INTERNAL-COMBUSTION ENGINE WITH DIRECT FUEL INJECTION IN THE DIRECTION OF THE INTAKE GAS MOTION

Abstract

The present invention relates to an internal-combustion engine comprising a combustion chamber provided with a single intake valve (2), a single exhaust valve (3), two plugs (4a, 4b) and a fuel injector (5). Furthermore, the combustion chamber comprises means for forming an aerodynamic swirling motion structure of the intake gas in the combustion chamber. Besides, fuel injector (5) is oriented so as to inject the fuel into the central area of the combustion chamber in the direction of the aerodynamic swirling motion structure.

Claims

1. An internal-combustion engine comprising at least one cylinder in which a piston moves, the cylinder being associated with a combustion chamber provided with a single intake valve, a single exhaust valve, a fuel injector and two plugs, wherein the combustion chamber comprises means for forming an aerodynamic motion structure of the intake gas with turbulences within the combustion chamber, and the fuel injector is oriented so as to inject the fuel into the central area of the combustion chamber between the two plugs, in the direction of the aerodynamic motion structure of the intake gas.

2. A combustion engine as claimed in claim 1, wherein the fuel injector is arranged between the intake valve and a plug.

3. A combustion engine as claimed in claim 1, wherein the fuel injector has a machined part of cylindrical shape.

4. A combustion engine as claimed in claim 1, wherein the fuel injector is inclined with respect to the direction of the axis of cylinder at an angle below 15.

5. A combustion engine as claimed in claim 1, wherein the fuel injector is arranged within the combustion chamber, close to the periphery of the combustion chamber.

6. A combustion engine as claimed in claim 1, wherein the plugs are positioned between said intake valve and the exhaust valve.

7. A combustion engine as claimed in claim 1, wherein the fuel injector is positioned at a distance ranging between 5 and 15 mm, more specifically between 9 and 10 mm, from the intake valve and at a distance ranging between 20 and 40 mm, more specifically between 25 and 30 mm, from exhaust valve.

8. A combustion engine as claimed in claim 1, wherein the plugs (4a, 4b ) are spaced apart by a distance ranging between 30% and 50% of the diameter of the cylinder.

9. A combustion engine as claimed in claim 1, wherein the plugs and the intake (2) and exhaust (3) valves are positioned in such a way that the centres thereof form the vertices of a square.

10. A combustion engine as claimed in claim 9, wherein the square has an edge of length ranging between 24 and 31 mm.

11. A combustion engine as claimed in claim 1, wherein the plug closest to the fuel injector is inclined with respect to the direction of the cylinder axis at an angle ranging between 25 and 30.

12. A combustion engine as claimed in claim 1, wherein the plug furthest from the fuel injector is inclined with respect to the direction of the axis of the cylinder at an angle ranging between 25 and 35.

13. A combustion engine as claimed in claim 1, wherein the combustion chamber has a substantially elliptical shape, the intake and exhaust valves being arranged at the ends of the major axis of the ellipse, and the plugs being arranged close to the minor axis of the ellipse.

14. A combustion engine as claimed in claim 1, wherein the means for forming the intake aerodynamic motion structure involve the shape of the combustion chamber and/or the shape of the intake pipe.

15. Use of an internal-combustion engine as claimed in claim 1 with a Miller cycle.

16. A method of using the combustion engine as claimed in claim 1, comprising operating the combustion engine in a Miller cycle in which the intake valve closes before bottom dead center of the piston.

17. A combustion engine as claimed in claim 1, wherein the fuel injector is inclined with respect to the direction of the axis of cylinder at an angle ranging between 6 and 10.

18. A combustion engine as claimed in claim 1, wherein the fuel injector is inclined with respect to the direction of the axis of cylinder at an angle substantially equal to 8.

19. A combustion engine as claimed in claim 1, wherein the plugs are spaced apart by a distance ranging between 35% and 45% of the diameter of the cylinder.

20. A combustion engine as claimed in claim 1, wherein the plug closest to the fuel injector is inclined with respect to the direction of the cylinder axis at an angle ranging between 28 and 29.

