U.S. patent number 3,661,126 [Application Number 04/856,758] was granted by the patent office on 1972-05-09 for fuel injection systems.
This patent grant is currently assigned to Brico Engineering Limited. Invention is credited to Albert E. Baxendale.
United States Patent |
3,661,126 |
Baxendale |
May 9, 1972 |
FUEL INJECTION SYSTEMS
Abstract
The invention relates to a fuel injection system wherein
enrichment of the fuel is effected, when the engine is conditioned
for acceleration, by means applying to the electromagnetic fuel
injection valves, further energizing pulses in addition to those
which are applied to the injectors during normal operation of the
engine.
Inventors: |
Baxendale; Albert E. (Coventry,
EN) |
Assignee: |
Brico Engineering Limited
(Coventry, EN)
|
Family
ID: |
10429030 |
Appl.
No.: |
04/856,758 |
Filed: |
September 10, 1969 |
Foreign Application Priority Data
|
|
|
|
|
Sep 12, 1968 [GB] |
|
|
43/503/68 |
|
Current U.S.
Class: |
123/492;
123/494 |
Current CPC
Class: |
F02D
41/102 (20130101) |
Current International
Class: |
F02D
41/10 (20060101); F02b 003/10 (); F02b
033/00 () |
Field of
Search: |
;123/32,119,140.3
;133/32 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Newman; Mark M.
Assistant Examiner: Cox; Ronald B.
Claims
I claim:
1. A fuel injection system for an internal combustion engine which
includes a plurality of electromagnetically operated fuel injection
valves, at least one pulse generator circuit producing electrical
pulses for energizing said valves, so that each valve is opened for
a period depending on the duration of the pulse by which it is
energized, to pass fuel to the engine, said pulse generator circuit
including a timing circuit for controlling the duration of said
pulses, means to feed at least one variable electrical potential,
which varies as a function of at least one parameter of engine
operation, to the pulse generator circuit to control said pulse
duration, trigger means to initiate said pulses, said trigger means
operating at a frequency depending on the rotational speed of the
engine, and further pulse-initiating means operable independently
of said trigger means to initiate further pulses when acceleration
of the engine is required, said further pulses being applied to the
fuel injection valves in addition to those pulses initiated by said
trigger means, whereby additional fuel is delivered through said
fuel-injection valves to enhance acceleration, said further pulse
initiating means including a plurality of auxiliary pulse generator
circuits for producing a plurality of successive further pulses
each of which simultaneously energizes all the valves, the number
of said generator circuits corresponding to the maximum number of
said successive further pulses, the system including a manifold
absolute pressure transducer which produces an output varying in
dependence upon changes in pressure in the induction manifold, the
output being fed simultaneously to said auxiliary pulse generator
circuits, the auxiliary pulse generator circuits being arranged to
be triggered by different levels of said output relative to a
quiescent level determined by the value of said output
corresponding to the manifold pressure before the engine is
conditioned to accelerate, said system further including a pair of
main pulse generator circuits, each including an output amplifier
connected to a group of fuel injection valves, the auxiliary pulse
generator circuits being connected in parallel between said
transducer and both of said output amplifiers.
Description
This invention relates to fuel injection systems for internal
combustion engines.
More particularly, the invention relates to a fuel injection system
for an internal combustion engine which includes a plurality of
electromagnetically operated fuel injection valves, a pulse
generator circuit producing electrical pulses for energizing said
valves, so that each valve is opened for a period depending on the
duration of the pulse by which it is energized, to pass fuel to the
engine, said pulse generator circuit including a timing circuit for
controlling the duration of said pulses, means to feed at least one
variable electrical potential, which varies as a function of at
least one parameter of engine operation, to the pulse generator
circuit to control said pulse duration, and trigger means to
initiate said pulses, said trigger means operating at a frequency
depending on the rotational speed of the engine. A system of this
type is described in U.S. Pat. No. 3272187.
In the said British Patent, it was proposed to provide fuel
enrichment during acceleration, so as to enhance acceleration, by
extending the duration of the pulses energizing the fuel -
injection valves.
It is an object of the present invention to provide a fuel
injection system incorporating improved means for providing fuel
enrichment to enhance acceleration.
According to the present invention, the system includes means to
initiate further pulses when acceleration of the engine is
required, in addition to those pulses initiated by said trigger
means, whereby additional fuel is delivered through said
fuel-injection valves to enhance acceleration.
