Technical Field
[0001] The invention relates to fuel injectors for delivering fuel into a combustion chamber
such as a cylinder of an internal combustion engine. It relates in particular, but
not exclusively, to fuel injectors including piezoelectric actuators used to control
movement of a needle in an injector valve.
Background of the Invention
[0002] The use of piezoelectric actuators is known as an alternative to solenoids for controlling
injections in a fuel injector. Typically, a stack of piezoelectric elements can be
arranged to control fuel pressure within an injector fuel chamber so as to consequentially
control the movement of an injector needle away from a valve seat so as to inject
fuel.
[0003] Known fuel injectors of the piezoelectric actuated type can be categorised into those
wherein a reduction of voltage across the piezoelectric stack initiates an injection
event, so called "de-energise to inject" type injectors, and those wherein an injection
event is initiated when voltage is increased across the piezoelectric element (stack),
so called "energise to inject" type injectors.
[0004] The "de-energise to inject" type actuators generally have a reduced piezoelectric
stack life compared to the "energise to inject" type actuators. Thus it is preferable
to actuate injection when the piezoelectric stack itself is actuated, i.e. becomes
elongated.
[0005] Piezoelectric actuators, typically positioned above a fuel injector nozzle, elongate
when energised. Such piezoelectric actuator elongation can be utilised to provide
injection in arrangements where the nozzle needle opens outwardly, such is the case
with many gasoline direct injection engines. In injectors for diesel engines, injector
needles are however adapted to move inwardly (retract) to release fuel. Thus, for
such injectors, an inverter arrangement is required between the actuator and the needle.
Mechanical inverters are known; however these have inherent disadvantages.
[0006] It is an object of the invention to overcome such disadvantages, and to provide for
an improved fuel injector of the "energise to inject type" actuator.
Summary of the Invention
[0007] In one aspect of the invention is provided a fuel injector including: piezoelectric
actuation means, a valve arrangement comprising a nozzle including a valve seat and
a valve needle, said needle adapted to be slidable within said nozzle so as to selectively
open and close the valve by respective disengagement/ engagement of the needle against
the seat to allow fuel from a pressurised source to be injected into a combustion
space, and hydraulic invertor means adapted such that activation/deactivation of said
piezoelectric activation means provides respective retraction/extension of said needle
away or to said valve seat so as to open/close the valve respectively.
[0008] The piezoelectric actuation means may include a piezoelectric element or stack of
elements.
[0009] The hydraulic invertor means may be adapted such that extension or elongation of
the piezoelectric element/stack causes retraction of said needle away from said valve
seat, and shortening of said piezoelectric element/stack causes said needle to extend
to said needle seat.
[0010] The hydraulic invertor portion may comprises: a first hydraulic chamber, and a first
piston located within said first hydraulic chamber, and adapted to move within said
first hydraulic chamber consequent to activation/deactivation of the piezoelectric
actuation means or extension/retraction of said piezoelectric element or stack of
elements, a second hydraulic chamber connected to said first hydraulic chamber via
a first conduit, and also connected to a pressurised fluid/fuel source via second
conduit, a second piston, adapted to be moveable within said second hydraulic chamber,
said piston generally located between said first and second conduits in said second
hydraulic chamber, so as to divide said second chamber into first and second volumes,
said second piston being connected to said needle, and arranged such that consequent
to said first piston moving in said first chamber, said second piston is adapted to
move in an opposite direction in said second chamber, so as to retract/extend said
needle from/to said seat on respective activation/deactivation of said actuation means.
[0011] The second piston may be attached to or be integral with the proximal portion of
said valve needle.
[0012] The first piston may be adapted to move within said first chamber from a force provided
by extension of piezoelectric stack/activation of piezoelectric actuator so as to
force fluid via said first conduit to said first volume of said second chamber, consequentially
increasing pressure therein so as to move said second piston against the pressure
from said pressurised fuel source and consequentially retract said valve needle from
said valve seat.