Description

BRIEF DESCRIPTION OF THE FIGURES

[0032] Other features and advantages of the system according to the invention will be clear from reading the description hereafter, given by way of non limitative example, with reference to the accompanying figures wherein:

[0033] FIG. 1 illustrates a combustion chamber according to an embodiment of the invention,

[0034] FIG. 2 is a cross-sectional view of a combustion engine according to an embodiment of the invention,

[0035] FIG. 3 is a cross-sectional view of a combustion engine according to an embodiment of the invention,

[0036] FIG. 4 illustrates the structure of the swumble formed in a cylinder by means of the combustion chamber according to an embodiment of the invention,

[0037] FIG. 5 illustrates the injection of fuel into the combustion chamber according to an embodiment of the invention, and

[0038] FIG. 6 illustrates the evolution of the flame front within the context of a combustion in the combustion chamber according to an embodiment of the invention.

DETAILED DESCRIPTION OF THE INVENTION

[0039] The present invention relates to an internal-combustion engine. The internal-combustion engine comprises: [0040] at least one cylinder in which a piston moves, [0041] a combustion chamber associated with the cylinder, the combustion chamber comprising: [0042] a single intake valve, allowing delivery of the gas mixture to the combustion chamber before the combustion phase, [0043] a single exhaust valve, allowing discharge of the burnt gas after the combustion phase, [0044] a single fuel injector, allowing direct injection of the fuel into the combustion chamber, [0045] two plugs (also referred to as ignition devices), allowing ignition of the gas/fuel mixture in the combustion chamber, and [0046] means for forming an aerodynamic motion structure of the intake gas with turbulences in the combustion chamber (in other words, means allowing swumble and/or squish to be formed in the combustion chamber).

[0047] The gas mixture can comprise supercharged air or not, or a mixture of air, supercharged or not, with recirculated burnt gas.

[0048] The fuel can notably be gasoline or diesel fuel.

[0049] According to the invention, the fuel injector is so oriented as to inject the fuel in the direction of the intake gas aerodynamic motion structure, while preventing wetting of the walls. In this case, the fuel injector is oriented towards the centre of the combustion chamber so as to promote fuel injection between the two ignition devices. Thus, this cocurrent fuel injection allows to prevent breaking the aerodynamic structure of the intake gas while maintaining good fuel mixture homogeneity thanks to the turbulence level.

[0050] Using only two valves (one for the intake and the other for the exhaust) involves several design advantages. Indeed, such an engine is less expensive (with a limited number of parts), lighter and more compact. Furthermore, this design provides more space for the plugs and the injector.

[0051] Using a single intake valve facilitates the creation of swumble. Indeed, it is more difficult to create swumble with two dispensing intake pipes.

[0052] According to an aspect of the invention, the fuel injector can have a machined part of cylindrical shape so as to prevent fuel splash on the walls. In other words, in-place machining of the fuel injector is performed up to the combustion chamber (protruding into the combustion chamber) so as to ensure that the injector is not partly obstructed by the combustion chamber.

[0053] In order to enable proper fuel orientation, the fuel injector can be inclined with respect to the direction of the cylinder axis (generally the vertical axis). The angle of inclination of the fuel injector with respect to this direction can be below 15, it preferably ranges between 6 and 10 and it is more preferably substantially equal to 8.

[0054] According to an implementation of the invention, the fuel injector can be positioned at a distance ranging between 5 and 15 mm from the intake valve, preferably between 9 and 10 mm from the intake valve, and at a distance ranging between 20 and 40 mm, more specifically between 25 and 30 mm from the exhaust valve. The main advantage of this configuration is to have the fuel injector closer to the intake than to the exhaust, which allows better management of the temperature and possibly cooling thereof.

[0055] According to a characteristic, the plugs can be spaced apart by a distance ranging between 30% and 50% of the diameter of the cylinder, preferably between 35% and 45% of the diameter of the cylinder. This spacing is optimal for a dual flame front development that minimizes the combustion duration, while avoiding unburnt gas zones and zones where engine knock is likely to appear.

[0056] According to a configuration of the invention, the two plugs and the two valves (intake and exhaust) can be positioned in such a way that the centres thereof form the vertices of a square. Advantageously, the square formed can have an edge of length ranging between 24 and 31 mm.

[0057] Preferably, the plugs can be inclined with respect to the direction of the axis of the cylinder (generally the vertical direction), and more preferably at two different angles. This allows to compensate for the constraints related to the combustion engine architecture. Indeed, it was not possible to position the plugs vertically in the chamber at their optimum location. Inclining them allows to recentre the ignition point without entirely moving the plug.

[0058] According to an example embodiment, the plug closest to the fuel injector can be inclined with respect to the direction of the cylinder axis at an angle ranging between 25 and 30, preferably between 28 and 29.

