Capacitor discharge type internal combustion engine ignition device

TECHNICAL FIELD OF THE INVENTION

The present invention relates to a capacitor discharge type internal combustion engine ignition device.

BACKGROUND OF THE INVENTION

A capacitor discharge type internal combustion engine ignition device is comprised of an ignition coil; an ignition capacitor provided at the primary side of the ignition coil and charged by an output voltage of a predetermined power supply at one polarity; a discharge thyristor, which becomes an on-state when an ignition signal is given and discharges a charge of the ignition capacitor through the primary coil of the ignition coil; a signal generating portion for generating a signal to obtain rotational information on the internal combustion engine; and an ignition control portion which gives the ignition signal to the discharge thyristor at an ignition position (a rotational angle position of a crank shaft at a time of performing an ignition operation) of the internal combustion engine decided based on the rotational information obtained from the signal generated by the signal generating portion.

As for the power supply to charge the ignition capacitor, an exciter coil is often used, which is provided inside a magneto-generator driven by the internal combustion engine and synchronizes with rotation of the engine so that an alternating voltage is induced.

In recent years, in order to purify an exhaust gas of the engine and attempt to reduce a fuel cost, it is necessary for the engine to have complex ignition characteristics. For this reason, there are frequent cases where a microcomputer is installed in the ignition control portion and the ignition position is decided in a software manner.

In the case where the ignition signal is generated at the ignition position decided in the software manner by using the microcomputer, a reference position is set at a position sufficiently advanced more than the rotational angle position corresponding to a top dead center of the internal combustion engine, and a time required for the engine to rotate to the ignition position arithmetically operated from the reference position is found as an ignition position detection time (time to be measured by the ignition timer for detecting the ignition position). When the reference position is detected, an ignition timer is allowed to start measuring the ignition position detection time and generate the ignition signal when the measurement has been completed.

As described above, in the internal combustion engine which controls the ignition position by using the microcomputer, since it is necessary to detect the reference position as the basis for measuring the ignition position decided in the software manner and the ignition position at a starting time and an extremely low speed state, the signal generating portion is comprised in such a manner that a reference position detection signal is generated at the reference position set at a position sufficiently advanced more than the rotational angle position of the crank shaft corresponding to the top dead center of the engine, and the ignition position detection signal for extremely low speed state is generated at the position adequate as the ignition position at the starting time and the extremely low speed state of the internal combustion engine.

Further, the ignition control portion is provided with an ignition control portion for extremely low speed state for giving the ignition signal to the discharge thyristor when the ignition position detection signal for extremely low speed state is generated and an ignition control portion for steady state for giving the ignition signal to the discharge thyristor at the ignition position decided based on the rotational information on the internal combustion engine, which is obtained from the output signal of the signal generating portion.

In the case where the ignition position is decided by using the microcomputer, if a battery is provided, the microcomputer can be operated from the starting time of the engine and, therefore, there arises no problem at all. However, in the case where no battery is provided or in the case where there is a necessity to make it possible to operate the engine even when the battery is exhausted for safety reason, it is necessary to give a power supply voltage to the microcomputer by an output of a generator mounted on the engine. For example, in an outboard motor, the engine is required to operate even when the battery is exhausted. For this reason, in the ignition device of this type, a control power supply circuit is provided, which rectifies a negative half-wave output of the exciter coil not used for charging the ignition capacitor and generates a constant direct current voltage so that, from this power supply circuit, the power supply voltage is given to the ignition control portion.

In a battery-less ignition device having a microcomputer provided with power voltage from the output of the control power supply circuit fed by the generator mounted on the internal combustion engine instead of a battery, since the microcomputer is not allowed to normally operate until the output voltage of the generator is raised to a certain level at a starting time of the engine, the ignition operation can not be performed as long as the rotational speed of the internal combustion engine is low. Further, even when the microcomputer can be normally operated, as long as the rotational speed of the engine is low, since fluctuation in the rotational speed accompanied by a stroke change of the engine is large, it is difficult to accurately measure the ignition position arithmetically operated by the microcomputer, thereby it is not possible to stably perform the ignition operation.

For this reason, in the battery-less ignition device, a signal is generated from the generator or a signal generator mounted on the engine at a position adequate as the ignition position at the starting time and the extremely low speed state of the engine, and when this signal has been generated, the ignition signal is given to the discharge thyristor through a hardware circuit, so that an ignition at the starting time and the extremely low speed state (a speed region below an idling rotational speed) is stably performed.

As described above, in the battery-less capacitor discharge type ignition device which decides the ignition position in the software manner by using the microcomputer, in order to stably perform the ignition at the starting time and the extremely low speed state of the engine, the ignition control portion for extremely low speed state is provided, wherein the ignition signal is given to the discharge thyristor through the hardware circuit. However, in a conventional ignition device of this type, since the power supply voltage was given to the ignition control portion for steady state provided with the microcomputer and to the ignition control portion for extremely low speed state from the same power supply circuit, there was a problem that the ignition control portion for extremely low speed state delays in starting an operation at the starting time of the engine.

That is, since the microcomputer constantly consumes electric power, when the rotational speed of the engine is low and a peak value of the negative half wave output voltage of the exciter coil is not in a sufficiently high level state (in a state whereby the peak value of the output voltage of the negative half-wave of the exciter coil barely reaches the power supply voltage of the microcomputer), even if the power supply circuit outputs the voltage of a value (5V) necessary for operating the microcomputer while the exciter coil generates the negative half-wave output voltage, the output of the control power supply circuit stops as soon as the exciter coils enters a time period for outputting a positive half-wave voltage. Accordingly, until the control power supply circuit, which drives the microcomputer, is put into a state of stably outputting a voltage held at a set value, it is necessary to wait until the rotational speed of the engine is further increased so that the output voltage of the exciter coil is increased. For this reason, in the case where the power supply voltage is given to the ignition control portion for extremely low speed state by the same power supply circuit as the power supply circuit driving the microcomputer, there arose problems that a start of the operation of the ignition control portion for extremely low speed state is delayed, a starting characteristic of the engine is deteriorated and an ignition operation at an idling time is unstable.

SUMMARY OF THE INVENTION

Hence, an object of the present invention is to provide a capacitor discharge type internal combustion engine ignition device, wherein a rotational speed of which the ignition control portion for extremely low speed state starts an operation is sufficiently lowered so that a starting characteristic of the internal combustion engine can be improved and an idling rotation can be stably performed.

The present invention is applied to a capacitor discharge type internal combustion engine ignition device which comprises: an exciter coil provided inside a magneto-generator to be driven by an internal combustion engine; an ignition coil; an ignition capacitor provided at an primary side of the ignition coil and charged by a positive half-wave output voltage of the exciter coil at one polarity; a discharge thyristor which becomes an on-state when an ignition signal is given and discharges a charge of the ignition capacitor through the primary coil of the ignition coil; a control power supply circuit which converts the output voltage of the exciter coil into a direct current voltage; a signal generating portion for generating a reference position detection signal at a reference position set at a position sufficiently advanced more than a rotational angle position of a crank shaft which corresponds to a top dead center of the internal combustion engine and generating an ignition position detection signal for extremely low speed state at a position adequate as an ignition position at the starting time and the extremely low speed state of the internal combustion engine; an ignition control portion for extremely low speed state for giving an ignition signal to the discharge thyristor when the ignition position detection signal for extremely low speed state is generated; and an ignition control portion for steady state for giving the ignition signal to the, discharge thyristor at the ignition position decided based on rotational information on the internal combustion engine obtained from an output signal of the signal generating portion, and the ignition control portion for extremely low speed state and the ignition control portion for steady state operate with a direct current power supply voltage which is obtained by the control power supply circuit.

