U.S. patent number 3,596,645 [Application Number 04/883,401] was granted by the patent office on 1971-08-03 for fuel feed devices for internal-combustion engines.
This patent grant is currently assigned to Societe Industrielle De Brevets et D'Etudes S.I.B.E.. Invention is credited to Andre Louis Mennesson.
United States Patent |
3,596,645 |
Mennesson |
August 3, 1971 |
FUEL FEED DEVICES FOR INTERNAL-COMBUSTION ENGINES
Abstract
The overall duration of opening of an injection valve in the
fuel feed is regulated by an auxiliary throttle member opening
automatically arranged upstream of a main throttle member. The
pressure of the fuel passing through the injection valve is
regulated by a system sensitive to the suction existing in the
space between the two throttle members. Correction means act by
feeding air into the system so as to reduce the suction and can
include a diaphragm-controlled return valve and/or a capsule-driven
piston obturating a calibrated orifice to the atmosphere.
Inventors: |
Mennesson; Andre Louis
(Neuilley-sur-seine, FR) |
Assignee: |
Societe Industrielle De Brevets et
D'Etudes S.I.B.E. (Neuilly-sur-Seine, FR)
|
Family
ID: |
8658235 |
Appl.
No.: |
04/883,401 |
Filed: |
December 9, 1969 |
Foreign Application Priority Data
Current U.S.
Class: |
123/477; 123/442;
123/463; 261/39.2; 123/510; 261/50.2 |
Current CPC
Class: |
F02M
51/02 (20130101); F02M 69/40 (20130101) |
Current International
Class: |
F02M
51/02 (20060101); F02M 69/40 (20060101); F02M
69/30 (20060101); F02m 051/02 () |
Field of
Search: |
;123/32EA,32AE,139AF,139AW,119,14FG,139BG,14MP ;261/5A |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Burns; Wendell E.
Claims
I claim:
1. In a fuel feed device for internal-combustion engines, which
comprise in the induction pipe, upstream of a main throttling
member operated by the driver, an auxiliary throttling member which
opens automatically and progressively as the rate of airflow in the
said pipe increases; means for injecting liquid fuel under pressure
into that portion of the induction pipe downstream of the main
throttling member; and a metering system adapted to respond to the
position of the auxiliary throttling member and so to regulate the
rate of flow of the fuel injected that the richness of the fuel-air
mixture entering the induction pipe is substantially constant, at
least for certain running conditions of the engine, the said
injection means being in the form of a source of fuel under
pressure of which the delivery circuit, leading into the said
portion of the induction pipe, is controlled by at least one valve
operated by an electromagnet, the metering system comprising a
member adapted to be rotated continuously and capable, by affecting
energization of the electromagnet of causing opening of the valve
during only a fraction of each of its rotation, this system being
so arranged that it increases this fraction the further the
auxiliary throttling member opens, and decreases this fraction the
further the auxiliary throttling member closes, the said fuel
source being arranged so that its delivery pressure is regulated by
a system adapted to respond to the suction prevailing in the space
defined in the induction pipe by the two main and auxiliary
throttling members, the improvement that the device comprises
correction means acting by introducing air into the said system in
order to reduce the suction, with the result that these correction
means can also vary said delivery pressure and consequently, for a
given position of the auxiliary throttling member, correct the rate
at which fuel is admitted to the induction pipe by the said
valve.
2. The improvement of claim 1, wherein the fuel source has an
injection pump delivering in parallel to the or each injection
valve and to a return pipe controlled by a return valve, said
return valve being operated by a movable or deformable element
which forms one wall of a chamber connected to the space defined in
the induction pipe by the two throttling members.
3. The improvement of claim 1, wherein the correction means
comprise an enclosed actuator adapted to respond to the suction
prevailing in the induction pipe downstream of the main throttling
member, said actuator controlling a calibrated orifice through
which said correction means communicate with the atmosphere.
4. The improvement of claim 3, wherein the calibrated orifice is
connected to a zone in the induction pipe, said zone being situated
at the air intake of this pipe.
5. The improvement of claim 4, wherein the zone is so situated that
it passes from upstream to downstream of the auxiliary throttling
member when the latter passes from its minimally open position to a
partially open position.
