FR2840015A1 - Control of compression ignition internal combustion engine, uses computer control of offset in inlet and exhaust valve opening times to control combustion and levels of residual burnt gas - Google Patents

Control of compression ignition internal combustion engine, uses computer control of offset in inlet and exhaust valve opening times to control combustion and levels of residual burnt gas Download PDF

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Publication number
FR2840015A1
FR2840015A1 FR0206305A FR0206305A FR2840015A1 FR 2840015 A1 FR2840015 A1 FR 2840015A1 FR 0206305 A FR0206305 A FR 0206305A FR 0206305 A FR0206305 A FR 0206305A FR 2840015 A1 FR2840015 A1 FR 2840015A1
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Prior art keywords
combustion
control
engine
valves
exhaust
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FR0206305A
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French (fr)
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FR2840015B1 (en
Inventor
Damien Maroteaux
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Renault SAS
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Renault SAS
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D13/00Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing
    • F02D13/02Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing during engine operation
    • F02D13/0261Controlling the valve overlap
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/34Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D15/00Varying compression ratio
    • F02D15/04Varying compression ratio by alteration of volume of compression space without changing piston stroke
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/30Controlling fuel injection
    • F02D41/3011Controlling fuel injection according to or using specific or several modes of combustion
    • F02D41/3017Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used
    • F02D41/3035Controlling fuel injection according to or using specific or several modes of combustion characterised by the mode(s) being used a mode being the premixed charge compression-ignition mode
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L2820/00Details on specific features characterising valve gear arrangements
    • F01L2820/01Absolute values
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/12Engines characterised by fuel-air mixture compression with compression ignition
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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

Abstract

The combustion control uses control of pressure and temperature in the combustion chamber during the compression phase and control of the mass of residual burnt gas. The control is exerted by phase offset in the opening and closing of the inlet (24) and exhaust (26) valves. The valves are controlled by a control computer (34) using a look-up table (36).

Description

Procede de controle de la combustion diun moteur a combustion interne deMethod for controlling the combustion of an internal combustion engine

type a allumage par compression et dispositif de commande pour la mise en aeuvre d'un tel procede La presente invention concerne un procede de contr81e de la combustion d'un moteur a combustion interne de type a allumage par compression. Wile concerne egalement un dispositif de commande du fonctionnement d'un moteur a combustion interne pour la mise en  The compression ignition type and control device for implementing such a process The present invention relates to a method of controlling the combustion of an internal combustion engine of the compression ignition type. Wile also relates to a device for controlling the operation of an internal combustion engine for setting

ccuvre d'un tel procede.work of such a process.

1 0 Plus particulierement, ['invention porte sur un pro cede de contr81e de la combustion d'un moteur a allumage par compression et sur un dispositif de commande correspondent permettant la reduction de la quantite de particules et d'oxydes d'azote emis dans les gaz d'echappement. Comme on le salt, les gaz d'echappement des moteurs a combustion interne, notamment des vehicules automobiles de type a allumage par compression, contiennent des especes chimiques nocives que lton traite couramment en dotant les lignes d'echappement de moyens de traitement, tels que des catalyseurs d'oxydation, des filtres a particules, des pieges a NOx, dont la fonction est essentiellement de transformer des especes chimiques emises par la combustion en  More particularly, the invention relates to a method for controlling the combustion of a compression-ignition engine and to a corresponding control device allowing the reduction of the quantity of particles and nitrogen oxides emitted in the exhaust gas. As it is salted, the exhaust gases of internal combustion engines, in particular of the compression ignition type motor vehicles, contain harmful chemical species which are commonly treated by providing exhaust systems with treatment means, such as oxidation catalysts, particle filters, NOx traps, the function of which is essentially to transform chemical species emitted by combustion into

substances non polluantes, ou de pieger ces especes chimiques.  non-polluting substances, or to trap these chemical species.

Des dispositions reglementaires tendent a imposer aux constructeurs de vehicules automobiles une reduction considerable des quantites de particules et d'oxyde d' azote emis dans les gaz d'echappement. Les moyens de traitement dont vent pourvues les lignes  Regulatory provisions tend to impose on motor vehicle manufacturers a considerable reduction in the quantities of particles and nitrogen oxide emitted in exhaust gases. The means of treatment with which the lines are provided

d'echappement ne peuvent, a eux seuls, permettre une telle reduction.  exhaust cannot, by themselves, allow such a reduction.

