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JP2003013785A - Control device for direct injection spark ignition type internal combustion engine - Google Patents

Control device for direct injection spark ignition type internal combustion engine

Info

Publication number
JP2003013785A
JP2003013785A JP2001197403A JP2001197403A JP2003013785A JP 2003013785 A JP2003013785 A JP 2003013785A JP 2001197403 A JP2001197403 A JP 2001197403A JP 2001197403 A JP2001197403 A JP 2001197403A JP 2003013785 A JP2003013785 A JP 2003013785A
Authority
JP
Japan
Prior art keywords
fuel
intake
engine
knock
rotation speed
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
Application number
JP2001197403A
Other languages
Japanese (ja)
Inventor
So Miura
創 三浦
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 JP2001197403A priority Critical patent/JP2003013785A/en
Publication of JP2003013785A publication Critical patent/JP2003013785A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/3094Controlling fuel injection the fuel injection being effected by at least two different injectors, e.g. one in the intake manifold and one in the cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D35/00Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for
    • F02D35/02Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions
    • F02D35/027Controlling engines, dependent on conditions exterior or interior to engines, not otherwise provided for on interior conditions using knock sensors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/3011Controlling fuel injection according to or using specific or several modes of combustion
    • F02D41/3017Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used
    • F02D41/3023Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used a mode being the stratified charge spark-ignited mode
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/32Controlling fuel injection of the low pressure type
    • F02D41/34Controlling fuel injection of the low pressure type with means for controlling injection timing or duration
    • F02D41/345Controlling injection timing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/40Controlling fuel injection of the high pressure type with means for controlling injection timing or duration
    • F02D41/402Multiple injections
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

(57)【要約】 【課題】混合気を亜成層化してノックの発生を抑制する
ノック改善制御を効果的に活用する。 【解決手段】所定の運転領域にて、要求される燃料の一
部を吸気部燃料噴射弁11により排気行程中に噴射して
燃焼室全体にリーンな混合気を形成し、残りの燃料を筒
内直接燃料噴射弁12により圧縮行程中に噴射すること
で混合気を亜成層化してノックの発生を抑制するノック
改善制御を行う内燃機関において、機関の回転速度が所
定の回転速度を超えるときは、前記ノック改善制御を禁
止するようにした。
(57) [Problem] To effectively utilize knock improvement control for suppressing stratification of an air-fuel mixture to suppress occurrence of knock. In a predetermined operation range, a part of required fuel is injected by an intake fuel injection valve during an exhaust stroke to form a lean mixture in the entire combustion chamber, and the remaining fuel is supplied to a cylinder. When the engine speed exceeds a predetermined speed in an internal combustion engine that performs knock improvement control that suppresses the generation of knock by sub-stratifying the air-fuel mixture by injecting during the compression stroke by the internal direct fuel injection valve 12 , The knock improvement control is prohibited.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は、所定の運転領域で
混合気を亜成層化することでノックの発生を抑制する直
噴火花点火式内燃機関の制御装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a control device for a direct injection spark ignition type internal combustion engine which suppresses knocking by substratifying an air-fuel mixture in a predetermined operation region.

【0002】[0002]

【従来の技術】従来から吸気行程中に燃料の一部を噴射
して燃焼室内に均質な形成すると共に、圧縮行程中に残
りの燃料を噴射することで点火プラグ周辺に層状の混合
気を形成するようにした火花点火式の内燃機関が知られ
ている(特開平5−118244号公報参照)。
2. Description of the Related Art Conventionally, a part of fuel is injected during an intake stroke to form a homogeneous mixture in a combustion chamber, and the remaining fuel is injected during a compression stroke to form a stratified mixture around a spark plug. There is known a spark ignition type internal combustion engine (see Japanese Patent Laid-Open No. 5-118244).

【0003】[0003]

【発明が解決しようとする課題】ところで、ノックの発
生しやすい高負荷領域にて、上記のように燃料を吸気行
程と圧縮行程とに分割して噴射することでノックの発生
を抑制できる。すなわち、吸気行程で燃焼室内全体がリ
ーンになる量の燃料を噴射し、圧縮行程で残りの燃料を
噴射して燃焼室内に亜成層化混合気を形成することによ
り、エンドガス部をリーン化してノックの発生を抑制し
改善するのである。
By the way, in a high load region where knock is likely to occur, the fuel is divided into the intake stroke and the compression stroke and injected as described above, so that the occurrence of knock can be suppressed. That is, the amount of fuel that makes the entire combustion chamber lean is injected in the intake stroke, and the remaining fuel is injected in the compression stroke to form a sub-stratified mixture in the combustion chamber, thereby leaning the end gas portion and knocking. It suppresses and improves the occurrence of.

【0004】このようなノック改善制御を行った結果、
低回転領域では、図6(A)に示すように、要求される
すべての燃料を吸気行程中に直接筒内に噴射する通常制
御の場合(破線)よりもノック改善制御を行った場合
(実線)の方が発生トルクを大きくすることができる
(トルク改善効果を得ることができる)。これは、ノッ
ク特性が悪く、点火時期をMBT(最大トルクが得られ
る点火時期:Minimum advance for
Best Torque)から離れた時期に設定せざ
るを得ない低回転領域においては、前記ノック改善制御
によって点火時期を進角させることが可能となるため、
機関発生トルクが大きくなるのである。
As a result of performing such knock improvement control,
In the low rotation speed region, as shown in FIG. 6 (A), when knock improvement control is performed (solid line), compared with normal control (broken line) in which all required fuel is directly injected into the cylinder during the intake stroke. ) Can increase the generated torque (a torque improving effect can be obtained). This is because the knock characteristic is poor, and the ignition timing is set to MBT (Ignition timing at which maximum torque is obtained: Minimum advance for).
In the low rotation speed region in which it is unavoidable to set the time away from the Best Torque), it becomes possible to advance the ignition timing by the knock improvement control.
The engine generated torque becomes large.

