Fuel regulation or control

Abstract

Fuel control or regulation system (44) for an engine (1), wherein the fuel control or regulation system (44) regulates or controls the behavior of fuel, which is injected directly into a combustion chamber (16) formed inside a cylinder (2) of the engine (1) by means of a swirl flow (T), and wherein the fuel control or regulation system (44) comprises: a wobble current generator (18) for generating the wobble current (T) within the combustion chamber (16); and a fuel injection device control or control module for causing the fuel injection device (28) to inject fuel at a first injection time and then inject a smaller quantity of fuel than that injected at the first injection time in a direction substantially opposite to a positive or necessary direction of the swirl flow (T) at a second injection time, wherein the first injection time is determined or selected to be in an intake stroke of the cylinder (2), and wherein the second injection time is determined or selected to be in a later half of a compression stroke of the cylinder (2). wherein the fuel injection device (28) is arranged at a position of a circumferential edge section of the ceiling of the combustion chamber (2) on a side where an inlet opening (18) is provided, and injects the fuel substantially obliquely downwards and in the direction of a side opposite the inlet opening (18), wherein the engine has a piston (14) which has a crown surface (46), and the crown surface (46) is formed with an inclined surface (50) which extends obliquely upwards from an end section of the crown surface (46) on the side facing away from the fuel injection device (28) towards a center of the crown surface (46), and wherein the second injection time is determined to be a time at which a positive direction of a lower section of the wobble flow (T) is oriented substantially obliquely upwards towards the fuel injection device (28) along the inclined surface (50) and the fuel is injected substantially opposite to the positive direction of the lower section of the wobble flow (T).

Description

BACKGROUND

[0001] The present invention relates to a fuel control system for an engine, particularly to a fuel control system of an engine that uses a tumble flow to control the behavior of fuel injected directly into a combustion chamber formed inside a cylinder of the engine. The present invention further relates to a corresponding engine, a fuel control method, and a computer program product.

[0002] When an operating range of an engine is within an operating range where an engine load is high and an engine speed is low, abnormal combustion such as knocking and pre-ignition easily occur due to inhomogeneous mixed gas and slow flame propagation after spark ignition inside a combustion chamber of the engine. To suppress such abnormal combustion (e.g., knocking), it is known to considerably retard an ignition timing to after a compression top dead center (CTDC). However, if the ignition timing is retarded to after the CTDC, a combustion pressure inside the combustion chamber reduces, and thus an output torque of the engine also reduces.

[0003] Therefore, a teaching of dividing fuel injection into a combustion chamber into a plurality of injections to ensure high torque while suppressing knocking is proposed. For example, with an engine control method disclosed in JP 4 924 751 B1, when an operating state of the engine is within a first engine speed range where the engine speed is relatively low, a retarding amount of ignition timing is determined.designed to be larger than within a second engine speed range where the engine speed is higher than the first engine speed range, a fuel injection mode is determined to be a split-injection mode in which fuel is injected at least twice, and a final injection timing thereof is determined to be in an early half of the compression stroke. The fuel injected into the combustion chamber in the early half of the compression stroke reduces a temperature of a mixed gas inside the combustion chamber by a latent heat of vaporization. Thus, knocking can be suppressed, and accordingly, the ignition timing can be advanced to increase torque.

[0004] Meanwhile, it is known that by increasing a flame propagation speed after spark ignition, a mixed gas can be burned normally before knocking occurs, thus improving the knock resistance.

[0005] However, with the engine control method in JP 4 924 751 B1 described above, ignition is performed in a state where the fuel injected into the combustion chamber in the early half of the compression stroke is substantially uniformly distributed inside the combustion chamber during the compression stroke. Therefore, compared with the case where the divided injections of fuel are not performed, there is no change in the air-fuel ratio of a mixture gas near a spark plug, and therefore there is no significant difference in the flame propagation speed.

[0006] Therefore, in the conventional engine control method described above, there is a range for further improving the knock resistance by increasing the flame propagation speed and advancing the ignition timing to increase the torque.

[0007] DE 602 00 744 T2 discloses a spark-ignited internal combustion engine with direct injection and turbocharger in which an operating range of high speed and high load is improved.

[0008] DE 602 02 247 T2 discloses a method and a device for a direct-injection Otto internal combustion engine and a computer-readable storage medium and a computer program.

[0009] AT 006 104 U1 describes a method for operating a spark-ignition four-stroke internal combustion engine with stabilization of idle operation.

[0010] US 2005 / 0 161 021 A1 describes a control device for a spark-ignition internal combustion engine with direct injection.

[0011] DE 10 2005 044 544 A1 discloses a method for operating a spark-ignition 4-stroke internal combustion engine. SUMMARY

[0012] The present invention has been made with a view to solving the problems of the above-described prior art and aims to provide a fuel control for an engine capable of achieving high torque while suppressing knocking even within an engine operating range where abnormal combustion such as knocking easily occurs.

[0013] This object is achieved according to the invention by the features of the independent claims. Particular embodiments of the invention are the subject of the dependent claims.

[0014] According to one aspect of the present invention, a fuel control system for an engine is provided. The fuel control system controls, through the use of a tumble flow, a behavior of fuel injected directly by a fuel injector into a combustion chamber formed inside a cylinder of the engine. The fuel control system includes a tumble flow generator for generating the tumble flow within the combustion chamber, and a fuel injector control module for inducing or controlling the tumble flow.Causing the fuel injector to inject the fuel at a first injection timing and then inject a smaller amount of fuel than an amount injected at the first injection timing in a direction substantially opposite to a positive direction of the tumble flow at a second injection timing, wherein the first injection timing is selected to be in an intake stroke of the cylinder, wherein the second injection timing is selected to be in a later half of a compression stroke of the cylinder.

[0015] With this configuration, the fuel injector control system causes the fuel injector to inject fuel at the first injection timing and then inject the smaller amount of fuel than the amount injected at the first injection timing in the direction substantially opposite to the positive direction of the tumble flow at the second injection timing. Therefore, in the fuel injection at the second injection timing, a kinetic energy of the fuel injected by the fuel injector is canceled (or greatly reduced) by a kinetic energy of the tumble flow opposite to the fuel injection direction, and thus the fuel does not permeate the tumble flow, and a region where the fuel is rich can be formed within a lower cross section.portion of the tumble flow. Moreover, by shifting the rich region along the tumble flow to be located near a tip of a spark plug at an ignition timing, ignitability by the spark plug can be improved, and since a flame propagation speed increases, knock resistance can be improved. Moreover, particularly, by injecting at the first injection timing the larger amount of fuel than the amount injected at the second fuel injection timing, evaporation of the fuel is stimulated to cool a mixed gas having latent heat, and knock resistance can be further improved. Therefore, even within an operating orIn the operating range where abnormal combustion such as knocking is likely to occur, knocking can be reliably suppressed, and accordingly, the ignition timing can be advanced to increase torque. Furthermore, especially by injecting a larger amount of fuel at the first injection timing, the fuel can be evenly distributed within the combustion chamber to achieve homogeneous combustion, and thus, emission performance can also be improved.