Des lors, un des soucis des constructeurs de vehicules automobiles est de limiter la quantite de particules nocives et d'oxydes  One of the concerns of motor vehicle manufacturers is therefore to limit the quantity of harmful particles and oxides

d'azote emis dans les gaz d'echappement.  of nitrogen emitted into the exhaust gases.

Dans les moteurs de type a allumage par compression, ceci est generalement obtenu en tentant d'homogeneiser la combustion. Ceci est realise, d'une part, en reduisant les zones riches et, d'autre part, en diluant le melange air-carburant, ce qui permet de reduire les temperatures maximales de la combustion et de limiter ainsi,  In compression ignition type engines, this is generally achieved by attempting to homogenize combustion. This is achieved, on the one hand, by reducing the rich zones and, on the other hand, by diluting the air-fuel mixture, which makes it possible to reduce the maximum temperatures of combustion and thus to limit,

notamment, les emissions d'oxyde d'azote.  in particular, nitrogen oxide emissions.

De maniere conventionnelle, cette homogeneisation est obtenue en usinant les pistons, de maniere a obtenir un taux de compression predetermine. Selon cette technique, les conditions de pression et de temperature au moment de ['injection du carburant, c'est-a-dire pendant la phase de compression, vent determinees par les pressions et temperatures d'admission d'air dans le moteur et par le taux de compression geometrique, loquel est lie a la forme de la chambre de compression. Pour une masse d' air introduite donnee, il n'existe aucun moyen pour faire varier la pression et la temperature regnant dans la chambre de combustion, ainsi que la masse de gaz brules residuals, lesquels influent grandement sur l'homogeneite de la combustion et sur  Conventionally, this homogenization is obtained by machining the pistons, so as to obtain a predetermined compression ratio. According to this technique, the pressure and temperature conditions at the time of fuel injection, that is to say during the compression phase, wind determined by the pressures and temperatures of air intake into the engine and by the rate of geometric compression, loquel is linked to the shape of the compression chamber. For a given mass of introduced air, there is no way to vary the pressure and temperature prevailing in the combustion chamber, as well as the mass of residual burnt gases, which greatly influence the homogeneity of combustion and sure

son calage dans le cycle de fonctionnement du moteur.  its timing in the engine operating cycle.

Le but de ['invention est de pallier cet inconvenient et de fournir un procede de contr81e de la combustion d'un moteur a combustion interne de type a allumage par compression, ainsi qu'un dispositif de commande de moteur correspondent, permettant de reduire efficacement la quantite de particules et d' oxydes d' azote emis  The object of the invention is to overcome this drawback and to provide a method of controlling the combustion of an internal combustion engine of the compression ignition type, as well as a corresponding engine control device, making it possible to effectively reduce the amount of particles and nitrogen oxides emitted

dans les gaz d'echappement.in exhaust gases.

Ainsi, ['invention propose un procede de contrGle de la combustion d'un moteur a combustion interne de type a allumage par compression, pour la reduction de la quantite de particules et d'oxydes d'azotes emis dans les gaz d'echappement, le moteur etant pourvu de cylindres qui delimitent interieurement une chambre de combustion et qui vent dotes d'un injecteur de carburant et de soupapes d' admission et d'echappement pilotees par un calculateur de commande selon des  Thus, the invention provides a method of controlling the combustion of an internal combustion engine of the compression-ignition type, for reducing the amount of particles and nitrogen oxides emitted in the exhaust gases, the engine being provided with cylinders which internally delimit a combustion chamber and which have a fuel injector and intake and exhaust valves controlled by a control computer according to

lois de levee des soupapes.valve lift laws.

Ce procede comprend une phase de contr81e de la pression et de la temperature regnant dans la chambre de combustion au cours d'une phase de compression et de contr81e de la masse de gaz brules residuals. Le contr81e de la pression et de la temperature regnant dans la chambre de combustion et le contr81e de la masse de gaz brules residuels vent realises par decalage de phases de fermeture des  This process comprises a phase of controlling the pressure and the temperature prevailing in the combustion chamber during a phase of compression and controlling the mass of residual burnt gases. The control of the pressure and the temperature prevailing in the combustion chamber and the control of the mass of residual burnt gases are achieved by shifting the closing phases of the

soupapes d'admission dans la loi de levee des soupapes d' admission.  intake valves in the law of lifting of intake valves.

On decale en outre les phases de fermeture des soupapes  The valve closing phases are also shifted

d'echappement dans la loi de levee des soupapes d'echappement.  in the law of lifting of the exhaust valves.

On decale en outre les phases d'ouverture des soupapes  We also shift the valve opening phases

d' admission dans les lois de levee des soupapes d'admission.  of admission in the laws of lifting of the valves of admission.

