Gasoline internal combustion engine with assisted compression ignition

Abstract

An internal combustion engine includes a combustion chamber with a cylinder head, a cylinder, and a piston. The internal combustion engine also includes at least one intake valve and at least one exhaust valve that are connected to the combustion chamber, a fuel injector that injects fuel into the combustion chamber, at least two ignition devices arranged in the combustion chamber, and control means that control the valves, the injector, and the ignition means. The control means operate the engine according to different combustion modes including a controlled ignition combustion mode, a compression ignition combustion mode, and an assisted compression ignition combustion mode. The control means activate the ignition means in the assisted compression ignition combustion mode.

Claims

1. An internal combustion engine comprising: a combustion chamber, the combustion chamber comprising: a cylinder head, a cylinder, and a piston, at least one air intake valve and one exhaust valve connected to the combustion chamber, a fuel injector configured to inject fuel into the combustion chamber, at least two ignition devices arranged in the combustion chamber, and control means configured to control the valves, the injector, and the ignition means, wherein the control means operate the engine according to different combustion modes including: a controlled ignition combustion mode, a compression ignition combustion mode, and an assisted compression ignition combustion mode, wherein the control means are configured to activate the at least two ignition devices in the assisted compression ignition combustion mode, and wherein the control means activate the at least two ignition devices during a transition between the different combustion modes.

2. The engine according to claim 1, wherein at least one of the ignition devices is a spark plug or a glow plug.

3. The engine according to claim 1, wherein the engine comprises a prechamber that houses one of the ignition devices.

4. The engine according to claim 1, wherein at least one of the ignition devices is located between 5% and 40% of a bore diameter of the cylinder in a radial direction with respect to an axis of the cylinder.

5. The engine according to claim 1, wherein the engine is configured to produce a vortex movement perpendicular to an axis of the cylinder, and wherein a location of at least one of the ignition devices is in an area which, from a fuel jet and in a direction of the vortex movement, covers half of an angle between two consecutive fuel jets produced by the injector, and wherein the angle is measured perpendicular to the axis of the cylinder.

6. The engine according to claim 1, wherein a difference between a triggering of the at least two ignition devices is not more than 30 degrees of a crankshaft angle.

7. The engine according to claim 1, wherein the control means are configured to activate the ignition devices during the assisted compression ignition combustion mode to control a desired phasing and a distribution of heat release between a flame propagation phase and a compression ignition combustion phase.

8. The engine according to claim 1, wherein the activation of the ignition devices during the transition between the different combustion modes controls a desired phasing and a distribution of heat release between a flame propagation phase and a compression ignition combustion phase.

9. The engine according to claim 1, wherein the control means are configured to activate the two ignition means between a first fuel injection that forms a premix in the combustion chamber and a second fuel injection that burn by compression ignition.

10. The engine according to claim 1, wherein the control means are configured to activate several fuel injections that burn by compression ignition to control a desired phasing and a distribution of heat release between a flame propagation phase and a compression ignition combustion phase.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Other features and advantages will become apparent upon reading the following description of a particular non-limiting embodiment of the invention, made with reference to the figures in which:

(2) FIG. 1 shows schematically an internal combustion engine of the invention.

(3) FIG. 2 shows an embodiment of the invention seen from the bottom of the engine cylinder head.

(4) FIG. 3 represents an example of an engine operating map according to distinct combustion modes, based on the engine speed and load.

(5) FIG. 4 shows the combustion heat release in the combustion chamber in an example of combustion by assisted compression ignition.

DETAILED DESCRIPTION

(6) FIG. 1 shows a four-stroke internal combustion engine 1 whose engine cycle is conventionally broken down into four phases: an intake phase, a compression phase, a combustion-expansion phase and an exhaust phase. This engine 1 can be fitted to a motor vehicle to provide the power required for its motion.

(7) The engine 1 comprises a cylinder block 2 comprising several cylinders 3 (only one cylinder is shown in FIG. 1), closed at the top by a cylinder head 4. Inside this cylinder 3 is housed a piston 5 which makes it possible to define a combustion chamber 6 with the cylinder 3 and the cylinder head 4. The piston 5 is mounted to move in translation between a top dead center (TDC) and a bottom dead center (BDC).

