[0001] This invention relates to a pump assembly and, in particular, to a pump assembly
for use in compression ignition engines.
[0002] Known fuel injection systems for supplying fuel to the cylinders of a compression
ignition engine include a fuel injection pump, or pump assembly, for generating injection
pressure and for delivering fuel at injection pressure to the injection nozzles of
the system via high-pressure fuel lines.
[0003] In one type of fuel injection system, known as the unit injector, a pump assembly
and a dedicated injection nozzle are arranged together within a common unit. The unit
injector is usually driven by a camshaft run off the engine via a cam drive arrangement.
[0004] Figure 1 is an example of a known unit injector design, in which a plunger 2 reciprocates
within a plunger bore 4 formed in a plunger housing or barrel 6. A pump or compression
chamber 8 is defined by an end face 10 of the plunger 2 and the blind end of the plunger
bore 4. A valve needle 12 of an injection nozzle 14 is responsive to the pressure
of fuel supplied from the pump chamber 8 to the nozzle 14 and is biased closed against
a valve needle seat 16 by means of a spring 18. In this particular unit injector the
spring 18 acts on the valve needle 12 through a rocker arm 20, although other unit
injector designs have the spring 18 axially aligned with the needle 12 at its pump
chamber end.
[0005] First and second ports, 22 and 24 respectively, are provided in the plunger barrel
6 to provide a flow path for fuel into and out of the pump chamber 8 from a low pressure
source 26 (via a storage space 28), depending on the position of the plunger 2 within
its bore 4.
[0006] The plunger 2 is provided with a slot formation including two slots which are cut
into its outer surface: a first longitudinal slot (not visible in Figure 1) which
cuts through the end face 10 of the plunger 2 (referred to as a "stop slot"), and
a second helical slot 30 which is cut at an angle to the stop slot and is arranged
to communicate at one end with the stop slot.
[0007] The plunger 2 is driven by a cam drive to perform a pumping cycle during which fuel
within the chamber 8 is pressurised to initiate an injection event and subsequently
depressurised to terminate injection. The provision of the helical groove 30 is the
means by which the quantity of fuel injected is controlled. During a forward stroke
of the plunger (from bottom-dead-centre (BDC) to top-dead-centre (TDC)), pressurisation
of fuel within the chamber 8 occurs when the plunger 2 has closed both ports 22, 24
and up until the point at which the edge of the helical groove 30 aligns with the
second port 24 to permit fuel to escape to low pressure. As fuel within the pump chamber
8 is pressurised, the valve needle 12 is caused to lift from its seating 16 to commence
injection. At the point at which the edge of the helical groove is aligned with the
port 24, the pressure of fuel within the pump chamber 8 decays rapidly as fuel escapes
through the helical groove 30 and the port 24 to low pressure, thereby causing the
valve needle 12 to re-seat to terminate injection. The rate of pressure collapse in
the pump chamber 8 at termination of injection is relatively rapid, and so the valve
needle 12 is caused to seat quickly.
[0008] For some applications it is desirable for the rate of pressure collapse to be reduced
or controlled carefully. In a modification of the unit injector in Figure 1, it is
known to provide an additional spring-biased plate valve for this purpose. The plate
valve is provided with a restricted orifice and is housed within an adapter plate
located between the barrel 6 and the associated nozzle 14 (referring to Figure 1),
within the high pressure connection between the pump chamber 8 and the nozzle 14.
Upon termination of injection (i.e. with fuel pressure within the pump chamber decreasing),
the plate valve is urged against its seating and the rate at which fuel can flow from
the nozzle to low pressure is restricted by the orifice to reduce the rate of pressure
collapse in the pump chamber. This is a satisfactory solution for some applications,
although the requirement for additional moving parts (the plate valve and associated
spring) adds cost and complexity to the unit. To some extent, the plate valve also
influences initiation of injection as the closing force of the plate valve spring
must be overcome before an unrestricted flow of high pressure fuel is able to flow
to the nozzle.
[0009] It is with a view to providing improvements to the above-mentioned prior art that
the following is presented.