Selon une autre caracteristique de ce procede, le decalage des phases de fermeture et/ou d'ouverture des soupapes d' admission et/ou des soupapes d'echappement est effectue en fonction des conditions de  According to another characteristic of this process, the offset of the closing and / or opening phases of the intake valves and / or the exhaust valves is carried out according to the conditions of

fonctionnement du moteur.engine operation.

On detecte de preference ['instant de demarrage de la combustion et l'on decale les instants de fermeture des soupapes d' admission et/ou d'echappement de maniere a provoquer le demarrage  The instant of combustion start is preferably detected and the instants of closing of the intake and / or exhaust valves are shifted so as to cause the start

de la combustion a un instant predetermine.  of combustion at a predetermined time.

Selon une autre caracteristique, ['instant de demarrage de la combustion est determine en fonction des conditions de  According to another characteristic, the instant of starting combustion is determined according to the conditions of

fonctionnement du moteur.engine operation.

Selon un mode de mise en ceuvre particulier, on met en ceuvre un contr81e de la combustion du moteur en fonction des conditions de fonctionnement du moteur et un contr81e de ['injection du carburant  According to a particular mode of implementation, one implements a control of the combustion of the engine as a function of the operating conditions of the engine and a control of the fuel injection.

pour chaque cycle de fonctionnement du moteur.  for each engine operating cycle.

L'invention propose egalement un dispositif de commande du fonctionnement d'un moteur a combustion interne de type a allumage par compression, pour la mise en aeuvre d'un procede tel que defini ci dessus, le moteur etant pourvu de cylindres delimitant chacun une chambre de combustion et dotes chacun d'un injecteur de carburant et  The invention also provides a device for controlling the operation of an internal combustion engine of the compression ignition type, for implementing a method as defined above, the engine being provided with cylinders each delimiting a chamber. and each has a fuel injector and

de soupapes d' admission et de soupapes d'echappement.  intake and exhaust valves.

Ce dispositif comprenant un calculateur de commande comportant, stockees en memoire, des lois de levee des soupapes pour provoquer leur ouverture et leur fermeture en fonction desdites lois de levee. I1 comporte en outre des moyens de contr81e de la temperature et de la pression regnant dans la chambre de combustion et de contr81e de la masse de gaz brules residuels par decalage de phases de fermeture et/ou d'ouverture des soupapes dans au moins une desdites  This device comprising a control computer comprising, stored in memory, laws of lifting of the valves to cause them to open and close as a function of said laws of lifting. It also comprises means for controlling the temperature and the pressure prevailing in the combustion chamber and for controlling the mass of residual burnt gas by shifting the phases of closing and / or opening of the valves in at least one of said

lois de levee.lifting laws.

Selon une autre caracteristique de ce dispositif, le calculateur comporte une cartographic dans laquelle vent stockees des valeurs de consigne de position des soupapes en fonction de parametres de  According to another characteristic of this device, the computer comprises a map in which the stored position values of the valves are stored as a function of parameters of

fonctionnement du moteur.engine operation.

De preference, il comporte en outre des moyens de detection du demarrage de la combustion dans la chambre de combustion et une cartographic dans laquelle vent stockes des instants de demarrage de combustion en fonction de conditions de fonctionnement du moteur, les moyens de contr81e provoquant un decalage des phases d'ouverture et/ou d'ouverture desdites soupapes de maniere a provoquer un demarrage de la combustion dans la chambre de combustion auxdits instants. D'autres buts, caracteristiques et avantages de ['invention  Preferably, it further comprises means for detecting the start of combustion in the combustion chamber and a map in which wind stores instants of start of combustion as a function of operating conditions of the engine, the control means causing an offset. opening and / or opening phases of said valves so as to cause combustion to start in the combustion chamber at said times. Other objects, features and advantages of the invention

apparatront a la lecture de la description qui va suivre, donnee  will appear on reading the description which follows, given

