[0001] A common rail-type fuel injection system is known as one of systems which inject
fuel into diesel engines. In the common rail-type injection system, a common accumulation
chamber (common rail) communicating with each engine cylinder is provided. The fuel
pressure in the accumulation chamber is maintained at a predetermined pressure by
pressure-feeding of fuel the necessary amount of high pressure fuel from a variable
discharge-type high pressure pump to the accumulation chamber. The high pressure fuel
in the accumulation chamber is injected into the combustion chamber of each cylinder
from an electromagnetically-operated injector at a predetermined injection timing.
[0002] The variable discharge-type high pressure pump has a pressure chamber which is connected
to the common rail and increases/decreases its displacement or volume. The amount
of fuel sucked into the pressure chamber is adjusted by opening and closing of a control
valve provided between the pressure chamber and a low pressure pump which feeds low
pressure fuel.
[0003] A pre-stroke type is generally used to produce the desired feed amount to the common
rail by closing the control valve at a predetermined timing when the displacement
of the pressure chamber is decreased to set the amount of fuel in the pressure chamber.
In the pre-stroke type, however, the control valve is required to operate with high
accuracy under high pressure condition because high pressure of fuel is applied to
the control valve. The system becomes large and cost increases, if a sufficient pressure-feed
amount control characteristics is required.
[0004] A variable discharge-type high pressure pump is proposed as shown in Fig. 18 to solve
this problem. In this variable discharge-type high pressure pump, a drive shaft 101
is extended through and held in a pump housing 100. The low pressure fuel is fed into
a fuel reservoir 105 from a low pressure pump (feed pump) 102 which rotates with the
drive shaft 101 through low pressure fuel passages 103 and 104.
[0005] An inner cam 106 is formed integrally with the right end part of the drive shaft
101. The left end part of a head 107 is press-inserted into the inner cam 106. Four
cylinders 108 (only two are shown in the figure) are formed in radial directions in
the left end part of the head 107. A plunger 109 is disposed reciprocally in each
cylinder 108. A pressure chamber 110 is defined by the radial inside end surface of
the plunger 109 and the inside wall of the cylinder 108, so that fuel introduced therein
may be pressurized by reciprocal movement of the plunger 109.
[0006] A control valve 111 and a suction valve 112 are disposed from the upstream side in
the flow passage extending from the fuel reservoir 105 to the pressure chamber 110.
The control valve 111 is an electromagnetic valve the power-on or energization of
which is controlled by an electronic control unit not shown. The suction valve 112
is a check valve which allows fuel to flow in the forward direction, that is, from
the control valve 111 to the pressure chamber 110.
[0007] The suction valve 112 opens when the pressure in the pressure chamber 110 decreases
in response to opening of the control valve 111 and increase of the displacement of
the pressure chamber 110 due to rearward movement of the plunger 109. It closes when
the control valve 111 closes. The flow passage to the pressure chamber 110 is closed
by the suction valve 112 from the start of pressurizing the low pressure fuel to the
end of pressure-feeding of fuel, after preliminarily supplying the required amount
of fuel from the feed pump 102 to the pressure chamber 110 in accordance with the
valve opening period of the control valve 111.
[0008] Thus, the pressure applied to the control valve 111 is limited at a maximum to the
feed pressure (about 15 atms). Therefore, the control valve 111 need not be the type
which operates with high accuracy under high pressure conditions, so that a sufficient
common rail pressure control may be attained in low cost.
[0009] In a control method for the variable discharge-type high pressure pump, for instance,
a valve opening period command value of the control valve 111 is determined in accordance
with a fuel injection amount which is the discharge amount of high pressure fuel from
the common rail and the control valve 111 is opened and closed in response to the
command value to refill the common rail with high pressure fuel.
[0010] In the above variable discharge-type high pressure pump, however, excessive pressure-feeding
of fuel occurs at the time of engine restarting after fuel shortage, before fuel shortage
or at the time of rapid turning. In this instance, it is likely that the normal high
controllability of the common rail pressure cannot be attained.
[0011] The present invention has been made in view of the above problem, and has an object
to provide a control method and apparatus for variable discharge-type high pressure
pumps so that excessive pressure-feeding of fuel is prevented and controllability
of pressure in an accumulation chamber is improved.
[0012] According to the present invention, a control valve is controlled in accordance with
a command value which is indicative of the amount of flow of fuel, and an accumulation
chamber is refilled with high pressure fuel in accordance with the amount of high
pressure fuel discharged from a pressure chamber.
