FUEL CONTROL APPARATUS FOR INTERNAL COMBUSTION ENGINES

Abstract: Disclosed is a fuel control apparatus in an internal combustion engine. When the running mode the engine is changed into acceleration again from decelera­ tion after acceleration, the fuel becomes too rich if the conventional continuous correcting factor (k CNT = 1.0) is used. In order to properly reduce the quantity of fuel supply in that case, the number of engine revolutions is counted from a point (a) of initiation of deceleration to a point (b) of initiation of acceleration again to there­ by calculate a proper value of the continuous correcting factor (k CNT ) corresponding to the count (CNT max ), so that fuel is supplied to the internal combustion engine (E) with a quantity corrected by the thus calculated value of the continuous correcting factor (k CNT ).

Description: Fuel control apparatus for internal combustion engines The present invention relates to a fuel control apparatus for internal combustion engines, and particularly to a fuel control apparatus which is suitable to obtain an optimum air-fuel ratio ("A/F") in acceleration again through deceleration after acceleration. Generally, the air flow rate changes in proportion to the opening of the throttle valve. However, even if the throttle valve is fully closed from a fully opened state, the air flow cannot immediately respond to the closure of the throttle valve but responds with a temporal delay. This is because the suction air path has a non-negligible length between the throttle valve and an air flow rate sensor which is provided upstream the throttle valve. Accordingly, in spite of the fact that the value A/F should be made rich when the throttle valve is moved toward the open side, that is, when the engine is accelerated, the value of A/F cannot be made so rich as to sufficiently accelerate the engine even if an optimum fuel supply quantity calculated on the basis of the suction air quantity detected by the air flow rate sensor is injected through the fuel injector. Therefore, the control delay due to determination of the fuel supply quantity by means of the air flow rate sensor has been conventionally corrected by increasing the opening of the throttle valve. Conventionally, in a system in which acceleration correction is performed by using a throttle sensor as disclosed in No. JP-A-58-185949, so-called constant acceleration correction in which the quantity of change per predetermined time unit, that is, the quantity of the differential quotient, of the output of the throttle sensor, is detected, and the fuel supply quantity calculated on the basis of the suction air quantity detected by the air flow rate sensor is multiplied by a certain factor (for example, 1.1) to thereby increase the fuel supply quantity when the change of rate of the output of the throttle sensor exceeds a predetermined value. Thus, in the conventional acceleration correction, even in the case where after acceleration, deceleration is once performed for a short time and then it is accelerated again, the fuel supply is increased by the same quantity as during the first acceleration. However, the whole of the increased fuel injected upstream the throttle valve is not evaporated so as to be sucked into a cylinder, but some of the fuel is liquefied and adheres to the side wall of the carburetor. Accordingly, if the fuel supply is increased by the same quantity as during the first time acceleration when it has to be accelerated again after a deceleration following a previous acceleration, the fuel becomes so disadvantageously rich that not only the fuel consumption rate becomes poor but complete combustion cannot be obtained, and the exhaust gas characteristics become poor. Gasoline atomized in the vicinity of the throttle chamber partially adheres thereto in liquid form in a quantity of several percent, and the remainder quantity of the gasoline is sucked into the engine through the intake manifold. On the contrary, the adhering fuel is evaporated by several percent of the whole quantity thereof and sucked into the engine together with the atomized fuel so as to contribute to the combustion. Accordingly, when the engine is in a steady state, the whole quantity of adhering fuel is constant and is called an equilibrated adhering quantity (hereinafter simply referred to "MFH"). The MFH is a function of the cooling water temperature and the load (it may be considered as a negative pressure quantity), so that MFH is large when the engine output is high, while it is small when the engine output is low. When acceleration is made by increasing the opening degree of the throttle valve, fuel is used for filling the quantity of increase of the MFH even if the fuel is injected in a quantity corresponding to the suction air quantity, so that the air-fuel mixture actually sucked into the engine becomes lean. To correct this state, the quantity of fuel to be injected is increased by a small quantity. This acceleration is called "increased-fuel acceleration". Different equations describing the dynamic process of wall wetting in internal combustion engines are disclosed in EP-A-152 019. It is an object of the present invention to solve the problems of the prior art as described above and to provide a fuel control apparatus for internal combustion engines which can properly control the air-fuel ratio when the engine is accelerated a short time after deceleration following a previous acceleration. The above object is achieved according to claim 1; the dependent claims relate to preferred embodiments. In accordance with the invention, the