来公知のがイス
トリピユータを用いて説明したが、本発明はこれに限ら
ず、池の点火時期制御手段でも良く、吸気系空燃比の制
御は補助エアづリートの開閉に限らず、池の空燃比制御
手段でも良く、また、零発94Ifi気化器式内燃機関
に限らず、燃料噴射式の内燃機関に適用できることはい
うまでもない。Although the above embodiment has been described using a conventionally known istry repeater to control the ignition timing, the present invention is not limited to this; a pond ignition timing control means may also be used, and the intake system air-fuel ratio may be controlled using auxiliary air. It goes without saying that the present invention is not limited to the opening and closing of the valve, and may also be used as an air-fuel ratio control means for the pond, and is applicable not only to the zero-engine 94 Ifi carburetor type internal combustion engine but also to a fuel injection type internal combustion engine.
以上の通り本発明は、ノツキングを点火時期の遅角処理
と、吸気系22!燃此の濃化処理の併用によって抑制制
御するに当り、吸気系空燃比の濃化処理を空燃比のフィ
ードバックシステムを利用して行なうようkしたから、
本発明者達の先験特許用−〇ように、吸気系に別の燃刺
増量手段を設ける必要がなく、装置の構造を簡略化でき
るのであり、しかも、空燃比のフィードバック・システ
ムを利用したことkよシ、フッ+4ンジを応答遅れなく
的確′K11lllilt、6e &#f、d’! !
d、61□。フィー。As described above, the present invention solves the knocking by retarding the ignition timing and by retarding the ignition timing and the intake system 22! When performing suppression control by combining fuel enrichment processing, the intake system air-fuel ratio enrichment processing was performed using an air-fuel ratio feedback system.
As shown in the inventors' prior patent - ○, there is no need to provide a separate fuel increase means in the intake system, and the structure of the device can be simplified.Moreover, the air-fuel ratio feedback system is used. Kotok Yoshi, Fu + 4 nge without any delay in response 'K11llilt, 6e &#f,d'! !
d, 61□. fee.
バ・ツクシステムにおける空燃比の設定値を理論空燃比
に設定することができ、且つ高圧到比が0工能となり、
機関の燃料消費量を低減できる効果をイ」する。The set value of the air-fuel ratio in the backup system can be set to the stoichiometric air-fuel ratio, and the high pressure ratio becomes 0,
It has the effect of reducing engine fuel consumption.
図面は本発明の実施例を示す図である。
(1)・°°機関、(5)・°°吸気マニホールド、(
8)・・・υF気マニホールド、(2)・・・点火栓、
(9)・・・ディストリじユータ、0(ト・・点火コイ
ル、161…ノツ+yタセンサー〜(1′n・・・点火
時期遅延回路、 1211ff12″・・・補助エアナ
リード、(わ)・・・アクチュエータ、(財)・°°排
気センサー、ば゛°°制御回路。
特許出願人 タイハツ工業株式会社
代″理 人 弁理士 石井暁 夫The drawings are diagrams showing embodiments of the invention. (1)・°°engine, (5)・°°intake manifold, (
8)...υF air manifold, (2)...ignition plug,
(9)... Distributor, 0 (g... Ignition coil, 161... Note+yta sensor ~ (1'n... Ignition timing delay circuit, 1211ff12''... Auxiliary air lead, (wa)... Actuator, °° exhaust sensor, and control circuit. Patent applicant: Taihatsu Kogyo Co., Ltd. Representative, Patent attorney: Akio Ishii
Claims (1)
じて点火時期を遅角するようにしたノックフィードバッ
クシステムと、排気系に設けた排気tシサーに応じて排
気系における空燃比か略理論空燃比になるように吸気系
の空燃比を制御するようにした空燃比フィードパ・シフ
システムとを備えた内燃機関において、前記フィードバ
ラクシステムを1rf記空燃比フイードバツクシステム
に、ノッキングセンサーがノツキングを検出したとき、
排気センサーの信号に優先して吸気系の空燃比fJ貧1
+(fだけ濃くなるよう忙関連づけたことを特徴とする
内燃機関のノツキング抑制装置。(1) A knock feedback system that retards the ignition timing in response to knocking detected by a knocking sensor, and an exhaust t-scissor installed in the exhaust system that adjusts the air-fuel ratio in the exhaust system to approximately the stoichiometric air-fuel ratio. In an internal combustion engine equipped with an air-fuel ratio feed shift system that controls the air-fuel ratio of the intake system as described above, when the knocking sensor detects knocking when the feed barrack system is set to the 1rf air-fuel ratio feedback system. ,
The air-fuel ratio of the intake system fJ poor 1 takes priority over the exhaust sensor signal.
+(A knocking suppression device for an internal combustion engine, characterized in that it is associated with a busy state so as to become darker by f).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP56157788A JPS5859334A (en) | 1981-10-02 | 1981-10-02 | Knocking suppressing device for internal-combustion engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP56157788A JPS5859334A (en) | 1981-10-02 | 1981-10-02 | Knocking suppressing device for internal-combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5859334A true JPS5859334A (en) | 1983-04-08 |
Family
ID=15657299
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP56157788A Pending JPS5859334A (en) | 1981-10-02 | 1981-10-02 | Knocking suppressing device for internal-combustion engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5859334A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59201948A (en) * | 1983-04-30 | 1984-11-15 | Mitsubishi Motors Corp | Air-fuel ratio controller for engine |
-
1981
- 1981-10-02 JP JP56157788A patent/JPS5859334A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59201948A (en) * | 1983-04-30 | 1984-11-15 | Mitsubishi Motors Corp | Air-fuel ratio controller for engine |
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