The said further pulse initiating means may be actuated by changes
in a parameter which occur when the engine accelerates or is
conditioned to accelerate, for example, changes in the position of
the throttle, or resultant changes in pressure in the induction
manifold of the engine. Said initiating means may be arranged to
energize all the fuel-injection valves simultaneously, either once
or several times upon initiation of, or during, acceleration, and
in the latter event the pulse spacing, or time delay between
successive energizations may vary in dependance upon the rate of
acceleration required.
The or each main pulse generator supplying the pulses to the fuel
injection valves during normal running of the engine i.e. when not
accelerating, may be activated by said initiating means to produce
said further pulses. Alternatively, said initiating means may
comprise, or be connected to, one or more auxilliary pulse
generators for producing said further pulses.
Said further pulse initiating means may be employed in the system
either alone or in combination with other acceleration enrichment
means, such as the means described in the aforementioned United
States Patent.
A number of embodiments of the invention will now be described by
way of example, with reference to the accompanying drawings, in
which:
FIG. 1 is a block circuit diagram of one embodiment,
FIG. 2 is a detail view of one alternative arrangement of part of
FIG. 1,
FIG. 3 is a detail view of another alternative arrangement of FIG.
1,
FIG. 4 is a diagram illustrating the operation of an embodiment of
fuel injection system in accordance with this embodiment of the
invention,
FIG. 5 is a block circuit diagram of a second embodiment, and
FIG. 6 is a circuit diagram of the auxilliary pulse generators and
associated circuitry.
Referring to FIG. 1, the fuel injection system shown is intended
for a six-cylinder engine and includes six fuel injection valves 11
arranged in two groups of three. The valves are screwed into
housings in the engine induction manifold, just upstream of the
inlet valve of the corresponding cylinder. Fuel is supplied at a
controlled pressure to each valve 11, for example as described in
U.S. Pat. No. 3,240,191, and the fuel injection valves are
electromagnetically operated and may be as described in U.S. Pat.
No. 3,247,833.
Each group of fuel injection valves 11 is electrically connected to
a pulse generator 12, the circuit of which produces a current pulse
to energize the group of valves, thereby to inject fuel into the
induction manifold. The main pulses are initiated by a trigger
device 13, which is in effect a switch which is operated once per
engine cycle for each group of cylinders. It will be understood
that a fuel injection system in accordance with the invention may
be designed for engines having any practical number of cylinders,
and moreover each group of valves connected to a pulse generator
may include any convenient number of valves, from one upwards.
Each pulse generator 12 includes a timing circuit controlling the
duration of the main pulses, and this duration is determined in
accordance with the values of two potentials V.sub.1 and V.sub.2,
which in turn depend on the values of certain engine operating
parameters. In this case, the potential V.sub.1 depends on the
engine manifold pressure which is sensed by a pressure transducer
forming part of a manifold pressure control circuit 14 and
connected to the induction manifold between the throttle and the
inlet valves of the engine, and also depends upon the rotational
speed of the engine which is sensed from the trigger device 13 by
means of an engine speed discriminator 15. The potential V.sub.2
depends on the engine water temperature and the ambient air
temperature, which temperatures are sensed, respectively, by a
water temperature transducer connected into the water cooling
system of the engine and by an air temperature transducer, both of
which form part of a start and warm up control circuit 16. These
various transducers may incorporate variable resistance elements,
the resistances of which will be varied in accordance with the
value of the respective operating parameters, and the resistance
elements may be incorporated in voltage dividers forming part of
associated circuits, namely the inlet manifold pressure control
circuit 14, the engine speed discriminator circuit 15, and the
start and warm up control circuit 16. Since the present invention
is not concerned with the means by which the main pulses or the
potentials V.sub.1 V.sub.2 are produced, the pulse generators 12,
the circuits 14, 15 16 will not be described or illustrated in
detail. It is to be understood, however, that each pulse generator
12, may, for example take the form of, and operate in the manner
of, the pulse generator 8 disclosed in the aforementioned U.S. Pat.
No. 3272187, and the said circuits and transducers may also take
the forms disclosed in this latter Patent, and for further details
of the construction and operation of these components, reference
should be made to this Patent.
The fuel injection system also includes a device 17, which responds
to an increase in induction manifold pressure on opening of the
throttle, and which activates the pulse generators 12 to produce
further pulses, in addition to the main pulses initiated by the
trigger device 13, when the increase in manifold pressure on
opening of the throttle valve exceeds certain values. This device
17 activates the pulse generators 12 simultaneously, so that said
further pulses are produced simultaneously at all the fuel
injectors 11, and therefore, additional fuel is delivered into the
induction manifold.
