BACKGROUND OF THE INVENTION
[0001] The present invention relates to a control method for fuel injection engines of the
type used in vehicles such as automobiles and more particularly to a fuel injection
control method so designed that the film mass deposited on the wall of the intake
manifold is estimated and the desired fuel injection quantity is determined on the
basis of the estimated film mass.
[0002] The fuel injected from the fuel injection valve is partly deposited on the intake
manifold wall or the fuel deposited as the film mass is vaporized and fed into each
cylinder thus failing to wholly supply the injected fuel into the cylinder and in
particular the quantity of fuel supplied to the engine deviates considerably from
the fuel quantity required from moment during the engine acceleration or deceleration.
[0003] Conventional techniques heretofore proposed for solving this problem include methods
in which the quantity of deposited fuel is estimated and the desired fuel injection
quantity is determined on the basis of the estimated deposited fuel (e.g., a fuel
injection quantity control method for fuel injection engines disclosed in Japanese
Patent Publication No. 58-8238 by Toyota Jidosha Co., Ltd.). In this method, a basic
fuel injection pulse width to injector is determined in accordance with the manifold
pressure and the engine speed and the quantity of film mass in the intake manifold
is estimated on the assumption that the fuel is injected for the duration of the pulse
width. However, the actual quantity of fuel injected into the intake manifold is the
quantity of fuel injected during the time that the injection valve or injector is
opened for the duration of an actual fuel injection pulse width calculated in accordance
with the fuel quantity carried over to the engine cylinder, the deposited fuel quantity,
a feedback correction factor, etc., as well as the basic fuel injection pulse width.
As a result, it is impossible to correctly estimate the actual quantity of film mass
unless the method of estimating the quantity of film mass deposited in the intake
manifold is such that the actually injected fuel quantity is fed back and a part of
the injected fuel quantity is deposited on the intake manifold wall. For these reasons,
the conventional estimating method cannot accurately estimate the quantity of film
mass and therefore there is a disadvantage that the quantity of fuel supplied to the
engine deviates from the required fuel quantity at the moment despite the fact that
the fuel injection quantity also takes the quantity of film mass into consideration.
[0004] Also included among the conventional fuel injection quantity control methods of controlling
the fuel injection quantity by estimating the quantity of film mass are methods in
which the desired fuel injection quantity is determined by subtracting the quantity
delivered to the cylinder or the carry-over quantity from the quantity of film mass
and adding the deposited quantity on the manifold wall to the basic fuel injection
quantity (e.g., Japanese Patent Publication No. 58-8238). In this case, of the quantity
of fuel injected the quantity of fuel deposition on the manifold wall is of such a
nature that it can be accurately determined only after the actual fuel injection quantity
has been determined. While this conventional method determines the deposition quantity
of fuel supposed to deposit on the manifold wall on the basis of a basic fuel injection
pulse width, there is a disadvantage that the fuel deposited on the intake manifold
wall does not represent a part of the actually injected fuel quantity and therefore
it is impossible to accurately determine the quantity of film mass (the quantity of
fuel deposition).
SUMMARY OF THE INVENTION
[0005] It is a first object of the present invention to provide a control method for a fuel
injection engine which controls the quantity of fuel injected in such a manner that
the air-fuel ratio of the mixture supplied to each cylinder attains a desired value
when the quantity of film mass deposited on the intake manifold wall, the deposition
rate or the rate of the film mass deposited on the manifold wall to the injected fuel
and the vaporization rate or the rate of vaporization of the film mass from the manifold
wall have been calculated from various sensor data.
[0006] It is a second object of the invention to provide a method of accurately estimating
the quantity of film mass deposited on the intake manifold wall of an engine so as
to control the quantity of fuel injected such that the quantity of fuel supplied to
the engine always coincides with the required fuel quantity.
[0007] To accomplish the first object, the quantity of injected fuel entering the cylinder
of an engine without depositing on the intake manifold wall is added to the quantity
of fuel entering the cylinder as a result of the vaporization of the deposited film
mass and this fuel quantity is injected as the actual fuel supply to the cylinder
to attain the desired air-fuel ratio in accordance with the mass of air flow to the
engine. Also, to accomplish the second object, the calculated value of a carry-over
fuel quantity delivered to the engine cylinder during the current cycle is subtracted
from the intake manifold wall film mass fuel quantity estimated during the preceding
cycle and then the value of an intake manifold wall fuel deposition per cycle calculated
on the basis of the actual injection quantity per stroke of the engine injected at
the latest moment during the preceding cycle is added to the remaining film mass fuel
quantity.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008]
Fig. 1A is a schematic diagram showing the construction of a fuel injection control
apparatus to which the present invention is applied.
Fig. 1B is a flow chart showing the fuel injection control procedure of the computer
1.
Fig. 2 is a diagram showing the behavior of the inducted air and fuel in the intake
manifold.
Fig. 3 is a block diagram of the fuel injection control system.
Fig. 4 is a flow chart of the ordinary computing processing and interrupt processing.
Figs. 5A to 5C are time charts illustrating the time relationship between the strokes
and the cycle periods.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0009] An embodiment of a control method for a fuel injection engine according to the invention
will now be described with reference to Figs. 1A to 2. Fig. 1A illustrates a schematic
diagram of a fuel injection control apparatus. In the Figure, the mass of air flow
in the intake manifold of an engine is detected by a hot-wire air flow meter 2 and
applied to a computer 1. The computer 1 receives the throttle position from a throttle
position sensor 3, the intake manifold pressure from a manifold pressure sensor 4,
the cooling water temperature from a water temperature sensor 5, the engine speed
from a crank angle sensor 6 and the binary air-fuel ratio signal from an 0
2 sensor 7. The computer 1 directs the desired fuel injection quantity to an injector
8.
[0010] As shown in Fig. 1B, at a step 1, the computer 1 calculates the rate of deposition
of the fuel injection quantity on the intake manifold wall and the rate of vaporization
of the film mass deposited on the intake manifold wall from the following equations
(1) and (2), respectively, according to the inputted data. If the deposition rate
is represented by X and the vaporization rate by 1/
T, the deposition rate X is simply given for example as a function of the throttle
position θth as follows

