JPWO2011036794A1 - Control device for internal combustion engine - Google Patents

Abstract

The combustion field flame temperature is given as a target value, and the target heat quantity is also given to the combustion field, and the volume of the combustion field where the fuel injected from the injector burns as a physical quantity that defines the flame temperature and the input heat quantity. By adjusting any one of the temperature before the start of combustion in the combustion field, the density of the gas present in the combustion field, and the specific heat of the gas present in the combustion field, the amount of NOx generated can be reduced by optimizing the flame temperature.

Description

  The present invention relates to a control device for a compression ignition type internal combustion engine represented by a diesel engine. In particular, the present invention relates to measures for achieving both the achievement of a target input heat amount for an internal combustion engine and the reduction of the amount of NOx generated due to combustion in the combustion chamber.

  In an engine that performs lean combustion, such as a diesel engine, the operating region that burns a mixture with a high air-fuel ratio (lean atmosphere) occupies most of the entire operating region, so nitrogen oxide (hereinafter referred to as NOx) There is a concern that a relatively large amount will be discharged.

  Further, as disclosed in Patent Document 1 and Patent Document 2, it is generally known that the amount of NOx generated has a correlation with the combustion temperature in the cylinder (hereinafter sometimes referred to as flame temperature). ing. Therefore, in order to reduce the amount of NOx generated, it is effective to appropriately control the flame temperature in the cylinder.

  As a measure for reducing the amount of NOx generated, it is also known to provide an exhaust gas recirculation (EGR) device that recirculates part of the exhaust gas to the intake passage. In other words, the exhaust gas is recirculated toward the cylinder to reduce the oxygen concentration and oxygen density in the cylinder. As a result, the combustion temperature (flame temperature) during the combustion stroke is lowered to suppress the generation of NOx, thereby improving exhaust emission.

  On the other hand, in this type of engine, fuel injection amount control is performed in order to obtain an output according to a driver's request. In other words, the fuel injection amount required to obtain the required output determined according to the operating state and environmental conditions such as the engine speed, the accelerator operation amount, the coolant temperature, the intake air temperature, etc. is obtained from the fuel injection amount setting map and the like. . The fuel injection amount is injected from the injector at a predetermined fuel injection timing (for example, near the compression top dead center of the piston) to achieve the required output.

JP-A-2005-90368 JP-A-2005-180220

  By the way, in the driving situation where the required output is relatively high, the fuel injection amount is also set relatively large.

  On the other hand, the energy generated by the combustion of the fuel injected into the combustion chamber includes kinetic energy for pushing the piston down toward bottom dead center (energy that becomes engine output), thermal energy that raises the temperature in the combustion chamber, It is roughly divided into thermal energy that is radiated to the outside (for example, cooling water) through the cylinder head.

  In a situation where the required output is relatively high and the fuel injection amount is set to be relatively large, the thermal energy (energy for raising the temperature in the combustion chamber) increases as the kinetic energy is obtained high. It has become. That is, combustion is performed in a situation where the temperature tends to increase in the combustion chamber.

  As described above, the amount of NOx generated in the combustion chamber has a correlation with the combustion temperature (flame temperature), so that the amount of heat generated in the combustion chamber greatly increases due to the high required output. If the flame temperature is significantly higher than the NOx generation temperature (for example, 2200K), a situation will occur in which the amount of NOx generation increases. In other words, hitherto, there has been a trade-off between achieving a high output required for the engine (achieving a target input heat amount for the internal combustion engine) and reducing the amount of NOx generated due to combustion in the combustion chamber.

  The present invention has been made in view of the above points, and an object of the present invention is to achieve both the achievement of the target input heat amount for the internal combustion engine and the reduction of the generation amount of NOx accompanying the combustion in the combustion chamber. It is in.

-Principle of solving the problem-
The solution principle of the present invention devised in order to achieve the above object is to give the flame temperature of the combustion field as a target value and also give a target value to the amount of heat input to the combustion field, and to determine the physical quantity that influences the flame temperature. By adjusting, the reduction in the amount of NOx generated by optimizing the flame temperature and the achievement of the target input heat amount for the internal combustion engine can both be achieved.

-Solution-
Specifically, the present invention is premised on a control device for a compression self-ignition internal combustion engine that burns fuel injected from a fuel injection valve by self-ignition in a combustion chamber. With respect to the control device for the internal combustion engine, the combustion field target temperature for limiting the NOx generation amount during combustion in the combustion field where the fuel burns to a predetermined target NOx generation amount, and the output of the internal combustion engine reach a required output. For the combustion chamber, the volume of the combustion field where the fuel burns, the temperature of the combustion field before the start of combustion, the density of the gas present in the combustion field, and the gas present in the combustion field By adjusting at least one physical quantity of the specific heat of the combustion chamber, the physical quantity adjustment is performed so that the temperature of the combustion field is made not more than the target temperature of the combustion field and the target input heat quantity is obtained as the input heat quantity into the combustion chamber Have a part.

  By adjusting at least one of the physical quantities in accordance with this specific matter, the temperature of the combustion field is made equal to or lower than the target temperature of the combustion field, and the target input heat quantity is obtained as the input heat quantity into the combustion chamber. It will be. For this reason, the output required for the internal combustion engine can be obtained, and the NOx generation amount at the time of combustion in the combustion field can be limited to the predetermined target NOx generation amount, so that exhaust emission can be improved.

  As a preferable configuration of the physical quantity adjustment unit, the combustion period in the combustion chamber is divided into a plurality of minute periods, and the physical quantity is adjusted so that the combustion temperature of the combustion field in each of these minute periods is equal to or lower than the combustion field target temperature. The structure to do is mentioned.

  According to this, the physical quantity for limiting the NOx generation amount at the time of combustion in the combustion field to the predetermined target NOx generation amount can be defined with high accuracy for each of the minute periods. As a result, the NOx generation amount in the combustion field can be limited to a predetermined target NOx generation amount or less over substantially the entire combustion period.

  As a more preferable configuration of the physical quantity adjusting unit, the temperature at the time of combustion in the combustion field is set to the combustion field target temperature only for the period until the heat generation rate reaches a substantially peak value in the combustion period in the combustion chamber. The structure which adjusts a physical quantity so that it may become the following is mentioned.

  If the heat generation rate exceeds the peak value during the combustion period, then the combustion field temperature tends to gradually decrease, and the possibility that the amount of NOx generated will increase accordingly decreases. Considering this, the period for controlling the physical quantity so that the temperature at the time of combustion in the combustion field is equal to or lower than the combustion field target temperature is only the period until the heat generation rate reaches a substantially peak value. This makes it possible to limit the NOx generation amount to a predetermined target NOx generation amount or less over the entire combustion period while minimizing the physical quantity control period.

  More specific preferred configurations include the following configurations.

  First, the physical quantity adjusting unit expands the volume of the combustion field where the fuel burns, and corrects the increase in the amount of fuel injected from the fuel injection valve into the combustion chamber, and from the fuel injection valve into the combustion chamber. In this configuration, at least one of the increase corrections of the injection pressure of the injected fuel is executed.

  Further, when the physical quantity adjusting unit adjusts the physical quantity so as to adjust the volume of the combustion field in which the fuel burns, in order to avoid that the volume of the combustion field becomes less than a predetermined value, Designs have been made to reduce the diameter of the nozzle hole and increase the operating speed of the needle provided in the fuel injection valve. In this case, “to avoid the combustion field volume from being less than a predetermined value” means that the combustion field volume is less than the predetermined value due to the fuel injection pressure being set low, and the exhaust gas volume is not less than a predetermined amount in the exhaust gas. It means to avoid the occurrence of soot.

  In addition, the physical quantity adjusting unit is for reducing the temperature of the combustion field before the start of combustion, and for increasing the cooling efficiency of the intercooler provided in the intake system with respect to the one provided with the supercharging device, Control for lowering the supercharging pressure, control for increasing the cooling efficiency of the EGR cooler for those equipped with an exhaust gas recirculation device for recirculating part of the exhaust gas discharged to the exhaust system to the intake system, from the fuel injection valve to the combustion chamber In this configuration, at least one of the increase corrections of the injection pressure of the fuel to be injected is executed.

  Further, the physical quantity adjusting unit increases the density of the gas present in the combustion field, and controls the lowering of the supercharging pressure with respect to the one provided with the supercharging device, and opens the valve provided in the intake system. At least one of the controls to reduce the intake air amount by decreasing the degree is executed.

  Further, the physical quantity adjusting unit is for increasing the specific heat of the gas existing in the combustion field, and having an exhaust gas recirculation device for recirculating a part of the exhaust gas discharged to the exhaust system to the intake system. In this configuration, the control for increasing the EGR rate is executed.

  With these configurations, the physical quantity control operation by the physical quantity adjusting unit can be specifically obtained.

  In the present invention, the flame temperature of the combustion field is given as a target value, the target value is also given to the amount of heat input to the combustion field, and the physical quantity that affects the flame temperature is adjusted to optimize the flame temperature. Yes. For this reason, it is possible to achieve both the reduction of the NOx generation amount and the achievement of the target input heat amount for the internal combustion engine.

