U.S. patent number 3,566,188 [Application Number 04/772,127] was granted by the patent office on 1971-02-23 for triggered ignition system.
This patent grant is currently assigned to Brunswick Corporation, Chicago, IL. Invention is credited to Floyd M. Minks.
United States Patent |
3,566,188 |
|
February 23, 1971 |
**Please see images for:
( Certificate of Correction ) ** |
TRIGGERED IGNITION SYSTEM
Abstract
This disclosure relates to an alternator-driven capacitor system
for a two-cylinder engine. A main capacitor is connected across the
output of the alternator. Separate discharge circuits for each of
the spark plugs are connected in parallel to the capacitor and each
includes a silicon-controlled rectifier and a pulse transformer. A
trigger capacitor in series with a resistor is connected across the
main capacitor. Paralleled trigger circuits are connected to the
trigger capacitor and each includes a pulse transformer in series
with a silicon-controlled rectifier. The pulse transformers are
connected to fire a corresponding main-controlled rectifier. The
controlled rectifiers of the trigger circuits are fired from a
separate pulse generator driven in synchronism with the engine.
Inventors: |
Floyd M. Minks (Kissimmee,
FL) |
Assignee: |
Brunswick Corporation, Chicago,
IL (N/A)
|
Family
ID: |
25094001 |
Appl.
No.: |
04/772,127 |
Filed: |
October 31, 1968 |
Current U.S.
Class: |
315/209T;
123/599; 315/219; 315/224; 315/241R; 315/243; 315/218; 315/223;
315/240; 315/242 |
Current CPC
Class: |
F02P
7/035 (20130101) |
Current International
Class: |
F02P
7/00 (20060101); F02P 7/03 (20060101); H05b
037/02 () |
Field of
Search: |
;315/209(CD),209(T),209(SCR),209(M),218,219,223,224,240,241,242,243
;123/148,148(E),148(AC) |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: John W. Huckert
Assistant Examiner: R. F. Polissack
Attorney, Agent or Firm: Andrus, Sceales & Sawall
Claims
1. A capacitor discharge ignition system, a first main firing
capacitor, a first main controlled rectifier connected in series
with the firing capacitor and defining a first discharge circuit to
discharge said main firing capacitor, a second discharge circuit
connected in parallel with the first discharge circuit to the main
firing capacitor, said second discharge circuit to the main firing
capacitor, said second discharge including a second main controlled
rectifier means, a trigger capacitor, an isolating resistor
connected in series with said trigger capacitor and in parallel
with said main firing capacitor, an alternator connected to
simultaneously charge said main firing capacitor and said trigger
capacitor, a flywheel connected to said alternator, a pulse-forming
circuit including a first pulse transformer in series with a
triggering controlled rectifier connected across said trigger
capacitor, said pulse transformer having a secondary winding
connected to said first main controlled rectifier, said
pulse-forming circuit including a second pulse transformer in
series with a second triggering control rectifier, said second
pulsing circuits connected to actuate the second main controlled
rectifier, a pulse-generating means including means rotating in
synchronism with said flywheel and including coil means for
producing time-spaced pulses in accordance with each revolution of
said flywheel, each pulse being an alternating current signal and
having a sharp leading edge, means connecting said coil means to
both said triggering controlled rectifier to periodically discharge
said trigger capacitor, and said pulse-generating means
establishing time-spaced alternating current signals and connected
to both of said triggering control rectifiers for cyclically
actuating said first and second triggering controlled
2. The ignition system of claim 1 having a voltage-sensitive means
connected directly in parallel with said capacitor in series with
the gated control switch and polarized to bypass reverse polarity
voltages
3. The ignition system of claim 1 wherein said voltage sensitive
means is a Zener diode means.
Description
This invention relates to a triggered ignition system and
particularly to an alternator driven capacitor discharge ignition
system for an internal combustion engine and the like.
