FR2879676A1 - Four stroke direct injection diesel engine for motor vehicle industry, has injector delivering fuel spray along narrow slick with angle and along wide slick having angle so that fuel impact point at wide slick is placed on side wall of bowl - Google Patents
Four stroke direct injection diesel engine for motor vehicle industry, has injector delivering fuel spray along narrow slick with angle and along wide slick having angle so that fuel impact point at wide slick is placed on side wall of bowl Download PDFInfo
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- FR2879676A1 FR2879676A1 FR0413769A FR0413769A FR2879676A1 FR 2879676 A1 FR2879676 A1 FR 2879676A1 FR 0413769 A FR0413769 A FR 0413769A FR 0413769 A FR0413769 A FR 0413769A FR 2879676 A1 FR2879676 A1 FR 2879676A1
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- angle
- bowl
- slick
- wide
- jets
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Classifications
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- 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
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- 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
- F02B23/0648—Means or methods to improve the spray dispersion, evaporation or ignition
- F02B23/0651—Means or methods to improve the spray dispersion, evaporation or ignition the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space
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- 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
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- 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
- F02B23/0696—W-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 wall
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- 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
- F02B23/08—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
- F02B23/10—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder
- F02B23/101—Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition with separate admission of air and fuel into cylinder the injector being placed on or close to the cylinder centre axis, e.g. with mixture formation using spray guided concepts
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- 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
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- 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
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Dispersion Chemistry (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Description
MOTEUR A INJECTION DIRECTEDIRECT INJECTION ENGINE
L'invention concerne un moteur à injection directe de carburant, et en particulier un moteur à injection directe de type diesel à quatre temps, tel qu'utilisé dans l'industrie automobile. The invention relates to a direct fuel injection engine, and in particular a four-stroke diesel direct injection engine, as used in the automotive industry.
Ces moteurs comprennent classiquement au moins un cylindre avec une culasse formant couvercle au-dessus du cylindre, sur laquelle sont montés, sensiblement parallèlement à l'axe du cylindre, au moins une soupape d'admission d'air frais, au moins une soupape d'échappement, et un injecteur central de carburant, et un piston monté coulissant dans le cylindre entre un point mort haut et un point mort bas et présentant à sa surface supérieure un bol muni d'un téton central. These engines conventionally comprise at least one cylinder with a cylinder head forming a lid above the cylinder, on which are mounted, substantially parallel to the axis of the cylinder, at least one fresh air intake valve, at least one exhaust, and a central fuel injector, and a piston slidably mounted in the cylinder between a top dead center and a bottom dead center and having on its upper surface a bowl provided with a central stud.
De nombreuses formes de profil du bol ont été proposées dans le but d'améliorer les performances du moteur et de réduire les émissions de polluants, tels que fumées, NOx, HC et CO. Many bowl profile shapes have been proposed in order to improve engine performance and reduce emissions of pollutants, such as fumes, NOx, HC and CO.
Classiquement, le bol du piston comporte un téton en forme de cône ou de tronc de cône, se raccordant à une paroi latérale qui peut être verticale ou comporter une concavité. L'injecteur pulvérise le carburant sous haute pression en plusieurs jets disposés sur un cône, dont l'axe coïncide avec l'axe vertical du bol. L'angle de nappe de l'injecteur est tel que les jets de carburant intersectent la paroi latérale du bol lorsque le piston est au point mort haut, et il en résulte un mouvement du mélange carburant/gaz d'admission vers le bas puis vers le centre du bol. Il a également été proposé, notamment dans le document EP 1 217 186, un injecteur avec un faible angle de nappe, de sorte que les jets de carburant issus de l'injecteur soient guidés par la paroi conique ou tronconique du téton central, le mélange effectuant alors un mouvement inverse de celui décrit précédemment. Conventionally, the bowl of the piston comprises a cone-shaped nipple or truncated cone, connecting to a side wall which can be vertical or have a concavity. The injector sprays the fuel under high pressure in several jets disposed on a cone, whose axis coincides with the vertical axis of the bowl. The web angle of the injector is such that the fuel jets intersect the side wall of the bowl when the piston is in the top dead center, and this results in a movement of the fuel / gas intake mixture downwardly and the center of the bowl. It has also been proposed, in particular in document EP 1 217 186, an injector with a low angle of coverage, so that the fuel jets coming from the injector are guided by the conical or frustoconical wall of the central nipple, the mixture then performing a reverse movement from that described above.
