 |
Description  |
|
|
BACKGROUND OF THE INVENTION
The present invention relates to a method of controlling the boost pressure
of a blower, known as a supercharger or a turbocharger, associated with an
internal combustion engine.
Blowers such as superchargers or turbochargers are generally driven by the
power output from the output shaft of or the exhaust gases emitted from
engines. As the rotational speed of the engine goes higher, the driving
force for the blower is also increased and the boost pressure thereof
becomes higher. Since an excessive boost pressure would cause troubles
such as knocking, it would be preferable to control the boost pressure at
an optimum level under all conditions. In the supercharger operated by the
engine power output, the boost pressure can be controlled by selectively
applying and cutting off the driving force to and from the supercharger or
opening and closing a bypass valve. In the turbocharger operated by the
engine exhaust gases, the boost pressure can be controlled by adjusting
movable vanes to restrict the exhaust gas supplied to the turbine wheel or
selectively opening and closing a wastegate.
All types of blowers are subject to a certain type delay in the response of
the boost pressure to the engine rotational speed or the throttle valve.
Therefore, under normal feedback control, the boost pressure that is
controlled tends to overshoot excessively or undergo hunting if control
characteristics are not appropriate. If the feedback control were to be
stabilized so as to be less responsive to the parameters, the response of
the control system would be greatly impaired. It has been found that the
intake air temperature and the atmospheric pressure are important as
control parameters.
Where open-loop control such as map control is relied upon, no control
stability problem occurs. Since, however, many parameters are involved and
many map addresses or locations are required, a control unit used should
have a large memory capacity and may be retarded in its response speed.
SUMMARY OF THE INVENTION
It is an object of the present invention to provide a method of controlling
the boost pressure of a blower with stability and good response.
According to the present invention, there is provided a method of
controlling the boost pressure of a blower driven by the exhaust gas or
the power output from an engine, comprising the steps of controlling the
boost pressure under closed-loop control when the boost pressure is in a
steady state, and controlling the boost pressure under open-loop control
when the boost pressure is in a transient state.
When the boost pressure is in the transient state, the open-loop control
which may be map control is carried out for relatively good accuracy and
high stability. When the boost pressure is in the steady state, the
closed-loop control, i.e., highly accurate feedback control is effected.
Therefore, the response and stability can be achieved in boost pressure
control.
The open-loop control is effected on the basis of map values which are
updated by data obtained in the closed-loop control. The map values are
updated for each of different temperatures of intake air supplied to the
engine. Since the intake air temperature is important as a control
parameter, the accuracy of controlling the boost pressure in the open-loop
control is increased.
A target boost pressure is varied as a function of the rate of change of
the actual boost pressure in the closed-loop control. By thus varying the
target boost pressure, the actual boost pressure can be caused to quickly
converge to the target boost pressure.
The boost pressure is controlled to reach a target boost pressure by
adjusting a command value as a function of the temperature of intake air
supplied to the engine or the atmospheric pressure. By adjusting the
command value as a function of the important parameter, the boost pressure
can quickly and stably be converged to the target boost pressure
irrespective of environments in which the engine operates.
The above and other objects, features and advantages of the present
invention will become more apparent from the following description when
taken in conjunction with the accompanying drawings in which preferred
embodiments of the present invention are shown by way of illustrative
example.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a schematic view of a blower system for charging air into the
cylinders of an internal combustion engine;
FIG. 2 is a flowchart of a control sequence of a boost pressure control
method according to an embodiment of the present invention;
FIG. 3 is a graph showing a table of corrective coefficients vs. intake air
temperatures, employed in the boost pressure control method;
FIG. 4 is a flowchart of a control sequence of a boost pressure control
method according to another embodiment of the present invention;
FIG. 5 is a block diagram of a modified control unit; and
FIG. 6A and 6B show additional steps of a control sequence executed by the
control unit shown in FIG. 5.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
FIG. 1 schematically shows a blower system for forcibly supplying air into
the cylinders of an internal combustion. Only one of the engine cylinders
is illustrated in FIG. 1 for the sake of brevity.
Intake air to be supplied to an internal combustion engine 1 is delivered
from an air cleaner 5 through an intake passage 6 to a compressor wheel 7
of a blower 2, shown as a turbocharger, from which the air is supplied
through an intake passage 8, an intercooler 9, a throttle body housing a
throttle valve 11, and an intake passage 10 into a combustion chamber of
the engine 1. A fuel injection valve 12 is disposed in the intake passage
10 downstream of the throttle valve 11. Exhaust gases discharged from the
combustion chamber are delivered through an exhaust passage 13 into a
turbine wheel 14 of the blower 2. After the exhaust gases have released
the energy to rotate the compressor wheel 7, the exhaust gases are
discharged via an exhaust passage 15 and a muffler 16 into the atmosphere.
A variable nozzle 3 comprising a number of vanes arranged in an annular
pattern is disposed immediately upstream of the turbine wheel 14. The
speed of flow of the exhaust gases toward the turbine wheel 14 can be
adjusted by varying the amount of opening of the variable nozzle 3 with an
adjusting mechanism 4.
