FR2888284A3 - Internal combustion engine for motor vehicle, has injector with nozzle, whose free end comprises secondary orifice for supplying fuel to primary orifices, where axis of secondary orifice is oriented towards end of preheater plug - Google Patents
Internal combustion engine for motor vehicle, has injector with nozzle, whose free end comprises secondary orifice for supplying fuel to primary orifices, where axis of secondary orifice is oriented towards end of preheater plug Download PDFInfo
- Publication number
- FR2888284A3 FR2888284A3 FR0507304A FR0507304A FR2888284A3 FR 2888284 A3 FR2888284 A3 FR 2888284A3 FR 0507304 A FR0507304 A FR 0507304A FR 0507304 A FR0507304 A FR 0507304A FR 2888284 A3 FR2888284 A3 FR 2888284A3
- Authority
- FR
- France
- Prior art keywords
- secondary orifice
- injector
- orifices
- axis
- nozzle
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0669—Details related to the fuel injector or the fuel spray having multiple fuel spray jets per injector nozzle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0645—Details related to the fuel injector or the fuel spray
- F02B23/0654—Thermal treatments, e.g. with heating elements or local cooling
- F02B23/0657—Thermal treatments, e.g. with heating elements or local cooling the spray interacting with one or more glow plugs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/14—Arrangements of injectors with respect to engines; Mounting of injectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/182—Discharge orifices being situated in different transversal planes with respect to valve member direction of movement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/1826—Discharge orifices having different sizes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
- F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
- F02M61/1806—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
- F02M61/1846—Dimensional characteristics of discharge orifices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/14—Direct injection into combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0618—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
- F02B23/0621—Squish flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B23/00—Other engines characterised by special shape or construction of combustion chambers to improve operation
- F02B23/02—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
- F02B23/06—Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
- F02B23/0672—Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Abstract
Description
DOMAINE TECHNIQUE AUQUEL SE RAPPORTE L'INVENTIONTECHNICAL FIELD TO WHICH THE INVENTION REFERS
La présente invention concerne de manière générale les moteurs à combustion interne. The present invention generally relates to internal combustion engines.
L'invention concerne plus particulièrement un moteur à combustion interne de véhicule automobile comprenant une chambre de combustion dans laquelle s'étend une extrémité libre chauffante d'un élément de préchauffage et une extrémité libre d'une buse d'un injecteur de carburant pourvue d'une rangée d'orifices primaires de giclage de carburant disposés circonférentiellement autour de l'axe de l'injecteur. The invention relates more particularly to an internal combustion engine of a motor vehicle comprising a combustion chamber in which extends a free heating end of a preheating element and a free end of a nozzle of a fuel injector provided with a row of primary fuel jet orifices arranged circumferentially around the axis of the injector.
L'invention trouve une application particulièrement avantageuse pour le démarrage à froid des moteurs à combustion interne à injection directe à allumage par compression de type diesel. The invention finds a particularly advantageous application for the cold start of compression-ignition internal combustion engines of the diesel type.
ARRIERE-PLAN TECHNOLOGIQUEBACKGROUND
Les moteurs de véhicules automobiles à injection directe à allumage par compression de type diesel comprennent généralement un injecteur de carburant agencé dans une chambre de combustion d'un cylindre dans lequel coulisse un piston. L'injecteur de carburant fait jaillir dans la chambre de combustion un certain volume de carburant dont une fraction est vaporisée et se mélange à un volume d'air frais admis par un collecteur d'admission dans la chambre de combustion, pour former un mélange de gaz frais. Diesel fuel injection direct injection engine engines generally comprise a fuel injector arranged in a combustion chamber of a cylinder in which a piston slides. The fuel injector discharges into the combustion chamber a certain volume of fuel, a fraction of which is vaporized and mixes with a volume of fresh air admitted by an intake manifold into the combustion chamber, to form a mixture of fresh gas.
Les conditions thermodynamiques favorables à l'inflammation du mélange de gaz frais sont fonction de la richesse, de la température et de la pression du mélange de gaz frais. Ainsi, pour une certaine richesse donnée du mélange de gaz frais, celui-ci s'enflamme automatiquement sous une certaine pression et une certaine température. The thermodynamic conditions favorable to the ignition of the fresh gas mixture are a function of the richness, the temperature and the pressure of the fresh gas mixture. Thus, for a given richness of the mixture of fresh gas, it automatically ignites under a certain pressure and a certain temperature.
Actuellement, le taux de compression du mélange de gaz frais dans la chambre de combustion des moteurs à injection directe de type diesel est faible, afin d'augmenter la puissance du moteur. Currently, the compression ratio of the fresh gas mixture in the combustion chamber of diesel direct injection engines is low, in order to increase the power of the engine.
Ce faible taux de compression du mélange de gaz frais entraîne une dégradation des conditions thermodynamiques dans la chambre de combustion permettant l'inflammation automatique du mélange de gaz frais. II s'ensuit, des difficultés de démarrage lorsque le moteur est encore froid, c'est-à-dire, lorsque le mélange de gaz frais dans la chambre de combustion est froid. This low compression ratio of the fresh gas mixture leads to a deterioration of the thermodynamic conditions in the combustion chamber allowing the automatic ignition of the fresh gas mixture. It follows, starting difficulties when the engine is still cold, that is to say, when the mixture of fresh gas in the combustion chamber is cold.
