[go: up one dir, main page]

JP2012117428A - Fuel injection control device - Google Patents

Fuel injection control device Download PDF

Info

Publication number
JP2012117428A
JP2012117428A JP2010266877A JP2010266877A JP2012117428A JP 2012117428 A JP2012117428 A JP 2012117428A JP 2010266877 A JP2010266877 A JP 2010266877A JP 2010266877 A JP2010266877 A JP 2010266877A JP 2012117428 A JP2012117428 A JP 2012117428A
Authority
JP
Japan
Prior art keywords
cylinder
fuel injection
amount
heat generation
target
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2010266877A
Other languages
Japanese (ja)
Other versions
JP5707901B2 (en
Inventor
Yasuhiro Nishiyama
康宏 西山
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.)
Isuzu Motors Ltd
Original Assignee
Isuzu Motors 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 Isuzu Motors Ltd filed Critical Isuzu Motors Ltd
Priority to JP2010266877A priority Critical patent/JP5707901B2/en
Publication of JP2012117428A publication Critical patent/JP2012117428A/en
Application granted granted Critical
Publication of JP5707901B2 publication Critical patent/JP5707901B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)

Abstract

【課題】燃料噴射弁の特性変化に対応でき、ドリフトがなく、マルチ噴射でも効果的な補正ができる燃料噴射制御装置を提供する。
【解決手段】筒内圧力データ列を基にして熱発生率を演算し、積分することによりパイロット噴射による熱発生量を演算し、パイロット噴射による目標熱発生量を設定し、各気筒における熱発生量と目標熱発生量との差が小さくなるように各気筒のパイロット噴射の燃料噴射量をそれぞれ補正し、筒内圧力データ列を基にして図示平均有効圧力を演算し、全気筒で平均して図示平均有効圧力平均値を演算し、各気筒における図示平均有効圧力と全気筒の図示平均有効圧力平均値との差が小さくなるように各気筒のメイン噴射の燃料噴射量をそれぞれ補正する。
【選択図】図1
A fuel injection control apparatus that can cope with a change in characteristics of a fuel injection valve, has no drift, and can be effectively corrected even with multi-injection.
A heat generation rate is calculated based on an in-cylinder pressure data string, and a heat generation amount by pilot injection is calculated by integration, a target heat generation amount by pilot injection is set, and heat generation in each cylinder is performed. The fuel injection amount of pilot injection in each cylinder is corrected so that the difference between the amount and the target heat generation amount is small, the indicated mean effective pressure is calculated based on the in-cylinder pressure data sequence, and averaged for all cylinders. Then, the indicated mean effective pressure average value is calculated, and the fuel injection amount of the main injection in each cylinder is corrected so that the difference between the indicated mean effective pressure in each cylinder and the indicated mean effective pressure average value of all the cylinders is reduced.
[Selection] Figure 1

Description

本発明は、燃料噴射弁の特性変化に対応でき、ドリフトがなく、マルチ噴射でも効果的な補正ができる燃料噴射制御装置に関する。   The present invention relates to a fuel injection control apparatus that can cope with a change in characteristics of a fuel injection valve, has no drift, and can effectively correct even multi-injection.

エンジンには複数の気筒があり、各気筒に燃料噴射弁が設けられる。各気筒における1回の噴射の燃料噴射量は燃料噴射弁の駆動時間幅に依存する。目標とする燃料噴射量は、エンジン状態で参照されるマップにより求められ、これに応じて燃料噴射弁に与える駆動時間幅が決められる。しかし、燃料噴射弁には機械的公差(例えば、噴射口面積の公差)があるため、各気筒の燃料噴射弁を同じ駆動時間幅で駆動しても気筒ごとに燃料噴射量がばらつく。その結果、気筒ごとの燃焼状態がばらつくことになる。   The engine has a plurality of cylinders, and a fuel injection valve is provided in each cylinder. The fuel injection amount of one injection in each cylinder depends on the driving time width of the fuel injection valve. The target fuel injection amount is obtained from a map that is referred to in the engine state, and the drive time width to be given to the fuel injection valve is determined accordingly. However, since the fuel injection valve has a mechanical tolerance (for example, an injection hole area tolerance), even if the fuel injection valve of each cylinder is driven with the same driving time width, the fuel injection amount varies from cylinder to cylinder. As a result, the combustion state for each cylinder varies.

これに対し、車両の出荷前に、気筒ごとの燃料噴射量特性(=燃料噴射弁の特性)を調べてマップに設定しておき、そのマップを参照して気筒ごとの駆動時間幅を決めることで燃料噴射量のばらつきを補正することが行われている。   On the other hand, before the vehicle is shipped, the fuel injection amount characteristics (= characteristics of the fuel injection valve) for each cylinder are checked and set in a map, and the driving time width for each cylinder is determined with reference to the map. Thus, the variation in the fuel injection amount is corrected.

特開2005−226631号公報JP 2005226663 A 特開2005−194893号公報JP 2005-194893 A

しかしながら、熱や経年変化により燃料噴射弁の特性が変化することがあり、車両の出荷時に設定されたマップに基づく補正では正確さが得られない。   However, the characteristics of the fuel injection valve may change due to heat or aging, and accuracy cannot be obtained by correction based on a map set at the time of vehicle shipment.

また、気筒間の燃料噴射量のばらつきを解消する方法として、各気筒における燃料噴射量が全気筒の平均値に収束するようそれぞれの気筒に補正を行うことが考えられる。しかし、全気筒の平均値が必ずしも目標燃料噴射量とは一致しないため、平均値に収束させる制御を続けるとドリフト(全体が目標からずれていくこと)が生じてしまう。   Further, as a method of eliminating the variation in the fuel injection amount between the cylinders, it is conceivable to correct each cylinder so that the fuel injection amount in each cylinder converges to the average value of all the cylinders. However, since the average value of all the cylinders does not necessarily coincide with the target fuel injection amount, if the control for converging to the average value is continued, drift (the whole shifts from the target) occurs.

また、燃料噴射の形態として、1燃焼サイクル内で目標噴射量を複数回に分割して噴射するマルチ噴射が知られている。例えば、燃焼を緩慢にさせNOxの排出量と騒音を抑制する目的でメイン噴射に先立ってパイロット噴射が行われる。しかし、1回の噴射量が小さいほど、燃料噴射弁の機械的なばらつきの影響が相対的に大きい。パイロット噴射のように非常に微少な噴射量を噴射するときは非常にばらつきが大きい。このため、マルチ噴射においては、気筒ごとの燃料噴射量のばらつきを効果的に補正することが難しい。   As a form of fuel injection, multi-injection is known in which a target injection amount is divided into a plurality of times and injected within one combustion cycle. For example, pilot injection is performed prior to main injection for the purpose of slowing combustion and suppressing NOx emissions and noise. However, the smaller the injection amount at one time, the greater the influence of mechanical variations of the fuel injection valves. When a very small injection amount is injected like pilot injection, the variation is very large. For this reason, in multi-injection, it is difficult to effectively correct the variation in the fuel injection amount for each cylinder.

そこで、本発明の目的は、上記課題を解決し、燃料噴射弁の特性変化に対応でき、ドリフトがなく、マルチ噴射でも効果的な補正ができる燃料噴射制御装置を提供することにある。   SUMMARY OF THE INVENTION Accordingly, an object of the present invention is to provide a fuel injection control device that solves the above-described problems, can cope with changes in the characteristics of the fuel injection valve, has no drift, and can effectively correct even multiple injections.