(8) The piston 5 is connected to a crankshaft 7 by means of a connecting rod 8, so that the reciprocating sliding of the piston 5 in the cylinder 3 allows the rotation of the crankshaft 7.

(9) The cylinder head 4 comprises an intake manifold 9 opening into the combustion chamber 6 through an intake opening. This intake exhaust opening can be closed by an intake valve 10 movable between a closed position and an open position in which the intake air enters inside the combustion chamber 6. This intake valve 10 is moved between these open and closed positions by actuating means 11. The opening and closing of the intake valve 10 take place at determined times during the engine cycle.

(10) The intake manifold 9 is connected to an air intake line 12 through which the air admitted into the engine 1 arrives.

(11) The cylinder head 4 also comprises an exhaust manifold 13 also opening into the combustion chamber 6 through an exhaust opening. This exhaust opening can be closed by an exhaust valve 14 movable between a closed position and an open position in which the flue gases contained inside the combustion chamber 6 can escape. This exhaust valve 14 is moved between these open and closed positions by actuating means 15. The opening and closing of the exhaust valves 14 take place at determined times during the engine cycle.

(12) The exhaust manifold 13 is connected to an exhaust line 16 through which the flue gases produced by the engine 1 are evacuated.

(13) The engine 1 may further include a flue gas recirculation line 20 extending between the exhaust line 16 and the air intake line 12. This line is conventionally equipped with a valve 20a for controlling the flue gas flow to be returned to the air intake line 3 and a cooler 20b for these flue gases.

(14) The engine 1 may also include a turbocharger 21 whose compressor wheel 21a is arranged in the intake line 12 and the turbine 21b is arranged in the exhaust line 16.

(15) The engine 1 also includes a valve 22 for metering air admitted into the engine 1.

(16) The engine also comprises a fuel injector 17, arranged in the cylinder head 4 and designed to inject fuel directly inside the combustion chamber 6. According to this embodiment, the engine 1 is a gasoline fuel engine, gasoline being used as fuel injected by the injector 17. However, this fuel called gasoline fuel is not necessarily entirely gasoline, and may contain a subcomponent such as alcohol. This injector 17 is a so-called high-pressure injector, in that the fuel is injected into the combustion chamber 6 at an injection pressure of between 200 and 2,500 bars, which allows good atomization of the fuel and reduces its evaporation time. The injection pressure may be variable and adjusted to the operating conditions of the engine by means of a pump (not shown).

(17) The geometric compression ratio of engine 1 is between 15 and 20, which makes it possible to achieve the pressure and temperature conditions required for autoignition by compression of the air/fuel mixture.

(18) In this embodiment, ignition means are provided for each cylinder 3. These ignition means comprise a first ignition device 18 arranged in the combustion chamber. This first ignition device 18 may be a spark plug which supplies an amount of energy to the air fuel mixture in the form of a spark. The function of this spark is to assist the compression ignition of the fuel load, if necessary. The triggering of the spark is controlled at specific times during the engine cycle.

(19) According to the invention, the ignition means further comprise, for each cylinder 3, a second ignition device 19 arranged in the combustion chamber, separate from the first ignition device 18. This second ignition device 19 may also be a spark plug which supplies an amount of energy to the air fuel mixture in the form of a spark. The triggering of the spark is controlled at specific times during the engine cycle.

(20) FIG. 2 shows an embodiment of the invention seen from the bottom of the cylinder head 4 of the engine 1.

(21) In this embodiment, the engine 1 comprises, for each cylinder, two air intake valves and two exhaust valves for the flue gases in the combustion chamber. The fuel injector 17 is mounted on the cylinder head in the axis of the cylinder. This injector 17 is shown in FIG. 2 as being capable of producing seven fuel jets 25. Each jet 25 is separated at an angle of 2θ, seen in a plane orthogonal to the axis of the cylinder. This number of jets is not limiting; other injectors can be provided with more or less fuel jets.

