AU488564B2 - High energy adaptive ignition via digital control - Google Patents
High energy adaptive ignition via digital controlInfo
- Publication number
- AU488564B2 AU488564B2 AU16936/76A AU1693676A AU488564B2 AU 488564 B2 AU488564 B2 AU 488564B2 AU 16936/76 A AU16936/76 A AU 16936/76A AU 1693676 A AU1693676 A AU 1693676A AU 488564 B2 AU488564 B2 AU 488564B2
- Authority
- AU
- Australia
- Prior art keywords
- ignition
- output
- pulse
- signal
- engine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Description
16.93 6/76
Background of the Invention
This invention relates to automotive ignition systems
and, more particularly, to a digitally implemented, constant
dwell time version thereof.
Electronically controlled ignition systems are well
known in the art. Such systems are favored over their
mechanical counterpart since the electronic system is more
accurate and reliable. Basically, the purpose of any
ignition system is to generate a spark suitable for firing
the combustion chambers at a predetermined engine angular
position. In mechanical breaker point type systems it has
been found that spark energy falls off at increasing engine
RPM. This may result in inefficient fuel combustion or even
engine misfiring. The use of electronic circuitry in the
ignition can result in a constant spark energy level over
the entire range of engine active operation.
While fully electronic ignition systems have resulted
in enhanced engine performance, they have suffered certain
limitations. For example, in inductive storage type systems,
spark energy level is a function of battery voltage and
ignition coil resistance. Each of these parameters is
temperature dependent, and, in automotive applications,
temperature extremes are to be expected. Prior ignition
systems have not compensated for these variables.
A further failing in prior art ignition systems is
acceleration response. For proper engine operation, an
ignition system must respond to accelerations of up to 4,000 2 488,564
16,93 6' /76
have a time ?M per second. Electronic ignitions ncrmally suitably responsive. ig, which prevents them from being ignitions have required a In addition, fully electronic resulting in a very arge number of electronic components, of the components are xpensive system. Moreover, many degradation due to aging emperature dependent and suffer
ffects.
Summary of the Invention therefore, to provide It is an object of this invention, which compensates for the Sfully electronic ignition system of the ignition components. nvironmental and aging effects invention, sensors in the Briefly, according to the type types of pulses. The first ignition system provide two synchronous to the desired isan ignition pulse which occurs firing. Between ignition time of engine combustion chamber pulses is generated. The pulses, a sequence of position corresponds to a given engine instance of a position pulse
angular position. position pulses whereby First circuitry processes the of engine position is an output signal representative first of an ignition pulse, the produced. At the occurrence level from which it again circuitry is reset to a reference pulses. In the digital begins processing the position the first circuitry is implementation of the invention, counter. comprised of a resettable position
488.564
16,93 6/76
Second circuitry also processes the position pulses to
produce at its output a signal representative of engine RPM.
In. the preferred embodiment of the invention, the second
circuitry is comprised of a clock, a speed counter, and a
speed register. The clock generates a signal of predeter-
mined time period which is suitable for activating the speed
counter. In its activated state, the speed counter produces
an output count representative of the number of position
pulses generated during each clock signal. At the conclu-
sion of a clock period, the total count from the speed
counter is transferred to the speed register.
A comparator monitors the output count from both the
first circuitry, e.g. position counter, and the second
circuitry, e.g. the speed register. The comparator produces
a trigger signal at a predetermined relationship between the
outputs from the first and second circuits. This rela-
tionship is such that once a trigger signal is generated, it
activates a switch which in turn maintains the ignition
system at a constant dwell time and thus a constant spark
energy level, provided there is a constant battery voltage
and ignition coil resistance.
To compensate for varying component values, such as
battery voltage and ignition coil resistance, a means moni-
tors the ignition energy level and generates a feedback
signal representative thereof. In a particular embodiment,
the feedback signal may be comprised of the synchronous
occurrence of a given current level in the ignition coil and
generated position pulses. In response to the feedback
signal, a control means alters the occurrence of the trigger
signal such that dwell time is adjusted to maintain a
488,564
16,93 6/76
substantially constant ignition energy level. In the pre-
ferred embodiment, the control means responds to the feed-
Dack signal to vary the clock period interval. When, for
3xample, the control means detects an increasing current
limit feedback signal, such as might happen with decreased
:oil resistance or increased battery voltage, the clock time
period is decreased whereby the comparator institutes dwell
at a later time in the engine cycle. In so doing, the
feedback provides a fully adaptive constant energy ignition
system. Finally, in the preferred embodiment, each compon-
ent may be implemented by using digital technology, whereby
the resulting system comprises a minimum of external com-
ponents. Brief Description of the Drawings
Fig. 1 is a graphical representation of the operation
of a system according to the invention;
Fig. 2 illustrates the preferred embodiment of the in-
vention in block diagram form; and Fig. 3 is a more detailed diagram of the preferred em-
bodiment. .Detailed Description of the
Preferred Embodiment of the Invention
The present system utilizes both engine position and
speed information to maintain a constant ignition energy
level. Since the energy of an inductive storage type ig-
nition is a function of dwell time the time during dwell which battery current is passed through the coil),
control may be utilized to provide the desired operation.