上記目的を達成するために本発明は、複数の気筒のそれぞれで筒内圧力センサが検出する筒内圧力をクランク角度センサが検出する信号に基づく一定のクランク角度間隔でサンプリングして各気筒の筒内圧力データ列を蓄えるサンプリング部と、前記筒内圧力データ列を基にして各気筒における熱発生率を所定クランク角度ごとに演算する熱発生率演算部と、熱発生率を積分することにより各気筒におけるパイロット噴射による熱発生量を演算する熱発生量演算部と、パイロット噴射による熱発生量の目標値である目標熱発生量を設定する目標熱発生量設定部と、各気筒における熱発生量と目標熱発生量との差が小さくなるように各気筒のパイロット噴射の燃料噴射量をそれぞれ補正するパイロット噴射量補正部と、前記筒内圧力データ列を基にして各気筒における図示平均有効圧力を演算する図示平均有効圧力演算部と、図示平均有効圧力を全気筒で平均して図示平均有効圧力平均値を演算する図示平均有効圧力平均値演算部と、各気筒における図示平均有効圧力と全気筒の図示平均有効圧力平均値との差が小さくなるように各気筒のメイン噴射の燃料噴射量をそれぞれ補正するメイン噴射量補正部とを備えたものである。   In order to achieve the above-mentioned object, the present invention is to sample the cylinder pressure detected by the cylinder pressure sensor in each of a plurality of cylinders at a constant crank angle interval based on a signal detected by the crank angle sensor. A sampling unit that stores an internal pressure data string, a heat generation rate calculation unit that calculates a heat generation rate in each cylinder based on the in-cylinder pressure data sequence for each predetermined crank angle, and each by integrating the heat generation rate A heat generation amount calculation unit that calculates the heat generation amount by pilot injection in the cylinder, a target heat generation amount setting unit that sets a target heat generation amount that is a target value of the heat generation amount by pilot injection, and a heat generation amount in each cylinder A pilot injection amount correction unit for correcting the fuel injection amount of the pilot injection of each cylinder so that the difference between the target pressure and the target heat generation amount is small, and the in-cylinder pressure data string An illustrated average effective pressure calculating unit that calculates an indicated average effective pressure in each cylinder, an indicated average effective pressure average value calculating unit that averages the indicated average effective pressure in all cylinders, and calculates an indicated average effective pressure average value, And a main injection amount correction unit that corrects the fuel injection amount of the main injection in each cylinder so that the difference between the indicated average effective pressure in each cylinder and the indicated average effective pressure average value in all cylinders is reduced. .

目標燃料噴射量とその目標燃料噴射量に対応する適正な図示平均有効圧力である目標図示平均有効圧力との関係が設定された目標図示平均有効圧力マップと、前記演算した図示平均有効圧力により前記目標図示平均有効圧力マップを参照して実際の燃料噴射量を推定する燃料噴射量推定部と、実際の燃料噴射量と目標燃料噴射量との差が小さくなるように全気筒の燃料噴射量を一括に補正する一括燃料噴射量補正部とを備えてもよい。   The target indicated mean effective pressure map in which the relationship between the target indicated fuel injection amount and the indicated indicated effective effective pressure corresponding to the target indicated fuel injection amount is set, and the calculated indicated indicated effective effective pressure. The fuel injection amount estimation unit that estimates the actual fuel injection amount with reference to the target indicated mean effective pressure map, and the fuel injection amounts of all cylinders so that the difference between the actual fuel injection amount and the target fuel injection amount is small. You may provide the collective fuel injection amount correction | amendment part correct | amended collectively.

吸入空気量と目標燃料噴射量に基づいて排気ガスの空燃比を推定演算する空燃比演算部と、空燃比センサにより検出される排気ガスの実空燃比と推定された空燃比との差が小さくなるように全気筒の燃料噴射量を一括に補正する一括燃料噴射量補正部とを備えてもよい。   The difference between the air-fuel ratio calculation unit that estimates the air-fuel ratio of the exhaust gas based on the intake air amount and the target fuel injection amount and the estimated air-fuel ratio detected by the air-fuel ratio sensor is small. A collective fuel injection amount correction unit that collectively corrects the fuel injection amounts of all cylinders may be provided.

本発明は次の如き優れた効果を発揮する。   The present invention exhibits the following excellent effects.

(1)燃料噴射弁の特性変化に対応して補正ができる。   (1) Correction can be made in response to changes in the characteristics of the fuel injection valve.

(2)ドリフトがなく補正ができる。   (2) Correction can be made without drift.

(3)マルチ噴射でも効果的な補正ができる。   (3) Effective correction can be performed even with multi-injection.

本発明の一実施形態を示す燃料噴射制御装置の構成図である。It is a block diagram of the fuel-injection control apparatus which shows one Embodiment of this invention. 図1の燃料噴射制御装置が適用されるエンジンシステムの構成図である。It is a block diagram of the engine system with which the fuel-injection control apparatus of FIG. 1 is applied. クランク角度に対する筒内圧力、熱発生率、熱発生量の特性図である。FIG. 5 is a characteristic diagram of in-cylinder pressure, heat generation rate, and heat generation amount with respect to a crank angle.

以下、本発明の一実施形態を添付図面に基づいて詳述する。   Hereinafter, an embodiment of the present invention will be described in detail with reference to the accompanying drawings.

図1に示されるように、本発明に係る燃料噴射制御装置1は、複数の気筒のそれぞれで筒内圧力センサ2が検出する筒内圧力をクランク角度センサ3が検出する信号に基づく一定のクランク角度間隔でサンプリングして各気筒の筒内圧力データ列を蓄えるサンプリング部4と、筒内圧力データ列を基にして各気筒における熱発生率を所定クランク角度ごとに演算する熱発生率演算部5と、熱発生率を積分することにより各気筒におけるパイロット噴射による熱発生量を演算する熱発生量演算部6と、パイロット噴射による熱発生量の目標値である目標熱発生量を設定する目標熱発生量設定部7と、各気筒における熱発生量と目標熱発生量との差が小さくなるように各気筒のパイロット噴射の燃料噴射量をそれぞれ補正するパイロット噴射量補正部8と、筒内圧力データ列を基にして各気筒における図示平均有効圧力(Indicate Mean Effective Pressure)を演算する図示平均有効圧力演算部9と、図示平均有効圧力を全気筒で平均して図示平均有効圧力平均値を演算する図示平均有効圧力平均値演算部10と、各気筒における図示平均有効圧力と全気筒の図示平均有効圧力平均値との差が小さくなるように各気筒のメイン噴射の燃料噴射量をそれぞれ補正するメイン噴射量補正部11とを備える。   As shown in FIG. 1, the fuel injection control device 1 according to the present invention has a constant crank based on a signal detected by the crank angle sensor 3 for the cylinder pressure detected by the cylinder pressure sensor 2 in each of a plurality of cylinders. A sampling unit 4 that samples at an angular interval and stores the in-cylinder pressure data sequence of each cylinder, and a heat generation rate calculation unit 5 that calculates a heat generation rate in each cylinder based on the in-cylinder pressure data sequence for each predetermined crank angle. And a heat generation amount calculation unit 6 that calculates the heat generation amount by pilot injection in each cylinder by integrating the heat generation rate, and a target heat that sets a target heat generation amount that is a target value of the heat generation amount by pilot injection. A pilot injection amount compensation that corrects the fuel injection amount of the pilot injection in each cylinder so that the difference between the heat generation amount and the target heat generation amount in each cylinder is reduced. Unit 8, an indicated mean effective pressure calculation unit 9 for calculating an indicated mean effective pressure in each cylinder based on the in-cylinder pressure data string, and an indicated average effective pressure for all cylinders. The indicated average effective pressure average value calculation unit 10 for calculating the average effective pressure average value, and the main injection of each cylinder so that the difference between the indicated average effective pressure in each cylinder and the indicated average effective pressure average value of all cylinders is reduced. And a main injection amount correction unit 11 for correcting the fuel injection amount.

本実施形態では、目標熱発生量設定部7として、熱発生量を全気筒で平均して熱発生量平均値を演算し、その熱発生量平均値を目標熱発生量とする熱発生量平均値演算部7aを用いる。したがって、パイロット噴射量補正部8では、各気筒における熱発生量と全気筒の熱発生量平均値との差が小さくなるように各気筒のパイロット噴射の燃料噴射量をそれぞれ補正することになる。   In the present embodiment, the target heat generation amount setting unit 7 calculates the heat generation amount average value by averaging the heat generation amount in all the cylinders, and uses the heat generation amount average value as the target heat generation amount. The value calculation unit 7a is used. Therefore, the pilot injection amount correction unit 8 corrects the fuel injection amount of the pilot injection in each cylinder so that the difference between the heat generation amount in each cylinder and the average heat generation amount in all cylinders becomes small.