Pour améliorer le mélange du carburant et de gaz d'admission, et donc augmenter le rendement de la combustion dans la chambre, il est connu de générer un flux tourbillonnaire des gaz d'admission, appelé communément "swirl", autour d'un axe sensiblement identique à celui du cylindre, en adoptant une géométrie 10 et une disposition particulière des conduits d'admission d'air. To improve the mixing of fuel and intake gas, and therefore increase the efficiency of combustion in the chamber, it is known to generate a swirling flow of the intake gas, commonly called "swirl", about an axis substantially identical to that of the cylinder, adopting a geometry 10 and a particular arrangement of the air intake ducts.
L'invention a pour but de proposer un nouveau moteur à injection directe garantissant un bon compromis entre des performances spécifiques élevées et une émission de gaz polluants réduite. The invention aims to propose a new direct injection engine ensuring a good compromise between high specific performance and reduced emission of pollutants.
A cet effet, la présente invention a pour objet un moteur à injection directe de carburant comprenant au moins un cylindre avec une culasse formant couvercle au-dessus du cylindre, sur laquelle sont montés, sensiblement parallèlement à l'axe du cylindre, au moins une soupape d'admission, au moins une soupape d'échappement, et un injecteur central de carburant apte à injecter des jets de carburant en au moins une nappe, et un piston monté coulissant dans le cylindre et présentant à sa surface supérieure un bol muni d'un téton central, caractérisé en ce que ledit injecteur central est apte à délivrer simultanément des jets de carburant selon une première nappe étroite, l'angle ((3') de ladite première nappe et l'angle (a) au sommet du téton étant déterminés de sorte que les jets de ladite première nappe soient guidés par le flanc du téton lorsque le piston se trouve au voisinage de son point mort haut, et des jets de carburant selon une deuxième nappe large ayant un angle ((3") tel que le point d'impact des jets de ladite seconde nappe se situe au niveau de la paroi latérale du bol, de préférence dans la moitié inférieure de la paroi latérale du bol, lorsque le piston se trouve au voisinage de son point mort haut. For this purpose, the subject of the present invention is a direct fuel injection engine comprising at least one cylinder with a cylinder head forming a cover above the cylinder, on which are mounted, substantially parallel to the axis of the cylinder, at least one an intake valve, at least one exhaust valve, and a central fuel injector adapted to inject fuel jets into at least one sheet, and a piston slidably mounted in the cylinder and having on its upper surface a bowl provided with a central stud, characterized in that said central injector is adapted to simultaneously deliver fuel jets in a first narrow ply, the angle ((3 ') of said first ply and the angle (a) at the top of the stud being determined so that the jets of said first web are guided by the side of the nipple when the piston is in the vicinity of its top dead center, and fuel jets according to a second broad web ay an angle ((3 ") such that the point of impact of the jets of said second ply is at the side wall of the bowl, preferably in the lower half of the side wall of the bowl, when the plunger is near his top dead center.
Selon une particularité, la paroi latérale du bol comporte un rentrant concave, de sorte que les jets de carburant de la seconde nappe soient guidés par ledit rentrant concave lorsque le piston se trouve au voisinage de son point mort haut. According to one feature, the side wall of the bowl has a concave recess, so that the fuel jets of the second web are guided by said concave reentrant when the piston is in the vicinity of its top dead center.
Selon un mode de réalisation, le rentrant concave est formé d'une partie curviligne et d'une partie rectiligne inclinée, l'angle de la seconde nappe et l'angle d'inclinaison de la partie rectiligne étant déterminés pour permettre le guidage vers le bas des jets issus de cette nappe large. According to one embodiment, the concave reentrant is formed of a curvilinear part and of an inclined rectilinear part, the angle of the second sheet and the angle of inclination of the rectilinear part being determined to allow the guidance towards the low jets from this wide tablecloth.
Avantageusement, l'angle ((3') de la première nappe est compris entre 55 et 65 , et/ou l'angle au sommet (a) 20 du téton du bol est supérieur à l'angle ((3') de la première nappe de 5 à 15 , et/ou l'angle ((3") de la nappe large est compris entre 120 et 160 . Advantageously, the angle ((3 ') of the first ply is between 55 and 65, and / or the apex angle (a) of the bolt stud is greater than the angle ((3') of the first ply from 5 to 15, and / or the angle ((3 ") of the wide ply is between 120 and 160.
