Electronic control unit for internal combustion engine

Internal-combustion engines – Spark ignition timing control – Electronic control

Reexamination Certificate

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Details

C073S117020, C123S406530, C123S406550, C123S479000

Reexamination Certificate

active

06170462

ABSTRACT:

BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to an electronic control unit for an internal combustion engine that identifies cylinders and detects crank angles from signals issued by a crank angle sensor.
2. Description of the Related Art
A signal in synchronization with the revolution of an engine is used to control the ignition timing, fuel injection, etc., of an internal combustion engine. A generator producing the signal usually detects the revolution of a camshaft or a crankshaft of the engine. An example of a crank angle sensor is shown in FIG.
5
and FIG.
6
. The crank angle sensor shown in these figures includes a rotary shaft
1
being rotatable in synchronization with an engine (not shown), a rotary disc
2
mounted on the rotary shaft and provided with a window
3
at a location corresponding to a desired detection angle, a light emitting diode
4
, a photodiode
5
for receiving the light emitted from the light emitting diode
4
, an amplifier circuit
6
connected to the photodiode
5
for amplifying an output signal of the photodiode
5
, and an output transistor
7
connected to the amplifier circuit
6
and having an open collector. A window
3
′ for identifying a particular cylinder is provided in the rotary disc
2
so that it is asymmetrical to the window
3
so as to identify another cylinder.
Thus, the crank angle sensor outputs a signal illustrated in FIG.
7
. The signal indicates that the falling edge of the signal for a particular cylinder, namely, cylinder #
1
, is offset 10 degrees toward delay side (ATDC 5 degrees or 5 degrees after the top dead center) from other cylinders, namely, cylinder #
2
, cylinder #
3
, and cylinder #
4
. The rising edge of the signal for all the cylinders is BTDC 75 degrees or 75 degrees before top dead center.
Referring now to FIG.
8
and
FIG. 9
, the operation for identifying a particular cylinder will be described. As shown in
FIG. 8
, the output signal of a crank angle sensor
8
is supplied to a microcomputer
10
via an interface circuit
9
. The microcomputer
10
identifies the cylinder according to a flowchart shown in FIG.
9
. First, in step S
1
, a high-level output period t and its rising section cycle T of a signal waveform shown in
FIG. 7
are calculated. Then, the sequence proceeds to step S
2
wherein a ratio t/T is calculated. Subsequently, in step S
3
, a mean threshold value &agr;n that gives t1/T>&agr;>t0/T is provided, and &agr;n is determined according to the following operational expression:
&agr;
n=
(1
−k
)&agr;
n−
1
+k
(
t/T
)
n where k=a constant
The value of &agr;n calculated in step S
3
is compared with the ratio t/T (step S
4
), and if t/T−&agr;n>0, then it is discriminated that the cylinder is the particular cylinder and an identification flag is set (step S
5
). If it is found in step S
4
that t/T−&agr;n<0, then it is determined that the cylinder is a different (i.e., non-particular) cylinder.
In the conventional cylinder identification apparatus for an internal combustion engine, if the duty of a signal in relation to the output signal cycle corresponding to a cylinder that is obtained from the crank angle sensor should indicate an abnormal value due to a fluctuating revolution of the engine or the like, then this is undesirably reflected on the threshold value &agr;n, posing a problem in that, even after the duty of the signal restores a normal value, the influence by the foregoing abnormal value stays on, resulting in erroneous determination.
A solution to the aforesaid problem has been proposed in Japanese Examined Patent Publication No. 6-84739. The second conventional prior art example is designed so that, if an abnormal signal duty occurs, then it is inhibited from affecting the calculation of a threshold value to thereby permit quick and accurate identification of a cylinder.
FIG. 10
is a simplified block diagram of a cylinder identification apparatus for an internal combustion engine in accordance with the conventional art, and
FIG. 11
is a flowchart illustrating a cylinder identification routine effected by the cylinder identification apparatus.
The cylinder identification apparatus shown in
FIG. 10
includes the same components
8
and
9
as those of the first prior art example, a microcomputer
10
A, an operational calculator or calculating means
11
, a comparator or comparing means
12
, and a cylinder identifier or cylinder identifying means
13
.
Referring to the flowchart of
FIG. 11
, the cylinder identification operation performed by the cylinder identification apparatus for an internal combustion engine configured as discussed above will be described. The microcomputer
10
A shown in
FIG. 10
calculates, by the calculating means
11
, the values of a high-level output period t and its rising section cycle T of a signal sent from the crank angle sensor
8
via the interface circuit
9
according to
FIG. 2
(step S
1
).
Then in step S
2
, by using the calculating means
11
, a ratio t/T is calculated on each cylinder by adopting t and T, which have been determined in step S
1
. In step S
6
, it is determined by the comparing means
12
whether or not the ratio t/T lies within a specified range; if the t/T has been found to lie outside the specified range, then the present ratio t/T is set to a specified value in step S
7
. In other words, step S
7
involves a calculation inhibiting means for inhibiting the value of the present ratio t/T from being reflected in the calculation of the threshold value &agr;n if the value of the present ratio t/T turns out to be abnormal. The microcomputer
10
A then advances to step S
3
wherein it causes the calculating means
12
to calculate a mean threshold value [&agr;n=(1−k)&agr;n−1+k(t/T)n] that is the mean value of the ratios of all cylinders based on the specified value.
On the other hand, if the value of t/T obtained in step S
6
is found to lie within the specified range, then the foregoing mean threshold value &agr;n is calculated based on the value of the present ratio t/T by the calculating means
12
. In step S
4
and step S
5
, the same operation as that in the conventional art is carried out, and the value of the ratio for each cylinder, which has been obtained as mentioned above, is compared with the mean threshold value &agr;n (step S
4
), and if the comparison result indicates that the former is larger than the latter, then the cylinder is identified as a particular cylinder. In this case, cylinder #
1
is identified and a flag is set at a register corresponding to cylinder #
1
(step S
5
). If the comparison result indicates that the former is smaller than the latter, then the process returns. Thus, when a particular cylinder or cylinder #
1
in this case has been identified, revolution signals will be obtained in the order of cylinder #
1
, cylinder #
3
, cylinder #
4
, and cylinder #
2
, so that the remaining cylinders can be identified in the order of cylinder #
3
, cylinder #
4
, and cylinder #
2
.
The cylinder identification technique discussed above enables accurate determination even if the signal duty should have an abnormal value due to fluctuations in revolution of an engine since the abnormal value is not reflected on the calculation of the mean threshold value.
The second conventional art, however, has the following shortcoming.
If an engine is started while it is cold or with a deteriorated battery or the like, marked cyclic variation is observed in the revolution of the engine. This may sometimes lead to cylinder identification errors, resulting in improper ignition, erroneous fuel injection, or other improper engine control.
Also if a hastened engine start is made or if hastened engine start is repeated, marked cyclic fluctuations in revolution may take place or the revolution of an engine may be reversed. This is also likely to lead to cylinder identification errors with a resultant possibility of errone

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