さらに、燃料噴射制御装置1は、全気筒の燃料噴射量が目標燃料噴射量からドリフトするのを防止するために全気筒の燃料噴射量を一括に補正する一括燃料噴射量補正部12を備える。全気筒の燃料噴射量の一括補正には、図示平均有効圧力に基づく形態と排気ガスの空燃比に基づく形態がある。このために、燃料噴射制御装置1は、目標燃料噴射量とその目標燃料噴射量に対応する適正な図示平均有効圧力である目標図示平均有効圧力との関係が設定された目標図示平均有効圧力マップ13と、前記演算した図示平均有効圧力により目標図示平均有効圧力マップ13を参照して実際の燃料噴射量を推定する燃料噴射量推定部14と、吸入空気量と目標燃料噴射量に基づいて排気ガスの空燃比を推定演算する空燃比演算部15とを備える。一括燃料噴射量補正部12は、図示平均有効圧力で推定した実際の燃料噴射量と目標燃料噴射量との差が小さくなるように全気筒の燃料噴射量を一括に補正するか又は、空燃比センサにより検出される排気ガスの実空燃比と推定された空燃比との差が小さくなるように全気筒の燃料噴射量を一括に補正する。   Furthermore, the fuel injection control device 1 includes a collective fuel injection amount correction unit 12 that collectively corrects the fuel injection amounts of all cylinders in order to prevent the fuel injection amounts of all cylinders from drifting from the target fuel injection amount. The collective correction of the fuel injection amounts for all cylinders includes a mode based on the indicated mean effective pressure and a mode based on the air-fuel ratio of the exhaust gas. For this purpose, the fuel injection control device 1 sets a target indicated average effective pressure map in which a relationship between a target fuel injection amount and a target indicated average effective pressure that is an appropriate indicated average effective pressure corresponding to the target fuel injection amount is set. 13, a fuel injection amount estimation unit 14 that estimates an actual fuel injection amount with reference to the target indicated average effective pressure map 13 based on the calculated indicated average effective pressure, and exhaust based on the intake air amount and the target fuel injection amount An air-fuel ratio calculating unit 15 for estimating and calculating the air-fuel ratio of the gas. The collective fuel injection amount correction unit 12 corrects the fuel injection amounts of all the cylinders in a batch so that the difference between the actual fuel injection amount estimated by the indicated mean effective pressure and the target fuel injection amount becomes small, or the air-fuel ratio The fuel injection amounts of all the cylinders are collectively corrected so that the difference between the actual air-fuel ratio of the exhaust gas detected by the sensor and the estimated air-fuel ratio becomes small.

各部材4〜15は、電子制御装置(Electronical Control Unit;以下、ECUという)16が実行するソフトウェア及び内部のメモリで実現される。ECU16は、エンジン制御に必要な全てのエンジンパラメータ(センサ検出値、演算値、制御値など)を把握しているものとする。   Each of the members 4 to 15 is realized by software executed by an electronic control unit (hereinafter referred to as ECU) 16 and an internal memory. It is assumed that the ECU 16 knows all engine parameters (sensor detection value, calculation value, control value, etc.) necessary for engine control.

図2に示されるように、燃料噴射制御装置1が適用されるエンジンシステム201は、4気筒ディーゼルエンジン(以下、エンジン)202の排気マニホールド203に、排気ガス再循環装置(Exhaust Gas Recirculation;EGR)を構成するEGR管204と高圧側排気管205とが接続される。高圧側排気管205には、ターボチャージャ206の排気タービン207の入口が接続される。排気タービン207の出口に排気管208が接続される。排気管208には、排気ガス浄化装置209が設置される。   As shown in FIG. 2, an engine system 201 to which the fuel injection control device 1 is applied includes an exhaust gas recirculation (EGR) in an exhaust manifold 203 of a four-cylinder diesel engine (hereinafter, engine) 202. The EGR pipe 204 and the high-pressure side exhaust pipe 205 are connected. An inlet of an exhaust turbine 207 of a turbocharger 206 is connected to the high pressure side exhaust pipe 205. An exhaust pipe 208 is connected to the outlet of the exhaust turbine 207. An exhaust gas purification device 209 is installed in the exhaust pipe 208.

大気からの空気が取り込まれるエアフィルタ210には吸気管211が接続され、吸気管211の下流端はターボチャージャ206の吸気コンプレッサ212の入口に接続される。吸気コンプレッサ212の出口には高圧側吸気管213が接続される。高圧側吸気管213は、EGR管204の下流端と合流されて吸気マニホールド214に接続される。   An intake pipe 211 is connected to the air filter 210 that takes in air from the atmosphere, and the downstream end of the intake pipe 211 is connected to the inlet of the intake compressor 212 of the turbocharger 206. A high-pressure side intake pipe 213 is connected to the outlet of the intake compressor 212. The high-pressure side intake pipe 213 joins the downstream end of the EGR pipe 204 and is connected to the intake manifold 214.

エンジン202の各気筒には燃料噴射弁215が設けられる。燃料噴射弁215はコモンレール216から供給される高圧の燃料をECU16が指令する噴射時期及び噴射時間幅で気筒内に噴射を行うようになっている。   Each cylinder of the engine 202 is provided with a fuel injection valve 215. The fuel injection valve 215 injects high-pressure fuel supplied from the common rail 216 into the cylinder at an injection timing and an injection time width commanded by the ECU 16.

高圧側排気管205には、排気ガスの流れを塞いだり調節する排気スロットル217が設けられる。EGR管204には、EGRガスの流れを塞いだり調節するEGRバルブ218が設けられる。高圧側吸気管213には、吸気の流れを塞いだり調節する吸気スロットル219が設けられる。   The high-pressure side exhaust pipe 205 is provided with an exhaust throttle 217 that blocks or adjusts the flow of exhaust gas. The EGR pipe 204 is provided with an EGR valve 218 that blocks or regulates the flow of EGR gas. The high-pressure side intake pipe 213 is provided with an intake throttle 219 that blocks or regulates the flow of intake air.

エンジン202の各気筒(区別が必要なときは符号S1〜S4を付す)には筒内圧力センサ2が設けられる。図示しないクランク軸には、クランク角度5度間隔ごとの信号を出力するクランク角度センサ3が設けられる。吸気マニホールド214には、吸気圧力センサ220が設けられる。排気管208には、排気ガスの空燃比を検出するλセンサ221が設けられる。   An in-cylinder pressure sensor 2 is provided in each cylinder of the engine 202 (indicated by reference numerals S1 to S4 when distinction is necessary). A crank angle sensor 3 that outputs a signal at intervals of 5 degrees of crank angle is provided on a crankshaft (not shown). The intake manifold 214 is provided with an intake pressure sensor 220. The exhaust pipe 208 is provided with a λ sensor 221 that detects the air-fuel ratio of the exhaust gas.

以下、本発明の燃料噴射制御装置1の動作を、1.筒内圧力信号処理、2.パイロット噴射量のばらつき補正、3.メイン噴射量のばらつき補正、4.図示平均有効圧力に基づく一括補正、5.排気ガスの空燃比に基づく一括補正の順で説明する。   Hereinafter, the operation of the fuel injection control device 1 of the present invention will be described as follows. 1. In-cylinder pressure signal processing 2. Correction of variation in pilot injection amount 3. Correction of variation in main injection amount 4. Batch correction based on the indicated mean effective pressure Description will be made in the order of collective correction based on the air-fuel ratio of the exhaust gas.

1.筒内圧力信号処理
サンプリング部4は、各気筒に設置された筒内圧力センサ2からの筒内圧力信号をECU16内のメモリにデータとして取り込む。このとき、筒内圧力信号は、クランク角度センサ3からのパルス信号を元に一定クランク角度ごとにサンプリングされて筒内圧力データ列として保存される。クランク角度センサ3としては、0.1度程度の高分解能のロータリエンコーダを利用してもよいし、クランク軸に取り付けたクランクパルサと呼ばれる金属製歯車による磁束変化を電磁ピックアップやホール素子で検出する一般的なクランク角度センサを利用してもよい。一般的なクランク角度センサは、5度程度の低分解能しかないが、クランク角度センサからのパルス信号を元にECU16での内部処理により0.1〜1.0度の分解能になるようなパルス信号を生成し、このパルス信号で筒内圧力信号をサンプリングするとよい。あるいは、クランク角度センサ3からのパルス信号でサンプリングするのではなく、一定時間間隔でのサンプリングを行い、そのサンプリングデータを時間間隔が一定でないクランク角度の情報に対応付けするようにしてもよい。
1. In-cylinder pressure signal processing The sampling unit 4 takes in-cylinder pressure signals from the in-cylinder pressure sensor 2 installed in each cylinder as data in a memory in the ECU 16. At this time, the in-cylinder pressure signal is sampled at every constant crank angle based on the pulse signal from the crank angle sensor 3 and stored as an in-cylinder pressure data string. As the crank angle sensor 3, a rotary encoder having a high resolution of about 0.1 degree may be used, and a magnetic flux change caused by a metal gear called a crank pulser attached to the crankshaft is detected by an electromagnetic pickup or a hall element. A general crank angle sensor may be used. A general crank angle sensor has only a low resolution of about 5 degrees, but the pulse signal has a resolution of 0.1 to 1.0 degrees by internal processing in the ECU 16 based on the pulse signal from the crank angle sensor. And in-cylinder pressure signal may be sampled with this pulse signal. Alternatively, instead of sampling with a pulse signal from the crank angle sensor 3, sampling may be performed at a constant time interval, and the sampling data may be associated with information on a crank angle at which the time interval is not constant.