[0016] According to a particular embodiment, the second injection timing is preferably determined to be between approximately 50° and approximately 90° before a top dead center of the compression stroke.

[0017] With this configuration, the fuel can be surely injected at a timing at which the injection direction of the fuel is opposite to the tumble flow, and thus the fuel-rich region can be formed within the tumble flow, and the rich region can be shifted along the tumble flow to be surely located near the tip of the spark plug at the ignition timing, and the flame propagation speed can be surely increased.

[0018] In particular, the fuel injector control module preferably causes the fuel injector to inject about 10% to about 20% of a total fuel injection quantity in an operating cycle of the cylinder at the second injection timing.

[0019] With this configuration, when the rich region formed within the tumble flow is shifted close to the tip of the spark plug at the ignition timing, the mixed gas near the tip of the spark plug can be appropriately enriched and the flame propagation speed can be surely increased, and moreover, the mixed gas within a region away from the spark plug can be prevented from becoming excessively lean and occurrence of unstable combustion can be prevented.

[0020] Furthermore, the tumble flow generator is or includes an intake port of the engine. A spark plug of the engine is preferably provided in a central portion of a ceiling of the combustion chamber. According to the invention, the fuel injector is arranged at a position of a peripheral edge portion of the ceiling of the combustion chamber on a side where the intake port is provided, and injects the fuel substantially obliquely downward and toward an opposite side from the intake port. The engine includes a piston having a crown surface, and the crown surface is formed with an inclined surface extending obliquely upward from an end portion of the crown surface on the side facing away from the fuel injector toward a center of the crown surface.The second injection timing is determined to be a timing at which a positive direction of a lower portion of the tumble flow is oriented substantially obliquely upward toward the fuel injector along the inclined surface of the crown surface and the fuel is injected substantially opposite to the positive direction of the lower portion of the tumble flow.

[0021] With this configuration, the fuel injector control module causes the fuel injector to inject the fuel at the second injection timing, which is determined to be the timing at which the fuel injection direction of the fuel injector is opposite to the extending direction of the inclined surface of the crown surface. Therefore, the fuel can be injected in the direction opposite to the positive direction of the lower section of the tumble flow, which is obliquely upward and toward the fuel injector along the inclined surface of the crown surface.Thus, the fuel-rich region can be formed within the tumble flow, the rich region can be shifted along the tumble flow to be surely located near the tip of the spark plug at the ignition timing, and the flame propagation speed can be surely increased.

[0022] Furthermore, in particular, the injection direction of the fuel by the fuel injection device is or lies substantially parallel to the extending direction of the inclined surface of the crown surface.

[0023] With this configuration, the fuel injection direction can be reliably opposite to the positive direction of the tumble flow, which is obliquely upward and toward the fuel injector along the inclined surface of the crown surface. Thus, the fuel-rich region can be formed within the tumble flow, the rich region can be shifted along the tumble flow to be more securely located near the tip of the spark plug at the ignition timing, and the flame propagation speed can be reliably increased.

[0024] The fuel injector control module preferably causes the fuel injector to inject the fuel at the second injection timing when an operating condition of the engine in a warm-up state is within an operating range of the engine where an engine load is relatively high and an engine speed is relatively low, and the fuel injector control module preferably does not cause the fuel injector to inject the fuel at the second injection timing when the operating condition of the engine in the warm-up state is outside the operating range where the engine load is relatively high and the engine speed is relatively low or when the engine is in a cold state.

[0025] With this configuration, when the operating condition of the engine in the warmed-up state is within the operating range where the engine load is relatively high and the engine speed is relatively low, in which knocking is likely to occur, the fuel is injected at the second injection timing to form the rich region near the spark plug at the ignition timing to increase the flame propagation speed and improve the knock resistance. On the other hand, when the operating condition of the engine is outside the operating range where the engine load is relatively high and the engine speed is relatively low, or in the cold state in which knocking is not likely to occur, the fuel can be injected in a single injection at the first injection timing to prevent evaporation.To stimulate fuel atomization and distribute the fuel evenly within the combustion chamber, emission performance can be improved.

[0026] According to another aspect of the invention, there is provided an engine comprising: a cylinder defining a combustion chamber; a fuel injector for directly injecting fuel into the combustion chamber; a fuel control system, in particular according to the above aspect of the invention or a particular embodiment thereof, which controls a behavior of fuel injected directly into the combustion chamber using a tumble flow, and comprises: a tumble flow generator for generating the tumble flow within the combustion chamber; and a fuel injector control module for initiatingCausing the fuel injector to inject the fuel at a first injection timing and then inject a smaller amount of fuel than an amount injected at the first injection timing in a direction substantially opposite to a positive direction of the tumble flow at a second injection timing, wherein the first injection timing is selected to be in an intake stroke of the cylinder, wherein the second injection timing is selected to be in a later half of a compression stroke of the cylinder.

[0027] According to a particular embodiment, the second injection timing is determined or selected to be between about 50° and about 90° before a top dead center of the compression stroke, and / or wherein the fuel injector control module causes the fuel injector to inject about 10% to about 20% of a total fuel injection quantity in an actuation cycle of the cylinder at the second injection timing.

[0028] In particular, the tumble flow generator comprises an intake port of the engine, a spark plug of the engine being provided in a central portion of a ceiling of the combustion chamber, the fuel injector being arranged at a position of a peripheral edge portion of the ceiling of the combustion chamber on a side where the intake port is provided, and injecting the fuel substantially obliquely downward and toward an opposite side from the intake port, the engine having a piston having a crown surface, and the crown surface being formed with an inclined surface extending obliquely upward from an end portion of the crown surface on the side facing away from the fuel injector toward a center of the crown surface, and the second injection timing being determined to be a timingwherein a positive direction of a lower portion of the tumble flow is oriented substantially obliquely upward toward the fuel injector along the inclined surface of the crown surface, and the fuel is injected substantially opposite to the positive direction of the lower portion of the tumble flow.