Fig. la represents the angle offset required at con-
stant engine speed to yield a constant dwell time, Tdo.
488.564
16,93 6/76
Plotted vertically is engine position angle and horizontally 0 is time. max represents the maximum allowable angle in a
given engine cycle, e.g. 450 of the distributor for an 8
cylinder engine. T represents the time corresponding to 0mmax
or the angle predictor, represents the angle with respect P to Omax which corresponds to the time Tp with respect to the T cycle time T such that dwell time do T Tp) remains
constant. Thus, it is seen that
Op Omax 10 do'
where w 0 is the angular velocity of the engine.
Fig. lb plots the desired angle offset as a function of
.time under engine acceleration. Note that the angle increases
exponentially with time while the angle predictor 0p
decreases linearly, since it is proportional to speed which
increases linearly under acceleration. Given an accelera-
tion a, it can be seen that
Op 00 Tdo 80 [0O a (d)
A predictor line can be constructed originating at the 0 T of the angle 00 O do and extending to the intersection
parabolic angle plot with the coordinate Op. The horizontal
coordinate of the intersection corresponds to the time Tp T such that T T do (a constant).
Thus, it should be observed that a constant dwell time
can be determined based on information as to engine position
and a predictor line which originates from the offset angle
corresponding to initial engine angular velocity, and descends
at a rate dependent upon engine acceleration. In substance
then, to maintain a constant dwell time the ignition system
must respond to engine position, speed, and acceleration. Fig. Ic illustrates a digital approximation to a constant
dwell type system. The approximation assumes that a sequence
6 488,564
16.93 6 /76
of digital pulses is generated between ignition pulses.
Each digital pulse corresponds to a particular engine angu-
lar position. Thus, engine angular position may be deter-
mined by counting the number of received position pulses
following an ignition pulse. For an accelerating engine,
the pulse count will rise at the parabolic rate previously
shown in Fig. lb. In turn, engine speed may be determined
by counting the number of position pulses generated during a
clock interval Tclk. For a given clock period Tclk the
number of pulses counted by the speed counter will increase
under engine acceleration. Thus, assuming the speed counter
starts at an initial count and counts down for each received
position pulse during the clock interval, it can be seen
that the final decremented count in the speed counter at the
end of a clock period traces the angle predictor line. At
a given number of clock intervals, the final count in the
speed counter will equal the count of the position counter.
This corresponds to the angle p and the time Tp that dwell
should be initiated if a constant dwell time Tdo is desired.
Hence, the time at which the output from the position counter
exceeds the output from the speed counter corresponds to the
time at which dwell should be initiated.
Fig. ld illustrates the desired angle offset 0 for a
system under acceleration and subject to a changing ignition
component, such as battery voltage or coil resistance. As-
suming that coil resistance decreases, or that battery
voltage increases, a corresponding correction to the pre-
dicted time Tp is easily made by decreasing the clock time
Tclk to T'clk This results in a new predicted time Tp
and a new desired dwell time Tdo' 7 488,564
16.93 6/76
Fig. 2 illustrates a block diagram implementation of
the system described with respect to Fig. Id. A first
engine sensor (not shown) generates a sync pulse at the
desired time of engine firing. The sync pulses are routed
to the ignition system via channel I. A series of position
pulses are generated by a second sensor (also not shown) and
routed to the system via channel II. Each position pulse
occurs at a particular engine angular position.
The position pulses are processed through a position
output counter 20, which begins at an initial value and
increments one count for each received position pulse. A
-reset input terminal 22 connects to channel I whereby a
subsequently received sync pulse resets the counter to its
initial value. Thus, the position output counter 20 produces
at its output terminal 24 a signal of the form Y K1 8,
where Y is representative of the output signal, K 1 represents
a constant, and 0 is the engine angular position. The
generated signal Y increases at a linear rate when the
engine is at constant velocity, and at a parabolic rate fo.*
engine acceleration. Hence, output signal Y may be used as
representative of the engine position signal indicated in
Figs. la-ld.