Pour corriger ce problème de démarrage à froid, il est connu d'utiliser une bougie de préchauffage, positionnée dans la chambre de combustion pour augmenter la température dans la chambre de combustion afin de compenser la baisse du taux de compression du mélange de gaz frais. Cependant, l'utilisation d'une bougie de préchauffage nécessite un temps de préchauffage qui est d'autant plus important que la température du mélange de gaz frais avant le démarrage du moteur est faible. En outre, le temps de préchauffage génère une consommation d'énergie électrique importante. To correct this cold start problem, it is known to use a glow plug, positioned in the combustion chamber to increase the temperature in the combustion chamber to compensate for the decrease in the compression ratio of the fresh gas mixture. However, the use of a glow plug requires a warm-up time which is even more important that the temperature of the fresh gas mixture before starting the engine is low. In addition, the preheating time generates a significant electrical energy consumption.
II est encore connu de rapprocher la bougie de préchauffage d'un des 10 orifices de l'extrémité libre de la buse de l'injecteur de carburant pour augmenter la température dans la zone où est réalisé le mélange de gaz frais. It is still known to bring the glow plug of one of the orifices of the free end of the nozzle of the fuel injector to increase the temperature in the zone where the mixture of fresh gas is made.
Lorsque l'extrémité libre de la buse de l'injecteur de carburant possède une seule rangée d'orifices de giclage de carburant, celle-ci est laissée libre quel que soit l'état de fonctionnement du moteur. La bougie de préchauffage est alors positionnée à proximité d'un orifice laissé libre appartenant à la rangée d'orifices de l'extrémité libre de la buse. L'extrémité libre de la buse peut aussi posséder plusieurs rangées d'orifices de giclage de carburant utilisées en fonction du régime du moteur. Ces rangées sont indépendantes les unes des autres et, à au moins un moment du fonctionnement du moteur, les différents orifices des différentes rangées sont obturés par un organe d'obturation coopérant avec la buse de l'injecteur. II s'ensuit que l'orifice situé à proximité de la bougie de préchauffage, approchée de celui-ci, est à un moment donné obturé de même que les autres orifices de la rangée à laquelle il appartient. When the free end of the nozzle of the fuel injector has a single row of fuel jet orifices, it is left free regardless of the operating state of the engine. The glow plug is then positioned near a free-left orifice belonging to the row of orifices of the free end of the nozzle. The free end of the nozzle may also have several rows of fuel spray ports used depending on engine speed. These rows are independent of each other and, at least one moment of operation of the motor, the different orifices of the different rows are closed by a closure member cooperating with the nozzle of the injector. It follows that the orifice located near the glow plug, close to it, is at a given time closed as well as the other holes of the row to which it belongs.
Cependant, un rapprochement de la bougie de l'injecteur de carburant, pénalise les performances du moteur après démarrage, car la bougie constitue alors un obstacle à la circulation tourbillonnaire de l'air frais dans la chambre de combustion. However, a reconciliation of the spark plug of the fuel injector, penalizes engine performance after startup, because the candle is an obstacle to the vortex flow of fresh air into the combustion chamber.
Il est enfin connu d'augmenter au démarrage le volume de carburant injecté afin d'augmenter la richesse du mélange de gaz frais. En effet, lorsque la température est faible dans la chambre de combustion, seule une petite fraction du volume de carburant injecté est vaporisée et peut alors se mélanger au volume d'air frais. II est alors nécessaire d'injecter un volume important de carburant pour avoir un volume plus important de carburant vaporisé. Cependant, cette solution entraîne une surconsommation et une émission de polluants importante. Finally, it is known to increase the amount of fuel injected at the start in order to increase the richness of the fresh gas mixture. Indeed, when the temperature is low in the combustion chamber, only a small fraction of the injected fuel volume is vaporized and can then mix with the volume of fresh air. It is then necessary to inject a large volume of fuel to have a larger volume of vaporized fuel. However, this solution leads to overconsumption and a significant emission of pollutants.
OBJET DE L'INVENTION Afin de remédier aux inconvénients de l'état de la technique précité, la présente invention propose un nouveau moteur à injection directe dans lequel il est prévu un injecteur de carburant adapté à favoriser le démarrage du moteur. OBJECT OF THE INVENTION In order to overcome the drawbacks of the prior art, the present invention proposes a new direct injection engine in which there is provided a fuel injector suitable for promoting the starting of the engine.
À cet effet, on propose selon l'invention un moteur à combustion interne de véhicule automobile comprenant une chambre de combustion dans laquelle s'étend une extrémité libre chauffante d'un élément de préchauffage et une extrémité libre d'une buse d'un injecteur de carburant pourvue d'une rangée d'orifices primaires de giclage de carburant disposés circonférentiellement autour de l'axe de l'injecteur, dans lequel ladite extrémité libre de la buse de l'injecteur comprend, en dehors de ladite rangée d'orifices primaires de giclage, un orifice secondaire, apte à être alimenté en carburant simultanément aux orifices primaires de ladite rangée, dont l'axe est orienté sensiblement vers ladite extrémité libre chauffante de l'élément de préchauffage. For this purpose, it is proposed according to the invention an internal combustion engine of a motor vehicle comprising a combustion chamber in which extends a free heating end of a preheating element and a free end of a nozzle of an injector fuel nozzle provided with a row of primary fuel jet orifices circumferentially disposed about the axis of the injector, wherein said free end of the nozzle of the injector comprises, outside of said row of primary orifices nozzle, a secondary orifice, adapted to be supplied with fuel simultaneously with the primary orifices of said row, whose axis is oriented substantially towards said free heating end of the preheating element.