Capacitor discharge ignition systems have recently been suggested
and developed for internal combustion engines and the like. A
highly satisfactory alternator driven capacitor discharge ignition
system is disclosed in applicant's copending application entitled
"Alternator Driven Capacitor Power System" which was filed Jun. 13,
1968 with Ser. No. 736,789 wherein a pair of windings are provided
for charging of a main igniting capacitor during one-half cycle of
the alternator voltage and for triggering of a controlled rectifier
to discharge such main capacitor during the alternate half-cycle.
As disclosed therein, a distributor is employed to sequentially
connect the main firing capacitor to the several spark plugs.
Alternatively, a plurality of parallel firing circuits may be
interconnected to the main firing capacitor with separate triggered
switches for sequentially discharging the capacitor to the several
spark plugs or other firing means. For example, in small internal
combustion engines for snowmobiles and the like it may be desirable
to provide separate firing circuits for each of the cylinders.
In triggered ignition systems and the like, the triggering pulse
must have sufficient power to positively fire the controlled
rectifier or other triggering means. Further, in an alternator
driven system where the power is derived from the one alternator,
it is important to maintain proper timing as well as to produce the
desired triggering power.
The present invention is particularly directed to an improved and
reliable capacitor discharge ignition system which has been
particularly applied to an internal combustion engine for a
snowmobile. In accordance with the present invention, a main firing
capacitor is connected in a charging circuit to a suitable power
source and in a discharge circuit through a main triggered switch
means. The power source is preferably an alternator coupled to and
driven by the internal combustion engine. A triggered circuit is
provided including a capacitive storage means such as a control
capacitor connected in circuit to the main firing capacitor and the
power source through a circuit isolating control means. A pulsing
circuit for the main switch means is connected across the control
capacitive means of the triggered circuit in series with a suitable
control switch means which is actuated in synchronism with the
internal combustion engine. The control switch means is preferably
a second triggered switch means such as a controlled rectifier or
the like which will rapidly discharge the energy of the capacitive
storage means. A separate pulse generator is coupled to the engine
and connected to the control switch means. The control switch means
responds to the leading edge of the engine generated pulse signal
and provides rapid discharge of the control capacitor to fire the
main triggered switch means and thereby provide rapid discharge of
the main firing capacitor to provide a highly satisfactory ignition
pulse to the engine. After the discharge pulse, the recharging of
the main firing capacitor may be immediately begun to store
sufficient energy for firing of the engine on the next cycle. The
control capacitor is connected through the isolating means which
reduces the charging current below the holding level of the control
switch means such that the control switch means is only responsive
to the engine synchronized control pulse. Consequently the circuit
of the control capacitor can be connected directly to the main
firing capacitor.
As applied to an alternator driven capacitor system for a
snowmobile, the main capacitor was connected across a dual winding
circuit generally in accordance with applicant's copending
application. A separate discharge circuit for each of the spark
plugs included a main firing control rectifier and a pulse
transformer. The discharge circuits were connected in parallel
across the main firing capacitor and each included a separate pulse
forming network for firing of the control rectifier. Each pulse
forming network included a pulse transformer in series with a
second control rectifier connected across a common trigger
capacitor. The second control rectifier was fired from a separate
pulse generator in synchronism with the engine. The triggered
capacitor was connected in series with an isolating resistor across
the main firing capacitor. The resistance of the isolating resistor
was selected with a sufficiently low resistance so that the trigger
capacitor would charge to a sufficient level to fire the second
control rectifier during the period between firing of the main
firing rectifier but of a sufficiently high value to prevent
establishment of the holding current through the resistor and the
triggered control rectifier, which were connected in parallel to
the triggered capacitor.
A Zener diode was connected in parallel with the main firing
capacitor to limit the level to which it is charged and to bypass
reflected voltages of the discharge circuit through the Zener diode
and a conducting silicon controlled rectifier to dissipate the
energy.
The drawing furnished herewith illustrates the best mode presently
contemplated by the inventor for carrying out the subject matter of
this invention and clearly discloses the above advantages and
features as well as others which will be readily understood by
those skilled in the art from the following description.
In the drawing:
FIG. 1 is a schematic circuit diagram of a capacitor discharge
ignition system constructed in accordance with the present
invention;
FIG. 2 is an illustration of novel pulse generating means for
controlling the ignition system; and
FIG. 3 is a graphical illustration of the output of the generating
means shown in FIG. 2.