The present invention provides a first power supply circuit for generating a constant direct current voltage for operating the ignition control portion for steady state when the output voltage of the exciter coil is equal to or more than a set value and a second power supply circuit for generating the direct current voltage for operating the ignition control portion for extremely low speed state since when the output voltage of the exciter coil is in a state of being below the set value.

Further, the ignition control portion for extremely low speed state is comprised in such a manner as to start the operation at the power supply voltage lower than the power supply voltage (usually 5V) of the ignition control portion for steady state.

Since the ignition control portion for extremely low speed state consumes electric power only for a few period when the ignition signal for extremely low speed state is generated, even when a rotational speed of the engine is low and the exciter coil is in a state where an output necessary for stably operating the ignition control portion for steady state is unable to be generated from the first power supply circuit, the power supply voltage necessary for operating the ignition control portion for extremely low speed state can be stably generated from the second power supply circuit. For this reason, as described above, when the second power supply circuit for exclusive use of the ignition control portion for extremely low speed state is provided, the operation of the ignition control portion for extremely low speed state can be started at a rotational speed lower than the rotation speed whereby the ignition control portion for steady state starts the operation so that the starting characteristic of the engine can be improved and an idling rotation can be stably performed.

As for the magneto-generator used for operating the capacitor discharge type internal combustion engine ignition device, a magneto-generator is frequently used, which comprises: a magnetic rotor having a rotational body mounted on a crank shaft of the internal combustion engine and one permanent-magnet mounted on an outer periphery of the rotor and comprising a three pole magnetic field by the permanent-magnet and an outer periphery portion of the rotational body abutting against the permanent-magnet; and a stator having an iron core with a magnetic pole portion opposing to the magnetic filed of the magnetic rotor and an exciter coil wound around the iron core, which outputs from the exciter coil an alternating current voltage of one and a half cycle where a first negative half-wave voltage and positive half-wave voltage and a second negative half-wave voltage appear in order.

In the case where such a magneto-generator is used, the signal generating portion can be comprised of the exciter coil and a waveform shaping circuit which waveform-shapes the first and the second negative half-wave voltages outputted by the exciter coil, respectively and converts them into the first and the second pulse signals of a rectangular waveform shape.

In this case, the magneto-generator is provided so that a rising edge position or a falling edge position of the second pulse signal corresponds to a position adequate as an ignition position at the starting time and the extremely low speed state of the internal combustion engine.

Further, taking each rising edge or falling edge of the first and the second pulse signals as the ignition position detection signal for the extremely low state, the ignition control portion for extremely low speed state is comprised so as to provide an ignition signal to the discharge thyristor at the position where the rising edge or the falling edge of the first pulse signal is appeared and where the rising edge or the falling edge of the second pulse signal is appeared. This ignition control portion for extremely low speed state is comprised of a hardware circuit.

The ignition control portion for steady state is comprised so that a microcomputer operates with the direct current voltage obtained from the first power supply circuit, and taking the rising edge or the falling edge of the first pulse signal as the reference position detection signal, the microcomputer performs an arithmetical operation of the ignition position in each rotational speed of the internal combustion engine and a detection of the operated ignition position, and the microcomputer gives the ignition signal to the discharge thyristor when the operated ignition position is detected.

When comprised as described above, even before the exciter coil generates the positive half-wave output voltage (before the ignition capacitor is charged), the ignition signal is given to the discharge thyristor. However, even though the ignition signal is given with the ignition capacitor being in a non-charged state, the discharge thyristor is not the on-state, so an ignition operation is not performed, thereby no trouble occurs for the ignition of the engine.

When comprised as described above, since there is no need to provide a signal generator separately from the magneto-generator, the ignition position can be decided by the arithmetical operation without the constitution of the engine made complex, so that the internal combustion engine ignition device capable of dealing with various ignition characteristics can be obtained.

In the present specification, the ignition signal given to the discharge thyristor from the ignition control portion for extremely low speed state comprising the hardware circuit is referred to as “a hardware ignition signal” in a sense that it is the ignition signal given from the hardware circuit. Further, the ignition operation performed by the hard ignition signal is referred to as a hard ignition.

On the other hand, the ignition signal given to the discharge thyristor at the ignition position arithmetically operated by allowing the microcomputer to execute a predetermined software is referred to as “a soft ignition signal” in a sense that it is the ignition signal to be generated at the ignition position decided in the software manner. Further, the ignition operation performed by the soft ignition signal is referred to as a soft ignition.

In a preferred mode of the present invention, an ignition signal cancel switch is further provided, which becomes an on-state when the cancellation command is given and bypasses the ignition signal given to the discharge thyristor from the ignition control portion for extremely low speed state. In this case, the microcomputer of the ignition control portion for steady state is programmed in such a manner as to comprise: reference position detection means for discriminating the first pulse signal and the second pulse signal from signal widths of the first and the second pulse signals and intervals of generating the first and the second pulse signals and detecting the rising or the falling edge of one of the discriminated signals as the reference position; rotational speed detection means for finding the data to detect the rotational speed of the internal combustion engine by using at least one of the first and the second pulse signals; ignition position arithmetical operation means for arithmetically operating the ignition position of said internal combustion engine for the detected rotational speed in the form of a time required for the crank shaft of the engine to rotate from said reference position to the ignition position; ignition position detection means for starting measurement of the ignition position when the reference position is detected and giving the ignition signal to the discharge thyristor when the measurement of the ignition position has been completed; and cancellation command generating means for generating a cancellation command when the rotational speed of the internal combustion engine exceeds a set value.

In the case where the cancel switch is provided as described above and the rotational speed of the internal combustion engine exceeds the set value and the microcomputer is in an operating state, when the cancel switch is the on-state so that the ignition signal given to the discharge thyristor from the ignition control portion for extremely low speed state is bypassed from the discharge thyristor, the discharge thyristor becomes the on-state by the ignition signal given to the discharge thyristor by the falling or the rising of the first pulse signal at the steady time operating time, thereby making it possible to put the ignition capacitor into a state of not being charged and prevent the engine from causing an accidental fire.

The ignition control portion for extremely low speed state may comprises: an ignition signal supply capacitor charged by the output voltage of the second power supply circuit through a current limiting element and between a gate and a cathode of the discharge thyristor; a transistor provided in such a manner as to become an on-state the first and the second pulse signals as base signals and bypass the charge current of the ignition signal supply capacitor from the capacitor; and a diode for linking between the ignition signal supply capacitor and the transistor so that the charge of the ignition signal supply capacitor is discharged through the transistor when the transistor is the on-state, wherein the ignition signal is given to the discharge thyristor by the falling edges of the first pulse signal and the second pulse signal.

In the above described example, though the negative half-wave output voltage is shaped into a pulse waveform so as to obtain the reference position detection signal and the ignition position detection signal for extremely low speed state, the reference position detection signal and the ignition position detection signal for extremely low speed state may be obtained from the output of the signal generator mounted on the internal combustion engine. In this case, the signal generating portion is mounted on the internal combustion engine, and can be comprised of a signal generator for generating a first signal when the rotational angle position of the crank shaft of the engine corresponds to the reference position and generating a second signal when the rotational angle position of the internal combustion engine corresponds to the position adequate as the ignition position at the starting time and the extremely low speed state and a waveform shaping circuit for shaping the first and the second signals outputted by the signal generator into predetermined waveforms, respectively and outputting them as the reference position detection signal and the extremely low speed state ignition detection signal.