Selon une autre particularité, la nappe large et la nappe étroite comprennent chacune au moins trois jets 25 répartis à intervalle angulaire régulier. According to another feature, the wide web and the narrow web each comprise at least three jets 25 distributed at regular angular intervals.
Avantageusement, les orifices de sortie des deux nappes sont disposés selon un même plan. Advantageously, the outlets of the two sheets are arranged in a same plane.
Selon une autre particularité, les deux nappes sont disposées en quinconce, chaque nappe comprend n jets, 30 les orifices de sortie d'une nappe étant disposés à 360/(2xn) degrés de ceux de l'autre nappe. According to another feature, the two plies are arranged in staggered rows, each ply comprises n jets, the outlet orifices of one ply being arranged at 360 / (2xn) degrees from those of the other ply.
Selon une autre particularité, le moteur présente un mouvement tourbillonnaire ou "swirl" dont l'intensité est inférieure à lNd/N. In another feature, the motor has a swirling movement or "swirl" whose intensity is less than lNd / N.
Selon un mode de réalisation, le bol comprend une paroi latérale comportant une partie curviligne de rayon de courbure R2, une partie sensiblement rectiligne inclinée avec un angle d'inclinaison 0, et un col rentrant, ladite paroi latérale étant reliée à la paroi tronconique ou conique du téton par une paroi de transition comprenant une partie curviligne de rayon de courbure R1 et éventuellement une paroi sensiblement plane, ledit bol ayant un diamètre d'ouverture du bol D1, un diamètre moyen de fond de bol D2, un diamètre de col D3, une profondeur de bol H1, une profondeur de col H2, une distance d entre le sommet du téton et la surface supérieure du piston, une section de sortie S et un volume total V, et remplissant au moins l'une des conditions suivantes. According to one embodiment, the bowl comprises a side wall having a curvilinear portion of radius of curvature R2, a substantially rectilinear portion inclined with an inclination angle θ, and a retreating collar, said side wall being connected to the frustoconical wall or tapered cone of the nipple by a transition wall comprising a curvilinear portion of radius of curvature R1 and optionally a substantially flat wall, said bowl having an opening diameter of the bowl D1, a mean diameter of the bottom of the bowl D2, a neck diameter D3 , a bowl depth H1, a neck depth H2, a distance d between the top of the stud and the upper surface of the piston, an output section S and a total volume V, and fulfilling at least one of the following conditions.
- D1/ H1 entre 2 et 3,5; - R2/Rl entre 0,6 et 0, 85; - D2/D1 inférieur à 0,7; - D3/D1 entre 0.7 et 0.9; - H2 /H1 entre 0,6 et 0,85. - D1 / H1 between 2 and 3.5; R2 / R1 between 0.6 and 0.85; - D2 / D1 less than 0.7; - D3 / D1 between 0.7 and 0.9; - H2 / H1 between 0.6 and 0.85.
- 0 inférieur à 35 ; et/ou, - S/V entre 0,75 mm-1 et 1,5 mm-1. - 0 less than 35; and / or - S / V between 0.75 mm-1 and 1.5 mm-1.
La Demanderesse a découvert qu'en utilisant un injecteur à deux angles de nappe, avec une géométrie de bol particulier, telle que défini précédemment, et de préférence avec un faible niveau de "swirl", il était possible d'assurer une utilisation optimale du comburant présent dans la chambre de combustion, généralement l'oxygène de l'air, et d'obtenir ainsi de bonnes performances en terme de couple et de puissance spécifique, un niveau de pollution faible, avec notamment un faible bruit de combustion. The Applicant has discovered that by using a two-angled web injector, with a particular bowl geometry, as defined above, and preferably with a low level of "swirl", it was possible to ensure optimal use of the oxidant present in the combustion chamber, usually oxygen from the air, and thus obtain good performance in terms of torque and specific power, a low level of pollution, including low combustion noise.
