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| United States Patent | 4889099 |
| Link to this page | http://www.wikipatents.com/4889099.html |
| Inventor(s) | Tomishawa; Naoki (Gunma, JP) |
| Abstract | An air/fuel ratio control system controls fuel delivery amount on the basis
of oxygen concentration in an exhaust gas. An air/fuel ratio dependent
correction value is derived on the basis of the oxygen concentration. The
air/fuel ratio control is performed in feedback mode and open loop mode.
In feedback mode, fuel delivery amount is corrected utilizing a correction
value which includes a learnt component. Learning of the learned component
is performed during feedback mode operation. The learned component
comprises a uniformly applicable air density dependent factor and an
engine driving range dependent factor which is set with respect to each of
the engine driving ranges. Learning of the air density factor and engine
driving range dependent factor are selectively performed depending upon
the engine driving condition. |
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Title Information  |
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Drawing from US Patent 4889099 |
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Air/fuel mixture ratio control system for internal combustion engine
with feature of learning correction coefficient including altitude
dependent factor |
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| Publication Date |
December 26, 1989 |
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| Priority Data |
May 28, 1987[JP]62-129893
May 29, 1987[JP]62-131826
Jun 16, 1987[JP]62-148035 |
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Title Information  |
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Market Review  |
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Technical Review  |
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Claims  |
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What is claimed is:
1. An air/fuel ratio control system for controlling a mixture ratio of an
air/fuel mixture to be introduced into a combustion chamber in an internal
combustion engine, comprising:
an air/fuel mixture induction system for introducing an intake air and a
fuel for forming an air/fuel mixture to be supplied into an engine
combustion chamber, said air/fuel mixture delivery system incorporating a
fuel metering means for delivering a controlled amount of fuel;
a first sensor means for monitoring a preselected basic first engine
operation parameter to produce a first sensor signal indicative thereof;
a second sensor means for monitoring an air/fuel mixture ratio indicative
parameter for producing a second sensor signal variable of the value
indicative of a deviation from a threshold value representative of a
stoichiometric value;
third means for deriving a basic fuel metering amount on the basis of said
first sensor signal value;
fourth means for deriving a air/fuel ratio dependent correction factor
variable of the value thereof depending upon said second sensor signal
value;
fifth means for deriving an air density dependent first correction
coefficient on the basis of said air/fuel ratio dependent correction
factor for air/fuel ratio dependent correction of said basic fuel metering
amount, which first correction coefficient is commonly applicable for
correction of said basic fuel metering amount in over all engine driving
ranges, said fifth means updating said first correction coefficient when a
first learning condition is satisfied;
a sixth means for deriving a second correction coefficient which is
variable depending upon the engine driving range on the basis of said
air/fuel ratio dependent correction factor, said sixth means setting a
plurality of said second correction coefficient in relation to
respectively corresponding engine driving range and updating each of said
second correction coefficient with an instantaneous value derived based on
said air/fuel ratio dependent correction factor in the corresponding
engine driving range;
a seventh means for detecting engine driving condition on the basis of said
first sensor signal values and governing said fifth and sixth means for
selectively operating one of said fifth and sixth means depending upon the
detected engine driving condition; and
an eighth means for correcting said basic fuel metering amount with said
correction coefficient to control said fuel metering means for delivering
the fuel in the amount corresponding to the corrected fuel metering amount
to said air/fuel mixture delivery system.
2. An air/fuel ratio control system as set forth in claim 1, wherein said
seventh means detects said engine driving condition satisfying a
predetermined feedback control condition for producing a feedback
condition indicative signal to selectively enable said fifth and sixth
means for updating one of said first and second correction coefficient and
to disable said fifth and sixth means when said feedback condition is not
satisfied.
3. An air/fuel ratio control system as set forth in claim 1, which further
comprises a ninth means for detecting engine driving condition in high
speed and high load, which is out of said feedback condition, to measure
an elapsed period where said high speed and high load condition is
maintained, said ninth means modifying said first correction coefficient
when the measured elapsed time becomes longer than or equal to a
predetermined period.
4. An air/fuel ratio control system as set forth in claim 3, wherein said
ninth means cyclically modifies said first correction coefficient by a
predetermined value while the engine is maintained at said high speed and
high load condition.
