U.S. patent number 3,724,435 [Application Number 05/006,656] was granted by the patent office on 1973-04-03 for remote metering system.
This patent grant is currently assigned to Holley Carburetor Company. Invention is credited to Kenneth C. Bier.
United States Patent |
3,724,435 |
Bier |
April 3, 1973 |
REMOTE METERING SYSTEM
Abstract
An internal combustion engine and a fuel supply tank, located
remote to the engine, are provided with transducers sensitive and
responsive to parameters of engine speed, engine intake manifold
pressure, engine temperature and ambient temperature for providing
control signals in accordance with such parameters; a fuel supply
pump, pressure regulator and fuel metering device are situated
within the fuel tank and connected by conduit means to a fuel
discharge valve situated for discharging metered fuel to the engine
induction passage; and control means responsive to the control
signals is operatively connected to the fuel metering device for
control thereof in order to thereby meter fuel to the engine in
accordance with the demand therefor.
Inventors: |
Bier; Kenneth C. (Bloomfield,
MI) |
Assignee: |
Holley Carburetor Company
(Warren, MI)
|
Family
ID: |
21721968 |
Appl.
No.: |
05/006,656 |
Filed: |
January 29, 1970 |
Current U.S.
Class: |
123/482; 123/446;
123/457 |
Current CPC
Class: |
G01F
9/001 (20130101) |
Current International
Class: |
G01F
9/00 (20060101); F02m 039/00 () |
Field of
Search: |
;123/32E,139E,139AV,134
;223/385 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
|
|
|
|
|
|
|
818,197 |
|
Aug 1958 |
|
GB |
|
718,649 |
|
Feb 1942 |
|
DD |
|
1,114,673 |
|
Oct 1961 |
|
DT |
|
1,171,205 |
|
May 1964 |
|
DT |
|
Primary Examiner: Goodridge; Laurence M.
Assistant Examiner: Cox; Ronald B.
Claims
I claim:
1. A remote fuel metering system for an internal combustion engine
and an associated fuel supply tank situated generally remote with
respect to said engine, comprising pressure supply means situated
within said tank, said pressure supply means including an inlet for
admitting said fuel from said tank and an outlet for discharging
said fuel under pressure, fuel metering means situated within said
fuel supply tank, said fuel metering means including inlet means
for receiving said pressurized fuel from said pressure supply means
and an outlet for discharging metered fuel, fuel delivery means
carried by said engine and operatively connected to said outlet of
said fuel metering means, said fuel delivery means being effective
for delivering said metered fuel to the intake of said engine,
pressure regulating means having an inlet communicating with said
outlet of said pressure supply means and an outlet communicating
with said inlet of said fuel metering means, said pressure
regulating means being enclosed within said tank and effective to
regulate the pressure of said fuel entering said inlet of said fuel
metering means, and additional means responsive to selected engine
operating parameters for controlling said fuel metering means in
order to thereby achieve a rate of metered fuel flow to said fuel
delivery means in accordance with said operating parameters, said
additional means comprising a plurality of individual engine
operating parameter sensing means each effective for producing an
output signal totally independent of and unaffected by the other of
said plurality of sensing means.
Description
BACKGROUND OF THE INVENTION
In recent time governmental bodies have enacted legislation which
limits the amount of contaminants that an automobile engine may
discharge into the atmosphere when the vehicle is driven according
to a prescribed schedule. In the course of complying with such
legislation, the automobile manufacturers have made modifications
which have resulted in increased temperatures within the engine
compartment. Certain automotive styling trends have further
aggravated the problem of increased underhood temperatures and the
total problem is still further compounded by the ever increasing
volatility of the fuels being marketed. Such conditions often
result in problems of starting the engine (when the engine is
extremely hot), getting the engine to idle properly (also when the
engine is hot), fuel vapor locks in the fuel supply system and
evaporative fuel losses to the atmosphere.
Additionally, in order to meet the requirements relating to exhaust
emission, it is necessary that the fuel system be sufficiently
flexible to provide the optimum quantity of fuel for each of the
operating modes of the emission cycle. That is, the quantity of
fuel supplied during any given mode of the emission cycle must be
adjustable (capable of calibration) independent of each of the
other modes of the cycle. The prior art fuel supply systems do not
have such characteristics.