L'invention sera mieux comprise, et d'autres buts, détails, caractéristiques et avantages apparaîtront plus clairement au cours de la description explicative détaillée qui va suivre d'un mode de réalisation particulier actuellement préféré de l'invention, en référence aux dessins schématiques annexés sur lesquels: - la figure 1 représente une vue schématique de dessus du toit de culasse d'un cylindre du moteur; - la figure 2 représente une vue partielle en coupe selon le plan II-II de la figure 1; - la figure 3 est une demi-coupe à échelle agrandie 15 du bol du piston de la figure 2; - la figure 4 représente une vue en coupe à échelle agrandie de la tête d'injection de la figure 2; et, - la figure 5 représente une vue de dessous de l'injecteur de la figure 4. The invention will be better understood, and other objects, details, features and advantages will become more clearly apparent from the following detailed explanatory description of a particular presently preferred embodiment of the invention, with reference to the schematic drawings. in which: - Figure 1 shows a schematic view from above of the cylinder head roof of the engine; - Figure 2 shows a partial sectional view along the plane II-II of Figure 1; FIG. 3 is an enlarged half-section of the bowl of the piston of FIG. 2; FIG. 4 represents a sectional view on an enlarged scale of the injection head of FIG. 2; and - Figure 5 shows a bottom view of the injector of Figure 4.
Les figures 1 et 2 illustrent un cylindre 1 de moteur à injection directe, en particulier d'un moteur de type diesel. Le cylindre est fermé à son extrémité supérieure par une culasse 2, et un piston 3 est monté coulissant, de manière étanche, dans l'alésage du cylindre. La chambre de combustion 4 est délimitée par la culasse et la face supérieure 31 du piston qui coulisse entre son point mort bas et son point mort haut. La face supérieure 31 du piston comporte une cavité circulaire ou bol profilé 5, sensiblement centré par rapport à l'axe A du cylindre. Le fond du bol comprend une élévation centrale ou téton 6 en forme de cône ou de tronc de cône d'angle au sommet a, relié par une paroi de transition 7 et une paroi latérale 8 à la face supérieure 31, cette dernière formant une zone de chasse frontale annulaire entourant le bol. La culasse 2 comprend l'injecteur central de carburant 9, une bougie 10 de réchauffage, ainsi que des soupapes 11 d'admission et d'échappement, par exemple deux soupapes d'admission et deux soupapes d'échappement, disposées autour de l'injecteur 9. Le moteur regroupe plusieurs cylindres avec des chambres de combustion analogues. Figures 1 and 2 illustrate a direct injection engine cylinder 1, in particular a diesel type engine. The cylinder is closed at its upper end by a cylinder head 2, and a piston 3 is slidably mounted, sealingly, in the bore of the cylinder. The combustion chamber 4 is delimited by the cylinder head and the upper face 31 of the piston which slides between its bottom dead center and its top dead center. The upper face 31 of the piston comprises a circular cavity or shaped bowl 5, substantially centered with respect to the axis A of the cylinder. The bottom of the bowl comprises a central elevation or cone-shaped taper 6 or angle cone frustum at the apex a, connected by a transition wall 7 and a side wall 8 to the upper face 31, the latter forming a zone annular frontal flush surrounding the bowl. The cylinder head 2 comprises the central fuel injector 9, a reheat plug 10, as well as intake and exhaust valves 11, for example two intake valves and two exhaust valves, arranged around the engine. Injector 9. The engine includes several cylinders with similar combustion chambers.
En référence aux figures 4 et 5, l'injecteur central 9 est disposé sensiblement selon l'axe A du cylindre et comprend, de manière connue, une tête ou nez d'injection 91 disposé en saillie dans la chambre de combustion et muni de trous ou passages pour injecter le carburant sous forme jets. Une aiguille d'injection 92 est montée dans la tête d'injection pour le réglage en débit et en pression des jets. Referring to Figures 4 and 5, the central injector 9 is disposed substantially along the axis A of the cylinder and comprises, in known manner, a head or injection nose 91 disposed projecting in the combustion chamber and provided with holes or passages for injecting fuel in jet form. An injection needle 92 is mounted in the injection head for adjusting the flow and pressure of the jets.