One form of the device 17 for sensing when acceleration is called
for is shown in FIG. 2. A housing 21 is secured to the exterior of
the induction manifold wall 22, downstream of the engine throttle,
and is divided by a diaphragm 23 into two spaces 24, 25. The space
24 communicates with the interior of the manifold through a large
hole 26 and is virtually at the same pressure as the interior while
the space 25 communicates with space 24 through a small hole 27.
The diaphragm carries one switch contact 28, and another contact 29
is carried by, but insulated from, the housing 21. A coil spring 30
loads the diaphragm, and also serves to connect switch contact 28
to one terminal of the switch, which is insulated from the terminal
connected to the other contact 29.
When the manifold pressure increases, the pressure in space 24
increases immediately, but that in space 25 lags due to the small
hole 27. If the rate of change of manifold pressure exceeds a
certain value, the contacts 28, 29 make, and, since they are
connected to the pulse generators 12, for example, connected via a
diode to the input terminal of each pulse generator 12, in parallel
with the trigger device 13, initiate a pulse, the duration of which
depends inter alia on potentials V.sub.1, V.sub.2. This additional
pulse opens the fuel injectors 11 simultaneously to deliver fuel
into the induction manifold.
Another form of device for sensing when acceleration is called for
is shown in FIG. 3, which, in this case responds to rate of change
of position of part of the linkage 40 between the accelerator pedal
and the engine throttle. This device includes a cylinder 41
containing air or a hydraulic fluid and two pistons 42, 43. One
piston 42 is connected to the throttle linkage, and has a bleed
orifice 44, the other piston 43 is connected so that, on movement
against a spring 45, it causes a switch 46 to make, the switch
contacts being connected to the pulse generators 12 as described
with reference to FIG. 2. The pressures in the two end spaces of
the cylinder are equalized by a connection 47, which is not
connected to the central space 48.
When the position of the throttle linkage changes at more than a
predetermined rate, the travel of piston 42 compresses the air or
other fluid in the central space 48, by reason of the small size of
the bleed orifice 44. This urges the piston 43 to the right against
the spring 45, causing the switch 46 to make. This in turn causes
additional fuel to be injected, exactly as described with reference
to FIG. 2.
The effect is illustrated in FIG. 4 in which, for convenience, both
the change in induction manifold pressure (trace 51) and the change
in throttle angle (trace 52) are plotted against time, together
with traces showing the current pulses supplied to different
injectors 11. The latter are drawn for a six-cylinder engine having
a firing order 153,624, with injectors for cylinders 1, 5 and 3
connected to the first pulse generator 12, and those for cylinders
6, 2 and 4 connected to the second pulse generator.
It will be seen that the further pulses 53 are fed simultaneously
to the different injectors, irrespective of the part of the cycle
of each cylinder at which the acceleration demand signal, e.g.
increase in manifold pressure or change of throttle angle, begins,
and this occurs irrespective of how the acceleration is sensed.
In the embodiment described with reference to FIGS. 1 to 4, it will
be apparent that the pulse generators 12 which produced the main
pulses are also employed to produce a single group of further fuel
enrichment pulses which simultaneously energize all of the fuel
injection valves once only. In the embodiment illustrated in FIGS.
5 and 6, however, successive groups of further fuel enrichment
pulses are produced by auxilliary pulse generators each time that
the engine is conditioned to accelerate.
Referring now to FIG. 5, this system is basically similar to that
previously described in that it incorporates two pulse generators
112 each connected to three fuel injectors 111, and operated by a
trigger device 113, and in that the duration of the main pulses is
dependant upon the two potentials V.sub.1 and V.sub.2. The
potential V.sub.1 is derived from an engine speed discriminator
115, and a manifold pressure control circuit 114 having a manifold
pressure transducer 114a. The potential V.sub.2 is derived from a
start and warm up control circuit 116 having a water temperature
transducer 116a, and, in this embodiment, connected to the manifold
pressure transducer 114a via a DC amplifier 160, resistor R1,
capacitor C1 and controlled-gain DC amplifier 161, all of which
form part of an auxilliary pulse generator circuit indicated
generally at 162, so that this input signal to circuit 116, and
therefore V.sub.2, will be dependant upon the rate of change of
pressure in the induction manifold. Thus, the duration of the main
pulses produced by the pulse generators 112 will be increased to
provide progressive fuel enrichment during, or upon initiation of,
acceleration, in addition to the fuel enrichment provided by the
further pulses. The air temperature transducer 116b, is connected
to an air temperature control circuit 163, the output V3 of which
is fed separately to the main pulse generators 112, so that the
duration of the main pulses will also be dependent upon this
potential V.sub.3. A compensator 170 is provided to compensate for
variations in supply voltage V.sub.S.
