[0001] This invention relates to a fuel injector for supplying fuel to a cylinder of an
internal combustion engine, particularly an electronic unit injector (EUI) which incorporates
an electromagnetically operated spill valve operation of which is controlled electronically
to control the delivery of fuel to the cylinder.
[0002] Conventionally an EUI incorporates a pumping mechanism which is supplied with fuel
at a relatively low pressure (feed pressure) from a feed rail of the injection system,
the pump greatly increasing the fuel pressure for injection purposes. Opening and
closing of the spill valve controls operation of the injector by controlling the application
to the injector of the pressure generated by the pump. Fuel under pressure dumped
when the spill valve opens is returned to the feed rail. Fuel leaking internally within
the injector in use is returned via a drain line to the fuel reservoir.
[0003] The moveable valve member of the spill valve is moved against the action of a return
spring by an armature of an electromagnet, the armature being moved within an armature
chamber of the electromagnet housing by energization of the electromagnet. It is known
to effect either closing, or opening, of the spill valve as a result of energization
of the electromagnet. Both ends of the range of movement of the moveable valve member
of the spill valve are determined by mechanical stops and it is recognised that rapid
movement, followed by rapid arrest, of the valve member can result in an undesirable
bounce of the valve member of the spill valve. Thus either the spill valve may bounce
when closing to give a transient second opening prior to full closure, or upon opening
may bounce to give a transient second partial closure before full opening. Bouncing
of the spill valve at the ends of its operating stroke, notably the closed end, is
a known problem giving rise to inefficient, uncontrolled operation of the injector,
and the mitigation or obviation of this problem is an object of the present invention.
[0004] Fuel returned to the feed rail from the spill valve is hotter than the fuel in the
feed rail and thus raises the fuel rail temperature undesirably. It is known to provide
a bypass flow of fuel from the fuel feed rail of the injection system which passes
through the electromagnet armature chamber back to the low pressure reservoir, thus
continually causing a flow of cool fuel from the reservoir through the feed rail to
balance the heating effect of fuel dumped via the spill valve and so stabilize the
temperature of the system.
[0005] In accordance with the present invention there is provided a fuel injector incorporating
an electromagnetically operated spill valve, the armature of the electromagnet being
moveable within an armature chamber through which fuel flows in use, and means controlling
the flow of fuel through said chamber so that the pressure of fuel within said chamber
is such that at least one of the opening and closing bounce of the armature and associated
spill valve is mitigated.
[0006] Preferably said means comprises a first flow restrictor in the fuel inlet to said
chamber, and a second flow restrictor in the fuel outlet from said chamber, the values
of the restrictions to flow formed by said first and second restrictors being chosen
in relation to the system feed and drain pressures and the flow characteristics of
the chamber, such that the fuel pressure in the chamber reduces the possibility of
armature and associated valve bounce at the open and/or closed limits of the spill
valve movement.
[0007] The invention also resides in a method of manufacturing a fuel injector of the kind
specified hereinbefore including the steps of selecting armature chamber inlet and
outlet flow restrictors to achieve a predetermined fuel pressure within the armature
chamber to minimize the possibility of armature/spill valve bounce.
[0008] One example of the invention will now be described in more detail with reference
to the accompanying drawing which is a diagrammatic representation of an electronically
controlled unit fuel injector.
[0009] Referring to the drawing, the injector includes a needle valve 10 biased into engagement
with a seating (not shown) by a spring 12. The injector includes a pumping chamber
14 which receives fuel from a low pressure fuel feed rail 20 and which communicates
with the needle valve 10 through a passageway 16 in known manner, whereby fuel under
pressure can be applied to the needle 10 to lift the needle 10 from its seating to
open the injector. A spill valve 18 incorporated within or mounted upon the injector
assembly communicates with the passage 16, and when open, connects the passage 16
to the feed rail 20 to dump high pressure fuel back into the fuel feed rail.
[0010] The feed rail 20 supplying pumping chamber 14 with fuel at relatively low pressure
(feed pressure), may be common to all of the injectors of an engine and supplies fuel
from the fuel reservoir to the injectors. The pumping mechanism 14a of the injector
is mechanically operated, and displaces fuel from the pumping chamber 14 into the
passage 16. If the spill valve 18 is open then hot high pressure fuel pumped from
the chamber 14 passes back to the rail 20. Closure of the spill valve 18 allows the
pump to further pressurize the fuel in the chamber 14 and passage 16, resulting in
the fuel pressure applied to the valve needle 10 increasing. At a predetermined pressure
in the passage 16 the needle 10 lifts against the action of the spring 12 allowing
fuel to be delivered past the seating and into the cylinder of the engine. Opening
of the spill valve 18 dumps the pressure in the passage 16 thus permitting the spring
12 to restore the needle 10 to the valve seating terminating fuel injection. The pressure
of fuel within the chamber 32 affects the intensity with which the pressure is re-established
in the region between the armature plate 28 and the stator of the actuator at the
instant after spill valve closure. The higher the chamber pressure, the more vigorous
the disturbing force applied to the armature end of the valve, and the larger the
bounce. Consequently reducing the armature chamber pressure reduces the magnitude
of the bounce, up to a point.
