EP1336041A1 - Method for injecting fuel during the start phase of an internal combustion engine - Google Patents
Method for injecting fuel during the start phase of an internal combustion engineInfo
- Publication number
- EP1336041A1 EP1336041A1 EP01996679A EP01996679A EP1336041A1 EP 1336041 A1 EP1336041 A1 EP 1336041A1 EP 01996679 A EP01996679 A EP 01996679A EP 01996679 A EP01996679 A EP 01996679A EP 1336041 A1 EP1336041 A1 EP 1336041A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- internal combustion
- injectors
- combustion engine
- crankshaft
- fuel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 26
- 238000000034 method Methods 0.000 title claims abstract description 26
- 239000000446 fuel Substances 0.000 title claims abstract description 21
- 238000002347 injection Methods 0.000 claims abstract description 21
- 239000007924 injection Substances 0.000 claims abstract description 21
- 239000000203 mixture Substances 0.000 abstract description 5
- 230000003466 anti-cipated effect Effects 0.000 abstract 1
- 239000002360 explosive Substances 0.000 abstract 1
- 239000003344 environmental pollutant Substances 0.000 description 3
- 231100000719 pollutant Toxicity 0.000 description 3
- 230000003111 delayed effect Effects 0.000 description 2
- 235000000621 Bidens tripartita Nutrition 0.000 description 1
- 240000004082 Bidens tripartita Species 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 208000006637 fused teeth Diseases 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/009—Electrical control of supply of combustible mixture or its constituents using means for generating position or synchronisation signals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/04—Introducing corrections for particular operating conditions
- F02D41/047—Taking into account fuel evaporation or wall wetting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/04—Introducing corrections for particular operating conditions
- F02D41/06—Introducing corrections for particular operating conditions for engine starting or warming up
- F02D41/062—Introducing corrections for particular operating conditions for engine starting or warming up for starting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/009—Electrical control of supply of combustible mixture or its constituents using means for generating position or synchronisation signals
- F02D2041/0092—Synchronisation of the cylinders at engine start
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2200/00—Input parameters for engine control
- F02D2200/02—Input parameters for engine control the parameters being related to the engine
- F02D2200/04—Engine intake system parameters
- F02D2200/0402—Engine intake system parameters the parameter being determined by using a model of the engine intake or its components
Definitions
- the present invention relates to a method for injecting fuel into a multi-cylinder internal combustion engine.
- the cylinders are divided into a first and a second cylinder group depending on the two different levels of the camshaft signal.
- the cylinders of the first group are supplied with the pre-injectors (group injectors) immediately after a start detection, while the pre-injectors for the cylinders of the second group are delayed.
- the fuel quantities of the pre-injector are chosen to be the same.
- the present invention is based on the object of specifying a method for injecting fuel into a multi-cylinder internal combustion engine, in which fuel-air mixtures with different lambda values are largely avoided in the starting phase.
- the present invention is based on the finding that an internal combustion engine always remains at certain discrete positions after being switched off in the disengaged state, the number of discrete positions over two crankshaft revolutions (760 °) corresponding to the number of cylinders. In the case of n cylinders, these are therefore n standstill angular positions which, moreover, have the same angular distances relative to one another. Experiments have also shown that the speed behavior of the internal combustion engine and the timing of the opening of the intake valves to the
- the fuel quantities of the pre-injectors can therefore be selected depending on the sequence of the pre-injectors and the air fillings to be expected, the air fillings to be expected being determined only once must and the corresponding values can then be used at every start. Since the air fillings primarily depend on the speed in the respective intake phase, the air fillings are preferably determined as a function of the expected speed in the respective intake phases.
- the fuel quantities of the pre-injectors are determined by multiplying a standard quantity by weighting factors assigned to a pre-injector in each case. If the weighting factors could also be estimated, they are expediently determined experimentally for each series of an internal combustion engine and then stored in the central control unit.
- the present invention takes advantage of the fact that the internal combustion engine always remains at certain discrete positions in the disengaged state after being switched off. However, it should be emphasized that it is not necessary to know these standstill positions in order to carry out the method according to the invention. Rather, it is sufficient for the method according to the invention to know the order of the pre-injectors in order to specify the fuel quantities of the pre-injectors as a function thereof.
- the pre-injectors are deposited in quantities which are at least approximately adequate for the respective air filling. Too rich or too lean fuel-air mixtures are avoided, which results in a corresponding reduction in pollutant emissions.
- Figure 1 is a schematic sectional view of an internal combustion engine in the form of a gasoline engine with gasoline injection;
- Figure 2 is a graph plotting speed, camshaft, crankshaft, injector, and intake valve signals over time.
- FIG. 1 shows a schematic partial section through an internal combustion engine which, in the exemplary embodiment described, is designed for illustration purposes as a four-cylinder gasoline engine with gasoline injection.
- a common electronic control unit 1 is assigned to the internal combustion engine 3, which controls the ignition, fuel injection and other processes of the internal combustion engine.
- At least one inlet valve 6 and at least one injection valve 2 are assigned to each cylinder 7.
- the injection valve 2 injects fuel into the intake manifold directly onto the valve plate of the intake valve 6.
- the crankshaft 8 is assigned a crankshaft sensor 4 with a toothed sensor wheel, which generates a crankshaft signal CRK representing the crankshaft angle (see lower half of FIGS. 2 and 3).
- the camshaft 5, which controls the intake valves 6 and rotates at half the speed of the crankshaft 8, is assigned a camshaft sensor 9 for generating a camshaft signal CAM (see lower half of FIGS. 2 and 3).
- the camshaft 5 can be adjustable in angle relative to the crankshaft 8, but this is by no means necessary for the method to be described.
- crankshaft signal CRK In FIGS. 2 and 3, lower half, the crankshaft signal CRK, the camshaft signal CAM and the speed N are plotted against time.
- Each pulse of the crankshaft signal CRK corresponds to one tooth of the transmitter wheel, with a double tooth gap after every 60 teeth as synchronization pulse S for one full revolution of the crankshaft.
- DJ 3 er Hi F for DJ F ⁇ 3 cn ⁇ d 3 3 DJ er DJ ⁇ 3 cn ⁇ O ⁇ F- er fr ⁇ ⁇ ⁇ ⁇ ⁇ J er ⁇ F- ⁇ d F- 3 FF d Hi A ⁇ F 1 F- ⁇ CL CO tr 3 ⁇ rt ⁇ rt P- ⁇ ⁇ tu O er cn F 3 A d ⁇ 3 O rt F- F " ⁇ 3 ⁇ F F- P-
- DJ er DJ ⁇ d ⁇ DJ rt F- cn ⁇ DJ DJ ⁇ F- A DJ ⁇ ⁇ T) tr S ⁇ 3 cn ⁇ F ⁇ P- ⁇ ⁇ ⁇ tr rt fr ⁇ t F ta Hi ⁇ 3 fr d 3 Hi ⁇ ⁇ ⁇ 3 rt ⁇ s: 3 F- ⁇ dof F- d: ⁇ DJ N rt ⁇ rt ⁇ ⁇ Fi rt F- DJ: FFFO fr F tu
- the method according to the invention can in principle be used in any pre-injection strategies, for example also in the method according to EP 0 371 158 B1 discussed above, in which the pre-injectors of a first cylinder group are released at the same time and the pre-injectors of the second cylinder group are delayed in time.
- the method according to the invention is used with particularly good success in a pre-injection strategy in which all the pre-injectors are placed one after the other in chronological order.
- An example of such a pre-injection strategy is explained in more detail below with reference to FIG. 2.
- the speed N of the internal combustion engine is plotted over time.
- the control signals IV1 - IV4 for the four injection valves are plotted over time for the four cylinders 1 to 4 of the four-cylinder internal combustion engine, the four pilot injectors I being designated II - 14.
- the control signals EV1-EV4 for the four intake valves are plotted over time, the opening pulses for the opening of the intake valves being designated E1-E4.
- the top two lines of FIG. 2 show the pulses for the top dead center (TDC1-TDC4) of the four cylinders and the top dead center (TDC1) of the cylinder 1.
- a starter identification E is provided for starting the internal combustion engine.
- the camshaft signal CAM is either high or low, in the example in FIG. 2 low.
- Figure 2 in a first group with the cylinders 3, 4 and a second group with the cylinders 1, 2).
- DJ DJ - 3 • F rt DJ rt 3 Hi rt ⁇ DJ F ⁇ rt s; 3 ⁇ 3 P- o ⁇ CL rt 3 ⁇ ! O 3 P- ⁇ H INI er 3 Hi cn 3 er F- 3 F- ⁇ tr 3 er to 3 ⁇ P- O tu CL O cn rt CO • ⁇ A d ⁇ cn et et ⁇ et F- er ⁇ 3 ⁇ 3 cn? -
- the internal combustion engine is synchronized, and thus a defined sequence of the pre-injections occurring after the synchronization pulse S can be determined by the central control unit 1.
- this pre-injection strategy results in a defined sequence of the cylinders supplied with pre-injectors I one after the other, in the illustrated case cylinder 4, cylinder 1, cylinder 2 and cylinder 3.
- the fuel quantities of the associated pre-injectors 14, II, 12 and 13 become determined by multiplying the standard quantity by the fixed weighting factors.
- the sequence of the cylinders supplied with the pre-injectors changes.
- the fuel quantities of the successive pilot injector I can always be determined using the same weighting factors.
- the pre-injection method described above is only one example of a pre-injection strategy in which the method according to the invention can be used.
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
Description
Beschreibungdescription
Verfahren zum Einspritzen von Kraftstoff während der Startphase einer BrennkraftmaschineMethod for injecting fuel during the starting phase of an internal combustion engine
Die vorliegende Erfindung betrifft ein Verfahren zum Einspritzen von Kraftstoff in eine mehrzylindrige Brennkraftmaschine.The present invention relates to a method for injecting fuel into a multi-cylinder internal combustion engine.
Es ist bekannt, beim Start eines Ottomotors die Zylinder je einmal mit einem sogenannten Vorabeinspritzer zu versorgen, um die Zylinderwände zu benetzen und gleichzeitig ein zündfähiges Gemisch für die erste Verbrennung bereitzustellen. Da zu diesem Zeitpunkt noch keine Synchronisation zwischen No- ckenwelle und der Kurbelwelle vorhanden und die Position der Kolben unbekannt ist, ist eine gezielte Vorabeinspritzstrategie erforderlich, um den Ausstoß von unverbranntem Kraftstoff und somit die Schadstoffemissionen während des Starts zu minimieren.It is known to supply the cylinders once with a so-called pre-injector each time a gasoline engine is started in order to wet the cylinder walls and at the same time to provide an ignitable mixture for the first combustion. Since there is no synchronization between the camshaft and the crankshaft at this point in time and the position of the pistons is unknown, a targeted pre-injection strategy is required to minimize the emission of unburned fuel and thus the pollutant emissions during takeoff.
Bei einem aus der EP 0 371 158 Bl bekannten Verfahren werden die Zylinder in Abhängigkeit von den beiden unterschiedlichen Pegeln des Nockenwellensignals in eine erste und eine zweite Zylindergruppe unterteilt. Die Zylinder der ersten Gruppe werden unmittelbar nach einer Starterkennung zeitgleich mit den Vorabeinspritzern (Gruppeneinspritzer) versorgt, während die Vorabeinspritzer für die Zylinder der zweiten Gruppe zeitlich verzögert abgesetzt werden. Hierbei werden die Kraftstoffmengen der Vorabeinspritzer gleich groß gewählt.In a method known from EP 0 371 158 B1, the cylinders are divided into a first and a second cylinder group depending on the two different levels of the camshaft signal. The cylinders of the first group are supplied with the pre-injectors (group injectors) immediately after a start detection, while the pre-injectors for the cylinders of the second group are delayed. The fuel quantities of the pre-injector are chosen to be the same.
