EP0106366A2 - Méthode de controle pour moteurs à combustion interne - Google Patents

Méthode de controle pour moteurs à combustion interne Download PDF

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Publication number
EP0106366A2
EP0106366A2 EP83110424A EP83110424A EP0106366A2 EP 0106366 A2 EP0106366 A2 EP 0106366A2 EP 83110424 A EP83110424 A EP 83110424A EP 83110424 A EP83110424 A EP 83110424A EP 0106366 A2 EP0106366 A2 EP 0106366A2
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EP
European Patent Office
Prior art keywords
task
engine
acceleration
amount
fuel injection
Prior art date
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Application number
EP83110424A
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German (de)
English (en)
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EP0106366B1 (fr
EP0106366A3 (en
Inventor
Mineo Kashiwaya
Kiyomi Morita
Masahide Sakamoto
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Hitachi Ltd
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Hitachi Ltd
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Priority claimed from JP57182904A external-priority patent/JPS5974339A/ja
Priority claimed from JP18290282A external-priority patent/JPS5974337A/ja
Application filed by Hitachi Ltd filed Critical Hitachi Ltd
Publication of EP0106366A2 publication Critical patent/EP0106366A2/fr
Publication of EP0106366A3 publication Critical patent/EP0106366A3/en
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/24—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means
    • F02D41/26—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using computer, e.g. microprocessor
    • F02D41/263—Electrical control of supply of combustible mixture or its constituents characterised by the use of digital means using computer, e.g. microprocessor the program execution being modifiable by physical parameters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/02—Circuit arrangements for generating control signals
    • F02D41/04—Introducing corrections for particular operating conditions
    • F02D41/10—Introducing corrections for particular operating conditions for acceleration
    • F02D41/105—Introducing corrections for particular operating conditions for acceleration using asynchronous injection

Definitions

  • the present invention relates to a fuel control apparatus employing a microcomputer, and, more particularly, to a fuel injection apparatus in which additional fuel for acceleration compensation is injected in accordance with the state of acceleration detected on the basis of the opening of a throttle valve.
  • a general purpose software that is a software in which correction, modification or addition can be effected onto the various control functions depending on the kind/use of car, is required in view of improvement in cost and/or in controllability.
  • the amount of suction air in an engine has been indirectly detected on the basis of the pressure in a suction manifold, or the total amount of suchtion air per suction stroke nas been obtained by directly detecting the air flow rate.
  • the accuracy is poor, the variations and/or deterioration in performence of engine may affect the detection, and the responsibility is not so good.
  • the latter method also has a disadvantage that a flow rate sensor having high accuracy (error: within + 1% of read value) and a wide dynamic range (1:50) is required, resulting in increase in cost.
  • hot-wire sensor a so-called hot-wire type flow rate sensor (hereinafter referred to as a hot-wire sensor) as the flow rate sensor, becuase the hot-wire sensor has a characteristic allowing a wide dynamic range and reduction in cost can be expected.
  • the suction air flow rate in engine is not constant but has pulsations, so that the output signal from a flow rate sensor has a non-linear charactristic with respect to the suction air flow, it becomes necessary to obtain the air flow rate in suction stroke in the form of integration of instantaneous air flow rates, and complex operations are required for the integration. That is, the hot-wire output voltages v shown in Fig. 1 can be obtained according to the following equation (1) : where q A represents the mass flow rate and C 1 , C 2 represent constants determined by the shape of intake manifold etc. This equation (1) can be changed into the following equation (2) :
  • the average or mean air flow rate in one suction stroke Q A can be expressed as follows: where A6 represents a crank angle between two adjacent sampling points of q A .
  • the amount of fuel injection Q F for one suction stroke can be expressed by the following equation (7) : where N represents the number of engine revolution and k a constant. This means that the amount of fuel injection Q F for one stroke can be determined on the basis of the obtained value of Q A and the number of engine revolution N.
  • the basic fuel injection amount Q F can be obtained in such a manner as described above, acceleration can not be smoothly effected by using only the thus obtained basic fuel injection amount Q F when acceleration becomes necessary, because of delay in computation of the value Q A , etc. It has been effected, therefore, to compensate the basic fuel injection amount in accordance with the detection of the state of acceleration on the basis of the change in the take-in amount of Q A .
  • the suction air flow rate Q A has pulsations as described above and an error may occur in detection of the state of acceleration. This applies to the case of decelerating operation. Therefore, the state of acceleration or deceleration is detected on the basis of the detection of the opening of the throttle valve.
  • the throttle opening TH is sampled at a predetermined regular interval of time, for example every 10 msec, (by interval interruption) so that the sampling value TH at present is compared every 10 msec with the sampling value TH(OLD) sampled before 30 msec to obtain the difference ⁇ TH therebetween and judgement is made such that the engine is in the state of acceleration when ATH > 0.
  • the additional fuel injection has been performed at the time of acceleration in accordance with the predetermined condition of the throttle opening change rate regardless of the operating conditions such as the engine speed or load.
  • the basic amount of fuel injection at low engine speed is smaller than that at high engine speed, it is difficult to accelerate the car sufficiently when the engine speed is low just before acceleration. This is because, at low engine speed, the basic amount of fuel injection is so small that it takes some time to wet the intake manifold well thereby making the fuel air mixture lean at the beginning of acceleration. This is also the case with the acceleration from an idle or decelerating state.
  • the additional fuel injection amount in acceleration is increased in accordance with the engine operating conditions just before acceleration.
  • a control apparatus for the whole of an engine system is illustrated.
  • suction air is supplied to a cylinder 8 through an air cleaner 2, a throttle chamber 4, and a suction pipe 6.
  • a gas burnt in the cylinder 8 is dishcarged from the cylinder 8 to the atomospher through an exhaust pipe 10.
  • An injector 12 for injecting fuel is provided in the throttle chamber 4. The fuel injected from the injector 12 is atomized in an air path of the throttle chamber 4 and mixed with the suction air to form a fuel-air mixture which is in turn supplied to a combustion chamber of the cylinder 8 through the suction pipe 6 when a suction valve 20 is opened.
  • Throttle valves 14 and 16 are provided in the vicinity of the output of the injector 12.
  • the throttle valve 14 is arragned so as to mechanically_interlocked with an accelerator pedal (not shown) so as to be driven by the driver.
  • the throttle valve 16 is arranged to be ariven by a diaphragm 18 such that it becomes its fully close state in a range where the air flow rate is small, and as the air flow rate increases the negative pressure applied to the diaphragm 18 also increases so that the throttle valve 16 begins to open, thereby suppressing the increase of suction resistance.
  • An air path 22 is provided at the upper stream of the throttle valves 14 and 16 of the throttle chamber 4 and an electrical heater 24 constituting a thermal air flow rate meter is provided in the air path 22 so as to derive from the heater 24 and electric signal which changes in accordance with the air flow velocity which is determined by the relation between the air flow velocity and the amount of heat transmission of the heater 24.