[0011] On the other hand, the vaporization rate 1/τ is given as a function of the water
temperature T
W as follows

[0012] Here, it is assumed so that 1/
T = 0.026 when T
W ≦ 23°C.
[0013] Then, at a step 102, in accordance with the resulting deposition rate X and vaporization
rate 1/
T, the current film mass quantity is calculated from the film mass quantity obtained
during the preceding cycle and the actually injected fuel quantity as follows

where AT is the computing cycle period, M
f is the film mass quantity, G
f is the fuel injection quantity and G
f·T is the actually injected fuel quantity in terms of the fuel quantity per unit time.
[0014] Then, at a step 103, the fuel injection quantity per unit time is determined in accordance
with the deposition rate and the film mass quantity in the following manner. The fuel
injection quantity of the engine must correspond to the intake air flow and therefore
the desired value of the fuel quantity to be supplied to each cylinder is given as
follows.

where Q
a is the intake air flow, (A/F) is the desired air-fuel ratio and G
fe* is the desired value of the quantity of fuel injected into the engine cylinder. Fig.
2 shows the behavior within the intake manifold of the fuel quantity entering the
engine cylinder. As shown in the Figure, if G
f represents the injected fuel quantity, X·G
f represents the quantity of the fuel deposited on an intake manifold wall 21 and (I
- X)G
f represents the quantity of the fuel supplied to the cylinder without deposition.
Also, M
f/T represents the quantity of fuel supplied to the cylinder by the vaporization of the
previously deposited fuel quantity (film mass quantity) on the intake manifold wall
21. As a result, if the quantity of fuel supplied to the cylinders is represented
by G
fe' then the following equation holds

If the value of G
fe is equal to the fuel quantity G
fe* to be supplied to the cylinder, the desired air-fuel ratio will be attained. Thus,
assuming that the equations (4) and (5) are equal,

[0015] Then, it is only necessary to determine the fuel injection quantity G
f such that the above equation holds. Thus, the following equation holds

[0016] The equation (7) is obtained as follows. The fuel quantity Q
a/(A/F) to be supplied to the cylinder to attain the desired air-fuel ratio is obtained
in accordance with the intake air flow Q
a and the fuel quantity M
f to be carried over to the cylinder is obtained in accordance with the vaporization
rate 1/
T and the film mass quantity M
f. The fuel quantity M
f is subtracted from the fuel quantity Q
a/(A/F) and the difference is divided by the non-deposition rate (1 - X) of the injection
fuel to be supplied to the cylinder without deposition thereby determining the desired
fuel quantity per unit time.
[0017] Since the value of G
f obtained at the step 103 is the fuel injection quantity per unit time, it is then
converted to a fuel injection pulse width per stroke of the engine at a step 104,
as follows

where N is the engine speed, k
i is a coefficient determined by the characteristics of the injector, T is the correction
factor fed back by the 0
2 sensor signal and T is a dead fuel injection time.
[0018] The fuel injection pulse width per stroke T is renewed at intervals of the computing
cycle and therefore the actual fuel injection takes place for the duration of the
fuel injection pulse width T
i existing at the time of arrival of an interrupt signal generated for every stroke.
Therefore, as the fuel injection quantity data required for the computer to calculate
the quantity of film mass during the next cycle, the actual fuel injection pulse width
in terms of the following quantity corresponding to the fuel quantity per unit time
is fed back