Referring to the drawing, the present invention is shown applied to
an internal combustion engine 1 having a pair of spark plugs 2 and
3. For example, the present invention has been applied to a
two-cycle two-cylinder engine forming a part of a snowmobile. An
alternator 4 is coupled to and driven in synchronism with the
engine 1. The output of the alternator 4 is connected to charge a
main firing capacitor 5 which is interconnected through separate
paralleled discharge circuits 6 and 7 to the spark plugs 2 and
3.
The output circuit as previously noted for the respective spark
plugs 2 and 3 is essentially identical and consequently the
discharge circuit 6 for spark plug 2 is described in detail with
the corresponding elements of the circuit 7 for spark plug 3
identified by corresponding primed numbers.
The circuit 6 includes a silicon-controlled rectifier 8 in series
with a pulse transformer 9 connected across the capacitor 5 to
provide a firing energy to the spark plug 2. A pulse-forming
circuit or network 10 is connected to fire the rectifier 8 and
includes a trigger coil actuated by alternator 4 to provide
sequential and alternate firing of the controlled rectifiers 8 and
8' with a corresponding sequential and alternate discharge of the
capacitor through the pulse transformers 9 and 9'. In the operation
of the circuit, the main firing capacitor is charged during one or
more positive half-cycles of the output of the alternator 4. The
trigger coils 11 or 11' are pulsed to turn on the related SCR's 8
or 8' for discharging of the main capacitor preferably during the
negative half-cycle.
In the illustrated embodiment of the invention, the alternator 4 is
generally constructed in accordance with applicant's previously
referred to copending application and includes a first winding 12
having a relatively low number of turns and a second winding 13
having a relatively high number of turns. The windings 12 and 13
are connected to provide a common charging of the main firing
capacitor 5 with a controlled characteristic as more fully
disclosed in applicant's copending application.
In the illustrated embodiment of the invention one side of the
windings are connected to ground line 14. The opposite side of the
winding 12 is connected in series with a pair of diodes 15 and 16
to the positive side of the capacitor 5, the opposite side of which
is connected to the common ground line 14. The winding 13 is
connected at one end to ground line 14. The opposite end is
connected in series with a diode 17 to the positive side of the
capacitor 5. A clipping diode 18 is connected directly across the
winding to bypass or clip the negative half cycle.
In the illustrated embodiment of the invention, transient
protective capacitors 19 and 20 are shown connected directly across
the respective windings 12 and 13 to bypass high transient voltage
signals. Further, a Zener diode 21 is connected directly across the
main firing capacitor 5 to control the maximum voltage to which it
is charged by alternator 4 and also functions as more fully
described hereinafter to bypass reflected voltages from the output
circuits 6 and 7 and dissipate the energy of such reflected
voltages in the Zener diode 21 and one of the controlled rectifiers
8 or 8'.
The pulse transformer of discharge circuit 6 includes a primary
winding 22 connected in series with the anode to cathode circuit of
the controlled rectifier 8 directed across the capacitor 5 with the
one side of the primary winding grounded. The secondary 23 of the
pulse transformer 9 is connected directly to the spark plug 2. A
protective diode 24 may be connected across the controlled
rectifier 8.
The gate of the controlled rectifier 8 is connected in the trigger
circuit 10 which is actuated by the trigger coil 11 and constructed
in accordance with the present invention, as follows.
A trigger capacitor 25 is connected in series with an isolating
impedance element 26 directly across the paralleled output of the
alternator windings 12 and 13 and across the main firing capacitor
5. The illustrated impedance 26 is shown as a resistor connected
between the positive side of the main firing capacitor 5 and the
positive side of the trigger capacitor 25. The trigger capacitor 25
is connected to be charged simultaneously with the main firing
capacitor 5 through the resistor 26. As more fully developed
hereinafter, the resistor 26 serves to permit proper charging of
the capacitor 25 for subsequent firing of the controlled rectifier
8 while essentially isolating the capacitor 25 from the charging
circuit during the discharging of the capacitor 25.