BRIEF DESCRIPTION OF THE DRAWINGS

The above and other objects and features of the invention will be apparent from the detailed description of the preferred embodiment of the invention, which is described and illustrated with reference to the accompanying drawings, in which;

FIG. 1

is a circuit diagram showing a constitution of an embodiment of the present invention;

FIG. 2

is a circuit diagram showing an another embodiment of the present invention;

FIG. 3

is a circuit diagram showing still a further embodiment of the present invention;

FIG. 4A

is a schematic front elevation showing the constitution of a magneto-generator to be used for an ignition device according to the present invention;

FIG. 4B

is a waveform chart showing a waveform of an output voltage to be obtained from the generator shown in

FIG. 4A

;

FIGS. 5A and 5B

are waveform charts for explaining an operation of a waveform shaping circuit to be used in the embodiment of

FIG. 1

;

FIGS. 6A and 6B

are waveform charts for explaining the operation of the waveform shaping circuit to be used in the embodiment of

FIG. 2

;

FIGS. 7A

to

7

E,

FIGS. 7G and 7H

are waveform charts wherein a voltage waveform of each portion of the embodiment shown in FIG.

1

and the embodiment shown in

FIG. 2

is shown for a rotational angle of a crank shaft of the engine;

FIG. 7F

is a view showing various times to be measured in the embodiments shown in FIG.

1

and

FIG. 2

;

FIGS. 8A

to

8

C are waveform charts for explaining the operations of the embodiments of the present invention;

FIGS. 8D

to

8

G are views showing various times to be measured in the embodiments of the present invention;

FIG. 9

is a flowchart showing one example of an algorism of a main routine of a program to be executed by a microcomputer of an ignition control portion for steady state in the embodiments of the present invention;

FIG. 10

is a flowchart showing one example of an algorism of a pulse edge interruption routine of the program to be executed by the microcomputer of the ignition control portion for steady state in the embodiments of the present invention;

FIG. 11

is a flowchart showing one example of an algorism of an ignition timer interruption routine of the program to be executed by the microcomputer of the ignition control portion for steady state in the embodiments of the present invention;

FIG. 12A

is a waveform chart of a voltage to be outputted by an exciter coil of an ignition device shown in

FIG. 3

; and

FIG. 12B

is a waveform chart showing one example of the waveform of the signal to be outputted by a pulsar coil of the ignition device shown in FIG.

3

.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

In the present invention, an ignition capacitor is charged by an output of an exciter coil provided in a magneto-generator to be driven by an internal combustion engine. As for the magneto-generator to be used for an internal combustion engine ignition device, a magneto-generator shown in

FIG. 4A

is often used. This magneto-generator has a rotational body

2

of a cup shape mounted on a crank shaft

1

of the internal combustion engine and one permanent-magnet

3

mounted in a concave portion

2

a

provided on peripheral of said rotational body and magnetized in a radial direction of the rotational body, and comprises a magnetic rotor

4

comprising a three pole magnetic field by the permanent-magnet

3

and the outer periphery of the rotational body

2

abutting against the permanent-magnet and a stator

7

comprised of an exciter coil

6

wound around an U-shaped iron core

5

having magnetic pole portions

5

a

and

5

b

opposing to the magnetic field of the magnetic rotor

4

. In the illustrated example, since a magnetic pole outside of the magnet

3

is an N pole, the three pole magnetic field is comprised of one N pole and two S poles formed respectively on the outer periphery portion of the rotational body at both sides of the N pole. The stator

7

is fixed to a stator attachment portion mounted on a case, a cover and the like of the engine, and the magnetic pole portions

5

a,

5

b

of the iron core

5

are opposed to the magnetic field of the magnetic rotor

4

through an air gap.

This generator outputs an alternating current voltage Ve of one and half a cycle from the exciter coil

6

, where, during the magnetic rotor

4

makes one rotation together with the crank shaft, the first negative half-wave voltage Vn

1

and a positive half-wave voltage Vp and the second negative half-wave voltage Vn

2

appear in order as shown in FIG.

4

B.

In case of using the generator shown in

FIG. 4A

, the positive half-wave voltage Vp outputted by the exciter coil

6

is used as the voltage for charging the ignition capacitor.

FIG. 1

shows a structural example of a hardware of a capacitor discharge type internal combustion engine ignition device according to the present invention. In the drawing, reference numeral

6

denotes an exciter coil provided inside the magneto-generator shown in FIG.

4

A and reference numeral IG denotes an ignition coil having a primary coil W

1

and a secondary coil W

2

. One end of the primary coil and the secondary coil of the ignition coil IG is grounded respectively, and the other end of the primary coil W

1

and the other end of the secondary coil W

2

are connected respectively to one end of an ignition capacitor Ci and a non-grounded side terminal of an ignition plug PL mounted on a cylinder head not shown of the engine.

As shown in

FIG. 4B

, the exciter coil

6

outputs the alternating current voltage Ve where, during the magnetic rotor

4

(see

FIG. 4A

) makes one rotation together with the crank shaft

1

, the first negative half-wave voltage Vn

1

and positive half-wave voltage Vp and the second negative half-wave voltage Vn

2

appear in order. Note that θ of a horizontal axis in

FIG. 4B

shows a rotational angle of the crank shaft.

The other end of the ignition capacitor Ci is connected to an anode of a discharge thyristor Thi whose cathode is grounded, and is connected to one end of the exciter coil

6

through a diode D

1

, whose cathode is directed to the ignition capacitor side. The other end of the exciter coil

6

is connected to a cathode of a diode D

2

, whose anode is grounded, and between one end of the exciter coil

6

and the ground, a diode D

3

is connected, whose anode is directed to the ground side.

In the illustrated example, an ignition circuit is comprised, wherein an essential portion of the ignition device is formed by the ignition coil IG, the ignition capacitor Ci and the discharge thyristor Thi. Further, a charging power supply portion of the ignition capacitor Ci is comprised of the exciter coil

6

and the diode D

1

to D

3

.

In the illustrated ignition circuit, the ignition capacitor Ci is charged to the illustrated polarity by the positive half-wave output voltage of the exciter coil

6

through the diode D

1

. When the capacitor Ci is in a state of being charged to the illustrated polarity (a state of a forward direction voltage being applied between the anode and the cathode of the tyristor Thi) and an ignition signal Vi is given to the discharge thyristor Thi from a circuit to be described later, the discharge thyristor is the on-state and, therefore, the charge of the ignition capacitor Ci is discharged through the discharge thyristor Thi and the primary coil W

1

of the ignition coil IG. In this way, an ignition high voltage is induced in the secondary coil of the ignition coil IG, and since this high voltage is applied to the ignition plug PL, an electric spark is caused by the ignition plug so that the engine is ignited.

Note that, though a resistor and a capacitor for protection purpose are connected between the gate and the cathode and between the anode and the cathode of the thyristor Thi, the illustration thereof is omitted.

In the present invention, one end of a resistor R

1

is connected to the other end of the exciter coil

6

through a diode D

10

whose anode is directed to the exciter coil side, and a first power supply capacitor C

1

is connected between the other end of the resistor R

1

and the ground. To both ends of the capacitor C

1

, a Zener diode ZD

1

whose anode is directed to the ground side is connected, and the voltage of both ends of the capacitor C

1

is kept below a constant value (Zener voltage) by the Zener diode. The voltage at both ends of the capacitor C

1

is inputted to a three terminal regulator Reg having a control function to keep the output voltage constant (5[V] in this example) for the fluctuation of the input voltage. The diode D

10

, the resistor R

1

, the first power supply capacitor C

1

, the Zener diode ZD

1

and the three terminal regulator Reg comprise a first power supply circuit

10

A, which converts the first and the second negative half-wave voltages Vn

1

and Vn

2

into the direct current voltage for control purpose, and an output terminal of the regulator Reg turns into an output terminal

10

a

of this power supply circuit

10

A.

Further, one end of a resistor R

1

′ is connected to the other end of the exciter coil

6

through a diode D

10

′ whose anode is directed to the exciter coil side, and a second power supply capacitor C

1

′ is connected between the other end of this resister and the ground. To both ends of the second power supply capacitor C

1

′, a Zener diode ZD

1

′ whose anode is directed to the ground side is connected in parallel. The diode D

1

′, the resistor R

1

′, the second power supply capacitor C

1

′ and the Zener diode ZD

1

′ comprise a second power supply circuit

10

B, and a non-grounded side output terminal

10

b

is derived from a non-grounded side terminal of the capacitor C

1

′.