[0013] The fuel injector may be adapted such that deactivation of piezoelectric actuator/retraction
of piezoelectric stack causes a reduction in force acting on said first piston so
as to reduce pressure in the first chamber and, by means of said first conduit connecting
said chambers, a consequential reduction in pressure in said first volume, so as to
move said second piston in a direction towards the first conduit connection by pressure
from said pressurised fuel source, and consequently force the valve needle onto said
valve seat to close said valve.
[0014] The hydraulic invertor means may be located within a generally cylindrical sleeve.
[0015] The sleeve may be part of the actuator housing which encloses the piezoelectric stack
or element.
[0016] The first fluid conduit may be provided by an insert, locatable or located within
said sleeve.
[0017] The fuel injector may include first and/or second spring means to urge said first
and/or second piston towards the piezoelectric stack/ valve tip region respectively.
[0018] The first and second chambers may be separated by a common wall.
[0019] The piston(s) include sealing rings and/or grooves.
[0020] The pressurised fuel source may be a fuel rail, fuel accumulator volume and/or a
pressurised fuel source which is common to the fuel supply for injection in the injector.
Brief Description of the Drawings
[0021] The present invention will now be described, by way of example, with reference to
the accompanying drawings, in which:
Figure 1 shows a schematic cross-section of a simple embodiment of the invention.
Figure 2 shows a cross-section through a fuel injector according to one example which
includes a hydraulic invertor mechanism.
Figures 3, 4a and4 b show partial cross-sectional views of a tip portion of a fuel
injector according to examples.
Figures 5a and b shows similar embodiments of hydraulic invertor mechanisms according
to examples.
Figure 6 shows an alternative embodiment of hydraulic invertor mechanism according
to an alternative example.
Description of the Preferred Embodiments
[0022] Figure 1 shows schematically a simple embodiment of the invention, showing a sectional
schematic portion of a fuel injector 1. A portion of the fuel injector/actuator housing
forms a generally hollow cylindrical, sleeve type arrangement 2. Within the sleeve/housing
are formed two chambers; a first (upper) chamber 3 and a second (lower) chamber, designated
by reference numeral 4a and 4b. These chambers are separated by a plug 5 shown in
the figure as being formed integrally within the injector housing sleeve. In practical
embodiments the invertor mechanism may be provided as an insert of e.g. a general
sleeve construction defining the chambers and separating wall, as will be described
in more detail below.
[0023] A first piston or plunger element 6 is also located within the first chamber and
adapted to move within the first chamber as a result of fluid pressure within the
first chamber in one direction, and the applied force (in the opposite direction)
from a piezoelectric stack 7 arranged so as to contact the piston element on the other
(upper) side.
[0024] The figure shows the top (proximal) portion of a fuel injector needle 8, which is
slidably located within the lower chamber. At this end of the needle is a widened
portion, which may alternatively be formed of an attachment rather than being integral
with the needle, and which is so adapted to form a further plunger/piston 9, susceptible
to movement as a result of differential fluidic pressures between the lower and upper
regions/volumes (4a, 4b) of the second chamber, either side of piston 9. In the figure,
only the top portion of the fuel injection needle is shown; the distal end of the
needle includes a needle tip portion which is adapted to engage on a valve seat, located
at the distal extremity (nozzle portion) of the valve body. Upward movement of the
needle away from the valve seat allows injection of fuel into a combustion space such
as a cylinder in a conventional manner. Fuel is supplied for injection via means such
as one or more supply conduits and fuel chambers formed adjacent to, or located in
an injector housing. Such fuel supply conduit arrangements are well known in the art
and will not be described in detail hereinafter, suffice to say that any such arrangement
can be utilised in conjunction with the invention.
[0025] The upper region of the second chamber includes a fluidic connection 10 to, for example,
a fuel source such as a fuel pressure rail; this may be manifested as a bore or other
suitable conduit. The first and second chambers are connected fluidly by means of
further conduit, such as a bore 11. This may be formed integral with the injector/actuator
sleeve. Alternatively, the conduit/bore may be provided as an insert to overcome practical
difficulties encountered when manufacturing a bore within the injector housing.