The adjusting mechanism 4 is actuated by an actuator 20 having a positive
pressure chamber 38 defined by a positive pressure diaphragm 25 normally
urged to move in one direction by a coil spring 33. The positive pressure
chamber 38 is connected to the intake passage 8 upstream of the throttle
valve 11 through a pipe 18 having a control valve 18a. The control valve
18a can be opened and closed under the control of a control unit 17
supplied with the intake air temperature TA, the intake boost pressure P2,
the engine rotational speed Ne and the throttle opening .theta.th as
parameters.
The control unit 17 may comprise a digital central processing unit (CPU)
that can be programmed to perform various control methods as will be
described later on.
A rod 28 is fixed to the center of the diaphragm 25 of the actuator 20 and
has an end coupled to the adjusting mechanism 4.
The control valve 18a is controlled in its duty ratio by the control unit
17.
FIG. 2 shows a control sequence or program which is executed by the control
unit 17 to generate a control signal D for controlling the control valve
18a.
When a power supply is switched on, the variables are cleared and the
control unit performs self-diagnosis in a step 1, identified as "ST 1" and
each of the subsequent steps are identified in the drawings by "ST"
followed by the number of that step. Then, a temporary control signal D0
is read in a step 2 from a map in the control unit 17 based on the
throttle opening .theta. and the engine rotational speed Ne which are
applied to the control unit 17. In a next step 3, a constant KT for intake
air temperature compensation is read out from a table in the control unit
17 based on the intake air temperature TA applied to the control unit 17.
A step 4 detects a change in the present boost pressure P2 of the blower
2, and a next step 5 ascertains whether the boost pressure P2 is in a
transient state or not. If the boost pressure P2 is in a steady state,
then a target boost pressure PT is read from a table based on the present
parameters .theta., Ne in a step 6. A step 7 finds the difference delta-P
between the target boost pressure PT and the present boost pressure P2,
followed by a step 8 which ascertains whether or not the absolute value of
the difference delta-P is equal to or greater than G, i.e., whether the
boost pressure P2 has been controlled at the boost pressure setpoint PT
within an allowable range (.+-.G) or not.
If the absolute value of delta-P is equal to or greater than G, then
constants KP, KI for proportional and integral control are found from a
table based on the engine rotational speed Ne in a step 9. The control
signal D is corrected in a step 12 by corrective quantities DP, DI that
are calculated by the constants KP, KI, respectively, in successive steps
10, 11. In the step 12, the temperature compensation constant KT obtained
in the step 3 is taken into account. Then, the limit of the control signal
D is checked in a step 13, and then the control signal D is issued in a
step 14 to control the control valve 18a. Thereafter, control goes back to
the step 2. The limit checking for the control signal D is effected in
view of the nonlinearity of the diaphragm actuator 20 so that the value of
the control signal D will forcibly be kept within a range in which the
actuator has a substantially linear characteristic.
If the absolute value of delta-P is smaller than G in the step 8, i.e., if
the present boost pressure P2 has reached substantially the target boost
pressure PT, then the corrective quantity DI which has been employed in
the preceding cycle is retained as it is, and the corrective quantity DP
is set to zero, in a step 15. A next step 16 calculates a ratio KL between
the value of the present control signal D and the output value of a
control signal given from the map value D0 only. In a step 17, a
corrective coefficient KL0 up to now is updated using a prescribed
weighting coefficient t (0.ltoreq.t.ltoreq.1) and the newly obtained
corrective coefficient KL.
The correcting coefficient KL0 is dependent on the engine rotational speed
Ne, the throttle opening .theta., and the intake air temperature TA, but
is strongly affected by the intake air temperature TA in particular. In
view of this, a table of corrective coefficients KL0 vs. intake air
temperatures TA as shown in FIG. 3 is updated for each of present intake
air temperatures TA1, . . . , TAn in a step 18. Then, control returns to
the aforesaid control loop by going to the step 12.
If the boost pressure P2 is in the transient state in the step 5, then the
corrective coefficient KL0 is read out of the KL0 table, the control
quantities DP, DI are set to zero, and the control signal D is set to
D=KT. KL0.D0 in a step 19, which is followed by the step 14. Therefore, in
the event that the boost pressure P2 is in the transient state, e.g., it
is abruptly changed, open-loop control such as map control is carried out.
Since a value updated in the step 18, i.e., a value obtained by
experience, is used as KL0 in such open-loop control, the control process
is highly accurate regardless of the fact that the stability of the
control system is high. The map control is of high accuracy because the
corrective coefficients KL0 are established for respective different
intake air temperatures TA1, . . . , TAn.