【0005】しかしながら、高回転領域において前記ノ
ック改善制御を行うと、図6(B)に示すように、通常
制御の場合(破線)よりもノック改善制御を行った場合
(実線)の方が、機関発生トルクが小さくなってしまう
といった問題がある。これは、高回転領域では低回転領
域の場合に比べてノック特性がよく点火時期がMBTか
らそれほど離れていないため、前記ノック改善制御によ
って点火時期を進角させることによるトルク向上効果よ
りも、燃料の一部を圧縮行程中(吸気弁が閉じた後)に
噴射することで筒内直噴の特徴である気化潜熱の有効利
用による吸気密度の向上効果が目減りし、吸入空気量が
減少してしまうことの影響の方が大きいためと考えられ
る。
However, when the knock improvement control is performed in the high rotation speed region, as shown in FIG. 6 (B), the knock improvement control (solid line) is more than the normal control (broken line). There is a problem that the engine generated torque becomes small. This is because the knock characteristic in the high rotation range is better than that in the low rotation range, and the ignition timing is not so far from the MBT. Therefore, rather than the torque improving effect by advancing the ignition timing by the knock improving control, By injecting a part of this during the compression stroke (after the intake valve is closed), the effect of improving the intake density by effectively utilizing the latent heat of vaporization, which is the characteristic of in-cylinder direct injection, is diminished, and the intake air amount is reduced. It is thought that the effect of the loss is greater.

【0006】本発明は、以上のような従来の問題を解決
するためになされたものであり、ノックの発生が問題と
なる高負荷領域において、発生トルクを十分に確保しつ
つ、ノックを効果的に回避できる直噴火花点火式の内燃
機関の制御装置を提供することを目的とする。
The present invention has been made in order to solve the conventional problems as described above, and in a high load region where the occurrence of knocking is a problem, it is possible to effectively secure the generated torque while effectively knocking. It is an object of the present invention to provide a control device for a direct injection spark ignition type internal combustion engine that can be avoided.

【0007】[0007]

【課題を解決するための手段】そのため、請求項1に係
る発明は、所定の運転領域にて、亜成層化混合気を形成
し亜成層燃焼を行う直噴火花点火式内燃機関の制御装置
において、機関の回転速度が所定回転速度を超える高回
転領域では亜成層燃焼を禁止し、前記所定回転速度を超
える高回転領域では、亜成層燃焼時の機関発生トルクは
要求される燃料のすべてを吸気行程中に筒内に噴射した
場合の機関発生トルクよりも小さくなることを特徴とす
る。
Therefore, the invention according to claim 1 is a control device for a direct injection spark ignition type internal combustion engine, which performs a substratified combustion by forming a substratified mixture in a predetermined operating region. In the high rotation speed region where the engine rotation speed exceeds the predetermined rotation speed, the sub-stratified combustion is prohibited, and in the high rotation speed region where the rotation speed of the engine exceeds the predetermined rotation speed, the engine generated torque during the sub-stratification combustion sucks all the required fuel. It is characterized in that it becomes smaller than the engine generated torque when the fuel is injected into the cylinder during the stroke.

【0008】請求項2に係る発明は、燃焼室の手前の吸
気通路内に燃料を噴射する吸気部燃料噴射弁を備え、該
吸気部燃料噴射弁によって、要求される燃料の一部を排
気行程中に噴射して燃焼室全体にリーンな混合気を形成
し、残りの燃料を圧縮行程中に筒内に直接噴射すること
で亜成層燃焼を行うこと特徴とする。
The invention according to claim 2 is provided with an intake portion fuel injection valve for injecting fuel into the intake passage in front of the combustion chamber, and a part of the required fuel is exhausted by the intake portion fuel injection valve. It is characterized by performing a sub-stratified combustion by injecting into the inside of the cylinder to form a lean mixture and injecting the remaining fuel directly into the cylinder during the compression stroke.

【0009】請求項3に係る発明は、吸気行程中に、要
求される燃料の一部を直接筒内に噴射して燃焼室全体に
リーンな混合気を形成し、残りの燃料を圧縮行程中に筒
内に直接噴射することで亜成層燃焼を行うことを特徴と
する。
According to the third aspect of the invention, during the intake stroke, a portion of the required fuel is directly injected into the cylinder to form a lean mixture in the entire combustion chamber, and the remaining fuel is compressed during the compression stroke. It is characterized by performing sub-stratified combustion by directly injecting into the cylinder.

【0010】請求項4に係る発明は、前記所定の回転速
度は、燃料のオクタン価が高いほど高回転速度側に設定
されることを特徴とする。
The invention according to claim 4 is characterized in that the predetermined rotation speed is set to a higher rotation speed side as the octane number of the fuel is higher.