Engine speed is determined in a speed output counter
Speed counter 30 has a first input 32 which connects
to channel II and a second input 34 which connects to a
clock 36. At its output 38 the speed output counter
produces a signal which is representative of the number of
position pulses generated during each clock 36 time period.
For a given clock period, the number of position pulses
counted increases, thereby increasing the output signal Z.
8 488,564
16.936/76
Y signal A comparator 40 accepts at its first input 42 the second input output from the position counter 20, and at its When the 44-the speed output Z from speed counter 30. the signal Z comparator senses the signal Y is greater than
it activates its output 46. The output 46 of comparator 50. The connects to the "set" terminal 52 of a flip-flop to channel flip-flop has a "reset" input 54 which connects output 46 I, and a Q output 56. An activated comparator a trigger causes the Q output 56 of flip-flop 50 to produce terminal 62 of signal which is coupled to the trigger input
a switch 60.. Switch 60 has a first terminal 64 which connects 68. A in series through an ignition coil 66 to a battery a current sense second switch terminal 70 connects through 74. resistor 72 to a reference, or ground, potential by a Feedback from the ignition output is provided to the load resis- current limit amplifier 80 which connects The current tor 72 for sensing the current therethrough. 82 a signal repre- limit amplifier 80 produces at its output 66 is passing a sentative of the time during which the coil drop across the given current level, i.e. a given voltage T lim is fed back load resistor 72. This current limit time input 33. to the speed output counter 30 its Tdo adjust output 46 In operation, comparator 40 activates its count Z. Refer- when the position of count Y exceeds speed time that dwell ring to Fig. i, this corresponds to the dwell time. An should be initiated to maintain a constant the flip-flop 50 to activated comparator output 46 causes activates switch 60 to create a trigger signal which in turn builds up from its conductive state. Thereafter, current
488.564
16.936 /76 the battery 68 through ignition coil 66 and load resistor 72
to ground potential 74. When an ignition pulse is generated,
it travels via channel I to the reset input 54 of flip-flop
thereby deactivating flip-flop output 56 and actuating
switch 60 to the nonconductive state. Coil 66 thereby
combustion produces a high voltage output which fires the
chamber. A change in battery 68 voltage, or the resistance of
at which ignition coil 66 can significantly alter the rate of the the coil 66 reaches a given current representative
desired ignition energy level. To compensate for these
a feed- variables, the current limit amplifier 80 generates
back signal representative of the total time the output coil
signal is 66 is at the desired current, which feedback
applied to the speed output counter 30. In turn, the speed
thus varying. output counter alters its clock period to T'clk time at the speed count output Z and thereby altering the This, in turn, which the comparator output 46 is activated. constant adjusts dwell time to maintain a substantially
ignition energy level. A more detailed block diagram of the preferred embodi-
ment of the invention is given in Fig. 3, wherein similar
numbers have been used to identify identical components.
Position pulses are routed via channel II to the position
counter 20. Counter 20 is of the "up" type whereby each
subsequently received position pulse increments the counter
output 24. to the next higher count state. At the end of a
position pulse sequence, a sync pulse via channel I is
applied to the counter reset terminal 22, thereby returning
the counter to its initial state in preparation for subse-
quent counting.
The speed output counter 30 is comprised of a series of
individual blocks including a modulus M counter 110, a
16.936/76
modulus M divider 120, a time delay 130, a speed counter
140, a preset N memory 150 and a speed count register 160.
Speed output counter operalion may be understood as
follows. The clock 36 provides a clock signal rclk having a
frequency f0 This in turn is fed to the input. 122 of the
modulus M divider 120. Modulus M divider 120 frequenqy_-
divides signals at its input 122 by the value of modulus M
it receiVes at its input 124 from the modulus M counter 110.
This divided output T'elk appears at the modulus M divider
output 126. There it is fed both to a time delay 130 and to
the strobe input 162 of the speed count register 160. After
the time delay 130 the count appears at Lhe first input.142
of speed counter 140, whose second input 144 connects to
channel II. A third input 146 connects to the preset memory
150. Speed counter 140 produces at its output 148 a count
representative of the number of position pulses received at
counter input 144 during the time counter input 142 is
activate, i.e. during the T' time. Since the output
from the speed output counter 30 is only significant at the
endof the T'clk period, the speed count register 160 is
strobed via the trailing edge of the T'clk signal to accept
the final count from the output 148 of speed counter 140.
Once speed counter 140 senses the conclusion of the T'clk
signal, it activates its third input 146 to preset the
counter 140 to the value dictated by preset N memory 150.