The signal from the manifold pressure transducer 114a, after DC
amplification by the amplifier 160, is AC coupled via capacitor
C.sub.2 to four auxilliary pulse generators 164 connected in
parallel. The outputs from the generators 164 are coupled via
diodes D1 to a further DC amplifier 165 connected to the amplifier
stages of both main pulse generators 112, for example to the input
of the transistor TR7 of the pulse generator shown in FIG. 2 of
U.S. Pat. No. 3272187.
The auxilliary pulse generators 164 have different sensitivities so
that they will be triggered by signals corresponding to different
manifold pressure levels relative to a quiescent level
corresponding to the manifold pressure before acceleration is
initiated. The generators 164 may, for example, be initially
adjusted so that they will be triggered by pressures evenly
distributed throughout the normal range of manifold pressures
between the fully closed and fully open conditions of the throttle.
Thus, prior to acceleration, the capacitor C2 will be charged to a
value dependent upon the engine speed to determine the quiescent
level, and upon opening of the throttle to initiate acceleration,
the pressure will increase, the rate and amount of increase
depending upon rate and amount of opening of the throttle, thus
triggering the auxilliary generators 164 in turn so that groups of
further pulses will be applied to the fuel injectors 111. For rapid
acceleration, four comparatively closely spaced groups of further
pulses will be applied to the injectors, while for lesser degrees
of acceleration the group-spacing will increase, and for light
accelerations, only one, two or three of the generators 164 may be
triggered.
The control potential V.sub.2 is applied to the auxilliary
generators 164 via a buffer 166, so that the pulse width of the
further pulses will be dependent upon water temperature.
The auxilliary pulse generator circuit 162 is shown in detail in
FIG. 6. In this Figure, the transistor TR1 and associated
components comprise the DC amplifier 160, the transistors TR2 to
TR5 and their associated components comprise the four auxilliary
pulse generators 164, TR6 constitutes the buffer 166, and TR8 to
TR11 and their associated components constitute the DC amplifier
165. The transistors TR12 to TR14 constitute the controlled gain DC
amplifier 161. The auxilliary pulse generators 164 are additionally
connected via the network 167 and terminal 168 to the starter motor
contact of the engine, which block the generators 164 during
starting of the engine, when fluctuating pressures are created in
the manifold which might otherwise trigger one or more of the
generators 164. The generators 164 are also coupled via terminal
169 to an on-off switch operated by the throttle, which is actuated
to block the generators 164 when the throttle is closed and the
engine is idling.
It will be understood that various modifications may be made
without departing from the scope of the present invention as
defined in the appended claims. For example, the system illustrated
in FIG. 1 may embody means for increasing the duration of the main
pulses triggered by the device 13 upon initiation of, or during,
acceleration, either progressively or by a fixed amount, to
supplement the fuel enrichment afforded by the further pulses
triggered by the device 17.
Moreover, the system illustrated in FIG. 5 may be designed so that
the main pulse duration is increased by a fixed amount, instead of
progressively, upon acceleration, or is independent of acceleration
whereby the fuel enrichment required upon acceleration will be
effected solely by the further pulses.
It will be understood that more or less than the four auxilliary
pulse generators 164 may be provided in the system of FIG. 5, and
these pulse generators may be arranged to be triggered at any
desired manifold pressures.
The systems described and illustrated may incorporate means to
provide a threshold, which may or may not be adjustable, to prevent
the further pulses from being produced, or fed to the fuel
injectors when rate of change of manifold pressure is below a
minimum value. Moreover, although the further pulses produced by
the systems have a variable duration, they may be of fixed
duration.
Although, in the embodiments illustrated, the further pulses are
produced as a result of signals derived from an absolute pressure
transducer connected into the induction manifold, a transducer
which detects the actual rate of change of pressure in the manifold
may be employed, or the signals may be derived from a transducer
associated with the throttle.
* * * * *