U.S. patent number 3,669,361 [Application Number 05/053,340] was granted by the patent office on 1972-06-13 for electromagnetic fuel injectors for internal combustion engines.
This patent grant is currently assigned to Societe des Procedes Modernes d'Injection Sopromi. Invention is credited to Herve Gueret.
United States Patent |
3,669,361 |
Gueret |
June 13, 1972 |
ELECTROMAGNETIC FUEL INJECTORS FOR INTERNAL COMBUSTION ENGINES
Abstract
An electromagnetically controlled injector for internal
combustion engines adapted to cut out the effects on uniformity of
feed of all parasitic phenomena such as the rebounds of the needle
and modifications in the pressure prevailing in the feed pipes. To
this end, the liquid fuel is protected against the formation of
waves by a throttling of the incoming liquid in a channel extending
laterally of the stationary armature or else axially through the
latter directly into the needle. Thus it is possible to obtain for
the curve of injected fuel amounts vs. time a straight line between
the desired minimum and maximum amount values.
Inventors: |
Gueret; Herve (Versailles,
FR) |
Assignee: |
Societe des Procedes Modernes
d'Injection Sopromi (Les Mureaux, FR)
|
Family
ID: |
9038493 |
Appl.
No.: |
05/053,340 |
Filed: |
July 9, 1970 |
Foreign Application Priority Data
Current U.S.
Class: |
239/585.5;
239/533.3 |
Current CPC
Class: |
F02M
51/0657 (20130101); F02M 51/0635 (20130101); F02M
51/08 (20190201) |
Current International
Class: |
F02M
51/06 (20060101); F02M 51/08 (20060101); B05b
001/30 () |
Field of
Search: |
;239/585,533 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
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217,249 |
|
Sep 1961 |
|
OE |
|
217,248 |
|
Feb 1961 |
|
OE |
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Primary Examiner: King; Lloyd L.
Claims
What I claim is:
1. An electromagnetic fuel injector for an internal combustion
engine comprising an elongated body having a fuel input port and a
fuel output port disposed adjacent the opposite ends thereof, a
stationary armature mounted in the body, an electromagnetic winding
for inducing flux in the stationary armature, a movable armature
slidably mounted within the body for longitudinal movement to and
from a closing position, the movable armature having a needle at
one end thereof for closing the output port when the movable
armature moves to the closing position, a fuel chamber surrounding
the needle of the movable armature adjacent to the output port and
being in communication with the fuel output port when the movable
armature is moved from the closing position, the fuel chamber
having a reduced volume, and an elongated fuel passage in the body
extending from the fuel input port to the fuel chamber, the fuel
passage having a small bore, the small bore of the fuel passage
restricting the flow of fuel from the fuel output port when the
movable armature initially moves from the closing position, thus
reducing the amount of fuel per unit of time initially discharged
from the fuel output port during the transient fuel flow period
when the needle is initially moved from the fuel output port.
2. An electromagnetic injector in accordance with claim 1 in which
the fuel passage has an approximately uniform cross-section.
3. An electromagnetic fuel injector in accordance with claim 2 in
which the fuel passage has a circular cross-section, the ratio of
the length of the fuel passage to the diameter thereof being equal
to or greater than about 10.
4. An electromagnetic fuel injector in accordance with claim 3 in
which the diameter of the fuel passage is approximately 2
millimeters.
5. An electromagnetic fuel injector in accordance with claim 2 in
which at least a substantial portion of the fuel passage extends
along the longitudinal axis of the stationary and movable
armatures, the movable armature having a port therein adjacent the
needle for communicatively connecting the longitudinally extending
fuel passage with the fuel chamber.
6. An electromagnetic fuel injector in accordance with claim 2 in
which the body further comprises a space surrounding the movable
armature, a first portion of the fuel passage communicatively
connecting the fuel input port and the space, the first portion of
the fuel passageway extending laterally around the electromagnetic
winding, and a second portion of the fuel passage communicatively
connecting the space and the fuel chamber.
7. An electromagnetic fuel injector in accordance with claim 1
wherein the body comprises an upper portion and a nozzle portion,
the upper portion for mounting the stationary armature therein with
a portion of the stationary armature adjacent one end thereof, the
one end of the upper portion being adapted to engage the nozzle
portion, the nozzle portion for mounting the movable armature for
longitudinal movement therein, the nozzle portion engaging the
upper portion for positioning the movable armature adjacent to but
spaced apart from the stationary armature, the movable armature
being biased against the nozzle portion, the nozzle portion being
constructed of a material having a low thermal expansion
coefficient, and a ring constructed of an amagnetic material being
disposed between the upper portion and the nozzle portion and
abutting a portion of the upper portion and another portion of the
nozzle portion for spacing the nozzle portion with respect to the
upper portion, the ring thus establishing the spaced apart
relationship of the stationary armature and the movable armature,
the combination of the amagnetic ring and the nozzle portion
constructed of a material having a low thermal expansion
coefficient for reducing the sensitivity of the fuel injector to
expansion caused by magnetic field generated by the electromagnetic
winding.