FIG. 1 is a diagram illustrating a schematic configuration of an engine and a control system thereof according to the embodiment. FIG. 2 is a cross-sectional view showing a combustion chamber of a diesel engine and its peripheral part. FIG. 3 is a block diagram showing a configuration of a control system such as an ECU. FIG. 4 is a schematic diagram of an intake / exhaust system and a combustion chamber for explaining the outline of the combustion mode in the combustion chamber. FIG. 5 is a cross-sectional view showing the combustion chamber and its surroundings during fuel injection. FIG. 6 is a plan view of the combustion chamber during fuel injection. FIG. 7 is an enlarged view showing the heat generation rate waveform and the minute period during the combustion period in the combustion chamber. FIG. 8 is a diagram showing a target combustion temperature setting map. FIG. 9 is a diagram illustrating an example of a fuel injection correction amount map in the first embodiment. FIG. 10 is a diagram showing an example of a fuel injection pressure correction map in the first embodiment. FIG. 11 is a diagram illustrating an example of an electromagnetic valve opening map in the third embodiment. FIG. 12 is a diagram illustrating an example of a nozzle vane opening degree map according to the third embodiment. FIG. 13 is a diagram illustrating an example of an injection pressure control map in the third embodiment. FIG. 14 is a diagram illustrating an example of an opening degree control map according to the fourth embodiment. FIG. 15 is a diagram illustrating an example of an opening degree control map in the fifth embodiment.

  Hereinafter, embodiments of the present invention will be described with reference to the drawings. In the present embodiment, a case where the present invention is applied to a common rail in-cylinder direct injection multi-cylinder (for example, in-line 4-cylinder) diesel engine (compression self-ignition internal combustion engine) mounted on an automobile will be described.

-Engine configuration-
First, a schematic configuration of a diesel engine (hereinafter simply referred to as an engine) according to the present embodiment will be described. FIG. 1 is a schematic configuration diagram of an engine 1 and its control system according to the present embodiment. Moreover, FIG. 2 is sectional drawing which shows the combustion chamber 3 of a diesel engine, and its peripheral part.

  As shown in FIG. 1, the engine 1 according to the present embodiment is configured as a diesel engine system having a fuel supply system 2, a combustion chamber 3, an intake system 6, an exhaust system 7 and the like as main parts.

  The fuel supply system 2 includes a supply pump 21, a common rail 22, an injector (fuel injection valve) 23, a shutoff valve 24, a fuel addition valve 26, an engine fuel passage 27, an addition fuel passage 28, and the like.

  The supply pump 21 pumps fuel from the fuel tank, makes the pumped fuel high pressure, and supplies it to the common rail 22 via the engine fuel passage 27. The common rail 22 has a function as a pressure accumulation chamber that holds (accumulates) the high-pressure fuel supplied from the supply pump 21 at a predetermined pressure, and distributes the accumulated fuel to the injectors 23. The injector 23 includes a piezoelectric element (piezo element) therein, and is configured by a piezo injector that is appropriately opened to supply fuel into the combustion chamber 3. Details of the fuel injection control from the injector 23 will be described later.

  The supply pump 21 supplies a part of the fuel pumped from the fuel tank to the fuel addition valve 26 via the addition fuel passage 28. The added fuel passage 28 is provided with the shutoff valve 24 for shutting off the added fuel passage 28 and stopping fuel addition in an emergency.

  The fuel addition valve 26 is configured so that the fuel addition amount to the exhaust system 7 becomes a target addition amount (addition amount that makes the exhaust A / F become the target A / F) by an addition control operation by the ECU 100 described later. In addition, it is constituted by an electronically controlled on-off valve whose valve opening timing is controlled so that the fuel addition timing becomes a predetermined timing. That is, a desired fuel is injected and supplied from the fuel addition valve 26 to the exhaust system 7 (from the exhaust port 71 to the exhaust manifold 72) at an appropriate timing.

  The intake system 6 includes an intake manifold 63 connected to an intake port 15a formed in the cylinder head 15 (see FIG. 2), and an intake pipe 64 that constitutes an intake passage is connected to the intake manifold 63. Further, an air cleaner 65, an air flow meter 43, and a throttle valve (intake throttle valve) 62 are arranged in this intake passage in order from the upstream side. The air flow meter 43 outputs an electrical signal corresponding to the amount of air flowing into the intake passage via the air cleaner 65.

  The intake system 6 is provided with a swirl control valve 66 for making the swirl flow (horizontal swirl flow) in the combustion chamber 3 variable (see FIG. 2). Specifically, as the intake port 15a, two systems, a normal port and a swirl port, are provided for each cylinder. Of these, a normal valve 15a shown in FIG. A swirl control valve 66 is disposed. An actuator (not shown) is connected to the swirl control valve 66, and the flow rate of air passing through the normal port 15a can be changed according to the opening of the swirl control valve 66 adjusted by driving the actuator. Yes. The larger the opening of the swirl control valve 66, the greater the amount of air taken into the cylinder from the normal port 15a. For this reason, the swirl generated by the swirl port (not shown in FIG. 2) becomes relatively weak, and the inside of the cylinder becomes low swirl. Conversely, the smaller the opening of the swirl control valve 66, the smaller the amount of air drawn into the cylinder from the normal port 15a. For this reason, the swirl generated by the swirl port is not weakened relatively, and the inside of the cylinder becomes a high swirl.

  The exhaust system 7 includes an exhaust manifold 72 connected to the exhaust port 71 formed in the cylinder head 15, and exhaust pipes 73 and 74 constituting an exhaust passage are connected to the exhaust manifold 72. In addition, a maniverter (exhaust gas purification device) 77 including a NOx storage catalyst (NSR catalyst: NOx Storage Reduction catalyst) 75 and a DPNR catalyst (Diesel Particle-NOx Reduction catalyst) 76 is disposed in the exhaust passage. Hereinafter, the NSR catalyst 75 and the DPNR catalyst 76 will be described.

The NSR catalyst 75 is an NOx storage reduction catalyst. For example, alumina (Al ₂ O ₃ ) is used as a support, and potassium (K), sodium (Na), lithium (Li), cesium (Cs), for example, is supported on this support. Alkali metal such as barium (Ba), alkaline earth such as calcium (Ca), rare earth such as lanthanum (La) and yttrium (Y), and noble metal such as platinum (Pt) were supported. It has a configuration.

The NSR catalyst 75 occludes NOx in a state where a large amount of oxygen is present in the exhaust gas, has a low oxygen concentration in the exhaust gas, and a large amount of reducing component (for example, an unburned component (HC) of the fuel). In the existing state, NOx is reduced to NO ₂ or NO and released. NO NOx released as NO ₂ or NO, the N ₂ is further reduced due to quickly reacting with HC or CO in the exhaust. Further, HC and CO are oxidized to H ₂ O and CO ₂ by reducing NO ₂ and NO. That is, by appropriately adjusting the oxygen concentration and HC component in the exhaust gas introduced into the NSR catalyst 75, HC, CO, and NOx in the exhaust gas can be purified. In the present embodiment, the oxygen concentration and HC component in the exhaust gas can be adjusted by the fuel addition operation from the fuel addition valve 26.

  On the other hand, the DPNR catalyst 76 is, for example, a porous ceramic structure carrying a NOx storage reduction catalyst, and PM in the exhaust gas is collected when passing through the porous wall. Further, when the air-fuel ratio of the exhaust gas is lean, NOx in the exhaust gas is stored in the NOx storage reduction catalyst, and when the air-fuel ratio becomes rich, the stored NOx is reduced and released. Further, the DPNR catalyst 76 carries a catalyst that oxidizes and burns the collected PM (for example, an oxidation catalyst mainly composed of a noble metal such as platinum).

  Here, the structure of the combustion chamber 3 of a diesel engine and its peripheral part is demonstrated using FIG. As shown in FIG. 2, a cylinder block 11 constituting a part of the engine body is formed with a cylindrical cylinder bore 12 for each cylinder (four cylinders), and a piston 13 is formed inside each cylinder bore 12. Is accommodated so as to be slidable in the vertical direction.

  The combustion chamber 3 is formed above the top surface 13 a of the piston 13. That is, the combustion chamber 3 is defined by the lower surface of the cylinder head 15 attached to the upper part of the cylinder block 11 via the gasket 14, the inner wall surface of the cylinder bore 12, and the top surface 13 a of the piston 13. A cavity (concave portion) 13 b is formed in a substantially central portion of the top surface 13 a of the piston 13, and this cavity 13 b also constitutes a part of the combustion chamber 3.

  As for the shape of the cavity 13b, the concave dimension is small in the central portion (on the cylinder center line P), and the concave dimension is increased toward the outer peripheral side. That is, as shown in FIG. 2, when the piston 13 is in the vicinity of the compression top dead center, the combustion chamber 3 formed by the cavity 13b is a narrow space having a relatively small volume at the center portion, and is directed toward the outer peripheral side. Thus, the space is gradually enlarged (expanded space).

  The piston 13 has a small end portion 18a of a connecting rod 18 connected by a piston pin 13c, and a large end portion of the connecting rod 18 is connected to a crankshaft which is an engine output shaft. As a result, the reciprocating movement of the piston 13 in the cylinder bore 12 is transmitted to the crankshaft via the connecting rod 18, and the engine output is obtained by rotating the crankshaft. Further, a glow plug 19 is disposed toward the combustion chamber 3. The glow plug 19 functions as a start-up assisting device that is heated red when an electric current is applied immediately before the engine 1 is started and a part of the fuel spray is blown onto the glow plug 19 to promote ignition and combustion.

  The cylinder head 15 is formed with the intake port 15a for introducing air into the combustion chamber 3 and the exhaust port 71 for exhausting exhaust gas from the combustion chamber 3, and intake air for opening and closing the intake port 15a. An exhaust valve 17 that opens and closes the valve 16 and the exhaust port 71 is provided. The intake valve 16 and the exhaust valve 17 are disposed to face each other with the cylinder center line P interposed therebetween. That is, the engine 1 is configured as a cross flow type. The cylinder head 15 is provided with the injector 23 that directly injects fuel into the combustion chamber 3. The injector 23 is disposed at a substantially upper center of the combustion chamber 3 in a standing posture along the cylinder center line P, and injects fuel introduced from the common rail 22 toward the combustion chamber 3 at a predetermined timing. It has become.