6. The improvement of claim 1, wherein the correction means
comprise a capsule adapted to respond to the characteristics of any
fluid capable of influencing operation of the device and by an
obturator operated by said capsule and adapted to establish or
prevent communication between the said correction means and the
atmosphere.
7. The improvement of claim 6, wherein said communication is via
the air intake of the induction pipe.
8. The improvement of claim 1, wherein the fuel source comprises an
injection pump, and said pump is driven by an electric motor
connected to the engine ignition circuit in such a way that the
pump operates only when the ignition circuit of the
internal-combustion engine is closed.
9. The improvement of claim 1, wherein said continuously rotated
member is driven by the internal-combustion engine.
Description
The invention relates to fuel feed devices for internal-combustion
engines, of the type comprising in the induction pipe, upstream of
a man throttling member operated by the driver, an auxiliary
throttling member which opens automatically and progressively as
the rate of airflow in the said pipe increases; means for injecting
liquid fuel under pressure into that portion of the induction pipe
downstream of the main throttling member; and a metering system
adapted to respond to the position of the auxiliary throttling
member and so to regulate the rate of flow of the fuel injected
that the richness of the fuel-air mixture entering the induction
pipe is substantially constant, at least for certain running
conditions of the engine, the said injection means being in the
form of a source of fuel under pressure of which the delivery
circuit, leading into the said portion of the induction pipe, is
controlled by at least one valve operated by an electromagnet.
The invention relates more particularly to those devices of this
type in which the metering system comprises a member adapted to be
rotated continuously, preferably by the internal-combustion engine,
and capable, by affecting energization of the electromagnet, of
causing opening of the valve during only a fraction of each of its
revolutions, this system being so arranged that it increases this
fraction the further the auxiliary throttling member opens, and
vice versa.
The invention relates more particularly, but not exclusively, to
devices of this type in which the member adapted to be continuously
rotated has means for transmitting to a stationary receiver a flow
of energy during a fraction of a revolution whose value varies
according to the relative positions of the rotary member and
receiver, the receiver being such that it controls the energizing
circuit for the electromagnet according to whether or not it
receives the flow of energy, and the auxiliary throttling member
being such as to modify the relative positions of the rotary member
and receiver; the means for emitting the flow of energy may be a
light source, and the receiver may be a photoelectric cell, the
source and cell being situated on each side of the said rotary
member, which forms an opaque screen containing at least one port
to permit illumination of the cell.
The rotary member is advantageously in the form of a flat, opaque
disc perpendicular to its axis of rotation, the stationary receiver
being such that it can be brought closer to or further from this
axis.
Feed devices (of whatever type) for engines preferably, of course,
have correction means for adapting the richness of the mixture
supplied by them to certain operating parameters, such as the
characteristics (pressure and/or temperature) of the ambient air
and the loads applied to the engines.
The object of the invention is to combine correction means which
are simple and economical in construction with feed devices of the
type described.
According to the invention, the feed device of the type described,
in which the fuel source is so arranged that its delivery pressure
is regulated by a system adapted to respond to the suction
prevailing in the induction pipe between the two main and auxiliary
throttling members, is characterized in that the feed device is
associated with correction means acting by introducing air into the
said system in order to reduce the suction, with the result that
these means can also vary the delivery pressure of the said source
and consequently, for a given position of the auxiliary throttling
member, the rate at which fuel is admitted to the induction pipe by
the said valve.
The invention will in any case be clear from the following
description and the accompanying drawings, relating to preferred
embodiments given purely by way of illustrative examples.
FIG. 1 of the drawings shows, by means of a diagrammatic elevation
with parts in section, a feed device embodying the invention;
and
FIG. 2 shows a section along a line II-II in FIG. 1, on a larger
scale.
A fuel feed device for a vehicle engine or the like is constructed
as follows or in a similar fashion.
As regards the device as a whole, it is constituted in any
appropriate manner, in such a way that it comprises (FIG. 1): In
the induction pipe 1, upstream of a main throttling member 2
operated by the driver, an auxiliary throttling member 3 which
opens automatically and progressively as the rate of airflow in the
said pipe 1 increases; means for injecting liquid fuel under
pressure into that portion of the induction pipe 1 downstream of
the main throttling member 2; and a metering system adapted to
respond to the position of the auxiliary throttling member 3 and so
to regulate the rate of flow of the fuel injected that the richness
of the fuel-air mixture entering the induction pipe 1 is
substantially constant, at least for certain running conditions of
the engine.