筒内圧力データ列は、図示しないローパスフィルタにより角度周期の短いノイズがカットされる。その際、ローパスフィルタによる位相遅れを回避するよう、移動平均フィルタやゼロ位相フィルタを利用するのが望ましい。一定時間間隔でのサンプリングを行う場合は、エンジン回転速度に応じて1回転当たりのデータ量が変化するので、所望するカットオフ角度周波数を維持するために、エンジン回転速度に応じてフィルタ係数を変更するのが望ましい。   The in-cylinder pressure data string is cut from noise having a short angular period by a low-pass filter (not shown). At that time, it is desirable to use a moving average filter or a zero phase filter so as to avoid a phase delay due to the low-pass filter. When sampling at regular time intervals, the amount of data per revolution changes according to the engine speed, so the filter coefficient is changed according to the engine speed to maintain the desired cutoff angular frequency. It is desirable to do.

ECU16では、クランク軸の2回転に1回のパルスが得られるカム信号を基準にして現在どの気筒がどの行程にあるか判別される。   The ECU 16 determines which cylinder is currently in which stroke, with reference to a cam signal that obtains one pulse for two rotations of the crankshaft.

一般に、ECU16では、気筒の上死点はクランク角度センサ3からのパルス信号ごとの離散的な角度で認識される。しかし、実際には、ピストンがシリンダの最も奥に来るクランク角度、言い換えると筒内容積が最小となるクランク角度が真の上死点であり、真の上死点とECU16が認識する上死点とは、クランク角度センサ3の取り付け精度、クランクパルサの加工精度の影響、クランク軸やコンロッド(conn-rod)、ピストンピンの組み付け精度の影響などにより、気筒ごとにずれを有し、エンジン個体ごとにずれを有する。そこで、本実施形態では、ECU16が真の上死点を認識するために、筒内圧力信号から真の上死点を検出することになる。   In general, the ECU 16 recognizes the top dead center of the cylinder at discrete angles for each pulse signal from the crank angle sensor 3. However, in reality, the crank angle at which the piston is located at the back of the cylinder, in other words, the crank angle at which the in-cylinder volume is minimum is the true top dead center, and the top dead center recognized by the ECU 16 as the true top dead center. Refers to the displacement of each cylinder due to the effects of the mounting accuracy of the crank angle sensor 3, the processing accuracy of the crank pulser, the mounting accuracy of the crankshaft, conn-rod, and piston pin. Have a gap. Therefore, in the present embodiment, in order for the ECU 16 to recognize the true top dead center, the true top dead center is detected from the in-cylinder pressure signal.

エンジン運転中(燃料噴射による燃焼運転中)には、燃焼によって筒内圧力が変動するので、筒内圧力から真の上死点を検出することは困難である。そこで、車両の減速時等の非燃焼運転中や工場出荷前に行われるモータリング試験時に、筒内圧力信号のピーク位置(クランク角度)を抽出し、このピーク位置とECU16にクランク角度センサ3からのパルス信号が入力されるクランク角度とのずれ量を算出し、その後はこのずれ量を上死点の補正及び筒内圧力データ列の補正に用いる。なお、エンジン回転数によっても、熱の収支やガスの漏洩が異なるため、検出される筒内圧力のピークが真の上死点とずれることがある。そこで、適宜なエンジン回転速度ごと、例えば、200rpmごとに上死点のずれ量を学習してマップに記憶するのが好ましい。工場出荷前のモータリング試験時であれば任意にエンジン回転速度を与えることができるので、マップの作成に好適である。また、筒内圧力センサ2の特性によっては、絶対圧力のドリフトが生じる可能性があり、各気筒の筒内圧力データを補正する必要がある。この補正は、各気筒の上死点前の180度付近での吸気マニホールド圧力を用いる公知の補正演算により行う。   During engine operation (during combustion operation by fuel injection), the cylinder pressure fluctuates due to combustion, so it is difficult to detect the true top dead center from the cylinder pressure. Therefore, the peak position (crank angle) of the in-cylinder pressure signal is extracted during the non-combustion operation such as when the vehicle is decelerated or before the factory shipment, and the peak position and the ECU 16 are connected to the ECU 16 from the crank angle sensor 3. The amount of deviation from the crank angle to which the pulse signal is input is calculated, and thereafter, this amount of deviation is used for correction of top dead center and correction of the in-cylinder pressure data string. In addition, since the heat balance and gas leakage differ depending on the engine speed, the peak of the detected in-cylinder pressure may deviate from the true top dead center. Therefore, it is preferable to learn the amount of deviation of the top dead center at every appropriate engine speed, for example, every 200 rpm, and store it in the map. Since the engine speed can be arbitrarily given at the time of a motoring test before factory shipment, it is suitable for creating a map. In addition, depending on the characteristics of the in-cylinder pressure sensor 2, absolute pressure drift may occur, and it is necessary to correct the in-cylinder pressure data of each cylinder. This correction is performed by a known correction calculation using the intake manifold pressure near 180 degrees before the top dead center of each cylinder.

以上により、サンプリング部4が蓄える筒内圧力データ列は、真の上死点を含む所定クランク角度ごとのデータに補正される。   As described above, the in-cylinder pressure data sequence stored by the sampling unit 4 is corrected to data for each predetermined crank angle including the true top dead center.

次に、熱発生率演算部5において、補正された所定クランク角度ごとの筒内圧力データ列と、幾何学的に決まるクランク角度ごとの筒内容積とを用い、式(1)により、熱発生率dQを演算する。筒内圧力をP、筒内容積をV、比熱比をκとする。   Next, the heat generation rate calculation unit 5 uses the corrected in-cylinder pressure data sequence for each predetermined crank angle and the in-cylinder volume for each crank angle determined geometrically, and generates heat according to equation (1). Calculate the rate dQ. The in-cylinder pressure is P, the in-cylinder volume is V, and the specific heat ratio is κ.

Figure 2012117428
Figure 2012117428

熱発生率dQは、所定クランク角度間に発生した燃料噴射による熱を表す。過去の適宜なクランク角度(例えば、燃料噴射弁215の駆動開始角度)からの熱発生率dQを現在のクランク角度まで積分することにより、現在までの熱発生量を演算することができる。筒内容積V及び筒内容積変化量dVは、エンジン仕様により決まるので、あらかじめECU16に設定しておくとよい。   The heat generation rate dQ represents heat generated by fuel injection generated during a predetermined crank angle. By integrating the heat generation rate dQ from the past appropriate crank angle (for example, the drive start angle of the fuel injection valve 215) to the current crank angle, the heat generation amount up to the present time can be calculated. Since the in-cylinder volume V and the in-cylinder volume change amount dV are determined by the engine specifications, they may be set in the ECU 16 in advance.

図3に示されるように、クランク角度が進むに従い、実際の筒内圧力波形に応じた筒内圧力データ列が得られる。なお、図3では、サンプリングを行うクランク角度間隔が十分に小さいので、データ列は滑らかな曲線で示される。熱発生率は、メイン噴射の駆動開始より前にパイロット噴射による小さいピークを有し、その後、メイン噴射による大きいピークを有する。熱発生量は、パイロット噴射によりやや増加し、その後、メイン噴射により大きく増加する。   As shown in FIG. 3, an in-cylinder pressure data string corresponding to an actual in-cylinder pressure waveform is obtained as the crank angle advances. In FIG. 3, since the crank angle interval for sampling is sufficiently small, the data string is shown as a smooth curve. The heat generation rate has a small peak due to pilot injection before the start of main injection driving, and then has a large peak due to main injection. The amount of heat generation increases slightly due to pilot injection, and then greatly increases due to main injection.

2.パイロット噴射量のばらつき補正
図3に示されるように、本実施形態では、パイロット噴射による熱発生量hr pilotは、メイン噴射による熱発生が生じる直前での熱発生量と定義する。熱発生量演算部6では、図示しないパイロット噴射の駆動開始からメイン噴射の駆動開始タイミング(時間)に遅延時間inj delay mainを加算したタイミングまでの熱発生量を演算する。遅延時間inj delay mainは、駆動開始から実際に噴射弁が開弁するまでに要する時間であり、あらかじめ設定しておく。この熱発生量hr pilotをパイロット噴射による熱発生量とする。生産時の個体差や径時変化により、熱発生量hr pilotが気筒ごとにばらつく。
2. Correction of variation in pilot injection amount As shown in FIG. 3, in this embodiment, the amount of heat generated by pilot injection hr pilot is defined as the amount of heat generated immediately before heat generation by main injection occurs. The heat generation amount calculation unit 6 calculates the heat generation amount from the start of pilot injection (not shown) to the timing obtained by adding the delay time inj delay main to the drive start timing (time) of the main injection. The delay time inj delay main is a time required from the start of driving to the actual opening of the injection valve, and is set in advance. This heat generation amount hr pilot is set as a heat generation amount by pilot injection. The amount of heat generation hr pilot varies from cylinder to cylinder due to individual differences during production and changes over time.