[0026] In operation, electrical actuation of the piezoelectric stack will cause elongation
thereof, such that it contacts and forces the piston/plunger element 6 downwards against
fluid pressure in the first chamber. This results in high pressure in the first chamber,
this pressure being higher than the fuel rail pressure, such that fluid (fuel) is
forced, via conduit 11, from the first chamber into the lower portion of the second
chamber, increasing the pressure therein, and consequentially urging the valve needle
to move upwards against the lower pressure in the upper region (volume) of the lower
chamber, the fluid therein can exit via bore 10. As a result the valve needle tip
is lifted upwardly away (i.e. retracted) from the valve seat, allowing fuel to be
injected into a combustion chamber.
[0027] Deactivation of the piezoelectric element allows a reduction in the pressure in the
first chamber, and via the conduit 11, a consequent reduction in pressure in the lower
region (volume) of the second chamber. The higher pressure in the upper region (volume)
of the lower chamber provided from e.g. pressurised fuel volume such as a fuel rail,
acts against the piston formed at the one end of the valve needle, so as to move the
needle downwards until the tip engages with the seat to close the valve and stop fuel
flow.
[0028] Figure 2 shows a sectional view of a practical fuel injector 12 according to one
aspect. Within an actuator housing 13 is located a piezoelectric actuator 14 including
a stack of piezoelectric elements. The stack is supplied by an electrical connection
means 15 towards the top of the housing.
[0029] The lower portion of the injector includes a nozzle body 16, within which core is
located a valve needle 17, shaped to form a sliding fit within the nozzle body, and
moveable along a vertical axis so as to open and close the valve by selective engagement/disengagement
with a valve seat 21. The nozzle body is located onto the actuator housing by means
of nut 19. The valve needle is slidable within a bore provided within an injector
nozzle body. The valve needle includes a needle tip region 20, which is engageable
with a valve (needle) seat 21 at one end of nozzle body so as to control fuel injection
to a combustion space by selective closing and opening of an orifice formed between
the needle tip and the valve seat. Fuel is supplied to the needle tip region by annular
bores 22 or other type of conduits, from a widened recess volume 23 within the nozzle
body, and fuel supplied to this volume by further conduit means (not shown).
[0030] Between one end of the piezoelectric stack and proximal end of the needle is located
a hydraulic inverter unit 24 which will be explained in more detail below. An intermediate
element 27 may be located between the distal end of the piezoelectric element (stack)
and the inverter unit
[0031] The piezoelectric actuator is selectively operable, via the hydraulic inverter unit,
to control movement of the valve needle between a non-injecting position, in which
it is seated against the valve needle seat and an injecting position in which the
valve needle is lifted away from the valve needle seat, and furthermore such that
actuation of the piezoelectric stack causes the needle to lift away (upwardly) so
as to retract it from the valve seat.
[0032] Figure 3 shows cross-sectional view showing the tip portion of the fuel injector
according to an embodiment in more detail, in order to show the location of the hydraulic
invertor unit; similar components have like reference numerals. Likewise figures 4a
and b show cross-sectional views of the tip portion elements of the fuel injector
according to examples, specifically showing the nozzle portion and adjacent hydraulic
invertor unit; in these figures the components would be attached/fitted to a main
actuator body.
