JPH062587A - Fuel control device for engine - Google Patents

Abstract

PURPOSE:To improve exhaust gas purifying performance and drivability by calculating a basic fuel injection amount, correcting a change amount of intake pipe pressure to obtain a correction intake pipe pressure change amount at the time of acceleration or deceleration, adding or subtracting a fuel injection correction amount calculated from this correction intake pipe pressure change amount, and properly providing air-fuel ratio. CONSTITUTION:Volumetric efficiency is calculated from outputs of an intake pipe pressure sensor 101 and a crank angle sensor 102, and a basic fuel injection amount is calculated in a basic fuel injection amount calculating means 104. 0n the other hand, a pressure change amount correction coefficient is calculated in a pressure change amount correction coefficient calculating means 109 based on a change rate of a throttle opening from an output of a throttle position sensor 108, and a fuel injection correction amount is calculated in a fuel correction amount calculating means 112 through an intake pipe pressure change amount correcting means 111. This fuel injection correction amount is added to or subtracted from the basic fuel injection amount, to calculate a fuel injection amount in accordance with the actual intake air amount. Thus, operation is performed by proper air-fuel ratio, to improve exhaust gas purifying performance and drivability.

Description

Detailed Description of the Invention

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a fuel control device for an engine, and is to correct the fuel amount during acceleration or deceleration of the engine.

[0002]

2. Description of the Related Art In engines, particularly gasoline engines, gasoline injection measures the amount of air taken into the engine, supplies an appropriate amount of gasoline, and controls the mixture ratio (air-fuel ratio) of this air and gasoline. . In this case, there is a speed density method among the air amount detection methods. This speed density system estimates the amount of air taken into the engine per cycle from the engine speed and the intake pipe pressure, and calculates the injection amount of gasoline based on the estimated amount of air.

FIG. 15 is a graph showing the relationship among the intake air amount and the intake pipe pressure, the internal EGR, and the combustion chamber wall surface temperature during acceleration of the engine, and FIG. 16 is the intake pipe pressure and its change amount.
The graph which shows the relationship of a fuel injection amount is shown.

As shown in FIG. 15, at the time of acceleration of the engine, the amount of air actually taken in is larger than the amount of air obtained by calculation based on the intake pipe pressure and the engine speed. There is. And, in fact, it rises earlier than the intake pipe pressure, and slightly overshoots in the middle.

Further, during acceleration, the wall temperature of the combustion chamber rises later than the intake pipe pressure, so it is lower than the wall temperature in the steady state. Therefore, since the temperature of the intake air does not rise due to the wall surface temperature, the filling efficiency increases. On the other hand, since the back pressure is low at the initial stage of acceleration, the internal EGR is small, and the air filling efficiency is increased as described above. Further, when the throttle valve is suddenly opened, the pressure in the intake pipe rises and the boiling point of the fuel rises, so that the amount of fuel adhering to the wall surface of the intake pipe increases. As a result, the air-fuel ratio (A /
F) becomes lean.

As described above, in a transient state such as during acceleration of the engine, the intake air amount calculated from the intake pipe pressure does not match the actual intake air amount. Must be done. Conventionally, the correction of the fuel amount in the transient state of the engine is performed based on the change amount (ΔPb) of the intake pipe pressure (Pb). That is, as shown in FIG. 16, the air amount is obtained based on the intake pipe pressure and the engine speed, and the basic fuel injection amount is calculated from this air amount, while the basic fuel injection amount is measured during a transient period or every predetermined number of strokes. The total fuel injection amount is calculated by calculating the corrected fuel injection amount during the transition from the amount of change in the intake pipe pressure and adding this corrected fuel injection amount to the basic fuel injection amount.

[0007]

A conventional engine fuel control apparatus for calculating a total fuel injection amount by obtaining a corrected fuel injection amount during a transition based on the intake pipe pressure change amount (ΔPb) as described above. If so, the above-mentioned wall temperature and internal EG
Due to the influence of R and the adhered fuel, the correction of the fuel amount according to the transient state of the engine was insufficient. However, as shown in FIG. 17, if the amount of fuel is simply increased by a predetermined amount in the initial stage of acceleration, the amount of fuel may be increased more than necessary, such as during slow acceleration, and the engine cannot be operated at an appropriate air-fuel ratio. .

Further, in the conventional engine fuel control device, when detecting whether or not the engine is accelerated from the change state of the intake pipe pressure, the change amount of the intake pipe pressure exceeds a preset reference value. When it is determined that acceleration is present, the fuel injection amount is increased. This reference value should be set as small as possible in order to properly perform the transient fuel correction. However, in certain operating conditions, if the reference value is small, acceleration / deceleration determination may fail.