5. An air/fuel ratio control system as set forth in claim 4, wherein said
second sensor means varies polarity of said second sensor signal value
when air/fuel ratio varies across a stoichiometric value, and which
further comprises a tenth means for measuring an elapsed time in which the
polarity of said second sensor signal value is held unchanged to detect
abnormality of said second sensor means.
6. An air/fuel ratio control system as set forth in claim 5, wherein said
tenth means disables said ninth means when abnormality of said second
sensor means is detected.
7. An air/fuel ratio control system as set forth in claim 1, wherein said
first sensor means includes means for monitoring an engine load indicative
parameter and means for monitoring an engine speed indicative parameter,
and said seventh means derives a first criterion on the basis of an engine
speed derived on the basis of the monitored engine speed indicative
parameter and compares an engine load derived based on said engine load
indicative parameter with said first criterion for enabling said fifth
means when said engine load is greater than or equal to said first
criterion, and enabling said sixth means when said engine load is smaller
than said first criterion.
8. An air/fuel ratio control system as set forth in claim 7, wherein said
seventh means further derives a second criterion on the basis of said
engine speed, which second criterion is set at a greater value than said
first criterion and compares said engine load with said second criterion
so as to disable said fifth means when said engine load is greater than
said second criterion.
9. An air/fuel ratio control system as set forth in claim 1, wherein said
second sensor means varies polarity of said second sensor signal value
when air/fuel ratio varies across a stoichiometric value, and said fifth
and sixth means, as being triggered by said seventh means, being
responsive to change of polarity of said second sensor signal to update
said first and second correction coefficients.
10. An air/fuel ratio control system as set forth in claim 1, which further
comprises a detector means detective of engine driving condition
satisfying a predetermined feedback control condition for producing a
feedback condition indicative signal to operate said eighth means in
feedback mode for correcting said basic fuel metering amount with said
first and second correction coefficients and to operate said eighth means
in open loop mode for disabling correction of said basic fuel metering
amount utilizing said first and second correction coefficients, and said
seventh means selectively enables said fifth and sixth means for updating
said first and second correction coefficients while said eighth means
operates in feedback mode.
11. An air/fuel ratio control system as set forth in claim 10, wherein said
fourth means is active in presence of said feedback condition indicative
signal to cyclically derive said correction factor, and said sixth means
is active for deriving said second correction coefficient on the basis of
said correction factor only when said feedback condition indicative signal
is present.
12. An air/fuel ratio control system as set forth in claim 11, wherein said
fourth means samples upper and lower peak values of said second sensor
signal value for deriving said correction factor by averaging said upper
and lower peak values.
13. An air/fuel ratio control system as set forth in claim 1, wherein said
first sensor means monitors an engine speed indicative parameter and an
engine load indicative parameter so that said third means derives said
basic fuel metering amount on the basis of said engine speed indicative
parameter and said engine load indicative parameter, and said fifth means
detects said engine driving range on the basis of said engine speed and
said basic fuel metering amount.
14. An air/fuel ratio control system as set forth in claim 13, wherein said
first sensor means monitors a throttle valve angular position and derives
said engine load indicative parameter on the basis of said throttle valve
angular position and said engine speed.