uniquement a titre d'exemple non limitatif et faite en reference aux dessins annexes sur lesquels: - la figure 1 est une representation schematique d'un moteur a combustion interne de type a allumage par compression destine a la propulsion d'un vehicule automobile; - la figure 2 est un diagramme montrant les lois de levee des soupapes d'admission et d'echappement au cours du fonctionnement normal du moteur; - la figure 3a est un diagramme montrant des lois de levee des soupapes d'admission et d'echappement dans lesquelles la phase de fermeture des soupapes d' admission est modifiee de maniere a contrGler la combustion du moteur; la figure 3b est un diagramme montrant un autre exemple de loi s de levee des soupapes d' admi ssion et d'echappement dont le s phases de fermeture et d'ouverture vent modifiees de maniere a contr81er la combustion du moteur; s - la figure 4 est une representation schematique illustrant un autre mode de realisation d'un dispositif de commande conforme a ['invention; et - la figure S montre des courbes illustrant des modifications des loi s de lev ee des soupapes d' admission en foncti on du point de  only by way of nonlimiting example and made with reference to the accompanying drawings in which: - Figure 1 is a schematic representation of an internal combustion engine of the compression ignition type intended for the propulsion of a motor vehicle; - Figure 2 is a diagram showing the laws of lifting the intake and exhaust valves during normal engine operation; - Figure 3a is a diagram showing laws of lifting of the intake and exhaust valves in which the closing phase of the intake valves is modified so as to control the combustion of the engine; FIG. 3b is a diagram showing another example of the law of lifting the intake and exhaust valves, the closing and opening phases of the wind being modified so as to control the combustion of the engine; s - Figure 4 is a schematic representation illustrating another embodiment of a control device according to the invention; and - Figure S shows curves illustrating modifications of the lift s laws of the intake valves according to the point of

fonctionnement du moteur.engine operation.

Sur la figure 1, on a represente un schema synoptique illustrant la structure generale d'un moteur a combustion interne de type a allumage par compression pour vehicule automobile, ses moyens d'alimentation en air et d'echappement des gaz de combustion, ainsi  In Figure 1, there is shown a block diagram illustrating the general structure of an internal combustion engine of the compression ignition type for a motor vehicle, its means of supplying air and exhausting combustion gases, as well

que ses moyens de pilotage.than its means of piloting.

Sur la figure 1, la reference numerique generale 10 designe de fapon tres schematique le carter du moteur, loquel comporte, dans l'exemple considere, quatre cylindres 12 en ligne. Chaque cylindre 12 1 5 est pourvu d'un conduit d'admissi on d' air frais et diun conduit  In FIG. 1, the general numerical reference 10 designates the engine casing very schematically, which, in the example under consideration, comprises four cylinders 12 in line. Each cylinder 12 1 5 is provided with a fresh air intake duct and a duct

d'echappement des gaz issus de la combustion.  of exhaust gases from combustion.

Les conduits d'admission d'air vent alimentes en air frais par l'intermediaire d'un repartiteur d'admission 14, lequel est alimente par  The air intake ducts supplied with fresh air through an intake distributor 14, which is supplied by

une conduite 16 pourvue d'un filtre a air 18.  a pipe 16 provided with an air filter 18.

En ce qui concerne les conduits d'echappement, ceux-ci vent raccordes a un collecteur d'echappement 20 qui recupere les gaz brules resultant de la combustion du melange air-carburant dans chaque cylindre 12 pour les rejeter dans l'environnement ambient par une ligne d'echappement 22, laquelle est pourvue, comme cela est classique, de moyens de traitement assurant, d'une part, un piegeage des particules nocives resultant de la combustion et, d'autre part, une conversion d'especes chimiques issues de la combustion en substances  As regards the exhaust ducts, these are connected to an exhaust manifold 20 which recovers the burnt gases resulting from the combustion of the air-fuel mixture in each cylinder 12 to discharge them into the ambient environment by a exhaust line 22, which is provided, as is conventional, with treatment means ensuring, on the one hand, a trapping of the harmful particles resulting from combustion and, on the other hand, a conversion of chemical species resulting from combustion of substances

non polluantes par un procede de catalyse.  non-polluting by a catalysis process.

Ces moyens de traitement vent constitues par des moyens de traitement de type classique. Ils ne seront done pas decrits en detail  These wind processing means constituted by conventional type processing means. They will therefore not be described in detail.

par la suite.thereafter.

On notera neanmoins qu'ils comportent un catalyseur d'oxydation ainsi que des moyens de post-traitement dit "actifs" tels  However, it should be noted that they comprise an oxidation catalyst as well as so-called "active" post-treatment means such as

qu'un filtre a particule et un piege a NOx.  than a particle filter and a NOx trap.

Les conduits d' admission et d'echappement vent chacun obtures par au moins une soupape, telle que 24 et 26, dont la levee est  The intake and exhaust ducts are each closed by at least one valve, such as 24 and 26, the lift of which is

commandee par un arbre a cames, respectivement 28 et 30.  controlled by a camshaft, respectively 28 and 30.