Selon l'invention, l'injecteur forme des jets de carburant disposés selon deux cônes ou nappes d'angles différents, dont les axes coïncident avec l'axe A du cylindre. Les jets de carburant sont disposés selon une première nappe dite étroite, ayant un angle de nappe I', et selon une deuxième nappe dite large ayant un angle de nappe Pu. Pour ce faire, le nez d'injection comprend une première série de trous ou passages 93a, 93b, 93c dont les axes sont disposés de manière à former la nappe étroite d'angle (3' et une deuxième série de passages ou trous 94a, 94b, 94c pour la formation de la nappe large d'angle (3". Les passages des deux nappes ont des sections transversales identiques, globalement circulaires, et disposés en quinconce à intervalle angulaire régulier. According to the invention, the injector forms fuel jets disposed in two cones or sheets of different angles, whose axes coincide with the axis A of the cylinder. The fuel jets are arranged in a first so-called narrow ply, having a lap angle I ', and in a second so-called wide ply having a ply angle Pu. To do this, the injection nose comprises a first series of holes or passages 93a, 93b, 93c whose axes are arranged so as to form the narrow corner ply (3 'and a second series of passages or holes 94a, 94b, 94c for the formation of the wide angle ply (3 ") The passages of the two plies have identical cross-sectional, generally circular, and arranged in staggered rows at regular angular intervals.
Les passages des deux nappes débouchent dans la chambre de combustion au même niveau, les orifices de sorties des passages étant centrés selon un même plan P, perpendiculaire à l'axe du cylindre. Dans le présent mode de réalisation, chaque nappe comprend trois passages 93a- b et 94a-b, les passages d'une même nappe étant espacés de 60 les uns des autres, les passages adjacents de deux nappes différentes étant disposés à 30 les uns des autres. The passages of the two plies open into the combustion chamber at the same level, the outlet orifices of the passages being centered on the same plane P, perpendicular to the axis of the cylinder. In the present embodiment, each web comprises three passages 93a-b and 94a-b, the passages of one and the same web being spaced apart from one another, the adjacent passages of two different webs being arranged on one of the webs. other.
En référence à la figure 3, sur laquelle sont représentées schématiquement les deux nappes d'angles R'et P", le téton 6 est disposé coaxialement aux axes des deux nappes de carburant issues de l'injecteur. Le téton présente une forme conique avec un sommet légèrement arrondi se poursuivant par une paroi conique ou flanc 62 sensiblement rectiligne en direction du fond du bol. Le flanc rectiligne se poursuit par la paroi de transition 7 comprenant une première partie curviligne 71 de rayon de courbure R1 et une paroi sensiblement plane 72 formant le fond du bol, et se termine par la paroi latérale 8 comprenant une deuxième partie curviligne 81 de rayon de courbure R2, une partie sensiblement rectiligne inclinée 82 formant un angle d'inclinaison A avec la verticale, raccordée à la face supérieure 31 annulaire par un congé 83 formant un col rentrant. With reference to FIG. 3, in which are shown diagrammatically the two plies of angles R 'and P', the stud 6 is arranged coaxially with the axes of the two fuel plies coming from the injector, the stud having a conical shape with a slightly rounded vertex continuing with a conical wall or flank 62 that is substantially rectilinear towards the bottom of the bowl The straight flank is continued by the transition wall 7 comprising a first curvilinear portion 71 of radius of curvature R1 and a substantially flat wall 72 forming the bottom of the bowl, and ends with the side wall 8 comprising a second curvilinear portion 81 of radius of curvature R2, a substantially straight inclined portion 82 forming an inclination angle A with the vertical, connected to the annular upper face 31 by a leave 83 forming a retreating collar.
En variante, le téton peut présenter une forme globalement tronconique avec un sommet sensiblement horizontal se poursuivant par un flanc sensiblement rectiligne, une partie de transition formée d'une seule partie curviligne, et une paroi latérale formée d'une partie curviligne, éventuellement de même rayon de courbure que celui de la partie de transition, et une partie sensiblement verticale reliée à la face supérieure du piston. As a variant, the stud may have a generally frustoconical shape with a substantially horizontal vertex continuing along a substantially rectilinear flank, a transition portion formed of a single curvilinear portion, and a lateral wall formed of a curvilinear portion, possibly likewise radius of curvature than that of the transition portion, and a substantially vertical portion connected to the upper face of the piston.
L'angle au sommet a du téton est adapté à l'angle R' de la nappe étroite de l'injecteur, de sorte que les jets de cette nappe étroite soient injectés sensiblement le long du flanc rectiligne du téton lorsque le piston est au voisinage du point mort haut. L'angle de nappe étroit R' est compris entre 55 et 65 . L'angle au sommet a du téton est supérieur à l'angle de nappe de la nappe étroite de 5 à 15 , les jets de carburant issus de l'injecteur forment donc un angle d'intersection d'au moins 5 avec le flanc du téton. La hauteur du téton est inférieure à la profondeur du bol, la distance d entre le sommet 61 du téton et la face supérieure du piston est comprise entre 4 et 5 mm. The angle at the apex of the stud is adapted to the angle R 'of the narrow ply of the injector, so that the jets of this narrow ply are injected substantially along the rectilinear flank of the stud when the piston is in the vicinity from the top dead center. The narrow ply angle R 'is between 55 and 65. The angle at the apex of the stud is greater than the ply angle of the narrow ply of 5 to 15, the fuel jets coming from the injector thus form an angle of intersection of at least 5 with the flank of the nipple. The height of the stud is less than the depth of the bowl, the distance d between the top 61 of the stud and the upper face of the piston is between 4 and 5 mm.