[0029] According to another aspect of the invention, there is provided a fuel control method for an engine, in particular according to the above aspect of the invention or a particular embodiment thereof, for controlling by using a tumble flow behavior of fuel injected directly by a fuel injector into a combustion chamber formed inside a cylinder of the engine, the method comprising: generatingGenerating the tumble flow within the combustion chamber; and causing the fuel injector to inject the fuel at a first injection timing and then inject a smaller amount of fuel than an amount injected at the first injection timing in a direction substantially opposite to a positive direction of the tumble flow at a second injection timing, wherein the first injection timing is determined to be in an intake stroke of the cylinder, wherein the second injection timing is determined to be in a later half of a compression stroke.compression stroke of the cylinder, wherein the fuel injection device is arranged at a position of a peripheral edge portion of the ceiling of the combustion chamber on a side where the intake port is provided, and injects the fuel substantially obliquely downward and toward an opposite side from the intake port. wherein the engine comprises a piston having a crown surface, and the crown surface is formed with an inclined surface extending obliquely upward from an end portion of the crown surface on the side facing away from the fuel injection device toward a center of the crown surface, and wherein the second injection timing is determined to be a timing at which a positive direction of a lower portion of the tumble flow is oriented substantially obliquely upward toward the fuel injector along the inclined surface and the fuel is injected substantially opposite to the positive direction of the lower portion of the tumble flow.

[0030] According to another aspect of the invention, a computer program product is provided, which is in particular embodied as a computer-readable medium, as a signal and / or data stream, comprising computer-readable instructions which, when loaded onto and executed on a suitable system, carry out the steps of a fuel control method according to the above aspect of the invention or a particular embodiment thereof.

[0031] These and other objects, features, and advantages of the present invention will become more apparent upon reading the following detailed description of preferred embodiments and the accompanying drawings. It should be understood that, even though embodiments are described separately, individual features thereof may be combined to form additional embodiments. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a view schematically illustrating a configuration of an engine to which a fuel control system according to an embodiment of the present invention is applied. Fig. 2 is a perspective view illustrating specific structures of an injector and a spark plug of the engine according to the embodiment of the present invention. Fig. 3A and Fig. 3B are views illustrating a piston of the engine according to the embodiment of the present invention, in which Fig. 3A a Top view of the piston and Fig. 3B is a view taken along a line AA in Fig. 3A is. Fig. 4 is a diagram illustrating operating regions of the engine according to the embodiment of the present invention. Fig. 5 illustrates timing charts of fuel injection timing controlled by the fuel control system of the engine according to the embodiment of the present invention. Fig. 6 is a cross-sectional view illustrating a state inside a combustion chamber when the fuel is injected in an intake stroke by the fuel control system according to the embodiment of the present invention. Fig. 7 is a cross-sectional view illustrating a state inside the combustion chamber when the fuel is injected around a bottom dead center by the fuel control system according to the embodiment of the present invention. Fig. 8 is a cross-sectional view illustrating a state inside the combustion chamber when the fuel is injected in a later half of a compression stroke by the fuel control system according to the embodiment of the present invention. Fig. 9 is a cross-sectional view illustrating a state inside the combustion chamber at an ignition timing controlled by the fuel control system according to the embodiment of the present invention. DETAILED DESCRIPTION OF AN EMBODIMENT

[0032] Hereinafter, a fuel control system of an engine according to an embodiment of the present invention will be described with reference to the accompanying drawings. [System configuration]

[0033] First, a configuration of an engine to which a fuel control system according to an embodiment of the present invention is applied will be described with reference to Fig. 1 described. Fig. 1 is a view schematically illustrating the configuration of the engine to which the fuel control system according to the embodiment of the present invention is applied.

[0034] In Fig. 1, reference numeral "1" denotes the engine to which the fuel control system according to this embodiment of the present invention is applied. The engine 1 is, in particular, a gasoline engine mounted on a vehicle and supplied with fuel containing at least gasoline. The engine 1 includes a cylinder block 4 provided with a plurality of cylinders 2 (it should be noted that, although only one cylinder 2 is used in Fig. 1, for example, four cylinders are arranged linearly), a cylinder head 6 which is arranged on the cylinder block 4, and an oil or lubricant pan 8 which is arranged below the cylinder block 4 and stores or receives a lubricant. A reciprocating piston 14, which is coupled to a crankshaft 12 via a connecting rod 10, is fitted into each of the cylinders 2. The cylinder head 6, the cylinders 2 and the pistons 14 define combustion chambers 16. In particular, two independent intake openings or ports 18 and two independent exhaust openings or ports 20 are formed in the cylinder head 6 for each of the cylinders 2, each of the intake and exhaust ports being...Inlet port(s) 18 are provided with an inlet valve 22 for opening and closing the inlet port 18 on the side of the combustion chamber 16, and each of the outlet port(s) 20 is provided with an outlet valve 24 for opening and closing the outlet port 20 on the side of the combustion chamber 16. In particular, the inlet port 18 functions as a tumble flow generator for substantially generating a swirling flow in the upward and downward directions of the piston (tumble flow) within the combustion chamber 16.

[0035] In addition, a bottom surface of the cylinder head 6 forms ceilings 26 of the respective combustion chambers 16. Each of the ceilings 26 has, in particular, a so-called pent roof shape or form, which has two opposite inclined surfaces which extend from a center of the ceiling 26 to a bottom end of the cylinder head 6.

[0036] Furthermore, an injector 28 for injecting fuel (in particular directly) into the cylinder 2 is mounted on the cylinder head 6 for each cylinder 2. Each injector 28 is arranged such that its plurality of nozzle holes 30 are oriented obliquely downward and toward an interior of the combustion chamber 16, at a position of a peripheral edge portion of the ceiling 26 of the combustion chamber 16, between the two intake ports 18. The injector 28 injects (in particular directly) into the combustion chamber 16 an amount of fuel corresponding to an operating state of the engine 1 at an injection timing determined according to the operating state of the engine 1. A specific configuration of the injector 28 will be described later.

[0037] Furthermore, at least one spark plug 32 for forcibly igniting mixed gas inside the combustion chamber 16 is mounted on the cylinder head 6 for each cylinder 2. Each spark plug 32 is arranged penetrating the cylinder head 6 to extend substantially downward from a central portion of the ceiling 26 of the combustion chamber 16. The spark plug 32 is connected to an ignition circuit 34 for supplying voltage to the spark plug 32.