rate of increase of fuel supply is lowered when the engine is accelerated again within a predetermined time after deceleration, because when the engine is accelerated again a predetermined time after deceleration, it is not necessary to increase the fuel supply with the rate of increase used during the preceding acceleration because of the existence of vapored fuel attached on an inner wall surface of a carburetor at that time. Accordingly, when acceleration is detected again after deceleration before the integral value of the number of engine revolutions reaches a predetermined value, the predetermined quantity of increasing the fuel supply is reduced in accordance with the value of this count value. In the following, the invention will be described with reference to preferred embodiments and the drawings. Fig. 1 is a schematic front view showing the principal arrangement of a fuel control system to which the fuel control apparatus according to the present invention is applicable; Fig. 2 is an operational waveform diagram for explaining the operation of an embodiment of the fuel control apparatus according to the present invention; Fig. 3 is a graph showing the relation between the continuous acceleration correction factor and the integrated value of the number of engine revolutions in the embodiment according to the present invention; Fig. 4 is a flow-chart for obtaining the continuous acceleration correction factor; and Fig. 5 is a perspective view showing a map for obtaining the continuous acceleration correction factor. Fig. 1 shows a carburetor system to which the present invention is applicable. In the drawing, the quantity of air sucked into the engine E is measured by means of an air flow rate sensor 1, and the value measured by the air flow rate sensor 1 is introduced into a control unit 2. The control unit 2 counts the pulses generated from a crank angle sensor so as to obtain the number of engine revolutions N, calculates the quantity of fuel supply corresponding to the value of N, and then applies the pulses having a pulse width corresponding to the calculated fuel supply quantity to an injector 3. The injector 3 injects fuel of a quantity corresponding to the pulse width of the pulse applied thereto. The basic pulse width T P applied to the injector 3 can be expressed by the following equation 1: wherein Q A . N, and k represent the quantity of suction air, the engine revolutional speed, and a constant, respectively. The control unit 2 further samples the output of a throttle sensor 5 representing the opening degree of a throttle valve 4 every T₁ (for example, 10 ms to thereby detect a change in the quantity of the throttle opening in the time of T₁ . The control unit 2 regards the running state as acceleration and selects a proper one of values of an acceleration correcting factor k D set in advance when the following expression is satisfied: where ϑ X and ϑ X-1 represent the latest value of the throttle opening and the value of throttle opening before T₁ ms, respectively. The value of the acceleration correction factor k D is determined on the basis of the engine speed, the throttle opening, and the rate of change of the throttle opening. The value is obtained in advance. The basis injection pulse width T P is corrected according to the following equation: wherein T i represents the corrected injection pulse width, and k CNT represents a continuous acceleration correction factor which will be described later. Fig. 2 shows a throttle sensor pattern for continuous accelerations and decelerations. It is assumed that the throttle sensor output voltage TV ο changes in accordance with the opening/closing operation of the throttle valve as shown in Fig. 2A. First, when acceleration is detected on the basis of the rate of change of TV ο of the throttle sensor voltage, the acceleration fuel increase is immediately performed with a continuous acceleration correction factor k CNT of 1.0. Next, when the running state is changed into deceleration at point a in Fig. 2, the acceleration correction factor k D is made zero, and the integration of the number of crank shaft revolutions represented by curve B in Fig. 2 is initiated from a point c corresponding to the above-mentioned point a . This integration of the number of crank shaft revolutions is continued to a point d corresponding to a point b of next acceleration. The count or the value of integration at the point d is CNT max1 . A continuous acceleration correction factor is determined in accordance with the continuous acceleration correction characteristics shown in Fig. 3 on the basis of the integrated value of the number of engine crank shaft revolutions at that time. That is, for example, g(CNT max1 ) which is 0.6 times of the normal value of the continuous acceleration correction factor k CNT used as the continuous acceleration correction factor at that time. Thus, a value of 0.6 which is smaller than 1.0, is given as the value of the acceleration correction factor in the range from the point b to the point f in the curve C of Fig. 2. If acceleration is performed from the point b , and then deceleration is effected again from the point g in curve A, the integration of the number of crank shaft revolutions is initiated again from point h corresponding to the point g and continued till next acceleration is detected again. A continuous acceleration correction factor of, for example, 0.8 is then determined in accordance with the continuous acceleration correction characteristics of Fig. 3 on the basis of the integrated value of the number of crank shaft revolutions