8. An electromagnetic fuel injector in accordance with claim 1
wherein the stationary armature has three parallel core members,
the middle core member being surrounded by the electromagnetic
winding, the stationary armature being laminated, the movable
armature comprising a laminated plate having an upper surface
adjacent to but spaced apart from the lower surface of the
stationary armature.
Description
BACKGROUND OF THE INVENTION
The present invention relates to improvements in electromagnetic
fuel injectors for internal combustion engines. It is a well known
fact that it is possible to measure the amount of fuel injected by
means of electromagnetic injectors adapted to receive for the
execution of each injection an electric signal of a predetermined
duration, which duration depends on the operative conditions of the
internal combustion engine. The injectors should operate at
considerable speeds ; by way of example, it should be remarked that
the durations of injection range between 0 and 2 ms for Diesel
engines and from 0.8 to 4 ms. for gasoline-operated engines, the
amounts of injected fuel ranging between 7 and 40 cubic mm.
The injectors resorted to are of the type provided with a needle
cooperating with a port defining the throughput. The needle is
rigid with the movable electromagnet armature constituted by the
lamellatted plate of the electromagnet. The movable armature
registers with the stationary armature.
The needle rises by amounts of a magnitude of 0.1 mm. and,with
injectors of such a type operating at such speeds to,it is
necessary to cut out all parasitic phenomena which may have an
influence on the amount of fuel injected in conformity with the
duration of the electric signals.
In fact, the speedy upward and downward movements of the injector
needle lead to rebounds and to large modifications in pressure in
the pipes,which are ascribable to the high instantaneous outputs
and wave effects.
Consequently, the amount of fuel injected with reference to time
does not follow a linear law and it depends on the following
characteristics: wave effects are produced by the reflection of
waves inside the pipe system ; there is a threshold below which it
is no longer possible to foresee to a sufficient extent the actual
amount of injected fuel. The slope of the curve corresponding to
the amount of fuel injected as a function of time is very high at
such a point by reason of the elastic properties of the liquid
inside the injector. The shape of the curve always shows a speedy
rise at the beginning, a relative maximum, and a relative minimum
produced by the rebounds of the needle on its abutments. It is only
beyond the minimum that the curve shows its useful section which
should be substantially linear. It should be remarked that the
pressure waves in the different injectors act mutually on one
another.
By reason of the influences and interactions mentioned hereinabove,
an injector, operating at an injection pressure selected to provide
the maximum amount of fuel to be injected during a predetermined
period, may not permit the amount of fuel injected to drop below a
minimum amount of fuel which is higher than the minimum amount
required for a proper operation of the engine. Conversely, if the
injection pressure is selected and the injector is designed so as
to provide the minimum amount of fuel required for the engine, it
is not possible to obtain the necessary maximum amount of fuel.
The present invention has for its object to solve such a problem by
causing the non-linear section of the curve defining the injected
amount of fuel vs. the time elapsed to assume a lower level in
order to obtain the minimum amount of fuel required at the
beginning of the linear section of the curve while the fuel
injection pressure is slightly increased so as to allow the maximum
fuel output to be obtained for a predetermined duration of
injection.
SUMMARY OF THE INVENTION
According to the present invention, the injector is designed so
that it has a minimum idle volume filled with gasoline and
communicating with the injection port so as to completely cut out
the effects of the elasticity of the liquid in the fuel injector.
Further, at least a portion of the channel between the seat of the
injector valve and the supply of compressed fuel has a
cross-section which retards the speed of progression of the liquid
by submitting it to a sufficient inertia so that it is possible to
obtain a comparatively slow fuel flow through the injector which
lasts substantially during the rebounds of the injector needle.
As a development of this general principle, no idle volume is
provided between the stationary electromagnet armature and the body
of the injector. The armature is provided with a central bore
having a diameter of about 2 mm. The bore provides fuel from the
supply to a central bore in the needle of the injector through a
central bore in the movable armature.
According to another embodiment of the invention, a tube having a
diameter of about 2 mm. is provided to supply fuel to the injector
port. The tube is bent so as to pass round the stationary armature
of the injector, thus presenting no idle volume within the injector
body, and opens into the space enclosing the movable armature of
the injector. This space in turn communicates with the injector
port when the injection valve is open.