【0011】[0011]

【発明の効果】請求項1に係る発明によれば、亜成層化
運転時の機関発生トルクが、要求される燃料のすべてを
吸気行程中に筒内に直接噴射した場合の機関発生トルク
を下回るようになる回転速度領域においては亜成層化運
転を禁止するようにしたので、ノック改善制御を効果的
に活用することができ、また、ノック改善制御を行うこ
とによるトルク低下を確実に防止することができる。
According to the first aspect of the present invention, the engine generated torque during the substratified operation is lower than the engine generated torque when all the required fuel is directly injected into the cylinder during the intake stroke. Since the sub-stratification operation is prohibited in the rotation speed range where it becomes like this, the knock improvement control can be effectively utilized, and the torque reduction due to the knock improvement control can be surely prevented. You can

【0012】特に、高負荷領域においては、ノックの発
生しやすい低・中回転領域にあるときにのみノック改善
制御を行うことで、ノックの発生の抑制及びトルク向上
といったノック改善制御の有利な効果を確実に得ること
ができる。請求項2に係る発明によれば、要求される燃
料の一部を、吸気部燃料噴射弁にて排気行程中に吸気通
路中に噴射し、残りの燃料を圧縮行程中に筒内に直接噴
射するので、確実に燃焼室全体にリーンな混合気を形成
することができ亜成層化を行うことができる。
Particularly, in the high load region, the knock improvement control is performed only in the low / middle rotation region where knock is likely to occur, so that advantageous effects of knock improvement control such as suppression of knock generation and torque improvement are achieved. Can be surely obtained. According to the second aspect of the present invention, a part of the required fuel is injected into the intake passage by the intake fuel injection valve during the exhaust stroke, and the remaining fuel is directly injected into the cylinder during the compression stroke. As a result, a lean air-fuel mixture can be reliably formed in the entire combustion chamber and substratification can be performed.

【0013】請求項3に係る発明によれば、燃焼室全体
にリーンな混合気を形成するために、別に燃料噴射弁を
設けることなく、1つの筒内直噴燃料噴射弁によりノッ
ク改善制御を行うことができ、かかる機関において確実
にノック改善効果を活用できる。請求項4に係る発明に
よれば、オクタン価の違う燃料に対してノック改善効果
を最大限活用することができる。
According to the third aspect of the present invention, in order to form a lean air-fuel mixture in the entire combustion chamber, knock improvement control is performed by one in-cylinder direct injection fuel injection valve without providing a separate fuel injection valve. Can be carried out, and the knock improvement effect can be surely utilized in such an organization. According to the invention of claim 4, the knock improving effect can be maximized for fuels having different octane numbers.

【0014】[0014]

【発明の実施の形態】以下、本発明の実施形態を図に基
づいて説明する。図1に示すシステム図において、機関
(エンジン)の燃焼室1は、シリンダヘッド2、シリン
ダブロック3及びピストン4により画成されており、該
燃焼室1には吸気通路5及び排気通路6が接続されてい
る。
BEST MODE FOR CARRYING OUT THE INVENTION Embodiments of the present invention will be described below with reference to the drawings. In the system diagram shown in FIG. 1, a combustion chamber 1 of an engine is defined by a cylinder head 2, a cylinder block 3 and a piston 4, and an intake passage 5 and an exhaust passage 6 are connected to the combustion chamber 1. Has been done.

【0015】吸気通路5の燃焼室1側の開口端には、図
示しない吸気カムによって開閉駆動される吸気弁7が設
けられ、排気通路6の燃焼室1側の開口端には、図示し
ない排気カムによって開閉駆動される排気弁8が設けら
れている。吸気通路5には、吸入空気量Qaを検出する
エアフローメータ9、吸入空気量Qaを制御するスロッ
トル弁10、吸気部燃料噴射弁11が設けられており、
吸気部燃料噴射弁11は燃料を燃焼室1手前の吸気通路
5内に噴射する。
An intake valve 7 that is opened and closed by an intake cam (not shown) is provided at the open end of the intake passage 5 on the combustion chamber 1 side, and an exhaust valve (not shown) at the open end of the exhaust passage 6 on the combustion chamber 1 side is provided. An exhaust valve 8 that is opened and closed by a cam is provided. The intake passage 5 is provided with an air flow meter 9 for detecting the intake air amount Qa, a throttle valve 10 for controlling the intake air amount Qa, and an intake fuel injection valve 11.
The intake fuel injection valve 11 injects fuel into the intake passage 5 in front of the combustion chamber 1.

【0016】シリンダヘッド2の吸気通路5下方には、
燃焼室1内に燃料を噴射する筒内直噴燃料噴射弁12が
設けられており、点火プラグ13は、燃焼室1の略中央
部を臨んで配設されている。前記吸気部燃料噴射弁11
及び筒内直噴燃料噴射弁12は、エンジンコントロール
ユニット(ECU)14からの駆動信号により開弁し、
その開弁時間が制御されて所定量の燃料を噴射する。
Below the intake passage 5 of the cylinder head 2,
An in-cylinder direct injection fuel injection valve 12 for injecting fuel is provided in the combustion chamber 1, and the ignition plug 13 is arranged so as to face a substantially central portion of the combustion chamber 1. The intake portion fuel injection valve 11
The in-cylinder direct injection fuel injection valve 12 is opened by a drive signal from the engine control unit (ECU) 14,
The valve opening time is controlled to inject a predetermined amount of fuel.