[0013] It is checked whether a predetermined control requirement is satisfied. The control
requirement includes that a detected actual pressure is higher than a target pressure
of the accumulation chamber by more than a predetermined tolerance value, and the
control valve is disabled to open thereby stopping suction of the low pressure fuel
into the pressure chamber, when it is determined that the control requirement is satisfied.
[0014] When air enters into the fuel discharged from the low pressure pump due to shortage
of fuel and causes air to remain in the fuel in a flow passage extending from the
control valve to a check valve, the air expands because the check valve opens and
the fuel feed pressure decreases with an increase in the displacement of the pressure
chamber. This tends to cause that fuel is forced out into the pressure chamber in
an amount corresponding to the expansion of air, and fuel is sucked into the pressure
chamber excessively. This results in excessive pressure-feeding of fuel.
[0015] However, the control valve is disabled to open when the control requirement is satisfied
to indicate a high possibility that air is admixed in the fuel discharged from the
low pressure pump. Thus, no air is discharged from the low pressure pump into the
flow passage part leading from the control valve to the check valve, so that excessive
pressure-feeding of fuel into the accumulation chamber is prevented.
Fig. 1 is a schematic diagram showing a common rail-type fuel injection system including
a variable discharge-type high pressure pump to which the present invention is applied;
Fig. 2 is a cross-sectional view showing the variable discharge-type high pressure
pump shown in Fig. 1;
Fig. 3 is a side view of an engine showing a driving mechanism for the variable discharge-type
high pressure pump;
Fig. 4 is another cross-sectional view showing a part of the variable discharge-type
high pressure pump;
Fig. 5 (A) is a cross-sectional view taken along line A-A in Fig. 4, and (B) is a
cross-sectional view taken along line B-B in Fig. 4;
Fig. 6 is a schematic view showing a main part of the variable discharge-type high
pressure pump;
Fig. 7 is a timing diagram showing operation of the variable discharge-type high pressure
pump;
Fig. 8 is a first flow diagram showing a control method for variable discharge-type
high pressure pump;
Fig. 9 is a second flow diagram showing a control method for variable discharge-type
high pressure pump;
Fig. 10 is a third flow diagram showing a control method for variable discharge-type
high pressure pump;
Fig. 11 is a fourth flow diagram showing a control method for variable discharge-type
high pressure pump;
Fig. 12 is a fifth flow diagram showing a control method for variable discharge-type
high pressure pump;
Fig. 13 is a sixth flow diagram showing a control method for variable discharge-type
high pressure pump;
Fig. 14 is a seventh flow diagram showing a control method for variable discharge-type
high pressure pump;
Fig. 15 is an eighth flow diagram showing a control method for variable discharge-type
high pressure pump;
Fig. 16 is a flow diagram showing another control method for variable discharge-type
high pressure pump;
Fig. 17 is a schematic view showing a main part of another variable discharge-type
high pressure pump to which the control method for variable discharge-type high pressure
pump according to the present invention;
Fig. 18 is a cross-sectional view showing a variable discharge-type high pressure
pump to which a conventional control method is applied; and
Fig. 19 is a timing diagram showing operation of the conventional control method for
comparison with the control method according to the present invention.
(First Embodiment)
[0016] A control method for a variable discharge-type high pressure pump according to the
present invention is described with reference to a case in which it is applied a common
rail-type fuel injection system for diesel engines.
[0017] In Fig. 1, a plurality of injectors I is mounted on an engine E in correspondence
with the combustion chamber of each cylinder. These injectors I are connected to a
common rail R which is an accumulation chamber common to each cylinder. The injection
of fuel from the injector I into the combustion chamber of the engine E is controlled
by on-off of an injection control electromagnetic valve B1. Fuel in the common rail
R is injected into the engine E during a period the electromagnetic valve B1 is open.
It is assumed that the engine E is a four cylinder-type.
[0018] A variable discharge-type high pressure pump P is connected to the common rail R
through a supply pipe R1 and discharge valves B2, so that fuel is continuously accumulated
in the common rail R at a high predetermined pressure which corresponds to a fuel
injection pressure. The variable discharge-type high pressure pump P pressurizes low
pressure fuel sucked from a fuel tank T by a feed pump P1 to high pressure so that
fuel in the common rail R is controlled to the predetermined high pressure.
[0019] The common rail injection system has an electronic control unit C. The electronic
control unit C is constructed with a generally known hardware including a CPU and
the like. It produces control signals to the injectors I and the variable discharge-type
high pressure pump P in response to inputs from various sensors S1, S2 and S3, so
that the injectors I and the variable discharge-type high pressure pump P may be electronically
controlled.