This second power supply circuit

10

B generates a direct current voltage at both ends of the capacitor C

1

′ which is controlled below the Zener voltage of the Zener diode ZD

1

. The Zener voltage of the Zener diode ZD

1

′ is set lower than a control voltage of the regulator Reg.

In this example, the control power supply circuit

10

is comprised of the first power supply circuit

10

A and the second power supply circuit

10

B.

A series of the waveforms of the voltage Ve outputted by the exciter coil

6

after the starting operation of the engine is performed and the waveforms of a voltage Vcl at both ends of the power supply capacitor C

1

of the first power supply circuit

10

A were shown in

FIGS. 7A and 7B

respectively. As shown in

FIG. 7B

, the terminal voltage Vcl of the capacitor C

1

is increased accompanied with the increase of the rotational speed of the engine. When the rotational speed is increased to some level so that the voltage Vcl exceeds more than 5 [V] which is a control voltage of the regulator Reg, as shown in

FIG. 7C

, the regulator Reg outputs a constant (=5[V]) direct current voltage Vdc.

Note that, in

FIG. 7B

, reference character Vz denotes a Zener voltage of the Zener diode ZD

1

, and the terminal voltage of the capacitor C

1

is limited below this Zener voltage Vz.

Further, a voltage Vci at both terminals of the ignition capacitor Ci which is charged by the positive half-wave output voltage Vp of the exciter coil

6

was shown in FIG.

7

H. The ignition capacitor Ci is charged during the positive half-wave voltage Vp rises and, after that, reaches a peak, and its terminal voltage Vci is increased.

In

FIG. 1

, reference numeral

11

denotes a waveform shaping circuit for waveform-shaping a first and a second negative waveform voltages Vn

1

and Vn

2

outputted by the exciter coil

6

and converting them into a first and a second pulse signals of a rectangular waveform shape. The illustrated waveform shaping circuit

11

comprises: a capacitor C

2

whose one end is connected to the other end of the exciter coil

6

; a resistor R

2

connected in parallel to the capacitor C

2

and having a sufficiently large resistance value; a diode D

5

whose anode is connected to the other end of the capacitor C

2

; a resistor R

3

whose one end is connected to a cathode of the diode D

5

; an NPN transistor TR

1

whose base is connected to the other end of the resistor R

3

and whose emitter is grounded; an NPN transistor TR

2

whose base is connected to the collector of the transistor TR

1

and whose emitter is grounded; and resistors R

4

and R

5

connected respectively between the collectors of the transistors TR

1

and TR

2

and the output terminal

10

a

of the first power supply circuit

10

A.

In this waveform shaping circuit

11

, a first and a second output terminals

11

a

and

11

b

are derived respectively from the connecting point between the base of the transistor TR

1

and the resistor R

3

and from the collector of the transistor TR

2

.

The waveform shaping circuit

11

, as shown below, detects a zero point and a peak point of each rising side of the negative half-wave voltages Vn

1

and Vn

2

of the exciter coil

6

, and as shown in FIG.

5

B and

FIG. 7D

, rises at the zero point of the rising side of each negative half-wave voltage, and generates a pulse signal of a rectangular waveform shape. The pulse signals of a rectangular waveform shape obtained by waveform-shaping the first negative half-wave voltage Vn

1

and the second negative half-wave voltage Vn

2

are taken as the first and the second pulse signals Vq

1

(or Vq

1

′) and Vq

2

(or Vq

2

′), respectively.

That is, as shown in FIG.

5

A and

FIG. 7A

, when the exciter coil

6

generates the negative half-wave voltage Vn

1

or Vn

2

, the current flows through the capacitor C

2

, the diode D

5

, the resister R

3

and between the base and the emitter of the transistor TR

1

. In this way, the transistor TR

1

is put into the on-state, and the transistor TR

2

is put into an off-state. At this time, since a potential of the base of the transistor TR

1

and the potential of the collector of the transistor TR

2

are increased, the potentials of the output terminals

11

a

and

11

b

rise to a high level state, and as shown in FIG.

5

B and

FIG. 7D

, the pulse signal Vq

1

or Vq

2

rises. When the negative half-wave voltage Vn

1

or Vn

2

reaches a peak, a charge current does not flow into the capacitor C

2

so that the transistor TR

1

is put into the off-state and the transistor TR

2

is put into the on-state. In this way, the potentials of the output terminals

11

a

and

11

b

rise to almost a zero level (ground potential).

Consequently, when the exciter coil

6

generates the first negative half-wave voltage Vn

1

, the waveform shaping circuit

11

outputs the first pulse signals Vq

1

and Vq

1

′ whose edges of the rising side and the falling side correspond respectively to the zero. point and the peak point of the voltage Vn

1

from the output terminals

11

a

and

11

b,

and when the second negative half-wave voltage Vn

2

is generated, it outputs the second pulse signals Vq

2

and Vq

2

′ whose edges of the rising side and the falling side corresponds respectively to the zero point and the peak point of the rising side of the voltage Vn

2

from the output terminals

11

a

and

11

b,

respectively. Among these pulses, since Vq

1

and Vq

2

are outputted through a passive element, they are generated when the exciter coil generates the negative half-wave voltage which is equal to or more than a threshold value immediately after the starting operation of the engine begins. Accordingly, the pulse signals Vq

1

and Vq

2

are generated at the rotational speed sufficiently lower than the rotational speed whereby the first power supply circuit

10

A generates output voltage. On the contrary, the pulse signals Vq

1

′ and Vq

2

′ are generated after the output voltage of the first power supply circuit

10

A is established.

As described above, when a control signal of a rectangular shape is generated by waveform-shaping the negative half-wave voltage of the magneto-generator mounted on the crank shaft of the engine with a predetermined positional relationship, rising edge positions θ

11

, θ

21

and falling edge positions θ

12

, θ

22

of the pulse signals Vq

1

(or Vq

1

′), Vq

2

(or Vq

2

′) correspond to a specific rotational angle position of the crank shaft.

In the present invention, as described above, the rotational information (the information on the rotational angle position and the rotational speed information) on the internal combustion engine is obtained from the rising edges or the falling edges of the first pulse signals Vq

1

, Vq

1

′ and the second pulse signals Vq

2

, Vq

2

′ which are obtained by waveform-shaping the negative half-wave output voltage of the exciter coil

6

, so that the ignition position at the starting time and the extremely low speed state is established, and at the same time, arithmetical operation of the ignition position at a steady state driving time and detection of the arithmetically operated ignition position are performed.

In order to decide the ignition position at the starting time and the extremely low speed state of the engine, the rising or the falling edge position of any pulse signal is set to a position adequate as the ignition position at the starting time and the extremely low speed state of the engine. The ignition position at the starting time and the extremely low speed state of the engine is usually a position slightly advanced more than a top dead center (rotational angle position of the crank shaft at a time when a piston reaches the top dead center).

In order that an ignition operation is performed at the starting time and the extremely low speed state of the engine, it is necessary to give the ignition signal Vi to the discharge thyrister Thi after the ignition capacitor Ci was charged by the positive half-wave voltage Vp of the exciter coil

6

. Hence, among the pulse signals, the rising edge position θ

21

or the falling edge position θ

22

of the second pulse signal Vq

2

is allowed to correspond to the ignition position at the starting time and the extremely low speed state of the engine.

In the example shown in

FIG. 1

, the magnetic rotor

4

and the stator

7

are mounted on the engine so that the falling edge position θ

22

of the pulse signal Vq

2

is allowed to correspond to the ignition position at the starting time and the extremely low speed state of the engine. That is, the falling edge of the pulse signal Vq

2

is taken as an ignition position for extremely low speed state detection signal.