Grâce à l'orientation de l'axe de l'orifice secondaire sensiblement vers l'extrémité libre chauffante de l'élément de préchauffage, le mélange de gaz est réalisé, au démarrage, à proximité de cette extrémité libre chauffante. Le mélange de gaz possède alors une richesse satisfaisante et une température suffisante pour satisfaire aux conditions thermodynamiques d'inflammation du mélange de gaz, compensant ainsi la dégradation des conditions thermodynamiques résultant du faible taux de compression du mélange de gaz dans la chambre de combustion. Due to the orientation of the axis of the secondary orifice substantially towards the free heating end of the preheating element, the gas mixture is produced, at startup, near this heating free end. The gas mixture then has a satisfactory richness and a temperature sufficient to satisfy the thermodynamic conditions of ignition of the gas mixture, thus compensating for the degradation of the thermodynamic conditions resulting from the low compression ratio of the gas mixture in the combustion chamber.
De plus, cette température suffisante du mélange de gaz est atteinte, du fait de la proximité de l'extrémité libre chauffante de l'élément chauffant, après une courte durée de préchauffage, ce qui réduit la consommation en énergie électrique et donc en carburant. In addition, this sufficient temperature of the gas mixture is reached, due to the proximity of the free heating end of the heating element, after a short preheating period, which reduces the consumption of electrical energy and therefore fuel.
En particulier, lors du démarrage à froid du moteur où la faible température de la chambre de combustion et donc du mélange de gaz pénalise l'inflammation du mélange de gaz, l'utilisation de l'orifice secondaire selon l'invention injectant le carburant à proximité de l'extrémité chauffante de l'élément de préchauffage permet ainsi de favoriser l'inflammation du mélange de gaz. In particular, during the cold start of the engine where the low temperature of the combustion chamber and therefore of the gas mixture penalizes the ignition of the gas mixture, the use of the secondary orifice according to the invention injecting the fuel with proximity of the heating end of the preheating element thus promotes the ignition of the gas mixture.
En outre, l'orientation de l'axe de l'orifice secondaire permet de ne faire pénétrer que faiblement l'extrémité libre chauffante de l'élément de préchauffage dans la chambre de combustion. Ainsi, grâce à l'orifice secondaire de la buse de l'injecteur selon l'invention, l'élément de préchauffage n'entrave pas le flux d'air tourbillonnaire destiné à favoriser l'homogénéisation du mélange de gaz. In addition, the orientation of the axis of the secondary orifice makes it possible to penetrate only slightly the free heating end of the preheating element in the combustion chamber. Thus, thanks to the secondary orifice of the nozzle of the injector according to the invention, the preheating element does not hinder the vortex flow of air to promote the homogenization of the gas mixture.
Enfin, l'orifice secondaire de giclage de carburant situé en dehors de la rangée d'orifices primaires est principalement dédié au démarrage du moteur mais reste ultérieurement alimenté en carburant comme les orifices primaires, ce qui permet d'avoir un mécanisme de fonctionnement simple pour l'injecteur. Finally, the secondary fuel jet orifice located outside the row of primary orifices is mainly dedicated to starting the engine, but remains fueled at the same time as the primary orifices, which makes it possible to have a simple operating mechanism for the injector.
Ainsi, l'utilisation d'un orifice secondaire selon l'invention favorise le démarrage du moteur et réduit les contraintes d'encombrement et de consommation auxquelles il est soumis lors de son fonctionnement après démarrage. Thus, the use of a secondary orifice according to the invention promotes the starting of the engine and reduces the constraints of space and consumption to which it is subjected during its operation after startup.
Selon une première caractéristique avantageuse du moteur selon l'invention, le diamètre de l'orifice secondaire est inférieur au diamètre des orifices primaires. According to a first advantageous characteristic of the engine according to the invention, the diameter of the secondary orifice is smaller than the diameter of the primary orifices.
Selon une autre caractéristique avantageuse du moteur selon l'invention, le diamètre de l'orifice secondaire est d'au plus de 80 microns. According to another advantageous characteristic of the engine according to the invention, the diameter of the secondary orifice is at most 80 microns.
Selon une autre caractéristique avantageuse du moteur selon l'invention, l'orifice secondaire est disposé au-dessus de la rangée d'orifices primaires de giclage, par rapport au centre de la chambre de combustion. According to another advantageous characteristic of the engine according to the invention, the secondary orifice is disposed above the row of primary orifices for spraying, with respect to the center of the combustion chamber.
