JP6233011B2 - Engine control device - Google Patents

Description

  The present invention relates to a technical field of an engine control device that controls an engine that can be operated while switching a plurality of combustion modes.

  As this type of device, for example, a device that switches between a lean combustion mode and a stoichiometric combustion mode using a combustion mode map based on an engine speed and an engine load has been proposed (see Patent Document 1).

  Alternatively, a device for predicting and recognizing a change in the load demand on the engine that changes depending on how the driver operates the clutch when the vehicle starts is proposed in advance to limit the engine combustion switching request (Patent Document). 2).

  Alternatively, the device can switch from the stratified combustion mode to the homogeneous combustion mode in accordance with the operating state of the engine, and when the engine load is expected to shift to a predetermined low load region, the homogeneous combustion from the stratified combustion mode is performed. An apparatus that prohibits switching to a mode has been proposed (see Patent Document 3).

  Alternatively, an apparatus that predicts switching of the combustion mode based on the change state of the target load of the engine that can be operated by switching between the stratified combustion mode and the uniform combustion mode has been proposed (see Patent Document 4).

JP 2008-157104 A JP 2003-214216 A JP 2001-152914 A JP 2000-205006 A

  The technique described in Patent Document 1 has a technical problem that when the required output to the engine increases, switching of the combustion mode frequently occurs and drivability may be reduced. With the techniques described in Patent Documents 2 to 4, it is difficult to solve this problem.

  The present invention has been made in view of the above problems, for example, and an object of the present invention is to provide an engine control device that can suppress frequent occurrence of switching of combustion modes.

In order to solve the above problems, an engine control device of the present invention is an engine control device mounted on a vehicle including an engine that can be operated by switching a plurality of combustion modes according to a combustion region. Due to the change in the accelerator operation amount, the current combustion mode of the engine is changed to the combustion mode corresponding to the second combustion region not adjacent to the first combustion region corresponding to the current combustion mode. The combustion mode corresponding to the third combustion region adjacent to the first combustion region and located between the first combustion region and the second combustion region from the current combustion mode , into the combustion mode corresponding to the second combustion region, than the time to change the operating state of the engine, from the current combustion mode, directly into the combustion mode corresponding to the second combustion zone If the time for changing the operating state is short, a control unit for the operating conditions, and controls the engine so that the unchanged from the current combustion mode to the combustion mode corresponding to the third combustion area.

  According to the engine control apparatus of the present invention, the engine control apparatus is mounted on a vehicle including an engine that can be operated by switching a plurality of combustion modes according to a combustion region. Here, the “combustion region” is predetermined by a map or the like for controlling the engine, for example, defined by the engine speed and the engine torque. The combustion mode is determined according to the combustion region to which the current operating state of the engine (for example, engine torque, engine speed, etc.) corresponds.

  The engine control device controls the operating state of the engine so that, for example, the fuel efficiency of the engine becomes good, according to the accelerator operation amount (for example, accelerator opening) related to the vehicle. At this time, the engine control device appropriately changes the combustion mode in accordance with the combustion region corresponding to the operating state of the engine.

The control means of the engine control device causes the engine to change from a current combustion mode to a second combustion region that is not adjacent to the first combustion region corresponding to the current combustion mode, due to a change in the accelerator operation amount related to the vehicle. When changing to the corresponding combustion mode, the following processing is performed. That is, the control unit, via a combustion mode corresponding to the third combustion area located between (i) the current combustion mode, as well as adjacent to the first combustion region, the first combustion zone and a second combustion region Te, the combustion mode corresponding to the second combustion region, the time and changing the operating state of the engine, from (ii) the current combustion mode, directly into the combustion mode corresponding to the second combustion region, to change the operating conditions Ask for time.

Subsequently, the control means directly from the current combustion mode, rather than the time to change from the current combustion mode to the combustion mode corresponding to the second combustion region via the combustion mode corresponding to the third combustion region. When the time for changing to the combustion mode corresponding to the second combustion region is short, the engine is controlled so that the operating state of the engine is not changed from the current combustion mode to the combustion mode corresponding to the third combustion region.

  If comprised in this way, it can suppress that switching of a combustion mode generate | occur | produces frequently, and the fall of drivability can be prevented.

Note that the current combustion mode is changed directly from the current combustion mode to the second combustion region through the combustion mode corresponding to the third combustion region, rather than the time for changing to the combustion mode corresponding to the second combustion region. When the time to change to the corresponding combustion mode is long, the control unit typically changes the combustion mode in accordance with the transition of the combustion region accompanying the transition of the operating state of the engine. If comprised in this way, the improvement of a fuel consumption can be aimed at, for example, and it is very advantageous practically.