In order to arithmetically operate the ignition position at the steady state, data including the information on the rotational speed of the engine is required. As for the data including the information on the rotational speed of the engine, time required for the crank shaft to make a constant angular rotation such as a period of each pulse signal, signal width of each pulse signal or intervals of two pulse signals can be used. When the ignition position is arithmetically operated, this time data may be converted into a speed or the time data may be used as it is.

Further, in order that the ignition operation is performed at the ignition position arithmetically operated at the steady state, it is necessary to be able to accurately detect the arithmetically operated ignition position. For that purpose, the rotational angle position serving as a reference of the crank shaft is established as a reference position, and the ignition position is arithmetically operated in the form of a time (time to be measured by an ignition timer) Tig required for the engine to rotate from the reference position to the ignition position at the arithmetically operated rotational speed, and when it is detected that the reference signal is generated, the ignition timer (timer provided in the microcomputer) is started, thereby measuring the ignition position. In the present specification, the time Tig which gives the ignition position is referred to as “an ignition position detection time”.

Although the reference position may be at a position where the phase is advanced more than the ignition position to be measured, in order to enhance detection accuracy of the ignition position, it is desirable that the edge position of the pulse signal generated at a position as close as possible to the ignition position is taken as the reference position. Here, the edge position (same as the falling edge position of Vq

1

) of the first pulse signal Vq

1

′ should be established as the reference position.

In this example, by the exciter coil

6

and the waveform shaping circuit

11

, the reference position detection signal is generated at the reference position established at a position sufficiently advanced more than the rotational angle position of the crank shaft corresponding to the top dead center of the internal combustion engine, and a signal generating portion for generating the ignition position detection signal for extremely low speed state is formed at a position adequate as the ignition position at the starting time and the extremely low speed state of the internal combustion engine.

The pulse signals Vq

1

and Vq

2

obtained from the output terminal

11

a

of the waveform shaping circuit

11

are applied between the base and the emitter of the NPN transistor TR

3

whose emitter is grounded. The collector of the transistor TR

3

is connected to the output terminal

10

b

of the non-grounded side of the second power supply circuit

10

B through a resistor R

6

, and at the same time, is connected to one end of an ignition signal supply capacitor C

3

, and the other end of the capacitor C

3

is connected to the gate of the discharge thyristor Thi through a diode D

6

whose anode is directed to the capacitor C

3

side. Further, between the other end of the capacitor C

3

and the ground, a diode D

7

whose anode is grounded is connected.

In this example, the transistor TR

3

, the capacitor C

3

, the resistor R

6

and the diode D

7

comprise the ignition control portion for extremely low speed state

12

, and a signal Vio outputted by this ignition control portion is given to the gate of the discharge thyristor Thi through the diode D

6

.

The operation of the illustrated ignition control portion for extremely low speed state

12

is as follows. When the pulse signal Vq

1

or Vq

2

rises and the transistor TR

3

becomes the on-state, the charge accumulated in the capacitor C

3

is instantaneously discharged between the collector and the emitter of the transistor TR

3

and through the diode D

7

. In a state where the pulse signal is at a high level and the transistor TR

3

is the on-state, the charging current of the capacitor C

3

is bypassed from the capacitor C

3

through the transistor TR

3

so that the charging of the capacitor C

3

is prevented. When the pulse signal Vq

1

or Vq

2

given in such a state falls and the transistor TR

3

is put into an off-state, by the output voltage of the second power supply circuit

10

B, the current flows through the resistor R

6

, the capacitor C

3

, the diode D

6

and between the gate and the cathode of the discharge thyristor Thi so that the capacitor C

3

is charged. By the charging current of this capacitor C

3

, the ignition signal is given to the discharge thyristor Thi. The ignition signal given to the discharge thyristor from the ignition control portion for extremely low speed state

12

is vanished when the charging of the capacitor C

3

is completed and the charging current no longer flows.

The illustrated ignition control portion for extremely low speed state

12

, in the manner as described above, gives to the discharge thyristor Thi an ignition signal Vih

1

or Vih

2

at the falling edge of the pulse signal Vq

1

or Vq

2

. The width of the ignition signal Vih

1

or Vih

2

is sufficiently narrow. One example of the waveforms of these ignition signals was shown in FIG.

7

E.

When the ignition control portion for extremely low speed state

12

gave the hard ignition signal Vih

1

to the discharge thyristor Thi by the falling edge of the first pulse signal Vq

1

whose phase is more advanced than the positive half-wave voltage Vp of the exciter coil, the ignition capacitor Ci is not yet charged; therefore, no ignition operation is performed. After the exciter coil

6

generates the positive half-wave voltage Vp and the ignition capacitor Ci is charged, when the hard ignition signal Vih

2

is given to the discharge thyristor Thi by the falling edge of the second pulse signal Vq

2

, the discharge thyristor Thi becomes the on-state and the charge of the ignition capacitor Ci is discharged through the primary coil W

1

of an ignition coil IG so that the ignition operation is performed.

That is, though the hard ignition signal Vih

1

generated by the falling edge of the pulse signal Vq

1

becomes useless, it does not exert any influence on the ignition operation.

In order to perform arithmetical operation of the rotational speed at the steady state driving time, arithmetical operation of the ignition position and detection of the arithmetically operated ignition position, an ignition control portion for steady state

13

equipped with a microcomputer

13

A comprising CPU, ROM, RAM, a timer and the like is provided, and the first and the second pulse signals Vq

1

′, Vq

2

′ which are obtained from the output terminal

11

b

of the waveform shaping circuit

11

are inputted to one port A

1

of the microcomputer

13

A. A power supply terminal

13

a

of the microcomputer

13

A is connected to the output terminal

10

a

of the first power supply circuit

10

A, and when an output voltage Vdc of the first power supply circuit

10

A is established, the microcomputer

13

A is put into an operable state.

The microcomputer

13

A, as described later, is programmed in such a manner as to switch a recognition mode of the signal inputted to the port A

1

to a first mode to recognize the rising edge and a second mode to recognize the falling edge and, from among each edge of the pulse signals Vq

1

′, Vq

2

′ inputted in order, recognizes the edge necessary to obtain the rotational information on the engine. In the present embodiment, the rising and falling edges of the pulse signal Vq

1

′ and the rising edge of the pulse signal Vq

2

′ are recognized.

The microcomputer

13

A, when its power supply voltage is established so as to put it into an operable state, first performs a processing to discriminate which signal is the first pulse signal and which signal is the second pulse signal among a series of pulse signals given from the waveform shaping circuit

11

. The discrimination of the first pulse signal Vq

1

and the second pulse signal Vq

2

can be performed by utilizing the fact that there is a relation ship of T

1

>>T

2

between a time T

1

from the generation of the first pulse signal Vq

1

to the generation of the second pulse signal Vq

2

and a time T

2

from the generation of the second pulse Vq

2

to the generation of the next first pulse signal Vq

1

. For example, a pulse recognition timer for measuring time intervals between the rising edges of the pulses is provided and, as shown in

FIG. 7

, measurement values of the timer are read by the rising edges of the pulse signals Vq

1

and Vq

2

so that the times T

1

, T

2

are measured and stored, and when there is a relationship of (T1/2)>T

2

established between T

1

and T

2

, it can be recognized that the edge at a time when the time T

1

was measured is the rising edge of the first pulse signal.

As described above, when the rising edge and the falling edge of the pulse signal is recognized by one port, the required number of ports can be reduced in contrast to the case where the pulse signal Vq

1

′ and Vq

2

′ are read and recognized from a separate port, respectively, so that those moderate in price can be used as the microcomputer.

The other port A

2

of the microcomputer

13

A serves as an output port of the ignition signal, and a soft ignition signal Vis outputted from the port A

2

is supplied to the gate of the discharge thyristor Thi as an ignition signal Vi through a diode D

8

whose cathode is directed to the discharge thyristor side.