[0011] The operating spool 22 of the spill valve 18 is linked by a pushrod 24 (depicted
diagrammatically in the drawing) to an armature plate 28 of an electromagnetic actuator
26. The armature plate 28 is in the form of a rectangular plate moveable transverse
to its plane within an armature chamber 32 defined in the casing 30 of the actuator
26. Energization of the winding 34 of the electromagnet moves the armature plate 28
axially to the position illustrated in the drawing wherein it is closely adjacent
the E-shaped core 36 of the electromagnet, and the spill valve is closed. De-energization
of the winding 34 allows the armature plate 28 to be moved under the action of a valve
spool return spring 29 to the opposite end of its travel wherein a stop means in the
form of a shim 31 abuts the casing 30, and the spill valve is open.
[0012] The armature chamber 32 is formed, adjacent one edge with a fuel inlet 38 which is
connected through a line 40 to the feed rail 20, and a fuel outlet 42 generally opposite
the inlet 38. The outlet 42 communicates with the fuel reservoir by way of a drain
line 44 connecting the outlet 42 to the fuel drain.
[0013] The feed rail pressure is significantly in excess of the drain line pressure and
thus fuel flows continually in a bypass path including the chamber 32 drawing cool
fuel from the reservoir into the rail to balance the heating effect of hot fuel dumped
into the rail by the spill valve.
[0014] The chamber 32 is thus continually full of fuel at a pressure between feed pressure
and drain pressure. A gap between the wall of the chamber 32 and the periphery of
the armature plate 28 permits fuel to flow around the armature plate 28 as the armature
plate moves within the chamber 32 in use. However, it has now been determined that
the pressure of the fuel within the chamber 32 is of significance in relation to minimizing
bounce of the plate 28, and thus the spool 22 of the spill valve at the ends of their
travel.
[0015] It will be recognised that the spill valve depicted in the drawing is most critical
to bounce at its closed position since there is a degree of latitude in the fully
open position of the spill valve. It can be seen that the spool 22, in the closed
position engages a seating 22
a in the spill valve body fractionally in advance of the plate 32 engaging the core
36, and bounce from this closed position, as the closed position is achieved, will
give a momentary second opening of the spill valve with disadvantageous effects on
the fuel delivery characteristic of the injector. It must be recognised that the drawing
is highly diagrammatic and in practice there is a direct link between the plate 28
and the valve spool 22.
[0016] It has been determined that for a given design and application of the injector and
a given design of spill valve/electromagnet, certain pressure conditions within the
chamber 32 will minimize armature/spill valve bounce. The relevant pressure will dependent
inter alia upon the application, and the design of the plate 28 and chamber 32, but can be determined
by experiment.
[0017] Once the desired pressure within the chamber 32 has been determined it can be achieved,
by selecting appropriately sized flow restrictors 46 and 48 in the lines 40 and 44
respectively to provide, on the basis of the pressure difference between the feed
line 20 and fuel drain, the desired flow rate of fuel through the chamber 32 for appropriate
cooling, while at the same time maintaining the optimum pressure in the chamber 32
to minimize armature plate, and therefore valve spool, bounce.
[0018] In one example the fuel has a density of 760 kg/m
3 at 100°C. The feed rail pressure is normally 7 bar but experiences pressure "spikes"
when the spill valve dumps high pressure fuel into the rail. The drain line pressure
is 1 bar and a fuel flow rate of 17 litre/hour through the chamber 32 is required
for rail cooling. It has been found in this particular application that the optimum
pressure in the chamber for bounce suppression is 2 bar and to achieve this pressure
the approximate diameters of the restrictor orifices 46 and 48 are 0.5 mm and 0.7
mm respectively.
1. A fuel injector incorporating an electromagnetically operated spill valve (18), the
armature (28) of the electromagnet being moveable within an armature chamber (32)
through which fuel flows in use, and means controlling the flow of fuel through said
chamber (32) so that the pressure of fuel within said chamber (32) is such that at
least one of the opening and closing bounce of the armature (28) and associated spill
valve (18) is mitigated.
2. A fuel injector as claimed in Claim 1, wherein said means comprises a first flow restrictor
(46) in the fuel inlet to said chamber (32), and a second flow restrictor (48) in
the fuel outlet from said chamber (32), the values of the restrictions to fuel flow
formed by said first and second restrictors (46, 48) being chosen in relation to the
system feed and drain pressures and the flow characteristics of the chamber (32),
such that the fuel pressure in the chamber reduces the possibility of armature and
associated valve bounce at the open and/or closed limits of the spill valve movement.
3. A fuel injector as claimed in Claim 2, wherein the first and second flow restrictors
(46, 48) are defined by orifices of diameter 0.5 mm and 0.7 mm respectively.
4. A fuel injector as claimed in any one of the preceding claims, wherein the fuel pressure
within the chamber (32) is approximately 2 bar.
5. A fuel injector as claimed in any one of the preceding claims, wherein the means controls
the fuel flow rate, holding the rate at approximately 17 litre/hour.
6. A method of manufacturing a fuel injector incorporating an electromagnetically operated
spill valve (18), the armature (28) of the electromagnet being moveable within an
armature chamber (32) through which fuel flows in use, and means controlling the flow
of fuel through said chamber (32) so that the pressure of fuel within said chamber
(32) is such that at least one of the opening and closing bounce of the armature (28)
and associated spill valve (18) is mitigated, said means comprising a first flow restrictor
(46) in the fuel inlet to said chamber (32), and a second flow restrictor (48) in
the fuel outlet from said chamber (32), the method including the steps of selecting
the size of the first and second flow restrictors (46, 48) to achieve a predetermined
fuel pressure within the chamber (32) to reduce the possibility of armature and associated
spill valve bounce.