【0017】排気行程中に吸気部燃料噴射弁11により
燃料を噴射した場合、噴射された燃料は燃焼室1内に拡
散して均質な混合気が形成される。また、圧縮行程中に
筒内直噴燃料噴射弁12にて燃料を噴射した場合、点火
プラグ13近傍に集中的な混合気を形成される。従っ
て、要求される燃料の一部を吸気部燃料噴射弁11にて
排気行程中に噴射し、残りの燃料を筒内直噴燃料噴射弁
12にて圧縮行程中に噴射することで亜成層燃焼を行う
ことができる。
When fuel is injected by the intake fuel injection valve 11 during the exhaust stroke, the injected fuel diffuses into the combustion chamber 1 to form a homogeneous mixture. When fuel is injected by the in-cylinder direct injection fuel injection valve 12 during the compression stroke, a concentrated air-fuel mixture is formed in the vicinity of the spark plug 13. Therefore, a part of the required fuel is injected by the intake fuel injection valve 11 during the exhaust stroke, and the remaining fuel is injected by the in-cylinder direct injection fuel injection valve 12 during the compression stroke, whereby the substratified combustion is performed. It can be performed.

【0018】一方、要求される燃料のすべてを筒内直噴
燃料噴射弁12にて、吸気行程中に噴射し点火すること
で均質燃焼を、また、圧縮行程中の噴射し点火すること
で成層燃焼を行うこともできる。エンジンの排気は、排
気弁8を介して燃焼室1から排気通路6に排出され、図
示しない排気浄化触媒を介して大気中へ排出される。
On the other hand, the in-cylinder direct injection fuel injection valve 12 injects and ignites all of the required fuel during the intake stroke for homogeneous combustion, and the injection and ignition during the compression stroke for stratification. It is also possible to carry out combustion. Exhaust gas of the engine is discharged from the combustion chamber 1 to the exhaust passage 6 via the exhaust valve 8 and is discharged into the atmosphere via an exhaust purification catalyst (not shown).

【0019】ECU14には、吸入空気量Qaを検出す
るエアフローメータ9、クランク軸の回転角位置を検出
するクランク角センサ15、エンジン冷却水温度Twを
検出する水温センサ16、アクセル開度ACCを検出す
るアクセル開度センサ17、図示しない空燃比センサ等
からの信号が入力される。なお、エンジンの回転速度N
eは、クランク角センサ15からの信号に基づいて算出
される。
The ECU 14 detects an air flow meter 9 for detecting the intake air amount Qa, a crank angle sensor 15 for detecting the rotational angle position of the crankshaft, a water temperature sensor 16 for detecting the engine cooling water temperature Tw, and an accelerator opening degree ACC. Signals from the accelerator opening sensor 17, an air-fuel ratio sensor (not shown), etc. are input. The engine speed N
e is calculated based on the signal from the crank angle sensor 15.

【0020】そして、ECU14は、これらの入力され
た信号に基づいて所定の演算処理を行って、スロットル
弁10のスロットル開度制御、吸気部燃料噴射弁11及
び筒内直噴燃料噴射弁12による燃料噴射量及び噴射時
期制御、点火プラグ13による点火時期制御等を行う。
なお、本エンジンの燃焼方式としては、ノックが発生す
るおそれがない低、中負荷領域においては、空燃比制御
との組み合わせで、成層リーン燃焼(目標空燃比tA/
Fが40程度)、均質リーン燃焼(目標空燃比tA/F
が20〜30程度)、均質ストイキ燃焼があり、エンジ
ン運転条件(エンジン回転速度Ne、目標エンジントル
クtT)に従っていずれかの燃焼方式(及び目標空燃比
tA/F)を設定できる。
Then, the ECU 14 performs predetermined arithmetic processing based on these input signals to control the throttle opening of the throttle valve 10, the intake portion fuel injection valve 11 and the in-cylinder direct injection fuel injection valve 12. The fuel injection amount and injection timing control, the ignition timing control by the spark plug 13 and the like are performed.
As a combustion method of this engine, in the low and medium load regions where knock does not occur, in combination with air-fuel ratio control, stratified lean combustion (target air-fuel ratio tA /
F is about 40), homogeneous lean combustion (target air-fuel ratio tA / F)
Is about 20 to 30), there is homogeneous stoichiometric combustion, and either combustion method (and target air-fuel ratio tA / F) can be set according to engine operating conditions (engine rotation speed Ne, target engine torque tT).

【0021】また、ノックが発生するおそれのある高負
荷領域においては、要求される燃料を分割して燃料を噴
射し、燃焼室1内の混合気を亜成層化してノックの発生
を抑制するノック改善制御を行うが、エンジン回転速度
が所定の回転速度を超えるときは、ノック改善制御を禁
止している(すなわち、高負荷・低、中回転領域でのみ
ノック改善制御を行う)。
In a high load region where knock may occur, the required fuel is divided and the fuel is injected, and the air-fuel mixture in the combustion chamber 1 is sub-stratified to suppress the knock. The improvement control is performed, but when the engine rotation speed exceeds a predetermined rotation speed, the knock improvement control is prohibited (that is, the knock improvement control is performed only in the high load / low / medium rotation range).

【0022】具体的には、前記吸気部燃料噴射弁11に
より排気行程中に燃料の一部を噴射(以下、排気行程噴
射とする)して燃焼室1全体にリーンな混合気を形成す
ると共に、残りの燃料を前記筒内直噴燃料噴射弁12に
より圧縮行程中に噴射(以下、圧縮行程噴射とする)し
て燃焼室1内に亜成層混合気を形成することにより、エ
ンドガス部をリーン化してノックの発生を抑制する。
Specifically, part of the fuel is injected by the intake fuel injection valve 11 during the exhaust stroke (hereinafter referred to as exhaust stroke injection) to form a lean mixture in the entire combustion chamber 1. By injecting the remaining fuel by the in-cylinder direct injection fuel injection valve 12 during the compression stroke (hereinafter referred to as compression stroke injection) to form a sub-stratified mixture in the combustion chamber 1, the end gas portion becomes lean. Suppresses the occurrence of knock.