Further, when the proper quantity of fuel is supplied to the engine
at any operating condition, it is imperative that the atomization
and/or vaporization thereof be sufficient to permit optimum
ignition or combustion of the fuel-air charge.
Accordingly, the invention as herein disclosed and described is
concerned with the solution of the above as well as other related
problems.
SUMMARY OF THE INVENTION
According to the invention, a remote fuel metering system for an
internal combustion engine and an associated fuel supply tank
situated generally remote with respect to said engine, comprises
pump means situated within said tank, said pump means including an
inlet for admitting said fuel from said tank and an outlet for
discharging said fuel under pressure, fuel metering means situated
within said fuel supply tank, said fuel metering means including
inlet means for receiving said pressurized fuel from said pump
means and an outlet for discharging metering fuel, fuel delivery
means carried by said engine and operatively connected to said
outlet of said fuel metering means, said fuel delivery means being
effective for delivering said metered fuel to the engine intake,
and additional means responsive to selected engine operating
parameters for controlling said fuel metering means in order to
thereby achieve a rate of metered fuel flow to said fuel delivery
means in accordance with said operating parameters.
DESCRIPTION OF THE DRAWINGS
In the drawings, where in one or more views certain elements may be
omitted for purposes of clarity;
FIG. 1 is a somewhat diagrammatic view, with partial electrical
circuitry, illustrating a fuel metering system constructed in
accordance with the teachings of the invention; and
FIG. 2 is an enlarged fragmentary cross-sectional view of one of
the elements shown in FIG. 1.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring now in greater detail to the drawings, FIG. 1 illustrates
a vehicular internal combustion engine 10, a fuel supply tank 12
situated remote to the engine 10, as well as electrical circuitry
14 and conduitry operatively interconnecting the fuel tank 12 and
the engine 10.
As generally depicted, the engine 10 may be comprised of an engine
block 16, an intake or induction manifold 18 leading to the inlet
valves associated with the pistons and cylinders within the engine
block 16, and an air induction passage 20, formed within a device
22, serving to communicate atmospheric air from its intake end 24
to the inlet 26 of the manifold 18. As shown, a throttle valve 28,
pivotally carried by a variably rotatably positioned throttle shaft
30, is situated within the induction passage means 20 so as to
variably control the rate of air flow therethrough in accordance
with operator demands. A throttle actuating lever 32 may be secured
to the throttle shaft 30 and operatively connected to suitable
control linkage as, for example, the usual foot-operated throttle
pedal situated within the passenger compartment of the related
vehicle.
A rotatable shaft 34, which may be, in effect, an extension of the
engine crankshaft, is shown as being provided with sheaves 36 and
38 secured thereto for rotation therewith. A second shaft 40, which
may be connected to an engine water (coolant) pump and a fan 42,
fixedly carries a sheave 44 enabling the rotation of such shaft 40
in accordance with the rotation of crankshaft 34 via suitable belt
means 46 engaging sheaves 36 and 44.
As schematically illustrated, a suitable transducer means 50 is
provided with a rotatable shaft 52 which fixedly carries a sheaves
54 operatively engaged to the second sheave 38 on crankshaft 34 as
by means of a drive belt 56. The transducer means 50 is shown as
having one terminal connected to ground potential as at 58, while
its other terminal is connected to one terminal 60 of a resistor,
R.sub.1, via conductor 48.
A second temperature responsive transducer means 62 is illustrated
as being located generally in the ambient atmosphere in which the
engine 10 is operating. Transducer 62 is shown having one of its
terminals electrically connected to ground as at 64 while its other
terminal is connected to one terminal 66 of a second resistor,
R.sub.2, by means of conductor 68.
Similarly, a third pressure responsive transducer means 70 is
suitably connected as at 72 so as to be responsive to the pressure
within the intake manifold 18. One terminal of transducer 70 is
connected to ground potential as at 74 while the other terminal is
electrically connected to one terminal 76 of a third resistor,
R.sub.3, via an electrical conductor 78.