Es hat sich nun gezeigt, dass infolge der Gasdynamik im Saugrohr die Luftfüllungen der Zylinder bereits beim Start nicht gleich sind. So werden die ersten Zylinder infolge der im Saugrohr stehenden Luftsäule nicht so gut gefüllt wie die nachfolgenden Zylinder, bei denen die Luft im Saugrohr bereits eine merkliche Strömungsgeschwindigkeit und entsprechende Bewegungsenergie erreicht hat. Die Folge ist, dass die Kraftstoff-Luft-Gemische (Larnbda-Werte) der ersten Vorabfüllungen fetter als die nachfolgenden Vorabfüllungen sind. Dies führt zu erhöhten Schadstoffemissionen in der Startphase, was insbesondere bei schadstoffoptimierten Brennkraftmaschinen zu vermeiden ist.It has now been shown that due to the gas dynamics in the intake manifold, the air fillings in the cylinders are not the same from the start. As a result of the air column standing in the intake manifold, the first cylinders are not filled as well as the subsequent cylinders, in which the air in the intake manifold has already reached a noticeable flow velocity and corresponding kinetic energy. The result is that the Fuel-air mixtures (Larnbda values) of the first pre-fillings are richer than the subsequent pre-fillings. This leads to increased pollutant emissions in the start-up phase, which should be avoided in particular with pollutant-optimized internal combustion engines.
Der vorliegenden Erfindung liegt die Aufgabe zugrunde, ein Verfahren zum Einspritzen von Kraftstoff in eine mehrzylindrische Brennkraftmaschine anzugeben, bei der in der Startpha- se Kraftstoff-Luft-Gemische mit unterschiedlichen Lambda- Werten weitgehend vermieden werden.The present invention is based on the object of specifying a method for injecting fuel into a multi-cylinder internal combustion engine, in which fuel-air mixtures with different lambda values are largely avoided in the starting phase.
Das Verfahren gemäß der Erfindung ist in Anspruch 1 definiert .The method according to the invention is defined in claim 1.
Die vorliegende Erfindung basiert auf der Erkenntnis, dass eine Brennkraftmaschine nach dem Abschalten im ausgekuppelten Zustand immer an bestimmten diskreten Positionen stehen bleibt, wobei die Anzahl der diskreten Positionen über zwei Kurbelwellenumdrehungen (760°) der Anzahl der Zylinder entspricht. Im Fall von n Zylindern sind dies somit n Still- stands-Winkelpositionen, die im übrigen gleiche Winkelabstände relativ zueinander haben. Ferner haben Versuche gezeigt, dass das Drehzahlverhalten der Brennkraftmaschine sowie die zeitliche Zuordnung der Öffnung der Einlassventile zu derThe present invention is based on the finding that an internal combustion engine always remains at certain discrete positions after being switched off in the disengaged state, the number of discrete positions over two crankshaft revolutions (760 °) corresponding to the number of cylinders. In the case of n cylinders, these are therefore n standstill angular positions which, moreover, have the same angular distances relative to one another. Experiments have also shown that the speed behavior of the internal combustion engine and the timing of the opening of the intake valves to the
Drehzahl während den Startphasen immer ähnlich sind, unabhängig davon, an welcher der diskreten Positionen die Brennkraftmaschine stehen geblieben ist. Somit ergibt sich bei jedem Start im wesentlichen die gleiche Folge unterschiedlicher Luftfüllungen für aufeinanderfolgende Vorabeinspritzer.Speed during the starting phases are always similar, regardless of which of the discrete positions the internal combustion engine has stopped. This means that each start essentially results in the same sequence of different air fillings for successive pre-injectors.
Dies erlaubt es, die zu erwartenden Luftfüllungen für die aufeinanderfolgenden Vorabeinspritzer abzuschätzen. Die Kraftstoffmengen der Vorabeinspritzer können daher in Abhän- gigkeit von der Reihenfolge der Vorabeinspritzer und den zu erwartenden Luftfüllungen entsprechend gewählt werden, wobei die zu erwartenden Luftfüllungen nur einmal bestimmt werden müssen und die entsprechenden Werte dann bei jedem Start verwendet werden können. Da die Luftfüllungen in erster Linie von der Drehzahl in der jeweiligen Ansaugphase abhängen, werden die Luftfüllungen vorzugsweise in Abhängigkeit von den zu erwartenden Drehzahlen in den jeweiligen Ansaugphasen bestimmt .This makes it possible to estimate the air fillings to be expected for the successive pre-injectors. The fuel quantities of the pre-injectors can therefore be selected depending on the sequence of the pre-injectors and the air fillings to be expected, the air fillings to be expected being determined only once must and the corresponding values can then be used at every start. Since the air fillings primarily depend on the speed in the respective intake phase, the air fillings are preferably determined as a function of the expected speed in the respective intake phases.
In besonders vorteilhafter Ausgestaltung des erfindungsgemäßen Verfahrens ist vorgesehen, dass die Kraftstoffmengen der Vorabeinspritzer durch Multiplikation einer Standardmenge mit jeweils einem Vorabeinspritzer zugeordneten Gewichtungsfaktoren bestimmt werden. Wenn auch die Gewichtungsfaktoren abgeschätzt werden könnten, werden sie zweckmäßigerweise für jede Baureihe einer Brennkraftmaschine experimentell ermittelt und dann im zentralen Steuergerät abgespeichert.In a particularly advantageous embodiment of the method according to the invention, it is provided that the fuel quantities of the pre-injectors are determined by multiplying a standard quantity by weighting factors assigned to a pre-injector in each case. If the weighting factors could also be estimated, they are expediently determined experimentally for each series of an internal combustion engine and then stored in the central control unit.
Wie erwähnt, macht sich die vorliegende Erfindung die Tatsache zunutze, dass die Brennkraftmaschine nach dem Abschalten im ausgekuppelten Zustand immer an bestimmten diskreten Posi- tionen stehen bleibt. Es sei jedoch betont, dass zum Durchführen des erfindungsgemäßen Verfahrens nicht erforderlich ist, diese Stillstandspositionen zu kennen. Vielmehr ist es für das erfindungsgemäße Verfahren ausreichend, die Reihenfolge der Vorabeinspritzer zu kennen, um in Abhängigkeit von diesen die Kraftstoffmengen der Vorabeinspritzer vorzugeben.As mentioned, the present invention takes advantage of the fact that the internal combustion engine always remains at certain discrete positions in the disengaged state after being switched off. However, it should be emphasized that it is not necessary to know these standstill positions in order to carry out the method according to the invention. Rather, it is sufficient for the method according to the invention to know the order of the pre-injectors in order to specify the fuel quantities of the pre-injectors as a function thereof.
Durch das erfindungsgemäße Verfahren wird erreicht, dass bereits in der Startphase die Vorabeinspritzer in Mengen abgesetzt werden, die zumindest näherungsweise für die jeweilige Luftfüllung adäquat sind. Somit werden zu fette oder zu magere Kraftstoffluftgemische vermieden, was eine entsprechende Reduzierung der Schadstoffemissionen zur Folge hat.It is achieved by the method according to the invention that, in the starting phase, the pre-injectors are deposited in quantities which are at least approximately adequate for the respective air filling. Too rich or too lean fuel-air mixtures are avoided, which results in a corresponding reduction in pollutant emissions.
Anhand der Zeichnungen wird das erfindungsgemäße Verfahren näher erläutert. Es zeigt: Figur 1 eine schematische Schnittdarstellung einer Brennkraftmaschine in Form eines Ottomotors mit Benzineinspritzung;The method according to the invention is explained in more detail with reference to the drawings. It shows: Figure 1 is a schematic sectional view of an internal combustion engine in the form of a gasoline engine with gasoline injection;
Figur 2 ein Diagramm, in dem über der Zeit Drehzahl-, Nocken- wellen-, Kurbelwellen-, Einspritzventil- und Einlassventil-Signale aufgetragen sind.Figure 2 is a graph plotting speed, camshaft, crankshaft, injector, and intake valve signals over time.
Die Figur 1 zeigt einen schematischen Teilschnitt durch eine Brennkraftmaschine, welche im beschriebenen Ausführungsbei- spiel zu Veranschaulichungszwecken als Vierzylinder-Ottomotor mit Benzineinspritzung ausgebildet ist.FIG. 1 shows a schematic partial section through an internal combustion engine which, in the exemplary embodiment described, is designed for illustration purposes as a four-cylinder gasoline engine with gasoline injection.
Der Brennkraftmaschine 3 ist in üblicher Weise ein zentrales elektronisches Steuergerät 1 zugeordnet, das die Zündung, Kraftstoffeinspritzung und andere Vorgänge der Brennkraftmaschine steuert. Jedem Zylinder 7 ist mindestens ein Einlassventil 6 und mindestens ein Einspritzventil 2 zugeordnet. Das Einspritzventil 2 spritzt Kraftstoff in das Saugrohr unmittelbar auf den Ventilteller des Einlassventils 6 ab.A common electronic control unit 1 is assigned to the internal combustion engine 3, which controls the ignition, fuel injection and other processes of the internal combustion engine. At least one inlet valve 6 and at least one injection valve 2 are assigned to each cylinder 7. The injection valve 2 injects fuel into the intake manifold directly onto the valve plate of the intake valve 6.
Der Kurbelwelle 8 ist ein Kurbelwellensensor 4 mit einem gezahnten Geberrad zugeordnet, das ein den Kurbelwellenwinkel darstellendes Kurbelwellensignal CRK (siehe untere Hälfte der Figuren 2 und 3) erzeugt. Der Nockenwelle 5, die die Einlass- ventile 6 steuert und mit der halben Drehzahl der Kurbelwelle 8 dreht, ist ein Nockenwellensensor 9 zum Erzeugen eines Nockenwellensignals CAM (siehe untere Hälfte der Figuren 2 und 3) zugeordnet. Die Nockenwelle 5 kann relativ zur Kurbelwelle 8 winkelverstellbar sein, was jedoch für das zu beschreibende Verfahren keineswegs erforderlich ist.The crankshaft 8 is assigned a crankshaft sensor 4 with a toothed sensor wheel, which generates a crankshaft signal CRK representing the crankshaft angle (see lower half of FIGS. 2 and 3). The camshaft 5, which controls the intake valves 6 and rotates at half the speed of the crankshaft 8, is assigned a camshaft sensor 9 for generating a camshaft signal CAM (see lower half of FIGS. 2 and 3). The camshaft 5 can be adjustable in angle relative to the crankshaft 8, but this is by no means necessary for the method to be described.