Enfin, chaque cylindre est pourvu d'un injecteur de carburant, tel que 32. Un calculateur electronique, designe par la reference numerique generale 34, dument programme, gere le fonctionnement du moteur, notamment la quantite de carburant injecte ou ['instant d'allumage du moteur, de maniere a delivrer le couple demande par le conducteur. En particulier, le calculateur 34 inc orpore tous le s moyens materiels et logiciels pour gerer le fonctionnement du moteur dans le respect de relations qui liens ['angle d'avance a ['injection au remplissage en air, a la dilution de gaz brules recircules et a divers parametres, tels que le regime du fonctionnement du moteur, la temperature de l'air ambient, celle du liquide de refroidissement,  Finally, each cylinder is provided with a fuel injector, such as 32. An electronic computer, designated by the general numerical reference 34, duly programmed, manages the operation of the engine, in particular the quantity of fuel injected or [instant of ignition of the engine, so as to deliver the torque requested by the driver. In particular, the computer 34 inc incorporates all the hardware and software means for managing the operation of the engine while respecting relationships which link the angle of advance to injection to filling with air, to the dilution of recirculated burnt gases. and to various parameters, such as engine operating speed, ambient air temperature, coolant temperature,

etc..., comme cela est bien connu de l'homme du metier.  etc ..., as is well known to those skilled in the art.

En particulier, le calculateur 34 comporte, stockees en memoire, des lois de levee des soupapes d' admission 24 et d'echappement 26, de maniere a piloter les arbres a cames 28 et 30 pour obtenir un comportement des soupapes 24 et 26 correspondent aux lois de levee memorisees ou elaborees par le calculateur a partir  In particular, the computer 34 comprises, stored in memory, laws for lifting the intake 24 and exhaust 26 valves, so as to control the camshafts 28 and 30 to obtain behavior of the valves 24 and 26 correspond to laws of lifting memorized or worked out by the computer from

de ces lois de levee.of these lifting laws.

On a represente sur la figure 2 un exemple de loi de levee des soupapes en fonction de ['angle de rotation des arbres a cames 28 et  FIG. 2 shows an example of a valve lift law as a function of the angle of rotation of the camshafts 28 and

, utilisee dans le fonctionnement normal du moteur.  , used in normal engine operation.

Sur cette figure, le terme PMH designe le point mort haut, le terme PMB designe le point mort teas, le terme OA designe la phase d'ouverture des soupapes d' admission, le terme OE designe la phase d'ouverture des soupapes d'echappement, le terme FA designe la phase de fermeture des soupapes d'admission, et le terme FE designe la phase  In this figure, the term TDC designates top dead center, the term PMB designates teas dead center, the term OA designates the opening phase of the intake valves, the term OE designates the opening phase of the intake valves exhaust, the term FA denotes the closing phase of the intake valves, and the term FE denotes the phase

de fermeture des soupapes d'echappement.  closing the exhaust valves.

Conformement a une caracteristique de ['invention, les phases d'actionnement des soupapes, dans le cycle de fonctionnement du moteur, vent determinees de maniere a contr81er la pression et la temperature regnant dans la chambre de combustion au cours de la compression, ainsi que la masse des gaz brules residuals, en procedant  In accordance with a feature of the invention, the valve actuation phases in the engine operating cycle are determined to control the pressure and temperature prevailing in the combustion chamber during compression, as well as the mass of residual burnt gases, proceeding

a un decalage des instants d'ouverture et de fermeture des soupapes.  to a shift of the instants of opening and closing of the valves.

Plus particulierement, en se referent a la figure 3a, le calculateur contr81e la pression et la temperature regnant dans la chambre de combustion pendant la phase de compression, et done au cours de ['injection de carburant, en agissant sur la phase de fermeture des soupapes d'admission. Cette commande correspond a la loi utilisee dans la zone B de la figure 5. De meme, on pourrait, comme visible sur la figure 3b, decaler les lois de levee des soupapes d' admission et d'echappement. Cette commande correspond a la loi utilisee dans la zone C de la figure 5 De meme, le calculateur controle le taux de gaz brules residuels en agissant sur les phases d'ouverture et de fermeture des  More particularly, with reference to FIG. 3a, the computer controls the pressure and the temperature prevailing in the combustion chamber during the compression phase, and therefore during the fuel injection, by acting on the closing phase of the intake valves. This command corresponds to the law used in the zone B of figure 5. In the same way, one could, as visible on figure 3b, to shift the laws of lifting of the valves of admission and exhaust. This command corresponds to the law used in zone C of FIG. 5 Likewise, the computer controls the rate of residual burnt gas by acting on the opening and closing phases of the

soupapes d'echappement et d' admission.  exhaust and intake valves.