Selon une autre caractéristique avantageuse du moteur selon l'invention, l'axe de l'orifice secondaire fait un angle compris entre 80 et 90 avec l'axe d'un piston agencé dans la chambre de combustion. According to another advantageous characteristic of the engine according to the invention, the axis of the secondary orifice makes an angle of between 80 and 90 with the axis of a piston arranged in the combustion chamber.
Selon une autre caractéristique avantageuse du moteur selon l'invention, l'orifice secondaire est disposé en dessous de la rangée d'orifices primaires de giclage, par rapport au centre de la chambre de combustion. According to another advantageous characteristic of the engine according to the invention, the secondary orifice is disposed below the row of primary spraying orifices relative to the center of the combustion chamber.
DESCRIPTION DETAILLEE D'UN EXEMPLE DE REALISATION DETAILED DESCRIPTION OF AN EXEMPLARY EMBODIMENT
La description qui va suivre en regard des dessins annexés d'un mode de réalisation, donné à titre d'exemple non limitatif, fera bien comprendre en quoi consiste l'invention et comment elle peut être réalisée. The following description with reference to the accompanying drawings of an embodiment, given by way of non-limiting example, will make it clear what the invention consists of and how it can be achieved.
Dans les dessins annexés: la figure 1 est une vue en coupe d'une partie d'un moteur selon l'invention dans lequel sont agencés un injecteur de carburant et un élément de préchauffage; - la figure 2 est une vue de face de l'extrémité libre de la buse de l'injecteur du moteur de la figure 1; la figure 3 est une vue selon la coupe A-A de la figure 2. In the accompanying drawings: FIG. 1 is a sectional view of a part of an engine according to the invention in which are arranged a fuel injector and a preheating element; FIG. 2 is a front view of the free end of the nozzle of the injector of the engine of FIG. 1; FIG. 3 is a view along section A-A of FIG.
Sur la figure 1, on a représenté une partie d'un moteur à combustion interne de véhicule automobile de type diesel à injection directe. Ce moteur comprend un cylindre 5 dans lequel coulisse un piston 7. La paroi supérieure du cylindre 5 délimite avec la face extérieure creusée 71 de la tête du piston 7 une chambre de combustion 6. Une extrémité libre chauffante 28 d'un élément de préchauffage 8 et une extrémité libre 19 d'une buse 10 d'un injecteur 9 de carburant s'étendent dans la chambre de combustion 6, en vis-à-vis du piston 7. In Figure 1, there is shown a portion of a direct injection diesel engine internal combustion engine with direct injection. This engine comprises a cylinder 5 in which a piston 7 slides. The upper wall of the cylinder 5 delimits, with the outer hollow face 71 of the piston head 7, a combustion chamber 6. A free heating end 28 of a preheating element 8 and a free end 19 of a nozzle 10 of a fuel injector 9 extend into the combustion chamber 6, opposite the piston 7.
Ici, cet élément de préchauffage 8 est une bougie de préchauffage 8 dont l'extrémité libre chauffante 28 pénètre faiblement dans la chambre de combustion 6 pour ne pas entraver un flux d'air tourbillonnaire destiné à favoriser l'homogénéisation du mélange de gaz. Here, this preheating element 8 is a glow plug 8 whose free heating end 28 penetrates weakly into the combustion chamber 6 so as not to impede a swirling air flow intended to promote the homogenization of the gas mixture.
D'une part, l'injecteur 9 de carburant et sa buse 10, et d'autre part, le piston 7, présentent des axes A9, A7 qui, ici, sont confondus. Comme représenté sur la figure 2, l'extrémité libre 19 de la buse 10 comprend une rangée 17 d'orifices 11,12,13,14,15,16 de giclage de carburant, appelés orifices primaires, répartis circonférentiellement autour de l'axe A9 de la buse 10 de l'injecteur 9 de carburant. Chacun de ces orifices primaires 11,12,13,14,15,16 présente un axe A20,A20' qui fait un angle B20 de l'ordre de 70 avec l'axe A7 du piston 7 (voir figure 3). Ces orifices primaires 11,12,13,14,15,16 permettent d'injecter du carburant en jets 20,20' dirigés vers la face creusée 71 de la tête du piston 7 (voir figure 1). On the one hand, the fuel injector 9 and its nozzle 10, and on the other hand, the piston 7, have axes A9, A7 which, here, are merged. As shown in FIG. 2, the free end 19 of the nozzle 10 comprises a row 17 of fuel injection orifices 11, 12, 13, 14, 15, 16, called primary orifices, distributed circumferentially about the axis. A9 of the nozzle 10 of the fuel injector 9. Each of these primary orifices 11, 12, 13, 14, 15, 16 has an axis A20, A20 'which makes an angle B20 of the order of 70 with the axis A7 of the piston 7 (see FIG. 3). These primary orifices 11, 12, 13, 14, 15, 16 make it possible to inject fuel in jets 20, 20 'directed towards the sunken face 71 of the piston head 7 (see FIG. 1).