According to the embodiment illustrated, the auxiliary throttling
member 3 is in the form of a butterfly valve keyed on a pivot 4.
This butterfly valve is operated by a pneumatic device with a
diaphragm 5 which separates two chambers 6,7 from one another. The
chamber 6 is connected by a duct 8 to a chamber 9 formed by that
portion of the pipe 1 between the main throttling member 2 and the
butterfly valve 3. The pivot 4 is attached to a lever 10 whose free
end bears a detent 11 cooperating with the end of a rod 12
connected to the diaphragm 5. A spring 13 tends to close the
butterfly valve 3, counteracting the influence of the suction
transmitted in the chamber 6. The chamber 7 is connected to the
atmosphere by a duct 14, preferably running from the air intake 15
of the pipe 1.
The angular position of the butterfly valve 3 within the pipe 1 at
any time corresponds, of course, to the rate of airflow in this
pipe. The higher this rate of flow, the more the butterfly valve 3
opens, a substantially constant suction (or a suction varying
according to the characteristics of the spring 13) establishing
itself in the chamber 9 between the two throttling members 2,3.
Equivalent throttling members might be substituted for the
butterfly valve 3, for example members adapted to move in
translation.
The injection means mentioned are in the form of a source of fuel
under pressure (see below) of which the delivery duct 40, which
joins the pipe 1 downstream of the main throttling member 2, is
controlled by at least one valve 16 operated by an electromagnet
17.
The metering system comprises a flat, opaque disc 18 which is
mounted on a shaft 19 connected to a motor, for example the
internal-combustion engine (not shown) supplied by the device, in
such a way that the disc is rotated continuously about an axis
perpendicular to its plane. The disc 18 is placed between a light
source 20 and a photoelectric cell 21 mounted on a common support
22 connected to the auxiliary throttling member 3, and it contains
at least one port 23 adapted to admit the beam from the light
source 20 to the photoelectric cell 21. The cell 21 is adapted to
cause energization of the electromagnet 17, depending on whether or
not it is illuminated, the assembly as a whole being such that the
electromagnet is energized during a fraction of each revolution of
the disc 18 which varies in the same sense as the degree of opening
of the auxiliary throttling member 3.
The light source 20 may be in the form of a lamp which can be
supplied by a battery 24 once the engine ignition switch 25 is on,
and which is housed in a hollow boss 26 containing a hole. This
hole is so arranged that it directs a light beam onto the cell 21,
through a hole in a hollow boss 27 housing this cell.
In the embodiment illustrated, the bosses 26,27 are mounted on the
ends of the U-shaped support 22, which is placed astride the disc
18 so that the source 20 and cell 21 are on opposite sides of this
disc, and which is attached to the pivot 4, the latter being
parallel to the shaft 19 and to the light beam received by the cell
21.
In order to make use of the currents produced in the cell 21, an
amplifying relay 28 and possibly an intensity limiting device 29
may be inserted between this cell and the electromagnet 17.
When the internal-combustion engine has a plurality of cylinders,
each supplied by a valve 16 operated by a separate electromagnet
17, a distributor 30 is provided, this distributor being
synchronized with the disc 18 in order to supply the intermittent
energizing current to the different electromagnets in succession,
along leads such as 31, the disc having as many ports 23 as there
are cylinders to be supplied. These ports are equispaced around the
shaft 19, and each is shaped in such a way that the fraction of a
revolution during which it normally permits illumination of the
cell 21 increases as the throttling member 3 opens, that is to say
(according to the embodiment illustrated), as the bosses 26,27 come
nearer to the shaft 19.
The feed device just recalled operates, of course, as follows:
As the rate of airflow in the pipe 1 increases, the throttling
member 3 opens, moving the support 22 in the direction which brings
the bosses 26,27 nearer the shaft 19. Each of the positions of
these bosses corresponds to a different radius of the disc 18.
Since the shape of each port 23 has been selected so that the
fraction of a revolution during which it admits the light ray from
the source 20 to the cell 21 (a current being produced in the lead
31) increases, the nearer the latter elements come to the shaft 19,
the rate at which fuel is supplied by each injection valve 16 will
necessarily vary in the same sense as the rate of airflow in the
pipe 1.