In this example, the diodes D

6

and D

8

comprise an OR circuit

14

giving the output of the ignition control portion for extremely low speed state

12

or the output of the ignition control portion for steady state

13

to the gate of the discharge thyristor Thi as the ignition signal.

Between the anode (the non-grounded side output terminal of the ignition control portion for extremely low speed state

12

) of the other diode D

6

comprising the OR circuit

14

and the ground, a cancel switch

15

is connected. The illustrated cancel switch

15

comprises an NPN transistor TR

4

whose emitter is grounded and collector is connected to the anode of the diode D

4

, and to the base of this transistor TR

4

, a cancel command signal Vk is inputted from a port A

3

of the microcomputer

13

A.

The microcomputer

13

A, when the rotational speed of the engine exceeds the set speed, is programmed in such a manner as to comprise cancel command generating means for generating a cancel command Vk during the rising edge of the first pulse signal Vq

1

′ is recognized till the rising edge of the second pulse signal Vq

2

′ is recognized, and when the ignition control portion for extremely low speed state

12

outputs an ignition signal Vio for the extremely low speed state during the cancel command is generated, the transistor TR

4

becomes the on-state so that the ignition signal Vio is bypassed from the discharge thyristor Thi.

One example of flowcharts showing an algorism of a program to be executed by the microcomputer

13

A in the present embodiment was shown in

FIG. 9

to

FIG. 11

, and a timing chart for explaining this program was shown in

FIG. 8A

to FIG.

8

D.

FIG. 9

shows a main routine of the program to be executed by the microcomputer

13

A, and

FIG. 10

shows a pulse signal edge interruption routine to be executed when the rising and falling edges of the first pulse signal Vq

1

′ is recognized and the rising edge of the second pulse signal Vq

2

′ is recognized. Further,

FIG. 11

shows an ignition timer interruption routine to be executed when the ignition timer has completed the measurement of the time set.

When the power supply of the microcomputer is established, at first, the main routine of

FIG. 9

is started. In this main routine, initialization of each portion is performed first in step

1

, and subsequently in step

2

, interruption is permitted and, after that, in step

3

, average rotational speed data of the engine is arithmetically operated. This average rotational speed data may be the time (=T

1

+T

2

) as it is, which is required for the crank shaft of the engine to make one rotation.

In step

3

, after the data of the average rotational speed N was found, in step

4

, whether or not the pulse signal edge interruption shown in

FIG. 10

was performed more than three times is determined. As described later, in the present invention, in order to recognize the pulse signals Vq

1

, Vq

2

, it is necessary to perform the interruption routine shown in

FIG. 10

three times after the microcomputer has been put into an operable state. In step

4

of the main routine, when the number of times (the edge interruption number of times) to perform the interruption of

FIG. 10

is less than three times, decision is made that the recognition of the pulse signal is not yet completed, and the step advances to step

5

and prohibits the output of the cancel signal Vk.

In step

4

, when decision is made that the edge interruption is performed three times or more, the step is advanced to step

6

and decision is made whether the average rotational speed N is more than the soft ignition rotational speed Ns. After that, decision is made that N<Ns, the step is advanced to step

5

and the output of the cancel signal is prohibited.

In step

6

, when decision is made that N≧Ns, the step is advanced to step

7

to allow the cancel signal Vk to be outputted from the port A

3

, and, next, in step

8

, by using an ignition position arithmetical operation map which gives a relationship between the data (time or rotational speed) giving the average rotational speed N and the ignition position, the ignition position in the arithmetically operated average rotational speed is arithmetically operated. This ignition position is arithmetically operated, for example by measuring an angle from the crank angle position corresponding to the top dead center of the engine toward an advanced angle side.

The microcomputer

13

A is programmed in such a manner as to switch the recognition mode of the signal inputted to the port A

1

to the first mode to recognize the rising edge of the pulse signal and the second mode to recognize the falling edge. However, in a state where initialization of each portion has been performed after the microcomputer was put into an operable state, the recognition mode of the signal to be inputted to the port A

1

is switched to the first mode. For this reason, when the rising edge of the pulse signal Vq

1

′ or Vq

2

′ is appeared after each portion of the microcomputer has been initialized, the interruption routine of

FIG. 10

is executed.

In this example, the interruption routine of

FIG. 10

is taken as being executed at the position of the crank angle θ

1

shown in FIG.

8

. In this interruption routine, first, in step

1

, decision is made as to whether or not the interruption of this time is an interruption by the rising edge. Since the pulse signal edge interruption to be initially executed is an interruption by the edge, step

2

is executed after step

1

. In step

2

, a pulse recognition time Tx which is a measurement value of a pulse recognition timer (a timer provided inside the microcomputer) is read and stored in a memory. Next, the step advances to step

3

, and performs a pulse recognition processing. In this pulse recognition processing, the a pulse recognition time Tx−1 read last time and the pulse recognition time Tx read this time are compared, and when Tx>2×Tx−1, the pulse signal whose rising edge was recognized this time is decided as the first pulse signal Vq

1

′, and when Tx≦Tx−½, the pulse signal whose rising edge was recognized this time is decided as the second pulse signal Vq

2

′.

After the pulse recognition processing was performed in step

3

, the step is advanced to step

4

, and decision is made as to whether or not the pulse signal inputted this time is a pulse signal of an advancing side (the first pulse signal) for the positive half-wave output voltage Vp of the exciter coil.

Since the pulse recognition timer is not set initially, the pulse recognition time Tx of the timer read in step

2

is zero, and, therefore, decision can not be made as to whether or not the pulse whose rising edge was recognized this time is the advancing side pulse. Consequently, the step is moved from step

4

to step

5

, and sets the pulse recognition timer so that the measurement of the pulse recognition time Tx is allowed to start from zero, and after that, is returned to the main routine.

Next, when the rising edge of the pulse signal is inputted to the port A

1

at the position of the crank angle θ

2

, steps

1

and

2

of the interruption routine of

FIG. 10

are executed again, and the pulse recognition time Tx (T

2

in the example shown in

FIG. 8D

) measured initially is read and stored. Subsequently, in step

3

, though the pulse recognition processing is performed, since the pulse recognition time Tx is measured still only for one at this point of time, the pulse recognition processing cannot be performed as yet. For this reason, in step

4

, decision cannot be made that the rising edge of this time is the rising edge of the advancing side pulse signal (the first pulse signal), so step

5

is executed. In step

5

, the pulse recognition timer is set again so that the measurement of the pulse recognition time Tx is resumed.

Next, when the third pulse signal edge interruption is executed at the position of the crank angle θ

3

, the pulse recognition processing is made possible from the pulse recognition time Tx (T

1

in the example shown in

FIG. 8

) measured in step

2

and the pulse recognition time Tx−1 (T

2

in the illustrated example) measured last time. In this pulse recognition processing (step

3

), the time TX measured this time and the time Tx−1 measured last time are compared, and when Tx>2×Tx−1, decision is made that the pulse signal whose rising edge was recognized this time is the first (advancing side) signal Vq

1

′, and when Tx≦Tx−½, decision is made that the pulse signal whose rising edge was recognized this time is the second (delaying side) pulse signal Vq

2

′. In the illustrated example, since T

1

>2×T

2

, decision is made that the pulse signal whose rising edge was recognized this time is the first pulse signal Vq

1

′ of the advancing side.

In this way, when the interruption routine of

FIG. 10

is executed three times after the microcomputer was made operable, the pulse signal generated in order by the waveform shaping circuit

11

can be recognized as to be either of the first and the second pulses.