Finally, a fourth transducer means 80, responsive to temperature,
is suitably connected as at 82 so as to be responsive to the
temperature of the engine 10. One terminal of the transducer 80 is
connected to ground as at 84 while the other terminal is
electrically connected as by conductor means 86 to one terminal 88
of a fourth resistor, R.sub.4.
The other terminals 90, 92, 94 and 96 of resistors R.sub.1,
R.sub.2, R.sub.3 and R.sub.4, respectively, are connected by a
common electrical conductor 98 which has a juncture point 100 to
which one end of a conductor 101, leading to an operational
amplifier 102, is connected. A feedback resistor, R.sub.F, is
placed in generally parallel relationship with amplifier 102 by
having its opposite terminals 104 and 106 respectively connected to
input conductor 101 and an output conductor 108 as by conductors
110 and 112. A third terminal of the amplifier 102 is connected to
ground 114 as by a conductor 106. As will be seen, the operational
amplifier 102 and the feedback resistor R.sub.F comprise an
operational amplifier summing system 118.
The fuel tank 12 may be comprised of a general housing 120,
provided with filler tube 122 and closure cap 124, containing
therein a fuel pump assembly 126, which may be electrically driven,
a pressure regulator assembly 128, a main metering valve assembly
130, an on-off type solenoid operated valve assembly 132 and a
pressure relief valve assembly 134. As generally depicted, all of
the preceding elements may be submerged within the fuel 136
contained in tank housing 120.
As shown, an intake conduit 138, having an open lower end 140, is
connected to the inlet of pump assembly 126 which serves to pump
such fuel at an elevated pressure through the pump discharge
conduit 142 to the inlet conduit portion 144 of the pressure
regulator assembly 128.
The regulator assembly 128 may be comprised of housing sections 146
and 148 which peripherally retain therebetween a pressure
responsive moveable diaphragm 150 which defines two distinct but
generally variable chambers 152 and 154. A valve member 156,
secured to the diaphragm 150 as by diaphragm plates 158 and 160,
has its stem portion 162 passing through the aperture 164 about
which is formed an annular valve seat 166. A compression spring
168, situated within chamber 154, normally urges diaphragm 150
upwardly so as to move valve member 156 away from valve seat 166 in
order to open the orifice 164. An outlet conduit 168 communicates
with the chamber 152 and serves to direct fuel flow to the inlet
conduit portion 170 of the metering valve assembly 130.
The metering valve assembly 130 may be comprised of a housing 172
having formed therein chambers 174 and 176 between which is
situated a wall portion 178 provided with a metering orifice 180
formed therethrough. A contoured metering valve portion 182,
operatively carried and actuated or positioned as by the armature
184 of a proportional solenoid assembly 185, coacts with the
metering orifice 180 in order to determine proper effective flow
areas therebetween for achieving the desired rate of fuel flow
therethrough. As shown, the proportional solenoid assembly 185, in
addition to armature 184, has a winding or field coil 186 having a
first terminal 188 connnected to ground 190 as by a conductor 192,
and a second terminal 194 connected to one end of a conductor -196
leading to the output conductor 108. Suitable spring means 199 may
be provided to normally urge the armature 184 and valve member 182
upwardly thereby tending to more nearly completely close the
effective flow area through metering orifice 180.
One end 198 of an outlet conduit 200 is connected to housing 172 so
as to be in communication with chamber 176 while its other end 202
is connected to the inlet end of a metered fuel discharge valve
assembly 204 which may be threadably carried by the housing of
induction device 22, as shown in FIG. 1, so as to have the
discharge end thereof in position for discharging metered fuel into
the induction passage 20.
A branch conduit 206 serves to connect the inlet of the solenoid
operated valve assembly 132 to conduit 200. The outlet of solenoid
operated valve assembly 132 is connected via a conduit 208 to the
inlet of the pressure relief valve assembly 134 while the outlet
thereof is open to the interior of fuel tank housing 120 via
conduit 210.