15. An air/fuel ratio control system for controlling a mixture ratio of an
air/fuel mixture to be introduced into a combustion chamber in an internal
combustion engine, comprising:
an air/fuel mixture induction system for introducing an intake air and a
fuel for forming an air/fuel mixture to be supplied into an engine
combustion chamber, said air/fuel mixture delivery system incorporating a
fuel metering means for delivering a controlled amount of fuel;
a first sensor means for monitoring a preselected basic first engine
operation parameter to produce a first sensor signal indicative thereof,
said first sensor signal including an engine load indicative component;
a second sensor means for monitoring an air/fuel mixture ratio indicative
parameter for producing a second sensor signal variable of the value
indicative of a deviation from a threshold value representative of a
stoichiometric value;
third means for deriving a basic fuel metering amount on the basis of said
first sensor signal value;
fourth means for deriving a air/fuel ratio dependent correction factor
variable of the value thereof depending upon said second sensor signal
value;
fifth means for deriving an air density dependent first correction
coefficient on the basis of said air/fuel ratio dependent correction
factor for air/fuel ratio dependent correction of said basic fuel metering
amount, which first correction coefficient is commonly applicable for
correction of said basic fuel metering amount in over all engine driving
ranges, said fifth means updating said first correction coefficient when a
first learning condition is satisfied;
a sixth means for deriving a second correction coefficient which is
variable depending upon the engine driving range on the basis of said
air/fuel ratio dependent correction factor, said sixth means setting a
plurality of said second correction coefficient in relation to
respectively corresponding engine driving range and updating each of said
second correction coefficient with an instantaneous value derived based on
said air/fuel ratio dependent correction factor in the corresponding
engine driving range;
a seventh means, associated with said fifth means, for deriving an altitude
dependent correction value for modifying said first correction value on
the basis of said engine load component of said first sensor signal and a
tendency of air/fuel ratio adjustment in a given cycles of said second
sensor signal variations;
an eighth means for correcting said basic fuel metering amount with said
correction coefficient to control said fuel metering means for delivering
the fuel in the amount corresponding to the corrected fuel metering amount
to said air/fuel mixture delivery system.
16. An air/fuel ratio control system as set forth in claim 15, wherein said
seventh means increases altitude dependent correction value according to
increase of said engine load.
17. An air/fuel ratio control system as set forth in claim 15, wherein said
seventh means detects tendency of richer side or leaner side air/fuel
ratio control depending upon distribution of richer side variation and
leaner side variation of given number of said second correction
coefficients updated by said sixth means in most recent given updating
cycles.
18. An air/fuel ratio control system as set forth in claim 17, wherein said
seventh means increases said altitude dependent correction value according
to increase of tendency of either richer side or leaner side air/fuel
control which is greater than the other.
19. An air/fuel ratio control system as set forth in claim 15, wherein said
seventh means detects tendency of richer side or leaner side air/fuel
ratio control depending upon distribution of said second correction values
residing richer side and leaner side of a predetermined threshold value.
20. An air/fuel ratio control system as set forth in claim 19, wherein said
seventh means increases said altitude dependent correction value according
to increase of tendency of either richer side or leaner side distribution
which is greater than the other.
21. An air/fuel ratio control system as set forth in claim 15, wherein said
seventh means derives said altitude dependent correction value
constituting a first component variable according to variation to
variation of said engine load and a second component derived depending
upon tendency of richer side or leaner side air/fuel ratio control
depending upon distribution of richer side variation and leaner side
variation of given number of said second correction coefficients updated
by said sixth means in most recent given updating cycles.
22. An air/fuel ratio control system as set forth in claim 21, wherein said
altitude dependent correction value is an average value of said first and
second components.
23. An air/fuel ratio control system as set forth in claim 15, wherein said
seventh means derives said altitude dependent correction value
constituting a first component variable according to variation to
variation of said engine load and a second component derived depending
upon tendency of richer side or leaner side air/fuel ratio control
depending upon distribution of said second correction values residing
richer side and leaner side of a predetermined threshold value.
24. An air/fuel ratio control system as set forth in claim 23, wherein said
altitude dependent correction value is an average value of said first and
second components.
25. An air/fuel ratio control system as set forth in claim 15, wherein said
seventh means derives said altitude dependent correction value
constituting a first component variable according to variation to
variation of said engine load, a second component derived depending upon
tendency of richer side or leaner side air/fuel ratio control depending
upon distribution of said second correction values residing richer side
and leaner side of a predetermined threshold value, and a third component
derived depending upon distribution of richer side variation and leaner
side variation of given number of said second correction coefficients
updated by said sixth means in most recent given updating cycles.
26. An air/fuel ratio control system as set forth in claim 25, wherein said
altitude dependent correction value is an average value of said first,
second and third components.
27. An air/fuel ratio control system as set forth in claim 15, wherein said
first sensor means includes means for monitoring an engine load indicative
parameter and means for monitoring an engine speed indicative parameter,
and said seventh means derives a first criterion on the basis of an engine
speed derived on the basis of the monitored engine speed indicative
parameter and compares an engine load derived based on said engine load
indicative parameter with said first criterion for enabling said fifth
means when said engine load is greater than or equal to said first
criterion, and enabling said sixth means when said engine load is smaller
than said first criterion.