[0038] The cylinder head 6 is further provided with valve drive mechanisms 36 for driving the intake and exhaust valves 22 and 24 of each cylinder 2, respectively. Specifically, the valve drive mechanisms 36 include, for example, a variable valve lift (VVL) mechanism (not illustrated) for changing lifts of the intake and exhaust valves 22 and 24, and / or a variable valve timing (VVT) mechanism (not illustrated) for changing a rotational phase of a camshaft relative to the crankshaft 12.

[0039] A fuel supply path couples a fuel tank (not illustrated) to the injectors 28. A fuel supply system 38 for supplying fuel to each of the injectors 28 at a desired fuel pressure is provided within the fuel supply path. The pressure of the fuel supplied to each injector 28 is varied, particularly according to the operating state of the engine 1.

[0040] On a side surface of the engine 1, as shown in Fig. 1, an intake passage 40 is connected to communicate with the intake ports 18 of the respective cylinders 2. On the other side surface of the engine 1, an exhaust passage 42 is connected to discharge burned gas (exhaust gas) discharged from the combustion chambers 16 of the respective cylinders 2.

[0041] The engine 1 is controlled by a powertrain control module (hereinafter referred to as the PCM) 44. The PCM 44 consists of a microprocessor that includes a CPU, a memory, a counter / timer group, an interface, and / or one or more paths for connecting these units. The PCM 44 represents a controller.

[0042] The PCM 44 receives one or more detection signals from one or more (particularly different) types of sensors. Specifically, the PCM 44 receives one or more detection signals from one or more of the following: a fluid temperature sensor for detecting a temperature of an engine coolant, a crankshaft angle sensor for detecting a rotation angle of the crankshaft 12, an accelerator position sensor for detecting an accelerator opening degree corresponding to an angle (depression amount) of an accelerator pedal of the vehicle, etc. It should be noted that these sensors are not illustrated.

[0043] By performing various types of operations based on this detection signal(s), the PCM 44 determines the operating state of the engine 1 and, further, the vehicle and outputs control signals to one or more of the following: the injectors 28, the ignition circuit 34, the valve drive mechanisms 36, the fuel supply system 38, etc., according to the determined state. In this way, the PCM 44 operates the engine 1. Although this will be described in detail later, the PCM 44 may be referred to as the fuel control system of the engine 1 and functions as a fuel injector control module. [Specific structures of pistons, injectors and spark plugs]

[0044] Next, specific structures of each piston 14, each injector 28 and each spark plug 32 of the engine 1 of this embodiment will be described with reference to Fig. 2, Fig. 3A and Fig. 3B described. Fig. 2 is a perspective view illustrating the specific structures of the injector 28 and the spark plug 32 of the engine 1 according to the embodiment of the present invention. Fig. 3A and Fig. 3B are views illustrating the piston 14 of the engine 1 according to the embodiment of the present invention, in which Fig. 3A is a plan view of the piston 14 and Fig. 3B is a view taken along a line AA in Fig. 3A is.

[0045] As this is Fig. 2, the injector 28 is, in particular, a multi-hole injector having the plurality of nozzle holes 30. The injector 28 is, in particular, substantially provided such that its axial direction inclines downward by an inclined angle α from a horizontal direction. Thus, a fuel spray injected from each nozzle hole 30 of the injector 28 spreads radially obliquely downward from the peripheral edge portion of the ceiling 26 of the combustion chamber 16.

[0046] As this is Fig. 2, Fig. 3A and Fig. 3B, a crown surface 46 constituting an upper portion of the piston 14 is formed to bulge toward its center. Specifically, the crown surface 46 includes an injector-side inclined surface 48 extending substantially obliquely upward along an extended direction from an end portion of the crown surface 46 on the injector 28 side toward the center of the crown surface 46, and an injector-remote-side inclined surface 50 extending substantially obliquely upward along an extended direction from an end portion of the crown surface 46 on a substantially opposite side from the injector 28 side (hereinafter may be referred to as the "injector-remote side") toward the center of the crown surface 46.The inclined surface 48 on the side of the injector and the inclined surface 50 on the side facing away from the injector are formed along the shape of the ceiling 26 of the combustion chamber 16.

[0047] Specifically, an inclined angle θ of the inclined surface 50 on the injector-remote side is formed such that the axial direction of the injector 28 (i.e., an injection direction of the fuel by the injector 28) is substantially parallel to a direction in which the inclined surface 50 on the injector-remote side extends obliquely upward from the end portion of the crown surface 46 on the injector-remote side toward the center (i.e., a direction extending obliquely upward and toward the injector 28). Specifically, the inclined angle α of the injector 28 is substantially the same as the inclined angle θ of the inclined surface 50 on the injector-remote side.

[0048] The end portion of the crown surface 46 on the side of the injection device 28 and the end portion on the side facing away from the injection device are in particular each formed with horizontal surfaces 52 as a reference surface of the crown surface 46.

[0049] Intake valve recesses 54 are formed in the horizontal surface 52 on the side of the injector 28 to avoid contact between the piston 14 and the intake valves 22, and / or exhaust valve recesses 56 are formed in the inclined surface 50 on the side facing away from the injector to avoid contact between the pistons 14 and the exhaust valves 24.

[0050] A cavity 58 (which is particularly substantially circularly recessed in a plan view) is formed substantially at the center of the crown surface 46. The cavity 58 is specifically formed by a horizontal bottom surface 60 having a substantially circular shape in a plan view and a side surface 62 that slopes radially upward from an outer periphery of the bottom surface 60. When the piston 14 is at top dead center (TDC), a tip of the spark plug 32 is disposed within the cavity 58, and thus, a substantially spherical combustion chamber centered around the tip of the spark plug 32 is formed. [Fuel injection timing control]

[0051] Next, control of the fuel injection timing by the fuel control system of the engine 1 of this embodiment will be described with reference to Fig. 4 to 9 described. Fig. 4 is a diagram illustrating operating ranges of the engine 1 according to the embodiment of the present invention, in which the horizontal axis indicates an engine speed and the vertical axis indicates an engine load. Fig. 5 illustrates time charts of fuel injection timings controlled by the fuel control system of the engine 1 according to the embodiment of the present invention, in which the horizontal axis indicates a crank angle before a compression stroke top dead center CTDC (deg BTDC), and the numbers on the bars indicating the fuel injection timings indicate fuel injection amounts at the respective fuel injection timings when the total fuel injection amount in one cycle (operation cycle of the cylinder) is 10. Fig. 6 is a cross-sectional view illustrating a state inside the combustion chamber 16 when the fuel is injected in an intake stroke by the fuel control system according to the embodiment of the present invention. Fig. 7 is a cross-sectional view illustrating a state inside the combustion chamber 16 when the fuel is injected around a bottom dead center by the fuel control system according to the embodiment of the present invention. Fig. 8 is a cross-sectional view illustrating a state inside the combustion chamber 16 when the fuel is injected in a later portion (particularly, half) of a compression stroke by the fuel control system according to the embodiment of the present invention. Fig. 9 is a cross-sectional view illustrating a state inside the combustion chamber 16 at an ignition timing controlled by the fuel control system according to the embodiment of the present invention.