  The effect | action and other gain of this invention are clarified from the form for implementing demonstrated below.

It is a conceptual diagram which shows the structure of the hybrid vehicle which concerns on embodiment. It is an example of a combustion mode map in which the horizontal axis represents the engine speed and the vertical axis represents the engine torque. It is an example of a required drive torque map. It is an example of a request drive power map. It is a flowchart which shows the engine control process which concerns on embodiment.

  An embodiment according to an engine control device of the present invention will be described with reference to the drawings.

(Configuration of hybrid vehicle)
First, the structure of the hybrid vehicle which concerns on embodiment is demonstrated with reference to FIG. FIG. 1 is a conceptual diagram illustrating a configuration of a hybrid vehicle according to an embodiment.

  In FIG. 1, the hybrid vehicle 1 includes an engine 10 and motor / generators MG1 and MG2 connected to the engine 10 via a power distribution mechanism 14, respectively. The motor / generator MG1 is mainly used for control of the engine 10 and power generation. On the other hand, motor generator MG2 is mainly used for driving hybrid vehicle 1 and for regenerative braking.

  The power distribution mechanism 14 includes a planetary gear mechanism. The crankshaft of the engine 10 is connected to the carrier of the planetary gear mechanism. The rotation shaft of the motor / generator MG1 is connected to the sun gear of the planetary gear mechanism. The rotation shaft of the motor / generator MG2 is connected to an output shaft that outputs the rotational power of the ring gear of the planetary gear mechanism.

  An intake passage 11 and an exhaust passage 12 are connected to the engine 10. In the intake passage 11, an air flow meter 21, an intake throttle valve 22, a compressor 23 c of a turbocharger 23 and an intercooler 24 are provided. In the exhaust passage 12, a turbine 23 t of the turbocharger 23, a start converter 25 and an aftertreatment device 26 are provided.

  The engine 10 is further provided with a low pressure EGR device that recirculates a part of the exhaust gas flowing in the exhaust passage 12 to the intake passage 11 at a low pressure. The low pressure EGR device communicates the downstream side of the start converter 25 in the exhaust passage 12 and the upstream side of the aftertreatment device 26 with the downstream side of the intake throttle valve 22 and the upstream side of the compressor 23c in the intake passage 11. A passage 13 is provided. The low pressure EGR passage 13 is provided with an EGR cooler 17 and an EGR valve 28.

  The hybrid vehicle 1 further includes an engine ECU (Electronic Control Unit) 32 that controls the engine 10, an MGECU 33 that controls the motor generators MG 1 and MG 2, and outputs of various sensors provided in the hybrid vehicle 1. And the HVECU 31 that controls the engine ECU 32 and the MGECU 33 in an integrated manner.

(Engine operation)
Next, the operation of the engine 10 will be described with reference to FIG. FIG. 2 is an example of a combustion mode map in which the horizontal axis represents the engine speed and the vertical axis represents the engine torque.

  As shown in FIG. 2, the engine 10 according to the embodiment has various powers required for the engine 10 (for example, an engine torque command value) (hereinafter, referred to as “engine required power” as appropriate). Take the combustion mode. The engine ECU 32 basically controls the engine 10 so that the operating point of the engine 10 transitions along, for example, an operation line a (see solid line a) that is a fuel efficiency optimum line according to the engine required power. To do. At this time, the combustion mode is appropriately switched according to the position of the operating point of the engine 10 on the combustion mode map. If comprised in this way, a fuel consumption can be improved and it is very advantageous practically.

  Here, since various known modes can be applied to the method for switching the combustion mode of the engine 10, a detailed description thereof will be omitted.

  In FIG. 2, “NA stoichiometric”, “NA lean”, “supercharged lean” and “supercharged stoichiometric” are respectively “non-supercharged stoichiometric combustion mode”, “non-supercharged lean combustion mode”, “ It means “supercharging lean combustion mode” and “supercharging stoichiometric combustion mode”. Moreover, the broken line in FIG. 2 has shown the equal power curve.

(Engine control processing)
Next, engine control processing according to the embodiment will be described with reference to FIGS. 3 to 5.

  The HVECU 31 determines the power required for the hybrid vehicle 1 according to the vehicle speed, the accelerator opening, the engine speed, the speed of each of the motor / generators MG1 and MG2, the state of charge of a battery (not shown), etc. (Referred to as “vehicle required power”).

  The HVECU 31 further determines a travel mode (for example, a so-called EV (Electric Vehicle) travel mode, a so-called HV (Hybrid Vehicle) travel mode, etc.) based on the set vehicle required power, and for example, engine required power, The required power of each of the motor generators MG1 and MG2, the presence / absence of a shift change, etc. are determined.