  • the heater 24 Being provided in the air path 22, the heater 24 is protected from the high temperature gas generated in the period of back fire of the cylinder 8 as well as from the pollution by dust or the like in the suction air.
  • the outlet of the air path 22 is opened in the vicinity of the narrowest portion of the venturi and the inlet of the same is opened at the upper stream of the venturi.
  • Throttle opening'sensors (not shown in Fig.3 but generally represented by a throttle opening sensor 116 in Fig.5) are respectively provided in the throttle valves 14 and 16 for detecting the opening thereof and the detection signals from these throttle opening sensors, that is the sensor 116, are taken into a multiplexer 120 of a first analog-to-digital converter as shown in Fig.5.
  • the fuel to be supplied to the injector 12 is first supplied to a fuel pressure regulator 38 from a fuel tank 30 through a fuel pump 32, a fuel damper 34, and a filter 36. Pressurized fuel is supplied from the fuel pressure regulator 38 to the injector 12 through a pipe 40 on one hand and fuel is returned on the other hand from the fuel pressure regulator 38 to the fuel tank 30 through a return pipe 42 so as to maintain constant the difference between the pressure in the suction pipe 6 into which fuel is injected from the injector 12 and the pressure of the fuel supplied to the injector 12.
  • the fule-air mixture sucked through the suction valve 20 is compressed by a piston 50, burnt by a spark produced by an ignition plug 52, and the combustion is converted into kinetic energy.
  • the cylinder 8 is cooled by cooling water 54, the temperature of the cooling water is measured by a water temperature sensor 56, and the measured value is utilized as an engine temperature.
  • a high voltage is applied from an ignition coil 58 to the ignition plug 52 in agreement with the ignition timing.
  • a crank angle sensor (not shown) for producing a reference angle signal at a regular interval of predetermine7u crank angles (for example 180 degrees) and a position signal at a regular interval of a predetermined unit crank angle (for example 0.5 degrees) in accordance with the rotation of engine, is provided on a not-shown crank shaft.
  • the output of the crank angle sensor, the output 56A of the water temperature sensor 56, and the electrical signal from the heater 24 are inputted into a control circuit 64 constituted by a microcomputer or the like so that the injector 12 and the ignition coil 58 are driven by the output of this control circuit 64.
  • a bypass 26 bypassing the throttle valve 16 to communicate with the suction pipe 6 is provided and a bypass valve 62 is provided in the bypass 26.
  • a control signal is inputted to a drive section of the bypass valve 62 from the control circuit 64 to control the opening of the bypass valve 62.
  • the opening of the bypass valve 62 is controlled by a pulse current such that the cross- sectional area of the bypass 26 is changed by the amount of lift of valve which is in turn controlled by a drive system driven by the output of the control circuit 64. That is, the control circuit 64 produces an open/close period signal for controlling the drive system so that the drive system responds to this open/close period signal to apply a control signal for controlling the amount of lift of the bypass valve 62 to the drive section of the bypass valve 62.
  • a pulse current is supplied to a power transistor 72 through an amplifier 68 to energize this transistor 72 so that a primary coil pulse current flows into an ignition coil 58 from a battery 66.
  • the transistor 74 is turned off so as to generate a high voltage at the secondary coil of the ignition coil 58.
  • This high voltage is distributed through a distributor 70 to ignition plugs 52 provided at the respective cylinders in the engine, in synchronism with the rotation of the engine.
  • a predetermined negative pressure of a negative pressure source 80 is applied to an EGR control valve 86 through a pressure control valve 84.
  • the pressure control valve 84 controls the ratio with which the predetermined negative pressure of the negative pressure source is released to the atomosphere 88, in response to the ON duty factor of the repetitive pulse applied to a transistor 90, so as to control the state of application of the negative pressure pulse to the EGR control valve 86. Accordingly, the negative pressure applied to the EGR control valve 86 is determined by the ON duty factor of the transistor 90 per se.
  • the amount of EGR from the exhaust pipe 10 to the suction pipe 6 is controlled by the controlled negative pressure of the pressure control valve 84.
  • Fig.5 is a diagram showing the whole configuration of the control system which is constituted by a central processing unit (hereinafter abbreviated as CPU ) 102, a read only memory (hereinafter abbreviated as a ROM ) 104, a random access memory (hereinafter abbreviated as RAM) 106, and an input/output (hereinafter abbreviated as I/O) circuit 108.
  • the CPU 102 operates input date from the I/O circuit 108 in accordance with various programs stored in the ROM 104 and returns the result of operation to the I/O circuit 108.
  • Temporary data storage necessary for such an operation is performed by using the RAM 106.
  • Exchange of various data among the CPU 102, the ROM 104, the RAM 106, and the I/O circuit 108 is performed through a bus line 110 constituted by a data bus, a control bus, and an address bus.
  • the I/O circuit 108 includes input means such as the above-mentioned first analog-to-digital converter (hereinafter abbreviated as ADC1), a second analog-to-digital converter (hereinafter abbreviated as ADC2), an angular signal processing circuit 126, and a discrete I/O circuit (hereinafter abbreviated as DIO) for inputting/outputting one bit information.
  • ADC1 first analog-to-digital converter
  • ADC2 second analog-to-digital converter
  • DIO discrete I/O circuit
  • the digital value of the output of the ADC 122 is stored in a register (hereinafter abbreviated as REG) 124.
  • An output signal of an air flow rate sensor (hereinafter abbreviated as AFS) 24 is inputted to the ADC2 in which the signal is A/D converted in an ADC 128 and set in a REG 130.
  • AFS air flow rate sensor
  • An angle sensor (hereinafter abbreviated as ANGS) 146 produces a reference signal representing a reference crank angle (hereinafter abbreviated as REF), for example as a signal generated at an interval of 180 degrees of crank angle, and a position signal representing a small crank angle (hereinafter abbreviated as POS), for example 1 (one) degree.
  • REF reference crank angle
  • POS position signal representing a small crank angle
  • the REF and POS are applied to the angular signal processing circuit 126 to be waveform-shaped therein.
  • IDLE-SW idle switch 148
  • TOP-SW top gear switch
  • START-SW starter switch
  • An injector circuit (hereinafter abbreviated as INJC) 134 is provided for converting the digital value of the result of operation into a pulse output. Accordingly, a pulse having a pulse width corresponding to the amount of fuel injection is generated in the I N JC 134 and applied to the injector 12 through an AND gate 136.
  • An ignition pulse generating circuit (hereinafter abbreviated as IGNC) 138 includes a register (hereinafter referred to as ADV) for setting ignition timing and another register (hereinafter referred to as DWL) for setting initiating timing of the primary current conduction of the ignition coil 58 and these data are set by the CPU 102.