Plus particulierement, la phase de fermeture des soupapes d'admi s si on est decal ee vers le point mort haut PMH de maniere a reduire la pression et la temperature dans le cylindre au cours de la compression. De meme, pour augmenter la quantite de gaz brules residuels pieges, on provoque un decalage de la phase de fermeture de la ou des  More particularly, the closing phase of the inlet valves if one is shifted towards the top dead center TDC so as to reduce the pressure and the temperature in the cylinder during compression. Likewise, to increase the amount of trapped residual burnt gas, a shift is made in the closing phase of the

soupapes d'echappement vers le point mort teas PMB.  exhaust valves to neutral teas PMB.

On peut ainsi regler et controler la pression et la temperature au moment de ['injection du carburant dans les cylindres, ainsi que la quantite des gaz residuels et, par consequent, ajuster le delai d'auto inflammation pour que la combustion se declenche dans toutes les  It is thus possible to regulate and control the pressure and the temperature at the time of the injection of the fuel into the cylinders, as well as the quantity of residual gases and, consequently, adjust the delay of self-ignition so that combustion starts in all the

conditions de fonctionnement autour du point mort haut.  operating conditions around top dead center.

Selon un premier exemple de realisation, represente sur la figure 1, le calculateur 34 comporte, en memoire, une cartographic dans laquelle vent stockees des valeurs de consigne de position des soup apes en foncti on de parametre s de fonctionnement du moteur, tel s que le regime, la charge, les conditions de pression et de temperature d'air admis dans les cylindres, la temperature d'eau,.... Ainsi, selon cet exemple de realisation, le calculateur 34 elabore des ordres de commande du deplacement des arbres a cames 28 et 30 a partir de ces valeurs de consigne, en fonction du point de fonctionnement du moteur. Selon un autre exemple de realisation represente sur la figure 4, le calculateur 34 est pourvu de moyens de regulation destines a reguler les instants de combustion autour d'instants de combustion predetermines cartographies dans le calculateur 34 en fonction du  According to a first exemplary embodiment, represented in FIG. 1, the computer 34 includes, in memory, a map in which the stored position values of the valves are stored according to the operating parameters of the engine, such as the speed, the load, the pressure and temperature conditions of air admitted into the cylinders, the water temperature, etc. Thus, according to this exemplary embodiment, the computer 34 draws up control commands for the displacement of the camshafts 28 and 30 from these setpoints, depending on the engine operating point. According to another exemplary embodiment shown in FIG. 4, the computer 34 is provided with regulation means intended to regulate the combustion times around predetermined combustion times mapped in the computer 34 as a function of the

point de fonctionnement du moteur.engine operating point.

Dans ce cas, le dispositif est pourvu de moyens de detection de ['instant de demarrage de la combustion. Ces moyens de detection vent constitues par des capteurs appropries, tels que, par exemple, un capteur de pression monte dans l'un des cylindres, un accelerometre place sur la structure du moteur ou enc ore une sonde a ionisati on, permettant de detecter ['instant de demarrage de la combustion. Le calculateur 34 contr81e alors la combustion de maniere que ['instant de demarrage de la combustion concide avec ['instant de demarrage cartographic.  In this case, the device is provided with means for detecting the instant of combustion start. These wind detection means constituted by appropriate sensors, such as, for example, a pressure sensor mounted in one of the cylinders, an accelerometer placed on the structure of the engine or still an ionization probe, making it possible to detect [ 'instant of combustion start. The computer 34 then controls the combustion in such a way that the instant of starting of the combustion coincides with the instant of cartographic starting.

On notera que, dans ces modes de realisation, le contr81e de la  It will be noted that, in these embodiments, the control of the

combustion s'effectue sur differents cycles de fonctionnement.  combustion takes place over different operating cycles.

De preference, le calculateur 34 procede en outre a une regulation cycle par cycle de la combustion en pilotant les injecteurs de carburant 32, de maniere a regler la strategic d'injection de carburant dans les cylindres en fonction du point de fonctionnement du moteur. Ainsi, par exemple, le calculateur 34 pilote les injecteurs 32 de maniere a agir sur le nombre et la phase des instants d'injection de  Preferably, the computer 34 also performs a cycle-by-cycle regulation of the combustion by controlling the fuel injectors 32, so as to adjust the strategy for injecting fuel into the cylinders as a function of the engine operating point. Thus, for example, the computer 34 controls the injectors 32 so as to act on the number and the phase of the injection instants of

carburant au cours de chaque cycle.fuel during each cycle.