A further object of the invention consists of producing an injector
body which has little sensitivity to thermic expansion. A nozzle of
case hardened steel is spaced with reference to the magnetic
circuit by a bronze ring. The ring is provided for locking the
nozzle on the body of the injector and for permanent positioning of
the magnetic circuit by its bearing against the lower section of
the latter. The magnetic circuit is adherently secured to the
injector body only along the lateral outer surface of its lower
section.
An embodiment of the invention is illustrated in the accompanying
drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a partial sectional view of an injector extending through
line I--I of FIG. 2;
FIG. 2 is a partial sectional view of the same injector as seen
through line II--II of FIG. 1;
FIG. 3 is a sectional view of a further embodiment of the injector;
and
FIG. 4 is a diagrammatic illustration of the curve showing the
amounts of fuel injected as functions of the duration of the
control signal.
BRIEF DESCRIPTION OF THE INVENTION
As illustrated FIGS. 1 and 2, the body 1 of the injector has at its
upper end terminals 2 and 3 feeding the inducing winding 4 of the
armature constituted by the magnetic circuit 5. The needle carrying
part 11 of the injector, which is held spaced from the central
section of the magnetic circuit by a washer 6, is guided inwardly
of the body 1 by a projection 8 on the magnetic circuit. The
projection is subjected to the pressure of the spring 12. The
needle carrying part 11 slides in the axial bore of the nozzle 9.
Both the movable part 11 and the nozzle 9 are made of case hardened
steel. A bronze ring 7 serves as a mechanical spacer between the
nozzle 9 and a shoulder on the injector body 1. The ring 7 is made
of an amagnetic material to prevent the magnetic flux from closing
over the movable needle and subjecting the latter to
friction-producing lateral strains.
The ring 7 projects inwardly of the shoulder and ensures the
permanent positioning of the magnetic circuit bearing along its
lower part.
The magnetic circuit does not adhere to the body of the injector
throughout its lateral surface,but only through the outer surface
of the enlarged lower end of the circuit. The outer surface engages
the upper surface of the ring 7. Thus, the longitudinal expansions
of the injector body and of the magnetic circuit are practically
independent. The reference points of the expansions of the body and
the circuit lies near the gap.
The recess in which the plate carrying the movable part and needle
11 and the recess formed in the vicinity of the injection port are
connected by a bore 14 formed in the nozzle 9. The injector is fed
with fuel through a pipe 13 of a small diameter allowing speeds of
progression which are generally above 1 m/ sec. The length and
diameter of the pipe 13 are selected so that upon opening of the
injector 1 and as a consequence of the phenomena of inertia of the
liquid and of the propagation of the wave inside the pipe, the
liquid reaches its speed corresponding to a continuous output only
at the end of the period during which the movable part or needle
rises and rebounds.
In the embodiment illustrated in FIG. 3,the pipe 13 is replaced by
an axial bore 13a extending through the stationary armature 5 and
communicating with the inside of the needle 11 through a bore 5b
formed in the projection 5a on the armature. The cross-section of
the bore 13a is substantiallyt the same as that of the pipe 13 so
that it is possible to obtain substantially the same effect of
inertia. However, the idle volume of the embodiment of FIG. 3 is
still more reduced since the recess in the plate 11a is no longer
in communication with the opening in the nozzle 9.
During the opening of the injector, the pressure in the injector
drops rapidly to a substantial extent so that the output is then
lower,if the amount of liquid stored elastically inside the
injector is small.
The throughput increases with time and the nominal output is
reached only at the end of the ballistic period during which the
movable section rises.
The output threshold is thus considerably lowered and the effects
of rebound are reduced to a minimum.
If the feed pressure varies speedily,for instance, by reason of
modifications in pressure ascribable to the action of the other
injectors, the mass of liquid carried in the pipe acts through its
inertia and limits the modifications in throughput produced by the
parasitic modulations in pressure.
In FIG. 4,there is illustrated the curve of fuel amounts injected
as a function of time. The solid line curve corresponds to the case
of an injector providing a maximum amount of fuel q for a duration
of the control signal of a predetermined value T2, but also
providing a minimum amount q which is too large for the engine
considered. By resorting to an injector according to the present
invention,it is possible to lower the curve as a whole so as to
obtain a minimum amount q min for a signal of a duration T1,
although in such a case only a lesser maximum amount q max is
obtained. With a slight increase in the injection pressure, it is
possible to increase the slope of the curve so as to obtain again
the desired maximum amount. It should be remarked that in all cases
the non-linear section of the curve between TO and T1 is entirely
unfit for use.
* * * * *