  • the ignition pulse generating circuit 138 produces a pulse on the basis of the thus set data and supplies this pulse through an AND gate 140 to the amplifier 68 described in detail with respect to Fig.3.
  • the rate of opening of the bypass valve 62 is controlled by a pulse supplied thereto by a control circuit (hereinafter referred to as ISCC) 142 through an AND gate 144.
  • the ISCC 142 has a register ISCD for setting a pulse width and another register ISCP for setting a repetitive pulse period.
  • the output pulse of the EGRC 154 is applied to the transistor 90 through an AND gate 156.
  • the one-bit I/O signals are controlled by the circuit DIO.
  • the I/O signals include the respective output signals of the IDLE-SW 148, the TOP-SW 150 and the START-SW 152 as input signals, and include a pulse signal for controlling the fuel pump 32 as an output signal.
  • the DIO includes a register DDR for determining whether a terminal be used as a data inputting one or a data outputting one, and another register DOUT for latching the output data.
  • a register (hereinafter referred to as MOD) 160 is provided for holding commands instructing various internal states of the I/O circuit 108 and arranged such that, for example, all the AND gates 136, 140, 144, and 156 are turned on/off by setting a command into the NOD 160.
  • the stoppage/start of the respective outputs of the INJC 134, IGNC 138, and ISCC 142 can be thus controlled by setting a command into the MOD 160.
  • Fig.6 is a diagram illustrating a basic configuration of a program system of the control circuit of Fig.6.
  • an initial processing program 202 is for executing preprocessing for causing a microcomputer to operate.
  • the initial processing program 202 for example, the contents of storage of the RAM 106 is cleared, the initial values of registers in the I/0 interface circuit 108 are set, and processing for taking-in data, such as the cooling water temperature Tw, the battery voltage, for performing the preprocessing necessary for performing the engine control is executed.
  • the interruption processing program 206 receives various interruptions, analyzes the factors of the interruptions, and produces a request for causing a desired one of tasks 210 to 226 to the task dispatcher 208.
  • the interruption factors include an A/ D conversion interruption (ADC) generated upon the completion of A/D conversion of the input data such as the power source voltage, the cooling water temperature as described later, an initial interruption (INTL) generated in synchronism with the engine revolution, an interval interruption (INTV) generated at a predetermined interval of time, for example every 10 msec, an engine stoppage interruption (ENST) generated upon the detection of the engine stoppage, or the like.
  • ADC A/ D conversion interruption
  • INTL initial interruption
  • INTV interval interruption
  • ENST engine stoppage interruption
  • Task numbers representing priority are allotted to the tasks 210 to 226, and the respective tasks belong to any one of the task levels "0", "1", and "2". That is, the task Nos. 0 to 2 belong to the task level "0", the task Nos. 3 to 5 belong to the task level "1", and the task Nos. 6 to 8 belong to the task level "2".
  • the task dispatcher 208 Upon the reception of the activation requests by the above-mentioned various interruptions, the task dispatcher 208 responds to the. activation requests to allot occupation time onto the CPU to the respective tasks in accordance with the priority rank attached to the respective tasks corresponding to the activation requests.
  • the task priority control by the task dispatcher 208 is performed by the following method:
  • Fig. 7 shows task blocks of'the same number as that of the task levels, that is three in this embodiment since there are three task levels "0" to "2", are provided in the RAM controlled by the dispatcher 208.
  • Eight bits are allotted to each control block.
  • Three of the eight bits, that is 0-th to 2nd bits (Q O - Q 2 ) are the activation bits for performing activation request task indication and the 7-th bit (R) is used for execution bit for indicating whether any one of the same task level is being executed or being interrupted.
  • the activation bits Qo - Q 2 are arranged in the order of decreasing the priority rank.
  • the activation bit corresponding to the task No.4 in Fig.6 is Q O in the task level "1".
  • a flag "1" is set to any one of the activation bits, and at the same time the task dispatcher 208 searches for the issued activation request in the activation bits in the order from the activation bit corresponding to the task of higher level so that the flag corresponding to the issued activation request is reset and flag "1" is set to the execution bit to thereby execute the processing for activating the task corresponding thereto.
  • Fig.8 shows an activation address table provided in the RAM 106 controlled by the task dispatcher 208.
  • SAO to SA8 represent the activation addresses correspond to the task Nos.0 to 8 of the tasks 210 to 226 as shown in Fig.6.
  • Sixteen bits are allotted to each activation address information which is used for the task dispatcher 208, as described later, to activate the task corresponding to the issued activation request.
  • Figs. 9 and 10 show flowcharts for the processing performed by the task dispatcher 208.
  • judgement is made as to whether the tasks belonging to the task level tare being executed or interrupted in a step 302. That is, if flag "1" is detected in the execution bit, the flag "1" indicates the state that the macro processing program 228 does not yet issue the task completion information to the task dispatcher 208 and the task which had been executed is being interrupted because interruption of higher priority rank has been generated. Accordingly, if flag "1" is detected in the execution bit, the processing is jumped to a step 314 in which the interrupted task is reactivated.
  • the processing is shifted to the step 304 in which judgement is made as to whether there is any task waiting for activation in the level 1. That is, the activation bits in the level l are searched for in the order of decreasing the priority rank of the tasks corresponding to the activation bits, that is in the order of Q 0 , Q 1 and Q 2 . If no flag "1" is detected in any one of the activation bits belonging to the level t, the processing comes to a step 306 in which the task level is altered.
  • the processing comes to a step 308 in which judgement is made as to whether all the task levels have been checked. In the case where all the task levels have been not yet checked, that is, when l ⁇ 2 in this embodiment, the processing comes back to the step 302 and the above-mentioned processing is repeated. In the case where the result of judgement proves that all the task levels have been checked in the step 308, the processing comes to a step 310 in which inhibit to interruption is released because interruption has been inhibited during the processing in the steps 302 to 308. Thereafter, in the next step 312, next issued interruption is waited for.
  • step 400 If there is a task waiting for activation in the level 1 in the step 304, that is if flag "1" is detected in one of the activation bits belonging to the task level l, the processing comes to a step 400.
  • search is made as to which one of the activation bits in which one of the task levels is provided with flag "1", in the order of decreasing the priority rank of the task levels, that is in the order of Q 0 , Q 1 , and Q 2 .
  • the processing comes to a step 404 in which the activation bit provided with flag "1” is reset and flag "1" is set to the execution bit (hereinafter referred-to R) of the same task level.
  • step 406 the number of the activated task is detected, and in a step 408, the activation address information as to the activated task is derived in accordance with the activation address table provided in the RAM as shown in Fig.8.
  • a step 410 judgement is made as to whether the activated task be executed or not.