In den Figuren 2 und 3, untere Hälfte, sind jeweils das Kurbelwellensignal CRK, das Nockenwellensignal CAM und die Drehzahl N über der Zeit aufgetragen. Jeder Impuls des Kurbelwel- lensignals CRK entspricht einem Zahn des Geberrades, wobei eine doppelte Zahnlücke nach jeweils 60 Zähnen als Synchronisationsimpuls S für jeweils eine volle Umdrehung der Kurbel- ω CO M > F1 F1 cπ O Cπ o cπ o CπIn FIGS. 2 and 3, lower half, the crankshaft signal CRK, the camshaft signal CAM and the speed N are plotted against time. Each pulse of the crankshaft signal CRK corresponds to one tooth of the transmitter wheel, with a double tooth gap after every 60 teeth as synchronization pulse S for one full revolution of the crankshaft. ω CO M> F 1 F 1 cπ O Cπ o cπ o Cπ
?v α ω ? N 3 F t ω --J s: F € t r+ > < 3 M rt 3 DJ tu tπ tu cn Ό d CL cn s:? v α ω? N 3 F t ω --J s: F € t r +> <3 M rt 3 DJ tu tπ tu cn Ό d CL cn s:
F φ Ό F DJ Φ D : DJ 3 φ rt- Φ DJ Φ F P- er φ P- F- P- F- d 3 F- F- φ rt d 3 Φ Ω ΦF φ Ό F DJ Φ D: DJ 3 φ rt- Φ DJ Φ F P- er φ P- F- P- F- d 3 F- F- φ rt d 3 Φ Ω Φ
Φ F F D> tr 3 O Ω- rr F- QJ F- F- Φ o cn F Ω 3 o Ω F A 3 F1 F- Φ CL F ^ rt F- ι-h P1 3" ω 3 IN! cn F- 3 3 Ω cn 3- Φ 3 3f er Φ cn Hi F1 cn P-Φ FF D> tr 3 O Ω- rr F- QJ F- F- Φ o cn F Ω 3 o Ω FA 3 F 1 F- Φ CL F ^ rt F- ι-h P 1 3 " ω 3 IN! Cn F- 3 3 Ω cn 3- Φ 3 3f er Φ cn Hi F 1 cn P-
Φ ESI O r T) cn o_ Ό φ α DJ: Φ α ω 3 Φ tr d rt rt Φ CO Ό φ 3 F1 Φ CL ^ Φ ΦΦ ESI O r T) cn o_ Ό φ α DJ: Φ α ω 3 Φ tr d rt rt Φ CO Ό φ 3 F 1 Φ CL ^ Φ Φ
F ^ tr 3 O rt Φ F F- 3- φ f 3 DJ Ω M N F-1 rt F o d 3 D d α r+ DJ Φ Cfl Φ cn Φ 3 N 3 F- cn o F F1 tr 3 P- Z er s; Φ F- F 3 cn F c»F ^ tr 3 O rt Φ F F- 3- φ f 3 DJ Ω MN F- 1 rt F od 3 D d α r + DJ Φ Cfl Φ cn Φ 3 N 3 F- cn o FF 1 tr 3 P- Z er s; Φ F- F 3 cn F c »
« F- ω F F- 3 O Φ « Φ 3 ( ι DJ cn rt Φ O: 3 P- Φ Φ d rt Φ 3 A ω er F-«F- ω F F- 3 O Φ« Φ 3 (ι DJ cn rt Φ O: 3 P- Φ Φ d rt Φ 3 A ω er F-
Φ 3 o r+ ^ 3" F F- ^ o Hi rt Φ IQ cn ω fr Φ N ω DJ ^ Φ Ω CL i-i H nr CO F- CG d Φ cn < φ f- 0 H Φ 3 3J F1 *Ü o DJ F <! P- φ d F1 t F- α Φ 3 F- rt O ^ H 3 ω Ω O H F 3 " DJ F- F, 3* 3 Φ rt Φ ^ Φ 3 F F s; Φ ΦΦ 3 o r + ^ 3 " F F- ^ o Hi rt Φ IQ cn ω fr Φ N ω DJ ^ Φ Ω CL ii H nr CO F- CG d Φ cn <φ f- 0 H Φ 3 3 J F 1 * Ü o DJ F <! P- φ d F 1 t F- α Φ 3 F- rt O ^ H 3 ω Ω OHF 3 "DJ F- F, 3 * 3 Φ rt Φ ^ Φ 3 FF s; Φ Φ
Φ F 3 F- 3 3 er 0_ φ " F er 0_ DJ Φ F- er Ω F- Φ 3 3 3 d 3 H er Φ 3Φ F 3 F- 3 3 er 0_ φ "F er 0_ DJ Φ F- er Ω F- Φ 3 3 3 d 3 H er Φ 3
3 N c- Φ Φ O Φ Φ o Φ Φ Φ cn 3 3 Φ 3- rt 3 rt cn d rt F > DJ φ T) rt3 N c- Φ Φ O Φ Φ o Φ Φ Φ cn 3 3 Φ 3- rt 3 rt cn d rt F> DJ φ T) rt
. 0) er H 3 3" F * 3 Φ F- F1 F O 3 • N ^ rt 3 P- σ t F d F1 F1 Φ •, 0 ) he H 3 3 " F * 3 Φ F- F 1 FO 3 • N ^ rt 3 P- σ t F d F 1 F 1 Φ •
3^ F ω cn h s; ω F- φ s: * er DJ d CL Φ α FJ Φ Φ er er ≤ Φ υ33 ^ F ω cn hs; ω F- φ s: * er DJ d CL Φ α F J Φ Φ er er ≤ Φ υ3
I-1 F- rf r+ er O Φ S! N α 3 Φ vl F- d ιQ 3 Φ d }-• Φ 1 rt Φ φ φ φ σI- 1 F- rf r + er O Φ S! N α 3 Φ vl F- d ιQ 3 Φ d} - • Φ 1 rt Φ φ φ φ σ
-Q Φ DJ Φ 3 Φ • F- Φ .) P* c: 3 Φ cn φ ιQ F 3 P* er ≤ F P- 3 F1 N H DJ-Q Φ DJ Φ 3 Φ • F- Φ.) P * c: 3 Φ cn φ ιQ F 3 P * er ≤ F P- 3 F 1 NH DJ
CL Φ * 3 et F- F- F1 Φ 3 O F Φ F- ιT! N d φ M Φ P- rt F1 d ^ cnCL Φ * 3 et F- F- F 1 Φ 3 OF Φ F- ιT! N d φ M Φ P- rt F 1 d ^ cn
P- 3 Φ F cn Φ cn F- cn cn Φ er er Φ φ F- 3 3 rt Φ cn Φ φ cQP- 3 Φ F cn Φ cn F- cn cn Φ er er Φ φ F- 3 3 rt Φ cn Φ φ cQ
Φ 3 ω : DJ 3 φ 3 Φ o F- 3 Φ cn rt f F- 3 o Φ 3 Di: P- F1 er cn F- 3 Φ CL -3 t 1 A rr cn 3 *< r+ cn F1 F- • d ιQ Ω cn rt 3 Φ T3 3 cn O P- O co SU er s rf P- Φ DJ Φ 3 F- Φ s: 3 T3 rt ω fV d F- 3 α P- Φ F- F Φ Ω rt rf F- O 3 F1 F •τj o O 3 C tu Ό φ Φ F- 3 A d= cn Φ Φ ιQ CL frΦ 3 ω: DJ 3 φ 3 Φ o F- 3 Φ cn rt f F- 3 o Φ 3 Di: P- F 1 er cn F- 3 Φ CL -3 t 1 A rr cn 3 * <r + cn F 1 F- • d ιQ Ω cn rt 3 Φ T3 3 cn O P- O co SU er s rf P- Φ DJ Φ 3 F- Φ s: 3 T3 rt ω fV d F- 3 α P- Φ F- F Φ Ω rt rf F- O 3 F 1 F • τj o O 3 C tu Ό φ Φ F- 3 A d = cn Φ Φ ιQ CL fr
F- φ 3 α 3 ω cn 1 O 3J 3 cn φ Φ A 3 n α er er F- F H Φ 3 3 N ΦF- φ 3 α 3 ω cn 1 O 3 J 3 cn φ Φ A 3 n α er er F- FH Φ 3 3 N Φ
P1 CΛ F- f DJ ω O t ω F Φ O F- CL d s: rt iQ F- DJ Φ ≤ 3P 1 CΛ F- f DJ ω O t ω F Φ O F- CL ds: rt iQ F- DJ Φ ≤ 3
F- er Φ 3 F- F na F P- O 3 F Φ P- rt DJ Φ Φ α s: F- 3 tu 3 F1 rt φ s:F- er Φ 3 F- F na F P- O 3 F Φ P- rt DJ Φ Φ α s: F- 3 tu 3 F 1 rt φ s:
Cn O rt P1 3 3 cn O Φ r+ 3 cn 3 φ Φ Φ cn 3 FJ A DJ φ Ω DJ F C F- φ r+ 3' •* 13 Ό ω 3 F- F- Φ cn P- 3 cn er ιQ 3 F t F" Φ Φ O cn F1 Cn O rt P 1 3 3 cn O Φ r + 3 cn 3 φ Φ Φ cn 3 F J A DJ φ Ω DJ FC F- φ r + 3 ' • * 13 Ό ω 3 F- F- Φ cn P- 3 cn er ιQ 3 F t F "Φ Φ O cn F 1
!U O P> d cπ F- 3 0 ω 3 F 3 F- Φ Hi P- φ cn 3 d 50 F- DJ F1 ! UO P> d cπ F- 3 0 ω 3 F 3 F- Φ Hi P- φ cn 3 d 50 F- DJ F 1
3 ιQ P_ cn > F1 rf V 3 DJ r+ φ ιQ Φ INI Φ Φ cn rt Φ 3 3 rt ^ 3 d φ3 ιQ P_ cn> F 1 rf V 3 DJ r + φ ιQ Φ INI Φ Φ cn rt Φ 3 3 rt ^ 3 d φ
Φ Φ F- o cn O F- F Φ rt ≤ Φ 3^ Φ F d F- d • 3 d fr F- CL Hi 3 n N F rt o 0- O D 3 F- Φ F c 3 cn 3 3 • cn 3 F A 3 Φ ωΦ Φ F- o cn O F- F Φ rt ≤ Φ 3 ^ Φ F d F- d • 3 d for F- CL Hi 3 n NF rt o 0- OD 3 F- Φ F c 3 cn 3 3 • cn 3 FA 3 Φ ω
1 Φ F- CΛ Φ 3 Hi O iQ 3 DJ < rt Φ Φ DJ F- φ CL DJ Φ F- P- F-1 Φ F- CΛ Φ 3 Hi O iQ 3 DJ <rt Φ Φ DJ F- φ CL DJ Φ F- P- F-
S! F- O F Φ r+ er 3 Φ Φ vQ F- DJ 3 d φ tu A Hi rt σ 3 iQS! F- O F Φ r + er 3 Φ Φ vQ F- DJ 3 d φ tu A Hi rt σ 3 iQ
P- iQ 3 3 Q 3 3 Φ cn F er • Φ 3 tu Ω φ d 3 rt INI DJ DJ 3P- iQ 3 3 Q 3 3 Φ cn F er • Φ 3 tu Ω φ d 3 rt INI DJ DJ 3
3 r+ N Φ Φ !\J DJ r F- Φ <J F 0- F u Φ r CΛ F- φ o 3 d cn ω 3 DJ3 r + N Φ Φ! \ J DJ r F- Φ <J F 0- F for Λ r CΛ F- φ o 3 d cn ω 3 DJ
? -. DJ 3 3 φ π Hi ω F 3 M 3 ^ P- N Φ F- F r 3 3 Ω DJ O Φ CL? -. DJ 3 3 φ π Hi ω F 3 M 3 ^ P- N Φ F- F r 3 3 Ω DJ O Φ CL
Φ 3" * Φ F C: O DJ: . o C: φ ^ F- 3 3 3 Φ rt fr cn F F- a ΦΦ 3 " * Φ FC: O DJ:. O C: φ ^ F- 3 3 3 Φ rt for cn F F- a Φ
P1 F O F ^ vQ cn F F 3 3 cn « o F1 ω F- Φ Ω α 3 O F nP 1 FOF ^ vQ cn FF 3 3 cn «o F 1 ω F- Φ Ω α 3 OF n