Under these conditions, the fuel source is arranged so that its
delivery pressure is regulated by a system adapted to respond to
the suction prevailing in the chamber 9, and the feed device is
associated with correction means acting by introducing air into the
said system in order to reduce the suction, with the result that
these means can vary the pressure of the said source and
consequently, for a given position of the auxiliary throttling
member, the rate at which fuel is admitted to the induction pipe 1
by the valve 16.
The fuel source has a reservoir (not shown) connected by a duct 32
to a pump 33, operated either by the internal-combustion engine or
by an electric motor; a float chamber 34 to which the delivery duct
35 from the pump 33 leads, the flow of fuel through the duct 35
being regulated by a needle 36 operated by a float 37; an injection
pump 38 with a relatively high delivery pressure, operated either
by the internal-combustion engine or, preferably, by an electric
motor (not shown) controlled by the ignition switch 25, the suction
duct 39 for this pump being connected to the bottom of the chamber
34 and the delivery duct 40 of the pump to the valve 16; and a
return duct 41, which is connected to the delivery duct 40 of the
pump 38 and whose connection to the reservoir, or rather the
chamber 34, is regulated by the said system adapted to respond to
the suction prevailing in the chamber 9.
As regards this latter system, it comprises a valve 42 cooperating
with a seat 43 formed by the bottom of a chamber 44, which is
immersed in the fuel in the float chamber 34 and to which the
return duct 41 leads; and a movable or deformable element such as a
diaphragm 45 connected to the valve 42, for example by a rod 46,
this element forming one wall of a chamber 47 connected by a duct
48 to the chamber 9 either directly or, as shown in FIG. 1, by way
of the duct 8. The duct 48 contains a calibrated orifice 49. That
side of the diaphragm 45 remote from the suction chamber 47 is
connected to the atmosphere. If, as shown in FIG. 1, this side of
the diaphragm 45 defines a second chamber 50, the latter may be
connected by an orifice 51 to the top of the float chamber 34,
which is itself ventilated by an orifice 52, preferably connected
to the air intake 15 downstream of an air filter. The assembly as a
whole is such that the suction derived from the chamber 9, by
acting on the diaphragm 45, tends to close the valve 42 when the
pressure of the fuel which is delivered to the chamber 44, and
which acts directly on this valve, tends to open it.
In accordance with the invention, the correction means are arranged
so that they act by introducing air into the chamber 47 in order to
reduce the suction inside it, this suction being transmitted to it
by the duct 48.
In a first embodiment, the correction means comprise an enclosed
actuator adapted to respond to the suction prevailing in the
induction tube 53 of the induction piping, which continues the pipe
1 downstream of the main throttling member 2. As FIG. 1 shows, this
enclosed actuator may be in the form of a movable or deformable
member such as a diaphragm 54, biased by a spring 55 and closing a
chamber 56 connected by a duct 57 to the tube 53. The central
portion of the diaphragm 54 forms an obturator for a calibrated
orifice 58, through which the suction chamber 47 can communicate
with the atmosphere. The assembly as a whole is such that the
suction prevailing in the chamber 56 of the actuator tends to open
the orifice 58, counteracting the spring 55.
Preferably, the orifice 58 communicates, by way of a chamber 59
defined by the diaphragm 54 on the opposite side from the suction
chamber 56, with the air intake 15 by way of a duct 60. As shown by
solid lines in FIG. 1, this duct may run from a site 61 permanently
upstream of the auxiliary throttling member 3. Often, however, as
shown by chain lines, it may be better to run it from a site 61a,
so that it moves from upstream to downstream of the auxiliary
throttling member 3 when the latter passes from its minimally open
position (shown by broken lines) to a partially open position
(beyond that shown by chain lines).
In a second embodiment, which may be used either separately or in
combination with the preceding embodiment, the correction means
comprise a capsule 62 adapted to respond to the characteristics of
any fluid capable of influencing operation of the device and
entailing a correction of the richness of the mixture, this capsule
62 operating a needle 63 (or equivalent obturating means) adapted
to establish or prevent communication between an orifice 64,
similar to the orifice 58, and a ventilating orifice 65, possibly
connected to a duct (not shown) similar to the duct 60. The fluid
mentioned above may be the ambient air, of which the temperature
and/or pressure may be determined by the capsule 62.