Pour ce faire, par exemple, le calculateur 34 comporte, stockee en memoire, une cartographic dans laquelle vent charges des parametres d'injection en fonction du point de fonctionnement du moteur. I1 elabore ainsi directement des ordres de pilotage des  To do this, for example, the computer 34 includes, stored in memory, a map in which the wind loads injection parameters as a function of the engine operating point. He thus directly develops piloting orders for

injecteurs 32 de maniere a obtenir une strategic souhaitee.  injectors 32 so as to obtain a desired strategy.

En variante, il est egalement possible de mettre en aeuvre une regulation des parametres d'injection en utilisant une boucle de  As a variant, it is also possible to implement regulation of the injection parameters using a loop of

regulation incorporee au calculateur 34.  regulation incorporated in the computer 34.

En se referent enfin a la figure S. on a represente a titre S d'exemple des courbes illustrant en fonction de la pression moyenne effective (PME) regnant dans les cylindres du moteur, et du regime de fonctionnement, les cartographies d'utilisation des lois de levee des soupapes d'admission et d'echappement conventionnelles (zone A), des lois de levee de soupapes d'admission modifiees (zone B) et des lois de levee de soupapes d'admission et d'echappement modifiees (zone C). Comme on le volt sur ces figures, la modification des instants d'actionnement des soupapes d'admission, ou des soupapes d'admission et d'echappement, est effectuee de fa,con a reduire les emissions de 1S particules et d'oxydes d'azote en charge partielle (zones B et C), sans  Referring finally to Figure S. we have represented by way of example S curves illustrating as a function of the effective average pressure (PME) prevailing in the engine cylinders, and of the operating regime, the maps of use of the laws of lifting of the conventional intake and exhaust valves (zone A), laws of lifting of modified intake valves (zone B) and laws of lifting of modified intake and exhaust valves (zone C) ). As shown in these figures, the modification of the actuation times of the intake valves, or of the intake and exhaust valves, is carried out in such a way as to reduce the emissions of particles and of oxides d nitrogen under partial load (zones B and C), without

degrader les performances du moteur en pleine charge (zone A).  degrade the performance of the engine under full load (zone A).

Claims (8)