Ό DJ DJ Φ 53 P_ F- r+ F1 . — . F- F- 3 fr 13 d Ω rt Φ 3 t 3 Φ Ω Hi yΌ DJ DJ Φ 53 P_ F- r + F 1 . -. F- F- 3 for 13 d Ω rt Φ 3 t 3 Φ Ω Hi y
O ω 3 H F- Φ C 3 ω 1+ O CL d 3 Φ F F F 3" d DJ 1 s: F- d 3 Ps- O 2 co ω Φ 1 3 F DJ Φ Cn 3" DJ O F SD P- er 3 F Φ 3 3 ΦO ω 3 H F- Φ C 3 ω 1+ O CL d 3 Φ FFF 3 " d DJ 1 s: F- d 3 Ps- O 2 co ω Φ 1 3 F DJ Φ Cn 3" DJ OF SD P- er 3 F Φ 3 3 Φ
F- F f cn O o cn cn Φ Fi rt Φ ^ ιQ rt φ r-1 Φ A o 3 A tr rt 3 φ ιQ φ J-- Φ 3 • 3J F- F DJ rt N Φ 3 F1 ^< ≤ Φ DJF- F f cn O o cn cn Φ Fi rt Φ ^ ιQ rt φ r- 1 Φ A o 3 A tr rt 3 φ ιQ φ J-- Φ 3 • 3 J F- F DJ rt N Φ 3 F 1 ^ <≤ Φ DJ
F- F- N F F- Cπ <! F F- F- r+ 1 3 3 er ?; F- α P- Φ fr C 3 Φ 3 rtF- F- N F F- Cπ <! F F- F- r + 1 3 3 er?; F- α P- Φ for C 3 Φ 3 rt
O rr << P* DJ CD ιQ r+ α IN! Φ Φ P- DJ Φ Φ 3 Φ cn tu 3 O: Φ O CLO rr << P * DJ CD ιQ r + α IN! Φ Φ P- DJ Φ Φ 3 Φ cn tu 3 O: Φ O CL
3 Φ r+ er INI F Φ Φ DJ: F F O CL cn rt Φ F rt F- cn 3 F * F-1 Φ N3 Φ r + er INI F Φ Φ DJ: FFO CL cn rt Φ F rt F- cn 3 F * F- 1 Φ N
Φ ιQ F- F- -» cn DJ: N er F1 F t er N 3 P- Ω F 3 F- 3 F Φ 3 SΦ ιQ F- F- - »cn DJ: N er F 1 F t er N 3 P- Ω F 3 F- 3 F Φ 3 S
3 F 3 3 rr 3" DJ Φ oo 3 Φ DJ Φ cn 3" F- Φ ω ?t L_J. cn uq φ ^ O 3 Φ3 F 3 3 rr 3 " DJ Φ oo 3 Φ DJ Φ cn 3 " F- Φ ω? T L_J. cn uq φ ^ O 3 Φ
O: Φ DJ 3 tr 3 o s Φ P- * 3 f F- Φ ^< O Φ T3 3 3 d 3 cn α F-O: Φ DJ 3 tr 3 os Φ P- * 3 f F- Φ ^ <O Φ T3 3 3 d 3 cn α F-
F- εp Φ DJ 3 Φ 3 o F- 3 F 3 er J 3 F DJ F P- F- 3F- εp Φ DJ 3 Φ 3 o F- 3 F 3 er J 3 F DJ F P- F- 3
3 Φ F tu ω α rt ω 3 O er (ϊ : Φ Φ 0 Ω er o F- P^ CL er cn vQ CL d3 Φ F tu ω α rt ω 3 O er (ϊ: Φ Φ 0 Ω er o F- P ^ CL er cn vQ CL d
§ l-i F cn < Φ F- . — . f CL Φ Φ er rt P- F 3" Φ Ω rt cn DJ Φ DJ 3 F 3§ li F cn <Φ F-. -. f CL Φ Φ er rt P- F 3 " Φ Ω rt cn DJ Φ DJ 3 F 3
Φ Φ Φ N O o 1+ φ Φ P- Φ Φ 3 ω 3^ F 3 3J N 3J F1 rt DJ Φ rtΦ Φ Φ NO o 1+ φ Φ P- Φ Φ 3 ω 3 ^ F 3 3 J N 3 J F 1 rt DJ Φ rt
F s: 3 3 s: F O 3" F fl Q F 3 DJ rt DJ O er Φ s: F- H ΦF s: 3 3 s: FO 3 " F fl QF 3 DJ rt DJ O er Φ s: F- H Φ
Φ r+ 3 F- F- Φ J-. DJ Ό Φ Ω 3 3 3 Φ F- F Φ 0 d FΦ r + 3 F- F- Φ J-. DJ Ό Φ Ω 3 3 3 Φ F- F Φ 0 d F
H 1 1 φ cn α er F- o er Cπ F- er LJ. TJ t F- o F- rt Φ F" 3 O 3 1H 1 1 φ cn α er F- or Cπ F- he LJ. TJ t F- o F- rt Φ F "3 O 3 1
P- O Φ Φ 3 o 1 O Φ φ o J Φ ω Ω φ F 3 F- ω > iQ cn 3 F F1 F 1 ω 3J 3 DJ - P- F- Φ F- S Φ 1 3 3 1 • cn 1 F- φ φ 1 Φ rt 3 3 3P- O Φ Φ 3 o 1 O Φ φ o J Φ ω Ω φ F 3 F- ω> iQ cn 3 FF 1 F 1 ω 3 J 3 DJ - P- F- Φ F- S Φ 1 3 3 1 • cn 1 F- φ φ 1 Φ rt 3 3 3
1 1 3 1+ 1 1 3 F er 1 1 1 1 3 1+ 1 1 3 F er 1 1
ω ω r NJ F1 cπ o cπ o cπ O cπω ω r NJ F 1 cπ o cπ o cπ O cπ
tu N ≤ Φ < ιQ rt P- DJ tu Φ tK H tu t-1 Hi 3 er α F1 CO A Ω H, ι d a O: er ω F- rt fr >U φ φ Φ F Φ Φ F- 3 d φ P- F 3 F d o Φ d F- F- DJ d * : H 3 Φ Hi Φ Ω Cn P- F Φtu N ≤ Φ <ιQ rt P- DJ tu Φ tK H tu t- 1 Hi 3 er α F 1 CO A Ω H, ι da O: er ω F- rt fr> U φ φ Φ F Φ Φ F- 3 d φ P- F 3 F do Φ d F- F- DJ d * : H 3 Φ Hi Φ Ω Cn P- F Φ
F F F- A F F ιQ cn Ω F- 3 DJ Φ Hi F> 3 3 Φ Ω d 3 Φ H Φ CL F Hi F- * rt A DJ FFF F- AFF ιQ cn Ω F- 3 DJ Φ Hi F > 3 3 Φ Ω d 3 Φ H Φ CL F Hi F- * rt A DJ F
Φ cn Φ cn c er er tr Φ Fi CL 3 rt iQ A A ω ^ ιQ cQ 3 F1 F- rt 3 3 P- d Hi 3Φ cn Φ cn c er er tr Φ Fi CL 3 rt iQ AA ω ^ ιQ cQ 3 F 1 F- rt 3 3 P- d Hi 3
P- Hi Φ F d Φ Φ CL F rt Φ 3 Hi Φ Φ cn φ Φ F d Ω 2 ^ φ 3 3 rt ΦP- Hi Φ F d Φ Φ CL F rt Φ 3 Hi Φ Φ cn φ Φ F d Ω 2 ^ φ 3 3 rt Φ
O Φ DJ: Ω F- ≤ cn DJ Φ cn F fr d: 3 φ F 3 O s: Φ 3 3J F1 3 o Φ d cQ 3 F tr n CL er cn Φ o 3 F CO rt F H α F- 3" Φ A Φ d Po 3 DJ rt F- Φ Φ F 3 CL er O π DJ 1 Φ CL 3 ω A F A 2! Φ er F- cn CL Hi DJ DJ CL cn trO Φ DJ: Ω F- ≤ cn DJ Φ cn F fr d: 3 φ F 3 O s: Φ 3 3 J F 1 3 o Φ d cQ 3 F tr n CL er cn Φ o 3 F CO rt FH α F - 3 " Φ A Φ d Po 3 DJ rt F- Φ Φ F 3 CL er O π DJ 1 Φ CL 3 ω AFA 2! Φ er F- cn CL Hi DJ DJ CL cn tr
< Φ Φ CL Φ tu DJ H, F H> d F Φ F1 DJ -~ Φ Φ 3 F1 Ω Φ 3 3 er Φ Ω DJ o F- Φ Hi Φ Φ F Φ 3 Hi DJ rt 3 F φ Ω Φ LQ 3 F φ tr • ω Φ vQ tr F 31 er<Φ Φ CL Φ tu DJ H, F H> d F Φ F 1 DJ - ~ Φ Φ 3 F 1 Ω Φ 3 3 er Φ Ω DJ o F- Φ Hi Φ Φ F Φ 3 Hi DJ rt 3 F φ Ω Φ LQ 3 F φ tr • ω Φ vQ tr F 3 1 er
3 cn LQ 3 F : 3 F Φ cn CL3 cn LQ 3 F: 3 F Φ cn CL
• 3 X 3 ιQ A F- tr F- F rt CL F- Φ 3 Φ DJ: F- Φ• 3 X 3 ιQ A F- tr F- F rt CL F- Φ 3 Φ DJ: F- Φ
O F A 3 F Φ rt DJ Φ F- DJ Φ Φ < rt < Ω O: CL Φ Φ er F N F1 3 tu 3 3 o O: Φ F- t P- F 3 ω cn 3 cn O d Φ " Φ F Φ 5 ≤ CL DJ iQ P- ΦOFA 3 F Φ rt DJ Φ F- DJ Φ Φ <rt <Ω O: CL Φ Φ er FNF 1 3 tu 3 3 o O: Φ F- t P- F 3 ω cn 3 cn O d Φ " Φ F Φ 5 ≤ CL DJ iQ P- Φ
£P ω rt CL D Φ Φ 3 CL ιQ Ω Φ F 3 F Φ F 3" 3 X O Φ Φ Cn F- 3 <£ P ω rt CL D Φ Φ 3 CL ιQ Ω Φ F 3 F Φ F 3 " 3 XO Φ Φ Cn F- 3 <
-J F- rt >es rt F- F- F- rt g 3 Φ ιQ tr CL rt DJ ιQ 3" cn F DJ 3 • F er F- cn ω iQ F- CL Φ φ 3 φ Φ Φ Φ 3 F d Φ 3 Φ F- Φ N er DJ P- A er DJ DJ CD rt Φ DJ DJ F er iQ O: F- F" F- 3 3 3^ 3 F rt Φ ιQ H 3 ≤ F Φ Ω cc Fi F- Φ Φ 3 α cn cn cn-J F- rt > es rt F- F- F- rt g 3 Φ ιQ tr CL rt DJ ιQ 3 " cn F DJ 3 • F er F- cn ω iQ F- CL Φ φ 3 φ Φ Φ Φ 3 F d Φ 3 Φ F- Φ N er DJ P- A he DJ DJ CD rt Φ DJ DJ F er iQ O: F- F "F- 3 3 3 ^ 3 F rt Φ ιQ H 3 ≤ F Φ Ω cc Fi F - Φ Φ 3 α cn cn cn
P- Φ A Ω rt t cn Φ Φ A A rt Φ Φ P- Φ rt CL Φ O: 3 3- F- rt 3 F DJ cn d co 3 P1 " F Φ F- er Φ Φ er 3 3 ω • F P -< Φ Φ cn CL cn <i <! σ ΩP- Φ A Ω rt t cn Φ Φ AA rt Φ Φ P- Φ rt CL Φ O: 3 3- F- rt 3 F DJ cn d co 3 P 1 " F Φ F- er Φ Φ er 3 3 ω • FP - <Φ Φ cn CL cn <i <! Σ Ω
F- Φ d Φ « 3 cn α F 3 < φ cn Ω F1 CL Φ F- F rt P- tu er d O Φ F ^F- Φ d Φ «3 cn α F 3 <φ cn Ω F 1 CL Φ F- F rt P- tu er d O Φ F ^
P1 Ω F 3 3 P- s; Φ Φ 3 DJ o rt < T3 3" DJ: Φ F CL 3 DJ O Φ F- Φ F 3 3 φ ΦP 1 Ω F 3 3 P- s; Φ Φ 3 DJ location <T3 3 "DJ: Φ F CL 3 DJ O Φ F- Φ F 3 3 φ Φ
F- 3J rt CL 3 Ω DJ F- F P- < 3 F F O F F- cn 3 P- DJ d Hi cn 3 3 CL • rt tr o Φ Φ . fT 3" 3 A rt o N Φ F F- cn ^ Φ 3 cn Hi Φ Φ F- N ιQF- 3 J rt CL 3 Ω DJ F- F P- <3 FFOF F- cn 3 P- DJ d Hi cn 3 3 CL • rt tr o Φ Φ. fT 3 "3 A rt o N Φ F F- cn ^ Φ 3 cn Hi Φ Φ F- N ιQ