  Furthermore, as shown in FIG. 1, the engine 1 is provided with a supercharger (turbocharger) 5. The turbocharger 5 includes a turbine wheel 52 and a compressor wheel 53 that are connected via a turbine shaft 51. The compressor wheel 53 is disposed facing the intake pipe 64, and the turbine wheel 52 is disposed facing the exhaust pipe 73. For this reason, the turbocharger 5 performs a so-called supercharging operation in which the compressor wheel 53 is rotated using the exhaust flow (exhaust pressure) received by the turbine wheel 52 to increase the intake pressure. The turbocharger 5 in the present embodiment is a variable nozzle type turbocharger, and a variable nozzle vane mechanism (not shown) is provided on the turbine wheel 52 side. By adjusting the opening of the variable nozzle vane mechanism, the engine 1 supercharging pressure can be adjusted.

  An intake pipe 64 of the intake system 6 is provided with an intercooler 61 for forcibly cooling the intake air whose temperature has been raised by supercharging in the turbocharger 5.

  The throttle valve 62 provided further downstream than the intercooler 61 is an electronically controlled on-off valve whose opening degree can be adjusted steplessly. It has a function of narrowing down the area and adjusting (reducing) the supply amount of the intake air.

  Further, the engine 1 is provided with an exhaust gas recirculation passage (EGR passage) 8 that connects the intake system 6 and the exhaust system 7. The EGR passage 8 is configured to reduce the combustion temperature by recirculating a part of the exhaust gas to the intake system 6 and supplying it again to the combustion chamber 3, thereby reducing the amount of NOx generated. In addition, the EGR passage 8 is opened and closed steplessly by electronic control, and the exhaust gas passing through the EGR passage 8 (recirculating) is cooled by an EGR valve 81 that can freely adjust the exhaust flow rate flowing through the passage. An EGR cooler 82 is provided. The EGR passage 8, the EGR valve 81, the EGR cooler 82, and the like constitute an EGR device (exhaust gas recirculation device).

-Sensors-
Various sensors are attached to each part of the engine 1, and signals related to the environmental conditions of each part and the operating state of the engine 1 are output.

  For example, the air flow meter 43 outputs a detection signal corresponding to the flow rate of intake air (intake air amount) upstream of the throttle valve 62 in the intake system 6. The intake air temperature sensor 49 is disposed in the intake manifold 63 and outputs a detection signal corresponding to the temperature of the intake air. The intake pressure sensor 48 is disposed in the intake manifold 63 and outputs a detection signal corresponding to the intake air pressure. The A / F (air-fuel ratio) sensor 44 outputs a detection signal that continuously changes in accordance with the oxygen concentration in the exhaust gas downstream of the manipulator 77 of the exhaust system 7. Similarly, the exhaust temperature sensor 45 outputs a detection signal corresponding to the temperature of the exhaust gas (exhaust temperature) downstream of the manipulator 77 of the exhaust system 7. The rail pressure sensor 41 outputs a detection signal corresponding to the fuel pressure stored in the common rail 22. The throttle opening sensor 42 detects the opening of the throttle valve 62.

-ECU-
As shown in FIG. 3, the ECU 100 includes a CPU 101, a ROM 102, a RAM 103, a backup RAM 104, and the like. The ROM 102 stores various control programs, maps that are referred to when the various control programs are executed, and the like. The CPU 101 executes various arithmetic processes based on various control programs and maps stored in the ROM 102. The RAM 103 is a memory that temporarily stores calculation results in the CPU 101, data input from each sensor, and the like. The backup RAM 104 is a non-volatile memory that stores data to be saved when the engine 1 is stopped, for example.

  The CPU 101, the ROM 102, the RAM 103, and the backup RAM 104 are connected to each other via the bus 107, and are connected to the input interface 105 and the output interface 106.

  The input interface 105 is connected with the rail pressure sensor 41, the throttle opening sensor 42, the air flow meter 43, the A / F sensor 44, the exhaust temperature sensor 45, the intake pressure sensor 48, and the intake temperature sensor 49. Further, the input interface 105 includes a water temperature sensor 46 that outputs a detection signal corresponding to the cooling water temperature of the engine 1, an accelerator opening sensor 47 that outputs a detection signal corresponding to the depression amount of the accelerator pedal, and the engine 1. A crank position sensor 40 that outputs a detection signal (pulse) each time the output shaft (crankshaft) rotates by a certain angle is connected.

  On the other hand, the output interface 106 is connected to the supply pump 21, the injector 23, the fuel addition valve 26, the throttle valve 62, the swirl control valve 66, the EGR valve 81, and the like. In addition, the output interface 106 includes an electromagnetic valve provided in the cooling water flow path connected to the intercooler 61, an electromagnetic valve provided in the cooling water flow path connected to the EGR cooler 82, and a variable nozzle vane mechanism of the turbocharger 5. A provided nozzle vane (both not shown) is also connected.

  Then, the ECU 100 executes various controls of the engine 1 based on outputs from the various sensors described above, calculated values obtained by arithmetic expressions using the output values, or various maps stored in the ROM 102. .

  For example, the ECU 100 performs fuel injection control of the injector 23. In the present embodiment, as the fuel injection control of the injector 23, a case where only one main injection is executed will be described in order to simplify the description. That is, description will be made assuming that sub-injection such as pilot injection, pre-injection, after-injection, and post-injection that is executed in a conventional general diesel engine is not executed. Moreover, it demonstrates as what does not perform the division | segmentation main injection in which main injection is intermittently performed in multiple times. The present invention can also be applied to a diesel engine that performs these sub-injections and split main injection.

  The fuel injection amount in the main injection is basically necessary to obtain a required torque that is determined according to operating conditions such as engine speed, accelerator operation amount, cooling water temperature, intake air temperature, and environmental conditions. It is set as the fuel injection amount. For example, the higher the engine speed (the engine speed calculated based on the detection value of the crank position sensor 40), the larger the accelerator operation amount (the accelerator pedal depression amount detected by the accelerator opening sensor 47). The higher the required torque value of the engine 1, the higher the accelerator opening, and the larger the fuel injection amount is set accordingly. By setting the fuel injection amount in this way, the amount of heat input into the combustion chamber 3 is uniquely determined accordingly.

  In this embodiment, as will be described later, combustion temperature adjustment control for making the combustion temperature in the combustion chamber 3 equal to or lower than the target temperature is executed, and the fuel is actually injected from the injector 23. The fuel injection amount is corrected as the combustion temperature adjustment control is executed. Details of the fuel injection amount adjustment operation in the combustion temperature adjustment control will be described later (described in the first embodiment below).

  Further, the ECU 100 controls the opening degree of the EGR valve 81 according to the operating state of the engine 1 to adjust the exhaust gas recirculation amount (EGR amount) toward the intake manifold 63. The EGR amount is set according to an EGR map stored in advance in the ROM 102. Specifically, this EGR map is a map for determining the EGR amount (EGR rate) using the engine speed and the engine load as parameters. This EGR map is created in advance by experiments, simulations, or the like. That is, by applying the engine speed calculated based on the detection value of the crank position sensor 40 and the opening of the throttle valve 62 (corresponding to the engine load) detected by the throttle opening sensor 42 to the EGR map. An EGR amount (opening degree of the EGR valve 81) is obtained.

  In addition, the ECU 100 controls the opening degree of the EGR valve 81 and adjusts the EGR amount also by the combustion temperature adjustment control described later. Details of the adjustment operation of the EGR amount in this combustion temperature adjustment control will be described later (described in the fifth embodiment below).

  Further, the ECU 100 executes the opening degree control of the swirl control valve 66. In order to control the opening degree of the swirl control valve 66, the amount of movement of the fuel spray injected into the combustion chamber 3 per unit time (or per unit crank rotation angle) in the circumferential direction in the cylinder is changed. Is called. As will be described later, the opening degree of the swirl control valve 66 is also changed with the execution of the combustion temperature adjustment control. Details of the opening control of the swirl control valve 66 in this combustion temperature adjustment control will be described later (described in the fourth embodiment below).

-Fuel injection pressure-
The fuel injection pressure for executing the main injection is determined by the internal pressure of the common rail 22. As the common rail internal pressure, generally, the target value of the fuel pressure supplied from the common rail 22 to the injector 23, that is, the target rail pressure, increases as the engine load (engine load) increases and the engine speed (engine speed) increases. It will be expensive. That is, when the engine load is high, the amount of air sucked into the combustion chamber 3 is large. Therefore, a large amount of fuel must be injected from the injector 23 into the combustion chamber 3, and therefore the injection from the injector 23 is performed. The pressure needs to be high. Further, when the engine speed is high, the injection period is short, so the amount of fuel injected per unit time must be increased, and therefore the injection pressure from the injector 23 needs to be increased. . Thus, the target rail pressure is generally set based on the engine load and the engine speed. The target rail pressure is set according to a fuel pressure setting map stored in the ROM 102, for example. That is, by determining the fuel pressure according to this fuel pressure setting map, the valve opening period (injection rate waveform) of the injector 23 is controlled, and the fuel injection amount during the valve opening period can be defined.

  The optimum value of the fuel injection parameter in the main injection varies depending on the temperature conditions of the engine 1 and the intake air.

  For example, the ECU 100 adjusts the fuel discharge amount of the supply pump 21 so that the common rail pressure becomes equal to the target rail pressure set based on the engine operating state, that is, the fuel injection pressure matches the target injection pressure. To measure.

  Further, as will be described later, this fuel injection pressure is also changed to an appropriate value (for example, the fuel injection pressure is corrected to the high pressure side) with the execution of the combustion temperature adjustment control. Details of the adjustment operation of the fuel injection pressure in this combustion temperature adjustment control will be described later (described in the first and third embodiments below).

-Outline of combustion mode-
Next, the outline of the combustion mode in the combustion chamber 3 in the engine 1 according to the present embodiment will be described.