La géométrie du bol et l'angle R" de la nappe large sont tels que, lorsque le piston est au voisinage du point mort haut, le point d'impact des jets de cette nappe large se situe en dessous du col rentrant 83, au niveau de la partie rectiligne 82 de la paroi latérale du bol, sensiblement à mi-profondeur (H1/2), de sorte que les jets de cette nappe soient guidés par cette partie rectiligne. The geometry of the bowl and the angle R "of the wide ply are such that, when the plunger is in the vicinity of the top dead center, the point of impact of the jets of this wide ply lies below the retreating collar 83, level of the rectilinear portion 82 of the side wall of the bowl, substantially at mid-depth (H1 / 2), so that the jets of this sheet are guided by this rectilinear part.
Le flux de carburant issu d'un jet de la nappe étroite et celui issu d'un jet de la nappe large ont été représentés schématiquement sur la même figure 3, par les flèches référencées respectivement F1 et F2, ces flux sont bien entendu décalés angulairement, un flux de carburant issu d'une nappe étant intercalé entre deux flux de carburant en sens inverse de l'autre nappe. Les jets de la nappe large s'enroulent dans le tore formé entre la paroi inclinée 82 et la partie curviligne 81, puis remontent vers le téton central 6. Inversement, les jets de la nappe étroite descendent le long du téton puis remontent le long de la paroi inclinée. Ces injections du carburant simultanément selon deux nappes en quinconce assurent un bon mélange du carburant et de l'air présent dans la chambre. The fuel flow from a jet of the narrow web and that from a jet of the wide web have been shown schematically in the same FIG. 3, by the arrows respectively referenced F1 and F2, these flows are, of course, angularly offset. , a fuel flow from a web being interposed between two fuel flows in the opposite direction of the other web. The jets of the broad ply wrap in the torus formed between the inclined wall 82 and the curvilinear portion 81, then back to the central nipple 6. Conversely, the jets of the narrow ply descend along the nipple and back up along the inclined wall. These fuel injections simultaneously in two staggered plies provide a good mixture of fuel and air in the room.
On désigne par D1 le diamètre d'ouverture du bol, avec un rayon correspondant à la distance entre l'axe A et le point le plus éloigné de la deuxième partie curviligne 81, par D2 le diamètre moyen de fond de bol avec un rayon correspondant à la distance entre l'axe A et le milieu de la paroi plane horizontale 72 formant le fond du bol, par D3 le diamètre de col avec un rayon correspondant à la distance entre l'axe A et l'extrémité du col. H1 désigne la profondeur du bol, soit la distance entre la face supérieure 31 et la paroi horizontale 72, et H2 désigne la profondeur de col considéré au diamètre de col. Avantageusement, le bol remplit les conditions suivantes: - le rapport D1/ H1 est compris entre 2 et 3,5; - le rapport R2/R1 est compris entre 0,6 et 0, 85; - le rapport D2/D1 est inférieur à 0,7; - l'angle d'inclinaison 0 est inférieur à 35 25 - D3/D1 est compris entre 0.7 et 0.9; et, - H2 /H1 est compris entre 0, 6 et 0,85. Denote by D1 the opening diameter of the bowl, with a radius corresponding to the distance between the axis A and the furthest point of the second curvilinear portion 81, by D2 the mean diameter of the bottom of the bowl with a corresponding radius at the distance between the axis A and the middle of the horizontal plane wall 72 forming the bottom of the bowl, by D3 the neck diameter with a radius corresponding to the distance between the axis A and the end of the neck. H1 denotes the depth of the bowl, the distance between the upper face 31 and the horizontal wall 72, and H2 designates the neck depth considered at the neck diameter. Advantageously, the bowl fulfills the following conditions: the ratio D1 / H1 is between 2 and 3.5; the ratio R2 / R1 is between 0.6 and 0.85; the ratio D2 / D1 is less than 0.7; the angle of inclination θ is less than 35 - D3 / D1 is between 0.7 and 0.9; and, - H2 / H1 is between 0, 6 and 0.85.