. DJ F rt CL Φ O F N d Fi DJ rt CL rt Φ CL A DJ tu • DJ F1 DJ Φ o ^ tr1 F" DJ d Hl 3 Φ O DJ s: A Fi er N Φ CL F F- Φ Hi d S cn F- d Φ 3" N φ F Φ cn Hi 3 F ω s; Φ er Φ Φ Φ Φ Φ F w F- 3 F O DJ Φ cn 3 n Φ s: DJ A rt A Φ Ω F- s: Φ Ω er 3 F- F rt F- Φ Φ F1 H F <5 H 3 F- < F-, DJ F rt CL Φ OFN d Fi DJ rt CL rt Φ CL A DJ tu • DJ F 1 DJ Φ o ^ tr 1 F "DJ d Hl 3 Φ O DJ s: A Fi er N Φ CL F F- Φ Hi d S cn F- d Φ 3 "N φ F Φ cn Hi 3 F ω s; Φ er Φ Φ Φ Φ Φ F w F- 3 FO DJ Φ cn 3 n Φ s: DJ A rt A Φ Ω F- s: Φ Ω er 3 F- F rt F- Φ Φ F 1 HF <5 H 3 F- <F-
F- Hi er F, 3 ω F- 3J Ω P- F- fr Φ CL 3 Ω 3 er LQ P- rt Φ DJ CL s: g Φ AF- Hi er F, 3 ω F- 3 J Ω P- F- fr Φ CL 3 Ω 3 er LQ P- rt Φ DJ CL s: g Φ A
Ω rt Φ DJ Hi Φ DJ tr Ω 3 3 3 Φ cn F- 3" L_l. CL Φ Φ rt rt Φ 3 cn Φ Φ g F rt - cn 3 cn ω DJ n Hi er tr ω DJ: • 3 O 3 CL ^« φ Φ F DJ •^ DJ: rt cn F F1 φ 3" » rt rt DJ rt Ω r - rt d er Ό tP F DJ CL 3 d rt er P- <! cn Ω F DJ d O 3 Φ " er Φ 3 d F F- INI F- > N « O t H) CL Φ Φ 3T 1 CLΩ rt Φ DJ Hi Φ DJ tr Ω 3 3 3 Φ cn F- 3 " L_l. CL Φ Φ rt rt Φ 3 cn Φ Φ g F rt - cn 3 cn ω DJ n Hi er tr ω DJ: • 3 O 3 CL ^ «φ Φ F DJ • ^ DJ: rt cn FF 1 φ 3" »rt rt DJ rt Ω r - rt d er Ό tP F DJ CL 3 d rt er P- <! cn Ω F DJ d O 3 Φ " er Φ 3 d F F- INI F-> N« O t H) CL Φ Φ 3T 1 CL
3 Hi F- O 3 3 A 3 F- ιQ ^ rt er d F- Ω ω φ cn DJ Hι F- c 3 DJ Φ A rt DJ ιQ Hi DJ S 3 F F1 ω vQ rt Φ N tr Φ tr rt F- Ω ω d= rt d F Φ cn ω 3 H Φ Φ φ DJ Hi ω N F F- Φ DJ: DJ F 31 tr cn F A Φ P- ω Φ 3 cn3 Hi F- O 3 3 A 3 F- ιQ ^ rt er d F- Ω ω φ cn DJ Hι F- c 3 DJ Φ A rt DJ ιQ Hi DJ S 3 FF 1 ω vQ rt Φ N tr Φ tr rt F - Ω ω d = rt d F Φ cn ω 3 H Φ Φ φ DJ Hi ω NF F- Φ DJ: DJ F 3 1 tr cn FA Φ P- ω Φ 3 cn
Hi Φ cn F 3 3 d Φ DJ Fi Φ ≤ 3 F 3 d er Hi O: Φ F- F- iQ T1 P-Hi Φ cn F 3 3 d Φ DJ Fi Φ ≤ 3 F 3 d er Hi O: Φ F- F- iQ T1 P-
DJ 3 er Hi F fr DJ F Φ 3 cn Φ d: 3 3 DJ er DJ φ 3 cn φ O Ω F- er fr ι ω Φ Φ Ξ <J er ^ F- φ d F- 3 F F d Hi A φ F1 F- Φ CL CO tr 3 Φ rt Φ rt P- Φ Φ tu O er cn F 3 A d Φ 3 O rt F- F" Ω 3 Φ F F- P-DJ 3 er Hi F for DJ F Φ 3 cn Φ d: 3 3 DJ er DJ φ 3 cn φ O Ω F- er fr ι ω Φ Φ Ξ <J er ^ F- φ d F- 3 FF d Hi A φ F 1 F- Φ CL CO tr 3 Φ rt Φ rt P- Φ Φ tu O er cn F 3 A d Φ 3 O rt F- F "Ω 3 Φ F F- P-
O DJ F- 3 F F F F O d Φ fr rt F- DJ A F1 Φ 3 Φ tr F- d: rt o t 3O DJ F- 3 FFFFO d Φ fr rt F- DJ AF 1 Φ 3 Φ tr F- d: rt ot 3
F Φ 3 3 Φ CL 3" Φ Φ F F er Φ N rt cn A 3 Φ N 3 Ω F- ΦF Φ 3 3 Φ CL 3 "Φ Φ F F er Φ N rt cn A 3 Φ N 3 Ω F- Φ
Φ F- C F Φ DJ 3 3 Φ Ω ω N CL F- Φ cn F1 A Φ CΛ CΛ F ≤. Φ ?T O Φ α>Φ F- CF Φ DJ 3 3 Φ Ω ω N CL F- Φ cn F 1 A Φ CΛ CΛ F ≤. Φ? TO Φ α>
3 3 DJ 3 F" 3 3 * o ≤ Φ rt 3 Φ Φ tsi rt rt Φ 3 rt 3 F DJ rt3 3 DJ 3 F "3 3 * o ≤ Φ rt 3 Φ Φ tsi rt rt Φ 3 rt 3 F DJ rt
Φ F DJ t er PT 3 • 3 F- ω F- ■< DJ DJ co F- "* rt- DJ er ω L cn DJ CL Φ F d: er S < <! 3 CO Ω 3- F F rt rt Φ α N F- FΦ F DJ t er PT 3 • 3 F- ω F- ■ <DJ DJ co F- " * rt- DJ er ω L cn DJ CL Φ F d: er S <<! 3 CO Ω 3- FF rt rt Φ α N F- F
Φ 3 d DJ 3 DJ cn Φ d o N o CL rt tr F F- rt rt DJ Φ F 3^ P- d O rtΦ 3 d DJ 3 DJ cn Φ do N o CL rt tr F F- rt rt DJ Φ F 3 ^ P- d O rt
F- < Φ N F " Pi cn cn F1 F Φ d 3 F- CL DJ s; Φ 3 ω F 3 cn DJ Φ 3 3 ω o 3 Φ Φ Φ rt Φ rt rt ** F Φ Φ F F- F L DJ rt rt rt F- ΦF- <Φ NF " Pi cn cn F 1 F Φ d 3 F- CL DJ s; Φ 3 ω F 3 cn DJ Φ 3 3 ω o 3 Φ Φ Φ rt Φ rt rt * * F Φ Φ F F-FL DJ rt rt rt F- Φ
Ό F tQ 3 F- F er 3 3 P- P- Φ F rt 3 Φ d d rt ^~. Φ tu 3 N F-Ό F tQ 3 F- F er 3 3 P- P- Φ F rt 3 Φ dd rt ^ ~. Φ do 3 N F-
F- DJ Φ rt * Φ DJ g } σ F Φ t cn O. tu F Ω 3 Φ 3^ 3 C F CL d 3 φ er F Φ N F cn 3 g DJ F SS F F tu P- Φ 3" vQ 3 O: P- φ φ ΦF- DJ Φ rt * Φ DJ g} σ F Φ t cn O. tu F Ω 3 Φ 3 ^ 3 CF CL d 3 φ er F Φ NF cn 3 g DJ F SS FF tu P- Φ 3 " vQ 3 O : P- φ φ Φ
Φ er DJ ≤ d: Ω DJ rt F- cn Φ DJ DJ Φ F- A DJ Φ Φ T) tr S Φ 3 cn α F ω P- Φ Φ Ω tr rt fr ω t F ta Hi ω 3 fr d 3 Hi Φ φ Φ 3 rt Φ s: 3 F- Φ d o f F- d: ≤ DJ N rt Φ rt Ω φ Fi rt F- DJ: F F F O fr F tuDJ er DJ ≤ d: Ω DJ rt F- cn Φ DJ DJ Φ F- A DJ Φ Φ T) tr S Φ 3 cn α F ω P- Φ Φ Ω tr rt fr ω t F ta Hi ω 3 fr d 3 Hi Φ φ Φ 3 rt Φ s: 3 F- Φ dof F- d: ≤ DJ N rt Φ rt Ω φ Fi rt F- DJ: FFFO fr F tu
Φ cn cn F & cn 3 F Φ rt CL DJ Φ F- ω tr P- Cn cn Φ " DJ Φ rt F H DJ: FΦ cn cn F & cn 3 F Φ rt CL DJ Φ F- ω tr P- Cn cn Φ "DJ Φ rt F H DJ: F
F- Ό Ό CΛ Ω 3 F- φ F1 F P- F- tr 3 - rt F Φ er Ω Ό F rt 3 Φ DJ tr tu Φ O F P- rt 3" DJ: Ω ** F- CL 0 Φ φ o Φ CD Φ 3- F t-1 d — 3- Fi 3 Φ 3F- Ό Ό CΛ Ω 3 F- φ F 1 F P- F- tr 3 - rt F Φ er Ω Ό F rt 3 Φ DJ tr tu Φ OF P- rt 3 " DJ: Ω * * F- CL 0 Φ φ o Φ CD Φ 3- F t- 1 d - 3- Fi 3 Φ 3
Φ P- φ Φ E * Ω Φ 3 Φ 3 Hi P- Φ 3 F1 Φ d F er N rt rt 3 rt H d F- 1 3* 3 3 1 Hi 1 3 DJ 1 Hi Φ DJ 3 F- J: 1Φ P- φ Φ E * Ω Φ 3 Φ 3 Hi P- Φ 3 F 1 Φ d F er N rt rt 3 rt H d F- 1 3 * 3 3 1 Hi 1 3 DJ 1 Hi Φ DJ 3 F- J : 1
F- 1 cn 1 1 1 rt P- 1 rt P- 3' DJ Ω 1F- 1 cn 1 1 1 rt P- 1 rt P- 3 'DJ Ω 1
3 1 F 1 3 1 3 1 tr 3 1 F 1 3 1 3 1 dr
Das erfindungsgemäße Verfahren lässt sich grundsätzlich bei beliebigen Vorabeinspritzstrategien einsetzen, beispielsweise auch bei dem Verfahren nach der eingangs diskutierten EP 0 371 158 Bl, bei der die Vorabeinspritzer einer ersten Zylin- dergruppe zeitgleich und die Vorabeinspritzer der zweiten Zylindergruppe zeitlich verzögert abgesetzt werden. Mit besonders gutem Erfolg wird das erfindungsgemäße Verfahren jedoch bei einer Vorabeinspritzstrategie eingesetzt, bei der sämtliche Vorabeinspritzer in zeitlicher Reihenfolge nacheinander abgesetzt werden. Ein Beispiel für eine derartige Vorabeinspritzstrategie wird im folgenden anhand der Figur 2 näher erläutert.The method according to the invention can in principle be used in any pre-injection strategies, for example also in the method according to EP 0 371 158 B1 discussed above, in which the pre-injectors of a first cylinder group are released at the same time and the pre-injectors of the second cylinder group are delayed in time. However, the method according to the invention is used with particularly good success in a pre-injection strategy in which all the pre-injectors are placed one after the other in chronological order. An example of such a pre-injection strategy is explained in more detail below with reference to FIG. 2.