【0023】なお、上記ノック改善制御における燃料噴
射量(すなわち、要求燃料量tQf)は、排気行程噴射
による燃料と圧縮行程噴射による燃料のトータル燃料量
であるが、全体としての空燃比が理論空燃比又は若干リ
ッチな混合気(例えば、目標空燃比tA/Fが12〜1
4.7)が形成されるように設定される。以下、本実施
形態に係るノック改善制御について説明する。
The fuel injection amount in the knock improvement control (that is, the required fuel amount tQf) is the total fuel amount of the fuel by the exhaust stroke injection and the fuel by the compression stroke injection. Fuel ratio or a slightly rich air-fuel mixture (for example, the target air-fuel ratio tA / F is 12 to 1
4.7) is set. The knock improvement control according to the present embodiment will be described below.

【0024】図2は、ノック改善制御を示すフローチャ
ートである。ステップ1(図ではS1と記す。以下同
様)では、吸入空気量Qa、エンジン回転速度Ne、目
標エンジントルクtTを読み込む。ステップ2では、現
在のエンジン運転条件がノック改善制御を行う負荷(ず
なわち、高負荷領域)にあるか否かを判断する。
FIG. 2 is a flowchart showing knock improvement control. In step 1 (denoted as S1 in the figure; the same applies hereinafter), the intake air amount Qa, the engine rotation speed Ne, and the target engine torque tT are read. In step 2, it is determined whether or not the current engine operating condition is in a load (that is, a high load region) for performing knock improvement control.

【0025】エンジン運転条件が高負荷領域にあればス
テップ3に進み、高負荷領域でなければ本制御を終了
し、運転条件に応じて成層燃焼又は均質燃焼である通常
の制御を行う。ステップ3では、エンジン回転速度Ne
がノック改善制御を行うことによりトルク改善効果につ
いても得ることができる所定の回転速度Ns以下である
か否かを判断する。
If the engine operating condition is in the high load region, the routine proceeds to step 3. If it is not in the high load region, this control is terminated and normal control of stratified combustion or homogeneous combustion is performed according to the operating condition. In step 3, the engine speed Ne
Performs a knock improvement control to determine whether the rotation speed is equal to or lower than a predetermined rotation speed Ns that can also obtain the torque improvement effect.

【0026】エンジン回転速度Neが所定の回転速度N
s以下であれば、ステップ4に進み、所定の回転速度N
sを超えていれば本制御を終了し、運転条件に応じて成
層燃焼又は均質燃焼である通常の制御を行う。なお、こ
こで言うトルク改善効果とは、同一のエンジン回転速度
のもとで、要求される燃料のすべてを吸気行程中に直接
筒内に噴射した場合のエンジン発生トルクよりも前記ノ
ック改善制御を行った場合のエンジン発生トルクの方が
大きくなることを意味する。
The engine rotation speed Ne is the predetermined rotation speed N.
If s or less, the process proceeds to step 4 and the predetermined rotation speed N
If it exceeds s, this control is terminated, and normal control that is stratified combustion or homogeneous combustion is performed according to operating conditions. The torque improving effect referred to here means the knock improving control rather than the engine generated torque when all the required fuel is directly injected into the cylinder during the intake stroke under the same engine rotation speed. It means that the torque generated by the engine becomes larger when it is performed.

【0027】前述したように、前記ノック改善制御を行
うことでノック限界点火時期を進角側にすることができ
るため、点火時期を進角させてエンジン発生トルクを増
大させることができる。しかし、エンジン回転速度Ne
が所定の回転速度Nsを超えると、点火時期を進角させ
ることによるトルクの増加分よりも、燃料の一部を圧縮
行程中に噴射するため筒内直噴の特徴である気化潜熱の
有効利用が目減りすることによるトルク減少(吸入空気
量の減少)分の方が大きくなってしまうといった問題が
ある。
As described above, since the knock limit ignition timing can be advanced by performing the knock improvement control, it is possible to advance the ignition timing and increase the engine generated torque. However, the engine speed Ne
Exceeds a predetermined rotation speed Ns, a portion of the fuel is injected during the compression stroke rather than the increase in the torque due to the advance of the ignition timing, so that the effective use of the latent heat of vaporization, which is the characteristic of the direct cylinder injection, is performed. However, there is a problem that the torque reduction (reduction in intake air amount) due to the decrease in the torque becomes larger.

【0028】また、高回転領域では中・低回転領域に比
べてノックの発生の心配が少ない。このため、エンジン
回転速度Neが所定の回転速度Ns以下のときのみノッ
ク改善制御を行うようにし、所定の回転速度Nsを超え
るときはノック改善制御を禁止することにしている。こ
こで、前記所定の回転速度Nsはあらかじめ実験等によ
り求めた値が設定されているが、燃料のオクタン価に応
じて異なる値を設定するようにしてもよい。この場合、
例えばハイオクガソリン使用時よりもレギュラーガソリ
ン使用時の方が高い回転速度に設定される。
Further, in the high rotation region, there is less fear of knocking as compared with the middle / low rotation region. Therefore, the knock improvement control is performed only when the engine rotation speed Ne is equal to or lower than the predetermined rotation speed Ns, and the knock improvement control is prohibited when the engine rotation speed Ne exceeds the predetermined rotation speed Ns. Here, the predetermined rotation speed Ns is set to a value obtained in advance by experiments or the like, but a different value may be set depending on the octane number of the fuel. in this case,
For example, the rotation speed is set higher when regular gasoline is used than when high-octane gasoline is used.