[0020] The electronic control unit C receives engine condition information from, for instance,
engine rotation sensor S2 and cylinder discrimination sensor (G1 sensor) S3. The pressure
sensor S1 is disposed on the common rail R to detect a common rail pressure, so that
information of the common rail pressure is applied to the electronic control unit
C.
[0021] The electronic control unit C calculates optimum injection timing and injection amount
(injection period) in response to those information, and produces a control signal
to the fuel injection control electromagnetic valve B1 so that the discharge amount
of the variable discharge-type high pressure pump P is controlled.
[0022] The variable discharge-type high pressure pump P is shown in detail in Fig. 2. In
the figure, a drive shaft D which is driven to rotate by the engine E at a one-half
rotation speed of the engine is inserted into and supported by a pump housing 1. A
pump timing pulley 51 is fixed to the left end part of the drive shaft D so that it
may be driven to rotate by a timing belt 52 looped over the outer periphery as shown
in Fig. 3.
[0023] In the figure, a camshaft timing pulley 53 is fixed to the camshaft of the engine,
and a crankshaft timing pulley 54 is connected to the crankshaft of the engine. The
pump timing pulley 51 and the camshaft timing pulley 53 are driven to rotate by rotation
of the crankshaft of the engine through the timing belt 52. Idlers 55 and 56 are used,
so that the idler 56 applies a tension to the timing belt 52 with the spring force
of a spring 57 to prevent slacking.
[0024] A vane-type feed pump P1 is coupled with the drive shaft D to supply fuel under low
pressure. The feed pump p1 rotates with the drive shaft D to suck fuel from the fuel
tank T and feeds it at a predetermined feed pressure (about 15 atms) to a fuel reservoir
5a formed inside a head 14 through low pressure flow passage 11, 12 and a low pressure
flow passage 13 in the head 14. The fuel discharge side and the fuel suction side
of the feed pump P1 are connected through a pressure regulating valve not shown, so
that the discharge pressure may be regulated. Thus, the variable discharge-type high
pressure pump P houses therein the feed pump P1 shown in Fig. 1.
[0025] The drive shaft D is supported rotatably in the pump housing 1 through bearings D1
and D2. An inner cam 8 is integrally formed on its right end part. The head 14 is
press-fit into the right end opening of the pump housing 1. The head 14 has a protrusion
at its left end central part to be inserted into the inner cam 8.
[0026] A control valve 6a is disposed in the lower end part of the head 14 to control the
amount of low pressure fuel flowing into the pressure chamber, that is, to control
the amount of fuel passing between the feed pump P1 and a suction valve 4a described
later. The suction valve 4a, which is a check valve, is disposed in the right end
central part of the head 14. A delivery valve 3 is disposed above the suction valve
4a. Although not shown, another control valve 6b and suction valve 4b are disposed
at different positions in addition to the control valve 6a and the suction valve 4a.
[0027] As shown in Fig. 4, the head 14 is formed with a flow passage 72 leading from the
control valve 6a to the suction valve 4a, flow passages 30a and 40a leading from the
suction valve 4a to a pressure chamber 23a described later, a discharge port 16a leading
from the flow passage 40a to the delivery valve 3. Although not shown, the head 14
is also formed with a flow passage 72 leading from the control valve 6a to the suction
valve 4b, flow passages 30b and 40b leading from the suction valve 4b to a pressure
chamber 23b described later, a discharge port 16b leading from the flow passage 40b
to the delivery valve 3.
[0028] The control valve 6a is an electromagnetic-type, and has a housing 61 accommodating
a coil 62 therein and a valve body 68 press-fit into the upper end part of the housing
61. A valve member 73 is held slidably in a cylinder 69 formed in the valve body 68.
The control valve 6a is fixed by threading bolts not shown through a flange 63 provided
on the outer periphery of the housing. An annular flow passage 74a is formed around
the upper end part of the valve member 73. The flow passage 74a is communicated with
the fuel reservoir 5a through the flow passage 74b, and with the flow passage 72 leading
to the suction valve 4a through a flow passage 74c.
[0029] An armature 64 is press-fit fixed to the lower end of the valve member 73 in such
a manner that the armature faces a stator 65 with a fixed spacing therebetween. The
coil 62 is disposed outside the stator 65. A spring 67 is disposed in a spring chamber
66 formed inside the stator 65 to bias the armature upward in the figure.