The present invention solves such a problem, and by making the fuel correction amount variable according to the degree of transition and the continuation state, it is possible to perform an appropriate fuel correction, thereby making the exhaust gas purification performance and drivability. It is an object of the present invention to provide a fuel control device for an engine, which is improved.

[0010]

To achieve the above object, an engine fuel control apparatus of the present invention is provided with an intake pipe pressure sensor for detecting a pressure in an intake pipe of an engine and a crank angle for detecting an engine speed. A sensor, basic fuel injection amount calculation means for calculating a basic fuel injection amount during steady operation of the engine based on the outputs of the intake pipe pressure sensor and the crank angle sensor, and an intake pipe based on the output of the intake pipe pressure sensor. An intake pipe pressure change amount calculating means for calculating the pressure change amount, a throttle position sensor for detecting the throttle opening, and a pressure change amount based on the throttle opening change rate calculated from the output of the throttle position sensor. Pressure change amount correction coefficient setting means for setting a correction coefficient, and acceleration / deceleration continuous state detection means for detecting an acceleration / deceleration continuous state of the engine. Intake pipe pressure change amount correcting means for correcting the intake pipe pressure change amount based on the outputs of the pressure change amount correction coefficient setting means and the acceleration / deceleration continuous state detecting means, and calculating a corrected intake pipe pressure change amount, Fuel correction amount calculation means for calculating the fuel injection correction amount based on the corrected intake pipe pressure change amount, and fuel injection for calculating the total fuel injection amount based on the outputs of the basic fuel injection amount calculation means and the fuel correction amount calculation means It is characterized in that it comprises an amount calculation means.

[0011]

The intake pipe pressure sensor measures the intake pipe pressure, the crank angle sensor measures the engine speed, and the basic fuel injection amount is calculated based on each measured value. On the other hand, when the engine is accelerated by correcting the amount of change in the intake pipe pressure for each predetermined time or the number of predetermined strokes in accordance with the pressure change amount correction coefficient based on the change rate of the throttle opening and the continuous state of acceleration / deceleration,
Alternatively, the corrected intake pipe pressure change amount during deceleration is obtained, and the fuel injection correction amount during transient engine operation is calculated based on the corrected intake pipe pressure change amount. Then, the fuel injection correction amount is added to or subtracted from the basic fuel injection amount to calculate the fuel injection amount according to the actual intake air amount.

[0012]

Embodiments of the present invention will now be described in detail with reference to the drawings.

FIG. 1 is a block diagram showing a schematic structure of an engine fuel control apparatus according to an embodiment of the present invention, FIG. 2 is a schematic diagram of an engine system, FIG. 3 is a block diagram showing hardware of an engine control system, and FIG. Intake pipe pressure and its change,
A graph showing the relationship between the acceleration correction amount and the fuel injection amount, FIG. 5 is a flow chart of a main routine showing fuel control, FIG. 6 is a time chart of intake pipe pressure data acquisition, FIG. 7 is a flow chart of a crank interrupt routine, and FIG. Through FIG.
FIG. 12 is a flowchart showing the calculation of the transient correction amount, FIG. 12 is a graph showing the upper limit value of the amount of change in intake pipe pressure with respect to engine speed, FIG. 13 is a graph showing the acceleration increase emphasis coefficient with respect to throttle speed, and FIG. 6 is a graph showing a dead zone region based on the graph.

The engine fuel control system of the present invention is shown in FIG.
As shown in, the intake pipe pressure sensor 101 that detects the pressure in the intake pipe of the engine, the crank angle sensor 102 that detects the engine speed, and the volume efficiency based on the outputs of the intake pipe pressure sensor 101 and the crank angle sensor 102. Volume efficiency calculation means 103 for calculating
Basic fuel injection amount calculation means 104 for calculating the basic fuel injection amount during steady operation of the engine based on the output of 03.
And an intake pipe pressure change amount calculation means 10 for calculating the amount of change in the intake pipe pressure based on the output of the intake pipe pressure sensor 101.
5, an upper limit comparison setting unit 106 for comparing the output of the intake pipe pressure change amount calculation unit 105 with an upper limit value of the intake pipe pressure change amount preset according to the engine speed, and an upper limit comparison setting unit. The output of 106 and the dead zone comparison means 107 for comparing with the dead zone value of the intake pipe pressure change amount preset according to the engine cooling water temperature, the throttle position sensor 108 for detecting the throttle opening, and the output of the throttle position sensor 108. Pressure change amount correction coefficient calculation means 109 for calculating the pressure change amount correction coefficient based on the change rate of the throttle opening calculated from the above, and acceleration / deceleration continuous state detection means 110 for detecting the continuous state of acceleration / deceleration of the engine.
And an intake pipe pressure change amount correction unit for calculating a corrected intake pipe pressure change amount during transient operation of the engine based on the outputs of the dead zone comparison unit 107, the pressure change amount correction coefficient calculation unit 109, and the acceleration / deceleration continuous state detection unit 110. 111, a fuel correction amount calculation unit 112 that calculates a fuel injection correction amount based on the output of the intake pipe pressure change amount correction unit 111, a basic fuel injection amount calculation unit 104, and a fuel correction amount calculation unit 11
The fuel injection amount calculation means 113 calculates the total fuel injection amount based on the output of 2.