[0052] First, as in Fig. 4, within an operating range where the engine load is relatively high and the engine speed is relatively low in a warmed-up state of the engine (a first range in Fig. 4), (specifically, based on the detection signal(s) obtained from the fluid temperature sensor, the crank angle sensor, the accelerator position sensor, etc.), the PCM 44 performs the fuel injection in each cycle by dividing the injection into, specifically, three injections to suppress knocking and improve output torque.

[0053] Within an operating range where the engine load is lower and the engine speed is higher than in the first range in the warmed-up state of the engine (in the warmed-up state of the engine, an operating range where the engine load is relatively in the middle and the engine speed is relatively low, and an operating range where the engine load is relatively high and the engine speed is relatively in the middle, ie a second range in Fig. 4), the PCM 44 performs the fuel injection in each cycle by dividing the injection into two injections in particular in order to suppress knocking and improve the output torque.

[0054] Within an operating range where the engine load is lower and the engine speed is higher than in the second range in the warmed-up state of the engine (in the warmed-up state of the engine, an operating range where the engine load is relatively low and an operating range where the engine load is relatively high and the engine speed is relatively high, ie a third range in Fig. 4), the PCM 44 injects all of the fuel, specifically, in a single injection in each cycle. Furthermore, the PCM 44 injects all of the fuel, specifically, in a single injection in each cycle even in a cold engine state. Thus, the PCM 44 switches the number of fuel injections in a cycle according to the operating state of the engine 1. It should be noted that the limits for switching the number of fuel injections are not limited to the illustrated example.

[0055] Specifically, as in Fig. 5, when the operating state of the engine 1 is within the first range of Fig. 4, the PCM 44, that the injector 28 injects the fuel by dividing the injection into three injections to a Timing on the intake stroke of the cylinder 2, specifically an intake stroke injection timing which is set or selected to be about 270 [deg BTDC] (first injection timing), a bottom dead center injection timing which is set or selected to be around the bottom dead center (180 [deg BTDC]), and a timing in the latter half of the compression stroke of the cylinder 2, specifically an injection timing in the latter half of the compression stroke which is set or selected to be between about 50 and about 90 [deg BTDC] (second injection timing). When a total fuel injection amount in one cycle is 10, a ratio of the fuel injection amounts to the respective injection timings is 5:4:1 (injection timing in the intake stroke : injection timing at bottom dead center : injection timing in a later half of the compression stroke).The PCM 44 causes the injector 28 to inject approximately 10% of the total fuel injection amount at the injection timing in the latter half of the compression stroke. Note that the total fuel injection amount in one cycle is specifically determined or selected so that the overall mixture gas becomes leaner than a theoretical air-fuel ratio.

[0056] If the operating state of engine 1 is within the second range of Fig. 4, the PCM 44 causes the injector 28 to inject the fuel by dividing the injection into two injections at a timing on the intake stroke of the 2nd cylinder, specifically the injection timing in the intake stroke, and a timing in the later half of the compression stroke of the 2nd cylinder, specifically the injection timing in the later half of the compression stroke. Specifically, when the total fuel injection amount in one cycle is 10, a ratio of the fuel injection amounts to the respective injection timings is 9:1 (intake stroke injection timing: compression stroke injection timing). Thus, the PCM 44 causes the injector 28 to inject 10% of the total fuel injection amount at the injection timing in the later half of the compression stroke.

[0057] If the operating condition of engine 1 is within the third range of Fig. 4 or is in the cold state, the PCM 44 causes the injector 28 to inject all of the fuel in a single injection on the intake stroke of the cylinder 2, specifically at the injection timing in the intake stroke.

[0058] First, the injection timing in the intake stroke, as shown in Fig. 6, a tumble flow T (the swirling flow in the up-and-down direction of the piston) is generated by intake air flowing into the cylinder chamber 16 from the intake ports 18 as the intake valves 22 are opened and the piston 14 moves downward. When the PCM 44 controls the injector 28 and the fuel supply system 38 to inject the fuel from the injector 28 at the injection timing in the intake stroke, the fuel injected by the injector 28 substantially flows within the combustion chamber 16 along the tumble flow T. Specifically, at about 270 [deg BTDC] corresponding to the injection timing in the intake stroke, the downward speed of the piston 14 reaches its peak, and the gas flow within the combustion chamber 16 is most active. Therefore, atomization can be achieved.Evaporation of the fuel injected into the combustion chamber 16 can be stimulated or promoted. Furthermore, since a period of time from the intake-stroke injection timing to the ignition timing is long, sufficient time can be ensured to vaporize or atomize the fuel injected at the intake-stroke injection timing, and the fuel can be evenly distributed within the combustion chamber 16.

[0059] Next, the injection timing at bottom dead center, as shown in Fig. 7, the tumble flow T generated on the intake stroke expands in the up-and-down direction of the piston 14 as the piston 14 moves downward. When the PCM 44 controls the injector 28 and the fuel supply system 38 to inject fuel from the injector 28 at this time, fuel is injected toward an area near a top end of the tumble flow T. Near the top end of the tumble flow T, a positive direction of the tumble flow T is substantially a direction toward the exhaust ports 20 from the intake ports 18, that is, away from the injector 28. Therefore, fuel is injected by the injector 28 in substantially the same direction as the positive direction of flow near the top end of the tumble flow T.Thus, the tumble flow T is enhanced by the fuel injection. As a result, the turbulence of the mixed gas flow within the combustion chamber 16 can be maintained until the ignition timing, resulting in an improvement in the flame propagation speed and maintaining homogeneous combustion.