[0030] A generally conical seat surface 75 is formed in the open end of the flow passage
74c so that the top end part of the valve member 73 seats on the seat surface 75 to
interrupt the flow passages 74a and 74c under the shown condition that the coil 62
is not powered on. When the coil 62 is powered on or energized in response to the
control signal from the electronic control unit C, the armature 64 is attracted and
the top end part of the valve member 73 integral with the armature 64 leaves away
from the seat surface 75 so that the flow passages 74a and 74c are opened. It is advantageous
to disable pressure-feeding of fuel at the time of breakage of the coil by thus constructing
the control valve 6a to close normally, that is, when not powered on. The control
valve 6b is constructed similarly, although not shown.
[0031] A first cylinder 2a and a second cylinder 2b are formed in the left end central part
of the head 14 to define pressure chambers inside the head 14. The cylinder 2a and
the cylinder 2b are spaced apart with a spacing therebetween in the axial direction
of the drive shaft D, so that the axes of the cylinders 2a and 2b cross perpendicularly
to each other. Further, the cylinders 2a and 2b are formed in the direction perpendicular
to the axis of the drive shaft D.
[0032] As shown in Fig. 5(A), a first pair of plungers 21a and 21c are disposed to face
each other in the first cylinder 2a, and are supported reciprocably and slidably relative
to the cylinder 2a. The space defined by the inside wall surface of the cylinder 2a
and the end faces of the plungers 21a and 21c provide a first pressure chamber 23a.
Similarly, as shown in Fig. 5(B), a second pair of plungers 21b and 21d are disposed
to face each other in the second cylinder 2b, and are supported reciprocably and slidably
relative to the cylinder 2b. The space defined by the inside wall surface of the cylinder
2b and the end faces of the plungers 21b and 21d provides a second pressure chamber
23b.
[0033] Of the pair of plungers 21a and 21c, one plunger 21a is formed shorter than the other
plunger 21c. As a result, the pressure chamber 23a is located at a position slightly
displaced from the center of the cylinder 2a. Similarly, of the pair of plungers 21b
and 21d, the plunger 21d is formed shorter than the other plunger 21b, and the pressure
chamber 23b is formed at a position slightly displaced from the center of the cylinder
2b. This construction provides an advantage that the flow passages 40a, 40b and the
flow passages 30a and 30b can be formed with ease.
[0034] Shoes 24a to 24d are provided at outside end parts of the plungers 21a to 21d. Cam
rollers 22a to 22d are supported rotatably on the corresponding shoes 24a to 24d.
The end surfaces of the shoes 24a to 24d are slidable on a shoe guide 15 and a plate
7. The shoe guide 15 and the plate 7 are fixed to the head 14 with bolts not shown.
A washer 76 is inserted between the plate 7 and the drive shaft D, so that the drive
shaft D and the washer 6 are rotatable from each other and the washer 6 and the plate
7 are rotatable from each other.
[0035] The inner cam 8 is provided in common relative to the cylinders 2a and 2b, so that
the plunger 21a to 21d may be reciprocaly moved within the cylinders 2a and 2b by
the rotation of the inner cam 8. The inside circumferentail surface of the inner cam
8 is shaped in a cam surface 81 having a plurality of cams. The cam rollers 22a to
22d are disposed so that the outside circumferences of the cam rollers 22a to 22d
are in sliding contact with the cam surface 81. Here, the inside circumferential surface
of the inner cam 8 is shaped in an elliptic form, and two cams are formed at equal
intervals (at positions to face the plungers 21a and 21c in Fig. 5(A)).
[0036] Thus, when the inner cam 8 integral with the drive shaft D rotates, the plungers
21a and 21c reciprocate within the cylinder 2a, and the plungers 21b and 21d reciprocate
in the cylinder 2b. Fuel in the pressure chambers 23a and 23b are pressurized respectively
by alternate radially inward movements of the plungers 21a, 21c and the plungers 21b,
21d.
[0037] The suction valve 4a which has the flow passage 43 passing through the housing 42
in the left and right directions and a valve member 44 for opening and closing the
flow passage 43. The flow passage 43 is enlarged in the middle of its extension in
the direction of the pressure chamber 23a (leftward in the figure) to form a conical
seat surface 45. The valve member 44 is biased in the right direction by a spring
46 held in a spring stopper 41, and seats on the seat surface 45. Thus, the check
valve 4a is normally closed in the normal condition shown in the figure. The check
valve 4a is so constructed that it opens when the control valve 6a opens to allow
low pressure fuel to flow from the fuel reservoir 5a and decrease the pressure in
the flow passage 30a (pressure in the pressure chamber 23a).