A suitable source of electrical potential 212 has one of its
terminals at ground potential, as at 214, while its other terminal
is connected to electrical conductor means 216 leading as to, for
example, the associated vehicular ignition system (not shown but
well known in the art). A convention key-operated ignition switch
218 may be aerially situated in conductor 216. Further, as
illustrated, one terminal of the solenoid valve assembly 132 is
connected to ground 220 by means of a conductor 222 while its
second terminal is connected to conductor 216, at a point 224, as
by a second conductor 226. As a consequence of such electrical
connections, whenever switch 218 is closed solenoid valve assembly
132 is energized thereby terminating all fluid flow therethrough;
whenever switch 218 is open, as shown, solenoid valve assembly 132
is in a de-energized state permitting free flow therethrough from
conduit 206 to conduit 208.
Although the fuel discharge valve means may take any suitable form
and may in fact be comprised of a plurality of individual valves
communicating with the engine induction system at spaced points of
discharge, the fuel discharge valve assembly 204, for purposes of
illustration, may be comprised of a suitable outer body or housing
228 with an internal passage means 230 having generally an inlet
end 232 (for coupling to conduit 200) and an outlet end 234. A
discharge aperture 236 is normally closed as by end 238 of a
spring-loaded pintle 240 the other end of which is operatively
connected to a compression spring 242 seated against an internal
shoulder 244. An externally formed threaded portion 246 is provided
for operative engagement with, for example, the body of air
induction device 22. A suitable tool engaging surface 248 may also
be provided for enabling the threadable engagement and
disengagement of the valve assembly 204 with respect to the related
supporting structure.
OPERATION OF INVENTION
Generally as is well known in the art, a transducer is a device
capable of being actuated by power from a first system and capable
of, in response thereto, supplying power to a second system
different from the first system. Accordingly, as indicated,
transducers 50, 62, 70 and 80 are selected as to be responsive to
different parameters and to, in turn, produce variable output
voltage signals in response thereto.
That is, transducer 50 is made responsive to engine speed and is
accordingly effective for producing a variable voltage signal
V.sub.1 on conductor 48. The magnitude of voltage signal V.sub.1
generally increases as the speed of the engine increases.
Transducer 62 is responsive to ambient temperature and is set as to
produce a voltage signal V.sub.2 on conductor 68. Generally, the
magnitude of voltage signal V.sub.3 decreases as the ambient
temperature increases.
Transducer 70 is responsive to manifold vacuum (or pressure) and is
set to produce a voltage signal V.sub.3 on conductor 78. Generally,
the magnitude of voltage signal V.sub.3 increases as the pressure
in the intake manifold increases (or if considered in terms of
vacuum, as the vacuum decreases).
Finally, transducer 80 is responsive to engine temperature and is
set to produce a fourth voltage signal V.sub.4 on conductor 86.
Generally, the magnitude of the voltage signal V.sub.4 decreased as
the engine temperature increases.
Resistors R.sub.1, R.sub.2, R.sub.3, and R.sub.4 are provided in
order to generate a current flow, through each of such resistors,
which is proportional to the respective voltage signals generated
and applied thereto. Normally, the impedance of the operational
amplifier 102 is so high as to preclude any current flow
therethrough. Accordingly, point 100 may be considered as a summing
point for such current flows regardless of the direction or
magnitude of the individual currents I.sub.1, I.sub.2, I.sub.3, and
I.sub.4. Since current cannot flow through the operational
amplifier, such current passes through the feedback resistor
R.sub.F and consequently results in the generation of an output or
control voltage V.sub.5 at the terminal 108 and conductor 196.
As should be evident in view of the preceding, the control voltage
V.sub.5 is automatically indicative of the total requirements for
fuel flow as sensed by the various transducers responsive to the
selected parameters. That is, for example, if engine temperature
should rise at any particular engine speed, the value of V.sub.4
will decrease thereby reducing the total value of generated current
at summing point 100. This, in turn, reduces the value or magnitude
of V.sub.5.
Accordingly, the normally closed valve 182 and armature 184 are
moved downwardly some distance in accordance with the magnitude of
the control voltage V.sub.5 applied to the winding 186. Generally,
as the magnitude of control voltage V.sub.5 increases the armature
184 and valve 182 are moved further downwardly thereby producing a
greater effective flow area through the metering restriction or
orifice 180.