【0029】ステップ4は、目標空燃比tA/F、吸入
空気量Qaに基づいて要求燃料噴射量tQfを、例えば
あらかじめ設定されたマップを参照して算出する。な
お、上述したように、分割燃料噴射の(全体としての)
出力空燃比tA/Fは理論空燃比又は若干リッチにあら
かじめ設定されており(A/Fが12〜14.3)、要
求燃料噴射量tQfは排気行程噴射で噴射する燃料量
(排気行程噴射燃料量)Qeと圧縮行程噴射で噴射する
燃料量(圧縮行程噴射燃料量)Qpとの合計として算出
される。
In step 4, the required fuel injection amount tQf is calculated based on the target air-fuel ratio tA / F and the intake air amount Qa, for example, by referring to a preset map. As described above, the split fuel injection (as a whole)
The output air-fuel ratio tA / F is preset to the stoichiometric air-fuel ratio or slightly rich (A / F is 12 to 14.3), and the required fuel injection amount tQf is the fuel amount injected in the exhaust stroke injection (exhaust stroke injected fuel Amount Qe and the amount of fuel injected in the compression stroke injection (compression stroke injected fuel quantity) Qp.

【0030】ステップ5では、排気行程噴射燃料量Qe
と圧縮行程噴射燃料量Qpを、図3に示すテーブル(エ
ンジン回転速度Ne―吸気噴射燃料量の比率KPAR
T)を参照して設定する。最適な燃料比率は仕様等によ
って異なり、ピストン形状あるいはガス流動の強さ等に
より変化する値である。本実施形態では、エンジン回転
速度Neが1000rpmのときは、排気行程噴射燃料
量Qeと圧程行程噴射燃料量Qpの比率が5:5程度、
エンジン回転速度Neが2000rpmのときはQeと
Qpの比率が4:6程度、エンジン回転速度Neが30
00rpmのときはQeとQpの比率が3:7程度とな
るようにしている。
In step 5, the exhaust stroke injection fuel amount Qe
And the compression stroke injection fuel quantity Qp are shown in the table (engine rotation speed Ne-intake injection fuel quantity ratio KPAR
Set it by referring to T). The optimum fuel ratio varies depending on the specifications and the like, and is a value that changes depending on the piston shape or the strength of gas flow. In the present embodiment, when the engine rotation speed Ne is 1000 rpm, the ratio of the exhaust stroke injection fuel amount Qe and the stroke stroke injection fuel amount Qp is about 5: 5,
When the engine speed Ne is 2000 rpm, the ratio of Qe and Qp is about 4: 6, and the engine speed Ne is 30.
At 00 rpm, the ratio of Qe and Qp is about 3: 7.

【0031】ステップ6では、排気行程噴射終了時期を
設定し、ステップ7では、所定のタイミングで吸気行程
噴射を実行する。例えば、図5(A)に示すように、噴
射終了時期(すなわち、閉弁時期)が30°〜50°B
TDC(排気上死点前30°〜50°のクランク角位
置)となるように吸気部燃料噴射弁11を制御してステ
ップ5で設定した排気行程噴射燃料量Qeを噴射する。
In step 6, the exhaust stroke injection end timing is set, and in step 7, the intake stroke injection is executed at a predetermined timing. For example, as shown in FIG. 5A, the injection end timing (that is, the valve closing timing) is 30 ° to 50 ° B.
The intake-portion fuel injection valve 11 is controlled so as to reach TDC (the crank angle position of 30 ° to 50 ° before exhaust top dead center), and the exhaust stroke injection fuel amount Qe set in step 5 is injected.

【0032】なお、このように排気行程噴射を噴射終了
時期制御とするのは、確実かつ十分に燃料を気化させて
筒内に均質でリーンな混合気を形成するためである。ス
テップ8では、圧縮行程噴射開始タイミングを、図4に
示すようなテーブル(エンジン回転速度Ne―噴射開始
タイミングITCOMP)を参照して設定する。
Incidentally, the reason why the exhaust stroke injection is controlled as the injection end timing in this way is to surely and sufficiently vaporize the fuel to form a homogeneous and lean air-fuel mixture in the cylinder. In step 8, the compression stroke injection start timing is set with reference to the table (engine speed Ne-injection start timing ITCOMP) as shown in FIG.

【0033】最適な噴射開始時期は仕様等により異なる
が、本実施形態では、噴射開始タイミングITCOMP
を、エンジン回転速度Neが1000rpmのときは2
60°ATDC(圧縮上死点後260°のクランク角位
置)程度、エンジン回転速度Neが2000rpmのと
きは220°ATDC程度、エンジン回転速度Neが3
000rpmのときは200°ATDC程度に設定して
いる。
Although the optimum injection start timing varies depending on the specifications and the like, in this embodiment, the injection start timing ITCOMP
2 when the engine speed Ne is 1000 rpm
About 60 ° ATDC (crank angle position of 260 ° after compression top dead center), about 220 ° ATDC when the engine speed Ne is 2000 rpm, and the engine speed Ne is 3
At 000 rpm, it is set to about 200 ° ATDC.