In step

4

, when it is confirmed that the pulse signal whose rising edge was inputted this time was decided as the pulse signal Vq

1

′ of the advancing side, subsequently in step

6

, the pulse recognition timer is set to resume the measurement of the pulse recognition time Tx, and in step

7

, an instantaneous speed measuring timer (a timer provided inside the microcomputer) is set to start the measurement of the time to obtain data of the instantaneous speed. Subsequently, in step

8

, the recognition mode of the port A

1

is reversed so that the port A

1

of the CPU recognizes the falling edge of the input signal, and after that (after the recognition mode of the signal is switched to the second mode), the step returns to the main routine.

As described above, when the rising edge of the first pulse signal Vq

1

′ is recognized, since the recognition:m ode of the signal to be inputted to the port A

1

is switched to the mode to recognize the falling of the signal, the interruption routine of

FIG. 10

is executed when the falling edge of the first pulse signal Vq

1

′ is inputted. At this time, in step

1

, since it is decided as the interruption by the falling edge, subsequently, step

9

is executed to read an instantaneous speed measurement time Tn of the instantaneous speed measuring timer set in step

7

in the interruption of the last time. Subsequently, in step

10

, an instantaneous rotational speed is arithmetically operated from this measurement time Tn, and in step

11

, the ignition position, which is arithmetically operated in the main routine, is converted into the ignition position detection time Tig. This ignition position detection time Tig is a time required for the crank shaft to rotate at the instantaneous rotational speed arithmetically operated in step

10

from the reference position (in this example, the falling position of the first pulse signal Vq

1

′) to the ignition position arithmetically operated in the main routine.

In step

11

, after the ignition position detection time Tig was arithmetically operated, in step

12

, the ignition position detection time Tig is set in the ignition timer (the timer inside the microcomputer) to start the measurement of the ignition position. After that, in step

13

, an ignition flag is set to “1” and, after that, in step

14

, the signal recognition mode of the port A of the CPU is reversed to the mode to recognize the rising of the input signal (the first mode), and after that, the step returns to the main routine.

When the ignition timer completes the measurement of the ignition position detection time Tig (completes the measurement of the ignition position), the ignition timer interruption shown in

FIG. 11

is executed. In this interruption routine, first, in step

1

, decision is made as to whether or not the ignition flag is “1”, and when the ignition flag is “1”, the step advances to step

2

to start the output of the soft ignition signal. Subsequently, in step

3

, an ignition signal output stop time detection time is set in the ignition timer to start the measurement thereof. Then, in step

4

, after the ignition flag is set to “0”, the step returns to the main routine. When the ignition timer completes the measurement of the ignition signal output stop time detection time, the ignition timer interruption shown in

FIG. 11

is executed again. At this time, since the ignition flag is set to “0”, step

5

is executed to stop the output of the ignition signal.

In the above described example, the ignition signal is given to the discharge thyristor Thi from the ignition control portion for extremely low speed state

12

at the starting time of the engine and at the time when the rotational speed is below a set value Ns (soft ignition starting rotational speed) so that the ignition operation is performed, and when the rotational speed of the engine has exceeded the set value Ns after the microcomputer

13

A was put into an operable state, the cancel signal Vk is generated from the microcomputer to put into the on-state the transistor TR

4

comprising the cancel switch, so that the hard ignition signal Vih to be given to the discharge thyristor Thi from the ignition control portion for extremely low speed state

12

is bypassed from the discharge thyristor.

When comprised in this way, the hard ignition signal can be prevented from being given to the discharge thyristor by the rising or the falling of the first pulse signal at the steady state driving time and, therefore, there is no fear of the engine causing an accidental fire due to a state developed where the ignition capacitor Ci is not charged.

In the case where the programs shown in

FIG. 9

to

FIG. 11

are executed by the microcomputer, reference :position detection means is comprised of step

1

to step

5

of

FIG. 10

, wherein the first and the second pulse signals are recognized from the signal widths of the first and the second pulse signals and the intervals of the first and the second pulse signals, and the position of the rising or the falling edge of one of the recognized pulse signals are detected as the reference position.

Further, average speed detection means is comprised of step

3

of the main routine of

FIG. 9

, wherein an elapsed time since when the rising edge position or the falling edge position of the first pulse signal (the rising edge in the above embodiment) is detected till the same position is detected after the crank shaft has made one rotation is found as data to detect the average rotational speed of the internal combustion engine.

Further, instantaneous speed measurement starting means is comprised of step

7

and step

8

of the interruption routine of

FIG. 10

, wherein a timekeeping for an instantaneous speed measurement is started when the rising edge of the first pulse signal was recognized so that the recognition mode of the signal to be inputted to the port A

1

is switched to the second mode, and instantaneous speed detection means is comprised of step

9

and step

10

of the interruption routine of

FIG. 10

, wherein the time measured from the time when the rising edge of the first pulse signal was recognized till the time when the falling edge was recognized is found as data to detect an instantaneous rotational speed of the internal combustion engine.

Rotational speed detection means is comprised of the average speed detection means and the instantaneous speed detection means, wherein the data to detect the rotational speed of the internal combustion engine by using at least one of the first and the second pulse signals is found.

Further, ignition position arithmetically operating means is comprised of step

8

of the main routine shown in FIG.

9

and step

11

of the interruption routine of

FIG. 10

, wherein the ignition position of the internal combustion engine for the detected rotational speed is arithmetically operated in the form of the time required for the crank shaft of the engine to rotate from the reference position to the ignition position, and ignition position detection means is comprised of steps

12

and

13

of the interruption routine of FIG.

10

and ignition timer interruption routine of

FIG. 11

, wherein the measurement of the ignition position is started when the reference position is detected, the ignition signal is given to the discharge thyristor Thi when the measurement of the ignition position is completed, and cancel command generating means is comprised of steps

4

to

7

of the main routine of

FIG. 9

, wherein a cancel command is generated when the rotational speed of the internal combustion engine exceeds the set value.

In the capacitor discharge type ignition device, it is necessary to put the discharge thyristor into the off-state before the positive half-wave voltage of the exciter coil rises. Accordingly, like the example as described above, in the case where the hard ignition signal Vih is generated by the falling edges of the first and the second pulse signals Vq

1

and Vq

2

which were obtained by waveform-shaping the negative half-wave voltages Vn

1

and Vn

2

of the exciter coil

6

, respectively, it is necessary to vanish the first and the second pulse signals Vq

1

and Vq

2

before the positive half-wave output voltage of the exciter coil rises.

In the example shown in

FIG. 1

, the waveform shaping circuit

11

was comprised in such a manner that the rising and falling edges of the first pulse signal are generated, respectively at the zero point and the peak point of the rising side of the first negative half-wave voltage outputted by the exciter coil

6

, and the rising and falling edges of the second pulse signal are generated, respectively at the zero point and the peak point of the rising side of the second negative half-wave voltage outputted by the exciter coil. However, as shown in

FIGS. 6A and 6B

, the waveform shaping circuit

11

can be also comprised in such a manner that the first pulse signal is generated during the first negative half-wave voltage Vn

1

outputted by the exciter coil exceeds a threshold level Vth, and the second pulse signal is generated during the second negative half-wave voltage outputted by the exciter coil exceeds a threshold level.

As shown in

FIGS. 6A and 6B

, in order to generate the first and second pulse signals Vq

1

and Vq

2

during the first and second negative half-wave output voltages Vn

1

and Vn

2

exceed the threshold level, for example, as shown in

FIG. 2

, the other end of the exciter coil

6

may be connected to the base of the NPN transistor TR

1

through a resistor R

2

′ and a Zener diode ZD

2

. In this case, the threshold level Vth can be adequately adjusted by a resistance value of the resistor R

2

′ and a Zener voltage of the Zener diode ZD

2

.

Further, the second power supply circuit

10

B which gives the power supply voltage to the ignition control portion for extremely low speed state

12

is not limited to the circuit shown in

FIG. 1

, and, for example, as shown in

FIG. 2

, can be also comprised of a diode D

10

′ whose anode is connected to the other end of the exciter coil

6

, an NPN transistor TR

5

whose collector is connected to the cathode of the diode through the resistor R

1

′, a resistor R

11

connected between the collector and the base of the transistor TR

5

, a Zener diode ZD

1

′ whose anode is directed to ground side between the base and the ground of the transistor TR

5

and the power supply capacitor C

1

′ connected between the emitter and the ground of the transistor TR

5

.