[0038] During the valve opening period, the low pressure fuel flows into the pressure chamber
23a through the flow passage 72, annular flow passage 48 provided around the outside
circumference of the housing 42, flow passage 49 in the housing 42, flow passage 43,
flow passage 50 in the spring stopper 41, and flow passages 30a, 40a provided in the
head 14.
[0039] Another suction valve 4b not shown in Fig. 4 is constructed similarly as the suction
valve 4a. As described later, the suction valve 4b also opens when the control valve
6b opens to allow low pressure fuel to flow from the fuel reservoir 5b and decrease
the pressure in the flow passage 30b (pressure in the pressure chamber 23b). Low pressure
fuel flows into the pressure chamber 23b through the flow passage 72, annular flow
passage 48 provided around the outside circumference of the housing 42, flow passage
49 in the housing 42, flow passage 43, flow passage 50 in the spring stopper 41, and
flow passages 30b, 40b provided in the head 14. The suction valves 4a and 4b are fixed
in the head 14 with screws 47.
[0040] The delivery valve 3 has a check valve function and has balls 31a and 31b as valve
members. The ball 31a is constructed to open and close the flow passage leading from
the discharge port 16a communicated with the pressure chamber 23a, and the ball 31b
is constructed to open and close the flow passage leading from the discharge port
16b communicated with the pressure chamber 23b.
[0041] That is, as shown in Fig. 6, two plungers are disposed in the two cylinders 2a and
2b which are independent from each other, respectively, so that two fuel pressure-feeding
routes are provided. The second pressure-feeding route comprises the cylinder 2b,
a pair of plungers 21b, 21d and pressure chamber 23b surrounded by those. The first
pressure-feeding route and the second pressure-feeding route alternately attain fuel
pressure-feeding operation. The pressure chamber 23a is communicated with the side
of the ball 31a of the delivery valve 3 through the flow passage 40a and the discharge
port 16a, and the pressure chamber 23b is communicated with the side of the ball 31b
of the delivery valve 3 through the flow passage 40b and the discharge port 16b.
[0042] The ball 31a or the ball 31b opens when the pressure in fuel pressurized in each
pressure chamber 23a, 23b, so that fuel is supplied to the common rail R through the
supply pipe R1. Here, the fuel is discharged alternately through the balls 31a and
31b, because the fuel in the pressure chambers 23a and 23b is pressurized alternately.
The feed pressure to the common rail R varies with operating conditions of the engine
E between 200 to 1200 atms.
[0043] The supply system of low pressure fuel to the pressure chambers 23a and 23b has two
routes, one being from the fuel reservoir 5a to the pressure chamber 23a through the
control valve 6a, suction valve 4a and the flow passage 30a and the other being from
the fuel reservoir 5b to the pressure chamber 23b through the control valve 6b, suction
valve 4b and the flow passage 30b.
[0044] The operation of the variable discharge-type high pressure pump P constructed as
above is described with reference to Fig. 7. In the figure, cam #1 indicates a lift
amount at the points 81a and 81c on the cam surface 81 which faces the plungers 21a
and 21c in Fig. 5(A). Cam #2 indicates a lift amount at the points 81b and 81d on
the cam surface 81 which faces the plungers 21b and 21d in Fig. 5(B). TCV #1 indicates
a lift amount of the valve member 73 of the control valve 6a, and TCV #2 indicates
a lift amount of the valve member 73 of the control valve 6b.
[0045] When the inner cam 8 rotates, the cams #1 and #2 repeats radially inward movement
and radially outward movement. Because the cylinders 2a and 2b are formed perpendicularly
to each other, the cams #1 and #2 are different 180° CA (crankshaft angle) in phase.
During a fuel suction operation in which one pressure chamber 23a (23b) is in no fuel
pressure-feeding operation, the other pressure chamber 23b (23a) is in the fuel pressure-feeding
operation.
[0046] Suction and fuel pressure-feeding operations in the pressure chambers 23a and 23b
are described below. The electronic control units C starts to power on the coil 62
of the control valve 6a in advance before the valve member 73 of the control valve
6a opens at the time of start of moving of the cam #1 in the radially outward direction.
With the control valve 6a being powered on, fuel flows into the pressure chamber 23a
from the fuel reservoir 5a through the flow passages 74c, 72 of the control valve
6a, flow passage 43 of the suction valve 4a and flow passages 30a, 40a. At this time,
the plungers 21a and 21c move in the radially outward direction while being pressed
down onto the cam surface 81 by the fuel flowing thereinto, so that fuel is sucked
as the displacement of the pressure chamber 23a is increased.