(22) FIG. 2 shows a direction 24 of circular aerodynamic vortex movement rotating around the central axis of the cylinder, also called “swirl”.

(23) As illustrated in FIG. 2, each of the locations of the two spark plugs 18, 19 is in a region which, from a fuel jet and in the vortex direction 24, covers half of the angle θ between two consecutive fuel jets produced by the injector 17, the angle being measured along a plane orthogonal to the axis of the cylinder 3. In the radial direction with respect to the axis of the cylinder, the spark plugs 18, 19 are between 5% and 40% of the cylinder bore diameter.

(24) As mentioned above, the ignition devices are spark plugs in that embodiment. However, other type of ignition devices may be provided for at least one of the ignition devices, such as a glow plug or corona igniter.

(25) In an embodiment not shown, the combustion chamber 6 may also include a prechamber housing one of the ignition devices. The prechamber may also house the fuel injector.

(26) The various components of the engine 1 which may be controlled, such as the valves 10, 14 via the actuators 11, 15, the ignition means 18 and 19, the fuel injector 17, the air metering valve 22 and, where appropriate, the flue gas flow control valve 20a, are controlled by means 23 for controlling the operation of the engine. This control means 23 may be an electronic computer.

(27) The control means 23 are also provided to make it possible to operate the engine 1 according to several combustion modes and to choose the combustion mode to be adopted based on operating parameters of the engine such as its speed and its load.

(28) FIG. 3 shows an example of the application of the different combustion modes adopted depending on the speed, N, and engine load, L. These different combustion modes are: a combustion mode by controlled ignition, SI: in this combustion mode, combustion is initiated by the spark plug. This combustion mode corresponds to the controlled ignition and flame propagation combustion mode generally adopted in spark ignition engines. In this combustion mode, the fuel load is mixed with air prior to ignition. a combustion mode by compression ignition, CI: in this combustion mode the combustion takes place by compression without the assistance of an external ignition.

(29) The temperature and pressure conditions are conducive to the autoignition of the fuel mixture. a combustion mode by assisted compression ignition, ACI: this combustion mode is a combination of the two previous combustion modes, SI and CI. In this combustion mode, a portion of the fuel load is premixed then ignited by at least one ignition device, while the remainder of the fuel load is then burned by compression ignition.

(30) Thus, this ACI combustion mode is a hybrid mode of combustion where both flame propagation and compression ignition occur sequentially.

(31) An example of the sequence of events is explained in more detail with reference to FIG. 4.

(32) FIG. 4 is a graph showing the rate of combustion heat release inside the combustion chamber of a conventional internal combustion engine in a fully hot condition including a cylinder head depicted in FIG. 2. In this example, the engine speed is 1500 rpm and the engine power corresponds to an average load. The x-axis represents the engine cycle and the value 0, the combustion top dead center.

(33) A fully hot engine condition is understood to mean an engine for which the engine coolant temperature is equal to 90° C. or higher. The engine condition will be qualified as partially hot for a coolant temperature between 30° C. and 90° C. The engine condition will be qualified as cold if the engine coolant temperature is below 30° C.

(34) The trigger signals to activate the fuel injection and the ignition are also displayed respectively by the references 26 and 27. In this example, two injection events are performed, one before the ignition is triggered and the other after the ignition is triggered.

(35) The graph of case A corresponds to the case where only the spark plug 18 is activated and the spark plug 19 is not activated. The graph of case B corresponds to the case where the two spark plugs 18 and 19 are activated simultaneously by the ignition trigger signal 27.

(36) The sequence of events leading to combustion for case A with reference to FIG. 4 is as follows:

(37) The first injection of the injector 17 takes place during the compression stroke of the engine when the piston is close to TDC (top dead center). This first injection is intended to form a premix in the combustion chamber 6. The spark plug 18 is activated, which triggers the combustion of the fuel injected from the very first injection in spark ignition mode. This results in a significant increase in the pressure and temperature inside the combustion chamber due to combustion.