Avantageusement selon l'invention, comme le montre la figure 2, ladite extrémité libre 19 de la buse 10 de l'injecteur 9 comprend un orifice secondaire 18 destiné à l'injection de carburant pour le démarrage du moteur et apte à être alimenté en carburant simultanément aux orifices primaires de la rangée 17. Cet orifice secondaire 18 est situé au-dessus de la rangée 17 d'orifices primaires 11,12,13,14,15,16 de giclage, par rapport au centre de la chambre de combustion 6. Advantageously according to the invention, as shown in FIG. 2, said free end 19 of the nozzle 10 of the injector 9 comprises a secondary orifice 18 intended for the injection of fuel for starting the engine and able to be supplied with fuel. simultaneously with the primary orifices of the row 17. This secondary orifice 18 is located above the row 17 of primary orifices 11, 12, 13, 14, 15, 16 of spray, with respect to the center of the combustion chamber 6 .
Le diamètre d'au plus de 80 microns de l'orifice secondaire 18 est inférieur au diamètre des orifices primaires 11,12,13,14,15,16 de la rangée 17. The diameter of at most 80 microns of the secondary orifice 18 is smaller than the diameter of the primary orifices 11, 12, 13, 14, 15, 16 of the row 17.
Cet orifice secondaire 18 possède un axe A21 orienté sensiblement vers ladite extrémité libre chauffante 28 de l'élément de préchauffage 8 et fait alors un angle B21 de l'ordre de 85 avec l'axe A7 du piston 7 coulissant dans la chambre de combustion 6 confondu ici avec l'axe A9 de la buse 10 de l'injecteur 9 (voir figure 1). This secondary orifice 18 has an axis A21 oriented substantially towards said free heating end 28 of the preheating element 8 and then makes an angle B21 of the order of 85 with the axis A7 of the piston 7 sliding in the combustion chamber 6 here confused with the axis A9 of the nozzle 10 of the injector 9 (see Figure 1).
Le fonctionnement du moteur selon l'invention est décrit ci-dessous. Avant le démarrage à froid du moteur, la température de la chambre de combustion 6 est basse et donc pénalise l'inflammation du mélange de gaz. Lors du démarrage du moteur, le carburant arrivant par l'injecteur 9 jaillit d'une part, par les orifices primaires 11,12,13,14,15,16 de la rangée 17, et d'autre part, selon l'invention, par l'orifice secondaire 18 situé au-dessus de la rangée 17 d'orifices primaires 11,12,13,14,15,16, en un jet 21 dirigé vers l'extrémité libre chauffante 28 de la bougie 8. The operation of the engine according to the invention is described below. Before the cold start of the engine, the temperature of the combustion chamber 6 is low and therefore penalizes the ignition of the gas mixture. When starting the engine, the fuel arriving through the injector 9 springs, on the one hand, through the primary orifices 11, 12, 13, 14, 15, 16 of the row 17, and on the other hand, according to the invention. by the secondary orifice 18 situated above the row 17 of primary orifices 11, 12, 13, 14, 15, 16, in a jet 21 directed towards the free heating end 28 of the spark plug 8.
Avantageusement, grâce à l'orientation de l'axe A21 de l'orifice secondaire 18 sensiblement vers l'extrémité libre chauffante 28 de l'élément de préchauffage 8, le mélange de gaz est réalisé à proximité de cette extrémité libre chauffante 28. Le mélange de gaz possède alors une richesse satisfaisante et une température suffisante pour satisfaire aux conditions thermodynamiques d'inflammation du mélange de gaz, compensant ainsi la dégradation des conditions thermodynamiques résultant d'un faible taux de compression du mélange de gaz dans la chambre de combustion 6 par le piston 7. Advantageously, thanks to the orientation of the axis A21 of the secondary orifice 18 substantially towards the free heating end 28 of the preheating element 8, the gas mixture is produced near this free heating end 28. The gas mixture then has a satisfactory richness and a temperature sufficient to satisfy the thermodynamic conditions of ignition of the gas mixture, thus compensating for the degradation of the thermodynamic conditions resulting from a low compression ratio of the gas mixture in the combustion chamber. by the piston 7.
Grâce au faible diamètre de l'orifice secondaire 18 selon l'invention, la vaporisation du carburant injecté par cet orifice secondaire 18 de giclage est améliorée. Un plus grand volume de carburant vaporisé participe alors à la réalisation du mélange de gaz à proximité de l'extrémité libre chauffante 28 de l'élément de préchauffage 8, fournissant ainsi une richesse et une température du mélange de gaz favorable à son inflammation. Due to the small diameter of the secondary orifice 18 according to the invention, the vaporization of the fuel injected by this secondary orifice 18 of spray is improved. A larger volume of vaporized fuel then participates in producing the gas mixture near the free heating end 28 of the preheating element 8, thus providing a richness and a temperature of the gas mixture favorable to its ignition.
Grâce au faible diamètre de l'orifice secondaire 18 selon l'invention, la pénétration du liquide et de la vapeur du jet de carburant injecté par cet orifice secondaire 18 est réduite. La pénétration du jet étant faible, la dilution du carburant dans le film d'huile présent sur le cylindre 5 est très limitée. II n'y a donc pas d'altération de la qualité de l'huile. Due to the small diameter of the secondary orifice 18 according to the invention, the penetration of the liquid and the vapor of the jet of fuel injected by this secondary orifice 18 is reduced. Penetration of the jet being low, the dilution of the fuel in the oil film present on the cylinder 5 is very limited. There is therefore no alteration of the quality of the oil.