[0047] When the electronic control unit C interrupts the power-on of the coil 62 of the
control valve 6a to close the valve member 73 of the control valve 6a and the suction
valve 4a, the fuel is stopped from flowing into the pressure chamber 23a. Although
the cam #1 continues to move in thereafter, the plungers 21a and 21c stop lifting
to separate from the cam rollers 22a, 22c and the inner cam 8 when the suction operation
ends.
[0048] Then, the cam #1 moves to come into the fuel pressure-feeding operation. The plungers
21a and 21c do not start moving in the radially inward direction immediately after
the cam #1 starts moving for fuel pressure-feeding operation. When the lift amount
of cam #1 reaches the lift amount of the plungers 21a and 21c, the cam rollers 22a
and 22c abut the inner cam 8 to drive the plungers 21a and 21c to move in the radially
inward direction through the shoes 24a and 24c. At this moment, the suction valve
4a is closed.
[0049] Then, as the plungers 21a and 21c move in the radially inward direction to decrease
the displacement of the pressure chamber 23a, the fuel in the pressure chamber 23a
is pressurized and the pressure in the pressure chamber 23a is increased gradually.
When the pressure of fuel in the pressure chambers 23a and 23c rises above a predetermined
pressure, high pressure fuel is supplied from the supply pipe R1 to the common rail
R through the discharge port 16a and the delivery valve 3. The fuel pressure-feeding
ends when the lift amount of the cam #1 reaches its maximum and the lift of plungers
21a and 21c reaches a maximum point.
[0050] The control valve 6b is powered on with about 180° CA delay from the control valve
6a in the above period, the cam #2 starts moving to effect suction and fuel pressure-feeding
operation in the pressure chamber 23b in the same manner as in the pressure chamber
23a. Thus, a maximum driving torque is reduced by differentiating the time points
of fuel pressure-feeding operation between the pressure chambers 23a and 23b.
[0051] The control method for preventing excessive pressure-feeding of fuel to the common
rail R is described with reference to flow diagrams of controlling the variable discharge-type
high pressure pump P executed in the electronic control unit C.
[0052] In Fig. 8, a NE-signal hardware interrupt routine is executed at every input of the
NE-signal produced 68 times per 720° CA. A pulse interval between the input NE-signal
and the previous one is measured at step S101, so that the pulse interval may be used
in a calculation of engine rotation speed Ne. A NE-pulse counter CNIRQ is updated
(one step increment) at step S102. It is checked at step S103 whether CNIRQ = 0 holds.
[0053] If affirmative (YES) a cylinder counter PCYLND (= 0, 1, 2, 3) is updated (one step
increment) at step S104 to proceed to step S105. If negative (NO), the processing
advances to step S105. A software interrupt process is called at step S105 in correspondence
with CNIRQ, thus ending the NE-signal hardware interrupt routine. Here, the cylinder
counter PCYLND = 0 is set in response to an input of G1-signal from the G1 sensor
S3.
[0054] The software interrupt process called at step S105 is described. In Fig. 9 showing
a software interrupt process called when CNIRQ = 1, the engine rotation speed Ne and
accelerator position Ac are read in at step S201. A command injection amount QF of
the injector I is calculated at step S202, and a command injection timing AF is calculated
at step S203 based on the command injection amount QF and the engine rotation speed
Ne. Finally, a target common rail pressure PF is calculated at step S204 based on
the command injection amount QF and the engine rotation speed Ne.
[0055] Fig. 10 shows a software interrupt process called when CNIRQ = 3. The common rail
pressure PC is read in at step S301, and a power-on period TQF to the injector I is
calculated at step S302 based on the actual common rail pressure PC and the command
injection amount QF. A pump power-on period TF is calculated at step S303 to indicate
the valve opening period command value as a command value to the control valves 6a
and 6b for controlling the amount of fuel passing between the feed pump 1 and the
suction valve 4a and between the feed pump P1 and the suction valve 4b.
[0056] Fig. 11 shows a calculation process of the pump power-on period TF executed at step
S303. A basic power-on period TFJP is calculated at step S401 based on the command
injection amount QF and the target common rail pressure PF. The subsequent steps S402
to S406 are for calculating corrective terms which are to be added to or subtracted
from the command injection amount QF. A proportional compensation amount TFJP is calculated
at step S402 from the difference between the common rail pressure PC and the target
common rail pressure PF.