式(2)に示すように、第一気筒S1の熱発生量をhr pilot1、第二気筒S2の熱発生量をhr pilot2、第三気筒S3の熱発生量をhr pilot3、第四気筒S4の熱発生量をhr pilot4とする。   As shown in the equation (2), the heat generation amount of the first cylinder S1 is hr pilot1, the heat generation amount of the second cylinder S2 is hr pilot2, the heat generation amount of the third cylinder S3 is hr pilot3, and the fourth cylinder S4 The amount of heat generated is hr pilot4.

Figure 2012117428
Figure 2012117428

次に、目標熱発生量設定部7としての熱発生量平均値演算部7aは、気筒ごとのパイロット噴射による熱発生量を均一に揃えるため、式(3)により全気筒のパイロット噴射による熱発生量の平均値hr pilot aveを演算する。   Next, the heat generation amount average value calculation unit 7a as the target heat generation amount setting unit 7 uniformly generates the heat generation amount by the pilot injection for each cylinder. Calculate the average value hr pilot ave of the quantity.

Figure 2012117428
Figure 2012117428

パイロット噴射量補正部8は、この平均値を目標熱発生量として、例えば、PI制御(比例積分制御)により各気筒のパイロット噴射量を補正する。例えば、第一気筒S1の熱発生量hr pilot1と平均値との偏差e hr pilot1は、式(4)により演算される。他の気筒についても同様である。   The pilot injection amount correction unit 8 corrects the pilot injection amount of each cylinder by, for example, PI control (proportional integration control) using the average value as the target heat generation amount. For example, the deviation e hr pilot1 between the heat generation amount hr pilot1 and the average value of the first cylinder S1 is calculated by Expression (4). The same applies to the other cylinders.

Figure 2012117428
Figure 2012117428

第一気筒S1のパイロット噴射の補正量dq pilot1は式(5)のようになる。Kpp、Kipは、あらかじめ設定するパイロット噴射補正係数である。他の気筒についても同様である。   The correction amount dq pilot1 of the pilot injection of the first cylinder S1 is as shown in Expression (5). Kpp and Kip are pilot injection correction coefficients set in advance. The same applies to the other cylinders.

Figure 2012117428
Figure 2012117428

3.メイン噴射量のばらつき補正
式(6)に示すように、図示平均有効圧力演算部9は、各気筒における図示平均有効圧力imep1、imep2、imep3、imep4を、それぞれの筒内圧力データ列を用い、公知の演算式により演算する。
3. As shown in the equation (6), the indicated mean effective pressure calculation unit 9 uses the indicated mean effective pressures imep1, imep2, imep3, and imep4 in each cylinder using the respective in-cylinder pressure data strings. It calculates with a well-known arithmetic expression.

Figure 2012117428
Figure 2012117428

図示平均有効圧力平均値演算部10は、全気筒の図示平均有効圧力を平均して得られる図示平均有効圧力平均値imep aveを式(7)により演算する。   The indicated average effective pressure average value calculation unit 10 calculates an indicated average effective pressure average value imep ave obtained by averaging the indicated average effective pressures of all the cylinders, using Expression (7).

Figure 2012117428
Figure 2012117428

メイン噴射量補正部11は、図示平均有効圧力平均値imep aveを目標として、例えば、PI制御により各気筒のメイン噴射量を補正する。例えば、第一気筒S1の図示平均有効圧力imep1と目標値との偏差e imep1は、式(8)により演算される。他の気筒についても同様である。   The main injection amount correction unit 11 corrects the main injection amount of each cylinder by PI control, for example, with the indicated average effective pressure average value imep ave as a target. For example, the deviation e imep1 between the indicated average effective pressure imep1 and the target value of the first cylinder S1 is calculated by the equation (8). The same applies to the other cylinders.

Figure 2012117428
Figure 2012117428

第一気筒S1のメイン噴射の補正量dq main1は式(9)のようになる。Kpm、Kimは、あらかじめ設定するメイン噴射補正係数である。他の気筒についても同様である。   The correction amount dq main1 of the main injection of the first cylinder S1 is as shown in Expression (9). Kpm and Kim are main injection correction coefficients set in advance. The same applies to the other cylinders.

Figure 2012117428
Figure 2012117428

メイン噴射量補正部11が実施する補正は、パイロット噴射とメイン噴射によるトータルの筒内圧力データ列から得た図示平均有効圧力に基づいているが、パイロット噴射に関して熱発生量に基づく補正済みであるので、実質的にメイン噴射におけるばらつきが補正されることになる。   The correction performed by the main injection amount correction unit 11 is based on the indicated mean effective pressure obtained from the total in-cylinder pressure data string by the pilot injection and the main injection, but has been corrected based on the heat generation amount with respect to the pilot injection. Therefore, the variation in the main injection is substantially corrected.

パイロット噴射のばらつき補正及びメイン噴射のばらつき補正では、ECU16内におけるパイロット噴射、メイン噴射の指示噴射量に補正量dq pilot1や補正量dq main1を加算して補正してもよいが、燃料噴射弁215の駆動信号のパルス幅に対して補正量に相当する補正時間を加算して補正してもよい。   In the pilot injection variation correction and the main injection variation correction, the correction amount dq pilot1 and the correction amount dq main1 may be added to the pilot injection and main injection command injection amounts in the ECU 16, but the fuel injection valve 215 may be corrected. Correction may be performed by adding a correction time corresponding to the correction amount to the pulse width of the drive signal.

また、補正量の演算は、エンジン202の運転状態が比較的安定したときに実施し、その補正量を記憶しておいて、エンジン202が急激な過渡状態や筒内圧力センサ2が失陥しているときは、記憶してある補正量を読み出して適用することもできる。   The calculation of the correction amount is performed when the operation state of the engine 202 is relatively stable. The correction amount is stored, and the engine 202 is in a sudden transient state or the in-cylinder pressure sensor 2 is lost. The stored correction amount can be read out and applied.

4.図示平均有効圧力に基づく一括補正
ここまでの処理により、気筒間の燃料噴射量のばらつきを抑えることができる。しかし、ばらつきに偏りがある場合では、平均噴射量が目標噴射量からドリフトしてしまう可能性がある。例えば、4つの気筒全てにおいて標準より噴射量が少ない場合は平均値は目標噴射量より少なくなる。逆に4つの気筒全てにおいて標準より噴射量が多い場合は平均値は目標噴射量より多くなる。
4). Collective correction based on the indicated mean effective pressure By the processing so far, it is possible to suppress variations in the fuel injection amount between the cylinders. However, when the variation is biased, the average injection amount may drift from the target injection amount. For example, when the injection amount is smaller than the standard in all four cylinders, the average value is smaller than the target injection amount. Conversely, when the injection amount is larger than the standard in all four cylinders, the average value is larger than the target injection amount.

そこで、本実施形態では、一括燃料噴射量補正部12において全気筒の燃料噴射量を一括に補正することにより、全気筒の燃料噴射量が目標燃料噴射量からドリフトするのを防止する。一括燃料噴射量補正部12では、図示平均有効圧力に基づく一括補正と排気ガスの空燃比に基づく一括補正を実行することができる。   Therefore, in this embodiment, the collective fuel injection amount correction unit 12 collectively corrects the fuel injection amounts of all the cylinders, thereby preventing the fuel injection amounts of all the cylinders from drifting from the target fuel injection amount. The collective fuel injection amount correction unit 12 can execute collective correction based on the indicated mean effective pressure and collective correction based on the air-fuel ratio of the exhaust gas.

ここではエンジン状態ごと(例えば、エンジン回転速度と噴射量)における目標噴射量q targetと目標図示平均有効圧力imep targetの関係が目標図示平均有効圧力マップ13にマップ化されている。燃料噴射量推定部14は、図示平均有効圧力演算部9が演算した図示平均有効圧力imepにより目標図示平均有効圧力マップ13を参照して実際の燃料噴射量q realを推定する。式(10)の右辺は、マップq imepを図示平均有効圧力imepで参照したことを表している。   Here, the relationship between the target injection amount q target and the target indicated average effective pressure imep target for each engine state (for example, engine speed and injection amount) is mapped to the target indicated average effective pressure map 13. The fuel injection amount estimation unit 14 estimates the actual fuel injection amount q real with reference to the target indicated average effective pressure map 13 based on the indicated average effective pressure imep calculated by the indicated average effective pressure calculation unit 9. The right side of Expression (10) indicates that the map q imep is referred to by the indicated mean effective pressure imep.