28. An air/fuel ratio control system as set forth in claim 15, wherein said
second sensor means varies polarity of said second sensor signal value
when air/fuel ratio varies across a stoichiometric value, and said fifth
and sixth means, as being triggered by said seventh means, being
responsive to change of polarity of said second sensor signal to update
said first and second correction coefficients.
29. An air/fuel ratio control system as set forth in claim 15, which
further comprises a detector means detective of engine driving condition
satisfying a predetermined feedback control condition for producing a
feedback condition indicative signal to operate said eighth means in
feedback mode for correcting said basic fuel metering amount with said
first and second correction coefficients and to operate said eighth means
in open loop mode for disabling correction of said basic fuel metering
amount utilizing said first and second correction coefficients, and said
seventh means selectively enables said fifth and sixth means for updating
said first and second correction coefficients while said eighth means
operates in feedback mode.
30. An air/fuel ratio control system as set forth in claim 29, wherein said
fourth means is active in presence of said feedback condition indicative
signal to cyclically derive said correction factor, and said sixth means
is active for deriving said second correction coefficient on the basis of
said correction factor only when said feedback condition indicative signal
is present.
31. An air/fuel ratio control system as set forth in claim 30, wherein said
fourth means samples upper and lower peak values of said second sensor
signal value for deriving said correction factor by averaging said upper
and lower peak values.
32. An air/fuel ratio control system as set forth in claim 15, wherein said
first sensor means monitors an engine speed indicative parameter and an
engine load indicative parameter so that said third means derives said
basic fuel metering amount on the basis of said engine speed indicative
parameter and said engine load indicative parameter, and said fifth means
detects said engine driving range on the basis of said engine speed and
said basic fuel metering amount.
33. An air/fuel ratio control system as set forth in claim 32, wherein said
first sensor means monitors a throttle valve angular position and derives
said engine load indicative parameter on the basis of said throttle valve
angular position and said engine speed. |
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Claims  |
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Description  |
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BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates generally to an air/fuel mixture ratio
control system for an internal combustion engine. More specifically, the
invention relates to a learning control system for controlling air/fuel
ratio in a fuel injection internal combustion engine, which air/fuel
ration control includes lambda (.lambda.) control for performing FEEDBACK
or CLOSED LOOP control on the basis of oxygen concentration contained in
an exhaust gas. Further particularly, the invention relates to an air/fuel
ratio learning control system including altitude depending control, which
can precisely adjust air/fuel ratio depending upon density of air to be
introduced for forming the air/fuel mixture.
2. Description of the Background Art
In the recent years, there have been proposed various air/fuel control
systems for internal combustion engines. Some of the recently developed
air/fuel ratio control systems incorporate learning control feature to
continuously update correction coefficient for correcting a basic fuel
injection amount based on oxygen concentration in an exhaust gas in order
to maintain air/fuel ratio at a stoichiometric value. In case that air
density dependent air/fuel ratio is concerned, the correction coefficient
may be uniformly updated based on an oxygen concentration indicative
sensor signal value (hereafter O.sub.2 sensor signal) regardless of the
engine driving range, in theory. However, in practice, because of
tolerance in fuel injection valves, throttle body and other engine
components, which causes deviation between arithmetically obtained basic
fuel injection amount and practically required fuel injection amount,
uniformly updating or learning of the correction coefficient regardless of
engine driving range is practically not possible. By this, it is
practically required to set learned correction coefficient for respective
engine driving range.
In this view, learning control systems with FEEDBACK control feature for
controlling air/fuel ratio have been recently proposed in the Japanese
Patent First (unexamined) Publication (Tokkai) Showa No. 60-90944 and the
Japanese Patent First Publication (Tokkai) Showa No. 61-190142. In the
disclosed system, a basic fuel injection amount is derived on the basis of
preselected basic fuel injection control parameter or parameters, such as
an intake air flow rate, an engine revolution speed and so forth. The
basic fuel injection amount thus derived is modified employing a feedback
correction coefficient which is derived on the basis of oxygen sensor in
an exhaust system and composed of a proportional (P) component and an
integral (I) component. By modifying the fuel injection amount on the
basis of the feedback correction coefficient, air/fuel ratio can be
FEEDBACK controlled toward a stoichiometric value. Furthermore, the
disclosed system derives a learnt correction coefficient with respect to
mutually distinct various engine operation range. In practice, the learned
correction coefficient is determined by deriving a difference between the
feedback correction coefficient and a predetermined reference value. This
learned correction coefficient is used in OPEN LOOP mode air/fuel ratio
control to derive the fuel injection amount. The learned correction
coefficient may also be used in the FEEDBACK or CLOSED LOOP mode air/fuel
ratio control together with the feedback correction coefficient.