[0060] Then, at the injection timing in the later half of the compression stroke, as shown in Fig. 8, the tumble flow T generated on the intake stroke is compressed in the upward and downward directions as the piston 14 moves upward. A positive direction of a lower section of the tumble flow T is oriented substantially obliquely upward and toward the injector 28 along the inclined surface 50 on the injector-remote side of the crown surface 46. Specifically, between 50 and 90 [deg BTDC] corresponding to the injection timing in the latter half of the compression stroke, a lower end portion of the fuel spray is located.-spray, which is injected obliquely downwards to spread radially from the injector 28, in particular substantially in an extended line of the inclined surface 50 on the side of the crown surface 46 facing away from the injector, and the injection direction of the fuel by the injector 28 is substantially opposite to the direction in which the inclined surface 50 on the side of the crown surface 46 facing away from the injector extends obliquely upwards and towards the injector 28. Therefore, when the PCM 44 controls the injector 28 and the fuel supply system 38.controls to inject the fuel from the injector 28 at the injection timing in the later half of the compression stroke, the fuel is injected in the direction substantially opposite to the positive direction of the lower cross section of the tumble flow T, which is directed obliquely upward and toward the injector 28 along the inclined surface 50 on the injector-remote side of the crown surface 46. In this case, a kinetic energy of the fuel injected by the injector 28 is canceled or greatly reduced by a kinetic energy of the tumble flow T, which is substantially opposite to the fuel injection direction, and thus the fuel does not penetrate the tumble flow T, and a region where the fuel is rich is formed.enriched, formed within the lower cross section of the tumble flow T (hatched area in . Fig. 8).

[0061] The rich area formed within the lower cross section of the tumble flow T by the fuel injection at the injection timing in the later half of the compression stroke shifts within the combustion chamber 16 along the tumble flow T. Then, at the ignition timing, as shown in Fig. As illustrated in Figure 9, the rich region is formed near the tip of the spark plug 32. Thus, ignitability by the spark plug 32 improves, and as the flame propagation speed increases, knock resistance improves.

[0062] As described above, when the operating state of the engine 1 is in the warmed-up state within the first range of Fig. 4, the PCM 44 divides the fuel injection timing into three timings, which are the injection timing in the intake stroke, the injection timing at the bottom dead center, and the injection timing in the later half of the compression stroke, and causes the injector 28 to inject the fuel so that the ratio of the fuel injection amounts to the respective injection timings becomes 5:4:1 (intake stroke injection timing : bottom dead center injection timing : compression stroke injection timing).

[0063] Specifically, when the operating state of the engine 1 is in the warmed-up state within the first range where knocking is likely to occur, by injecting the large amount of fuel at the intake stroke injection timing and the bottom dead center injection timing, the evaporation of the fuel is stimulated to cool the mixed gas with the latent heat of evaporation, by injecting the fuel at the bottom dead center injection timing, the tumble flow T is enhanced to maintain the turbulence of the mixed gas flow, and / or by injecting the fuel at the later half of the compression stroke injection timing to form the rich region near the spark plug 32 at the ignition timing, the flame propagation speed is increased and thus the knock resistance is improved.In addition, by injecting the fuel at the timing in the intake stroke and at the timing at bottom dead center to substantially evenly distribute the fuel within the combustion chamber 16, emission performance is also improved.

[0064] When the operating state of the engine 1 in the warmed-up state is within the second range of Fig. 4, the PCM 44 divides the fuel injection timing into the two timings of the injection timing in the intake stroke and the injection timing in the later half of the compression stroke, and causes the injector 28 to inject the fuel such that the ratio of the fuel injection amounts to the respective injection timings becomes 9:1 (intake stroke injection timing : compression stroke injection timing).

[0065] Specifically, when the operating state of the engine 1 is in the warmed-up state within the second region where knocking occurs less easily compared to the first region but more easily compared to the third region, or when the engine 1 is in the cold state, by injecting the large amount of fuel at the injection timing in the intake stroke, the vaporization of the fuel is stimulated to cool the mixed gas with the latent heat of vaporization, and by injecting the fuel at the injection timing in the later half of the compression stroke to form the rich region near the spark plug 32 at the ignition timing, the flame propagation speed is increased and thus the knock resistance is improved.In addition, by injecting the large amount of fuel at the injection timing in the intake stroke, the fuel is evenly distributed within the combustion chamber 16 and the emission performance is improved.

[0066] When the operating state of the engine 1 in the warmed-up state is within the third range of Fig. 4 or when the engine 1 is in the cold state, the PCM 44 causes the injector 28 to inject all of the fuel in a single injection at the injection timing in the intake stroke.

[0067] When the operating state of the engine 1 is in the warmed-up state within the third range or the engine 1 is in the cold state where knocking does not easily occur, by injecting all of the fuel in a single injection at the injection timing in the intake stroke to stimulate the evaporation of the fuel and distribute the fuel evenly within the combustion chamber 16, the emission performance is improved.

[0068] Next, modifications of this embodiment will be described.

[0069] In the embodiment described above, the two independent intake ports 18 and the two independent exhaust ports 20 are formed in the cylinder head 6 for each of the cylinders 2; however, the number of the intake and exhaust ports 18 and 20 may be different, respectively.

[0070] In the above-described embodiment, the PCM 44 determines the operating state of the engine 1 based on the one or more detection signals obtained from at least one of the fluid temperature sensor, the crankshaft angle sensor, the accelerator position sensor, etc.; however, the operating state of the engine 1 may be determined by using a detection signal(s) obtained from other sensor(s) (e.g., a detection signal obtained from a catalyst temperature sensor for detecting a temperature of a catalyst for purifying exhaust gas).

[0071] In the above-described embodiment, the total fuel injection amount in one cycle is determined so that the mixture gas as a whole becomes lean, which is thinner than the theoretical air-fuel ratio; however, it may be selected so that the ratio of the mixture gas as a whole becomes substantially the same as the theoretical air-fuel ratio.

[0072] In the embodiment described above, when the operating state of the engine 1 is within one of the first and second ranges of Fig.4, the PCM 44 causes the injector 28 to inject about 10% of the total fuel injection amount at the injection timing in the later half of the compression stroke; however, the PCM 44 may cause the injector 28 to inject about 10% to about 20% of the total fuel injection amount at the injection timing in the later half of the compression stroke. Thus, the mixed gas near the tip of the spark plug 32 at the ignition timing can be appropriately enriched, and the flame propagation speed can be surely increased, and moreover, the mixed gas within a region away from the spark plug 32 (i.e., end gas) can be prevented from becoming excessively lean, and unstable combustion can be prevented from occurring.