  As described above, the engine ECU 32 controls the engine 10 so that the operating point of the engine 10 changes along a predetermined operation line in accordance with the determined required engine power. The MGECU 33 controls the motor generators MG1 and MG2 according to the determined required power (for example, a motor torque command value or the like).

  Specifically, for example, the HVECU 31 stores in advance a required drive torque map defined by the propeller shaft speed and the required drive torque, which is set for each accelerator opening, for example, as shown in FIG. The HVECU 31 adds a loss power to the product of the required drive torque and the propeller shaft rotational speed in the required drive torque map, for example, a request defined by the propeller shaft rotational speed and the required drive power as shown in FIG. The drive power map is obtained sequentially.

  When the driver of the hybrid vehicle 1 depresses the accelerator, the HVECU 31 performs a requested drive from the propeller shaft speed, the accelerator opening Pap (see the black circle a in FIG. 4) and the accelerator opening change rate δPap at the start of the accelerator depression. The power change rate δPv (corresponding to the arrow between the black circles a and b in FIG. 4) is calculated.

  Here, in this embodiment, it is assumed that the power of the engine 10 does not change abruptly except when the driver changes the demand (that is, when the accelerator opening changes), and the HVECU 31 calculates the calculated required drive power change rate. δPv is substituted for the engine required power change rate δPe. Subsequently, the HVECU 31 arrives at the operating point of the engine 10 (ie, the engine required power) on the combustion mode map (see FIG. 2) based on the product of the engine required power change rate δPe and the accelerator depression time. Predict.

  Here, for example, when the accelerator is depressed at the operating point p0 in FIG. 2 and the operating point of the engine 10 reaches the combustion region corresponding to the non-supercharged stoichiometric combustion mode (that is, between the operating point p2 and the operating point p3). Assume that it was predicted.

  The HVECU 31 calculates the engine required power Pe_Start at the operating point p0 and the lower limit value of the engine required power related to the combustion mode on the higher power side than the operating point P0. Here, the HVECU 31 has a lower limit value Pe_Turbo-Lean (corresponding to the operating point p1) of the engine required power related to the supercharged lean combustion mode and a lower limit value Pe_NA-Stoiki of the engine required power related to the non-supercharged stoichiometric combustion mode (operation). And a lower limit value Pe_Turbo-Stoiki (corresponding to the operating point p3) of the engine required power related to the supercharged stoichiometric combustion mode.

  When the operating point of the engine 10 when the accelerator is depressed is in the combustion region corresponding to the supercharged lean combustion mode, the HVECU 31 calculates the lower limit value Pe_NA-Stoiki and the lower limit value Pe_Turbo-Stoiki.

  Next, the HVECU 31 calculates the difference between the lower limit value Pe_Turbo-Lean, the lower limit value Pe_NA-Stoiki and the lower limit value Pe_Turbo-Stoiki and the engine required power Pe_Start, and calculates the calculated difference as the engine required power change rate δPe. Divide.

  Accordingly, (i) the predicted time T_Turbo-Lean = ((Pe_Turbo-Lean)-(Pe_Start)) / δPe for switching from the non-supercharged lean combustion mode to the supercharged lean combustion mode, and (ii) the non-supercharged lean Prediction time T_NA-Stoiki = ((Pe_NA-Stoiki)-(Pe_Start)) / δPe for switching from the combustion mode to the non-supercharged stoichiometric combustion mode, and (iii) from the non-supercharged lean combustion mode to the supercharged stoichiometric combustion mode Predicted time T_Turbo-Stoiki = ((Pe_Turbo-Stoiki)-(Pe_Start)) / δPe for switching is obtained.

  Next, the HVECU 31 determines (i) the predicted time T_NA-Stoiki when switching directly from the non-supercharged lean combustion mode to the non-supercharged stoichiometric combustion mode, and (ii) the supercharged lean from the non-supercharged lean combustion mode. The time required for switching to the non-supercharged stoichiometric combustion mode via the combustion mode is compared with the sum of the time determined in advance according to the drivability requirements such as the engine water temperature and the outside air temperature.

  Here, “the time required to switch from the non-supercharged lean combustion mode to the non-supercharged stoichiometric combustion mode via the supercharged lean combustion mode” is the “supercharged lean combustion mode to supercharged lean combustion mode”. It means the sum of the time required to switch to and the time required to switch from the supercharged lean combustion mode to the non-supercharged stoichiometric combustion mode.