[0059] According to an example embodiment, the plug furthest from the fuel injector can be inclined with respect to the direction of the cylinder axis at an angle ranging between 25 and 35, more specifically between 28 and 32, and preferably at an angle of substantially 30.

[0060] The means for forming the intake aerodynamic structure with turbulences (swumble and/or squish) can notably comprise the shape of the combustion chamber and/or the shape of the intake pipe.

[0061] According to an embodiment of the invention, the combustion chamber can have substantially the shape of an ellipse. This shape promotes considerable squish. Indeed, the ratio of the surface area of this ellipse to the surface area of a section of the cylinder is particularly small, which corresponds to a great squish.

[0062] In order to promote swumble and squish, the components of the combustion chamber can be arranged in a specific manner: [0063] the intake valve and the exhaust valve are arranged at the ends of the major axis of the ellipse, thus the valves are located at opposite ends and spaced apart, [0064] the plugs are arranged close to the minor axis of the ellipse, thus the plugs are located between the intake valve and the exhaust valve, and [0065] the fuel injector is arranged inside the ellipse, close to the periphery thereof, between the intake valve and a plug, this location promoting mixing of the gas and the fuel thanks to the swumble motion.

[0066] This elliptical design of the combustion chamber associated with this arrangement of the components allows to generate an aerodynamic swumble structure and to promote homogenization of the fuel mixture. Furthermore, it enables a high combustion rate while preventing autoignition phenomena. Indeed, it is reminded that swumble allows to benefit from excellent homogenization and a better combustion rate thanks to a higher turbulence level during the intake phase than those observed with the best current spark-ignition engines.

[0067] According to an embodiment of the invention, the ellipse can comprise a recess extending towards the intake valve. The recess is arranged substantially symmetrically to the fuel injector with respect to the major axis. In other words, the recess is on the side of the intake valve opposite the side on which the fuel injector is positioned. The recess thus is located between a plug and the intake valve. A recess is understood to be a modification in the outer shape of the ellipse, this modification being achieved towards the inside of the ellipse. The recess enables swirl type turbulences to be intensified. Indeed, the purpose of the recess is to promote the formation of the swirl part of the swumble motion. This recess creates an extension of the pipe in the chamber, which provides continuation of the aerodynamic structure formation.

[0068] According to an embodiment of the invention, the intake valve can be tangential to the ellipse. Thus, filling of the combustion chamber is optimized.

[0069] According to a characteristic of the invention, the exhaust valve can be tangential to the ellipse. Thus, emptying of the combustion chamber is optimized.

[0070] According to a configuration of the invention, the plugs are not positioned on the periphery of the ellipse. This arrangement of the plugs provides optimal propagation of the flame front in order to prevent engine knock and unburnt gas.

[0071] According to an embodiment of the invention, the combustion engine can comprise an air intake pipe connected to the combustion chamber, in which the intake valve configured to initiate a swumble motion, i.e. a rotating motion of the air about the cylinder axis (tumble) and a rotating motion about an axis perpendicular to the cylinder axis (swirl), is positioned.

[0072] FIG. 1 schematically illustrates, by way of non limitative example, a combustion chamber 1 according to an embodiment of the invention. Combustion chamber 1 substantially has the shape of an ellipse 6. Ellipse 6 is defined by the major axis 8 and the minor axis 9 thereof. Combustion chamber 1 comprises a single intake valve 2 located at one end of a semi-major axis 8. Intake valve 2 is tangential to ellipse 6. Combustion chamber 1 comprises a single exhaust valve 3 located at one end of a semi-major axis 8. This end lies opposite the end on which intake valve 2 is positioned. Exhaust valve 3 is tangential to ellipse 6. Combustion chamber 1 further comprises two plugs 4a and 4b. Plugs 4a and 4b are substantially arranged on minor axis 9 (close to minor axis 9). Furthermore, combustion chamber 1 comprises a single fuel injector 5. Fuel injector 5 is positioned inside ellipse 6, on the periphery thereof. Besides, fuel injector 5 is located between intake valve 2 and a plug 4a. On the side opposite to injector 5, ellipse 6 comprises a rectilinear recess 7. Rectilinear recess 7 is positioned between a plug 4b and intake valve 2. Rectilinear recess 7 extends towards intake valve 2.

[0073] In addition to promoting squish, elliptical shape 6 as presented also promotes the development of the swirl motion that starts in the intake pipe. This combustion chamber is somehow the extension thereof.