[0033] The nozzle body may be provided with a bore 25 which may define a first upper delivery
chamber for receiving fuel under high pressure and a second lowed delivery chamber
22 for fuel. Towards the distal end 26 of the internal surface of the bore is of frusto-conical
form so as to define a valve seating surface. The arrangement of the fuel supply conduits,
bores and fuel chamber is such that vertical movement of the injector needle acts
to open and close the injector valve by successively lifting the needle tip away from
the seat to allow fuel to be injected into a combustion chamber under pressure before
closing the valve and cutting fuel flow by the needle tip closing (re-engaging on
the seat). As mentioned, various arrangements are known in the art of mechanisms and
designs which control the flow and pressure of fuel for injection and will not be
detailed here, suffice to say that the invention can be used in conjunction with any
such designs. Fuel is supplied to the injector from a high pressure fuel source such
as from a common rail or accumulator volume, and flows through conduit(s) formed,
for example, between the actuator housing and hydraulic invertor housing/nozzle body
to a nozzle supply chamber formed by a widened portion of the bore in the upper region
of the nozzle body.
[0034] Located within the actuator housing is a piezoelectric stack 14. The inverter unit
24 is located generally between an actuator (piezoelectric stack) and the nozzle body
19. Again an injection needle 17 is slidably located within a bore formed in a nozzle
body. The nozzle body may be attached to actuator housing via a nut which also forms
a sleeve. Alternatively as shown in figure 3b and c, the nozzle body may be attachable/attached
directly to the actuator housing without the use of a nut. In alternative arrangements
the nozzle body may be attached to one end of the inverter unit, particularly if the
inverter unit not located within the actuator housing.
[0035] The inverter unit can be provided as an insert having a housing of sleeve construction
incorporating the elements of the invertor; this is may be insertable or located within
the actuator housing. Alternatively elements of the invertor unit are located within
the fuel injector (e.g. within the actuator housing without a separate inverter sleeve).
Thus the hydraulic invertor housing and in some examples also the injector nozzle
body, are located within an overall actuator housing. The hydraulic invertor unit
may be contained in a sleeve which may be provided separate to, or integral with,
the actuator housing Specifically the hydraulic invertor unit is adapted and configured
such that extension (elongation of the stack) causes upward movement of the injector
needle, and conversely retraction of the stack causes downward movement of the needle.
Examples of the hydraulic actuator unit for actuating the needle in conjunction with
the piezoelectric stack is shown and described in more detail in figures 5 and 6.
[0036] Figure 5a and 5b show similar embodiments of the hydraulic invertor unit in more
detail, also showing a portion of the actuator housing 13 in which it is located.
The hydraulic invertor unit includes a first cup-formed hollow cylindrical member
28 which is closed at one end by a wall 29 of the member 28; the opposite (piezoelectric
stack) end is open-ended. Within this is located a piston 30, which is urged by spring
means 36 away from the wall end, so as to form a first hydraulic chamber 38. The exterior
face of the piston abuts (i.e. is in contact with) the end of the piezoelectric stack
14 or an intermediate member (intermediate between the exterior piston face and the
distal end of the piezoelectric stack). A first sleeve member 31 which includes an
internal annular ridge 32 may be provided for location within the actuator inner sleeve
and to locate the cup member. In addition, the annular ridge locates a further second
sleeve member 33 which is of hollow cylindrical form. In alternative embodiment of
figure 5b, the first and second sleeve members may be integrally formed.
[0037] Within the second sleeve member is located a second piston 34 so as to define as
second hydraulic chamber 39 bounded by the second sleeve member, piston and exterior
face of the cup member. Second spring means 37 are located within this chamber so
as to urge the second piston away from the exterior face of the cup member. The second
piston is attachable/attached to the proximal end of the nozzle needle 17or alternatively
is integral with it.
[0038] The first hydraulic chamber is fluidly connected to the lower region (volume) 41
of the second chamber by a fluid path/conduit (not shown). The second hydraulic chamber
39 can be regarded as comprising a first (upper) volume 40 bounded by the wall, second
sleeve and top face of the piston and a second lower volume 41, bounded by the bottom
face of the piston, second sleeve and the and bottom face of the piston. Differential
pressures in the first and second volumes will cause a corresponding force on the
piston and so as to consequently slidably move the needle 17 upwards or downwards,
that is to say from and to an open/closed (retracted/extended) position. The upper
portion of the second hydraulic chamber is connected to a pressurised supply of fuel.