REVEND ICATIONSRESELL ICATIONS 1. Procede de contr81e de la combustion d'un moteur a combustion interne de type a allumage par compression, pour la reduction de la quantite de particules et d'oxydes d'azote emis dans les gaz d'echappement, le moteur etant pourvu de cylindres (12) qui delimitent interieurement une chambre de combustion et qui vent dotes d'un injecteur de carburant (32) et de soupapes d' admission (24) et d'echappement (26) pilotees par un calculateur de commande (34) selon des lois de levee des soupapes, caracterise en ce qu'il comprend une phase de contr81e de la pression et de la temperature regnant dans la chambre de combustion au cours d'une phase de compression et de contr81e de la masse de gaz brules residuals, et en ce que le contr81e de la pression et de la temperature regnant dans la chambre de combustion et le contr81e de la masse de gaz brules residuels vent realises par decalage de phases de fermeture et/ou d'ouverture des soupapes d' admission et/ou d'echappement dans la loi de levee  1. Method for controlling the combustion of an internal combustion engine of the compression ignition type, for reducing the amount of particles and nitrogen oxides emitted in the exhaust gases, the engine being provided with cylinders (12) which internally delimit a combustion chamber and which have a fuel injector (32) and inlet (24) and exhaust (26) valves controlled by a control computer (34) according to laws of valve lift, characterized in that it comprises a phase of controlling the pressure and the temperature prevailing in the combustion chamber during a phase of compression and controlling the mass of residual burnt gases, and in that the control of the pressure and the temperature prevailing in the combustion chamber and the control of the mass of residual burnt gases are achieved by shifting the closing and / or opening phases of the intake valves and / or escape in the law of lifting desdites soupapes.of said valves. 2. Procede selon la revendication 1, caracterise en ce que le decalage des phases de fermeture et/ou d'ouverture des soupapes d'admission (24) et/ou des soupapes d'echappement (26) est effectue  2. Method according to claim 1, characterized in that the shift of the closing and / or opening phases of the intake valves (24) and / or the exhaust valves (26) is carried out en fonction des conditions de fonctionnement du moteur.  depending on engine operating conditions. 3. Procede selon la revendication 2, caracterise en ce que l' on detecte ['instant de demarrage de la combustion et l'on decale les instants de fermeture des soupapes d' admission et/ou d'echappement de maniere a provoquer le demarrage de la combustion a un instant predetermine.  3. Method according to claim 2, characterized in that one detects ['instant of combustion start and one shifts the instants of closing the intake and / or exhaust valves so as to cause the start of combustion at a predetermined time. 4. Procede selon la revendication 3, caracterise en ce que ['instant de demarrage de la combustion est determine en fonction des4. Method according to claim 3, characterized in that ['instant of combustion start is determined according to conditions de fonctionnement du moteur.  engine operating conditions. 5. Procede selon l'une quelconque des revendications 1 a 4,  5. Method according to any one of claims 1 to 4, caracterise en ce que l' on met en aeuvre un contr81e de la combustion du moteur en fonction des conditions de fonctionnement du moteur et un controle de ['injection du carburant pour chaque cycle de  characterized in that a control of the combustion of the engine is implemented as a function of the operating conditions of the engine and a control of the fuel injection for each cycle of fonctionnement du moteur.engine operation. 6. Dispositif de commande du fonctionnement d'un moteur a combustion interne de type a allumage par compression, pour la mise  6. Device for controlling the operation of an internal combustion engine of the compression ignition type, for setting en ccuvre d'un procede selon l'une quelconque des revendications 1 a  in accordance with a process according to any one of claims 1 a S. le moteur etant pourvu de cylindres (12) delimitant chacun une chambre de combustion et dotes chacun d'un injecteur de carburant (32) et de soupapes d'admission (24) et de soupapes d'echappement (26), le dispositif comprenant un calculateur de commande (34) comportant, stockees en memoire, des lois de levee des soupapes pour provoquer leur ouverture et leur fermeture en fonction desdites lois de levee, caracterise en ce que le calculateur (34) comporte des moyens de contr81e de la temperature et de la pression regnant dans la chambre de combustion et de controle de la masse de gaz brules residuels par decalage de phases de fermeture et/ou d'ouverture des soupapes dans  S. the engine being provided with cylinders (12) each delimiting a combustion chamber and each provided with a fuel injector (32) and inlet valves (24) and exhaust valves (26), the device comprising a control computer (34) comprising, stored in memory, valve lift laws to cause them to open and close according to said lift laws, characterized in that the computer (34) comprises means for controlling the temperature and pressure prevailing in the combustion chamber and controlling the mass of residual burnt gases by shifting the closing and / or opening phases of the valves in au moins une desdites lois de levee.  at least one of said lifting laws. 7. Dispositif selon la revendication 6, caracterise en ce que le calculateur comporte une cartographic (36) dans laquelle vent stockees des valeurs de consigne de position des soupapes en fonction de  7. Device according to claim 6, characterized in that the computer comprises a map (36) in which wind stored values of position values of the valves as a function of parametres de fonctionnement du moteur.  engine operating parameters. 8. Dispositif selon la revendication 7, caracterise en ce qu'il comporte en outre des moyens de detection du demarrage de la combustion dans la chambre de combustion et une cartographic dans laquelle vent stockes des instants de demarrage de combustion en fonction de conditions de fonctionnement du moteur, les moyens de controle provoquant un decalage des phases d'ouverture et/ou de fermeture desdites soupapes de maniere a provoquer un demarrage de  8. Device according to claim 7, characterized in that it further comprises means for detecting the start of combustion in the combustion chamber and a map in which wind stores instants of start of combustion as a function of operating conditions of the engine, the control means causing a shift in the opening and / or closing phases of said valves so as to cause a starting of
FR0206305A 2002-05-23 2002-05-23 METHOD FOR CONTROLLING THE COMBUSTION OF A COMPRESSION IGNITION TYPE INTERNAL COMBUSTION ENGINE AND CONTROL DEVICE FOR IMPLEMENTING SUCH A METHOD Expired - Fee Related FR2840015B1 (en)

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WO2000028197A1 (en) * 1998-10-26 2000-05-18 Ab Volvo Method of controlling the process of combustion in an internal combustion engine, and engine with means for controlling the engine valves
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US6234123B1 (en) * 1998-08-21 2001-05-22 Nissan Motor Co., Ltd. Four-cycle internal combustion engine and valve timing control method thereof
WO2000028197A1 (en) * 1998-10-26 2000-05-18 Ab Volvo Method of controlling the process of combustion in an internal combustion engine, and engine with means for controlling the engine valves
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US8019527B2 (en) 2005-03-17 2011-09-13 Daimler Ag Method for operating an internal combustion engine, and associated internal combustion engine

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