[0010] According to a first aspect of the invention, there is provided a pump assembly for
use in a compression ignition engine, the pump assembly comprising:
a plunger which is reciprocal within a plunger housing, in use, to pressurise fuel
within a compression chamber,
a first flow path providing communication between the compression chamber and a low
pressure circuit to permit filling of the compression chamber, and being closed to
fuel flow to initiate pressurisation of fuel within the compression chamber,
a second flow path providing communication between the compression chamber and the
low pressure circuit, and being open to fuel flow to terminate pressurisation of fuel
within the compression chamber after closure of the first flow path,
wherein the second flow path is provided with flow restriction means to restrict
the rate of flow of fuel to the low pressure circuit at the end of pressurisation.
[0011] Where the pump assembly is of the type for supplying pressurised fuel to an injection
nozzle to initiate injection, the invention provides the advantage that the rate of
pressure collapse within the pump chamber to terminate injection is reduced. The valve
needle of the nozzle therefore experiences a cushioning effect as it seats, reducing
wear and prolonging service life. The effects of gas blow-by are also reduced. It
is a particular advantage that the invention achieves these benefits without the requirement
to provide additional or moving parts in known pump assembly designs, such as unit
injectors or unit pumps.
[0012] A further beneficial feature of the invention is that the supply of high pressure
fuel to the associated nozzle is not affected by the provision of the flow restriction
means, which only influences the rate of depressurisation of the compression chamber.
Thus, a passage for high pressure fuel between the compression chamber and the nozzle
is provided which permits fuel flow to and from an associated injection nozzle at
a substantially unrestricted rate.
[0013] In one preferred embodiment, for example, the second flow path is at least partially
provided in a portion of the plunger housing itself and the flow restriction means
is provided within said portion of the plunger housing.
[0014] Alternatively, the second flow path may be at least partially provided in a portion
of the plunger and the flow restriction means is provided within said portion of the
plunger.
[0015] Advantageously, said portion of the second flow path may include a passageway or
drilling along an axis substantially parallel to a first longitudinal axis of the
plunger, and said flow restriction means is provided along this passageway.
[0016] Alternatively, said portion of the second flow path may include a passageway or drilling
along an axis substantially perpendicular or transverse to the longitudinal axis of
the plunger, and said flow restriction means is provided along this passageway.
[0017] It is preferable that the plunger housing comprises a plunger bore within which the
plunger is reciprocable, with plunger motion being guided directly by an inner wall
of the plunger bore.
[0018] Advantageously, the first flow path comprises a filling port provided in the housing
and opening to the plunger bore.
[0019] The second flow path may include a second port provided in the plunger housing and
opening to the plunger bore, wherein the second port is provided with the flow restriction
means (as mentioned above).
[0020] In one embodiment, the pump assembly is a fuel pump (for example, a unit pump) for
supplying pressurised fuel to a dedicated injector remote from the pump assembly,
in use.
[0021] Alternatively, the pump assembly may be a unit injector, also comprising an injector
arranged within a common unit with the pump assembly.
[0022] A second aspect of the invention relates to a plunger suitable for use with any of
the aforementioned pump assemblies, characterised in that the plunger comprises a
passageway along which is provided said flow restriction means.
[0023] In this context, the pump assembly unit of the invention may be incorporated into
a unit pump, in which a dedicated injector is arranged remote from the pump assembly,
a unit injector where the pump assembly and dedicated injector/injection nozzle are
arranged in a common housing to form a single unit or any other kind of pump unit
for supplying pressurised fuel to a dedicated injection nozzle/injector.
[0024] It will therefore be appreciated that the phrase "unit pump assembly" is intended
to include reference to unit pumps and unit injectors, and the like.
[0025] The present invention is now described with reference to the accompanying figures
wherein:
Figure 1 is a schematic view of a known unit injector;
Figure 2 is a sectional view of a unit injector according to a first embodiment of
the invention; and
Figure 3 is a detailed view of part of the unit injector mechanism shown in Figure
2.
[0026] Referring to Figures 2 and 3, a pump assembly of one embodiment of the present invention
takes the form of a unit injector having many similar features to the prior art unit
injector described previously. Where possible, similar parts to those shown in Figure
1 will be referred to with like reference numerals.