In der unteren Hälfte der Figur 2 sind neben dem Kurbelwel- lensignal CRK und dem Nockenwellensignal CAM die Drehzahl N der Brennkraftmaschine über der Zeit aufgetragen. In der oberen Hälfte der Figur 2 sind für die vier Zylinder 1 bis 4 der Vierzylinder-Brennkraftmaschine die Ansteuersignale IV1 - IV4 für die vier Einspritzventile über der Zeit aufgetragen, wo- bei die vier Vorabeinspritzer I mit II - 14 bezeichnet sind. Außerdem sind die Ansteuersignale EV1 - EV4 für die vier Einlassventile über der Zeit aufgetragen, wobei die Öffnungsimpulse für die Öffnung der Einlassventile mit El - E4 bezeichnet sind. Außerdem sind in den beiden obersten Zeilen der Fi- gur 2 die Impulse für den oberen Totpunkt (TDC1 - TDC4) der vier Zylinder bzw. den oberen Totpunkt (TDC1) des Zylinders 1 dargestellt .In the lower half of FIG. 2, in addition to the crankshaft signal CRK and the camshaft signal CAM, the speed N of the internal combustion engine is plotted over time. In the upper half of FIG. 2, the control signals IV1 - IV4 for the four injection valves are plotted over time for the four cylinders 1 to 4 of the four-cylinder internal combustion engine, the four pilot injectors I being designated II - 14. In addition, the control signals EV1-EV4 for the four intake valves are plotted over time, the opening pulses for the opening of the intake valves being designated E1-E4. In addition, the top two lines of FIG. 2 show the pulses for the top dead center (TDC1-TDC4) of the four cylinders and the top dead center (TDC1) of the cylinder 1.
Wie in Figur 2 in Zusammenhang mit der Drehzahl angedeutet, ist für den Start der Brennkraftmaschine eine Starterkennung E vorgesehen. Zu diesem Zeitpunkt ist das Nockenwellensignal CAM entweder hoch- oder niederpegelig, im Beispiel der Figur 2 niederpegelig. Damit können - z.B. wie bei dem eingangs beschriebenen Verfahren nach der EP 0 371 158 Bl - die Zylinder 1 bis 4 in zwei Gruppen unterteilt werden (im Beispiel derAs indicated in FIG. 2 in connection with the speed, a starter identification E is provided for starting the internal combustion engine. At this time, the camshaft signal CAM is either high or low, in the example in FIG. 2 low. With this - e.g. as in the method described at the outset according to EP 0 371 158 B1 - the cylinders 1 to 4 are divided into two groups (in the example the
Figur 2 in eine erste Gruppe mit den Zylindern 3, 4 und einer zweiten Gruppe mit den Zylindern 1, 2) . Außerdem ist hier- co co ro ιo F1 F1 cπ o cπ o Cπ O Cπ ω tu CL u cn ! cn cn < S! rt D 1 cn <! CL Q < G N CL CL er cn CL t cn to er CL er F- Φ Φ et d er cπ O O P- Φ Φ P- Φ Φ Φ Φ ω er d : d Φ Φ X) Φ φ rt F rt Φ dFigure 2 in a first group with the cylinders 3, 4 and a second group with the cylinders 1, 2). In addition, co co ro ιo F 1 F 1 cπ o cπ o Cπ O Cπ ω tu CL u cn! cn cn <S! rt D 1 cn <! CL Q <GN CL CL er cn CL t cn to er CL er F- Φ Φ et d er cπ OO P- Φ Φ P- Φ Φ Φ Φ ω er d: d Φ Φ X) Φ φ rt F rt Φ d
Φ φ P- F - Φ F Φ O tr F φ rt F iQ 3 3 F 3 F φ ιQ F F F P" F- 3 P- DJ d: F- F- FΦ φ P- F - Φ F Φ O tr F φ rt F iQ 3 3 F 3 F φ ιQ F F F P "F- 3 P- DJ d: F- F- F
3* cn DJ tr er tr P- DJ Φ d rt DJ: er F φ CL Ω ιQ s: φ 3 Ω H α Ω3 * cn DJ tr er tr P- DJ Φ d rt DJ: er F φ CL Ω ιQ s: φ 3 Ω H α Ω
Φ ^ xs Φ F1 φ Φ Φ O 3 er er < F P- P- CO cP F Fi 3" Φ tr F Φ F1 P- CL fr H Φ trΦ ^ xs Φ F 1 φ Φ Φ O 3 er <F P- P- CO cP F Fi 3 " Φ tr F Φ F 1 P- CL for H Φ tr
3 c F- F co 3 F1 3 C Φ φ Φ tr1 O o F" rt DJ Φ O: d cn 3 Φ cn rt cn 33 c F- F co 3 F 1 3 C Φ φ Φ tr 1 O o F "rt DJ Φ O: d cn 3 Φ cn rt cn 3
F Φ cn o ≤ Φ P- F F- F M rt DJ 3 rt F l_l. CL 13 F" « 3 1 rt DJ cQ er P1 et A Φ ιQ F DJ 3 Φ 3 DJ 3 F Φ 3 rt F- φ F- 13 Φ Φ < S3 DJ ω dF Φ cn o ≤ Φ P- F F- FM rt DJ 3 rt F l_l. CL 13 F "« 3 1 rt DJ cQ er P 1 et A Φ ιQ F DJ 3 Φ 3 DJ 3 F Φ 3 rt F- φ F- 13 Φ Φ <S3 DJ ω d
Φ Φ Φ to Φ F1 φ 3 n F- F- er P- F- rt F rt d ^Q CL φ φ 3 F- O <! P- F 3 rt O er CL o er 1 er to X) rt Φ Φ cn 3 rt Φ Φ 3 Φ O cn cn F O 3 Φ F- trΦ Φ Φ to Φ F 1 φ 3 n F- F- er P- F- rt F rt d ^ Q CL φ φ 3 F- O <! P- F 3 rt O er CL or 1 er to X) rt Φ Φ cn 3 rt Φ Φ 3 Φ O cn cn FO 3 Φ F- tr
P" s; Φ to Φ O CL F cn F- rt p- F er 3 A 3 Ω < N Φ Φ A F fr ωP "s; Φ to Φ O CL F cn F- rt p- F er 3 A 3 Ω <N Φ Φ A F fr ω
F- Φ F ^ INI F- P- Φ F- d 3 rt to P 1 Φ 3 O φ 3 Φ er φ d 13 P* er φ H 3 DJ: Φ IO Φ INI F rt Φ ω CL F- Φ <! L tu F F- cn 3 A Φ H N O cn Φ er F1 fU Ω 3" er O er DJ: N F DJ X) F- Ω 3 o F Φ P- CL DJ rt O DJ Φ K 13 F- cn rt frF- Φ F ^ INI F- P- Φ F- d 3 rt to P 1 Φ 3 O φ 3 Φ er φ d 13 P * er φ H 3 DJ: Φ IO Φ INI F rt Φ ω CL F- Φ < ! L tu F F- cn 3 A Φ HNO cn Φ er F 1 fU Ω 3 " er O er DJ: NF DJ X) F- Ω 3 o F Φ P- CL DJ rt O DJ Φ K 13 F- cn rt fr
Φ Φ F- 3" 3 Φ Φ 3- Φ Φ 3 F Φ Φ 3J 3 F DJ ω 3 Φ er A F Ω er DJ O φ F- DJ DJΦ Φ F- 3 "3 Φ Φ 3- Φ Φ 3 F Φ Φ 3 J 3 F DJ ω 3 Φ AF Ω er DJ O φ F- DJ DJ
3 KQ F φ 3 INI 3 3 F F DJ: iQ F- cn 3 Φ d N Hi P1 F Φ cn 3^ Φ 3 cn F rt 3 33 KQ F φ 3 INI 3 3 FF DJ: iQ F- cn 3 Φ d N Hi P 1 F Φ cn 3 ^ Φ 3 cn F rt 3 3
IO d o • J: Φ cn cn 3- Φ rt F 3 d rt ^ DJ P- Φ - — 3 3 P- rt F- CL 3IO d o • J: Φ cn cn 3- Φ rt F 3 d rt ^ DJ P- Φ - - 3 3 P- rt F- CL 3
≤ O F 3 3 tr F- rt 3 CL N CL < tr A ιQ n F cn < 3 F- DJ Φ rt rt O • ω rt≤ O F 3 3 tr F- rt 3 CL N CL <tr A ιQ n F cn <3 F- DJ Φ rt rt O • ω rt
DJ F DJ ■2, 3 cn <! Φ Pt rt Φ Φ Φ o Φ er rt DJ cn O cn Ω CL Ω 3 Φ F- cn 3 1 ^ DJ F DJ ■ 2, 3 cn <! Φ Pt rt Φ Φ Φ o Φ er rt DJ cn O cn Ω CL Ω 3 Φ F- cn 3 1 ^
F INI to cn o Φ Φ rt O 3 *- d F F F P- tu Φ O Hi <5 F 13 * P- " 3 O F- Φ sF INI to cn o Φ Φ rt O 3 * - d FFF P- tu Φ O Hi <5 F 13 * P- "3 O F- Φ s