【0034】ステップ9では、圧縮行程噴射を実行す
る。すなわち、図5(A)に示すように、噴射開始時期
が(すなわち、開弁時期)をステップ8で設定した噴射
開始タイミングITCOMPとなるように筒内直噴燃料
噴射弁12を制御して、ステップ5で設定した圧縮行程
噴射燃料量Qpを噴射する。なお、このように圧縮行程
噴射を噴射開始時期制御とするのは、過渡時に噴射時期
の決定を最大限遅らせることができ、ノック改善制御を
効果的に行えるからである。
In step 9, compression stroke injection is executed. That is, as shown in FIG. 5 (A), the in-cylinder direct injection fuel injection valve 12 is controlled so that the injection start timing (that is, the valve opening timing) becomes the injection start timing ITCOMP set in step 8. The compression stroke injection fuel amount Qp set in step 5 is injected. The reason why the compression stroke injection is controlled as the injection start timing is that the determination of the injection timing can be delayed as much as possible during the transition, and the knock improvement control can be effectively performed.

【0035】以上のように、燃料を排気行程と圧縮行程
とで分割噴射し、混合気を亜成層化してノック改善制御
を行うに際し、エンジン回転速度Neがノック改善制御
によってトルク改善効果も得られる回転速度(すなわ
ち、前記所定の回転速度Ns)以下であるか否かを判断
し、所定の回転速度Ns以下のときにのみに実行し、所
定の回転速度Nsを超えるときは禁止するので、高回転
領域におけるトルク低下を確実に防止すると共に、低・
中回転領域においては、ノック及びトルクの改善を効果
的に行うことができる。
As described above, when the fuel is split and injected in the exhaust stroke and the compression stroke, and the air-fuel mixture is substratified to perform knock improvement control, the engine speed Ne is also improved by the knock improvement control. It is determined whether or not the rotation speed is lower than the predetermined rotation speed Ns and is executed only when the rotation speed is equal to or lower than the predetermined rotation speed Ns. When the rotation speed exceeds the predetermined rotation speed Ns, it is prohibited. It surely prevents torque reduction in the rotation range and
In the middle rotation range, knock and torque can be effectively improved.

【0036】なお、以上の説明では、筒内直噴燃料噴射
弁12とは別に吸気部燃料噴射弁11を設け、これによ
り排気行程噴射を行っているが、これに限られず筒内直
噴燃料噴射弁12のみで吸気行程噴射と圧縮行程噴射を
行うタイプの機関に本発明を適用してもよい。この場合
は、図5(B)に示すように、吸気行程噴射、圧縮行程
噴射共に噴射開始時期制御とする。例えば、吸気行程噴
射開始時期が20〜50°ATDC程度になるように筒
内直噴燃料噴射弁12を制御する。このときのフローチ
ャートを図7に示す。図中のステップで図2のフローチ
ャートと同じものは図2と同じ番号としている。図7に
おいて、ステップ5'では、吸気行程噴射燃料量Qiを
演算しおり、ステップ6'では、吸気行程噴射開始時期
を設定している。
In the above description, the intake portion fuel injection valve 11 is provided separately from the in-cylinder direct injection fuel injection valve 12 to perform the exhaust stroke injection. However, the present invention is not limited to this. The present invention may be applied to an engine of a type in which the intake stroke injection and the compression stroke injection are performed only by the injection valve 12. In this case, as shown in FIG. 5B, the injection start timing control is performed for both the intake stroke injection and the compression stroke injection. For example, the in-cylinder direct injection fuel injection valve 12 is controlled so that the intake stroke injection start timing is about 20 to 50 ° ATDC. The flowchart at this time is shown in FIG. Steps in the figure that are the same as those in the flowchart in FIG. 2 are given the same numbers as in FIG. In FIG. 7, in step 5 ′, the intake stroke injection fuel amount Qi is calculated, and in step 6 ′, the intake stroke injection start timing is set.

【0037】ステップ7'では、ステップ5'で演算され
た吸気行程噴射燃料量Qiを噴射し、圧縮行程噴射につ
いては、図2におけるステップ8、9と同様に行う。ま
た、上記実施形態のように吸気行程噴射を行わず、要求
された燃料のすべてを圧縮行程中に直接筒内に噴射し
て、混合気を成層化することによってもエンドガス部に
燃料がほとんど存在しなくなるのでノックの発生を抑制
できる。このように混合気を成層化してノック改善制御
を行うタイプの内燃機関においても、エンジン回転速度
が所定の回転速度以下の低、中回転領域でのみノック改
善制御を行うようにして高回転領域ではノック改善制御
(混合気の成層化)を禁止することにより、上記実施形
態の場合と同様にノック改善制御を効果的に活用でき
る。
In step 7 ', the intake stroke injection fuel amount Qi calculated in step 5'is injected, and the compression stroke injection is performed in the same manner as in steps 8 and 9 in FIG. Further, almost no fuel exists in the end gas portion by stratifying the air-fuel mixture by injecting all of the requested fuel directly into the cylinder during the compression stroke without performing the intake stroke injection as in the above embodiment. Since it does not occur, knocking can be suppressed. Even in an internal combustion engine of a type in which the air-fuel mixture is stratified to perform knock improvement control, the engine rotation speed is equal to or lower than a predetermined rotation speed. By prohibiting knock improvement control (stratification of the air-fuel mixture), knock improvement control can be effectively utilized as in the case of the above embodiment.

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

【図1】本発明の実施形態を示すシステム図。FIG. 1 is a system diagram showing an embodiment of the present invention.

【図2】一実施形態に係るノック改善制御を示すフロー
チャート。
FIG. 2 is a flowchart showing knock improvement control according to an embodiment.