En outre, la vaporisation du carburant par son passage dans l'orifice secondaire 18 étant importante, il n'est pas nécessaire d'injecter, en particulier au démarrage du moteur, un grand volume de carburant liquide pour obtenir un grand volume de carburant vaporisé. Ainsi, au démarrage, les émissions polluantes sont réduites. In addition, the vaporization of the fuel through its passage in the secondary orifice 18 is important, it is not necessary to inject, especially at engine start, a large volume of liquid fuel to obtain a large volume of vaporized fuel . Thus, at startup, the pollutant emissions are reduced.
Puis, après l'inflammation du mélange de gaz à proximité de l'extrémité chauffante 28 de la bougie 8, l'inflammation se propage au carburant injecté, par les orifices primaires 11,12,13,14,15,16 de plus gros diamètres, dans la chambre de combustion 6. Then, after the ignition of the gas mixture near the heating end 28 of the spark plug 8, the ignition is propagated to the injected fuel, through the primary orifices 11, 12, 13, 14, 15, 16 of larger diameters in the combustion chamber 6.
Après le démarrage à froid du moteur, le carburant continue de jaillir non seulement par les orifices primaires 11,12,13,14,15,16 mais aussi par l'orifice secondaire 18. Après le démarrage du moteur, l'injection du carburant par les orifices primaires 11,12,13,14,15,16 selon les jets 20, 20', orientés chacun de l'angle B20 par rapport à l'axe A7 du piston 7, permet d'optimiser la combustion du mélange de gaz dans la chambre de combustion 6. Le flux de carburant continuant à jaillir de l'orifice secondaire 18 est faible comparé à celui jaillissant des orifices primaires 11,12,13,14,15,16 et cet orifice secondaire peut donc rester alimenté en carburant simultanément aux orifices primaires durant tout le fonctionnement du moteur, ce qui simplifie le fonctionnement de l'injecteur 9 de carburant. After the cold start of the engine, the fuel continues to flow not only through the primary orifices 11,12,13,14,15,16 but also through the secondary orifice 18. After starting the engine, the fuel injection by the primary orifices 11, 12, 13, 14, 15, 16 depending on the jets 20, 20 ', each oriented by the angle B20 with respect to the axis A7 of the piston 7, makes it possible to optimize the combustion of the mixture of gas in the combustion chamber 6. The flow of fuel continuing to flow from the secondary orifice 18 is small compared to that springing from the primary orifices 11,12,13,14,15,16 and this secondary orifice can therefore remain powered by fuel simultaneously to the primary ports during the entire operation of the engine, which simplifies the operation of the fuel injector 9.
La présente invention n'est nullement limitée au mode de réalisation décrit et représenté, mais l'homme du métier saura y apporter toute variante conforme à son esprit. The present invention is not limited to the embodiment described and shown, but the art can apply any variant within his mind.
En variante, il est possible de prévoir que l'orifice secondaire est situé en dessous de la rangée d'orifices primaires de giclage, par rapport au centre de la chambre de combustion. L'angle entre l'axe de cet orifice secondaire et l'axe du piston est alors adapté de sorte que l'axe de cet orifice secondaire soit orienté sensiblement vers ladite extrémité libre chauffante de l'élément de préchauffage. Alternatively, it is possible to provide that the secondary orifice is located below the row of primary spray orifices relative to the center of the combustion chamber. The angle between the axis of this secondary orifice and the axis of the piston is then adapted so that the axis of this secondary orifice is oriented substantially towards said free heating end of the preheating element.
On peut aussi utiliser un injecteur dont l'extrémité libre de la buse comporte plusieurs rangées d'orifices primaires. Ces différentes rangées sont alors obturées selon le mode de fonctionnement du moteur par un organe d'obturation coopérant avec la buse de l'injecteur, indépendamment de l'orifice secondaire orienté vers la bougie de préchauffage. It is also possible to use an injector whose free end of the nozzle comprises several rows of primary orifices. These different rows are then closed according to the operating mode of the motor by a closure member cooperating with the nozzle of the injector, independently of the secondary orifice directed towards the glow plug.