The primary winding 27 of a trigger pulse transformer 28 is
connected in series with a trigger-controlled rectifier 29 directly
across the trigger capacitor 25. A diode 29a is connected across
the trigger capacitor 25 to prevent the inductance of primary 27
from charging the capacitor in a negative direction. Diode 29a may
be a Zener-type diode, if desired, to reduce the required rating of
the control rectifiers 29 and 29'. The secondary winding 30 of the
transformer 28 is connected across the gate to cathode circuit of
the main control rectifier 8. A parallel resistor 31 may be also
connected across the gate to cathode circuit to reduce the
sensitivity of rectifier 8 to spurious input signals.
In operation when the trigger rectifier 29 is fired, it will
rapidly discharge the capacitor 25 through the primary 27 of the
pulse transformer 28 and provide a pulse signal to the gate of the
main rectifier 8 to turn it on and rapidly discharge the main
firing capacitor 5. In the illustrated embodiment of the invention,
the trigger signal coil 11 is connected in series with a resistor
32 across the gate to cathode circuit of the trigger control
rectifier 29. A magnet 33 is secured to the engine flywheel 34 and
thus rotates in synchronism with the alternator 4 and is
sequentially coupled to the coil 11 by the rotation of the flywheel
and alternator 4 to provide sequential pulsing of the gate circuit
of the rectifier 29 and a corresponding sequential discharging of
the trigger capacitor 25.
In the illustrated embodiment of the invention, a transient
protective capacitor 35 and a protective diode 36 are shown
connected in parallel across the gate to cathode circuit of the
control rectifier 29.
In the operation of the illustrated embodiment of the invention,
the alternator 4 provides an output which charges the main firing
capacitor 5 and the trigger capacitor 25. The charging of the
trigger capacitor 25 is through the resistor 26. This resistor is
particularly selected to establish, with the trigger capacitor 25,
a time constant which allows charging of the capacitor 25 to a
sufficient level for firing of the main control rectifier 8 within
the charging period of the capacitor 5. However, it is further
selected to have a sufficiently large value to effectively isolate
the circuit of the transformer 28 and the controlled rectifier 29.
Thus, when the magnet 33 and 33' actuates the trigger coil 11 to
fire the controlled rectifier 29, a circuit is established to
discharge the firing capacitor. However, the circuit for the
controlled rectifier 29 through the pulse transformer is now
connected in series with the resistor 26 directly across the
alternator 4, which provides a holding current path through the
controlled rectifier 29. If the output of the alternator 4 should
go positive and initiate charging of the main firing capacitor 5
prior to resetting of the controlled rectifier 29, the rectifier 29
would remain conducting and bypass the capacitor 25 if the current
in this path were at or above the holding current level. This may
be particularly true where the firing of the engine is advanced to
the latter portion of the negative cycle of the alternator output.
In accordance with the present invention, however, the resistance
of resistor 26 maintains the current from the alternator 4 through
the resistor 26, the transformer 28 and the controlled rectifier 29
below the holding current level of the rectifier 29. Consequently,
the conduction of rectifier 29 is completely controlled by the
signal applied to the gate to cathode circuit by coil 11.
Consequently, the charging of the main firing capacitor 5 can be
initiated immediately after the discharge of the capacitor and
independently of the conductive condition of the controlled
rectifier 29 which are essentially responsive solely to the input
pulse signal at the related gate. This allows a maximum charging
period for the main firing capacitor 5 under all operating
conditions.
The holding current level of the usual controlled rectifiers 29 and
29' is dependent on the gate to cathode impedance. The resistor 32
provides a resistance in the gate to cathode circuit and
consequently the holding current level depends on the parameters of
the rectifiers and the resistance of resistors 32 and 32' to permit
varying of the holding current level.
The capacitors 5 and 25 are charged during the positive half-cycle
of the output of the alternator 4 in accordance with the plurality
of the diodes connected between the windings 12 and 13 and the
capacitors. The trigger coils 11 and 11' are mounted adjacent the
flywheel 34 and alternately pulsed by the associated magnets 33 and
33' to provide alternate firing of the controlled rectifiers 29 and
29' to thereby sequentially discharge the capacitor 25 through the
alternate firing pulse transformers 28 and 28'.