In the second power supply circuit

10

B shown in

FIG. 2

, the transistor TR

5

becomes the on-state when the negative half-wave output voltage of the exciter coil is below the set value, and allows the charging current to flow into a second power supply capacitor C

1

′. When the negative half-wave output voltage of the exciter coil exceeds the set value, the Zener diode ZD

1

′ becomes the on-state, and the current to be given to the base of the transistor TR

5

′ from the exciter coil through the resistors R

1

′ and R

11

is bypassed from the transistor, and, therefore, the transistor TR

5

′ is put into the off-state so as to stop the charging of the capacitor C

1

′. Consequently, the terminal voltage (the output voltage of the second power supply circuit

10

B) of the capacitor C

1

′ is limited below the set value and the second power supply circuit

10

B is prevented from outputting an excessive direct current voltage.

In this example, a charging control circuit is comprised of the diode D

10

′, the resistors R

1

′ and R

11

and the transistor TR

5

, wherein the second power supply capacitor C

1

′ is charged when the negative half-wave output voltage of the exciter coil is below the set value, and the charging of the second power supply capacitor C

1

′ is stopped when the negative half-wave voltage of the exciter coil exceeds the set value.

Since the power supply voltage required for generating the hard ignition signal from the ignition control portion for extremely low speed state

12

may be lower than the voltage (5[V]) required for operating the microcomputer

13

A, when a separate power supply is provided for the ignition control portion for extremely low speed state

12

as shown in

FIG. 3

, the rotational speed (the starting rotational speed) whereby the supply of the hard ignition signal to the discharge thyristor is started is lowered and the starting characteristic of the engine can be improved.

Note that, in the example shown in

FIGS. 1 and 2

, the circuit (the circuit comprising the diode D

10

, the resistor R

1

, the capacitor C

1

and the Zener diode ZD

1

) of the stage portion preceding to the regulator Reg of the first power supply circuit

10

A can be also replaced by a circuit having the same constitution as the second power supply circuit

10

B shown in FIG.

2

.

In the above described example, the signal generating portion is comprised of the exciter coil

6

and the waveform shaping circuit which waveform-shapes the negative half-wave output voltage of the exciter coil and converts it into the pulse signal, and the rising or the falling edge of the pulse signal obtained by waveform-shaping the negative half-wave output voltage of the exciter coil is used as the reference position detection signal or the ignition position detection signal for extremely low speed state. However, the signal generating portion can be also comprised of the signal generator which is mounted on the internal combustion engine and generates the signal pulse at the reference position and the ignition position for extremely low speed state, respectively and the waveform shaping circuit for waveform-shaping the output of the signal generator.

FIG. 3

shows an example wherein the signal generating portion is comprised of the signal generator and the waveform shaping circuit. In

FIG. 3

, reference numeral

20

denotes a pulsar coil provided in the signal generator which is mounted on the internal combustion engine, and this pulsar coil is provided in the signal generator mounted on the internal combustion engine not shown, and as shown in

FIG. 12B

, when the rotational angle position θ of the crank shaft of the internal combustion engine corresponds to the reference position θ

1

set at the position sufficiently advanced more than a rotational angle position TDC which corresponds to the top dead center of the engine, a first signal P

1

having a pulse waveform is generated, and when the rotational angle position of the internal combustion engine corresponds to a position θ

2

adequate as the ignition position at the starting time and the extremely low speed state, a second signal P

2

having the pulse waveform is generated.

The signal generator comprises, for example, the rotor mounted on the crank shaft and the like having a reluctor and synchronously rotating with the engine, an iron core having a magnetic pole portion opposing to the reluctor of the rotor at its top end, a pulsar coil wound around the iron core and a permanent magnet letting magnetic flux flow to the iron core, and is comprised of a signal armature for generating the signals P

1

and P

2

of a pulse waveform having a different polarity when the edge of the front end side and the edge of the rear end side in the rotational direction of the reluctor were detected, respectively.

Reference numeral

11

denotes the waveform shaping circuit, which waveform-shapes the first signal P

1

and the second signal P

2

outputted by a pulsar coil

20

, respectively and outputs the reference position detection signal Vs

1

and the ignition position detection signals for extremely low speed state Vs

2

, Vs

2

′. Among these signals, the ignition position detection signal for extremely low speed state Vs

2

, similar to the pulse signal Vq

2

of the example shown

FIGS. 1 and 2

, is a signal outputted through the passive element (parallel circuit of a capacitor and a resistor, and a Zener diode) when the input signal P

2

exceeds. the threshold value, and is a signal generated immediately after the starting operation of the engine is started. Other signals Vs

1

and Vs

2

′ are signals outputted through an amplifier element such as transistor and the like. Among each portion of the waveform shaping circuit

11

, the portion generating the signals Vs

1

and Vs

2

′ operates with the output voltage of the first power supply circuit

10

A as the power supply voltage.

The reference position detection signal Vs

1

and the ignition position detection signal for extremely low speed state Vs

2

′ are inputted to the ports A

11

and A

12

of the microcomputer

13

A.

The ignition control portion for extremely low speed state

12

comprises a PNP transistor TR

6

whose emitter is connected to an output terminal

20

b

of the second power supply circuit

10

B through a resistor R

20

and collector is connected to the gate of the discharge thyristor Thi through the diode D

6

and an NPN transistor TR

7

whose emitter is grounded and collector is connected to the base of the transistor TR

6

, and the ignition position detection signal for extremely low speed state Vs

2

is inputted to the base of the transistor TR

7

. Other portions are comprised similarly to the ignition device of FIG.

1

.

In the example shown in

FIG. 3

, when the pulsar coil

20

generates the second signal P

2

and the waveform shaping circuit

11

generates the ignition position detection signal for extremely low speed state Vs

2

, the transistor TR

7

is put into the on-state. In this way, the transistor TR

6

becomes the on-state to give the ignition signal to the discharge thyristor Thi.

The microcomputer

13

A detects the rotational speed of the engine from the intervals of the signals Vs

1

and Vs

2

′, and arithmetically operates the ignition position in the detected rotational speed. Further, the microcomputer starts the measurement of the ignition position which was arithmetically operated when the reference position detection signal Vs

1

was generated, and when the measurement has been finished, the ignition signal Vk is outputted so as to perform the ignition operation.

As described above, according to the present invention, since the power supply circuit provided in the ignition control portion for extremely low speed state for giving the ignition signal to the discharge thyristor at the starting time and the extremely low speed state of the internal combustion engine is separately provided from the power supply circuit for giving the power supply voltage to the ignition control portion for steady state, the extremely low speed state control portion can be operated before the ignition control portion for steady state starts the operation.

Consequently, not only the starting rotational speed of the engine can be lowered to improve the starting characteristic of the engine, but also the rotation in the idling region of the engine can be stably performed.

Although preferred embodiments of the invention have been described and illustrated with reference to the accompanying drawings, it will be understood by those skilled in the art that it is by way of example, and that various changes and modifications may be made without departing from the spirit and scope of the invention, which is defined only to the appended claims.

Number	Name	Date	Kind
3736914	Schmaldienst et al.	Jun 1973	A
4402298	Morita	Sep 1983	A
4462363	Nanjyo et al.	Jul 1984	A
4911126	Notaras et al.	Mar 1990	A

Capacitor discharge type internal combustion engine ignition device

Information

Patent Number

Date Filed

Date Issued

Inventors

Original Assignees

Examiners

Agents

CPC

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US

International Classifications

Abstract

Description

Claims

Priority Claims (1)

US Referenced Citations (4)