Figure 2012117428
Figure 2012117428

マップq imepを目標図示平均有効圧力imep targetで参照すると式(11)のように目標噴射量q targetが得られる。   When the map q imep is referred to by the target indicated mean effective pressure imep target, the target injection amount q target is obtained as shown in Expression (11).

Figure 2012117428
Figure 2012117428

マップq imepを図示平均有効圧力平均値imep aveで参照すると式(12)のように実際の燃料噴射量q imep aveが得られる。   When the map q imep is referred to by the indicated average effective pressure average value imep ave, the actual fuel injection amount q imep ave is obtained as shown in Expression (12).

Figure 2012117428
Figure 2012117428

一括燃料噴射量補正部12は、図示平均有効圧力平均値imep aveで推定した実際の燃料噴射量q imep aveと目標噴射量q targetとの差をドリフト量q errorとして演算する。ドリフト量q errorは、パイロット噴射のばらつき補正において第一気筒に式(5)を、他の気筒に同様の式を適用すると共に、メイン噴射のばらつき補正において第一気筒に式(9)を、他の気筒に同様の式を適用したことによって生じたものである。そこで、一括燃料噴射量補正部12は、ドリフト量q errorが小さくなるように、式(13)により補正量q correctを演算する。   The collective fuel injection amount correction unit 12 calculates a difference between the actual fuel injection amount q imep ave estimated by the indicated average effective pressure average value imep ave and the target injection amount q target as a drift amount q error. The drift amount q error is obtained by applying the equation (5) to the first cylinder in the pilot injection variation correction, and applying the equation (9) to the first cylinder in the main cylinder variation correction. This is caused by applying the same formula to other cylinders. Therefore, the collective fuel injection amount correction unit 12 calculates the correction amount q correct according to the equation (13) so that the drift amount q error becomes small.

Figure 2012117428
Figure 2012117428

一括補正の最終的な指示噴射量q fnlは、式(14)により演算される。   The final command injection quantity q fnl of the collective correction is calculated by the equation (14).

Figure 2012117428
Figure 2012117428

なお、全気筒の図示平均有効圧力平均値imep aveを用いず、気筒ごとに、例えば、第一気筒S1であれば式(15)のように図示平均有効圧力imep1でマップq imepを参照して実際の燃料噴射量q imep1を得ることで補正量dq main1を演算してもよい。Kpm、Kimは、あらかじめ設定するメイン噴射補正係数である。   Note that the indicated average effective pressure average value imep ave of all the cylinders is not used, but for each cylinder, for example, for the first cylinder S1, refer to the map q imep with the indicated average effective pressure imep1 as shown in Expression (15). The correction amount dq main1 may be calculated by obtaining the actual fuel injection amount q imep1. Kpm and Kim are main injection correction coefficients set in advance.

Figure 2012117428
Figure 2012117428

5.排気ガスの空燃比に基づく一括補正
燃料密度(ここでは固定値とする)をRoFuel、理論空燃比をAfrStoichとしたとき、空燃比演算部15は、吸入空気量センサ(図示せず)で検出される吸入空気量MAFと目標燃料噴射量q targetに基づいて排気ガスの空燃比λcalを式(16)により推定演算する。
5. Collective correction based on the air-fuel ratio of exhaust gas When the fuel density (here fixed value) is RoFuel and the theoretical air-fuel ratio is AfrStoich, the air-fuel ratio calculation unit 15 is detected by an intake air amount sensor (not shown). The air-fuel ratio λcal of the exhaust gas is estimated and calculated based on the intake air amount MAF and the target fuel injection amount q target.

Figure 2012117428
Figure 2012117428

一方、排気管208に設置されたλセンサ221により、排気ガスの空燃比λsenseが検出される。   On the other hand, the air-fuel ratio λsense of the exhaust gas is detected by the λ sensor 221 installed in the exhaust pipe 208.

一括燃料噴射量補正部12では、λセンサ221により検出される排気ガスの実空燃比λsenseと推定された空燃比λcalとの差が小さくなるように式(17)により全気筒の燃料噴射量を一括に補正する。Kp、Kiは、あらかじめ設定する噴射補正係数である。   In the collective fuel injection amount correction unit 12, the fuel injection amounts of all the cylinders are calculated by equation (17) so that the difference between the actual air-fuel ratio λsense of the exhaust gas detected by the λ sensor 221 and the estimated air-fuel ratio λcal becomes small. Correct all at once. Kp and Ki are injection correction coefficients set in advance.

Figure 2012117428
Figure 2012117428

一括補正の最終的な指示噴射量q fnlは、式(18)により演算される。   The final command injection amount q fnl of the collective correction is calculated by the equation (18).

Figure 2012117428
Figure 2012117428

補正量の演算は、エンジン202の運転状態が比較的安定したときに実施し、その補正量を記憶しておいて、エンジン202が急激な過渡状態のときは、記憶してある補正量を読み出して適用することもできる。   The calculation of the correction amount is performed when the operation state of the engine 202 is relatively stable, and the correction amount is stored. When the engine 202 is in a sudden transient state, the stored correction amount is read. Can also be applied.

ところで、図示平均有効圧力に基づく一括補正と排気ガスの空燃比に基づく一括補正とは、互いに置換が可能な制御であり、いずれか一方を実行すれば十分である。そこで、一括燃料噴射量補正部12は、λセンサ221が健全なときには排気ガスの空燃比に基づく一括補正を実行し、λセンサ221が失陥のとき図示平均有効圧力に基づく一括補正を実行するようにしてもよい。また、車種の価格設定等に応じていずれか一方の制御のみ可能なように構成してもよい。   Incidentally, the collective correction based on the indicated mean effective pressure and the collective correction based on the air-fuel ratio of the exhaust gas are controls that can be replaced with each other, and it is sufficient to execute either one. Therefore, the collective fuel injection amount correction unit 12 executes collective correction based on the air-fuel ratio of the exhaust gas when the λ sensor 221 is healthy, and executes collective correction based on the indicated mean effective pressure when the λ sensor 221 fails. You may do it. Further, only one of the controls may be configured according to the price setting of the vehicle type.

また、パイロット噴射のばらつき補正及びメイン噴射のばらつき補正では、全気筒のパイロット噴射による熱発生量の平均値hr pilot ave、全気筒の図示平均有効圧力の平均値imep aveを演算したが、これらの演算において、全気筒の平均値ではなく、最大値と最小値を除外した残りの値の平均値を演算してもよい。例えば、4気筒なら2気筒分の平均値、6気筒なら中央値付近の2〜4気筒分の平均値を演算する。このように最大値と最小値を除外した場合、極端にずれがある気筒の値が除外されるので、ドリフトは小さくなる。これにより、燃料噴射量のばらつきが大きい場合でもばらつき補正ができ、しかもドリフトを小さくすることができる。   In addition, in the pilot injection variation correction and main injection variation correction, the average value hr pilot ave of the heat generation amount by pilot injection of all cylinders and the average value imep ave of the indicated average effective pressure of all cylinders were calculated. In the calculation, the average value of the remaining values excluding the maximum value and the minimum value may be calculated instead of the average value of all the cylinders. For example, the average value for two cylinders is calculated for four cylinders, and the average value for two to four cylinders near the median value is calculated for six cylinders. When the maximum value and the minimum value are excluded in this way, the value of the cylinder that is extremely shifted is excluded, so that the drift is reduced. Thereby, even when the variation in the fuel injection amount is large, the variation can be corrected and the drift can be reduced.

本実施形態では、目標熱発生量設定部7として、熱発生量を全気筒で平均した熱発生量平均値を目標熱発生量とする熱発生量平均値演算部7aを用いたが、エンジンパラメータに基づいて目標熱発生量を設定するようにしてもよい。例えば、あらかじめ実験により求めてECU16に格納された目標熱発生量マップ7bを用いる。目標熱発生量マップ7bで参照される目標熱発生量hr expは、式(19)で表される。   In this embodiment, as the target heat generation amount setting unit 7, the heat generation amount average value calculation unit 7a having the heat generation amount average value obtained by averaging the heat generation amounts in all cylinders as the target heat generation amount is used. The target heat generation amount may be set based on the above. For example, a target heat generation amount map 7b that is obtained in advance through experiments and stored in the ECU 16 is used. The target heat generation amount hr exp referred to in the target heat generation amount map 7b is expressed by Expression (19).

Figure 2012117428
Figure 2012117428

目標熱発生量マップ7bを参照する指標は、指示噴射量Qfin、エンジン回転速度Ne、指示パイロット噴射量Qpilot、コモンレール圧Prailである。   The indices referring to the target heat generation amount map 7b are the command injection amount Qfin, the engine speed Ne, the command pilot injection amount Qpilot, and the common rail pressure Prail.