Il peut être aussi intéressant de prévoir un grand nombre d'orifices primaires sur la rangée correspondante afin de mieux répartir l'injection de carburant dans la partie centrale de la chambre de combustion. Ceci améliore alors la répartition du mélange de gaz dans la chambre de combustion et ainsi permet, lors du fonctionnement du moteur après démarrage, d'optimiser les performances dudit moteur. En outre, plus le nombre d'orifices primaires est important moins l'ajout d'un orifice secondaire pénalisera le débit de carburant dans la rangée d'orifices primaires nécessaire au fonctionnement du moteur après démarrage. It may also be advantageous to provide a large number of primary orifices on the corresponding row in order to better distribute the fuel injection in the central part of the combustion chamber. This then improves the distribution of the gas mixture in the combustion chamber and thus allows, during operation of the engine after startup, to optimize the performance of said engine. In addition, the greater the number of primary orifices is less the addition of a secondary orifice will penalize the flow of fuel in the primary row of orifices necessary for operation of the engine after startup.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0507304A FR2888284A3 (en) | 2005-07-08 | 2005-07-08 | Internal combustion engine for motor vehicle, has injector with nozzle, whose free end comprises secondary orifice for supplying fuel to primary orifices, where axis of secondary orifice is oriented towards end of preheater plug |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0507304A FR2888284A3 (en) | 2005-07-08 | 2005-07-08 | Internal combustion engine for motor vehicle, has injector with nozzle, whose free end comprises secondary orifice for supplying fuel to primary orifices, where axis of secondary orifice is oriented towards end of preheater plug |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2888284A3 true FR2888284A3 (en) | 2007-01-12 |
Family
ID=36121393
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0507304A Withdrawn FR2888284A3 (en) | 2005-07-08 | 2005-07-08 | Internal combustion engine for motor vehicle, has injector with nozzle, whose free end comprises secondary orifice for supplying fuel to primary orifices, where axis of secondary orifice is oriented towards end of preheater plug |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2888284A3 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2910072A1 (en) * | 2006-12-18 | 2008-06-20 | Peugeot Citroen Automobiles Sa | MOTOR VEHICLE, INJECTOR AND METHOD OF USING THE VEHICLE |
FR2927664A1 (en) * | 2008-02-15 | 2009-08-21 | Renault Sas | Internal combustion engine's e.g. diesel engine, fuel injector controlling method for motor vehicle, involves controlling two closing members at cold when temperature of cooling liquid is less than threshold value of cold start of engine |
EP3173614A1 (en) * | 2015-11-26 | 2017-05-31 | Robert Bosch Gmbh | Nozzle assembly for a fuel injector and fuel injector |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5979031A (en) * | 1982-10-29 | 1984-05-08 | Isuzu Motors Ltd | Direct-injection type diesel engine |
JPS6143216A (en) * | 1984-08-07 | 1986-03-01 | Isuzu Motors Ltd | Combustion chamber of diesel engine |
JPH02199218A (en) * | 1989-01-27 | 1990-08-07 | Mazda Motor Corp | Fuel injection device of diesel engine |
JPH02252917A (en) * | 1989-03-27 | 1990-10-11 | Hino Motors Ltd | Diesel engine |
JPH03202618A (en) * | 1989-12-28 | 1991-09-04 | Isuzu Motors Ltd | Alcoholic engine |
JPH0412174A (en) * | 1990-04-30 | 1992-01-16 | Isuzu Motors Ltd | Fuel collision dispersion type engine |
JPH0674131A (en) * | 1992-06-05 | 1994-03-15 | Agency Of Ind Science & Technol | Two-stage injection methanol engine |
WO2003078824A1 (en) * | 2002-03-13 | 2003-09-25 | Robert Bosch Gmbh | Fuel injection valve for internal combustion engines |
WO2004031551A2 (en) * | 2002-10-02 | 2004-04-15 | Westport Research Inc. | Control method and apparatus for gaseous fuelled internal combustion engine |
FR2857698A1 (en) * | 2003-07-18 | 2005-01-21 | Renault Sa | Diesel engine with direct fuel injection has angle between conical combustion chamber surface and cylinder head thrust face made for higher power and less pollution |
-
2005
- 2005-07-08 FR FR0507304A patent/FR2888284A3/en not_active Withdrawn
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5979031A (en) * | 1982-10-29 | 1984-05-08 | Isuzu Motors Ltd | Direct-injection type diesel engine |
JPS6143216A (en) * | 1984-08-07 | 1986-03-01 | Isuzu Motors Ltd | Combustion chamber of diesel engine |
JPH02199218A (en) * | 1989-01-27 | 1990-08-07 | Mazda Motor Corp | Fuel injection device of diesel engine |
JPH02252917A (en) * | 1989-03-27 | 1990-10-11 | Hino Motors Ltd | Diesel engine |
JPH03202618A (en) * | 1989-12-28 | 1991-09-04 | Isuzu Motors Ltd | Alcoholic engine |
JPH0412174A (en) * | 1990-04-30 | 1992-01-16 | Isuzu Motors Ltd | Fuel collision dispersion type engine |
JPH0674131A (en) * | 1992-06-05 | 1994-03-15 | Agency Of Ind Science & Technol | Two-stage injection methanol engine |
WO2003078824A1 (en) * | 2002-03-13 | 2003-09-25 | Robert Bosch Gmbh | Fuel injection valve for internal combustion engines |
WO2004031551A2 (en) * | 2002-10-02 | 2004-04-15 | Westport Research Inc. | Control method and apparatus for gaseous fuelled internal combustion engine |
FR2857698A1 (en) * | 2003-07-18 | 2005-01-21 | Renault Sa | Diesel engine with direct fuel injection has angle between conical combustion chamber surface and cylinder head thrust face made for higher power and less pollution |