  • the necessity of the execution is judged on the basis of the value of the activation address information. That is, when the activation address information has a specific value, for example "0", the judgement is such that the execution is not necessary. It is necessary to provide this judgement step in order to cause a car to have a function of performing only a specific one of the task functions for performing engine control selected depending on the kind of the car.
  • the processing comes to a step 414 in which the R-bit of the specific task level : is reset. then, the processing comes back to the step 302 in which judgement is made as to whether the task level 1 is being interrupted or not. This is because there may be a case where a plurality of activation bits are provided with flag "1".
  • the processing comes to a step 412 in which jump is made to the specific task so as to execute the task.
  • Fig.11 shows a flowchart for processing the macro processing program 228.
  • This program is constituted by steps 562 and 564.
  • the task levels are searched in the order of increasing the task level, that is in the order from the level "0" so as to find completed task level or levels.
  • the processing comes to a step 568 in which the execution (RUN) flag provided in the 7th bit in the task control block of the completed task is reset. thus, the execution of the task has been completed.
  • the processing comes back to the task dispatcher 208 in which the next execution task is determined.
  • the execution of the CPU is shifted to the control program OS
  • the completion of execution of the task No.3 is reported by the macro program 228 to the task dispatcher 208
  • the execution of the task N o.4 corresponding to the activation request N 12 of lower priority rank is initiated at the time T ll
  • the execution is shifted to the control program OS upon the completion of execution of the task No.4 at the time T 12
  • the execution of the task No.6 which corresponds to the activation request N 21 and which has been so far interrupted is restarted at the time T 13 .
  • the task priority control is performed in the manner as described above.
  • the state of transition in the task priority control is illustrated in Fig.13 "Idle" represents the state in which activation is waited for and no task activation request has been issued. Then, if an activa- tin request is issued, flag "1" is set to the activation bit of the task control block so as to indicate the necessity of activation.
  • the time required for shifting from the state “Idle” to the state “Queue” is determined by the level of the respective task. In the state "Queue", the order of execution is determined on the basis of the rank of priority.
  • the specific task is brought into the state of execution after the flag of the activation bit of the task control block has been reset by the task dispatcher 208 in accordance with the control program OS and a flag "1" has been set to the R - bit (7th bit).
  • the execution of task is initiated. This is the state "Run”.
  • the flag of the R-bit of the task control block is cleared and the completion report is terminated.
  • the state "Run” ends and the state "Idle” is recovered to wait for the issuance of the next activation request. If an interruption request IRQ is generated in executing a task, that is in the state "Run", the execution of the task has to be interrupted. For this, the contents of the CPU is shunted and the execution is interrupted.
  • Fig.13 shows a typical flow.
  • a flag "1" is set to the activation bit of the task control block in the state "Ready”. This is the case, for example, in the state of interruption of activation of a task, the next activation request timing of the task is reached. In this case the flag in the R-bit takes preference and the task which is being interrupted is terminated.
  • each of the tasks Nos.0 to 7 is in any one of the four states of Fig.3.
  • Fig.14 shows a particular embodiment of the program system as shown in Fig.6.
  • a control program OS includes an initial processing program 202, an interruption processing program 206, a task dispatcher 208, and a macro processing program 228.
  • the interruption program 206 includes various kinds of interruption processing programs in which an initial interruption processing (hereinafter referred to as an INTL interruption processin) 602 generates initial interruptions in the number of half the number of the engine cylinders per revolution, for example twice per revolution in the case of four cylinders, due to an initial interruption signal generated in synchronism with the engine revolution.
  • the date indicative of the fuel injection timing computed by an EGI task 612 in response to the above-mentioned INTL interruption is set in a register INJD in the INJC 134 included in the I/0 interface circuit 108 (Fig.5).
  • An A/D conversion interruption processing 604 includes two kinds of interruption, that is, an ADC1 (Fig.5) interruption and an ADC2 (Fig.5) interruption.
  • the ADCl (Fig.5) has the accuracy of 8 bits, and is used for inputting data such as the battery voltage, the cooling water temperture, the suction air temperature, the regulated voltage, etc., applied thereto.
  • the ADC1 starts the A/D conversion as soon as the input point to the MPX 120 (Fig.5) is assigned, and issues the ADC1 interruption upon the completion of the A/D conversion.
  • the ADC1 interruption is used only before cranking.
  • the ADC 128 in the ADC2 (Fig.5) is used for inputting the data indicative of the air flow rate and generates the ADC2 interruption immediately after the A/D conversion.
  • the ADC2 interruption is also used only before cranking.
  • an INTV interruption signal is generated at a time interval of a predetermined time of, for example, 10 msec set in an INTV register (not shown) and is used as a basic signal for monitoring the activating timing of tasks to be activated at a predetermined interval of time.
  • This INTV interruption signal updates the soft timer thereby activating the mask now ready to be activated.
  • interruption processing program 608 is for detecting state of ENST and starts counting in response to the detection of an INTL interruption signal so as to issue an ENST interruption when no INTL interruption signal can not be detected-within a predetermined period of time of, for example, 1 sec.
  • the processing steps are performed in the manner as described above.
  • Tasks belonging to the task level "0" include a fuel cutting processing task (hereinafter referred to as an AC task), a fuel injection control task (hereinafter referred to as an EGI task), and a starting timing monitoring task (hereinafter referred to as an MONIT task).
  • Tasks belonging to the task level "1” include an AD1 input task (hereinafter referred to as an ADIN1 task) and a time coefficient processing task (hereinafter referred to as an AFCIA task).
  • Tasks belonging to the task level "2" include an idling rotation control task (hereinafter referred to as an ISC task), a compensation computation task (hereinafter referred to as an HOSE I task), and a pre-starting processing task (hereinafter referred to as an ISTRT task).
  • ISC task idling rotation control task
  • HOSE I task compensation computation task
  • ISTRT task pre-starting processing task
  • Table 2 shows the allocation of the task levels and the functions of the individual tasks.
  • Fig.15 shows the manner of processing of the output signal from the hot-wire type flow rate sensor employed in the present-invention.
  • the instantaneous air flow rate q A can be computed from the hot-wire sensor output voltage v from the equation (5). Since the instantaneous air flow rate q A is an instantaneous value in the pulsating state as shown in Fig.15, it is sampled at a predetermined time interval ⁇ t.
  • the mean air flow rate Q A can be computed from the respective sampled values of the instantaneous air flow rate Q A according to the following equation:
  • the air flow rate sucked into the n cylinder can be obtained as ⁇ q An from the equation (8).
  • n l
  • the integrated air flow rate can be obtained by the above-mentioned signal processing.
  • the fuel injection may be performed in such a manner that the amount of fuel injected per revolution of the engine is computed on the basis of the equation (7), to thereby perform fuel injection once per one suction stroke in each cylinder, for example, once every 180° rotation of the crank in the case of engine provided with 4 cylinders.
  • the fuel injection may be performed when the integrated air flow rate actual value attains a given level.