  In FIG. 4, gas is sucked into one cylinder of the engine 1 through the intake manifold 63 and the intake port 15 a, and combustion is performed by fuel injection from the injector 23 into the combustion chamber 3. FIG. 6 is a diagram schematically showing a state in which is discharged to the exhaust manifold 72 through the exhaust port 71.

  As shown in FIG. 4, the gas sucked into the cylinder includes fresh air sucked from the intake pipe 64 through the throttle valve 62 and from the EGR passage 8 when the EGR valve 81 is opened. Inhaled EGR gas is included. The ratio of the amount of EGR gas to the sum of the amount of fresh air (mass) to be sucked and the amount of mass of EGR (mass) to be sucked (that is, the EGR rate) is appropriately controlled by the ECU 100 according to the operating state. It changes according to the opening degree of 81.

  The fresh air and EGR gas sucked into the cylinder in this way are sucked into the cylinder as the piston 13 (not shown in FIG. 4) descends via the intake valve 16 which is opened in the intake stroke. It becomes in-cylinder gas. This in-cylinder gas is sealed in the cylinder by closing the intake valve 16 when the valve is determined according to the operating state of the engine 1, and is compressed as the piston 13 is raised in the subsequent compression stroke. Is done. When the piston 13 reaches the vicinity of the top dead center, the injector 23 is opened for a predetermined time by the injection amount control by the ECU 100 described above, so that the fuel is directly injected into the combustion chamber 3.

  FIG. 5 is a cross-sectional view showing the combustion chamber 3 and its peripheral portion at the time of fuel injection, and FIG. 6 is a plan view of the combustion chamber 3 at the time of fuel injection (a view showing the upper surface of the piston 13). As shown in FIG. 6, the injector 23 of the engine 1 according to the present embodiment is provided with eight injection holes at equal intervals in the circumferential direction, and fuel is injected equally from these injection holes. It has become so. The number of nozzle holes is not limited to eight.

  The fuel sprays A, A,... Injected from the nozzle holes diffuse in a substantially conical shape. Further, since the fuel injection from each nozzle hole is performed when the piston 13 reaches the vicinity of the top dead center, as shown in FIG. 5, the sprays A, A,... Of each fuel diffuse in the cavity 13b. Will do.

  As described above, the fuel sprays A, A,... Injected from the respective injection holes formed in the injector 23 are mixed with the in-cylinder gas with the passage of time and become air-fuel mixtures in the cylinder. It diffuses in a conical shape and burns by self-ignition. That is, each of the fuel sprays A, A,... Forms a substantially conical combustion field together with the in-cylinder gas, and combustion is started in each of the combustion fields (eight combustion fields in this embodiment). It will be.

  The energy generated by this combustion is kinetic energy for pushing down the piston 13 toward the bottom dead center (energy serving as engine output), thermal energy for raising the temperature in the combustion chamber 3, cylinder block 11 and cylinder head 15 It becomes the heat energy radiated to the outside (for example, cooling water) through.

  The in-cylinder gas after combustion is discharged to the exhaust port 71 and the exhaust manifold 72 as the piston 13 rises through the exhaust valve 17 that opens in the exhaust stroke, and becomes exhaust gas.

-Combustion temperature in the combustion field-
There are various factors that affect the combustion temperature (flame temperature) when the air-fuel mixture burns in the combustion chamber 3 as described above. For example, the volume V _c (α) of the combustion field burning in the combustion chamber 3 (the mixture is present and the mixture is burning: the conical space) is present in the combustion field. The temperature of the air-fuel mixture before the start of combustion (for example, the temperature of the air-fuel mixture immediately after the start of fuel injection and the timing at which combustion has not yet started: Thα), the gas present in the combustion field (the air-fuel mixture before the start of combustion) ) And the specific heat σ of the gas (air mixture before the start of combustion) existing in the combustion field.

In the present embodiment, first, the input heat quantity Q (α) into the combustion chamber 3 is set according to the output required for the engine 1 or the like. This input heat amount Q (α) is a value correlated with the fuel injection amount from the injector 23. Basically, the greater the fuel injection amount, the greater the input heat amount Q (α). And while defining target value _TN of the flame temperature in the said combustion field, the combustion period from the start of the combustion of the fuel injected by the main injection to the end is made into a lot of minute periods (for example, a period of several μsec) ). Further, at least one of the factors is defined for each minute period so that the temperature of the combustion field in each minute period is equal to or lower than the combustion field target temperature _TN . In this way, the flame temperature is optimized by controlling the factors that affect the combustion temperature (flame temperature).

  Hereinafter, the minute period and each factor will be specifically described.

(Small period and typical value during that period)
As a minute period for defining the amount of heat input into the combustion chamber 3, for example, the crank angle and the heat generation rate in FIG. 7 (the entire combustion field (the eight combustion fields) in the combustion chamber 3) are shown. As shown in FIG. 4, the combustion period is divided into a large number in the time axis direction, and the temperature of the combustion field in each minute period is set to be equal to or lower than the combustion field target temperature _TN .

  FIG. 7 shows an ideal heat generation rate waveform related to combustion of fuel injected by main injection, with the horizontal axis representing the crank angle and the vertical axis representing the heat generation rate. TDC in FIG. 7 indicates a crank angle position corresponding to the compression top dead center of the piston 13. As this heat generation rate waveform, for example, combustion of fuel injected by main injection is started from before the compression top dead center (BTDC) of the piston 13, and a predetermined piston position after the compression top dead center (for example, compression top dead center). The heat generation rate reaches a maximum value (peak value) at 10 ° after the point (ATDC 10 °), and a predetermined piston position after the compression top dead center (for example, 25 ° after the compression top dead center (ATDC 25 °) The combustion of the fuel injected in the main injection ends. The heat generation rate waveform is not limited to this.

In the following description, when the minute period is, for example, a period from time ta to tb in FIG. 7 (period hatched in FIG. 7), the representative value of the crank angle in that period is “α”. This “α” is, for example, the median value of the above-described period (the period from ta to tb), and is given by an arithmetic expression such as α = (ta + tb) / 2. That is, in this minute period, the “combustion field volume V _c (α)”, which will be described later, is considered to be constant, and the median value in this minute period is represented.

  The length of this minute period (or the number of compartments in the combustion period) is arbitrary, and the shorter the period length is set (the more the number of compartments in the combustion period is set), The calculation accuracy of the physical quantity to be adjusted can be increased. Further, this minute period can be set as a period each time the crankshaft rotates by a minute crank angle (for example, 0.5 ° CA).

(Combustion field volume)
In the combustion chamber 3, the volume of the combustion field (air mixture is present and the space in which the air mixture is burning: the above eight conical spaces) (hereinafter simply referred to as the combustion field volume V _c). (Referred to as (α)), assuming that the ignition delay period is “0” in the diffusion combustion of diesel combustion, the volume occupied by the spray of fuel injected within that time (the above eight conical shapes) Total volume of space).

For this reason, this combustion field volume V _c (α) is obtained from the penetration (penetration force) or spray spread angle which is required under the influence of the injection hole diameter, number of injection holes, fuel injection pressure, fuel properties, etc. of the injector 23. Is possible.

For example, a map and an arithmetic expression for determining the combustion field volume V _c (α) using the nozzle hole diameter, the number of nozzle holes, the fuel injection pressure, and the fuel properties of the injector 23 as parameters are stored in the ROM 102 to store the combustion field. The volume V _c (α) is obtained. In this case, the fuel injection pressure is set based on the engine load, the engine speed, and the like as described above. The fuel injection pressure for obtaining the combustion field volume V _c (α) uses a detection value detected by the rail pressure sensor 41 or is read from the fuel pressure setting map stored in the ROM 102 in advance.

Actually, since there is a possibility that there is a delay in the ignition of the spray, the combustion field volume V _c (α) can be obtained with higher accuracy in consideration of this. For example, the combustion field volume V _c (α) in consideration of the ignition delay can be obtained by multiplying the combustion field volume obtained from the map or the arithmetic expression by a predetermined correction coefficient (for example, 0.8). The correction coefficient may be changed according to the in-cylinder temperature (for example, the temperature before combustion start described later). For example, the in-cylinder temperature is within a range of 0.5 to 1.0. The higher the value, the higher the value.

(Temperature before starting combustion)
The temperature before starting combustion of the air-fuel mixture existing in the combustion field (hereinafter simply referred to as pre-combustion temperature Thα) is the temperature of the air-fuel mixture existing in the combustion field when fuel injection is performed. .

  For example, at the start of the compression stroke of the engine 1, the intake valve 16 is generally closed when the piston 13 reaches near bottom dead center, and thereafter, until the fuel is injected from the injector 23, There is no new gas inflow or outflow. Therefore, the gas temperature (combustion start temperature Thα) in the combustion chamber 3 near the compression top dead center is determined by the gas state in the cylinder when the intake valve 16 is closed.

  For this reason, the map and the calculation formula (general adiabatic compression formula) for obtaining the pre-combustion temperature Thα using the gas temperature in the cylinder when the intake valve 16 is closed and the compression ratio of the engine 1 as parameters are described above. By storing the data in the ROM 102, the pre-combustion temperature Thα can be obtained. In this case, as the gas temperature in the cylinder at the time when the intake valve 16 is closed, a detected value detected by the intake temperature sensor 49 is used, or an intake temperature estimation map (external air temperature or A map for estimating the intake air temperature from the engine operating state or the like).

(Mixture density)
The density of the air-fuel mixture before the start of combustion existing in the combustion field (hereinafter simply referred to as the air-fuel mixture density ρ) is determined by the amount of gas in the cylinder when the intake valve 16 is closed and the combustion field volume V _c ( It is possible to calculate from the mass of fuel existing in α). Further, a map for obtaining the mixture density ρ from the amount of gas in the cylinder when the intake valve 16 is closed and the mass of fuel existing in the combustion field volume V _c (α) is stored in the ROM 102. The mixture density ρ may be obtained from this map.