[0027] The plunger 2 is reciprocal within a plunger bore 4 provided in a plunger housing
or barrel 6, with the plunger end face 10 defining the pump or compression chamber
8 at the blind end of the bore 4. The associated injection nozzle 14 includes a valve
needle 12 provided with thrust surfaces (not identified), which are exposed to fuel
pressure within a delivery chamber 32 defined within a nozzle bore 34. The delivery
chamber 32 communicates with the pump chamber 8 of the pump assembly through channels
which are not visible in the sections shown in Figures 2 and 3. The nozzle 14 is provided
with nozzle spray holes (not shown) through which pressurised fuel is delivered to
an associated engine cylinder when the valve needle 12 is caused to lift from its
seating. The injection nozzle 14 and a lower end of the plunger housing 6 are retained
between first and second housings 36, 38 respectively in a conventional manner.
[0028] First and second ports 22, 24 respectively are provided in the plunger housing 6
to open to the plunger bore 4, as described previously. A low pressure circuit including
a storage space 28 and a supply rail 26 (typically at a pressure of 4 bar) is able
to communicate with the pump chamber 8 through one or both of the first and second
ports 22, 24 when they are open. Whether the ports 22, 24 are open or closed depends
on the position of the plunger 2 within the bore 4.
[0029] Both the first and second ports 22, 24 provide a flow path by which the pump chamber
8 is filled during the pumping cycle. Notably, the unit injector shown in Figures
2 and 3 and the prior are unit injector in Figure 1 differ in the means by which the
pump chamber 8 is brought into communication with the low pressure circuit 26, 28
at the end of an injection event. The distinctive feature of Figures 2 and 3, and
that which distinguishes the invention from prior art assemblies, is shown in the
highlighted portion X of Figure 2 and is reproduced in greater detail in Figure 3.
[0030] Referring in particular to Figure 3, the plunger 2 is provided with two additional
drillings or passageways 40, 42 forming flow paths within the plunger 2. The drillings
40, 42 are provided instead of the stop slot in the pump assembly of Figure 1. A first
longitudinal drilling 40 cuts through the plunger end face 10, preferably along the
longitudinal axis of the plunger 2 for ease of manufacture, and meets with a second
transverse drilling 42, perpendicular to the plunger axis, through a restriction 44.
Much in the same way as in Figure 1, a helical groove or slot 30 is also provided
in the plunger surface, only a portion of which is visible in Figure 3. The transverse
drilling 42 is able to communicate with the second port 24 through the helical groove
30. The longitudinal drilling 40, the restriction 44, the transverse drilling 42 and
the helical groove 30 together define a fuel flow path, having restricted flow means
44, by which the pump chamber 8 is able to communicate with the storage space 28 and
the low pressure fuel rail 26. Typically, for example, the restriction is of the order
of 1.0-1.5 mm diameter.
[0031] As an aside, it is preferable (although inessential) to provide the plunger 2 with
a circumferential leakage groove 46, which serves to collect leakage fuel down the
plunger bore 4 from the pump chamber 8. A further port 48 in the plunger housing 6
enables fuel collected within the leakage groove 46 to flow into the storage space
28 and to the low pressure rail 26. Other means for providing leakage collection are
also envisaged, for example the plunger bore 4 may be provided with a leakage groove
instead.
[0032] The pump assembly in Figures 2 and 3 has a similar pumping cycle to that described
previously for the prior art, but its operation will now be described in detail to
emphasise the functional advantages it provides.
[0033] In use, the plunger 2 is driven by the engine-driven cam to perform a pumping cycle
having two extreme positions of motion. At top dead centre (TDC) the plunger 2 is
at the innermost position within the bore 4 and at bottom dead centre (BDC) the plunger
2 is at the outermost position within the bore 4.
From a starting position of TDC, the pumping chamber 8 is at its minimum volume and
the end of the helical groove 30 is at least partially aligned with the second port
24. As the plunger 2 begins to travel towards BDC (referred to as the plunger return
stroke), the pump chamber volume is expanding and a point will be reached at which
the plunger end face 10 passes the edge of the first port 22 causing a substantially
unrestricted flow of fuel to be drawn into the pump chamber 8 from the low pressure
rail 26. As the plunger 2 continues to move towards BDC, the plunger end face 10 clears
the lowermost edge of the second port 24 also so that further fuel is admitted into
the pump chamber 8 through the second port 24.