  • Fig.16 shows the timing of fuel injection according to the above-mentioned latter fuel injection system.
  • the instantaneous air flow rate q A is integrated for a predetermined period of time, and, when the integrated air flow rate actual value attains or exceeds an integrated air flow rate reference level Q R , fuel is injected for a predetermined period of time t as seen in Fig.16. That is, fuel is injected at the timing at which the integrated instantaneous air flow rate actual value has attained the integrated air flow rate referece level Ql.
  • FIG. 16 there are shown three integrated air flow rate reference levels Q l1 , Q 12 and Q 13 .
  • the integrated air flow rate reference value Q 1 is suitably shifted so as to adjust the air-fuel ratio (A/F) as described.
  • a rich fuel-air mixture is required during warming-up in the engine starting stage, and this can be achieved by reducing the integrated air flow rate reference level Qy.
  • the integrated air flow rate reference level Q t can be suitably adjusted by the ON-OFF of the output from an 0 2 sensor (not shown).
  • F ig.17 is a flowchart for processing the taking-in of the output signal of the hot-wire type flow rate sensor and the timing of the fuel injection.
  • step 801 judgement is made in a step 801 as to whether the interruption is an INTL interruption or not.
  • the ADV REG in IGNC 138 is set so as to complete the INTL interruption processing program.
  • step 801 When the result of judgement in the step 801 proves that the interruption is a Q A timer interruption, activation is made for taking-in the output of the hot-wire type flow rate sensor in a step 806,-and taking-in of the output of the hot-wire type flow rate sensor is performed in a step 807.
  • the instantaneous air flow rate q A as shown in the equation (5) is computed in a step 808 and the integration processing is performed in a step 809.
  • Judgement is made in a step 810 as to whether the integrated value of instantaneous air flow rate has reached the integrated air flow rate reference level.
  • a period of time of fuel injection t corresponding to the integrated air flow rate reference level is set in a step 811 into the INJD REG of INJC 134 (Fig.5), and basic injection pulse is produced in a step 812 from the INJD REG of INJC 134 to the injector 12 through the AND gate 136 to initiate the injection with the basic fuel amount Tp .
  • the width of the basic injection pulse is determined by the period of time t for injection, and the amount of basic fuel injection Tp is determined by the integrated air flow rate reference level.
  • a step 813 the difference between the integrated air flow rate actual value and the integrated air flow rate reference level is computed to regard it as the present integrated air flow rate.
  • the hot-wire type flow rate sensor is activated and the output of the same is taken-in in a step 817.
  • the thus taken-in value of the air flow rate is used for detection of the engine start due to rotation torque of wheels.
  • the processing is shifted to the INTV interruption processing 606 in Fig.14.
  • Fig.18 shows the relation between the temperature TW of engine cooling water sensed by the cooling water temperature sensor 56 and the air flow rate reference level. That is, Fig.lB shows how the reference level is varied relative to the output signal of the water temperature sensor 56.
  • the temperature range of from -40°C to 40°C corresponds to the warming-up level in which the engine is started from its cold state.
  • the temperature range from 40°C to 85°C corresponds to the normal starting level, and the temperature range higher than 85°C corresponds to the hot re-starting level.
  • the sensor output signal indicative of the temperature of the engine cooling water is taken into to the ADC1 so that the air amount reference level corresponding to the sensed temperature can be set by comparison according to the relation shown in Fig.18.
  • the INTST program 624 shown in Fig.14 is executed for this purpose.
  • Fig. 19 shows a fuel control processing flow in acceleration from an idle or deceleration state.
  • the amount of additional fuel injection is increased when the engine is accelerated from an idle or deceleration state. This process is executed at intervals of the 10 msec.
  • step 901 decides whether or not the idle switch 148 shown in Fig. 5 is turned on, and if it is on, in step 902 the idle switch flag "1" is set in RAM, followed by step 903. If it is proved that the idle switch is off in step 901, on the other hand, the process is passed to step 903, where the throttle valve opening TH is detected by the throttle valve opening sensor l16 and is stored in RAM.
  • step 907 the product of the compensation factor K and a predetermined value n (n > 1) is determined, so that the factor nK is multiplied by the basic amount of injection T determined in step 812 in Fig. 17, thus computing the additonal amount of fuel injection T 0 .
  • the flag is not "1"
  • the additional amount of fuel injection TO is computed from the compensation factor K.
  • step 909 the additional amount of fuel injection T 0 is injected. Namely, an interruption injection pulse c is produced after the basic pulse a and an additional injection pulse b in addition to th basic injection pulse a is produced.
  • Step 910 decides whether or not the idle switch is off, and if the switch is off, the flag "1" is reset. Thus, in the acceleration just after an idle or deceleration 'state, a greater amount of fuel injection than at other acceleration states is injected.
  • interruption injection pulses c are produced at step 909 at intervals of 10 msec after the basic injection pulse a produced at step 812 of Fig. 17. Further, an additional injection pulse b is produced in addition to the basic injection pulse a.
  • the pulse widths of the interruption injection pulse c and the additional injection pulse b are determined by the additional injection amount TO and are set to a value larger than in the conventional systems.
  • the additional injection amount T 0 is computed on the basis of ⁇ TH so that an interruption injection pulse and an additional injection pulse with the pulse width determined by the additional injection amount TO are produced.
  • the fuel air mixture is prevented from being lean near the start of acceleration (initial stage of acceleration corresponding to a period t l - t 2 ) thereby improving acceleration.
  • additional injection may be performed either by the interruption injection pulse or by the additional injection pulse.
  • step 921 fetches and subjects the throttle opening TH to A/D conversion and the result is stored in the RAM.
  • step 922 the difference ATH between the value TH fetched presently and the value TH (OLD) introduced 30 msec before is determined, followed by step 923 for deciding whether or not the difference ⁇ TH is larger than zero, that is, whether or not an acceleration is involved. If it is decided that an acceleration is involved, step 924 computes the compensation factor K 1 for acceleration injection from the throttle opening change rate ⁇ TH.
  • step 925 multiplies the compensation factor K 1 for acceleration injection by the basic injection amount T P to compute the additional fuel amount TO for acceleration.
  • a value representing the engine load that is, the negative pressure Pn at or about the throttle valve is detected from the output of the negative pressure sensor 119 (Fig. 5).
  • the embodiment under consideration uses the negative pressure as a value representing the load so that the smaller the negative pressure, that is, the nearer to the atmospheric pressure, it is decided that the opening of the throttle valve is larger, that is, the load is larger.
  • the load may be measured from the basic fuel injection amount ( ).
  • step 928 the compensated additional fuel injection amount T for acceleration is injected.
  • an interruption inejction pulse c and an additional injection pulse b the pulse widths of which are determined by the additional injection amount T, are produced.