Such a system assures to perform air/fuel ratio control in the FEEDBACK
mode operation to maintain the air/fuel ratio precisely at the
stoichiometric value. Furthermore, since the learned correction
coefficient may serve to maintain desired air/fuel ratio even in OPEN LOOP
mode operation.
However, in the aforementioned type of learning control system, drawback
may be encountered in an engine driving condition where the engine driving
or operation range frequently fluctuates. For example, in hill or mountain
climbing, the air/fuel ratio control mode is held in transition mode
condition between FEEDBACK mode and OPEN LOOP mode to too frequently
change engine driving range to update learned correction coefficient
during FEEDBACK mode operation. Therefore, the learned correction
coefficient may not reflect the instantaneous air density. This causes
delay in FEEDBACK mode control after the driving condition returns to
stable state satisfying FEEDBACK condition. Furthermore, in the OPEN LOOP
control, the air/fuel ratio tends to deviate far from the stoichiometric
value to degrade drivability.
SUMMARY OF THE INVENTION
It is an object of the present invention to provide an air/fuel ratio
control system which can precisely control fuel delivery amount at any
altitude condition and can provide sufficiently high response
characteristics to altitude change.
Another object of the invention is to introduce a control feature in the
air/fuel ratio control for optimizing air/fuel control at any
environmental condition.
In order to accomplish aforementioned and other objects, an air/fuel ratio
control system, according to the present invention, controls fuel delivery
amount on the basis of oxygen concentration in an exhaust gas. An air/fuel
ratio dependent correction value is derived on the basis of the oxygen
concentration. The air/fuel ratio control is performed in feedback mode
and open loop mode. In feedback mode, fuel delivery amount is corrected
utilizing a correction value which includes a learned component. Learning
of the learnt component is performed during feedback mode operation. The
learned component comprises an uniformly applicable air density dependent
factor and a engine driving range dependent factor which is set with
respect to each of the engine driving ranges. Learning of the air density
factor and engine driving range dependent factor are selectively performed
depending upon the engine driving condition.
This introduces altitude dependent air/fuel ratio control. According to the
invention, altitude dependent control can be taken place even in engine
high speed and high load condition for improving response characteristics
in air/fuel ratio control at any altitude condition.
In the alternative, the control feature may be introduced in the air/fuel
ratio control for optimizing air/fuel ratio control at any altitude.
According to one aspect of the invention, an air/fuel ratio control system
for controlling a mixture ratio of an air/fuel mixture to be introduced
into a combustion chamber in an internal combustion engine, comprises an
air/fuel mixture induction system for introducing an intake air and a fuel
for forming an air/fuel mixture to be supplied into an engine combustion
chamber, the air/fuel mixture delivery system incorporating a fuel
metering means for delivering a controlled amount of fuel, a first sensor
means for monitoring a preselected basic first engine operation parameter
to produce a first sensor signal indicative thereof, a second sensor means
for monitoring an air/fuel mixture ratio indicative parameter for
producing a second sensor signal variable of the value indicative of a
deviation from a threshold value representative of a stoichiometric value,
third means for deriving a basic fuel metering amount on the basis of the
first sensor signal value, fourth means for deriving a air/fuel ratio
dependent correction factor variable of the value thereof depending upon
the second sensor signal value, fifth means for deriving an air density
dependent first correction coefficient on the basis of the air/fuel ratio
dependent correction factor for air/fuel ratio dependent correction of the
basic fuel metering amount, which first correction coefficient is commonly
applicable for correction of the basic fuel metering amount in over all
engine driving ranges, the fifth means updating the first correction
coefficient when a first learning condition is satisfied, a sixth means
for deriving a second correction coefficient which is variable depending
upon the engine driving range on the basis of the air/fuel ratio dependent
correction factor, the sixth means setting a plurality of the second
correction coefficient in relation to respectively corresponding engine
driving range and updating each of the second correction coefficient with
an instantaneous value derived based on the air/fuel ratio dependent
correction factor in the corresponding engine driving range, a seventh
means for detecting engine driving condition on the basis of the first
sensor signal values and governing the fifth and sixth means for
selectively operating one of the fifth and sixth means depending upon the
detected engine driving condition, and an eighth means for correcting the
basic fuel metering amount with the correction coefficient to control the
fuel metering means for delivering the fuel in the amount corresponding to
the corrected fuel metering amount to the air/fuel mixture delivery
system.