[0034] Once the plunger 2 reaches BDC, the pump chamber 8 is at its maximum volume and filled
with fuel. As the plunger 2 starts to move towards TDC (referred to as the plunger
forward stroke), the volume of the pump chamber 8 starts to decrease and, initially,
fuel is dispelled from the pump chamber 8 to the low pressure circuit 26, 28 through
the uncovered ports 22, 24. As the plunger 2 moves further through the forward stroke,
the end face 10 clears, initially, the lowermost edge of the second port 24 and subsequently
the lowermost edge of the first port 22. Fuel remaining in the pump chamber 8, with
the first and second ports 22, 24 closed by the plunger 2, will undergo pressurisation
as the plunger 2 moves further through the forward stroke. It will be appreciated
that pressurisation of fuel within the pump chamber 8 is only initiated when the first
port 22 is also closed to break all communication routes between the pump chamber
8 and the low pressure rail 26.
[0035] Pressurised fuel within the pump chamber 8 is delivered to the delivery chamber 32
of the nozzle 14 through channels and passages of the pump and nozzle assembly (not
shown) and a point will be reached at which the force due to the shut-off spring 18
is overcome and the needle 12 lifts from its seating 16. Under such circumstances
fuel flows out of the nozzle holes into the engine cylinder to commence injection.
It will be appreciated that this flow of high pressure fuel to the nozzle 14 is not
restricted, and in particular the provision of the restricted drilling 44 has no bearing
on this flow of fuel.
[0036] As the plunger 2 moves further through the forward stoke, a point will be reached
at which the lowermost edge of the helical groove 30 passes the uppermost edge of
the second port 24. As the plunger 2 moves further through the forward stroke, fuel
within the pump chamber 8 is therefore able to flow through the longitudinal drilling
40, into the restriction 44, through the transverse drilling 42, into the helical
groove 30 and into the second port 24 to low pressure. Fuel pressure within the pump
chamber 8 is therefore reduced, or collapses, at a rate determined by the size of
the restriction 44. The longitudinal drilling 40, the restriction 44, the transverse
drilling 42 and the second port 24 therefore form part of a restricted flow passage
for fuel between the pump chamber 8 and the low pressure circuit 26, 28.
[0037] As the pressure of fuel being supplied to the delivery chamber 32 of the nozzle 14
is reduced, a point will be reached at which the force due to the spring 18 is sufficient
to re-seat the valve needle 12, thereby terminating injection through the nozzle holes.
For the remainder of the plunger forward stroke, the plunger 2 moves to fully align
the helical groove 30 with the second port 24, and may move beyond this point although
at all times ensuring the flow passage to low pressure through the drillings 40, 44,
42, the groove 30 and the second port 24 is maintained.
[0038] During the subsequent plunger return stroke the plunger 2 moves outwardly from the
bore 4, expanding the volume of the pump chamber 8 and filling the pump chamber 8
through the first and second ports 22, 24 ready for the next forward stroke, as described
previously.
[0039] It is an important feature of the present invention that the rate of pressure collapse
at the end of injection is controlled, or reduced, due to the provision of the restriction
44 in the plunger 2. By reducing the rate of pressure collapse at the end of injection,
fuel suck-back through the nozzle holes, nozzle passageways and the pump chamber 8
is slowed, resulting in fuel remaining in the region of the valve needle seating 16
for a slightly longer period so as to cushion the valve needle 12 during the seating
process. It is a benefit of this that valve needle and needle seat wear is reduced.
[0040] The provision of the restriction 44 within the plunger 2 itself is easy to accommodate
and requires no additional parts to those in existing units. The jet of high pressure
fuel expelled from the restriction 44 also impinges an internal surface of the plunger
2, which being made from a hard wearing material does not wear significantly as a
result.
[0041] It is a further benefit of the invention that the detrimental effects of gas blow-by
are minimised. Gas blow-by is known to occur in injection nozzles generally, due to
combustion gasses being sucked from the combustion cylinder up into the nozzle, and
can result in blocked flow passageways and contamination of the fuel system. Reducing
the rate of pressure collapse in the pump chamber 8 at the end of injection minimises
these effects.