  • the X-axis represents the negative pressure Pn and the Y-axis the cooling water temperature Tw and the Z-axis the compensation factor K for acceleration.
  • the compensation factor K is determined continuously for all the load conditions by use of a three-dimentional map.
  • the additional fuel injection amount alternatively be increased only when the load is below a predetermined value (such as when the negative pressure Pn is more than a predetermined value).
  • step 906 decides whether or not the load is smaller than a predetermined value, and only when it is decided that the load is smaller than the predetermined value, the compensation factor K determined by the cooling water temperature Tw may be read from a two-dimensional map.
  • the additional injection amount TO may be injected in step 928. In this embodiment, the additional injection amount may be obtained without regard to the cooling water temperature Tw.
  • a sufficient amount of additional fuel is injected in acceleration from small load state, so that the mixture is prevented from being lean near the start of acceleration, thus achieving a superior acceleration.
  • Fig. 23 is s flowchart for achieving a satisfactory acceleration by preventing the mixture from being lean near the start of acceleration from low engine speed by changing the amount of additional fuel injection in accordance with the engine speed.
  • the flowchart of Fig. 23 is executed at intervals of 10 msec.
  • Step 943 determines whether or not this value ⁇ TH is larger than zero, and if it is decided that it is larger than zero, that is, an acceleration is involved, then step 944 computes the compensation factor K 1 for acceleration injection from the throttle opening change rate ⁇ TH. Then, step 945 computes the additional fuel injection amount T 0 for acceleration from the basic fuel injection amount T p and the compensation factor K for accelerating injection. That is, T 0 is determined from Tp x K.
  • the amount of additional fuel injection is large near the start of acceleration and decreases with increase in the load or engine speed, thereby maintaining a proper air-fuel ratio and performing satisfactory acceleration.
  • the amount of fuel injection is increased in order to prevent the mixture gas from being lean near the start of acceleration.
  • the air-fuel ratio is likely to be reduced, that is, the mixture is likely to become rich near the end of acceleration (i.e., during the period from t 2 to t 3 ).
  • the air-fuel ratio can be maintained at a proper value by increasing the additional fuel injection amount near the start of acceleration and then by reducing the same gradually.
  • step 950 decides whether or not the throttle opening change rate ⁇ TH is positive, that is, an acceleration is involved. If it is decided that an acceleration is involved, step 951 determines the number of compensations for additional fuel injection amount on the basis of ⁇ TH and sets the number in a soft counter in the RAM. This number of compensations is proportional substantially to the value ⁇ TH.
  • step 952 the compensation factor K 1 for acceleration injection is computed on the basis of ⁇ TH, followed by step 953 for computing the initial value TO of the additional fuel injection amount for accerelation by multiplying the basic fuel injection amount T by K 1 .
  • Step 954 computes the additional fuel injection amount T from the initial value T 0 and the content of the counter for counting the number of compensations provided in the RAM.
  • the additional injection amount T is substantially proportional to the product of the initial value T 0 and the content of the counter, and is reduced with the decrease of the content of the counter.
  • next step 955 the additional fuel injection amount T is set in the register 134, and an additional injection pulse and an interruption injection pulse are produced on the basis of the value T .
  • step 956 it is decided whether or not the data in the counter is zero, and if it is zero, the additional injection is ended, while if the data in the counter is not zero, the process is passed to step 957.
  • step 957 it is decided whether or not a predetermined time (10 msec in this case) has passed, and if the predetermined time has passed, the data in the counter is reduced by one in step 958.
  • the counter data may be reduced in accordance with the reference angle pulse REF produced for crank revolution of each 180 degrees in steps 957 and 958.
  • the fuel air mixture is likely to be rich because the additional fuel injection responding to the interruption injeciton pulse c is performed each 10 msec even though the suction air flow rate increases very slowly.
  • the acceleration involves a small value of the throttle opening change rate ⁇ TH
  • the additional injection compensation factor K 1 is not computed according to the value ⁇ TH, but is determined according to the opening range to which the value 6TH belongs. Further, when the value ATH is less than a predetermined value, it is decided that it is a show acceleration to thereby perform the additional injection only once for one acceleration. Alternatively, when the value ⁇ TH is not less than the predetermined value, it is decided that it is a normal acceleration to thereby perform the additonal acceleration every 10 msec.
  • step 1001 fetches the throttle opening TH by interruption at 10 msec intervals, which throttle opening TH subjected to A/D conversion and is stored in the RA M.
  • step 1002 fetches the throttle opening TH by interruption at 10 msec intervals, which throttle opening TH subjected to A/D conversion and is stored in the RA M.
  • step 1003 decides whether or not the value ⁇ TH is larger than a predetermined value ⁇ 1 , it is decided that it is not an acceleration state so that step 1004 resets the flag 1 for non-execution of additional injection.
  • step 1005 decides whether or not ⁇ TH is a predetermined value a 2 ( ⁇ 2 > a l ) or more. If step 1005 decides that ⁇ TH is smaller than a 2 , it is decided that the value ⁇ TH belongs to a throttle opening range "1", that is ⁇ 2 > ⁇ TH > ⁇ 1 . Further, it is decided that it is a slow acceleration state, so that the value of the compensation factor K 1 determined from the opening range "1" and water temperature Tw is retrieved from the map in step 1006.
  • step 1007 the amount of additoinal fuel injection for acceleraiton commensurate with the compensation factor K 1 is computed, followed by step 1008 for deciding whether the flag 1 is "0" or not. If it is decided in step 1008 that the flag 1 is not "0", that is, the flag is set, then the decision is that one additional injection based.on the range "1" has already been completed and therefore no additional injection is effected any more.
  • step 1009 effects additional injection once, followed by step 1010 for setting the flag 1.
  • step 1010 for setting the flag 1.
  • step 1011 decides whether or not ⁇ TH is ⁇ 3 ( ⁇ 3 > a 2 ) or more. If it is decided at this step 1011 that ⁇ TH is less than ⁇ 3 , the resulting decision is that ⁇ TH is belongs to an opening range "2", that is, a3 > ⁇ TH ⁇ a 2 . Further, it is decided that it is a slow acceleration and so in step 1012, the compensation factor K 1 is determined from the water temperature Tw and the range "2". The additional fuel injection amount for acceleration based on this compensation factor K 1 is computed at step 1013, folloed by step 1014 where it is decided whether or not the flag 2 is "0".
  • step 1014 decides that the flag 2 is not "0", that is, the flag is set, then no additional fuel injection is effected.
  • step 1015 performs additional fuel injection once so that the flag 2 is set to in step 1016.