The seventh means may detect the engine driving condition satisfying a
predetermined feedback control condition for producing a feedback
condition indicative signal to selectively enable the fifth and sixth
means for updating one of the first and second correction coefficient and
to disable the fifth and sixth means when the feedback condition is not
satisfied.
The air/fuel ratio control system further comprises a ninth means for
detecting engine driving condition in high speed and high load, which is
out of the feedback condition, to measure an elapsed period where the high
speed and high load condition is maintained, the ninth means modifying the
first correction coefficient when the measured elapsed time becomes longer
than or equal to a predetermined period. The ninth means cyclically
modifies the first correction coefficient by a predetermined value while
the engine is maintained at the high speed and high load condition. The
second sensor means varies polarity of the second sensor signal value when
air/fuel ratio varies across a stoichiometric value, and which further
comprises a tenth means for measuring an elapsed time in which the
polarity of the second sensor signal value is held unchanged to detect
abnormality of the second sensor means. The tenth means disables the ninth
means when abnormality of the second sensor means is detected.
The first sensor means preferably includes means for monitoring an engine
load indicative parameter and means for monitoring an engine speed
indicative parameter, and the seventh means derives a first criterion on
the basis of an engine speed derived on the basis of the monitored engine
speed indicative parameter and compares an engine load derived based on
the engine load indicative parameter with the first criterion for enabling
the fifth means when the engine load is greater than or equal to the first
criterion, and enabling the sixth means when the engine load is smaller
than the first criterion. The seventh means further derives a second
criterion on the basis of the engine speed, which second criterion is set
at a greater value than the first criterion and compares the engine load
with the second criterion so as to disable the fifth means when the engine
load is greater than the second criterion.
The second sensor means may vary polarity of the second sensor signal value
when air/fuel ratio varies across a stoichiometric value, and the fifth
and sixth means, as being triggered by the seventh means, being responsive
to change of polarity of the second sensor signal to update the first and
second correction coefficients.
The air/fuel ratio control system further comprises a detector means
detective of engine driving condition satisfying a predetermined feedback
control condition for producing a feedback condition indicative signal to
operate the eighth means in feedback mode for correcting the basic fuel
metering amount with the first and second correction coefficients and to
operate the eighth means in open loop mode for disabling correction of the
basic fuel metering amount utilizing the first and second correction
coefficients, and the seventh means selectively enables the fifth and
sixth means for updating the first and second correction coefficients
while the eighth means operates in feedback mode. The fourth means is
active in presence of the feedback condition indicative signal to
cyclically derive the correction factor, and the sixth means is active for
deriving the second correction coefficient on the basis of the correction
factor only when the feedback condition indicative signal is present. The
fourth means samples upper and lower peak values of the second sensor
signal value for deriving the correction factor by averaging the upper and
lower peak values. The first sensor means monitors an engine speed
indicative parameter and an engine load indicative parameter so that the
third means derives the basic fuel metering amount on the basis of the
engine speed indicative parameter and the engine load indicative
parameter, and the fifth means detects the engine driving range on the
basis of the engine speed and the basic fuel metering amount. The first
sensor means monitors a throttle valve angular position and derives the
engine load indicative parameter on the basis of the throttle valve
angular position and the engine speed.