First, the schematic construction of the engine of this embodiment will be described. As shown in FIG. 2, the engine 10 is provided with an intake port 11 and an exhaust port 12, and an intake valve 13
Also, it can be opened and closed by the exhaust valve 14. A piston 17 is connected to the crankshaft 15 via a connecting rod 16 and is supported in the cylinder so as to be vertically movable. A combustion chamber 18 is formed above the piston 17, and a spark plug 19 is attached to the combustion chamber 18.

The air cleaner 20 is for removing floating dust in the intake air, and is connected to the surge tank 22 and the intake port 11 of the engine 10 by an intake pipe 21. A throttle valve 23 and a throttle position sensor 24 are provided on the surge tank 22 side of the intake pipe 21, and a bypass passage 25 and an idle speed control (ISC) valve (idle switch) 26 are provided. Also,
The surge tank 22 is provided with a vacuum sensor 27 as an intake pipe pressure sensor and an intake air temperature sensor 28.

The throttle position sensor 24
The vacuum sensor 27 and the intake air temperature sensor 28 are connected to an engine control unit (ECU) 29 so that the detection result can be output to the ECU 29. The ISC valve 26 is also connected to the ECU 29,
It can operate based on a command from the ECU 29. Further, an injector 30 is attached to each intake cylinder 11 of the engine 10 for each cylinder.
The injector 30 is connected to a fuel tank via a fuel pressure regulator (not shown), and can inject a predetermined amount of gasoline stored in the fuel tank based on a command from the ECU 29.

An exhaust pipe is provided at the exhaust port 12 of the engine 10.
31 is connected and O ₂Sensor 32 and touch
A medium converter (three-way catalyst) 33 is mounted. That
O this₂The sensor 32 is connected to the ECU 29,
The detection result can be output to the ECU 29.
Further, the engine 10 has a water temperature sensor 3 for the engine cooling water.
4 is provided, and further, the distribution of the engine 10
A crank angle sensor 35 (cylinder discrimination sensor) is installed in the
The crank angle sensor 35 is attached to the ECU 29.
It is possible to output the detection result to the ECU 29.
Growling.

The air sucked from the air cleaner 20 is sent to the surge tank 22 via the intake pipe 21,
Then, it is supplied to the intake port 11 of the engine 10.
At this time, the throttle valve 23 controls the intake air amount. On the other hand, the ECU 29 uses the vacuum sensor 27.
Intake pipe pressure detected by the crank angle sensor 35
The fuel injection amount is calculated from the engine speed detected by, and the injector 30 is driven for a predetermined time based on a command from the ECU 29 to inject a predetermined amount of gasoline. Therefore, a mixture of air and gasoline is supplied into the combustion chamber 18.

Air-fuel mixture is supplied from the intake port 11 into the combustion chamber 18, the piston 17 moves up and down by the drive of the crankshaft 15, the air-fuel mixture inside the combustion chamber 18 is compressed, and the spark plug 19 produces sparks. As a result, the compressed air-fuel mixture explodes and expands to operate the engine.
Then, the exhaust gas generated by the combustion of the air-fuel mixture is exhausted from the exhaust port 12 to the exhaust pipe 31, purified by the catalytic converter 33 and released to the atmosphere.

The ECU 29 has a signal from a battery sensor 50 for detecting the voltage of the battery 49 and an ignition switch (key switch) 36 in addition to the above-mentioned sensors.
Signal from the knock sensor 37 and the signal from the knock sensor 37 are input (see FIG. 3).

The hardware configuration of the ECU 29 is as follows.
As shown in FIG. 3, the ECU 29 is provided with a CPU 38 as its main part, and the CPU 38 is provided with an intake air temperature sensor 28, a knock sensor 37, a throttle position sensor 24, an O ₂ sensor 32, a water temperature sensor 34, and a battery sensor 50. The detection signal from the input interface 3
9 and the A / D converter 40, the detection signals from the idle switch 26 and the ignition switch 36 are input through the input interface 41, and the detection signal from the vacuum sensor 27 is input through the input interface 42. Also, the detection signal from the crank angle sensor 35 (cylinder discrimination sensor) is directly input to the input port.

Further, the CPU 38 stores, via a bus line, program data for various controls, preset fixed value data and a ROM 43 for storing data maps.
Data content rewritable RAM 44 and battery 49
BURAM retains stored contents during connection
Data is exchanged with 45.