  • step 1017 decides whether or not ⁇ TH is not less than a predetermined value a4 (a4 > a3). If step 1017 decides that ⁇ TH is smaller than a 4' the resulting decision is that ⁇ TH belongs to an opening range "3", that is, a4 > ⁇ TH ⁇ ⁇ 3 . Further, it is decided that it is a slow acceleration, so that step 1018 retrieves the map for the compensation factor K 1 determined from the range "3" and the water temperature Tw, followed by step 1019 where the additional fuel injection amount for acceleraiton is computed. Next, in step 1020, it is decided whether or not the flag 3 is "0", and if it is decided that the flag 3 is "0", step 1021 effects an additonal injection, followed by step 1022 for setting the flag 3.
  • step 1020 decides that the flag 3 is not "0", on the other hand, no additional fuel injection is effected.
  • step 1017 decides that ATH is ⁇ 4 or more, the resulting decision is that ⁇ TH belongs to an opening range "4". Further, it is decided that it is not a slow acceleration but a normal acceleration, so that step 1023 retrieves the map for the compensation factor K 1 determined from the range "4" and the water temperature Tw, followed by step 1024 for computing the additoinal fuel injection amount for acceleration, further followed by step 1025 for additional injection.
  • the compensation factor K may be modified in accordance with the cooling water temperature Tw.
  • the additional fuel injection amount TO may be obtained from a map.
  • Fig.29 shows a soft timer table which is provided in the RAM 106 and which is provided with timer blocks in the same number as that of different activation periods activated by various kinds of interruptions.
  • the term "timer block” is defined as a storage area into which time information with respect to the activation period of the task stored in the ROM 104.
  • TMB head address of the soft timer table in the R A M 106.
  • the time information with respect to the above-mentioned activation period is stored from the ROM 104 in starting the engine. That is, when the INTV interruption is performed, for example, at a regular period of time of 10 msec,.a value which is integral multiples of 10 msec and which represents the respective activation period is transferred and stored in the respective timer block.
  • Fig.30 shows a flowchart for executing the IN TV interruption processing 606.
  • the judgement is concluded that the soft timer is in the state of stoppage and that the corresponding task to be activated by the specific soft timer is in the state of stoppage, so that processing is jumped to a step 640 in which the soft timer table is renewed. That is, the above-mentioned judgement is made on the basis of the fact that when the task is stopped, the residual timer is left it as it is without being initialized when it becomes 0 (zero).
  • the processing is shifted to a step 632 in which the residual timer in the time block is renewed.
  • the residual timer T 1 is decremented by 1 (one).
  • judgement is made in a step 634 as to whether the soft timer has reached the activation period or not.
  • the processing is shifted to a step 636. If the judgement is concluded that the soft timer has not reached the activation period, on the contrary, the processing is jumped to the step 640 in which the soft timer table is renewed.
  • the residual time T 1 of the soft timer table is initialized in the step 636. That is, the timer information with respect to the activation period of the specific task is transferred from the ROM 104 to the RAM 106.
  • an activation request for the task corresponding to the soft timer table is issued in a step 638.
  • the soft timer table is renewed in the step 640. That is, the contents of the soft timer table is incremented by 1 (one). Further judgement is made in a step 642 as to whether all the soft timers have been checked or not.
  • the task ADIN1 is first activated so that the data, such as the cooling water temperature, the battery voltage, necessary for the starting of the engine are taken from the various sensors into the ADC 122 through the MPX 120, and every time all these data have been successively inputted, the task HOSEI, that is, the compensation task, is activated so that compensation is computed on the basis of the inputted data. Further, every time all the data from the various sensors have been successively inputted to the ADC 122 in accordance with the ADIN1, the task ISTRT is activated so that the fuel injection amount necessary in starting of the engine.
  • the above-mentioned three tasks, that is, the task ADIN1, the task HOSEI and the task ISTRT are activated in accordance with the initial processing program 202.
  • the three tasks that is, the task ADIN1, the task H OSE I and the task ISTRT are activated by-the interruption signal of the task ISTRT. That is, these tasks have to be executed only in the period in which the START-SW 152 is in its ON state (in the period of cranking of the engine).
  • pieces of time information with respect to the predetermined activation periods are transferred from the ROM 104 to the soft timer tables corresponding to the respective tasks provided in the RAM 106. Further, in this period, the residual time T 1 in the respective soft timer table is initialized and the setting of activation period is repeatedly performed.
  • the task MONIT Being provided for computing the fuel injection amount in the starting of the engine, the task MONIT becomes unnecessary after the engine starting, and therefore after the task has been executed predetermined times, the activation of the soft timer is stopped and tasks necessary in the post-starting state of the engine other than the task MONIT are activated in response to a stoppage signal produced upon the termination of the task MONIT.
  • "0" is stored in the soft timer table corresponding to the task in response to a signal indicating the termination of the task at the judgement point of time at the end of the task. That is, the stoppage of task is effected by clearing the contents of the soft timer corresponding to the task.
  • Fig.32 shows an IRQ generating circuit.
  • An I N T V I RQ generating circuit is constituted by a register 735, a counter 736, a comparator 737, and a flip-flop 738, and a period for generating INTV IRQ, for example 10 msec, is set into the register 735.
  • a clock pulse is set into the counter 736, and when the count of the counter 736 becomes coincident with the contents of the register 735, the flip-flop 738 is set. In this set state of the flip-flop 738, the counter 736 is cleared and the counting is restarted. Therefore, the INTV IRQ is generated at a predetermined regular interval of time (10 msec).
  • An ENST IRQ generating circuit for detecting engine stoppage is constituted by a register 741, a counter 742, a comparator 743, and a flip-flop 744.
  • the register 741, the counter 742 and the comparator 743 operate in the same manner as described above in the INTV IRQ generating circuit so that when the count of the counter 742 has reached the contents of the register 741, an ENST IRQ is generated.
  • the counter 742 is cleared by an REF pulse generated by a crank angle sensor at a predetermined interval of crank angles during the rotation of engine, the count of the counter 742 can not reach the contents of the register 741 so that no ENST IRQ is generated.
  • An INTV IRQ generated by the flip-flop 738, an ENST IRQ generated by the flip-flop 744, and IRQs generated by the ADC1 and ADC2 are set into flip-flops 740, 746, 764, and 768 respectively.
  • a signal for generating/inhibiting IRQ is set into each of flip-flops 739, 745, 762, and 766. If "H” is set in any one of the flip-flops 739, 745, 762, and 766, corresponding one of AND gates 748, 750, 770, and 772 is enabled so that an IRQ is immediately generated through an OR gate 751.
  • an IRQ can be generated, inhibited, or released from inhibition by setting "H” or "L” into the respective flip-flops 739, 745, 762 and 766.