According to another aspect of the invention, an air/fuel ratio control
system for controlling a mixture ratio of an air/fuel mixture to be
introduced into a combustion chamber in an internal combustion engine,
comprises an air/fuel mixture induction system for introducing an intake
air and a fuel for forming an air/fuel mixture to be supplied into an
engine combustion chamber, the air/fuel mixture delivery system
incorporating a fuel metering means for delivering a controlled amount of
fuel, a first sensor means for monitoring a preselected basic first engine
operation parameter to produce a first sensor signal indicative thereof,
the first sensor signal including an engine load indicative component, a
second sensor means for monitoring an air/fuel mixture ratio indicative
parameter for producing a second sensor signal variable of the value
indicative of a deviation from a threshold value representative of a
stoichiometric value, third means for deriving a basic fuel metering
amount on the basis of the first sensor signal value, fourth means for
deriving a air/fuel ratio dependent correction factor variable of the
value thereof depending upon the second sensor signal value, fifth means
for deriving an air density dependent first correction coefficient on the
basis of the air/fuel ratio dependent correction factor for air/fuel ratio
dependent correction of the basic fuel metering amount, which first
correction coefficient is commonly applicable for correction of the basic
fuel metering amount in over all engine driving ranges, the fifth means
updating the first correction coefficient when a first learning condition
is satisfied, a sixth means for deriving a second correction coefficient
which is variable depending upon the engine driving range on the basis of
the air/fuel ratio dependent correction factor, the sixth means setting a
plurality of the second correction coefficient in relation to respectively
corresponding engine driving range and updating each of the second
correction coefficient with an instantaneous value derived based on the
air/fuel ratio dependent correction factor in the corresponding engine
driving range, a seventh means, associated with the sixth means, for
deriving an altitude dependent correction value for modifying the second
correction value on the basis of the engine load component of the first
sensor signal and a tendency of air/fuel ratio adjustment in a given
cycles of the second sensor signal variations, an eighth means for
correcting the basic fuel metering amount with the correction coefficient
to control the fuel metering means for delivering the fuel in the amount
corresponding to the corrected fuel metering amount to the air/fuel
mixture delivery system.
The seventh means may derive the altitude dependent correction value
constituting a first component variable according to variation to
variation of the engine load and a second component derived depending upon
tendency of richer side or leaner side air/fuel ratio control depending
upon distribution of richer side variation and leaner side variation of
given number of the second correction coefficients updated by the sixth
means in most recent given updating cycles. In the alternative, the
seventh means may derive the altitude dependent correction value
constituting a first component variable according to variation to
variation of the engine load and a second component derived depending upon
tendency of richer side or leaner side air/fuel ratio control depending
upon distribution of the second correction values residing richer side and
leaner side of a predetermined threshold value.
BRIEF DESCRIPTION OF THE DRAWINGS
The present invention will be understood more fully from the detailed
description given herebelow and from the accompanying drawings of the
preferred embodiment of the invention, which, however, should not be taken
to limit the invention to the specific embodiment but are for explanation
and understanding only.
In the drawings:
FIG. 1 is a diagram of the preferred embodiment of a learning air/fuel
ratio control system according to the invention;
FIG. 2 is a block diagram of a control unit employed in the preferred
embodiment of the air/fuel ratio control system of the invention;
FIG. 3 is a flowchart of a routine for deriving and setting a fuel
injection pulse width representative of a fuel injection amount;
FIG. 4 is a block diagram of an input/output unit in the control unit to be
employed in the preferred embodiment of the air/fuel ratio control system
of FIG. 2;
FIG. 5 is a flowchart of a routine for discriminating engine operating
condition for governing control operation mode between FEEDBACK control
mode and OPEN LOOP control mode;
FIG. 6 is a flowchart of a routine for deriving feedback correction
coefficient composed of a proportional component and an integral
component;
FIG. 7 is a flowchart of a learning governing routine for governing
learning of K.sub.ALT and K.sub.MAP ;
FIG. 8 is a flowchart of a K.sub.ALT learning routine for updating a map
storing an air density dependent uniform correction coefficients;
FIG. 9 is a flowchart showing a K.sub.MAP learning routine for updating an
engine driving range based correction coefficients;
FIG. 10 is a timing chart showing operation of the preferred embodiment of
the air/fuel ratio control system of the invention;
FIG. 11 is a flowchart of an automatically modifying routine for K.sub.ALT
for modifying the K.sub.ALT automatically;
FIG. 12 is a chart showing FEEDBACK control range which is defined in terms
of engine speed N and engine load Tp;
FIG. 13 is a chart showing range to perform learning of K.sub.ALT which is
defined by throttle angular position .theta..sub.th, intake air flow rate
Q and engine speed N;
FIGS. 14 and 15 are flowcharts showing a sequence of K.sub.MAP learning
routine as modification of the routine of FIG. 8.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring now to the drawings, particularly to FIGS. 1 and 2, the preferred
embodiment of an air/fuel ratio control system, according to the
invention, is applied to a fuel injection internal combustion engine which
is generally represented by the reference numeral "1". The engine 1 has an
air induction system including an air cleaner 2, a throttle body 3 and an
intake manifold 4. A throttle valve 5 is disposed within the throttle body
3 for adjusting induction rate of an air/fuel mixture.