Focusing solely on the fuel injection control, a fuel injection amount control signal calculated mainly based on a program described later is output from the CPU 38 to the injector 30 via the driver 46, and the injector 30 of each cylinder is driven. It is designed to be driven sequentially according to the phase. Further, this control signal is sent from the CPU 38 to the driver 4
7 to the fuel pump relay 48.

The fuel injection amount control signal is the injector 30 corresponding to the basic fuel injection amount calculated according to the intake air amount.
It is designed to be obtained by adding various correction data according to the operating condition to the basic drive time data of the. A main routine that is obtained in a crank interrupt routine that is executed by using the crank angle signal from the sensor 35 as a trigger, and on the other hand, that of the correction data that changes relatively slowly is always executed when there is no program execution due to an interrupt. Sought in.

That is, in the engine fuel control system of this embodiment, as shown in FIG.
For example, if the intake pipe pressure Pb rises during acceleration,
The change amount ΔPb per the predetermined number of strokes is calculated, and the corrected fuel injection amount is calculated according to the change amount ΔPb, and
The corrected fuel injection amount is further increased in the initial stage of acceleration.

The main routine and crank interrupt routine of the engine fuel control of this embodiment will be described below. As shown in FIG. 5, in the main routine,
After the ignition switch is turned on, initialization (initialization) is performed in step M1, and engine operating conditions (engine speed N
e, intake pipe pressure Pb, engine cooling water temperature WT, battery voltage V, intake pipe pressure change amount ΔPb, etc.) are input. Then, in step M3, the amount of change ΔPb in the intake pipe pressure is larger than the acceleration dead zone, or −ΔPb
Is larger than the deceleration dead zone, that is, whether the fuel injection amount should be corrected (increased or decreased). Then, when it is not necessary to make a correction, the process proceeds to step M4, and the volume efficiency K _MAP is set based on the engine speed Ne and the average value Pb _mean (n) of the intake pipe pressure Pb for each predetermined stroke number. When it is necessary to make a correction in step M3, the process proceeds to step M5, and the volumetric efficiency K is calculated based on the engine speed Ne and the intake pipe pressure Pbi (n) immediately before injection.
Set the _MAP . After setting the volume efficiency K _MAP ,
In step M6, each correction coefficient (intake correction coefficient K _AT , other correction coefficient K _ELSE , dead time T _D, etc.) is set.

Data acquisition of the intake pipe pressure Pb will be described with reference to a time chart. As shown in FIG. 6, the cylinder discrimination signal (SGC) from the crank angle sensor 35.
And a cylinder injection signal (SGT) are output, and the injector 38 of each cylinder (four cylinders in this embodiment) is output from the CPU 38.
The drive signal is output to. On the other hand, the vacuum sensor 27
Detects A / D conversion of the intake pipe pressure Pb every predetermined time. Then, the signal in the normal operation state of the engine flows as shown by the solid line arrow in FIG. 6, and the average value Pb _mean (n) of the intake pipe pressure Pbi (n) between the two strokes is taken as data, and the volume efficiency is taken. Calculate K _MAP . on the other hand,
The signal in the transient state of the engine flows as shown by a dotted arrow in FIG. 6, and the A / D value Pbi of the intake pipe pressure immediately before the injection is obtained.
(N) is taken in as data and the volumetric efficiency K _MAP is calculated.

Next, the crank interrupt routine will be described. As shown in FIG. 7, in step C1, the average value Pb _mean (n) of the intake pipe pressure for each predetermined number of strokes is calculated. That is, when the A / D value of the intake pipe pressure detected by the vacuum sensor 27 for each predetermined time is Pbi and the number of data taken in is m, it is calculated by the following formula 1.

[Equation 1] Then, in step C2, the transient fuel correction amount is calculated. That is, the acceleration fuel correction amount Q _ACC when the engine is in the accelerating state is the conversion coefficient of the intake pipe pressure change-the discharge amount is XK.
Q, the water temperature correction coefficient at the time of acceleration is K _AC WT, and the value of the corrected pressure change amount is DPB.

[Formula 2] Q _ACC = XKQ × K _AC WT × DPB (n) Also, the deceleration fuel correction amount Q when the engine is in the deceleration state.
_DCC is calculated by the following mathematical formula 3 when the water temperature correction coefficient at the time of deceleration is K _DC WT.

[Expression 3] Q _DCC = XKQ × K _DC WT × DPB (n)

In step C3, it is determined whether the amount of change in intake pipe pressure ΔPb (-ΔPb) is larger or smaller than the dead zone, that is, whether fuel correction should be performed. If no correction is necessary, step C4 is entered. If correction is required, the process proceeds to step C5. And step C
In 4, the basic fuel injection amount Q _B is calculated based on the average value Pb _mean (n), and in step C5, the basic fuel injection amount Q _B is calculated based on the intake pipe pressure Pbi (n) immediately before the injection.