The preset number N is the'maximum number of position pulses
that may occur during a cycle. To prevent speed counter 140
from transferring the preset number N to the speed count
register 160 on the conclusion of every T'clk signal, the
time delay 130 provides a slight time lag, whereby when the 11 488 564
16,93 6/76
speed count registers strobe 162 is activated, the speed
counter output 148 is at or near its maximum value during a
T'clk interval. The speed count register 160 produces the
stored total speed count Z at its output 164.
A comparator 40 couples the Y output from output terminal
24 of position counter 20 to its first input 42, and the Z
output of the speed output counter 30 to its second input
44. The comparator 40 logic is such that when the Y count
output exceeds the Z count output the comparator activates
its output 46.
The comparator output 46 feeds to the first input 172
of an AND gate 170. The AND gate second input 174 connects
to the output 182 of a maximum dwell comparator 180. Maximum
dwell comparator 180 has its first input 184 connected to
the output 24 of position counter 20, and its second input
186 connected to the output of an N/4 memory 190. At the
highest desired engine RPM the system should be automatically
set to a 75% dwell time. Since N is the total number of
pulses per engine cycle, N/4 pulses should be encountered
prior to initiating maximum dwell time. Thus, gate 170
produces an activated output 176 over the active RPM range,
i.e. 300-5000 rpm, when Y is greater than Z, and when Y is
greater than N/4.
The output 176 from gate 170 connects to the set input
52 of flip-flop 50. As discussed with respect to Fig. 2,
once input 52 is activated the flip-flop output 56 produces
a trigger signal, which is amplified by drive circuitry 200
and applied to the control terminal 62 of a switch
Thereafter the switch 60 passes current from the battery 68
through the coil 66 and current sense resistor 72 to ground
I)488.564
16,93 6 176
potential 74. When the reset input 54 of flip-flop
receives a sync, or ignition, pulse, the trigger signal at
output 56 ceases, whereby the switch 60 opens thus generat-
ing the ignition spark via coil 66.
A current limit amplifier 80 monitors the voltage
created by coil 66 current through current sense resistor
72. Current limit amp 80 produces at its output 82 a pulse
whose width Tli m is representative of the length of time a
predetermined current passes through ignition coil 66. The
Tlim signal is applied to one input 212 of an AND gate 210,
whose second input 214 connects to channel II. The gate 210
produces at its output 216 a signal representative of the
synchronous occurrence of the Tlim signal and the input
position pulses. Thus as the current limit time increases,
as' it will for increased battery 68 voltage or decreased
coil resistance 66, a greater number of position pulses
appears at the gate output 216.
The output of gate 216 is connected to the count down
input 112 of the modulus M counter 110. Connected to the up
count terminal 114 of modulus M counter 110 are the sync
pulses on channel I. During one cycle the modulus M counter
110 up counts via a received sync pulse, and down counts via
the number of pulses from gate 210. In stable operation
there is one T im pulse per cycle, whereby the modulus M
output remains constant. However, should the number of
feedback pulses from gate 210 change for a given cycle, the
modulus number M from the counter 110 will vary, whereby the
modulus M divider 120 will create a correspondingly changed
TI signal. Referring to Fig. id, as the number of feed- clk back pulses from gate 210 increases per cycle, indicating
13 488564
16.93 676
increased battery voltage or decreased coil resistance, the
modulus M is decremented whereby the divider 120 produces a
shorter T' clk signal at its output 126. As Fig. Id illus-
trates, this causes the system to initiate dwell at a later
point in the cycle, whereby the desired ignition energy
level is maintained. In general, the feedback provided by
gate 210 and modulus M counter 110 is sufficient to cause desired the system to always return to a state providing the
ignition energy.
In summary, an ignition system has been described which variations maintains a given ignition energy level despite effects on in engine acceleration, or temperature, or aging
ignition components. Moreover, the entire system may be
implemented by digital circuitry, thereby avoiding a large
number of age and temperature sensitive components.