  The time required for the predicted time T_NA-Stoiki to switch from the non-supercharged lean combustion mode to the non-supercharged stoichiometric combustion mode via the supercharged lean combustion mode, and drivability such as engine water temperature and outside air temperature, for example When the HVECU 31 is shorter than the sum of the predetermined time due to the requirements relating to the above, the HVECU 31 causes the engine 10 to be switched via the engine ECU 32 so as to switch directly from the non-supercharged lean combustion mode to the non-supercharged stoichiometric combustion mode. (I.e., control is performed so that the engine 10 is not switched to the supercharged lean combustion mode).

  On the other hand, the estimated time T_NA-Stoiki is the time required for switching from the non-supercharged lean combustion mode to the non-supercharged stoichiometric combustion mode via the supercharged lean combustion mode, for example, the engine water temperature, the outside air temperature, etc. When longer than the sum of the predetermined time due to the requirements relating to drivability, the HVECU 31 controls the engine 10 via the engine ECU 32 so that the combustion mode of the engine 10 is switched according to the combustion mode map.

  For example, when the so-called power mode switch or the so-called sports mode switch is ON or the manual shift mode is used, the time required by the drivability requirement is determined by the driver requesting vehicle responsiveness. If it is, it is set relatively long. On the other hand, when the driver does not request vehicle responsiveness, for example, when a so-called snow mode switch or eco mode switch is ON, the time predetermined by the drivability requirement is set to be relatively short. Is done.

  Alternatively, for example, when the load factor related to the motor / generator MG1 or MG2 is limited, or when the battery output is limited, it is difficult to compensate for torque fluctuation at the time of switching the combustion mode. The predetermined time is set to be relatively long according to the requirements relating to the above.

  Next, engine control processing that is mainly performed by the HVECU 31 while the hybrid vehicle 1 is traveling will be described with reference to the flowchart of FIG. 5.

  In FIG. 5, first, the HVECU 31 calculates the engine required power change rate δPe as described above (step S101).

  Next, as described above, the HVECU 31 predicts the arrival point of the operating point of the engine 10 and predicts when the current combustion mode is directly switched to the combustion mode corresponding to the combustion region in which the predicted arrival point corresponds. Time (here, predicted time T1) is calculated (step S102).

  In parallel with or before or after the process of step S102, the HVECU 31 adds the time required for switching the combustion mode according to the combustion mode map and the time determined in advance according to the drivability requirement as described above. (Here, the sum T2) is calculated (step S103).

  Next, the HVECU 31 determines whether or not the predicted time T1 is shorter than the sum T2 (step S104). When it is determined that the predicted time T1 is shorter than the sum T2 (step S104: Yes), the HVECU 31 directly switches from the current combustion mode to the combustion mode corresponding to the combustion region in which the predicted arrival point corresponds. Then, the engine 10 is controlled via the engine ECU 32 (step S105).

  On the other hand, when it is determined that the predicted time T1 is longer than the sum T2 (step S104: No), the HVECU 31 controls the engine 10 via the engine ECU 32 so as to switch the combustion mode according to the combustion mode map (step S106). ).

  The “HV ECU 31” and the “engine ECU 32” according to the embodiment are examples of the “engine control device” and the “control unit” according to the present invention. The “non-supercharged lean combustion mode”, “non-supercharged stoichiometric combustion mode”, and “supercharged lean combustion mode” according to the embodiment are respectively “current combustion mode” and “second combustion region” according to the present invention. It is an example of "corresponding combustion mode" and "combustion mode corresponding to the third combustion region".

  The present invention is not limited to the above-described embodiments, and can be changed as appropriate without departing from the scope or spirit of the invention that can be read from the claims and the entire specification. Is also included in the technical scope of the present invention.

  DESCRIPTION OF SYMBOLS 1 ... Hybrid vehicle, 10 ... Engine, 31 ... HVECU, 32 ... Engine ECU, 33 ... MGECU, MG1, MG2 ... Motor generator

Claims (1)

An engine control device mounted on a vehicle including an engine that can be operated by switching a plurality of combustion modes according to a combustion region,
Due to a change in accelerator operation amount related to the vehicle, the current combustion mode of the engine is changed to a combustion mode corresponding to a second combustion region that is not adjacent to the first combustion region corresponding to the current combustion mode. When the operation is performed, the current combustion mode passes through the combustion mode corresponding to the third combustion region that is adjacent to the first combustion region and located between the first combustion region and the second combustion region. The operation state is changed from the current combustion mode directly to the combustion mode corresponding to the second combustion region rather than the time for changing the operation state of the engine to the combustion mode corresponding to the second combustion region. Control means for controlling the engine so that the operation state is not changed from the current combustion mode to the combustion mode corresponding to the third combustion region when the time for changing is short. Engine control device, characterized in that.

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