[0057] It is checked at step S403 whether a power-on flag TFON described later is 1. If
the power-on flag TFON = 1, an integral compensation amount TFJI is calculated and
updated at step S404 from the difference between the common rail pressure PC and the
target common rail pressure PF. If the power-on flag TFON = 0, the calculation of
the integral compensation amount TFIJ (step S403) is skipped. As described later,
the power-on flag TFON is set to 0 when it is likely that the excessive pressure-feed
occurs.
[0058] The above corrective terms operates to shorten the pump power-on period TF. However,
if the integral compensation amount TFJI is updated, it results in that the integral
compensation value TFJI will in the end includes component which corresponds to the
difference between the abnormal common rail pressure PC at this moment and the target
common rail pressure PF. Therefore, this updating is not desired. The appropriate
compensation amount can be calculated by skipping the updating of the integral compensation
amount TFJI based on the above difference at the time of abnormality.
[0059] An electromagnetic valve closing delay compensation amount TFD is calculated at step
S405 to compensate for the response delay of closing operation of the control valves
6a and 6b relative to the valve closing signal (interruption of power-on to the coil
62). The electromagnetic valve closing delay compensation amount TFD is calculated
using the following equation (1), that is, by converting the valve closing delay time
TFDB (µs) of the control valves 6a and 6b stored preliminarily into the crankshaft
angle in accordance with the engine rotation speed Ne.

[0060] The pump power-on period TF is calculated at step S406 using the equation (2).

In the above equation, TFOF is added for the reason that, because fuel is sucked
into the pressure chambers 23a and 23b after the power-on of the control valves 6a
and 6b are started and the plungers 21a to 23d start moving in the radially outward
direction, the power-on period before that time point does not contribute to the suction
of fuel. Therefore, as described above, TFOF is added to an effective fuel suction
period TFJ (

) to calculate the pump power-on period TF.
[0061] Fig. 12 shows a software interrupt called when CHIRQ = 4, the on-timing AF of the
injector is set at step S501, and an off-timing tQF of the injector is set at step
S502 after the injector-on period (TQF) at the time of the on-timing AF, thus ending
this software interrupt.
[0062] Fig. 13 shows a software interrupt called when CNIRQ = 5. It is checked at steps
S601 and S602 whether required control conditions are satisfied. It is checked at
step S601 whether the pump power-on period TF is shorter than a predetermined lower
limit value. The lower limit value is determined preliminarily to 5° CA, for instance.
It is checked at step S602 whether the actual common rail pressure PC is higher than
the target common rail pressure PF + tolerance value. Here, the tolerance value is
set preliminarily to 5 Mpa, for instance. If the check result of either step S601
or S602 is negative, the power-on flag TFON is set to 1 at step S603, and a power-on
process is executed at step 604. If both the check results of steps S601 and S602
are affirmative, the following step S605 is executed.
[0063] Fig. 14 shows the power-on process of step S604. The cylinder counter PCYLND is read
in at step S701, and it is checked at step S702 whether the PCYLND = 0 or 2. If affirmative,
the processing proceeds to step S703 to power on the control valve 6b. If negative,
the processing proceeds to step S704 to power on the control valve 6a, thus ending
this power-on process.
[0064] Fig. 15 shows a software interrupt called when CNIRQ = 6. The cylinder counter PCYLND
is read in at step S801, and it is checked at step S802 whether PCYLND = 0 or 2. If
affirmative, the processing proceeds to step S803 to set the power-off timing after
the pump power-on period TF from the power-on timing with respect to the control valve
6b. If negative, the processing proceeds to step S804 to set power-off timing with
regard to the control valve 6b, thus ending this routine.
[0065] In the above software interrupt process executed when CNIRQ = 5, the routine ends
after setting the power-on flag TFON at step S605 and without executing the above
power-on process when the pump power-on period TF is shorter than the lower limit
value and the common rail pressure PC is higher than the target common rail pressure
PF + tolerance value (steps S601 and S602). That is, if the check results at steps
S601 and S602 are both affirmative, no fuel is refilled into the common rail in connection
with fuel injection from the injectors.
[0066] A difference between the control method according to the present invention and the
conventional method is described below. In the control method according to the present
invention, the control valve 6a is not opened when the control conditions to be checked
at steps S601 and S602 are satisfied. In the conventional method, the control valve
is opened for a predetermined period in accordance with the required amount of fuel
to be refilled in the common rail in connection with the fuel injection from the fuel
injector.