488.5 64
Claims (1)
16.936 f76
The claims defining the invention are as follows:-
1. A system for controlling the ignition dwell
of an internal combustion engine comorising an ignition pulse generating means, coupled
to the engine, and-producing ignition pulses suitable
for ignition firing, a position pulse generating means coupled to
the engine and producing position pulses representative
of engine angular position, a first circuit means for processing the
position pulses and producing an output signal
representative of engine position. the first means
resettable to an initial state prior to the occurrence
of the first position pulse following a trigger pulse, a second circuit means processing the position
pulses and producing an output representative of engine
RPI'I, a comparator means for comparing the first
circuit means output with the second circuit means
output and producing a trigger signal in response to a
predetermined relationship between the two outputs, switch means initiating dxwell time in response
to a trigger signal from the comparator means and firing
the ignition in response to an ignition pulse, means for generating a feedback signal
representative of the ignition energy level and, control means for predeterminedly altering the
occurrence of the trigger signal in response to the
.feedback signal, whereby the dwell time is adjusted to maintain
488.564
16,936/76
a, substantially constant ignition energy level. 2. The system of' claim 1 wherein each structural element is imrlemented using di-ital circuitry. 3. The system of claim 1 or claim 2 wherein the first circuit means includes an angle counter for counting the number of position pulses generated between ignition pulses. 4j. The system as claimed in any one of' the preceding claims wherein the second circuit means includes clock means for generating a clock signal ~r~od~tczirn~time period, havng and speed counter means for counting the number of' position pulses generated during each clock signal period. The system of' claim 4~ wherein the second circuit means further comprises speed register means, responsive to the clock signal, for registering the count of' the speed counter means immediately prior to the conclusion of the cnlock signal, and applying the registered count to the comparator means. 6. The system of' claim 5 wherein the second circuit means further comrises means for presetting the speed counter to a predetermined count prior to its reception of rosition pulses generated during each clock signal period, and wherein the speed counter fLurther cocori- ses means for decrementing the predetermined count by the number of received position pulses during each clock-
16 488,5 64
16.93 6 76
signal period.
7. The system as claimed in any one of the
preceding claims wherein the comparator means produces a trigger pulse when the output of the first circuit
means is greater than or equal to the output of the
second circuit means.
8. The system as claimed in any one of the coil preceding claims in combination with an ignition wherein the feedback signal generating means includes
means for generating a circuit limit pulse whose width is is representative of the time during which the coil
conducting a predetermined current and, gating means for generating a pulse train the representative of the synchronous occurrence of current limit pulse and the position pulses.
9. The system of claim 8 wherein the control
means comprises a modulus N register for generating a modulus
number M, the register incrementing the number for each
ignition pulse and decrementing its count for each pulse in the pulse train, and means for varying the clock signal period
responsive to the modulus number M. The system of claim 9 wherein the control means
further comprises an oscillator producing a signal of constant
frequency fo, and a modulus P programmable divider, responsive
to the modulus register, for dividing the frequency fo
by the modulus number H and applying the output clock 17 488.5 64
16,93676
signal to-the Specd counter means. 11. The system of claim 1 further comnris ig means for fixing.- a maximum allowable dwell time. 12. The systemi for controlling the ignition dwell of an internal conbustion engine substantially as hereinbefore described with reference to the accompanying- drawings.
DATED: 22nd July, 1976. 0D MOTOROLA, IN~C. 4(9 4 By their P--atent attorneys: PHII.LIF"P OR-'IC'I--'DE ';FdZATIC
488,5 64
16,93 6/76
POSITION PULSES CHAN.2
488,5 64
16.936/76
488.5 6 4
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| USUS633,737 | 1975-11-02 | ||
| US05/633,737 US4018202A (en) | 1975-11-20 | 1975-11-20 | High energy adaptive ignition via digital control |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| AU488564B2 true AU488564B2 (en) | 1977-12-01 |
| AU1693676A AU1693676A (en) | 1977-12-01 |
Family
ID=
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| ZA764640B (en) | High energy adaptive ignition via digital control | |
| AU498680B2 (en) | Adaptive equaliser | |
| AU498679B2 (en) | Adaptive equalizer | |
| AU508160B2 (en) | Cyclization | |
| AU507030B2 (en) | Servomotor | |
| ZA762796B (en) | High energy adaptive ignition system | |
| AU1220476A (en) | Treating solid fuels | |
| CA1021964A (en) | Mechanical actuator | |
| AU504325B2 (en) | Telephone-line values control | |
| CA1031585A (en) | Penstocks | |
| AU501023B2 (en) | Ignition circuit | |
| AU503732B2 (en) | Marine turbine control | |
| AU503865B2 (en) | Lactones | |
| AU500506B2 (en) | Ignition circuit | |
| AU508663B2 (en) | Spark advanced control | |
| AU500737B2 (en) | Treating solid fuels | |
| CA1027016A (en) | Variably biased control mechanism | |
| AU505460B2 (en) | 3-(2-iminobenzyl)-4-hydroxy-2-pyridones | |
| AU501554B2 (en) | Solar still | |
| AU508142B2 (en) | Document feeder | |
| AU508411B2 (en) | Vacuum ignition control | |
| CA1018143A (en) | Damper arrangement | |
| AU483392B2 (en) | High energy adaptive ignition system | |
| AU500420B2 (en) | 6-aminomethylated 3-oxygenated chloest-5-enes | |
| SU586402A1 (en) | Digital ohmmeter |