[0042] As is known in unit injectors generally of the aforementioned type, the plunger 2
is movable angularly about its longitudinal axis so that the point in the forward
stroke at which the edge of the helical groove 30 is brought into communication with
the second port 24 may be adjusted. Hence, the quantity of fuel that is injected during
each pumping cycle can be controlled by adjusting the angular position of the plunger
2.
[0043] It is noted that the helical groove 30 necessarily does not cut through to the plunger
end face 10, otherwise depressurising fuel would flow through the helical slot, bypassing
the longitudinal drilling 40 and through the restriction 44. Were this to happen the
benefits of the restriction 44 in controlling fuel pressure collapse would not be
realised.
[0044] Although the embodiment described shows a restriction 44 between two drillings 40,
42, it is to be noted that the invention does not preclude location of the restriction
along other positions in the fuel depressurisation circuit to achieve the same benefits
as those described above. As an example, an alternative location for the restriction
would be in the transverse drilling 42, although this embodiment may be less preferable
as the depressurising fuel jet may impinge on other parts of the pump assembly, and
not on internal surfaces of the plunger 2.
[0045] Another embodiment provides one of the ports 22, 24 with a restriction whilst the
other is unrestricted. The ports must be positioned so that pump chamber filling can
occur through the unrestricted port, whilst depressurisation of the pump chamber 8
occurs through the restricted port. In this embodiment the plunger housing 6 of existing
units therefore requires modification, and the plunger 2 also requires the provision
of the drillings 40, 42 (with no stop slot).
1. A pump assembly for use in a compression ignition engine, the pump assembly comprising:
a plunger (2) that is reciprocable within a plunger housing (6) to pressurise fuel
within a compression chamber (8),
a first flow path (22) providing communication between the compression chamber (8)
and a low pressure circuit (26, 28) to permit filling of the compression chamber (8),
and being closed to fuel flow to initiate pressurisation of fuel within the compression
chamber (8),
a second flow path (40, 42, 24) providing communication between the compression chamber
(8) and the low pressure circuit (26, 28), and being opened to fuel flow to terminate
pressurisation of fuel within the compression chamber after said closure the first
flow path (22);
characterised in that:
the second flow path (40, 42, 24) is provided with flow restriction means (44) to
retard the rate of depressurisation of the compression chamber (8).
2. A pump assembly according to Claim 1, further characterised in that the second flow path (40, 42, 24) is at least partially provided in a portion of
the plunger housing (6) and the flow restriction means is provided within said portion.
3. A pump assembly according to Claim 1, further characterised in that the second flow path (40, 42, 24) is at least partially provided in a portion of
the plunger (2) and the flow restriction means (44) is provided within said portion.
4. A pump assembly according to Claim 3, further characterised in that said portion of the second flow path comprises a drilling (40) along an axis parallel
with a longitudinal axis of the plunger (2), and said flow restriction means (44)
is provided along the drilling (40).
5. A pump assembly according to Claim 3, further characterised in that said portion of the second flow path comprises a drilling (42) along an axis transverse
to a longitudinal axis of the plunger (2) and said flow restriction means is provided
along the drilling (42).
6. A pump assembly according to any one of the preceding claims, further characterised in that the plunger housing (6) is provided with a plunger bore (4), which serves to guide
reciprocal motion of the plunger (2) within the plunger housing (6).
7. A pump assembly according to any one of the preceding claims, wherein the first flow
path comprises a filling port (22) provided in the plunger housing (6) and opening
to the plunger bore (4).
8. A pump assembly according to any one of claims 1 to 7, in the form of a fuel pump
for supplying pressurised fuel to a dedicated injector remote from the pump assembly,
in use.
9. A pump assembly according to any one of claims 1 to 7, in the form of a unit injector,
which also comprises an injection nozzle (14) arranged within a common unit with the
pump assembly (2, 6).
10. A pump assembly as claimed in claim 9, including a passage for high pressure fuel
between the compression chamber (8) and the nozzle (14), which permits fuel flow to
and from the injection nozzle (14) at a substantially unrestricted rate.
11. A plunger (2) suitable for use with any one of the preceding claims,
characterised in that the plunger (2) comprises a fuel flow passage (40, 42) along which is provided restriction
flow means (44).