Par ailleurs, le rapport de la section de sortie S du bol, considérée au niveau du diamètre de col D3, sur le volume total du bol V, soit S/V, est compris entre 0,75 mm-1 et 1,5 mm-1. Furthermore, the ratio of the outlet section S of the bowl, considered at the neck diameter D3, to the total volume of the bowl V, ie S / V, is between 0.75 mm-1 and 1.5 mm. -1.
L'intensité du mouvement de "swirl" est relativement faible, le rapport de la vitesse des gaz d'admission dans la chambre de combustion (Nd) en tour/min sur le régime moteur (N) en tour/min étant inférieur à 1, le niveau de "swirl" dans les moteurs de l'art antérieur étant classiquement compris entre 2 et 3,5 Nd/N. Cette géométrie de bol combinée à un injecteur à deux angles de nappe, et avec un "swirl" de faible intensité permet de concilier un niveau de performance spécifique élevé, notamment une puissance spécifique supérieure à 60 kW/1 à 4000 tr/min, et un niveau de polluants faible. The intensity of the "swirl" movement is relatively low, the ratio of the speed of the intake gases in the combustion chamber (Nd) in rev / min on the engine speed (N) in rev / min being less than 1 , the level of "swirl" in the engines of the prior art being conventionally between 2 and 3.5 Nd / N. This bowl geometry combined with an injector at two angles of the sheet, and with a low intensity "swirl" makes it possible to reconcile a high specific performance level, especially a specific power greater than 60 kW / l at 4000 rpm, and a low level of pollutants.
Bien que l'invention ait été décrite en liaison avec un mode de réalisation particulier, il est bien évident qu'elle n'y est nullement limitée et qu'elle comprend tous les équivalents techniques des moyens décrits ainsi que leurs combinaisons si celles-ci entrent dans le cadre de l'invention. Although the invention has been described in connection with a particular embodiment, it is obvious that it is not limited thereto and that it comprises all the technical equivalents of the means described and their combinations if they are within the scope of the invention.
Claims (10)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0413769A FR2879676A1 (en) | 2004-12-22 | 2004-12-22 | Four stroke direct injection diesel engine for motor vehicle industry, has injector delivering fuel spray along narrow slick with angle and along wide slick having angle so that fuel impact point at wide slick is placed on side wall of bowl |
DE102005058424A DE102005058424A1 (en) | 2004-12-22 | 2005-12-07 | Engine with direct injection |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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FR0413769A FR2879676A1 (en) | 2004-12-22 | 2004-12-22 | Four stroke direct injection diesel engine for motor vehicle industry, has injector delivering fuel spray along narrow slick with angle and along wide slick having angle so that fuel impact point at wide slick is placed on side wall of bowl |
Publications (1)
Publication Number | Publication Date |
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FR2879676A1 true FR2879676A1 (en) | 2006-06-23 |
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Family Applications (1)
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---|---|---|---|
FR0413769A Pending FR2879676A1 (en) | 2004-12-22 | 2004-12-22 | Four stroke direct injection diesel engine for motor vehicle industry, has injector delivering fuel spray along narrow slick with angle and along wide slick having angle so that fuel impact point at wide slick is placed on side wall of bowl |
Country Status (2)
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DE (1) | DE102005058424A1 (en) |
FR (1) | FR2879676A1 (en) |
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WO2009045641A1 (en) * | 2007-10-01 | 2009-04-09 | General Electric Company | Diesel combustion system with re-entrant piston bowl |
WO2009077506A1 (en) * | 2007-12-19 | 2009-06-25 | Renault S.A.S. | Combustion engine combustion chamber |
EP2169194A2 (en) | 2008-09-24 | 2010-03-31 | Deere & Company | Piston for an internal combustion (IC) reciprocating engine and piston |