CNT max2 at that time. When the count CNT max2 exceeds a predetermined value (for example, 50), the continuous acceleration correcting factor is never corrected (region k of curve C in Fig. 2). Fig. 4 is a flowchart for calculating the continuous acceleration correction factor k CNT . According to this process, a judgement is made in a step 100 as to whether acceleration is detected or not. When no acceleration is detected, the count of a counter CNT is incremented by the number N of crank shaft revolutions so that the number of crank shaft revolutions is integrated in step 101. When acceleration is detected in step 100, on the contrary, the maximum value (CNT max ) of the counter CNT is registered in step 102, and the counter CNT is cleared in step 103. Next, a judgement is made in step 104 as to whether detection of deceleration has been recorded or not in the period of stopping acceleration. If there is no record, the flow is ended, and the counter CNT is incremented by the number of engine revolutions (CNT max3 ). If the judgement proves that there is a record of detection of deceleration in the period of stopping acceleration, that is, if the judgement proves that there is the second-time acceleration starting from point b or a point I, in step 104, a continuous acceleration correction factor g (CNT max ) is calculated by reducing the continuous acceleration correction factor k CNT corresponding to the count of the counter CNT and puts the calculated value out. The value of the continuous acceleration correction factor k CNT can be obtained by reading of a table. That is, various values of k CNT corresponding to various representative points of CNT max are stored in advance, so that a proper value of k CNT corresponding to the value of CNT max can be read out of the stored values. A proper value of k CNT corresponding to an intermediate value between two adjacent stored values of CNT max can be obtained by interpolation calculation. A map M can be used instead of the table. That is, since the above-mentioned equilibrated adhering quantity (MFH) is a function of the engine cooling water temperature TW, a map can be made as shown in Fig. 5, by preparing a plurality of tables of the relation between CNT max and k CNT for various values of the engine cooling water temperature. Although a sensor for detecting the throttle valve opening degree is used as means for detecting an acceleration state in the embodiment described above, the air flow rate sensor 1 (Fig. 1) or a pressure sensor 6 (Fig. 1) detecting the pressure in the throttle chamber may be used in place of the throttle sensor. As described above, according to the present invention, the air fuel ratio can be optimized for subsequent acceleration and deceleration states in a short time after deceleration.

Claims: A fuel control apparatus for injection-type internal combustion engines for controlling the amount of fuel to be injected in dependence of the engine rotational speed (N) and the intake air amount (Q A )which is designed to perform an acceleration correction of the fuel amount to be injected (T P ), comprising detection means (2, 5) for detecting acceleration and deceleration of the engine (E), calculation means (2; 104, 105) for determining a correction factor for correcting the fuel amount (T P ) to be injected, and fuel supply means (3) for supplying fuel to the engine in accordance with an output of the calculation means (2; 104, 105), characterized in that counting means (CNT; 102, 103) are provided which are arranged to count the number of engine revolutions (CNT max ) from a point in time (c, h) when deceleration is detected immediately or within a predetermined time after a previous acceleration until a point in time (d, I) when the next acceleration is detected, a map is provided comprising stored values of a continuous acceleration correction factor (k CNT ) < 1,0 as a function of values of the number of engine revolutions (CNT max ) in such a dependence that k CNT is increased with increasing CNT max , and the calculation means (2; 104, 105) are arranged to read out the continuous acceleration correction factor for the respective count CNT max from the map, and to perform therewith a multiplicative correction of the amount of fuel to be injected (T P ) (Figs. 2, 3). The fuel control apparatus according to claim 1, characterized in that the detection means (2) include a throttle sensor (5) detecting the opening of the throttle valve (4). The fuel control apparatus according to claim 1, characterized in that the detection means (2) include an air flow rate sensor (1) detecting the air flow rate. The fuel control apparatus according to claim 1, characterized in that the detection means (2) include a pressure sensor (6) detecting the pressure in the throttle chamber. The fuel control apparatus according to one of claims 1 to 4, characterized in that the map comprises a plurality of tables of values of the continuous acceleration correction factor (k CNT ) as a function of the number of engine revolutions (CNT max ) for various values of the engine cooling water temperature (TW). The fuel control apparatus according to one of claims 1 to 5, characterized in that the counting means (CNT; 102, 103) are arranged to increment the count of the counter (CNT, 101) by the number of engine revolutions (CNT max 3 ) when no deceleration has been detected after stoppage of acceleration (Fig. 4).

Inventors: HATANAKA, KEIJI, MIYAKE, JUNJI, MORITA, KIYOMI, SAKUMA, KIYOTOSHI
Applicants: HITACHI, LTD.
Application year: 1987
Main classification: F02D41
IPC codes: F02D41