以上説明したように、本発明の燃料噴射制御装置1によれば、筒内圧力から得られる熱発生量、図示平均有効圧力に基づいて各気筒が全気筒の平均値に揃うよう噴射量の補正をするので、燃料噴射弁の特性変化によく対応して補正ができる。また、このとき平均値の演算に最大値と最小値を除外した残りの値の平均値を演算することで、ドリフトを小さくすることができる。   As described above, according to the fuel injection control device 1 of the present invention, the injection amount is corrected so that each cylinder is equal to the average value of all the cylinders based on the heat generation amount obtained from the in-cylinder pressure and the indicated mean effective pressure. Therefore, correction can be made in response to changes in the characteristics of the fuel injection valve. At this time, the drift can be reduced by calculating the average value of the remaining values excluding the maximum value and the minimum value in the calculation of the average value.

本発明の燃料噴射制御装置1によれば、燃料噴射弁の機械的なばらつきの影響が相対的に大きいパイロット噴射量のばらつき補正を実行し、それからメイン噴射量のばらつき補正を実行するようにしたので、マルチ噴射でも効果的な補正ができる。   According to the fuel injection control device 1 of the present invention, the variation correction of the pilot injection amount that is relatively affected by the mechanical variation of the fuel injection valve is executed, and then the variation correction of the main injection amount is executed. Therefore, effective correction can be performed even with multi-injection.

本発明の燃料噴射制御装置1によれば、図示平均有効圧力で推定した実際の燃料噴射量と目標噴射量との差が小さくなるように補正量を演算するので、仮に平均値がドリフトしても、ドリフトの影響を解消する補正ができる。   According to the fuel injection control device 1 of the present invention, the correction amount is calculated so that the difference between the actual fuel injection amount estimated by the indicated mean effective pressure and the target injection amount becomes small. Can be corrected to eliminate the effects of drift.

本発明の燃料噴射制御装置1によれば、空燃比センサにより検出される排気ガスの実空燃比と推定された空燃比との差が小さくなるように補正をするので、仮に平均値がドリフトしても、ドリフトの影響を解消する補正ができる。   According to the fuel injection control device 1 of the present invention, the correction is made so that the difference between the actual air-fuel ratio of the exhaust gas detected by the air-fuel ratio sensor and the estimated air-fuel ratio becomes small, so that the average value drifts temporarily. However, it is possible to correct the influence of drift.

1 燃料噴射制御装置
2 筒内圧力センサ
3 クランク角度センサ
4 サンプリング部
5 熱発生率演算部
6 熱発生量演算部
7 目標熱発生量設定部
7a 熱発生量平均値演算部
7b 目標熱発生量マップ
8 パイロット噴射量補正部
9 図示平均有効圧力演算部
10 図示平均有効圧力平均値演算部
11 メイン噴射量補正部
12 一括燃料噴射量補正部
13 目標図示平均有効圧力マップ
14 燃料噴射量推定部
15 空燃比演算部
16 ECU
DESCRIPTION OF SYMBOLS 1 Fuel injection control apparatus 2 In-cylinder pressure sensor 3 Crank angle sensor 4 Sampling part 5 Heat generation rate calculation part 6 Heat generation amount calculation part 7 Target heat generation amount setting part 7a Heat generation amount average value calculation part 7b Target heat generation amount map 8 Pilot injection amount correction unit 9 Graphical average effective pressure calculation unit 10 Graphical average effective pressure average value calculation unit 11 Main injection amount correction unit 12 Batch fuel injection amount correction unit 13 Target graphic average effective pressure map 14 Fuel injection amount estimation unit 15 Sky Fuel ratio calculation unit 16 ECU

Claims (3)

複数の気筒のそれぞれで筒内圧力センサが検出する筒内圧力をクランク角度センサが検出する信号に基づく一定のクランク角度間隔でサンプリングして各気筒の筒内圧力データ列を蓄えるサンプリング部と、
前記筒内圧力データ列を基にして各気筒における熱発生率を所定クランク角度ごとに演算する熱発生率演算部と、
熱発生率を積分することにより各気筒におけるパイロット噴射による熱発生量を演算する熱発生量演算部と、
パイロット噴射による熱発生量の目標値である目標熱発生量を設定する目標熱発生量設定部と、
各気筒における熱発生量と目標熱発生量との差が小さくなるように各気筒のパイロット噴射の燃料噴射量をそれぞれ補正するパイロット噴射量補正部と、
前記筒内圧力データ列を基にして各気筒における図示平均有効圧力を演算する図示平均有効圧力演算部と、
図示平均有効圧力を全気筒で平均して図示平均有効圧力平均値を演算する図示平均有効圧力平均値演算部と、
各気筒における図示平均有効圧力と全気筒の図示平均有効圧力平均値との差が小さくなるように各気筒のメイン噴射の燃料噴射量をそれぞれ補正するメイン噴射量補正部とを備えたことを特徴とする燃料噴射制御装置。
A sampling unit that samples the in-cylinder pressure detected by the in-cylinder pressure sensor in each of the plurality of cylinders at a constant crank angle interval based on a signal detected by the crank angle sensor, and stores an in-cylinder pressure data string of each cylinder;
A heat generation rate calculation unit that calculates a heat generation rate in each cylinder for each predetermined crank angle based on the in-cylinder pressure data sequence;
A heat generation amount calculation unit that calculates the heat generation amount by pilot injection in each cylinder by integrating the heat generation rate;
A target heat generation amount setting unit for setting a target heat generation amount that is a target value of the heat generation amount by pilot injection;
A pilot injection amount correction unit that corrects the fuel injection amount of pilot injection in each cylinder so that the difference between the heat generation amount and the target heat generation amount in each cylinder is reduced;
An indicated average effective pressure calculation unit that calculates an indicated average effective pressure in each cylinder based on the in-cylinder pressure data string,
An illustrated average effective pressure average value calculating unit that calculates the indicated average effective pressure average value by averaging the indicated average effective pressure for all cylinders;
A main injection amount correction unit that corrects the fuel injection amount of the main injection of each cylinder so that the difference between the indicated average effective pressure in each cylinder and the indicated average effective pressure average value of all cylinders is reduced; A fuel injection control device.
目標燃料噴射量とその目標燃料噴射量に対応する適正な図示平均有効圧力である目標図示平均有効圧力との関係が設定された目標図示平均有効圧力マップと、
前記演算した図示平均有効圧力により前記目標図示平均有効圧力マップを参照して実際の燃料噴射量を推定する燃料噴射量推定部と、
実際の燃料噴射量と目標燃料噴射量との差が小さくなるように全気筒の燃料噴射量を一括に補正する一括燃料噴射量補正部とを備えたことを特徴とする請求項1記載の燃料噴射制御装置。
A target indicated mean effective pressure map in which a relationship between a target fuel injection amount and a target indicated mean effective pressure that is an appropriate indicated mean effective pressure corresponding to the target fuel injection amount is set;
A fuel injection amount estimation unit that estimates an actual fuel injection amount by referring to the target indicated average effective pressure map based on the calculated indicated average effective pressure;
2. The fuel according to claim 1, further comprising a collective fuel injection amount correction unit that collectively corrects the fuel injection amounts of all the cylinders so that a difference between the actual fuel injection amount and the target fuel injection amount becomes small. Injection control device.
吸入空気量と目標燃料噴射量に基づいて排気ガスの空燃比を推定演算する空燃比演算部と、
空燃比センサにより検出される排気ガスの実空燃比と推定された空燃比との差が小さくなるように全気筒の燃料噴射量を一括に補正する一括燃料噴射量補正部とを備えたことを特徴とする請求項1記載の燃料噴射制御装置。
An air-fuel ratio calculation unit that estimates and calculates the air-fuel ratio of the exhaust gas based on the intake air amount and the target fuel injection amount;
A collective fuel injection amount correction unit that collectively corrects the fuel injection amounts of all cylinders so that the difference between the actual air-fuel ratio of the exhaust gas detected by the air-fuel ratio sensor and the estimated air-fuel ratio becomes small; The fuel injection control device according to claim 1, wherein
JP2010266877A 2010-11-30 2010-11-30 Fuel injection control device Active JP5707901B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2010266877A JP5707901B2 (en) 2010-11-30 2010-11-30 Fuel injection control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2010266877A JP5707901B2 (en) 2010-11-30 2010-11-30 Fuel injection control device

Publications (2)

Publication Number Publication Date
JP2012117428A true JP2012117428A (en) 2012-06-21
JP5707901B2 JP5707901B2 (en) 2015-04-30

Family

ID=46500566

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010266877A Active JP5707901B2 (en) 2010-11-30 2010-11-30 Fuel injection control device