[0039] When a voltage is applied across the stack from an external voltage source, the stack
length will increase, and as a result one end of the stack pushes against a first
piston member portion of the hydraulic inverter unit, causing pressurisation in the
upper chamber of the unit, and causing fluid (such as fuel) therein to be forced via
first conduit into the lower region of lower chamber, increasing the pressure therein,
and causing a piston member located at the top end of the needle located in the second
chamber to move upwards, causing upward vertical movement of the needle. The piezoelectric
stack may be surrounded by a sleeve and include an end piece. In any case, the end
piece or a surface of the sleeve abuts (i.e. is in contact with) the first piston
member.
[0040] Figure 6 shows an alternative embodiment similar to the figure 5 embodiment, showing
alternative design of hydraulic inverter unit. The hydraulic inverter unit 24 is shown
on its own and can be provided as a unit locatable by e.g. insertion within a fuel
injector, e.g. within the inner sleeve of the actuator housing. However in alternative
embodiments the unit may be attached to the end of the actuator housing rather than
located within it; in any case the invertor unit is generally located between the
distal end of the piezoelectric actuator element (stack) and the proximal portion
of the needle/nozzle body.
[0041] The unit includes a generally hollow cylindrical (outer) sleeve housing 42. The housing
is separated into two (first and second) hydraulic chambers 38, 39, by a wall 29 of
a cup shaped portion including inner sleeve 33, generally forms the second hydraulic
chamber. Located within the (upper) first hydraulic chamber 38 is a first piston 30,
urged away from the proximal face of the wall by spring means 36 to provide the volume
of the chamber. The exterior face of the piston abuts (i.e. is in contact with) the
end of the piezoelectric stack or alternatively an intermediate member (which is intermediate
between the face and the distal end of the piezoelectric stack).
[0042] The sleeve 33 also defines a second hydraulic chamber 39, A second piston 34, connectable
to (or integral with) the proximal end of the nozzle needle (not shown) divides the
second hydraulic chamber into a first and second volumes 40,41. The lower volume of
the first hydraulic chamber is fluidly connected to the lower volume 41 of the second
chamber (the lower volume being bounded by the distal face of the wall, sleeve and
the top face of the needle) by a conduit 45. This conduit may be formed by a bore
in the sleeve member, or alternatively by an insert. On the outer perimeter of the
sleeve is located a collar member for appropriate location/retention within the actuator
housing. The upper (first) volume 40 of the second chamber is fluidly connected to
a pressurised fuel source via orifice 46.
[0043] The following will now describe the operation of the above described examples. To
provide injection, the piezoelectric stack is energized and this may be initiated
via a command signal from the Electronic Control Unit of a vehicle. Extension of the
piezoelectric element/stack pushes (or causes the intermediate member to push) against
piston 30 so as to force the piston downwards, decreasing the volume in the first
hydraulic chamber 38, and consequentially increasing the pressure therein. This causes
fluid (fuel) to move through the conduit 45 (joining the two hydraulic chambers) causing
an increase in pressure in the lower volume 41 of the second chamber. The needle shaft
17 is urged upwards due to a higher pressure in the lower volume 41 of the second
hydraulic chamber than in the upper volume 40 thereof, wherein fuel can exits the
upper volume of the second hydraulic chamber to a pressurised fuel source. Lifting
of the needle away from the nozzle seat allows fuel to be injected. Conversely to
close the valve, the piezoelectric stack is de-energized. This reduces the downward
force on the first piston and with the assistance of the first spring means, allows
the first piston to move upwards, thus reducing the pressure in the first hydraulic
chamber. As a consequence of fluid flowing though the connecting conduit between the
two hydraulic chamber, the pressure in the lower volume of the second hydraulic chamber
is consequentially reduced. The pressure in the upper volume of the second chamber
provided by the pressurized fuel source becomes higher than the reduced pressure on
the lower volume, causes a downward force on the second piston (with the assistance
of downward force from the second spring means), and hence pushes the needle downwards
so as to close the valve by engaging the needle tip to the valve (nozzle) seat.