• DJ: DJ - 3 • F rt DJ rt 3 Hi rt Φ DJ F Φ rt s; 3 Ω 3 P- o ^ CL rt 3 <! O 3 P- Φ H INI er 3 Hi cn 3 er F- 3 F- < Φ tr 3 er to 3 φ P- O tu CL O cn rt CO •< Φ A d < cn et et Φ et F- er Φ 3 Φ 3 cn ?-• DJ: DJ - 3 • F rt DJ rt 3 Hi rt Φ DJ F Φ rt s; 3 Ω 3 P- o ^ CL rt 3 <! O 3 P- Φ H INI er 3 Hi cn 3 er F- 3 F- <Φ tr 3 er to 3 φ P- O tu CL O cn rt CO • <Φ A d <cn et et Φ et F- er Φ 3 Φ 3 cn? -
O Φ F o Φ CL F Φ φ Φ Ω rt ~> - F- Φ F O O F- P- N rt Φ F r F CL rt Φ CL er 3 3 DJ F- 3 F tr P- 3 cn F Hi Hi 3 Φ F- fT Φ Hi DJ P- Φ F" P- J <! f cn 3" N N s: 3 cn O CL DJ d: Hi cn cn F CL CL DJ F1 DJ d φ tr 13 φO Φ F o Φ CL F Φ φ Φ Ω rt ~> - F- Φ FOO F- P- N rt Φ F r F CL rt Φ CL er 3 3 DJ F- 3 F tr P- 3 cn F Hi Hi 3 Φ F- fT Φ Hi DJ P- Φ F "P- J <! F cn 3 " NN s: 3 cn O CL DJ d: Hi cn cn F CL CL DJ F 1 DJ d φ tr 13 φ
F1 O DJ P- φ Φ Φ CL φ N 3 d d F- CL •Ö tr Φ er tr 1 13 Φ Φ 3 DJ tr Hi φ OF 1 O DJ P- φ Φ Φ CL φ N 3 dd F- CL • Ö tr Φ er tr 1 13 Φ Φ 3 DJ tr Hi φ O
CL F 3 F F 3 Φ F s; F- 3 F Φ F F- F Φ F F1 tu F Ft 3 3 3 er F > 3 cn tuCL F 3 FF 3 Φ F s; F- 3 F Φ F F- F Φ FF 1 tu F Ft 3 3 3 er F> 3 cn tu
F1 13 cn 3 cn Φ Ω CL CL F F- O L-J. F- φ d < F- co rt cn Φ N 3 F- FF 1 13 cn 3 cn Φ Ω CL CL F F- O LJ. F- φ d <F- co rt cn Φ N 3 F- F
CL d rt 3 Φ rt F- 3- C J P- rt cn φ 3 3 Hi co rt " < INI Φ rt 3 s: N A rt φCL d rt 3 Φ rt F- 3- C J P- rt cn φ 3 3 Hi co rt "<INI Φ rt 3 s: N A rt φ
Φ Φ P- F1 Φ DJ F tu Φ rt rt Φ Φ CL .fc> N cn 3 cn rt N O • 3 DJ φ DJ Φ F- 3Φ Φ P- F 1 Φ DJ F tu Φ rt rt Φ Φ CL .fc> N cn 3 cn rt NO • 3 DJ φ DJ Φ F- 3
F 3 cn ω 3 Ω cn φ 3 Φ F- cn DJ Φ Φ F- 3 s: 1 DJ Φ d F 3 3 F- tr er O 3 rt " rt P- 3 er rt Φ i 3 F 3 A F d: Q er F 3 DJ F- d CL DJ 3 fr o CO — co < Φ cn to Φ S 3 Φ F- Φ F- F Φ iQ CL er 3 3 Ω P- Φ FF 3 cn ω 3 Ω cn φ 3 Φ F- cn DJ Φ Φ F- 3 s: 1 DJ Φ d F 3 3 F- tr er O 3 rt " rt P- 3 er rt Φ i 3 F 3 AF d: Q er F 3 DJ F- d CL DJ 3 fr o CO - co <Φ cn to Φ S 3 Φ F- Φ F- F Φ iQ CL er 3 3 Ω P- Φ F
* ^ O M 3 13 *< to fr d ιQ rt < O rt CL 3 Φ H Φ CL N tr CL φ 3 DJ* ^ O M 3 13 * <to fr d ιQ rt <O rt CL 3 Φ H Φ CL N tr CL φ 3 DJ
3 3 DJ F 00 P- 3 rt DJ 3 tsi Φ Φ CL INI N Φ F- A CO d3 3 DJ F 00 P- 3 rt DJ 3 tsi Φ Φ CL INI N Φ F- A CO d
DJ co Φ Ω P- 3 Ps- Φ 3 F Φ > cn • cn ^» P) P- φ φ er HDJ co Φ Ω P- 3 Ps- Φ 3 F Φ > cn • cn ^ »P) P- φ φ er H
Ω Ω ω d Φ J-- 3 F A F CL F Φ O rtΩ Ω ω d Φ J-- 3 F A F CL F Φ O rt
3J 3" o Hi er IN) >< F1 tr P" 3 et P- ^ Φ cn F F1 rt Ω er cn d: Φ 3 CL 33 J 3 " o Hi er IN)><F 1 tr P" 3 et P- ^ Φ cn FF 1 rt Ω er cn d: Φ 3 CL 3
F F ιQ Φ DJ: 3 F F1 rt rt 3 O F- F tr Φ fr DJ 13 CO F1 to F d Φ DJFF ιQ Φ DJ: 3 FF 1 rt rt 3 O F- F tr Φ for DJ 13 CO F 1 to F d Φ DJ
O 0 F- φ P- tr Ω p_ 0 cn ** CL X) € F d: 3 DJ ω 3 d 3 F •«» rt rt 3 F- F cnO 0 F- φ P- tr Ω p_ 0 cn * * CL X) € F d: 3 DJ ω 3 d 3 F • «» rt rt 3 F- F cn
3 3 01 et 3 3 3* Φ 3 rt Φ d F- < A er α rt F A P- P- DJ t er cn Ω3 3 01 et 3 3 3 * Φ 3 rt Φ d F- <A er α rt FA P- P- DJ t er cn Ω
F- F- et F cn Φ F F F- DJ O F 3 Φ O er φ Φ Φ d s: N Φ rt J-. A F Φ rt C tr ω cn Φ 13 3 O n 3 er fr F » F F A 3 Φ CL N Φ rt fr • Φ F-F- F- et F cn Φ F F F- DJ O F 3 Φ O er φ Φ Φ d s: N Φ rt J-. A F Φ rt C tr ω cn Φ 13 3 O n 3 er fr F »F F A 3 Φ CL N Φ rt fr • Φ F-
DJ DJ Φ rt F 3 ^ DJ α > et DJ F- CL F <! Φ Φ α 3 Φ O DJ 3 3 rt rt F Φ F- DJ F- P- rt cn L er d er F- F- Φ CL O d F Φ F 3 > ΦDJ DJ Φ rt F 3 ^ DJ α> et DJ F- CL F <! Φ Φ α 3 Φ O DJ 3 3 rt rt F Φ F- DJ F- P- rt cn L er d er F- F- Φ CL O d F Φ F 3> Φ
F- F- 3 et er cn ιQ F- 1 F- ιQ 3 F Φ 3 Φ o_ N Φ F rt 3 F INI r co 3 3 NF- F- 3 et er cn ιQ F- 1 F- ιQ 3 F Φ 3 Φ o_ N Φ F rt 3 F INI r co 3 3 N
O O Φ N DJ d O s: Φ DJ F- Ω F- ι φ s: d 3 Φ J: Φ ^1 rt CL s: F-O O Φ N DJ d O s: Φ DJ F- Ω F- ι φ s: d 3 Φ J: Φ ^ 1 rt CL s: F-
3 3 3 F- Φ ω et F 3 F- er Ω tr 3 tu Φ cn F- 3 -* to et < Φ tr 3 Φ Φ Φ 3 cn ω 3 cn F rt F- cn 3 tu Φ 3* cn Φ 3 cn F Ω Φ F 3 3 3 F F-3 3 3 F- Φ ω et F 3 F- er Ω tr 3 tu Φ cn F- 3 - * to et <Φ tr 3 Φ Φ Φ 3 cn ω 3 cn F rt F- cn 3 tu Φ 3 * cn Φ 3 cn F Ω Φ F 3 3 3 F F-
F- F- er rt DJ O t P- W F rt Φ Ό F- CL Φ CL ≤ tr μ. F cn Φ d F1 cn rt CLF- F- er rt DJ O t P- WF rt Φ Ό F- CL Φ CL ≤ tr μ. F cn Φ d F 1 cn rt CL
3 3 DJ H F 3 3 Φ ro CL F- F C0 3 d DJ F1 cn n rt t Φ Φ3 3 DJ HF 3 3 Φ ro CL F- F C0 3 d DJ F 1 cn n rt t Φ Φ
X! X) F . — 3 3 Cπ oX! X) F. - 3 3 Cπ o
J-» et ω F- •σ F1 3 Φ DJ 3 F- 13 CL co co F- rt O Φ A CD rt DJ 3 3 d d ** t, - — Φ p- ω d X) 3 cn er φ rt F- Φ tu DJ cn φ • F 3 CL F- dJ- »et ω F- • σ F 1 3 Φ DJ 3 F- 13 CL co co F- rt O Φ A CD rt DJ 3 3 dd * * t, - - Φ p- ω d X) 3 cn er φ rt F- Φ tu DJ cn φ • F 3 CL F- d
F" F1 DJ F fT A N Φ ω er Φ cn cn CL cn er fr Ü 13i rt o F- tr rt N tP A Φ u t F1 ω cn cn F φ Φ A Φ Ω 3 Φ O d φ tc et INI cn F- ιQ Φ FF "F 1 DJ F fT AN Φ ω er Φ cn cn CL cn er fr Ü 13i rt o F- tr rt N tP A Φ ut F 1 ω cn cn F φ Φ A Φ Ω 3 Φ O d φ tc et INI cn F- ιQ Φ F
DJ Φ φ d C F- DJ F A Φ F tr F1 F tP 3 F- ^ 1 Φ F- cn o CO Cn F- F 3 F1 P- to rt Hi cn φ XS DJ Φ Φ t er 1 CL rt cn 3 Φ 3 cn Φ — P- rt rt er d H Φ o ω 3 d F- CL F Z F- d Φ Φ φ ΦDJ Φ φ d C F- DJ FA Φ F tr F 1 F tP 3 F- ^ 1 Φ F- cn o CO Cn F- F 3 F 1 P- to rt Hi cn φ XS DJ Φ Φ t er 1 CL rt cn 3 Φ 3 cn Φ - P- rt rt er d H Φ o ω 3 d F- CL FZ F- d Φ Φ φ Φ
P- d O 3 Φ Φ 3 *> F cn cn DJ 3 3 Φ er F- 3 F F- F 3 3 rt 3 to 3 DJ 3 3 Ps1 • 1 1 Ω 1 Φ cn Φ Φ 1 1 1 1 cn ιQ ! • 1 tr F F- P- d O 3 Φ Φ 3 *> F cn cn DJ 3 3 Φ er F- 3 F F- F 3 3 rt 3 to 3 DJ 3 3 Ps 1 • 1 1 Ω 1 Φ cn Φ Φ 1 1 1 1 cn ιQ! • 1 tr F F-
aufgetreten ist, ist die Brennkraftmaschine synchronisiert, und somit kann eine definierte Reihenfolge der nach dem Synchronisationsimpuls S erfolgenden Vorabeinspritzer von dem zentralen Steuergerät 1 bestimmt werden.has occurred, the internal combustion engine is synchronized, and thus a defined sequence of the pre-injections occurring after the synchronization pulse S can be determined by the central control unit 1.