The rate of metered fuel flow through the metering orifice 180 is,
of course, dependent primarily on the effective flow area of the
metering orifice 180 and the magnitude of the pressure differential
thereacross. However, the factor of the pressure differential is
effectively eliminated by the invention. That is, the upstream
pressure of the fuel, supplied by the pump assembly, is maintained
substantially constant by the pressure regulating or throttling
valve assembly 128. For example, any tendency for an increase in
such upstream pressure is sensed by the diaphragm 150 which
responds thereto by moving downwardly causing valve member 156 to
more nearly close the orifice or passageway 164, and conversely, as
a decrease in upstream pressure is sensed diaphragm 150 is moved
upwardly causing valve member 156 further open the orifice or
passageway 164. Consequently, it can be seen that the pressure of
the fuel within chamber 174 is maintained substantially
constant.
Similarly, the downstream fuel pressure is also maintained
substantially constant. That is, the fuel discharger valve assembly
204 is so calibrated so as to permit valve portion 238 to open only
upon the attainment of a predetermined fuel pressure within passage
means 230; this being primarily determined by the pre-load force of
spring 242. Therefore, it can be seen that during normal engine
operation, the downstream fuel pressure (downstream of metering
orifice 180) will also be at a substantially constant value but
less than the fuel pressure upstream of metering orifice 180.
Therefore, it should be apparent that the volume rate of fuel flow
through the metering orifice 180 will be generally in accordance
with the position of the metering valve 182 with respect to the
metering orifice 180.
From the preceding it should be apparent that when the engine is
cold and initially started the transducer 80 will sense the cold
engine temperature and thereby create an output signal V.sub.4 of
relatively high magnitude, if the engine remains at idle transducer
70 will sense a relatively high manifold vacuum and in accordance
therewith produce an output signal V.sub.3 of relatively high
magnitude, and transducer 50 will sense the relatively low engine
speed (at idle) and produce in accordance therewith an output
signal V.sub.1 of relatively low magnitude. Consequently, the
summing point 100 senses a relatively low total current and the
feedback resistor, R.sub.F, consequently causes a relatively low
control voltage V.sub.5 on conductor 196 causing the metering valve
182 and solenoid armature 184 to be positioned relatively close to
the metering restriction 180 reducing the volume rate of metered
fuel flow. Of course, it can be seen that with an increase in
engine speed, an increase in engine temperature or an increase in
engine load, the value of signal V.sub.1 will increase, while in
the case of transducers 70 and 80, the magnitudes of signals
V.sub.4 or V.sub.3, as the case may be, will decrease and in
accordance therewith alter the total current sensed at summing
point 100.
The disclosure of the invention is intended to be merely exemplary
of the many types of arrangement which can be employed within the
scope of the inventive concept. To this extent it should be
apparent, for example, that various transducers devices could be
employed and that, if desired, suitable diodes could be employed
within the transducer circuitry shown for providing maximum values
of voltage signals generated by the transducers.
From the preceding disclosure, it should also be apparent that the
invention provides a fuel metering system responsive to a group of
selected parameters wherein the responsiveness of the metering
system to any one of the group of selected parameters can be
critically tailored or adjusted without in any way influencing the
action of the means employed for sensing the remaining parameters
of such a group.
Further, as was previously mentioned, during conditions of engine
operation, solenoid valve 132 is closed; however, during engine
shut-down, solenoid valve 132 is opened so as to permit flow
therethrough. The pressure relief valve 134, may contain suitable
spring means, as is well known in the art, which may be set so that
the valve 134 will open at a somewhat lower fuel pressure than that
at which the delivery valve 204 is set to open. This then provides
a discharge or return flow path to the tank 120 in order to
accommodate any fuel expansion, due to heat, in the metered fuel
supply conduit 200.
Although only one embodiment of the invention has been disclosed
and described, it is apparent that other embodiments and
modifications of the invention are possible within the scope of the
appended claims.
* * * * *