Non-Patent Citations (7)
Title |
---|
PATENT ABSTRACTS OF JAPAN vol. 008, no. 189 (M - 321) 30 August 1984 (1984-08-30) * |
PATENT ABSTRACTS OF JAPAN vol. 010, no. 200 (M - 498) 12 July 1986 (1986-07-12) * |
PATENT ABSTRACTS OF JAPAN vol. 014, no. 488 (M - 1039) 24 October 1990 (1990-10-24) * |
PATENT ABSTRACTS OF JAPAN vol. 014, no. 583 (M - 1064) 26 December 1990 (1990-12-26) * |
PATENT ABSTRACTS OF JAPAN vol. 015, no. 473 (M - 1185) 29 November 1991 (1991-11-29) * |
PATENT ABSTRACTS OF JAPAN vol. 016, no. 161 (M - 1237) 20 April 1992 (1992-04-20) * |
PATENT ABSTRACTS OF JAPAN vol. 018, no. 325 (M - 1625) 21 June 1994 (1994-06-21) * |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2910072A1 (en) * | 2006-12-18 | 2008-06-20 | Peugeot Citroen Automobiles Sa | MOTOR VEHICLE, INJECTOR AND METHOD OF USING THE VEHICLE |
WO2008078038A2 (en) * | 2006-12-18 | 2008-07-03 | Peugeot Citroën Automobiles SA | Automotive vehicle, injector and method for using said vehicle |
WO2008078038A3 (en) * | 2006-12-18 | 2009-03-19 | Peugeot Citroen Automobiles Sa | Automotive vehicle, injector and method for using said vehicle |
FR2927664A1 (en) * | 2008-02-15 | 2009-08-21 | Renault Sas | Internal combustion engine's e.g. diesel engine, fuel injector controlling method for motor vehicle, involves controlling two closing members at cold when temperature of cooling liquid is less than threshold value of cold start of engine |
EP3173614A1 (en) * | 2015-11-26 | 2017-05-31 | Robert Bosch Gmbh | Nozzle assembly for a fuel injector and fuel injector |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0057150B1 (en) | Combustion chamber of an internal combustion piston engine for the generation of turbulence during combustion | |
EP1187982B1 (en) | Device for injecting a fuel into a combustion chamber of an internal combustion engine cylinder | |
EP1464804B1 (en) | Internal combustion engine having pre-chamber and spark ignition | |
FR2902462A1 (en) | Diesel type direct injection internal combustion engine for vehicle, has fuel injector injecting fuel in direction of cavities, where one of cavity directs injected fuel in direction of heater plug integrated to cylinder head | |
FR2888284A3 (en) | Internal combustion engine for motor vehicle, has injector with nozzle, whose free end comprises secondary orifice for supplying fuel to primary orifices, where axis of secondary orifice is oriented towards end of preheater plug | |
EP1344914B1 (en) | Internal combustion engine having fuel injection device | |
FR2770873A1 (en) | INTERNAL COMBUSTION ENGINE WITH SPARK IGNITION AND DIRECT INJECTION | |
FR2887304A1 (en) | Diesel type direct injection combustion ignition engine for motor vehicle, has gas pump nozzle`s free end with circumferential row whose angular sector has secondary orifice having axis oriented towards free end of preheating unit | |
EP1861596B1 (en) | Internal combustion engine, in particular with direct injection, with a piston provided with a trough comprising a dog point | |
FR2893673A1 (en) | Internal combustion engine e.g. spark ignition engine, has duct with channel emerging into pre-combustion chamber to supply fresh air, where chamber is delimited by wall having bend to generate whirling movement of fresh gas mixture | |
FR2830570A1 (en) | I.c. engine with controlled ignition has direct fuel injection system operating at very high pressure | |
FR2716495A1 (en) | Direct fuel injection for diesel engine | |
FR2463861A1 (en) | FUEL INJECTOR FOR DIESEL ENGINE | |
FR2895465A3 (en) | Fuel injector for e.g. common rail type direct injection diesel engine, has hollow nozzle with injection holes, where one hole includes main and secondary passages, whose structure permits to form zone at level of intersection of passages | |
WO2000017505A1 (en) | Spark ignition internal combustion engine | |
FR2831604A1 (en) | I.c. engine has cylinder head with central and peripheral spark plug holes for combustion chamber | |
FR3114614A1 (en) | Pre-chamber ignition device for a positive-ignition internal combustion engine | |
FR2743109A1 (en) | Controlled ignition I.C. engine, with spark produced in pre-combustion chamber | |
EP0661423B1 (en) | Diesel engine with directed gas flow at the exit of a swirl chamber | |
FR2910539A1 (en) | Preheater plug arrangement for e.g. direct injection oil engine, has preheater plug with heating element positioned in vertical plane passing through vertical axis of piston, vertical axis of combustion housing and lower end of injector | |
EP0907827B1 (en) | System for directly injecting fuel into a cylinder combustion chamber of an internal combustion engine | |
FR2878906A1 (en) | Direct injection internal combustion engine e.g. diesel engine, has fuel injector, and tulip with side wall forming negative inclination angle whose absolute value is equal to half crown angle of fuel jets and at least equal to zero degrees | |
FR2879722A1 (en) | Glow plug for air/fuel mixture in internal combustion chamber, has heating expanded with respect to cylindrical section to increase heat exchange surface with air/fuel mixture, where head presents aerodynamic profile | |
FR2712028A1 (en) | Internal combustion engine with indirect fuel injection | |
FR2904053A1 (en) | Internal combustion engine i.e. direct fuel injection type diesel engine, has base with internal deflector i.e. rectilinear wall, that guides fuel jet injected by fuel injector, where angle of deflector is equal to angle of lateral wall |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20070330 |