In the shown embodiment, a fuel injection valve 6 is disposed within the
throttle body 3 and upstream of the throttle valve 5. Therefore, the
air/fuel mixture is formed at the position in the induction system
upstream of the throttle valve. The air/fuel mixture flows through the
throttle body 3 and introduced into an engine combustion chamber via the
intake manifold 4 and an intake port which is open and closed by means of
an intake valve.
The air/fuel mixture introduced into the engine combustion chamber is
combustioned by spark ignition taken place by means of an ignition plug 7
which receives an ignition power from an ignition coil unit 8 via a
distributor 9.
The engine 1 also has an exhaust system including an exhaust manifold 10,
an exhaust duct 11, a catalytic converter unit 12 and a muffler 13.
In order to monitor the angular position of the throttle valve 5, a
throttle angle sensor 15 is associated with the throttle valve 5 to
produce a throttle angle indicative signal .theta..sub.th having a value
indicative of the monitored throttle angle. In practice, the throttle
angle sensor 15 comprises a potentiometer producing analog form throttle
angle indicative signal having a voltage variable depending upon the
throttle valve angular position. Also, an an engine idling condition
detector switch 16 is associated with the throttle valve 5 for detecting
fully closed or approximately fully closed position of the throttle valve.
The engine idling condition detector switch 16 outputs an engine idling
condition indicative signal IDL which is held LOW level while the throttle
valve 5 is not in fully closed or approximately fully closed position and
is held HIGH level while the throttle valve is maintained at fully closed
or approximately fully closed position.
A crank angle sensor 17 is coupled with the distributor 9 for monitoring a
crank shaft angular position. For this, the crank angle sensor 17 has a
rotary disc which is so designed as to rotate synchroneously with rotation
of a rotor of the distributor. The crank angle sensor 17 produces a crank
reference signal .theta..sub.ref at each of predetermined angular position
and a crank position signal .theta..sub.pos at every time of predetermined
angle of angular displacement of the crank shaft. In practice, the crank
reference signal is generated every time the crank shaft is rotated at an
angular position corresponding on 70.degree. or 66.degree. before
top-dead-center (BTDC) in compression stroke of one of engine cylinder.
Therefore, in case of the 6-cylinder engine, the crank reference signal
.theta..sub.ref is produced at every 120.degree. of the crank shaft
angular displacement. On other hand, the crank position .theta..sub.pos,
is generated every given angular displacement, i.e. 1.degree. or
2.degree., of the crank shaft.
An engine coolant temperature sensor 18 is disposed within an engine
cooling chamber to monitor a temperature of an engine coolant filled in
the cooling chamber. The engine coolant temperature sensor 18 is designed
for monitoring the temperature of the engine coolant to produce an engine
coolant temperature indicative signal Tw. In practice, the engine coolant
temperature sensor 18 produces an analog form signal having a voltage
variable depending upon the engine coolant temperature condition. A
vehicle speed sensor 19 monitors a vehicle speed for producing a vehicle
speed indicative signal Vs. Furthermore, the shown embodiment of the
air/fuel ratio control system includes an oxygen sensor 20 disposed in the
exhaust manifold 10. The oxygen sensor 20 monitors oxygen concentration
contained in the exhaust gas to produce an oxygen concentration indicative
signal V.sub.ox indicative of the monitored oxygen concentration. The
oxygen concentration indica | | |