That is, the basic fuel injection amount Q _B supplied to the normal operating state of the engine is such that the conversion coefficient of the intake pipe pressure-fuel injection amount is XKQPLS, the volumetric efficiency is K _MAP , the intake temperature correction coefficient K _AT , and other factors. The correction coefficient K _ELSE is calculated by the following mathematical formula 4.

Equation 4] The _{Q B = XKQPLS × Pb mean (} n) × K MAP × K AT × K ELSE, the basic fuel injection amount Q _B to be supplied to the transient operating condition of the engine is calculated by the following formula 5.

[Equation 5] Q _B = XKQPLS × Pbi (n) × K _MAP × K _AT × K _ELSE

In step C6, the calculated basic fuel
Injection amount Q_BAnd acceleration fuel correction amount Q _ACC, Deceleration fuel correction
Quantity Q_DCCCalculate the total fuel injection amount Q from
To do.

[Equation 6] Q = Q _B + Q _ACC + Q _DCC

Subsequently, in step C7, the injector drive time T _INJ is calculated from the following formula 7 from the fuel injection amount Q, where the discharge amount-drive time conversion coefficient is XK _INJ and the dead time is T _D.

[ _Equation 7] T _INJ = Q × XK _INJ + T _D

Then, in step C8, the injector drive time data T _INJ is set in the driver 46, and when the driver 46 is triggered in step C9, the injector 30 is opened for the time corresponding to the drive time data T _INJ. Fuel is supplied to the engine 10.

Now, the calculation of the transient fuel correction amount will be described. As shown in FIG. 8, in step S1, the intake pipe pressure is detected by the vacuum sensor 27, and in the case of a four-cylinder engine, the change amount ΔPb of the intake pipe pressure Pb for every four strokes of the engine is calculated by the following formula 8. .

## EQU00008 ## .DELTA.Pb = Pbi (n) -Pbi (n-4) Note that the amount of change .DELTA.Pb in the intake pipe pressure is calculated for each cylinder. That is, the change amount ΔPb corresponds to the difference between the intake pipe pressure immediately before the current injection and the intake pipe pressure immediately before the previous injection in the same cylinder. In the present embodiment, the correction fuel injection amount is increased according to the value of this change amount ΔPb, but at the initial stage of rapid acceleration, the correction fuel injection amount is too large according to this change amount ΔPb, and the air-fuel ratio is kept appropriate. I can't. Therefore, in step S2, the upper limit value is applied to the value of the change amount ΔPb. Then, this upper limit value is obtained by the map shown in FIG.

As shown in FIG. 12, the data map of the acceleration increase pressure change amount upper limit value is obtained by a graph of the upper limit value with respect to the engine speed Ne. Then, the upper limit value becomes higher as the engine speed becomes lower, decreases as the engine speed becomes higher, and becomes constant at a predetermined engine speed.

Therefore, in step S2, the change amount ΔPb of the intake pipe pressure is compared with the upper limit value obtained from the map, and if the change amount ΔPb is less than or equal to the upper limit value, step S2 is performed.
If it is equal to or more than the upper limit value, ΔPb = upper limit value is taken in in step S3 and the data is taken in, and the process proceeds to step S4. In step S4, it is determined whether or not this change amount ΔPb is in the acceleration dead zone, and it is compared and determined with the previously obtained corrected intake pipe pressure change amount value DPB (n-1).

This acceleration dead zone is a value set in terms of exhaust gas and drivability. From the perspective of exhaust gas, it is preferable that it be small in order to enable fine correction.
In terms of drivability, it is better to increase it to some extent. In this embodiment, a value preset based on the operating state (intake pipe pressure) is applied. Therefore, in this step S4, ΔPb> acceleration dead zone set value, and
If ΔPb ≧ DPB (n−1), the process proceeds to step S5. If not, the process proceeds to the tailing flowchart (FIG. 9).

In step S5, the engine cooling water temperature WT detected by the water temperature sensor 34 and the acceleration initial filling amount correction switching water temperature are compared and judged. If the engine cooling water temperature WT is equal to or higher than the acceleration initial filling amount correction switching water temperature, step S5 is performed. The process proceeds to S6. Subsequently, in step S6, the corrected intake pipe pressure change amount value DPB (n) obtained in this correction routine.
Is greater than 0, it is determined whether it is within the S stroke, and if it is within the S stroke, the process proceeds to step S7.

In step S7, the acceleration initial filling correction coefficient α is read from the map. As shown in FIG. 13, this map is a graph showing the acceleration increase amount enhancement coefficient with respect to the throttle speed (the change rate Δθ of the stoll opening), which increases from coefficient 1 as the throttle speed increases, and is constant at a predetermined value. Becomes Then, after reading the correction coefficient α, in step S8, the value DPB (n) of the current corrected intake pipe pressure change amount is calculated by the following mathematical expression 9.