The resulting device operates as follows.
The pump 38 is preferably driven by an electric motor connected by
the switch 25 to the engine ignition circuit so that, as soon as
the engine starts, the pressure required to supply the or each
injection valve 16 is produced in the duct 40. When the engine
turns, a certain suction appears in the chamber 9 between the
throttling members 2 and 3 and therefore in the duct 48, and this
suction acts on the diaphragm 45 and closes the valve 42, by
drawing it onto its seat 43. This suction regulates the pressure
prevailing in the duct 40.
Subsequently, under all engine running conditions, the delivery
pressure of the fuel in the duct 40 is regulated by the leakage
through the valve 42, which always depends on the suction
prevailing between the throttling members 2 and 3. In general,
therefore, the suction in the chamber 47 is the same as that in the
chamber 6 or 9.
In certain cases, however, it may be necessary to reduce this
suction, If the shapes of the ports 23 have been designed for the
full load curve, the shapes of these ports may be unsuitable for
the "partial load" curves and may lead to excessive richness of the
mixture. The fuel pressure under partial load must then be reduced
at the or each valve 16 in order to correct the mixture.
Running under a reduced load increases the suction in the tube 53,
and therefore in the duct 57 and chamber 56. The diaphragm 54 is
therefore moved, counteracting the spring 55, and the orifice 58 is
uncovered so that air drawn in along the duct 60 can enter the
chamber 47. The existence of the calibrated orifice 49 makes it
possible to produce in this chamber 47 a suction slightly less than
that in the chambers 6 and 9.
The pressure of the fuel in the duct 40 is therefore reduced to
extents depending on the respective sizes of the calibrated
orifices 49 and 58, so that, whenever the engine is running under a
reduced load, a lower fuel pressure, and therefore a lower rate of
fuel flow, can be produced for the same rate of airflow as under
full load conditions.
Similarly, if the atmospheric pressure drops or the air temperature
is too high, the fuel pressure must be modified in order to prevent
the mixture from becoming too rich. To this end, the capsule 62,
which may be a barometric capsule if compensation of the barometric
pressure is required, expands if the atmospheric pressure drops,
moving the needle 63 beyond the orifice 64 so that air can enter
the chamber 47, producing the same effect as the intake of air
through the orifice 58. The fuel pressure therefore drops, and with
it the total delivery from the injection valves 16. If the mixture
is to be corrected on account of the temperature, it is merely
necessary for the capsule 62 to be temperature responsive.
As already explained above, the two devices may be used
simultaneously, as shown in FIG. 1.
Also, if, in the case of the arrangement having the enclosed
actuator with the diaphragm 54, the air is drawn in through the
orifice 61a as shown by chain lines, the fuel pressure can be
corrected for certain rates of airflow, for example for low rates
of airflow and under a reduced load. As long as the throttling
member 3 is between the closed position shown by broken lines and
the position shown by chain lines, the air is, of course, drawn in
upstream of the throttling member 3, so that, if the diaphragm 54
uncovers the orifice 58, the air introduced through the duct 60
helps to reduce the fuel pressure in the duct 40. As soon as the
throttling member 3 moves past the position shown by chain lines on
the other hand, the duct 60 is opened downstream of the throttling
member 3, and it is subjected to substantially the same suction as
the duct 8. As a result the air arriving through the duct 60 and
orifice 58 is at the same pressure as the air arriving through the
duct 48, and the actuator with the diaphragm 54 becomes
inoperative. This actuator, therefore, can be used not only to
compensate for reduced loads as compared with full loads, but also
to correct the mixture within a certain range of airflow rates, as
compared with other ranges of airflow rates.
Lastly, when the engine stops, the pump 38 is stopped and the
suction in the duct 48, and therefore in the chamber 47,
disappears, so that the valve 42 opens and the pressure in the duct
40 returns to zero. This prevents any leakage from the injection
valves 16 while the engine is off.
The present device therefore offers innumerable correction
possibilities, which can be very simply realized, to adapt the
metering device to all types of engines and any physical
characteristics of the air fed to the engine.
* * * * *