1. A fuel injector including:
piezoelectric actuation means,
a valve arrangement comprising a nozzle including a valve seat and a valve needle,
said needle adapted to be slidable within said nozzle so as to selectively open and
close the valve by respective disengagement/ engagement of the needle against the
seat to allow fuel from a pressurised source to be injected into a combustion space,
and
hydraulic invertor means adapted such that activation/deactivation of said piezoelectric
activation means provides respective retraction/extension of said needle away or to
said valve seat so as to open/close the valve respectively.
2. A fuel injector as claimed in claim 1 wherein said piezoelectric actuation means includes
a piezoelectric element or stack of elements.
3. A fuel injector as claimed in claim 2 wherein said hydraulic invertor means is adapted
such that extension or elongation of the piezoelectric element/stack causes retraction
of said needle away from said valve seat, and shortening of said piezoelectric element/stack
causes said needle to extend to said needle seat.
4. A fuel injector as claimed in claims 1 to 3 wherein said hydraulic invertor portion
comprises:
a first hydraulic chamber, and
a first piston located within said first hydraulic chamber, and adapted to move within
said first hydraulic chamber consequent to activation/deactivation of the piezoelectric
actuation means or
extension/retraction of said piezoelectric element or stack of elements.
a second hydraulic chamber connected to said first hydraulic chamber via a first conduit,
and
also connected to a pressurised fluid/fuel source via second conduit,
a second piston, adapted to be moveable within said second hydraulic chamber, said
piston generally located between said first and second conduits in said second hydraulic
chamber, so as to divide said second chamber into first and second volumes, said second
piston being connected to said needle, and arranged such that consequent to said first
piston moving in said first chamber, said second piston is adapted to move in an opposite
direction in said second chamber, so as to retract/extend said needle from/to said
seat on respective activation/deactivation of said actuation means.
5. A fuel injector as claimed in wherein said second piston is attached to or integral
with the proximal portion of said valve needle.
6. A fuel injector as claimed in claims 4 or 5 wherein said first piston is adapted to
move within said first chamber from a force provided by extension of piezoelectric
stack/activation of piezoelectric actuator so as to force fluid via said first conduit
to said first volume of said second chamber, consequentially increasing pressure therein
so as to move said second piston against the pressure from said pressurised fuel source
and consequentially retract said valve needle from said valve seat.
7. A fuel injector as claimed in claims 4 to 6 adapted such that deactivation of piezoelectric
actuator/retraction of piezoelectric stack causes a reduction in force acting on said
first piston so as to reduce pressure in the first chamber and, by means of said first
conduit connecting said chambers, a consequential reduction in pressure in said first
volume, so as to move said second piston in a direction towards the first conduit
connection by pressure from said pressurised fuel source, and consequently force the
valve needle onto said valve seat to close said valve.
8. A fuel injector as claimed in claims 1 to 7 wherein said hydraulic invertor means
is located within a generally cylindrical sleeve.
9. A fuel injector as claimed in claims 1 to 8 wherein said sleeve is part of the actuator
housing which encloses the piezoelectric stack or element.
10. A fuel injector as claimed in claims 1 to 9 wherein said first fluid conduit is provided
by an insert, locatable or located within said sleeve.
11. A fuel injector as claimed in claims 1 to 10 including first and/or second spring
means to urge said first and/or second piston towards the piezoelectric stack/ valve
tip region respectively.
12. A fuel injector as claimed in claims 1 to 11 wherein said first and second chambers
are separated by a common wall.
13. A fuel injector as claimed in any previous claim wherein said piston(s) include sealing
rings and/or grooves.
14. A fuel injector as claimed in any previous claim wherein said pressurised fuel source
is a fuel rail, fuel accumulator volume and/or a pressurised fuel source which is
common to the fuel supply for injection in the injector.