Country Status (1)

Country Link
JP (1) JP5707901B2 (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015094307A (en) * 2013-11-13 2015-05-18 トヨタ自動車株式会社 Control device of internal combustion engine
JP2015197083A (en) * 2014-04-02 2015-11-09 本田技研工業株式会社 In-cylinder pressure detection device for internal combustion engine
WO2016039455A1 (en) * 2014-09-12 2016-03-17 いすゞ自動車株式会社 Device for controlling internal combustion engine
JP2016056717A (en) * 2014-09-08 2016-04-21 日立オートモティブシステムズ株式会社 Control device for internal combustion engine and method of correcting crank angle
KR20160046250A (en) * 2014-10-20 2016-04-28 현대자동차주식회사 Method and system for controlling engine using combustion pressure sensor
KR20180004941A (en) * 2016-07-05 2018-01-15 현대중공업 주식회사 method and system for decreasing pressure deviation of engine
JP2020059082A (en) * 2018-10-10 2020-04-16 日本電産サンキョー株式会社 Determination device and determination method for action completion time of robot
CN115306539A (en) * 2022-07-27 2022-11-08 清华大学 Double-constant-volume thermodynamic cycle engine and combustion control method thereof
WO2025083936A1 (en) * 2023-10-17 2025-04-24 川崎重工業株式会社 Fuel injection amount control system and fuel injection amount control method

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62132252U (en) * 1986-02-17 1987-08-20
JPH08326576A (en) * 1995-05-31 1996-12-10 Nissan Motor Co Ltd Engine combustion control device
JPH11148410A (en) * 1997-11-14 1999-06-02 Isuzu Motors Ltd Method and apparatus for controlling pilot fuel injection amount in engine
JPH11173201A (en) * 1997-12-05 1999-06-29 Isuzu Motors Ltd Method and apparatus for controlling pilot fuel injection in engine
JP2005147025A (en) * 2003-11-18 2005-06-09 Honda Motor Co Ltd Fuel injection control device for internal combustion engine
JP2006009670A (en) * 2004-06-25 2006-01-12 Honda Motor Co Ltd Control device for internal combustion engine
JP2006138293A (en) * 2004-11-15 2006-06-01 Toyota Motor Corp Abnormality diagnosis device for fuel injection system
JP2008019745A (en) * 2006-07-11 2008-01-31 Toyota Motor Corp Control device for internal combustion engine
JP2008169717A (en) * 2007-01-10 2008-07-24 Denso Corp Engine control device
JP2009281143A (en) * 2008-05-19 2009-12-03 Honda Motor Co Ltd Fuel control for internal combustion engine
JP2010059823A (en) * 2008-09-02 2010-03-18 Denso Corp Fuel injection control device
JP2010127220A (en) * 2008-11-28 2010-06-10 Mitsubishi Fuso Truck & Bus Corp Fuel control device of diesel engine
JP2010168944A (en) * 2009-01-21 2010-08-05 Nissan Motor Co Ltd Fuel injection control device for engine

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62132252U (en) * 1986-02-17 1987-08-20
JPH08326576A (en) * 1995-05-31 1996-12-10 Nissan Motor Co Ltd Engine combustion control device
JPH11148410A (en) * 1997-11-14 1999-06-02 Isuzu Motors Ltd Method and apparatus for controlling pilot fuel injection amount in engine
JPH11173201A (en) * 1997-12-05 1999-06-29 Isuzu Motors Ltd Method and apparatus for controlling pilot fuel injection in engine
JP2005147025A (en) * 2003-11-18 2005-06-09 Honda Motor Co Ltd Fuel injection control device for internal combustion engine
JP2006009670A (en) * 2004-06-25 2006-01-12 Honda Motor Co Ltd Control device for internal combustion engine
JP2006138293A (en) * 2004-11-15 2006-06-01 Toyota Motor Corp Abnormality diagnosis device for fuel injection system
JP2008019745A (en) * 2006-07-11 2008-01-31 Toyota Motor Corp Control device for internal combustion engine
JP2008169717A (en) * 2007-01-10 2008-07-24 Denso Corp Engine control device
JP2009281143A (en) * 2008-05-19 2009-12-03 Honda Motor Co Ltd Fuel control for internal combustion engine
JP2010059823A (en) * 2008-09-02 2010-03-18 Denso Corp Fuel injection control device
JP2010127220A (en) * 2008-11-28 2010-06-10 Mitsubishi Fuso Truck & Bus Corp Fuel control device of diesel engine
JP2010168944A (en) * 2009-01-21 2010-08-05 Nissan Motor Co Ltd Fuel injection control device for engine

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015094307A (en) * 2013-11-13 2015-05-18 トヨタ自動車株式会社 Control device of internal combustion engine
JP2015197083A (en) * 2014-04-02 2015-11-09 本田技研工業株式会社 In-cylinder pressure detection device for internal combustion engine
JP2016056717A (en) * 2014-09-08 2016-04-21 日立オートモティブシステムズ株式会社 Control device for internal combustion engine and method of correcting crank angle
WO2016039455A1 (en) * 2014-09-12 2016-03-17 いすゞ自動車株式会社 Device for controlling internal combustion engine
JP2016061149A (en) * 2014-09-12 2016-04-25 いすゞ自動車株式会社 Control device for internal combustion engine
KR101628106B1 (en) * 2014-10-20 2016-06-08 현대자동차 주식회사 Method and system for controlling engine using combustion pressure sensor
KR20160046250A (en) * 2014-10-20 2016-04-28 현대자동차주식회사 Method and system for controlling engine using combustion pressure sensor
US9885300B2 (en) 2014-10-20 2018-02-06 Hyundai Motor Company Method and system for controlling engine using combustion pressure sensor
KR20180004941A (en) * 2016-07-05 2018-01-15 현대중공업 주식회사 method and system for decreasing pressure deviation of engine
KR102542339B1 (en) 2016-07-05 2023-06-12 에이치디한국조선해양 주식회사 method for decreasing pressure deviation of engine
JP2020059082A (en) * 2018-10-10 2020-04-16 日本電産サンキョー株式会社 Determination device and determination method for action completion time of robot
JP7186571B2 (en) 2018-10-10 2022-12-09 日本電産サンキョー株式会社 Apparatus and method for determining operation completion time of robot
CN115306539A (en) * 2022-07-27 2022-11-08 清华大学 Double-constant-volume thermodynamic cycle engine and combustion control method thereof
CN115306539B (en) * 2022-07-27 2023-08-22 清华大学 Double-isovolumetric thermodynamic cycle engine and combustion control method thereof
WO2025083936A1 (en) * 2023-10-17 2025-04-24 川崎重工業株式会社 Fuel injection amount control system and fuel injection amount control method

Also Published As

Publication number Publication date
JP5707901B2 (en) 2015-04-30

Similar Documents

Publication Publication Date Title
JP5707901B2 (en) Fuel injection control device
US8612120B2 (en) Control apparatus for internal combustion engine
US8265853B2 (en) Cylinder pressure measurement system and method
JP5758862B2 (en) In-cylinder pressure detection device for internal combustion engine
CN100357581C (en) Four-stroked engine control device and control method
JP4788640B2 (en) In-cylinder pressure estimation method and cylinder pressure estimation apparatus for internal combustion engine
JP5331613B2 (en) In-cylinder gas amount estimation device for internal combustion engine
US8645046B2 (en) Controller for internal combustion engine
US20110213544A1 (en) Fuel injection controller for internal combustion engine
CN104541041A (en) In-cylinder pressure detection device for internal combustion engine
US8751137B2 (en) Apparatus for estimating exhaust gas recirculation quantity
CN103180591B (en) Control devices for internal combustion engines
JP6462311B2 (en) Engine control device
US7178494B2 (en) Variable valve timing controller for internal combustion engine
JP5691438B2 (en) In-cylinder pressure waveform processing device
JPWO2011117972A1 (en) Control device for internal combustion engine
JP2007278223A (en) In-cylinder injection type spark ignition internal combustion engine control device
JP2007231883A (en) Air-fuel ratio control device for internal combustion engine
JP2010133353A (en) Engine control device
JP4792453B2 (en) Intake air amount detection device
JP4747977B2 (en) In-cylinder pressure sensor calibration device
US9822726B2 (en) Fuel injection controller for internal combustion engine, and engine including the same
JP2008202461A (en) Fuel injection control device for internal combustion engine
JP4618009B2 (en) Control device for internal combustion engine
JP6267279B2 (en) Control device for internal combustion engine

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20131016

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20140526

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20140603

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20140730

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20150203

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20150216

R150 Certificate of patent or registration of utility model

Ref document number: 5707901

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150