  • the cause of generation of IRQ is removed by taking the contents of the flip-flops 740, 746, 764 and 768 into the CPU.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
EP83110424A 1982-10-20 1983-10-19 Méthode de controle pour moteurs à combustion interne Expired EP0106366B1 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP182902/82 1982-10-20
JP57182904A JPS5974339A (ja) 1982-10-20 1982-10-20 燃料噴射装置
JP182904/82 1982-10-20
JP18290282A JPS5974337A (ja) 1982-10-20 1982-10-20 燃料噴射装置

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0164125A2 (fr) * 1984-06-08 1985-12-11 Hitachi, Ltd. Méthode de commande de l'injection de carburant pour moteurs à combustion interne
EP0167839A2 (fr) * 1984-06-15 1986-01-15 Hitachi, Ltd. Appareil de commande de l'injection de carburant pour moteur à combustion interne
EP0204211A2 (fr) * 1985-05-21 1986-12-10 Toyota Jidosha Kabushiki Kaisha Système pour contrôler la pression d'admission dans un moteur à combustion interne suralimenté
EP0205861A2 (fr) * 1985-06-26 1986-12-30 Pierburg Gmbh Procédé d'optimalisation d'une quantité de carburant
EP0258864A1 (fr) * 1986-09-01 1988-03-09 Hitachi, Ltd. Méthode et dispositif de commande de carburant
WO1988006317A1 (fr) * 1987-02-21 1988-08-25 Robert Bosch Gmbh Procede permettant le traitement par priorite de plusieurs demandes d'un ordinateur
EP0316772A2 (fr) * 1987-11-10 1989-05-24 Japan Electronic Control Systems Co., Ltd. Système de contrôle pour moteur à combustion avec comportement transitoire modifié
EP0286644B1 (fr) * 1986-10-10 1990-09-19 Robert Bosch Gmbh Procede pour determiner electroniquement le debit de carburant d'un moteur a combustion interne
EP0400942B1 (fr) * 1989-05-29 1993-06-02 Hitachi, Ltd. Dispositif d'alimentation en mélange air-carburant pour moteur à combustion interne
US7591135B2 (en) * 2004-12-29 2009-09-22 Honeywell International Inc. Method and system for using a measure of fueling rate in the air side control of an engine

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US4184458A (en) * 1977-10-19 1980-01-22 Toyota Jidosha Kogyo Kabushiki Kaisha Method of controlling fuel injection in engine and unit therefor
GB2030730A (en) * 1978-09-22 1980-04-10 Bosch Gmbh Robert Control circuit for increasing fuel feed to internal combustion engines during acceleration
US4227490A (en) * 1978-02-13 1980-10-14 Toyota Jidosha Kogyo Kabushiki Kaisha Electronic control fuel injection system which compensates for fuel drying in an intake passage
EP0026643A2 (fr) * 1979-09-27 1981-04-08 Ford Motor Company Limited Système de dosage de carburant pour moteur à combustion interne
EP0047969A2 (fr) * 1980-09-12 1982-03-24 Hitachi, Ltd. Méthode de commande de la combustion dans un moteur
EP0054112A2 (fr) * 1980-12-12 1982-06-23 Robert Bosch Gmbh Méthode et système de dosage de carburant commandé électroniquement pour un moteur à combustion interne
JPS5848726A (ja) * 1981-09-09 1983-03-22 Toyota Motor Corp 内燃機関の燃料噴射制御装置

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US4227490A (en) * 1978-02-13 1980-10-14 Toyota Jidosha Kogyo Kabushiki Kaisha Electronic control fuel injection system which compensates for fuel drying in an intake passage
GB2030730A (en) * 1978-09-22 1980-04-10 Bosch Gmbh Robert Control circuit for increasing fuel feed to internal combustion engines during acceleration
EP0026643A2 (fr) * 1979-09-27 1981-04-08 Ford Motor Company Limited Système de dosage de carburant pour moteur à combustion interne
EP0047969A2 (fr) * 1980-09-12 1982-03-24 Hitachi, Ltd. Méthode de commande de la combustion dans un moteur
EP0054112A2 (fr) * 1980-12-12 1982-06-23 Robert Bosch Gmbh Méthode et système de dosage de carburant commandé électroniquement pour un moteur à combustion interne
JPS5848726A (ja) * 1981-09-09 1983-03-22 Toyota Motor Corp 内燃機関の燃料噴射制御装置

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Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0164125B1 (fr) * 1984-06-08 1988-09-21 Hitachi, Ltd. Méthode de commande de l'injection de carburant pour moteurs à combustion interne
EP0164125A2 (fr) * 1984-06-08 1985-12-11 Hitachi, Ltd. Méthode de commande de l'injection de carburant pour moteurs à combustion interne
EP0167839A2 (fr) * 1984-06-15 1986-01-15 Hitachi, Ltd. Appareil de commande de l'injection de carburant pour moteur à combustion interne
EP0167839B1 (fr) * 1984-06-15 1989-01-04 Hitachi, Ltd. Appareil de commande de l'injection de carburant pour moteur à combustion interne
EP0204211B1 (fr) * 1985-05-21 1991-09-25 Toyota Jidosha Kabushiki Kaisha Système pour contrôler la pression d'admission dans un moteur à combustion interne suralimenté
EP0204211A2 (fr) * 1985-05-21 1986-12-10 Toyota Jidosha Kabushiki Kaisha Système pour contrôler la pression d'admission dans un moteur à combustion interne suralimenté
EP0205861A3 (fr) * 1985-06-26 1988-03-30 Pierburg Gmbh Procédé d'optimalisation d'une quantité de carburant
EP0205861A2 (fr) * 1985-06-26 1986-12-30 Pierburg Gmbh Procédé d'optimalisation d'une quantité de carburant
EP0258864A1 (fr) * 1986-09-01 1988-03-09 Hitachi, Ltd. Méthode et dispositif de commande de carburant
GB2195190B (en) * 1986-09-01 1990-10-17 Hitachi Ltd Method of and apparatus for fuel control
EP0286644B1 (fr) * 1986-10-10 1990-09-19 Robert Bosch Gmbh Procede pour determiner electroniquement le debit de carburant d'un moteur a combustion interne
WO1988006317A1 (fr) * 1987-02-21 1988-08-25 Robert Bosch Gmbh Procede permettant le traitement par priorite de plusieurs demandes d'un ordinateur
EP0316772A2 (fr) * 1987-11-10 1989-05-24 Japan Electronic Control Systems Co., Ltd. Système de contrôle pour moteur à combustion avec comportement transitoire modifié
EP0316772B1 (fr) * 1987-11-10 1993-03-03 Japan Electronic Control Systems Co., Ltd. Système de contrôle pour moteur à combustion avec comportement transitoire modifié
EP0400942B1 (fr) * 1989-05-29 1993-06-02 Hitachi, Ltd. Dispositif d'alimentation en mélange air-carburant pour moteur à combustion interne
US7591135B2 (en) * 2004-12-29 2009-09-22 Honeywell International Inc. Method and system for using a measure of fueling rate in the air side control of an engine

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DE3376995D1 (en) 1988-07-14
EP0106366A3 (en) 1984-12-19

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