(Specific heat of combustion gas)
The specific heat of the gas existing in the combustion field before the start of combustion (hereinafter simply referred to as the combustion gas specific heat σ) is the combustion field volume determined from the gas composition constituting the gas mixture density ρ and the specific heat of the liquid phase substance. It is the specific heat as an air-fuel mixture in V _c (α). Also in this case, the combustion gas specific heat σ is obtained by storing in the ROM 102 a map or an arithmetic expression for obtaining the combustion gas specific heat σ using the mixture density ρ or the like as a parameter.

(Target combustion field temperature)
The combustion field target temperature _TN is the temperature of the combustion gas set to regulate the generation amount of NOx generated with the combustion of the fuel to a preset target generation amount. That is, since the generation amount of NOx has a correlation with the combustion temperature (flame temperature) in the combustion field, for example, a target combustion temperature setting map as shown in FIG. 8 is stored in the ROM 102 and the target generation amount of NOx. The target temperature T _{N of the} combustion field is obtained from (the upper limit value of the allowable generation amount of NOx). According to this target combustion temperature setting map, the target temperature _TN of the combustion field can be easily obtained after setting the allowable NOx generation amount as the target generation amount.

Further, when the NOx target generation amount is set as a predetermined fixed value, the target combustion temperature setting map does not need to be stored in the ROM 102, and corresponds to the NOx target generation amount set as the fixed value. The target temperature T _N of the combustion field is also determined as a fixed value. The target temperature T _N of this combustion field is set to 2500K, for example. The target temperature T _N of this combustion field is not limited to this value.

−Relationship formula of physical quantity−
Next, the relational expression of each physical quantity described above will be described. That is, a relational expression of the combustion field volume V _c (α), the temperature before combustion start Thα, the mixture density ρ, and the combustion gas specific heat σ with respect to the target temperature _TN and input heat quantity Q (α) given in advance will be described. To do.

  First, from a general heat capacity relationship, a relational expression of a heat generation rate due to combustion of fuel injected from one injection hole at a certain moment (the minute period described above) is defined as the following expression (1).

Here, ρ (t) is the density of the combustion space at time t (time in one of the minute periods), and V _L (i, t) is i-th (divided into a large number) corresponding to time t. The volume of the combustion space in the i-th) combustion period, σ (t) is the constant volume specific heat in the volume V _L (i, t) of the combustion space in the i-th combustion period corresponding to time t. It is.

  Regarding the second term (the product of the pressure and the volume change in the minute period) on the right side in the equation (1), since the expression (1) is a relational expression in the minute period, the first term on the right side. Can be included or ignored. In the following description, it is assumed that the second term on the right side is not considered.

When the total volume of the combustion space burning at the time t is V _c (t), the following equation (2) is obtained.

  Here, N is the total number of sections in the minute period.

  When the above equation (1) is deformed with respect to the temperature change using the above equation (2) or the like, the following equation (3) is obtained.

  When there is fuel that burns at the time α of the spray mass for each combustion unit, the temperature after the combustion becomes the following equation (4) by integrating the above equation (3).

  Here, T (i, α) is the temperature of the spray mass after combustion in the i-th minute period (median value α), and Thα is the mixture gas before combustion including the spray combusted in the i-th combustion period. Temperature.

At this time, since dt is very small, ρ (t) and V _L (i, t) can be regarded as constant at time α and a minute time before and after the time α. For this reason, the following formula | equation (5) is calculated | required.

  Further, when the latter half of the above formula (5) is integrated with respect to the heat generation amount, the following formula (6) is obtained.

  Here, when the temperature rise in the minute period is ΔT (i, α), the following equation (7) is obtained.

  Here, the temperature at which the entire combustion region (combustion field) rises is obtained as the following equation (8) by adding the individual temperature and volume of the spray mass.

  Here, M is the number of injection holes of the injector 23 (“8” in this embodiment). Also,

  When the quantity of heat input within the target time is Q (α), the following equation (10) is obtained.

Here, since the amount of NOx produced is determined by the combustion temperature, in order to keep the amount of NOx produced below the desired value (below the NOx target generation amount), the target combustion temperature T _N is set and Thα + ΔT (i, The condition is that α, j) ≦ T _N. By applying this to the above equation (10), the following equation (11) is obtained.

  By transforming this equation (11), the following equation (12) is obtained as a relational expression of each physical quantity.

That is, while the input heat quantity Q (α) and the target combustion temperature T _N are given in the equation (12) and at least one of other physical quantities is appropriately adjusted, the input heat quantity Q (α) is secured. The flame temperature can be suppressed to the target combustion temperature _TN , and the NOx generation amount can be suppressed to a desired value or less (the NOx target generation amount or less). That is, by applying this equation (12) to each minute period, the amount of heat input Q (Q) (in the combustion chamber 3 in each minute period (i = 1, i = 2,..., I = N)). It is possible to suppress the combustion temperature to the target combustion temperature T _N while securing α). That is, in this embodiment, the flame temperature is optimized by controlling the physical quantity by feedforward control.

-Determination of physical quantity-
Next, the physical quantity controlled to achieve the amount of heat input Q (α) into the combustion chamber 3 and the target combustion temperature T _N in the above equation (12) (factors affecting the combustion temperature (flame temperature)). A plurality of embodiments of the control operation (physical quantity adjustment operation by the physical quantity adjustment unit: combustion temperature adjustment control) for obtaining the above will be described. In the following embodiments, the flame temperature is optimized by controlling one of the plurality of physical quantities.

(First embodiment)
In the present embodiment, the combustion temperature in the combustion chamber 3 is adjusted to be equal to or lower than the target combustion temperature T _N by controlling the combustion field volume V _c (α) among the various physical quantities in the equation (12). is there. In other words, the combustion temperature in the combustion chamber 3 either match to the target combustion temperature T _N, or, in order to suppress to less than the target combustion temperature T _N, and controls the combustion field volume V _c (alpha) is there. In the following description, the other physical quantities are fixed values obtained by detection or estimation. Specific control operations (combustion temperature adjustment control) include a fuel injection amount adjustment operation and a fuel injection pressure adjustment operation of the injector 23. Hereinafter, each combustion temperature adjustment control will be described.

<Adjustment of fuel injection amount>
First, the adjustment operation of the fuel injection amount of the injector 23 includes performing an increase correction on the basic fuel injection amount set based on the engine speed, the accelerator operation amount, and the like as described above. Thereby, the occupation volume of the fuel spray in the combustion chamber 3 at the time of fuel injection execution is expanded. That is, the combustion field volume V _c (α) is increased.

In this way, when set to a large combustion field volume V _c (alpha), if the above expression combustion field volume V _c on the right-hand side of (12) (α) was transposed to the left side, combustion field volume V _c ( Since the value on the left side becomes smaller as (α) is larger (other parameters are fixed values), the relationship of this equation (12) can be easily achieved. That is, the input heat quantity Q (α) and the target combustion temperature T _N into the combustion chamber 3 given in advance can be achieved by adjusting the combustion field volume V _c (α).

As a specific method for obtaining the increase correction amount with respect to the basic fuel injection amount, fuel injection is performed so that the combustion field volume V _c (α) becomes the minimum value within the range in which the inequality of the equation (12) is established. By storing a map and an arithmetic expression for obtaining the amount in the ROM 102, the increase correction amount that does not increase the combustion field volume V _c (α) more than necessary is obtained. . FIG. 9 shows an example of a fuel injection correction amount map. Thus, the fuel injection correction amount of the injector 23 is increased as the combustion field volume V _c (α) obtained by the above equation (12) is larger.

The combustion field volume V _c (α) is a value larger than the minimum value (the minimum value of the combustion field volume V _c (α) within the range in which the inequality of Expression (12) is satisfied). Since the inequality of equation (12) is established, the required combustion field volume V _c (α) is not limited to the minimum value within the range in which the inequality of equation (12) is established. Absent. However, if the fuel injection amount is increased more than necessary, the amount of heat input is greatly increased, and engine output exceeding that required by the driver is generated, leading to deterioration in drivability. For this reason, a predetermined upper limit value is set for the correction amount of the fuel injection amount.

By adjusting the fuel injection amount in this manner, the combustion temperature can be made not more than the combustion field target temperature T _N over the entire combustion period, and the amount of NOx generated can be kept below the target generation amount. .

In the physical quantity control (adjustment of the fuel injection amount in this embodiment) actually performed based on the above equation (12), the heat generation rate is increased after the combustion in the combustion chamber 3 is started. Until the peak value is reached (during the period S in FIG. 7), the combustion pre-combustion temperature Thα gradually increases as the combustion in the combustion chamber 3 progresses. That is, assuming that the combustion field volume V _c (α) is constant, as the combustion in the combustion chamber 3 proceeds, the value on the right side of the above equation (12) gradually decreases, and the target There is a possibility that the input heat quantity Q (α) to be achieved cannot be achieved. Therefore, at least until the heat generation rate reaches the peak value, the combustion field volume V _c (α) is controlled so that the target input heat quantity Q (α) can be achieved (for example, combustion in the combustion chamber 3). Therefore, it is necessary to control the combustion field volume V _c (α) to be increased). Also in the present embodiment, the physical quantity is controlled only for this period S. In addition, you may make it control physical quantity based on said Formula (12) over the whole area | region of a combustion period.

<Fuel injection amount adjustment timing>
Specific examples of the timing for determining the corrected fuel injection amount as described above include the vicinity of when the intake valve 16 is closed. This will be specifically described below.