[0073] Next, operations and effects of the fuel control system of the engine 1 of the embodiment and the modifications thereof described above will be described.

[0074] First, the PCM 44 causes the injector 28 to inject fuel at the injection timing in the intake stroke, and to inject a smaller amount of fuel than the fuel injection amount at the injection timing in the intake stroke, at the injection timing in the later half of the compression stroke, in the direction substantially opposite to the positive direction of the tumble flow T within the combustion chamber 16. Therefore, in the fuel injection at the injection timing in the later half of the compression stroke, by canceling or greatly reducing the kinetic energy of the fuel injected by the injector 28 with the kinetic energy of the tumble flow T directed substantially opposite to the fuel injection direction, the rich region can be formed within the tumble flow T without the fuel penetrating the tumble flow T.Furthermore, by shifting the rich region along the tumble flow T to be located near (or closer to) the tip of the spark plug 32 at the ignition timing, the ignitability by the spark plug 32 can be improved, and since the flame propagation speed increases, knock resistance can be improved. Moreover, especially by injecting a large amount of fuel at the injection timing in the intake stroke, evaporation of the fuel is stimulated to cool the mixed gas with the latent heat of evaporation, and knock resistance can be further improved. Therefore, even within the operating range where abnormal combustion such as knocking is likely to occur, knocking can be securely suppressed, and accordingly, the ignition timing can be advanced to increase torque.Furthermore, by injecting the large amount of fuel at the injection timing of the intake stroke, the fuel can be evenly distributed within the combustion chamber 16 to achieve homogeneous combustion, and thus the emission performance can also be improved.

[0075] Specifically, since the PCM 44 particularly causes the injector 28 to inject the fuel at the injection timing in the later half of the compression stroke, which is set to be between 50 and 90 [deg BTDC], the fuel can be surely injected at the timing at which the injection direction of the fuel is opposite to the tumble flow T, and thus the fuel-rich region can be formed within the tumble flow T, and the rich region can be substantially shifted along the tumble flow T to be surely located near the tip of the spark plug 32 at the ignition timing, and the flame propagation speed can be surely increased.

[0076] Moreover, since the PCM 44 specifically causes the injector 28 to inject about 10% to about 20% of the total fuel injection amount at the injection timing in the later half of the compression stroke, when the rich region formed within the tumble flow T is shifted near the tip of the spark plug 32 at the ignition timing, the mixed gas near the tip of the spark plug 32 can be appropriately enriched and the flame propagation speed can be surely increased, and furthermore, the mixed gas within the region away from the spark plug 32 can be prevented from becoming excessively lean, and unstable combustion can be prevented from occurring.

[0077] Moreover, since the PCM 44 specifically causes the injector 28 to inject the fuel at the injection timing in the later half of the compression stroke selected to be in the period in which the injection direction of the fuel by the injector 28 is substantially opposite to the direction in which the inclined surface 50 on the injector-remote side of the crown surface 46 extends substantially obliquely upward and toward the injector 28, the fuel can be injected in the direction opposite to the positive direction of the lower cross section of the tumble flow T, which is obliquely upward and toward the injector 28 along the inclined surface 50 on the injector-remote side of the crown surface 46.Thus, the fuel-rich region can be formed within the tumble flow T, the rich region can be shifted along the tumble flow T to be surely located near (or closer to) the tip of the spark plug 32 at the ignition timing, and the flame propagation speed can be surely increased.

[0078] Specifically, since the fuel injection direction by the injector 28 is substantially parallel to the direction in which the inclined surface 50 on the injector-remote side of the crown surface 46 extends obliquely upward and toward the injector 28, the fuel injection direction can be securely opposed to the positive direction of the tumble flow T, which is obliquely upward and toward the injector 28 along the inclined surface 50 on the injector-remote side of the crown surface 46. Thus, the fuel-rich region can be formed within the tumble flow T, the rich region can be shifted along the tumble flow T to be more securely located near the tip of the spark plug 32 at the ignition timing, and the flame propagation speed can be securely increased.

[0079] Moreover, when the operating state of the engine 1 in the warmed-up state is within one of the first and second ranges, the PCM 44 causes the injector 28 to inject the fuel at the injection timing in the later half of the compression stroke, and when the operating state of the engine 1 in the warmed-up state is outside the first and second ranges (i.e., within the third range) or the engine 1 is in a cold state, the PCM 44 does not cause the injector 28 to inject the fuel at the injection timing in the later half of the compression stroke.Therefore, when the operating state of the engine 1 is in the warmed-up state within one of the first and second ranges where knocking is likely to occur, the fuel is injected at the injection timing in the later half of the compression stroke to form the rich region near the spark plug 32 at the ignition timing to increase the flame propagation speed and improve knock resistance. On the other hand, when the operating state of the engine 1 is one within the third range and in the cold state where knocking is not likely to occur, by injecting all of the fuel in a single injection at the injection timing in the intake stroke to stimulate fuel vaporization and evenly distribute the fuel within the combustion chamber 16, the emission performance can be improved.

[0080] Accordingly, a fuel control system of an engine is described, which controls, by utilizing a tumble flow, a behavior of fuel injected directly into a combustion chamber formed inside a cylinder of the engine. The fuel control system includes a fuel injector for directly injecting the fuel into the combustion chamber, a tumble flow generator for generating the tumble flow within the combustion chamber, and a fuel injector control unit.-Control module for causing the fuel injector to inject the fuel at a first injection timing and then inject a smaller amount of fuel than an amount injected at the first injection timing in a direction opposite to a positive direction of the tumble flow at a second injection timing, wherein the first injection timing is determined to be in an intake stroke of the cylinder, wherein the second injection timing is determined to be in a later half of the compression stroke of the cylinder.