DPB (n) = α × ΔPb

On the other hand, when the engine cooling water temperature WT ≧ correction switching water temperature is not satisfied in step S5, or step S6
When the corrected intake pipe pressure change amount value DPB (n) exceeds 0 and exceeds the S stroke, the process proceeds to step S9, and DPB (n) = ΔPb is not multiplied by the correction coefficient α. Then, in step S10, the acceleration fuel correction amount Q _ACC is calculated based on the above-described formula 2. That is, in the early stage of rapid acceleration with a large throttle speed, the intake pipe pressure change amount ΔPb is estimated to be large, and the acceleration fuel correction amount Q _ACC is increased.

By the way, in step S4, ΔPb>
If it is not the acceleration dead zone or ΔPb ≧ DPB (n−1), tailing is performed. As shown in FIG. 4, this tailing corrects the initial filling amount during the acceleration operation of the engine, and thereafter, it is performed to gently maintain the air-fuel ratio by gradually reducing the filling amount even after the correction period has passed. It is a thing. When the temperature is low, the temperature rise delay of the combustion chamber and the wall of the port increases, so it is necessary to lengthen the correction period. Since the tailing coefficient is <1, the number of tailing strokes must be increased to further lengthen the correction period. It corresponds.

As shown in FIG. 9, in step S11, it is determined from the map whether or not the amount of change in intake pipe pressure −ΔPb is in the deceleration dead zone. As shown in FIG. 14, the map of the deceleration dead zone is a graph of the amount of change ΔPb (a positive value) of the intake pipe pressure with respect to the engine cooling water temperature WT.
When the engine cooling water temperature WT is low, it is desirable to set a large dead zone to improve drivability. on the other hand,
At high temperatures, we want to set a small dead zone to improve the exhaust gas purification performance. Therefore, this graph is set to be smaller as the engine water temperature WT increases, and the upper side is the correction area and the lower side is the non-correction area. Therefore, if -ΔPb is in this correction region, the fuel injection amount is decelerated and reduced.

If -ΔPb> deceleration dead zone is not found in step S11, the process proceeds to step S12, and the tailing of the first stage is determined. That is, the comparison determination between the previous corrected intake pipe pressure change amount value DPB (n-1) and the tailing switching determination deviation value is performed. If DPB (n-1)> tailing deviation value, the process proceeds to step S13. Where acceleration 1
Engine cooling water temperature WT
Read from the map that represents the values for changes in. Then, in step S14, the value DPB (n) of the present corrected intake pipe pressure change amount is calculated by the following mathematical expression 10.

DPB (n) = DPB (n−1) × TKATL Then, as shown in FIG. 8, the acceleration fuel correction amount Q _ACC is calculated in step S10 described above.

In step S12, DPB (n-
1)> If it is not the tailing deviation value, the process proceeds to step S15, and the tailing of the second stage is determined. That is, in step S15, the engine cooling water temperature WT is compared with the second stage tailing cycle switching determination water temperature, and if WT ≧ tailing switching water temperature, the process proceeds to step S16.
Here, the acceleration second-stage tailing coefficient XLATL2 is read, and in step S17, the corrected intake pipe pressure change amount value DPB (n) is calculated from the following Equation 11.

DPB (n) = DPB (n-1) × XKATL2 On the other hand, if WT ≧ tailing switching water temperature is not satisfied in step S15, the process proceeds to step S18 to read the cycle of m stroke in the second acceleration tailing. In step S19, the value DPB (n) of the corrected intake pipe pressure change amount is calculated for each m strokes based on the above-described formula 11.

In step S11 described above, -ΔP
If B> deceleration dead zone, that is, if it is necessary to perform deceleration reduction, the process proceeds to step S20. Here, the value of the corrected intake pipe pressure change amount (acceleration) DPB (n) = 0 is set, and the process proceeds to step S21. To do. Then, here, the acceleration fuel correction amount Q _ACC is set to 0, and the process proceeds to the deceleration amount reduction flowchart.

During rapid deceleration of the engine, the response of the intake pipe pressure deteriorates. Further, when the throttle valve is closed suddenly, the negative pressure in the intake pipe increases, and the boiling point of the fuel drops. Then, the fuel adhering to the wall surface of the intake pipe evaporates and the air-fuel ratio becomes rich. Therefore, in order to prevent this, the reduction amount of the fuel injection amount is increased at the initial stage of deceleration.

In step S22, the change amount of the intake pipe pressure during deceleration -ΔPb and the upper limit value are compared and determined, and -ΔPb
If ≦ upper limit value, the process proceeds to step S24, but if not so, the data is taken in as −ΔPb = upper limit value in step S23, and the process proceeds to step S24. Step S
At 24, the change amount of the intake pipe pressure −ΔPb is compared with the previously obtained corrected intake pipe pressure change amount value DPB1 (n−1).