As described above, when the intake valve 16 is closed, no new gas flows into or out of the cylinder until fuel is injected from the injector 23 thereafter. That is, the state of the combustion field is determined when the intake valve 16 is closed. For this reason, each parameter in said Formula (12) is determined by the valve closing time of the intake valve 16 or the state in the cylinder just before valve closing. That is, at this time, based on the above equation (12), the fuel injection amount (combustion field volume V _c (combustion field volume V _c (1)) in the minute period (first minute period: i = 1) at the start of combustion. The fuel injection amount) for enlarging α) can be defined. Further, by determining the fuel injection amount in the first minute period, the pre-combustion temperature Thα in the second minute period (i = 2) is defined. For this reason, the fuel injection amount (fuel injection amount for expanding the combustion field volume V _c (α)) in this minute period is specified for the second minute period based on the above equation (12). can do. In this way, the fuel injection amount in each minute period can be obtained before the fuel injection start timing. Therefore, at this fuel injection start timing, the combustion temperature in all the minute periods is the combustion field target temperature T _N. It becomes possible to set the fuel injection mode (fuel injection rate waveform) as follows.

As described above, in this embodiment, a fuel injection mode (fuel injection rate waveform) in which the combustion temperature in all the minute periods is equal to or lower than the combustion field target temperature T _N can be set, and NOx in the combustion chamber 3 can be set. It is possible to make the generation amount equal to or less than the target generation amount.

In the above description, the fuel injection amount determination timing is in the vicinity of when the intake valve 16 is closed. That is, it has been described that the fuel injection amount in the combustion stroke performed immediately after is obtained and the fuel injection rate waveform is set accordingly. The present invention is not limited to this, and the fuel injection amount for obtaining the combustion field volume V _c (α) obtained by the above equation (12) is used for setting the fuel injection amount for the cylinder that reaches the combustion stroke in the next cycle. Alternatively, it may be used to set the fuel injection amount for the next cycle of the own cylinder (the cylinder that reaches the combustion stroke immediately after calculation of the fuel injection amount), that is, the cylinder that reaches the combustion stroke after a crank angle of approximately 720 ° CA. May be. Further, as the timing for determining the fuel injection amount, that is, the timing for determining the fuel injection amount into the combustion chamber 3 based on the combustion field volume V _c (α) defined by the above equation (12), the intake valve 16 is used. It is not limited to when the valve is closed but may be during the combustion stroke. In this case, as described above, it is used for setting the fuel injection rate waveform in the cylinder that reaches the combustion stroke in the next cycle or in the next cycle of the own cylinder.

<Adjustment of fuel injection pressure>
Further, the adjustment operation of the fuel injection pressure includes performing an increase correction on the basic fuel injection pressure set based on the fuel pressure setting map as described above. Also in this case, the occupied volume of the fuel spray in the combustion chamber 3 when the fuel injection is executed is increased. That is, the combustion field volume V _c (α) is increased.

In this way, when set to a large combustion field volume V _c (alpha), if the above expression combustion field volume V _c on the right-hand side of (12) (α) was transposed to the left side, combustion field volume V _c ( Since the value on the left side becomes smaller as (α) is larger (other parameters are fixed values), the relationship of this equation (12) can be easily achieved. That is, the input heat quantity Q (α) and the target combustion temperature T _N into the combustion chamber 3 given in advance can be achieved by adjusting the combustion field volume V _c (α).

As a specific method for obtaining the increase correction amount with respect to the basic fuel injection pressure, the fuel injection is such that the combustion field volume V _c (α) becomes the minimum value within the range where the inequality of the above equation (12) holds. By storing a map for calculating the pressure and an arithmetic expression in the ROM 102, the increase correction amount that does not increase the combustion field volume V _c (α) more than necessary is obtained. . FIG. 10 shows an example of the fuel injection pressure correction map. Thus, the fuel injection pressure correction amount increases as the combustion field volume V _c (α) obtained by the above equation (12) increases. Specifically, the fuel discharge amount of the supply pump 21 is adjusted so that the common rail pressure is increased and corrected.

The combustion field volume V _c (α) is a value larger than the minimum value (the minimum value of the combustion field volume V _c (α) within the range in which the inequality of Expression (12) is satisfied). Since the inequality of equation (12) is established, the required combustion field volume V _c (α) is not limited to the minimum value within the range in which the inequality of equation (12) is established. Absent. However, if the fuel injection pressure is increased more than necessary, there is a possibility that problems such as adhesion of fuel to the wall surface may occur. For this reason, a predetermined upper limit value is set for the correction amount of the fuel injection pressure.

By adjusting the fuel injection pressure in this manner, the combustion temperature can be made lower than the combustion field target temperature T _N over the entire combustion period, and the amount of NOx generated can be suppressed below the target generated amount. .

  Further, as the timing for determining the corrected fuel injection pressure in this case, the vicinity of the time when the intake valve 16 is closed may be mentioned, similar to the timing for determining the fuel injection amount described above. Further, not only near the time when the intake valve 16 is closed, it may be during the combustion stroke.

(Second Embodiment)
In the present embodiment, when the combustion field volume V _c (α) is controlled among the various physical quantities in the above equation (12), a countermeasure when the required combustion field volume V _c (α) is relatively small is obtained. It is.

When the required combustion field volume V _c (α) is obtained relatively small in this way, in the first embodiment, for example, the fuel injection pressure is set low. However, when the fuel injection pressure is set low in this way, a large amount of soot may be generated in the exhaust gas. That is, even if the NOx generation amount can be suppressed to the target generation amount or less by controlling the combustion field volume V _c (α) according to the equation (12), the generation amount of Soot increases as a contradiction. Exhaust emissions may be worsened. That is, even when the fuel injection pressure is set low, if the amount of heat generation is sufficient in the above calculation, the ignition delay is short and diffusion combustion often proceeds. At this time, since the mixing of air and fuel is delayed, the intake of air (oxygen) with respect to the fuel spray is delayed, and the generation amount of soot may increase.

  This second embodiment takes into consideration the occurrence of such a situation.

  In the second embodiment, the design of the injector 23 is changed to suppress the generation amount of the soot. Specifically, the injection hole diameter of the injector 23 can be reduced, or the needle speed of the injector 23 can be increased.

  When the atomization of the fuel in the combustion chamber 3 is promoted, an overrich air-fuel mixture is generated in the combustion chamber 3 and the intake of air (oxygen) to the fuel spray increases. Means for promoting atomization of the fuel include increasing the fuel injection pressure, reducing the nozzle hole diameter, and increasing the needle speed. In this embodiment, the first embodiment (fuel injection pressure) In this case, the soot generation amount is reduced by reducing the nozzle hole diameter or by increasing the needle speed of the injector 23. Since specific means for reducing the diameter of the nozzle hole or increasing the needle speed of the injector 23 are known, the description thereof is omitted here.

  Thereby, in this embodiment, it is possible to suppress both the generation amount of NOx and the generation amount of Soot, and the exhaust emission can be improved.

(Third embodiment)
In the present embodiment, the combustion temperature in the combustion chamber 3 is adjusted to be equal to or lower than the target combustion temperature T _N by controlling the pre-combustion temperature Thα among the various physical quantities in the equation (12). In other words, if the combustion temperature in the combustion chamber 3 match to the target combustion temperature T _N, or, in order to suppress to less than the target combustion temperature T _N, and controls the combustion start temperature before Tharufa.

To explain using the above equation (12), when ( _TN −Thα) on the right side in this equation (12) is shifted to the left side, the lower the pre-combustion temperature Thα, the smaller the value on the left side. (Other parameters are fixed values) The relationship of this equation (12) can be easily achieved. That is, the input heat quantity Q (α) and the target combustion temperature T _N into the combustion chamber 3 given in advance can be achieved by adjusting the pre-combustion temperature Thα.

  The pre-combustion temperature Thα is determined by the in-cylinder gas temperature at the time of in-cylinder compression, the temperature of the fuel, and the degree of atomization of the fuel.

  In order to lower the in-cylinder gas temperature, it is necessary to lower the intake air temperature. Specific methods for this include controlling the efficiency of the intercooler 61, controlling the EGR gas temperature, controlling the supercharging pressure by the turbocharger 5, and controlling the fuel injection pressure. Hereinafter, each combustion temperature adjustment control will be described.

<Control of efficiency of intercooler 61>
As described above, the intercooler 61 forcibly cools the intake air whose temperature has been raised by supercharging in the turbocharger 5, and a heat exchanger for cooling the intake air with cooling water is provided therein. Is provided. In the present embodiment, the efficiency of the intercooler 61 can be controlled by changing the flow rate of the cooling water flowing into the heat exchanger.

  Specifically, an electromagnetic valve whose opening degree can be adjusted is provided in the middle of the cooling water flow path connected to the intercooler 61, and the flow rate of the cooling water flowing into the heat exchanger is adjusted by adjusting the opening degree of the electromagnetic valve. This is a configuration that can be changed. That is, when lowering the intake air temperature to lower the in-cylinder gas temperature, the opening of the electromagnetic valve is increased so that the flow rate of the cooling water flowing into the heat exchanger is increased.

  As for the opening degree of the electromagnetic valve, a map and an arithmetic expression for obtaining an opening degree at which the pre-combustion temperature Thα becomes the maximum value within the range in which the inequality of the expression (12) is established are stored in the ROM 102. By setting, the efficiency of the intercooler 61 is adjusted. FIG. 11 shows an example of a solenoid valve opening map. Thus, the lower the pre-combustion temperature Thα determined by the above equation (12), the larger the electromagnetic valve opening.

In this way, by adjusting the efficiency of the intercooler 61 and controlling the pre-combustion temperature Thα, the combustion temperature is kept below the combustion field target temperature T _N over the entire combustion period, and the amount of NOx generated is reduced as described above. It becomes possible to suppress it to the target generation amount or less.

<Control of EGR gas temperature>
The EGR cooler 82 has substantially the same configuration as the intercooler 61 described above, and includes a heat exchanger for cooling the EGR gas with cooling water. In the present embodiment, the efficiency of the EGR cooler 82 can be controlled by changing the flow rate of the cooling water flowing into the heat exchanger.