This in turn results in the alternate triggering of the main
controlled rectifiers 8 and 8' to alternately fire the spark plugs
2 and 3.
Although any suitable means can be employed for triggering of
controlled rectifiers 29, a novel and highly satisfactory means is
shown in FIGS. 1 and 2. The trigger coils 11 and 11' are wound as a
single center tapped winding on a rectangular core 37 having an air
gap 38. The center tap 39 of the winding is connected to the ground
line 14 and the opposite ends of the winding are connected in
series with the resistors 32 and 32' to the respective gates of the
rectifiers 29 and 29'. The core 37 is mounted adjacent the
periphery of the flywheel 34 as diagrammatically shown in FIG. 2.
The pair of magnets 33 and 33' are located on diagrammatically
opposite sides of the flywheel 34 and are thus sequentially and
cyclically aligned with the air gap 38 of core 37. The magnets 33
and 33' are oppositely polarized with respect to the core 37 to
establish oppositely directed magnetic flux through the core. As a
result, the magnets induce oppositely phased alternating voltage
pulses across the winding generally as shown in FIG. 3.
In FIGS. 1 and 2, the magnet 33 is aligned with the winding of
coils 11 and 11' and produces a pulse signal as shown at 40 in FIG.
3. The pulse signal goes positive and then negative with respect to
the dotted end of winding, as shown in FIG. 1 and 2. The positive
portion of the pulse drives the rectifier 29 into conduction and
rapidly discharges the capacitor 25. The following negative portion
biases the alternate rectifier 29' of the discharge circuit 7 to
conduct. However, the capacitor 25 has discharged its energy and
essentially no current or power is supplied to the transformer
28'.
One hundred and eighty degrees later, the opposite magnet 33' moves
past the core 37. The opposite polarization of magnet 33' generates
an alternating pulse signal which goes negative and then positive
with respect to the previously assumed polarity designation, as
shown at 41 in FIG. 3.
The negative portion of the signal turns on the rectifier 29'. The
capacitor 25' is sufficiently charged and thus discharges through
the circuit of the pulse transformer 28' and rectifier 29'. The
pulse transformer 28' applied the pulse to the main rectifier 8'
and discharges capacitor 5 through the transformer 9'.
The positive portion of pulse 41 will turn on the rectifier 29.
However, the energy in capacitor 25 has been discharged and
consequently circuit 6 remains off.
The pulse generating thus provides a simple and inexpensive means
for reliable sequencing a pair of controlled rectifiers or the
like.
If the alternators output frequency is sufficiently higher than the
engine-firing frequency, the phasing of the alternator may be
random or continually varying compared to the trigger pulse, even
through a somewhat smaller alternator can be used if the phasing is
controlled. If the gate of the main rectifiers 8 or 8' is
energized, either to create an output pulse or continues to be
energized thereafter, during the positive portion of the output
waveform of alternator 4 that positive cycle may be shorted out and
of no effect in charging capacitor 5.
Since it is not possible to arbitrarily reduce the width of pulses
40 and 41, a purpose of the invention is to isolate the controlled
rectifiers 8 and 8' from all except the leading edge of these
pulses to allow greater time for the recharging of capacitor 5.
This allows greater output under random phase conditions, or under
synchronized phase conditions allows a greater phase variation
between alternator 4 and alternator 34 including coils 11 and 11'
and magnets 33 and 33'. This phase variation can be necessitated by
timing advance when only means to rotate alternator 34 may be
available, or due to manufacturing tolerances in the components
involved.
Although the coils 11 and 11' are shown in the preferred novel
construction of a single center tapped winding wound on a single
core, any other suitable construction may be employed. For example,
separate coils may be employed. Further, the magnets may be
connected to a completely separate element driven in synchronism
with the engine through any suitable means to sequentially couple
the magnets to the coil means.
The present invention has been found to provide a highly reliable
and long life ignition system which is particularly adapted to
two-cylinder engines such as employed in a snowmobile or the
like.
* * * * *