At step S24, -ΔPb ≧
If DPB1 (n-1), the process proceeds to step S25,
If not, the flow proceeds to the tailing flowchart (FIG. 11). Then, in step S25, the engine cooling water temperature WT and the deceleration initial filling amount correction switching water temperature are compared and determined, and if the engine cooling water temperature WT is equal to or higher than the deceleration initial filling amount correction switching water temperature, the process proceeds to step S26.
Subsequently, in step S26, it is determined whether or not the corrected intake pipe pressure change amount value DPB1 (n) obtained by the correction routine is greater than 0 and within the S1 stroke. If within the S1 stroke, the process proceeds to step S27. Transition.

In step S27, the deceleration initial filling correction coefficient β is read from the map. This map is a graph showing the coefficient with respect to the throttle speed (the change rate Δθ of the stotling opening) like the acceleration initial filling amount correction coefficient α, but it is omitted here. Then, after reading the correction coefficient β, in step S8, the value DPB1 of the present corrected intake pipe pressure change amount is calculated from the following mathematical expression 12.
Calculate (n).

DPB1 (n) = β × (−ΔPb)

On the other hand, when the engine cooling water temperature WT ≧ correction switching water temperature is not satisfied in step S25, or in step S25.
At 26, the value DPB1 (n) of the corrected intake pipe pressure change amount becomes 0.
If it exceeds the S1 stroke after it becomes larger, the process proceeds to step S29, and DPB1 (n) = − ΔPb is set and the correction coefficient β is not multiplied. Then, in step S30, the acceleration fuel correction amount Q _{DCC is calculated} based on the above-mentioned formula 3.
Is calculated.

By the way, in step S24, -ΔP
If b ≧ DPB1 (n−1), the process proceeds to step and tailing is performed. As shown in FIG. 11, step S
At 31, it is determined whether the variation ΔPb of the intake pipe pressure is in the acceleration dead zone. And this step S3
If ΔPb> acceleration dead zone in 1 is not satisfied, the process proceeds to step S32, and the tailing of the first stage is determined. That is, the comparison value between the previous corrected intake pipe pressure change amount value DPB1 (n-1) and the tailing switching determination deviation value is compared to determine the DPB.
If (n-1)> tailing deviation value, step S33.
Move to. Acceleration 1st stage tailing coefficient TGET
L is read from the map showing the value with respect to the change of the engine cooling water temperature WT. Then, in step S34, the value DPB1 of the present corrected intake pipe pressure change amount is calculated from the following equation 13.
Calculate (n).

DPB1 (n) = DPB1 (n−1) × TGETL Then, as shown in FIG. 8, the deceleration fuel correction amount Q _DCC is calculated in step S30 described above.

In step S32, DPB1 (n-
1)> If it is not the tailing deviation value, the process proceeds to step S35, and the tailing of the second stage is determined. That is, in step S35, the engine cooling water temperature WT and the second stage tailing cycle switching determination water temperature are compared and determined, and if WT ≧ tailing switching water temperature, the process proceeds to step S36.
Here, the acceleration second stage tailing coefficient XGETL2 is read, and in step S37, the corrected intake pipe pressure change amount value DPB1 (n) is calculated from the following equation 14.

DPB1 (n) = DPB1 (n-1) × XGETL2 On the other hand, if WT ≧ tailing switching water temperature is not satisfied in step S35, the process proceeds to step S38 to read the second deceleration tailing cycle (m1 stroke). In step S39, the corrected intake pipe pressure change amount value DPB1 (n) is calculated for each m1 stroke on the basis of the above-described formula 14.

In step S31 described above,
If ΔPB> acceleration dead zone, the process proceeds to step S40, where the current correction intake pipe pressure change amount value DPB1
(N) = 0.

As described above, in the engine fuel control system according to the present embodiment, the correction of the fuel injection amount at the time of acceleration or deceleration of the engine is performed by the change amount of the intake pipe pressure Pb for each predetermined number of strokes, that is, When performing based on the change amount ΔPb of the intake pipe pressure, in the initial stage of acceleration (deceleration), the pressure change amount correction coefficient is read from the map for the change rate of the throttle opening due to rapid acceleration (deceleration) and gentle acceleration (deceleration). Therefore, the intake pipe pressure change amount is corrected and the fuel injection correction amount is calculated. Therefore, as shown in FIG. 17A, it is possible to increase (decrease) the amount of fuel commensurate with the increased (decreased) air amount in the initial stages of sudden acceleration (deceleration) and gentle acceleration (deceleration) of the engine, and it is appropriate. It can be operated with a wide air-fuel ratio.