FR3016926A1 (en) * | 2014-01-29 | 2015-07-31 | IFP Energies Nouvelles | COMBUSTION ENGINE WITH DIRECT FUEL INJECTION, ESPECIALLY COMPRESSION IGNITION ENGINE WITH LOW COMPRESSION RATE |
FR3034137A1 (en) * | 2015-03-24 | 2016-09-30 | Ifp Energies Now | INTERNAL COMBUSTION ENGINE WITH DIRECT FUEL INJECTION OF LOW THERMAL TRANSFER, IN PARTICULAR FOR MOTOR VEHICLE. |
CN113719342A (en) * | 2021-07-29 | 2021-11-30 | 东风商用车有限公司 | Jet-compression ignition combustion system with double swirl combustion chambers |
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EP1357274A1 (en) * | 2002-04-24 | 2003-10-29 | Renault s.a.s. | Combustion chamber for a multi-cylinder compression ignition engine, particularly a direct injection Diesel engine, and associated engine |
US20040237929A1 (en) * | 2003-05-30 | 2004-12-02 | Caterpillar Inc. | Fuel injector nozzle for an internal combustion engine |
WO2005001255A1 (en) * | 2003-06-30 | 2005-01-06 | Daimlerchrysler Ag | Compression-ignition internal combustion engine |
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- 2004-12-22 FR FR0413769A patent/FR2879676A1/en active Pending
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US20020117146A1 (en) * | 2000-12-20 | 2002-08-29 | Bertrand Gatellier | Direct-injection engine with small nappe angle and processes allowing such an engine to be used |
US20030172902A1 (en) * | 2002-03-15 | 2003-09-18 | Bertrand Gatellier | Internal-combustion engine with fuel injection device |
EP1357274A1 (en) * | 2002-04-24 | 2003-10-29 | Renault s.a.s. | Combustion chamber for a multi-cylinder compression ignition engine, particularly a direct injection Diesel engine, and associated engine |
US20040237929A1 (en) * | 2003-05-30 | 2004-12-02 | Caterpillar Inc. | Fuel injector nozzle for an internal combustion engine |
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Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
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WO2009045641A1 (en) * | 2007-10-01 | 2009-04-09 | General Electric Company | Diesel combustion system with re-entrant piston bowl |
US8881706B2 (en) | 2007-12-19 | 2014-11-11 | Renault S.A.S. | Combustion engine combustion chamber |
WO2009077506A1 (en) * | 2007-12-19 | 2009-06-25 | Renault S.A.S. | Combustion engine combustion chamber |
FR2925601A1 (en) * | 2007-12-19 | 2009-06-26 | Renault Sas | COMBUSTION CHAMBER FOR THERMAL ENGINE |
JP2011506847A (en) * | 2007-12-19 | 2011-03-03 | ルノー・エス・アー・エス | Combustion engine combustion chamber |
EP2169194A2 (en) | 2008-09-24 | 2010-03-31 | Deere & Company | Piston for an internal combustion (IC) reciprocating engine and piston |
EP2169194A3 (en) * | 2008-09-24 | 2012-09-05 | Deere & Company | Piston for an internal combustion (IC) reciprocating engine and piston |
FR3016926A1 (en) * | 2014-01-29 | 2015-07-31 | IFP Energies Nouvelles | COMBUSTION ENGINE WITH DIRECT FUEL INJECTION, ESPECIALLY COMPRESSION IGNITION ENGINE WITH LOW COMPRESSION RATE |
WO2015113803A1 (en) * | 2014-01-29 | 2015-08-06 | IFP Energies Nouvelles | Direct fuel injection combustion engine and more particularly a compression-ignition engine having a low compression ratio |
CN105940200A (en) * | 2014-01-29 | 2016-09-14 | Ifp新能源公司 | Direct fuel injection combustion engine and more particularly a compression-ignition engine having a low compression ratio |
US10215082B2 (en) | 2014-01-29 | 2019-02-26 | IFP Energies Nouvelles | Direct fuel injection combustion engine and more particularly a compression-ignition engine with a low compression ratio |
CN105940200B (en) * | 2014-01-29 | 2019-10-25 | Ifp新能源公司 | The compression ignition engine of fuel direct injection internal combustion engine and more specifically little compressible |
FR3034137A1 (en) * | 2015-03-24 | 2016-09-30 | Ifp Energies Now | INTERNAL COMBUSTION ENGINE WITH DIRECT FUEL INJECTION OF LOW THERMAL TRANSFER, IN PARTICULAR FOR MOTOR VEHICLE. |
CN113719342A (en) * | 2021-07-29 | 2021-11-30 | 东风商用车有限公司 | Jet-compression ignition combustion system with double swirl combustion chambers |
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