(38) After a few degrees of crankshaft angle of the engine, a second fuel injection takes place, as shown in FIG. 4. During this second injection, combustion of the fuel from the first injection is still in progress. Due to the high temperature of the mixture inside the combustion chamber, the fuel entering during this second injection begins to ignite rapidly in the compression ignition combustion mode. The unburned fuel from the first injection and any partially burned fuel from the flame propagation combustion mode are now rapidly burned in the compression ignition combustion mode. After the completion of both fuel injections, any remaining unburned or partially burned fuel is burned in the compression ignition mode.

(39) It can be seen from FIG. 4 that, in case A where only one ignition device 18 is activated, the rate of heat release is comparatively higher than in case B where both ignition devices 18 and 19 are activated. The second ignition device 19 creates an additional flame which increases the combustion rate in the flame propagation combustion mode before the start of the second injection, thereby controlling the total amount of injected fuel that burns in the flame propagation mode and in the compression ignition mode. It can be seen in FIG. 4 that the heat release under the first peak corresponds to combustion in flame propagation mode and the heat release under the second upper peak corresponds to combustion in compression ignition mode. In this example, case B has a higher heat release in flame propagation mode and a lower heat release in compression ignition mode compared to case A. The control means 23 are arranged to activate the ignition devices 18, 19 during the combustion mode by assisted compression ignition (ACI) for controlling the phasing, in other words, the desired timing during the engine cycle, and distribution of heat release between a flame propagation phase and a combustion phase by compression ignition.

(40) This technique of using a secondary ignition device for controlling the heat release in controlled ignition or flame propagation combustion mode, and in compression ignition combustion mode, is advantageous in that it optimizes combustion performance.

(41) The timing of the triggering of the second ignition device 19 with respect to the timing of the triggering of the first ignition device 18 may be optimized for different operating conditions depending on the speed, engine load and engine condition. By optimizing the triggering times of the injection and ignition devices, the distribution of heat release between the flame propagation phase and the autoignition combustion phase may be modified and easily controlled, which makes it possible to improve combustion performance and control. The maximum difference between the triggering of the first ignition device and the last ignition device, here the second ignition device 19, is preferably not more than 30 degrees of crankshaft angle. The use of at least two ignition devices as described is advantageous to achieve the desired combustion mode, in particular when the engine is in a cold or partially hot condition, and during the transition between the different combustion modes, in order to control the phasing, in other words, the timing in the engine cycle, and the desired distribution of heat release between a flame propagation phase and a combustion phase by compression ignition. This results in improved efficiency, reduced emissions and better combustion stability.

(42) The invention is not limited to the above embodiment. As a variant, the second fuel injection may be replaced by several fuel injections intended to burn by autoignition in order to control the phasing, in other words, the timing in the engine cycle, and the desired distribution of heat release between a flame propagation phase and a combustion phase by compression ignition.

(43) The invention is not limited to the illustration in FIG. 2. The orientation and the number of ignition devices are not restrictive. The number of injector holes is also not restrictive. The activation sequences of the ignition devices with respect to the injection times are not restrictive. The ignition systems may be activated or deactivated depending on certain engine operating conditions.

(44) For economic reasons, this engine 1 may be an internal combustion engine with compression ignition initially intended to run on diesel. This engine, initially intended to run on diesel, conventionally includes a housing for a glow plug and, in order to maximize the investment, it is provided to use this glow plug housing to install one of the two ignition devices 18, 19.

(45) Nevertheless, a more optimal location for combustion, and therefore different from the position of the glow plug, may also be envisaged. However, this option is less economical because additional manufacturing operations are to be expected: sealing of the glow plug housing, fitting of a spark plug housing in the cylinder head.

(46) By using an additional second ignition device, the invention makes it possible to increase the flexibility in combustion control and, therefore, this leads to improved optimization of engine performance. The use of the combustion mode by assisted compression ignition can be applied over broader engine speed/load/temperature ranges than the prior art.

(47) Therefore, the invention improves the operation of such combustion mode by assisted compression ignition, thereby improving thermal efficiency, reducing emissions and achieving better combustion control.