[0081] It should be understood that the embodiments herein are illustrative and not restrictive, since the scope of the invention is defined by the appended claims rather than by the description preceding them, and that all changes which come within the limits and limitations of the claims, or an equivalence of such limits and limitations thereof, are intended to be embraced by the claims. LIST OF REFERENCE SYMBOLS 1 engine 2 cylinders 14 pistons 16 Combustion chamber 18 Inlet opening or port (as a special tumble flow generator) 20 Outlet opening or port 26 Ceiling 28 Injection device 30 nozzle hole 32 Spark plug 44 Powertrain control module (PCM) 46 crown area 50 inclined surface on the side facing away from the injection device T tumbling current

Claims

[1] A fuel control system (44) for an engine (1), wherein the fuel control system (44) uses a tumble flow (T) to control a behavior of fuel injected directly by a fuel injector (28) into a combustion chamber (16) formed inside a cylinder (2) of the engine (1), the fuel control system (44) comprising: a tumble flow generator (18) for generating the tumble flow (T) within the combustion chamber (16); and a fuel injector control module for causing the fuel injector (28) to inject the fuel at a first injection timing and then to inject a smaller amount of fuel than an amount injected at the first injection timing in a direction substantially opposite to a positive or forced direction of the tumble flow (T) at a second injection timing, wherein the first injection timing is determined or selected to be in an intake stroke of the cylinder (2), wherein the second injection timing is determined or selected to be in a later half of a compression stroke of the cylinder (2), wherein the fuel injection device (28) is arranged at a position of a peripheral edge portion of the ceiling of the combustion chamber (2) on a side where an inlet opening (18) is provided, and injects the fuel substantially obliquely downward and toward an opposite side from the inlet opening (18), wherein the engine comprises a piston (14) having a crown surface (46), and the crown surface (46) is formed with an inclined surface (50) which extends obliquely upwards from an end portion of the crown surface (46) on the side facing away from the fuel injection device (28) towards a center of the crown surface (46), and wherein the second injection timing is determined to be a timing at which a positive direction of a lower portion of the tumble flow (T) is oriented substantially obliquely upward toward the fuel injector (28) along the inclined surface (50) and the fuel is injected substantially opposite to the positive direction of the lower portion of the tumble flow (T). [2] The fuel control system of claim 1, wherein the second injection timing is determined to be between about 50° and about 90° before a top dead center of the compression stroke, and / or wherein the fuel injector control module causes the fuel injector (28) to inject about 10% to about 20% of a total fuel injection quantity in an actuation cycle of the cylinder (2) at the second injection timing. [3] A fuel control system according to any one of the preceding claims, wherein the tumble flow generator (18) comprises an intake port (18) of the engine (1), and wherein a spark plug (32) of the engine (2) is provided in a central portion of a ceiling of the combustion chamber (16). [4] A fuel control system according to any preceding claim, wherein the direction of injection of fuel by the fuel injector (28) is substantially parallel to the extending direction of the inclined surface (50) of the crown surface (46). [5] A fuel control system according to any one of the preceding claims, wherein the fuel injector control module causes the fuel injector (28) to inject the fuel at the second injection timing when an operating condition of the engine (1) in a warmed-up state is within an operating range of the engine (1) where an engine load is relatively high and an engine speed is relatively low, and the fuel injector control module does not cause the fuel injector (28) to inject the fuel at the second injection timing when the operating condition of the engine (1) in the warmed-up state is outside the operating range where the engine load is relatively high and the engine speed is relatively low or when the engine (1) is in a cold state. [6] Engine (1), comprising: a cylinder (2) defining a combustion chamber (16); a fuel injection device (28) for directly injecting the fuel into the combustion chamber (16); a fuel control system (44) which, using a tumble flow (T), controls a behavior of fuel injected directly into the combustion chamber (16), and comprises: a tumble flow generator (18) for generating the tumble flow (T) within the combustion chamber (16); and a fuel injector control module for causing the fuel injector (28) to inject the fuel at a first injection timing and then to inject a smaller amount of fuel than an amount injected at the first injection timing in a direction substantially opposite to a positive or forced direction of the tumble flow (T) at a second injection timing, wherein the first injection timing is determined or selected to be in an intake stroke of the cylinder (2), wherein the second injection timing is determined or selected to be in a later half of a compression stroke of the cylinder (2), wherein the fuel injection device (28) is arranged at a position of a peripheral edge portion of the ceiling of the combustion chamber (2) on a side where an inlet opening (18) is provided, and injects the fuel substantially obliquely downward and toward an opposite side from the inlet opening (18), wherein the engine comprises a piston (14) having a crown surface (46), and the crown surface (46) is formed with an inclined surface (50) which extends obliquely upwards from an end portion of the crown surface (46) on the side facing away from the fuel injection device (28) towards a center of the crown surface (46), and wherein the second injection timing is determined to be a timing at which a positive direction of a lower portion of the tumble flow (T) is oriented substantially obliquely upward toward the fuel injector (28) along the inclined surface (50) and the fuel is injected substantially opposite to the positive direction of the lower portion of the tumble flow (T). [7] The engine of claim 6, wherein the second injection timing is determined to be between about 50° and about 90° before a top dead center of the compression stroke, and / or wherein the fuel injector control module causes the fuel injector (28) to inject about 10% to about 20% of a total fuel injection quantity in an actuation cycle of the cylinder (2) at the second injection timing. [8] An engine according to claim 6 or 7, wherein the tumble generator (18) comprises an intake port (18) of the engine (1), and wherein a spark plug (32) of the engine (2) is provided in a central portion of a ceiling of the combustion chamber (16). [9] A fuel control method for an engine (1) for controlling by using a tumble flow (T) a behavior of fuel injected directly by a fuel injector (28) into a combustion chamber (16) formed inside a cylinder (2) of the engine (1), the method comprising: generating the tumble flow (T) within the combustion chamber (16); and causing the fuel injector (28) to inject the fuel at a first injection time and then inject a smaller amount of fuel than an amount injected at the first injection time in a direction substantially opposite to a positive or forced direction of the tumble flow (T) at a second injection time, wherein the first injection time is determined or selected to be in an intake stroke of the cylinder (2), wherein the second injection time is determined or selected to be in a later half of a compression stroke of the cylinder (2), wherein the fuel injection device (28) is arranged at a position of a peripheral edge portion of the ceiling of the combustion chamber (2) on a side where the inlet opening (18) is provided, and injects the fuel substantially obliquely downward and toward an opposite side from the inlet opening (18), wherein the engine comprises a piston (14) having a crown surface (46), and the crown surface (46) is formed with an inclined surface (50) which extends obliquely upwards from an end portion of the crown surface (46) on the side facing away from the fuel injection device (28) towards a center of the crown surface (46), and wherein the second injection timing is determined to be a timing at which a positive direction of a lower portion of the tumble flow (T) is oriented substantially obliquely upward toward the fuel injector (28) along the inclined surface (50) and the fuel is injected substantially opposite to the positive direction of the lower portion of the tumble flow (T). [10] A computer program product comprising computer readable instructions which, when loaded onto and executed on a suitable system, perform the steps of a fuel control or regulation method according to claim 9.

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