FIG. 4 shows a flowchart of a control sequence of a boost pressure control
method according to another embodiment of the present invention. When a
power supply is switched on, the variables are cleared and the control
unit performs self-diagnosis in a step 1. Then, a temporary target boost
pressure PT and a temporary control signal D0 are read from maps in the
control unit 17 based on the throttle opening .theta. an the engine
rotational speed Ne in a step 2. A next step 3 determines the difference
delta-PD between a present boost pressure P2,n and a preceding boost
pressure P2,n-1.
In a step 4, an increase delta-PT in the target boost pressure PT is read
out of a table in the control unit 17 as a function of delta-PD, i.e., the
rate of change of the boost pressure. Then, the target boost pressure PT
is corrected by a quantity commensurate with the increase delta-PT in a
step 5. The difference delta-P2 between the target boost pressure PT and
an actual boost pressure P2 is determined in a step P6, followed by a step
7 in which a constant KT for intake air temperature compensation is read
out from a table in the control unit 17 based on the intake air
temperature TA applied to the control unit 17. A step 8 ascertains whether
or not delta-P2 is equal to or greater than zero. If delta-P2 is equal to
or greater than zero, i.e., if the actual boost pressure P2 is equal to or
lower than the target boost pressure PT, then an indicator I is set to +1
in a step 9. If delta-P2 is smaller than zero, i.e., if the actual boost
pressure P2 is higher than the target boost pressure PT, then the
indicator I is set to -1 in a step 10.
A next step 11 ascertains whether the indicator I is changed or not from
the preceding value. If not, i.e., if the actual boost pressure P2 does
not cross the target boost pressure P, then a step 12 ascertains whether
the absolute value of delta-P2 is greater than a constant G or not. If the
absolute value of delta-P2 is greater than the constant G, i.e., if the
actual boost pressure P2 should be adjusted to approach the target boost
pressure PT, then constants KP, KI for proportional and integral control
are found from a table based on the engine rotational speed Ne in a step
13. Corrective quantities DP, DI are calculated by the constants KP, KI,
respectively, in successive steps 14, 15. The limit of the corrective
quantity DI is checked in a step 16. Then, a control signal D is
calculated from the corrective quantities DP, DI in a step 17 in which the
temperature compensation constant KT obtained in the step 7 is also taken
into account.
Then, the limit of the control signal D is checked in a step 18. The limit
checking for the control signal D is effected in view of the nonlinearity
of the diaphragm actuator 20 so that the value of the control signal D
will forcibly be kept within a range in which the actuator has a
substantially linear characteristic. Then, the control signal D is issued
in a step 19 to control the control valve 18a. Thereafter, control goes
back to the step 2.
If the indicator I is changed from the preceding value in the step 11, then
DA is read from a table in the control unit 17 as a function of delta-P2
in a step 21. The corrective quantity DI for integral control is corrected
by DA in a step 22, and the corrective quantity DP for proportional
control is set to zero in a step 23, from which control goes to the step
16.
If the absoluted value of delta-P2 is smaller than G in the step 12, i.e.,
if the actual boost pressure P2 is substantially equal to the target boost
pressure PT, then the corrective quantity DI is retained as it is and the
corrective quantity DP is set to zero in a step 20 which is then followed
by the step 17.
As described above the control method of the present invention is based on
proportional plus integral control using the digital CPU. As indicated by
the steps 3 through 6 in FIG. 4, when the rate of change delta-P2 of the
actual boost pressure P2 is large, the target boost pressure PT is set
apart from the actual boost pressure P2. Therefore, control action to
bring the actual boost pressure P2 closely to the target boost pressure PT
is increased, and the actual boost pressure is caused to converge quickly
to the target boost pressure.
As shown in the steps 8 through 11 and 21 through 23 in FIG. 4, when the
actual boost pressure P2 crosses the target boost pressure PT, the
corrective quantity DI for integral control is reduced, also allowing the
actual boost pressure to converge quickly to the target boost pressure.
FIG. 5 illustrates a modified control unit 17' which is supplied with data
on atmospheric pressure PA as an additional parameter.
FIGS. 6A and 6B show steps 7', 17', respectively, of a control sequence to
be executed by the control unit 17' shown in FIG. 5. The steps 7', 17' are
substituted for the respective steps 7, 17 of the control sequence of FIG.
4. In the step 7', constants KT, KA are found from respective tables for
intake air temperature compensation and atmospheric pressure compensation
based on the intake air temperature TA and the atmospheric pressure, PA
applied to the control unit 17'. In the step 17', both of the constants
KT, KA for intake air temperature compensation and atmospheric pressure
compensation, obtained in the step 7', are taken into account in
calculating the control signal D.
The principles of the present invention have been shown as being applied to
the control of the variable nozzle of a turbocharger. However, the control
method of the present invention may also be used for controlling the
turn-on/-off of the input shaft or the opening/closing of the bypass valve
of a supercharger, or the wastegate of a turbocharger, or a two-stage or
hybrid blower system employing a plurality of blowers of like or different
types.
Although certain preferred embodiments have been shown and described, it
should be understood that many changes and modifications may be made
therein without departing from the scope of the appended claims.
* * * * *
|
|
 |
|
 |
Description |
|