The expression (9) is used during the next computing cycle as shown by the equation
(3).
[0019] Fig. 3 illustrates a block diagram of the fuel injection control system in the computer
1 of Fig. lA. In the Figure, a fuel injection quantity per unit time G
f is calculated by computing means 12 in accordance with the film mass estimated by
computing means 13 for estimating the film mass quantity M
f deposited on the intake manifold wall and the mass of air flow. In response to the
signal generated from the 0
2 sensor 7, computing means 14 calculates an air-fuel ratio feedback correction factor
δ = f(O
2) aiming at a stoichiometric air fuel ratio. Computing means 11 calculates the quantity
of fuel injected per stroke as shown by the following equation

where k is a coefficient which is used in the conversion to the fuel injection quantity
per stroke and dependent on the injector characteristics and T
S is a dead injection time.
[0020] The computing means 13 computes the quantity of film mass in the intake manifold
as follows

Here, the right member M
f represents the film mass quantity for the preceding cycle and the left member M
f is the newly estimated film mass quantity. Also, 1/
T represents the rate of vaporization of the film mass and X represents the rate of
fuel deposition on the intake manifold wall to the injected fuel quantity (referred
to as a deposition rate). Represented by AT is one cycle period of the computation
by the blocks of Fig. 3. Thus, the following in the right member represents the quantity
of fuel delivered to the cylinder by the vaporization of the film mass during one
cycle period

[0021] Also, of the quantity of fuel actually injected per unit time the quantity of fuel
deposition during the cycle period is given by the second term of the right member
in the equation (11) or the following expression

While a description will be made later of T·G
f in consideration of the time relationship between the time per stroke and the cycle
period of computation, the fuel injection quantity per unit time
T-G
f resulting from the integration of the feedback correction factor T represents the
quantity of fuel injected per unit time which is renewed in response to the application
of a stroke start signal from the crank angle sensor. While the deposition rate X
and the vaporization rate 1/
T (
T is a vaporization time constant) are obtained by experiments in accordance with the
throttle position 6th, the water temperature T
W, the manifold pressure P, the mass air flow Q
a, etc., in this embodiment the deposition rate X is given as a function of the throttle
position for purposes of simplicity, as follows

[0022] Also, the vaporization rate is given as a function of the water temperature as follows

Here, it is assumed that 1/
T = 0.0266 when T < 23°C.
[0023] As described hereinabove, a feature of the construction of the control system resides,
as will also be seen from Fig. 3, in the fact that the feedback loop for feeding back
the correction factor T in response to the 0
2 sensor signal and the loop of the fuel injection quantity T·G
f for calculating the deposited quantity or the deposited part of the injected fuel
overlap doubly.
[0024] Next, the timing of the injection per stroke and the timing of the computing cycle
will be described. The computational operations shown in Fig. 3 are performed at intervals
of a given period T and the injection pulse width is renewed by injection timing adjusting
means 16 of Fig. 3 at a step 31 of Fig. 4 for every period. The actual injection is
initiated by an interrupt signal INT generated for every stroke. As a result, the
fuel is actually injected for the duration of the most lately calculated injection
pulse width T
i as shown in Figs. 5A to 5C. Figs. 5A to 5C respectively show interrupt signals each
generated for every stroke, injection pulse widths and calculated T-G
f with the lapse of time. In accordance with the embodiment, when an interrupt signal
is applied, the timely existing T-G
f is stored in a T·G
f memory. This operation is performed by injection synchronizing means 15 of Fig. 3
and its timing corresponds to the application of the interrupt signal as shown at
a step 32 of Fig. 4. By performing these operations, the actually injected fuel quantity
is fed back and used for the accurate estimation of the quantity of film mass.
[0025] In accordance with the present invention, the occurrence of lean spikes during the
engine acceleration and the occurrence of rich spikes during the engine deceleration
are eliminated as compared with the conventional method in which a basic fuel injection
quantity is determined in accordance with the flow of intake air. This has the effect
of improving the engine performance during the acceleration and ensuring effective
removal of the harmful gases during the deceleration. Thus, it is possible to reduce
the amount of the three-way catalyst by this method making it also effective economically.
Further, while it has been necessary in the past to prepare various memory maps for
providing acceleration and deceleration corrections on the basis of changes in the
throttle position, etc., and search for the corresponding map values, in accordance
with the present invention the desired acceleration and deceleration corrections can
be provided by matching only the deposition rate of the fuel injection and the vaporization
rate of the film mass in accordance with the acceleration and deceleration air-fuel
ratios and thus the invention has the effect of providing more efficient manufacturing
steps.
[0026] Further, in accordance with the invention, by virtue of the fact that the quantity
of the film mass deposited on the intake manifold wall is estimated by newly estimating
the film mass quantity by using the actually injected fuel quantity, it is possible
to estimate an accurate film mass quantity closer to the actual film mass quantity.
By using the method which determines the desired fuel injection quantity in consideration
of such estimated film mass, the air-fuel ratio of the mixture supplied to the engine
can be controlled at around the stoichiometric air-fuel ratio even during the engine
acceleration and deceleration. Thus, the invention has the effect of improving the
exhaust gas purification and the engine performance.