【図3】亜成層運転時の吸気行程で噴射する燃料比率算
出用のテーブルの一例を示す図。
FIG. 3 is a diagram showing an example of a table for calculating a fuel ratio to be injected in an intake stroke during substratified operation.

【図4】亜成層運転時の圧縮行程噴射の噴射開始タイミ
ング算出用のテーブルの一例を示す図。
FIG. 4 is a diagram showing an example of a table for calculating injection start timing of compression stroke injection during substratified operation.

【図5】亜成層運転時の燃料噴射時期を示すタイミング
チャート(A:吸気部燃料噴射弁と筒内直噴燃料噴射弁
とを併用した場合、B:筒内直噴燃料噴射弁のみで行う
場合)。
FIG. 5 is a timing chart showing fuel injection timing during substratified operation (A: when an intake portion fuel injection valve and an in-cylinder direct injection fuel injection valve are used together, B: only an in-cylinder direct injection fuel injection valve is used. If).

【図6】点火時期と機関発生トルクの関係を示す図
(A:低回転領域、B:高回転領域)。
FIG. 6 is a diagram showing a relationship between ignition timing and engine generated torque (A: low rotation range, B: high rotation range).

【図7】他の実施形態に係るノック改善制御を示すフロ
ーチャート。
FIG. 7 is a flowchart showing knock improvement control according to another embodiment.

【符号の説明】[Explanation of symbols]

1 燃焼室 2 シリンダヘッド 3 シリンダブロック 11 吸気部燃料噴射弁 12 筒内直噴燃料噴射弁 13 点火プラグ 14 エンジンコントロールユニット(ECU) 15 クランク角センサ 16 水温センサ 17 アクセル開度センサ 1 combustion chamber 2 cylinder head 3 cylinder block 11 Intake fuel injection valve 12 In-cylinder direct injection fuel injection valve 13 Spark plug 14 Engine control unit (ECU) 15 Crank angle sensor 16 Water temperature sensor 17 Accelerator position sensor

フロントページの続き (51)Int.Cl.7 識別記号 FI テーマコート゛(参考) F02D 41/02 F02D 41/02 330F Front page continuation (51) Int.Cl. 7 Identification code FI theme code (reference) F02D 41/02 F02D 41/02 330F

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】所定の運転領域にて、亜成層化混合気を形
成し亜成層燃焼を行う直噴火花点火式内燃機関の制御装
置において、 機関の回転速度が所定回転速度を超える高回転領域では
亜成層燃焼を禁止し、 前記所定回転速度を超える高回転領域では、亜成層燃焼
時の機関発生トルクは要求される燃料のすべてを吸気行
程中に筒内に噴射した場合の機関発生トルクよりも小さ
くなることを特徴とする直噴火花点火式内燃機関の制御
装置。
1. A controller for a direct injection spark ignition type internal combustion engine which forms a sub-stratified air-fuel mixture and performs sub-stratified combustion in a predetermined operating region, in a high rotation region where the rotational speed of the engine exceeds a predetermined rotational speed. In sub-stratified combustion is prohibited in the above, the engine generated torque during sub-stratified combustion is higher than the engine generated torque when injecting all of the required fuel into the cylinder during the intake stroke in the high rotation speed range exceeding the predetermined rotation speed. A control device for a direct injection spark ignition type internal combustion engine, characterized in that
【請求項2】燃焼室の手前の吸気通路内に燃料を噴射す
る吸気部燃料噴射弁を備え、 該吸気部燃料噴射弁によって、要求される燃料の一部を
排気行程中に噴射して燃焼室全体にリーンな混合気を形
成し、 残りの燃料を圧縮行程中に筒内に直接噴射することで亜
成層燃焼を行うこと特徴とする請求項1記載の直噴火花
点火式内燃機関の制御装置。
2. An intake-portion fuel injection valve for injecting fuel into an intake passage in front of a combustion chamber, wherein the intake-portion fuel injection valve injects a portion of required fuel during an exhaust stroke to burn the fuel. The control of a direct injection spark ignition type internal combustion engine according to claim 1, wherein a lean air-fuel mixture is formed in the entire chamber and the remaining fuel is directly injected into the cylinder during the compression stroke to perform substratified combustion. apparatus.
【請求項3】吸気行程中に、要求される燃料の一部を直
接筒内に噴射して燃焼室全体にリーンな混合気を形成
し、 残りの燃料を圧縮行程中に筒内に直接噴射することで亜
成層燃焼を行うことを特徴とする請求項1記載の直噴火
花点火式内燃機関の制御装置。
3. A part of required fuel is directly injected into the cylinder during the intake stroke to form a lean mixture in the entire combustion chamber, and the remaining fuel is directly injected into the cylinder during the compression stroke. The control device for a direct injection spark ignition type internal combustion engine according to claim 1, wherein the sub-stratified combustion is performed.
【請求項4】前記所定の回転速度は、燃料のオクタン価
が高いほど高回転速度側に設定されることを特徴とする
請求項1から請求項3のいずれか1つに記載の直噴火花
点火式内燃機関の制御装置。
4. The direct injection spark ignition according to any one of claims 1 to 3, wherein the predetermined rotation speed is set to a higher rotation speed side as the octane number of the fuel is higher. Control device for internal combustion engine.
JP2001197403A 2001-06-28 2001-06-28 Control device for direct injection spark ignition type internal combustion engine Pending JP2003013785A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
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Application Number Priority Date Filing Date Title
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