  Specifically, an electromagnetic valve whose opening degree can be adjusted is provided in the middle of the cooling water flow path connected to the EGR cooler 82, and the flow rate of the cooling water flowing into the heat exchanger is adjusted by adjusting the opening degree of the electromagnetic valve. This is a configuration that can be changed. That is, when lowering the EGR gas temperature to lower the in-cylinder gas temperature, the opening of the electromagnetic valve is increased so that the flow rate of the cooling water flowing into the heat exchanger is increased.

  As for the opening degree of the electromagnetic valve, a map and an arithmetic expression for obtaining an opening degree at which the pre-combustion temperature Thα becomes the maximum value within the range in which the inequality of the expression (12) is established are stored in the ROM 102. By setting, the efficiency of the EGR cooler 61 is adjusted. The electromagnetic valve opening map in this case is the same as that shown in FIG. That is, the lower the pre-combustion temperature Thα determined by the above equation (12), the larger the electromagnetic valve opening.

In this way, by adjusting the efficiency of the EGR cooler 61 and controlling the pre-combustion temperature Thα, the combustion temperature is made not more than the combustion field target temperature T _N over the entire combustion period, and the amount of NOx generated is reduced as described above. It becomes possible to suppress it to the target generation amount or less.

  In addition, a configuration in which a cooler bypass passage (not shown) for bypassing the EGR cooler 82 is provided as the EGR passage 8 and an electromagnetic valve whose opening degree can be adjusted is provided in the cooler bypass passage may be applied. That is, the amount of EGR gas that bypasses the EGR cooler 82 can be adjusted by adjusting the opening of the electromagnetic valve. When the EGR gas temperature is lowered in order to lower the in-cylinder gas temperature, the opening of the electromagnetic valve is reduced so that the amount of EGR gas flowing into the EGR cooler 82 is increased. Thereby, EGR gas temperature can be reduced. As a result, the pre-combustion temperature Thα can be reduced.

<Supercharging pressure control>
The turbocharger 5 is a variable nozzle type turbocharger, and a variable nozzle vane mechanism (not shown) is provided on the turbine wheel 52 side. By adjusting the opening degree of the nozzle vane provided in the variable nozzle vane mechanism, The supercharging pressure of the engine 1 can be adjusted. Since this variable nozzle vane mechanism is publicly known, the description of the configuration here is omitted.

  In order to reduce the in-cylinder gas temperature, the opening degree of the nozzle vane is increased, and the rotational speed of the turbocharger 5 is decreased (the rotational speed of the compressor wheel 53 is decreased: supercharging efficiency (supercharging pressure)). Reduced).

  As for the opening degree of the nozzle vane, a map and an arithmetic expression for obtaining an opening degree at which the pre-combustion temperature Thα becomes the maximum value within the range where the inequality of the above expression (12) is established are stored in the ROM 102. It has come to adjust. FIG. 12 shows an example of the nozzle vane opening degree map. Thus, the lower the pre-combustion temperature Thα determined by the above equation (12), the larger the nozzle vane opening.

In this way, by adjusting the supercharging pressure of the turbocharger 5 and controlling the pre-combustion temperature Thα, the combustion temperature is kept below the combustion field target temperature T _N over the entire combustion period, and the amount of NOx generated Can be suppressed to the target generation amount or less.

<Control of fuel injection pressure>
The in-cylinder gas temperature can also be lowered by controlling the fuel injection pressure. That is, if the fuel injection pressure is set high, atomization of the fuel injected into the combustion chamber 3 is promoted, and the combustion field (space where the fuel exists) is caused by the latent heat generated when the fuel is vaporized. The temperature can be lowered. That is, the temperature before combustion start Thα can be lowered by setting the fuel injection pressure high.

  The fuel injection pressure is stored in the ROM 102 as a map or an arithmetic expression for obtaining an opening degree at which the pre-combustion temperature Thα becomes the maximum value within the range where the inequality of the expression (12) is established. Thus, the fuel injection pressure is adjusted. FIG. 13 shows an example of the injection pressure control map. Thus, the fuel injection pressure is increased as the pre-combustion temperature Thα determined by the above equation (12) is lower.

In this way, by adjusting the fuel injection pressure and controlling the pre-combustion temperature Thα, the combustion temperature is kept below the combustion field target temperature T _N over the entire combustion period, and the amount of NOx generated is the target generation. It becomes possible to keep it below the amount.

  Even when the fuel injection pressure is adjusted in this way to control the pre-combustion temperature Thα, as described above, the fuel injection pressure will not be increased more than necessary (for example, fuel wall adhesion). A predetermined upper limit is set for the fuel injection pressure so that no malfunction occurs.

(Fourth embodiment)
In the present embodiment, the combustion temperature in the combustion chamber 3 is adjusted to be equal to or lower than the target combustion temperature _TN by controlling the mixture density ρ among the various physical quantities in the above formula (12). In other words, if the combustion temperature in the combustion chamber 3 match to the target combustion temperature T _N, or, in order to suppress to less than the target combustion temperature T _N, and controls the air-fuel mixture density [rho.

To explain using the above formula (12), when the mixture density ρ on the right side is moved to the left side in this formula (12), the higher the mixture density ρ, the smaller the value on the left side (otherwise The parameter of (12) is a fixed value), and the relationship of this equation (12) can be easily achieved. That is, the input heat quantity Q (α) and the target combustion temperature _TN into the combustion chamber 3 given in advance can be achieved by adjusting the mixture density ρ.

  Hereinafter, the combustion temperature adjustment control in this case will be specifically described.

The air-fuel mixture density ρ is determined from the amount of gas (air amount and EGR gas amount) and the amount of fuel in the combustion field (space where fuel spray exists), and the volume V _c (α) of the combustion field. For this reason, assuming that this combustion field volume V _c (α) is recognized (detected or estimated) in advance, it is preferable that the amount of gas in the space be smaller, so the boost pressure by the turbocharger 5 is increased. The amount of gas is decreased by the above control, the opening degree control of the throttle valve 62, the opening degree control of the swirl control valve 66, etc., and the mixture density ρ is increased.

  That is, the nozzle vane opening of the variable nozzle vane mechanism is increased to decrease the rotational speed of the turbocharger 5 (reducing supercharging efficiency), the opening of the throttle valve 62 is decreased, and the swirl control valve 66 is operated. The amount of gas is reduced by reducing the opening of the gas.

  In such opening degree control, the ROM 102 stores a map and an arithmetic expression for obtaining an opening degree at which the air-fuel mixture density ρ becomes the minimum value within the range in which the inequality of the expression (12) is established. Thus, the opening degree is adjusted. The broken line in FIG. 14 shows an example of an opening degree control map for controlling the nozzle vane opening degree. Thus, the higher the air-fuel mixture density ρ determined by the above equation (12), the larger the nozzle vane opening. On the other hand, the solid line in FIG. 14 shows an example of an opening degree control map for controlling the opening degree of the throttle valve 62 or the swirl control valve 66. Thus, the higher the air-fuel mixture density ρ determined by the above equation (12), the smaller the opening degree of the throttle valve 62 and the swirl control valve 66.

By controlling the air-fuel mixture density ρ in this way, the combustion temperature can be kept below the combustion field target temperature T _N over the entire combustion period, and the amount of NOx generated can be kept below the target generation amount. Become.

(Fifth embodiment)
In the present embodiment, the combustion temperature in the combustion chamber 3 is adjusted to be equal to or lower than the target combustion temperature T _N by controlling the combustion gas specific heat σ among the various physical quantities in the equation (12). In other words, if the combustion temperature in the combustion chamber 3 match to the target combustion temperature T _N, or, in order to suppress to less than the target combustion temperature T _N, and controls the combustion gas specific heat sigma.

When the above equation (12) is used for explanation, when the combustion gas specific heat σ on the right side is shifted to the left side in this equation (12), the higher the combustion gas specific heat σ, the smaller the value on the left side (otherwise The parameter of (12) is a fixed value), and the relationship of this equation (12) can be easily achieved. That is, the heat quantity Q (α) and the target combustion temperature _TN supplied to the combustion chamber 3 given in advance can be achieved by adjusting the combustion gas specific heat σ.

  Hereinafter, the combustion temperature adjustment control in this case will be specifically described.

  As control for increasing the combustion gas specific heat σ, increasing the amount of EGR gas can be mentioned. That is, the opening degree of the EGR valve 81 is set large, and the exhaust gas recirculation amount (EGR amount) toward the intake manifold 63 is increased. That is, the EGR rate is increased and the oxygen concentration in the combustion chamber 3 is decreased.

  Such an opening degree control of the EGR valve 81 is performed in the ROM 102 with a map and an arithmetic expression for obtaining an opening degree at which the combustion gas specific heat σ becomes the minimum value within a range where the inequality of the above expression (12) is established. The opening degree of the EGR valve 81 is adjusted by storing the value. FIG. 15 shows an example of an opening degree control map for controlling the opening degree of the EGR valve 81. As described above, the higher the combustion gas specific heat σ obtained by the above equation (12), the larger the opening degree of the EGR valve 81 is.

By controlling the combustion gas specific heat σ in this way, the combustion temperature can be kept below the combustion field target temperature T _N over the entire combustion period, and the amount of NOx generated can be kept below the target generation amount. Become.

Further, the execution timing of the combustion temperature adjustment control (physical quantity control) using the above-described second to fifth embodiments is similar to that at the time when the intake valve 16 is closed, as in the first embodiment described above. Or during the combustion stroke. The first to fifth embodiments described above may be applied to the engine 1 individually, that is, only one embodiment may be applied to the engine 1, or a plurality may be combined and applied to the control of the engine 1. May be. That is, by simultaneously adjusting a plurality of physical quantities, the combustion temperature may be made lower than the combustion field target temperature T _N over the entire combustion period, and the amount of NOx generated may be kept below the target generated quantity.