[0074] FIG. 2 schematically illustrates, by way of non limitative example, a partial cross-sectional view of a combustion engine according to an embodiment of the invention. It is a cross-section along axis AA of FIG. 1. FIG. 2 illustrates within the engine crankcase 16 (in white in the figure) notably a combustion chamber 1, an intake valve 2, located between an intake pipe 14 and the combustion chamber, and a plug 4a. This figure also shows actuator 15 of intake valve 2. Furthermore, axes 17a and 17b of plugs 4a and 4b respectively are also illustrated in this figure. Axis 17a corresponds to plug 4a and axis 17b corresponds to plug 4b (not shown in cutting plane AA). Both plugs 4a and 4b are inclined to the vertical (i.e. in the direction of the cylinder), the angles of inclination of axes 17a and 17b are different.

[0075] FIG. 3 schematically illustrates, by way of non limitative example, a partial cross-sectional view of a combustion engine according to an embodiment of the invention. It is a cross-section along axis BB of FIG. 1. FIG. 3 illustrates within engine crankcase 16 (in white in the figure) notably a combustion chamber 1 and a fuel injector 5. Fuel injector 5 comprises a machined part of substantially cylindrical shape 18 protruding into combustion chamber 1 so as to ensure that the injector is not partly obstructed by the combustion chamber. Furthermore, this figure also shows axis 19 of fuel injector 5. The fuel injector is inclined to the vertical (i.e. the direction of the cylinder), the angle of inclination of axis 19 being smaller than angles 17a and 17b of plugs 4a and 4b of FIG. 2.

[0076] According to an aspect of the invention, the internal-combustion engine comprises at least one cylinder. For example, the combustion engine can comprise two, three or four cylinders.

[0077] According to a characteristic of the invention, the combustion engine can comprise a burnt gas recirculation circuit (EGR).

[0078] The invention relates to a combustion engine specifically designed to obtain good fuel mixture homogeneity and thus to provide better combustion efficiency.

[0079] In particular, the combustion engine according to the invention is particularly suited for use with a so-called Miller cycle over a wide operating range. This cycle is characterized by an intake valve closure before the bottom dead center of the piston. This allows to have increased work recovery, in addition to cooling of the charge admitted.

[0080] Such a combustion engine can be used in the field of transport, road or air transport for example, or in the field of stationary installations such as a generator set.

Application Example

[0081] The features and advantages of the combustion engine according to the invention will be clear from reading the application example below.

[0082] FIG. 4 schematically shows, by way of non limitative example, a graphic representation of the aerodynamic swumble structure within intake pipe 10 and cylinder 11, for an engine provided with a combustion chamber according to the invention. FIG. 4 illustrates various gas streams 13 in these elements.

[0083] It is also observed that the combustion duration is independent of the distribution law spread and calibration, which is not found in current spark-ignition engines. This enables the overall efficiency of the internal-combustion engine to be positively impacted.

[0084] Thus, the combustion chamber according to the invention enables a high swumble in the cylinder, which optimizes the efficiency of the combustion and therefore of the combustion engine.

[0085] FIG. 5 schematically shows, by way of non limitative example, a visual representation of the fuel injection in combustion chamber 1 and cylinder 11, for a combustion engine according to the invention. Combustion chamber 1 is in accordance with the embodiment of FIG. 1: it has a substantially elliptical shape and it comprises an intake valve 2, two plugs 4a and 4b, and a fuel injector 5. Fuel injector 5 is so oriented as to inject the fuel in the direction of the aerodynamic motion structure of the intake gas while preventing wetting of the walls. In the present case, fuel injector 5 is oriented towards the centre of combustion chamber 1 so as to favour fuel injection between the two plugs 4a and 4b. FIG. 5 illustrates in dark grey several fuel sprays 20 coming from fuel injector 5. These sprays are directed towards the central area between the two plugs 4a and 4b.

[0086] FIG. 6 shows the evolution of the front flame during combustion for an engine comprising a combustion chamber as illustrated in FIGS. 1 and 2, FIG. 6 being a top view of cylinder 11 and of the combustion chamber. The combustion engine comprises an elliptical combustion chamber with a single intake valve 2, a single exhaust valve 3, two spark plugs 4a and 4b, and an injector (not shown). Each thumbnail image of FIG. 6 corresponds to a different time (Time) (time is defined by the crank angle, with 360 as the reference corresponding to the top dead centre of the piston during the engine combustion phase). The darker areas 18 correspond to the flame front. These thumbnails clearly show the advantage provided by the dual ignition point optimized according to the invention. Indeed, it can be noted that the flame front is circular and that it leaves no dead zone where unburnt gas might persist.