[0056]

As described above in detail with reference to the embodiments, according to the engine fuel control apparatus of the present invention, the intake pipe pressure sensor, the crank angle sensor, and the basic fuel injection amount for calculating the basic fuel injection amount. Calculating means and intake pipe pressure change amount calculating means for calculating the intake pipe pressure change amount; and pressure change amount correction coefficient setting means for setting a pressure change amount correction coefficient based on a change rate of the throttle position sensor and throttle opening. An acceleration / deceleration continuous state detecting means for detecting a continuous state of acceleration / deceleration; a pressure change amount correcting means for calculating a corrected intake pipe pressure change amount during transient operation of the engine; and a fuel correction amount calculating means for calculating a fuel injection correction amount. Since the fuel injection amount calculation means for calculating the total fuel injection amount is provided, the intake pipe pressure change amount is corrected according to the transient state of the engine, and a large amount of fuel is supplied during rapid acceleration / deceleration of the engine. While weight loss at the time of slow acceleration and deceleration can be performed properly fuel correction during a transient by performing increment or decrement of a small amount of fuel. As a result, it is possible to operate at an appropriate air-fuel ratio, and it is possible to improve exhaust gas purification performance and drivability.

[Brief description of drawings]

FIG. 1 is a block diagram showing a schematic configuration of an engine fuel control apparatus according to an embodiment of the present invention.

FIG. 2 is a schematic diagram of a system of an engine.

FIG. 3 is a block diagram showing hardware of an engine control system.

FIG. 4 is a graph showing a relationship between an intake pipe pressure and a change amount of the intake pipe pressure, an acceleration correction amount, and a fuel injection amount by a fuel control device of the engine.

FIG. 5 is a flowchart of a main routine showing fuel control.

FIG. 6 is a time chart of data acquisition of intake pipe pressure.

FIG. 7 is a flowchart of a crank interrupt routine.

FIG. 8 is a flowchart showing a calculation of a transient correction amount.

FIG. 9 is a flowchart showing a calculation of a transient correction amount.

FIG. 10 is a flowchart showing a calculation of a transient correction amount.

FIG. 11 is a flowchart showing a calculation of a transient correction amount.

FIG. 12 is a graph showing the upper limit value of the amount of change in intake pipe pressure with respect to the engine speed.

FIG. 13 is a graph showing an acceleration increase emphasis coefficient with respect to throttle speed.

FIG. 14 is a graph showing a dead zone region based on changes in water temperature.

FIG. 15 is a graph showing the relationship among the intake air amount, intake pipe pressure, internal EGR, and combustion chamber wall surface temperature during engine acceleration.

FIG. 16 is a graph showing a relationship between an intake pipe pressure, a change amount of the intake pipe pressure, and a fuel injection amount by a conventional engine fuel control device.

FIG. 17 is a graph showing a combustion state by fuel correction of a conventional engine fuel control device.

[Explanation of symbols]

 10 Engine 18 Combustion Chamber 21 Intake Pipe 23 Throttle Valve 24 Throttle Position Sensor 27 Vacuum Sensor 29 Engine Control Unit (ECU) 30 Injector 35 Crank Angle Sensor 101 Intake Pipe Pressure Sensor 102 Crank Angle Sensor 103 Volume Efficiency Calculation Unit 104 Basic Fuel Injection Amount Calculation means 105 Intake pipe pressure change amount calculation means 106 Upper limit comparison setting means 107 Dead zone comparison means 108 Throttle position sensor 109 Pressure change amount correction coefficient calculation means 110 Acceleration / deceleration continuous state detection means 111 Pressure change amount correction means 112 Fuel correction amount Calculation means 113 Fuel injection amount calculation means

Claims (1)

[Claims] 1. An intake pipe pressure sensor for detecting a pressure in an intake pipe of an engine, a crank angle sensor for detecting an engine speed, and a steady operation of the engine based on outputs of the intake pipe pressure sensor and the crank angle sensor. , A basic fuel injection amount calculating means for calculating a basic fuel injection amount, an intake pipe pressure change amount calculating means for calculating an intake pipe pressure change amount based on the output of the intake pipe pressure sensor, and a throttle opening degree are detected. A throttle position sensor, a pressure change amount correction coefficient setting means for setting a pressure change amount correction coefficient based on a change rate of the throttle opening calculated from the output of the throttle position sensor, and an engine acceleration / deceleration continuation state. Based on the output of the acceleration / deceleration continuous state detecting means for detecting, the pressure change amount correction coefficient setting means and the acceleration / deceleration continuous state training means, Note: An intake pipe pressure change amount correction means for correcting the intake pipe pressure change amount to calculate a corrected intake pipe pressure change amount, and a fuel correction amount calculation for calculating a fuel injection correction amount based on the corrected intake pipe pressure change amount A fuel control device for an engine, comprising: a fuel injection amount calculation unit that calculates a total fuel injection amount based on outputs of the basic fuel injection amount calculation unit and the fuel correction amount calculation unit.