-Other embodiments-
In each of the embodiments described above, the case where the present invention is applied to an in-line four-cylinder diesel engine mounted on an automobile has been described. The present invention is applicable not only to automobiles but also to engines used for other purposes. Further, the number of cylinders and the engine type (separate type engine, V-type engine, horizontally opposed engine, etc.) are not particularly limited.

  In each of the above embodiments, the NSR catalyst 75 and the DPNR catalyst 76 are provided as the manipulator 77, but the NSR catalyst 75 and a DPF (Diesel Particle Filter) may be provided.

  In each of the above embodiments, the EGR device is configured to recirculate the exhaust gas in the exhaust manifold 72 to the intake system 6. The present invention is not limited to this, and an LPL (Low Pressure Loop) EGR device that recirculates exhaust gas downstream of the turbine wheel 52 in the turbocharger 5 to the intake system 6 may be employed.

As described above, the present embodiment can also be applied to a diesel engine that performs sub-injection or split main injection. In this case, the present invention is applied to each of the sub-injections (pilot injection, pre-injection, after-injection, post-injection), and the combustion temperature is the combustion field target temperature T _N not only in the main injection but also in any sub-injection. It is preferable to make the following. Further, when performing split main injection, the present invention is applied to each of the split main injections so that the combustion temperature is equal to or lower than the combustion field target temperature T _N in any split main injection. It is preferable to keep it.

  Further, in each of the above-described embodiments, the engine to which the piezo injector 23 that changes the fuel injection rate by being in a fully opened valve state only during the energization period has been described. However, the present invention applies a variable injection rate injector. It can also be applied to the engine.

  The present invention is applicable to control for reducing NOx emission in a common rail in-cylinder direct injection multi-cylinder diesel engine mounted on an automobile.

1 engine (internal combustion engine)
3 Combustion chamber 23 Injector (fuel injection valve)
V _c (α) Combustion field volume Thα Temperature before combustion start in combustion field _TN Target combustion field temperature ρ Gas density σ Gas specific heat Q (α) Input heat quantity

-Solution-
Specifically, the present invention is premised on a control device for a compression self-ignition internal combustion engine that burns fuel injected from a fuel injection valve by self-ignition in a combustion chamber. With respect to the control device for the internal combustion engine, the combustion field target temperature for limiting the NOx generation amount during combustion in the combustion field where the fuel burns to a predetermined target NOx generation amount, and the output of the internal combustion engine reach a required output. For the combustion chamber, the volume of the combustion field where the fuel burns, the temperature of the combustion field before the start of combustion, the density of the gas present in the combustion field, and the gas present in the combustion field By adjusting at least one physical quantity of the specific heat of the combustion chamber, the physical quantity adjustment is performed so that the temperature of the combustion field is made not more than the target temperature of the combustion field and the target input heat quantity is obtained as the input heat quantity into the combustion chamber Have a part. The physical quantity adjusting unit divides the combustion period in the combustion chamber into a plurality of minute periods, and adjusts the physical quantity so that the combustion temperature of the combustion field in each of the minute periods is equal to or lower than the combustion field target temperature. It has become.

By adjusting at least one of the physical quantities in accordance with this specific matter, the temperature of the combustion field is made equal to or lower than the target temperature of the combustion field, and the target input heat quantity is obtained as the input heat quantity into the combustion chamber. It will be. For this reason, the output required for the internal combustion engine can be obtained, and the NOx generation amount at the time of combustion in the combustion field can be limited to the predetermined target NOx generation amount, so that exhaust emission can be improved. In addition, a physical quantity for limiting the NOx generation amount during combustion in the combustion field to a predetermined target NOx generation amount can be defined with high accuracy for each of the minute periods. As a result, the NOx generation amount in the combustion field can be limited to a predetermined target NOx generation amount or less over substantially the entire combustion period.

-Solution-
Specifically, the present invention is premised on a control device for a compression self-ignition internal combustion engine that burns fuel injected from a fuel injection valve by self-ignition in a combustion chamber. With respect to the control device for the internal combustion engine, the combustion field target temperature for limiting the NOx generation amount during combustion in the combustion field where the fuel burns to a predetermined target NOx generation amount, and the output of the internal combustion engine reach a required output. For the combustion chamber, the volume of the combustion field where the fuel burns, the temperature of the combustion field before the start of combustion, the density of the gas present in the combustion field, and the gas present in the combustion field By adjusting at least one physical quantity of the specific heat of the combustion chamber, the physical quantity adjustment is performed so that the temperature of the combustion field is made not more than the target temperature of the combustion field and the target input heat quantity is obtained as the input heat quantity into the combustion chamber Have a part. Then, the physical quantity adjusting unit divides the combustion period in the combustion chamber into a plurality of minute periods, and only the period until the heat generation rate reaches a substantially peak value in the combustion period in the combustion chamber. The physical quantity is adjusted so that the combustion temperature of the combustion field in each period is equal to or lower than the combustion field target temperature.

By adjusting at least one of the physical quantities in accordance with this specific matter, the temperature of the combustion field is made equal to or lower than the target temperature of the combustion field, and the target input heat quantity is obtained as the input heat quantity into the combustion chamber. It will be. For this reason, the output required for the internal combustion engine can be obtained, and the NOx generation amount at the time of combustion in the combustion field can be limited to the predetermined target NOx generation amount, so that exhaust emission can be improved. In addition, a physical quantity for limiting the NOx generation amount during combustion in the combustion field to a predetermined target NOx generation amount can be defined with high accuracy for each of the minute periods. As a result, the NOx generation amount in the combustion field can be limited to a predetermined target NOx generation amount or less over substantially the entire combustion period.
In addition, when the heat generation rate exceeds the peak value during the combustion period, the combustion field temperature tends to gradually decrease thereafter, and the possibility that the NOx generation amount increases correspondingly decreases. Considering this, the period for controlling the physical quantity so that the temperature at the time of combustion in the combustion field is equal to or lower than the combustion field target temperature is only the period until the heat generation rate reaches a substantially peak value. This makes it possible to limit the NOx generation amount to a predetermined target NOx generation amount or less over the entire combustion period while minimizing the physical quantity control period.

Claims (8)

In a control device for a compression self-ignition internal combustion engine that burns fuel injected from a fuel injection valve by self-ignition in a combustion chamber,
Combustion field target temperature for limiting the NOx generation amount during combustion in the combustion field where the fuel burns to a predetermined target NOx generation amount, and target input heat amount into the combustion chamber for the output of the internal combustion engine to reach the required output And give
Adjusting at least one physical quantity of the volume of the combustion field where the fuel burns, the temperature of the combustion field before combustion, the density of the gas present in the combustion field, and the specific heat of the gas present in the combustion field An internal combustion engine comprising: a physical quantity adjusting unit that makes the temperature of the combustion field equal to or lower than the combustion field target temperature and that obtains the target input heat quantity as the input heat quantity into the combustion chamber. Control device. The control apparatus for an internal combustion engine according to claim 1,
The physical quantity adjusting unit is configured to divide the combustion period in the combustion chamber into a plurality of minute periods and adjust the physical quantity so that the combustion temperature of the combustion field in each of the minute periods is equal to or lower than the combustion field target temperature. A control device for an internal combustion engine. The control device for an internal combustion engine according to claim 1 or 2,
The physical quantity adjusting unit adjusts the combustion temperature in the combustion field to be equal to or lower than the combustion field target temperature only for the period until the heat generation rate reaches a substantially peak value in the combustion period in the combustion chamber. A control device for an internal combustion engine, characterized in that a physical quantity is adjusted. The control device for an internal combustion engine according to claim 1 or 2,
The physical quantity adjusting unit expands the volume of the combustion field in which the fuel burns, and corrects the increase in the amount of fuel injected from the fuel injection valve into the combustion chamber and is injected from the fuel injection valve into the combustion chamber. A control apparatus for an internal combustion engine, wherein at least one of the corrections for increasing the fuel injection pressure is executed. The control device for an internal combustion engine according to claim 1 or 2,
When the physical quantity adjusting unit adjusts the physical quantity so as to adjust the volume of the combustion field in which the fuel burns, in order to avoid that the volume of the combustion field becomes less than a predetermined value, the nozzle hole diameter of the fuel injection valve A control device for an internal combustion engine, which is designed to reduce the diameter and increase the operating speed of a needle provided in a fuel injection valve. The control device for an internal combustion engine according to claim 1 or 2,
The physical quantity adjusting unit lowers the temperature of the combustion field before the start of combustion, and performs control and supercharging to increase the cooling efficiency of the intercooler provided in the intake system with respect to the one provided with the supercharging device. Control that lowers the pressure, control that improves the cooling efficiency of the EGR cooler for those equipped with an exhaust gas recirculation device that recirculates part of the exhaust gas discharged to the exhaust system, and injects from the fuel injection valve into the combustion chamber A control apparatus for an internal combustion engine, wherein at least one of the increase corrections of the injected fuel injection pressure is performed. The control device for an internal combustion engine according to claim 1 or 2,
The physical quantity adjusting unit is for increasing the density of the gas present in the combustion field, and for reducing the supercharging pressure relative to the one equipped with the supercharging device, and opening the valve provided in the intake system. A control apparatus for an internal combustion engine, characterized in that at least one of control for reducing the intake air amount by reducing it is executed. The control device for an internal combustion engine according to claim 1 or 2,
The physical quantity adjustment unit increases the specific heat of the gas present in the combustion field, and has an EGR rate compared to an apparatus equipped with an exhaust gas recirculation device that recirculates a part of the exhaust gas discharged to the exhaust system to the intake system. A control device for an internal combustion engine, characterized in that control for increasing the engine is executed.

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