Wie aus Figur 2 ersichtlich, ergibt sich bei dieser Vorabeinspritzstrategie eine definierte Reihenfolge der nacheinander mit Vorabeinspritzern I versorgten Zylinder, im dargestellten Fall Zylinder 4, Zylinder 1, Zylinder 2 und Zylinder 3. Die Kraftstoffmengen der zugehörigen Vorabeinspritzer 14, II, 12 und 13 werden durch Multiplikation der Standardmenge mit den fest vorgegebenen Gewichtungsfaktoren bestimmt.As can be seen from FIG. 2, this pre-injection strategy results in a defined sequence of the cylinders supplied with pre-injectors I one after the other, in the illustrated case cylinder 4, cylinder 1, cylinder 2 and cylinder 3. The fuel quantities of the associated pre-injectors 14, II, 12 and 13 become determined by multiplying the standard quantity by the fixed weighting factors.
Wenn die Brennkraftmaschine an einer der anderen drei mögli- chen Stillstands-Winkelpositionen stehen geblieben ist, so ändert sich zwar die Reihenfolge der mit den Vorabeinspritzern versorgten Zylinder. Da jedoch das Drehzahlverhalten während der Startphase in Relation zu den Ansaugphasen der nacheinander öffnenden Einlassventile im wesentlichen immer gleich bleibt, können die Kraftstoffmengen der aufeinanderfolgenden Vorabeinspritzer I immer mit Hilfe derselben Gewichtungsfaktoren bestimmt werden.If the internal combustion engine has stopped at one of the other three possible standstill angular positions, the sequence of the cylinders supplied with the pre-injectors changes. However, since the speed behavior during the starting phase in relation to the intake phases of the successively opening intake valves remains essentially the same, the fuel quantities of the successive pilot injector I can always be determined using the same weighting factors.
Bei dem oben beschriebenen Vorabeinspritzverfahren handelt es sich nur um ein Beispiel einer Vorabeinspritzstrategie, bei der das erfindungsgemäße Verfahren verwendet werden kann. Insbesondere sei nochmals hervorgehoben, dass es zum Durchführen des erfindungsgemäßen Verfahrens nicht erforderlich ist, die Stillstands-Winkelpositionen der Brennkraftmaschine zu kennen. The pre-injection method described above is only one example of a pre-injection strategy in which the method according to the invention can be used. In particular, it should again be emphasized that it is not necessary to know the standstill angular positions of the internal combustion engine in order to carry out the method according to the invention.
Claims
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10056863A DE10056863C1 (en) | 2000-11-16 | 2000-11-16 | Fuel injection method for start phase of multi-cylinder IC engine uses fuel pre-injection for providing wall film in each engine cylinder |
DE10056863 | 2000-11-16 | ||
PCT/DE2001/004285 WO2002040848A1 (en) | 2000-11-16 | 2001-11-15 | Method for injecting fuel during the start phase of an internal combustion engine |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1336041A1 true EP1336041A1 (en) | 2003-08-20 |
EP1336041B1 EP1336041B1 (en) | 2006-06-28 |
Family
ID=7663547
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01996679A Expired - Lifetime EP1336041B1 (en) | 2000-11-16 | 2001-11-15 | Method for injecting fuel during the start phase of an internal combustion engine |
Country Status (4)
Country | Link |
---|---|
US (1) | US6769412B2 (en) |
EP (1) | EP1336041B1 (en) |
DE (2) | DE10056863C1 (en) |
WO (1) | WO2002040848A1 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6931840B2 (en) * | 2003-02-26 | 2005-08-23 | Ford Global Technologies, Llc | Cylinder event based fuel control |
DE102004028092A1 (en) | 2004-06-09 | 2005-12-29 | Robert Bosch Gmbh | Method for starting an internal combustion engine |
DE102004057260A1 (en) * | 2004-11-26 | 2006-06-01 | Robert Bosch Gmbh | Internal combustion engine operating method for motor vehicle, involves obtaining periodic signal from operation value of engine, and evaluating cylinder-specific characteristic of value for determining current operating phase of cylinders |
DE102005000612A1 (en) * | 2005-01-03 | 2006-07-13 | Robert Bosch Gmbh | Starting process for internal combustion engine involves setting starting requirements before starting, and operating ignition and direct injection at setting |
DE102005016067B4 (en) * | 2005-04-07 | 2007-06-21 | Siemens Ag | Method for increasing the start reproducibility during start-stop operation of an internal combustion engine |
CN110566358B (en) * | 2019-09-30 | 2022-03-01 | 潍柴动力股份有限公司 | Engine start control method, device, device and storage medium |
CN113217248B (en) * | 2021-06-02 | 2022-08-16 | 江门市大长江集团有限公司 | Motorcycle, fuel injection amount control method and device, and computer readable storage medium |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3623042A1 (en) | 1986-07-09 | 1988-01-14 | Bosch Gmbh Robert | FUEL INJECTION METHOD |
ES2024616B3 (en) | 1988-11-28 | 1992-03-01 | Siemens Ag | PROCEDURE FOR INJECTING FUEL IN AN INTERNAL COMBUSTION MACHINE |
DE3923478C2 (en) * | 1989-07-15 | 2000-02-03 | Bosch Gmbh Robert | Sequential fuel injection with pre-spray |
DE4141714C2 (en) * | 1991-12-18 | 2002-11-14 | Bosch Gmbh Robert | Control system for an internal combustion engine |
DE4141713C2 (en) * | 1991-12-18 | 2003-11-06 | Bosch Gmbh Robert | Encoder arrangement for cylinder detection and emergency operation in an internal combustion engine with n cylinders |
US5209202A (en) * | 1992-07-27 | 1993-05-11 | Ford Motor Company | Multiple functions cam sensing |
DE4230616A1 (en) * | 1992-09-12 | 1994-03-17 | Bosch Gmbh Robert | Device for recognizing the position of at least one shaft having a reference mark |
JPH06185387A (en) * | 1992-12-18 | 1994-07-05 | Nippondenso Co Ltd | Fuel injection controller for internal combustion engine |
DE4304163A1 (en) * | 1993-02-12 | 1994-08-25 | Bosch Gmbh Robert | Device for controlling fuel injection in an internal combustion engine |
DE19524112A1 (en) | 1994-07-30 | 1996-02-01 | Volkswagen Ag | Method and device for rapid starting of multi=cylinder IC engine |
DE19734595A1 (en) * | 1997-08-09 | 1999-02-11 | Bosch Gmbh Robert | Procedure for determining segment times |
DE19735720A1 (en) * | 1997-08-18 | 1999-02-25 | Bayerische Motoren Werke Ag | Method for recognizing the combustion stroke of a specific cylinder when starting an internal combustion engine |
DE19741966C2 (en) * | 1997-09-23 | 2002-11-07 | Siemens Ag | Method for injecting fuel in a multi-cylinder internal combustion engine |
JP2000199445A (en) * | 1998-12-28 | 2000-07-18 | Hitachi Ltd | Engine drive motor control device |
DE19933845A1 (en) * | 1999-07-20 | 2001-01-25 | Bosch Gmbh Robert | Device for detecting the turning back of a rotating part of an internal combustion engine |
US6679223B2 (en) * | 2001-04-20 | 2004-01-20 | Denso Corporation | Engine control system with cam sensor |
-
2000
- 2000-11-16 DE DE10056863A patent/DE10056863C1/en not_active Expired - Fee Related
-
2001
- 2001-11-15 WO PCT/DE2001/004285 patent/WO2002040848A1/en active IP Right Grant
- 2001-11-15 EP EP01996679A patent/EP1336041B1/en not_active Expired - Lifetime
- 2001-11-15 US US10/181,604 patent/US6769412B2/en not_active Expired - Lifetime
- 2001-11-15 DE DE50110362T patent/DE50110362D1/en not_active Expired - Lifetime
Non-Patent Citations (1)
Title |
---|
See references of WO0240848A1 * |
Also Published As
Publication number | Publication date |
---|---|
US20030000501A1 (en) | 2003-01-02 |
DE10056863C1 (en) | 2002-03-14 |
US6769412B2 (en) | 2004-08-03 |
EP1336041B1 (en) | 2006-06-28 |
DE50110362D1 (en) | 2006-08-10 |
WO2002040848A1 (en) | 2002-05-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE60117143T2 (en) | METHOD AND DEVICE FOR PRODUCING FUEL MULTIPLE INJECTION IN THE CYLINDERS OF AN INTERNAL COMBUSTION ENGINE | |
EP0640762B1 (en) | Cylinder synchronization of a multi-cylinder internal combustion engine via detection of a directed misfire | |
EP0785346B1 (en) | Method of operating an internal combustion engine | |
DE19748018C2 (en) | Direct fuel injection control unit for an internal combustion engine | |
DE19815266B4 (en) | Method for injecting fuel into an internal combustion engine | |
DE3312950A1 (en) | FUEL INJECTION CONTROL SYSTEM FOR AN ENGINE WITH INTERNAL COMBUSTION OF THE DIRECT INJECTION TYPE | |
DE10221162A1 (en) | Separate injector master timing cards for use with and without pilot injection | |
EP1336040B1 (en) | Method for injecting fuel during the starting phase of an internal combustion engine | |
WO2004070184A1 (en) | Method for controlling a direct injection of an internal combustion engine | |
DE102013213749A1 (en) | Method and device for controlling a four-stroke internal combustion engine | |
DE4143094C2 (en) | Method and arrangement for electronic control of fuel injectors for an internal combustion engine | |
DE60131652T2 (en) | DEVICE AND METHOD FOR REGULATING FUEL INJECTION SIGNALS DURING THE ACCELERATION AND DELAY OF AN INTERNAL COMBUSTION ENGINE | |
EP1149239A1 (en) | Fuel supply system for an internal combustion engine, especially a motor vehicle | |
WO2002040848A1 (en) | Method for injecting fuel during the start phase of an internal combustion engine | |
DE3200398A1 (en) | METHOD AND DEVICE FOR IGNITING AN INTERNAL COMBUSTION ENGINE | |
WO1999020882A1 (en) | Method for starting an internal combustion engine | |
EP1179130A1 (en) | Method for operating a multi-cylinder internal combustion engine | |
DE10342703B4 (en) | Method for starting a multi-cylinder internal combustion engine and internal combustion engine | |
DE602004003358T2 (en) | METHOD FOR SYNCHRONIZING INJECTION WITH THE PHASE OF AN ENGINE WITH ELECTRONICALLY ASSEMBLED FUEL INJECTION NOZZLES | |
DE10258229A1 (en) | Combustion engine start-up method for a fuel-injected engine, in which for a warm start a number of sequential fuel injection processes are carried out prior to ignition | |
DE19741966C2 (en) | Method for injecting fuel in a multi-cylinder internal combustion engine | |
DE102013214261B4 (en) | Method for controlling direct fuel injection | |
DE19517767A1 (en) | Fuel injection system for IC engine | |
DE10322014A1 (en) | Method for starting an internal combustion engine, in particular a motor vehicle | |
DE102015225607A1 (en) | Method for restarting a multi-cylinder internal combustion engine with intake manifold injection without externally supplied torque |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR |
|
17P | Request for examination filed |
Effective date: 20030607 |
|
RBV | Designated contracting states (corrected) |
Designated state(s): DE FR GB |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REF | Corresponds to: |
Ref document number: 50110362 Country of ref document: DE Date of ref document: 20060810 Kind code of ref document: P |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20061004 |
|
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20070329 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20081113 Year of fee payment: 8 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20081117 Year of fee payment: 8 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20091115 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20100730 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20091130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20091115 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20181130 Year of fee payment: 18 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 50110362 Country of ref document: DE Owner name: VITESCO TECHNOLOGIES GMBH, DE Free format text: FORMER OWNER: CONTINENTAL AUTOMOTIVE GMBH, 30165 HANNOVER, DE Ref country code: DE Ref legal event code: R119 Ref document number: 50110362 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200603 |