[0067] In Fig. 19 showing the conventional method, the control valve is powered on to open
at the stage ①. With the opening of the control valve, low pressure fuel flows into
the flow passage part (fuel reservoir part) from the control valve to the suction
valve, and the pressure in the fuel reservoir part rises from the atmospheric pressure
to the feed pressure. As the suction valve is maintained closed, the pressure in the
pressure chamber is the same as that in the common rail and the plunger is pressed
to the cam surface. Here, when the low pressure pump sucks air with fuel from the
fuel tank in which the remaining amount of fuel is less such as in fuel shortage condition,
air admixes in the fuel supplied to the fuel reservoir part.
[0068] At the following stage ②, the cam lift decreases with the plunger being pressed to
the cam surface and moving in the radially outward direction. The displacement of
the pressure chamber is increased and the pressure in the pressure chamber is decreased.
However, the suction valve is maintained closed, because the pressure in the pressure
chamber is higher than the feed pressure.
[0069] At the following stage ③, the pressure in the pressure chamber decreases below the
feed pressure. The suction valve opens so that low pressure fuel is sucked into the
pressure chamber through the suction valve, even when the control valve has already
been closed. The pressure in the fuel reservoir part communicated with the pressure
chamber further decreases from the feed pressure toward the atmospheric pressure in
the same manner as the pressure chamber, and the admixed air in the fuel reservoir
part expands. The air expands much more than fuel because of decrease in the pressure,
and forces out the fuel in the fuel reservoir part to the pressure chamber.
[0070] Thus, when fuel with admixed air under the feed pressure flows into the fuel reservoir
part, the fuel forced out by the expansion of admixed air due to change from the feed
pressure to the atmospheric pressure is forced out to the pressure chamber as excessive
fuel irrespective of the power-on period of the control valve. As a result, the fuel
is not regulated to the amount corresponding to the power-on period of the control
valve.
[0071] After the pressure in the pressure chamber decreases to the atmospheric pressure
and the cam lift stops decreasing, the cam lift increases again at the stage ④. The
cam starts to press the plunger. Thus, the fuel in the pressure chamber is pressurized,
and the pressure in the pressure chamber increases.
[0072] At the following stage ⑤, the pressure in the pressure chamber increases further,
and exceeds the pressure defined by the valve opening pressure of the delivery valve
to open the delivery valve. The fuel is pressure-fed from the pressure chamber to
the common rail R. Because the regulation of the suction amount of fuel into the pressure
chamber at the excessive amount side has errors as described above, the fuel is fed
excessively.
[0073] Thus, the pressure in the common rail tends to rise excessively. The power-on period
TF is shortened to counter this. However, as long as fuel admixed with air from the
low pressure pump is sucked, excessive fuel flows into the pressure chamber in the
end in an amount corresponding to the air amount. It is thus highly likely that the
excessive pressure-feed condition cannot be countered.
[0074] On the contrary, in the control method according to the present invention, the above
steps S601 and S602 are executed so that the power-on of the control valve 6a is disabled
(step 605) when the influence of shortening of the command power-on period TF and
occurrence of excessive pressure-feeding of fuel is large. The excessive pressure-feeding
of fuel condition can thus be avoided. As a result, good vehicle driveability and
less exhaust gas emission can be attained without causing lessening of pressure controllability.
[0075] Further, the variable discharge-type high pressure pump P pressure-feeds fuel to
the common rail R alternately from a plurality of pressure chambers 23a and 23b. As
a result, it is advantageous that the maximum driving torque can be reduced and the
load to the timing belt 52 can be reduced to prevent lessening of durability.
[0076] However, the suction valves 4a and 4b need be provided for the pressure chambers
23a and 23b in one-to-one correspondence. As a result, from the relation of laying
out the suction valves 4a, 4b and the control valves 6a, 6b, the flow passage (fuel
reservoir part) 73, 74c, 72, 71a, 48, 49 or 73, 74c, 72, 71b, 48, 49 leading from
the control valves 6a, 6b to the suction valves 4a, 4b become lengthened. The admixed
air which will cause the excessive pressure-feeding of fuel flows into the flow passages,
when the feed pump P1 sucks air with fuel. That is, the variable discharge-type high
pressure pump P shown in the figures provides an excessive pressure-feeding of fuel
preventing effect when controlled according to the control method of the present invention.
[0077] The lower limit value and the tolerance value at steps S601 and S602 are not necessarily
limited to the above values. It is preferred to set the values preliminarily through
experiments to match the specifications of the variable discharge-type high pressure
pump and the like.
(Second Embodiment)
[0078] Fig. 16 shows a control method for a variable discharge-type high pressure pump according
to the second embodiment of the present invention. In this embodiment, the software
interrupt process executed by the electronic control unit C when CNIRQ = 5 is replaced
with the software interrupt process shown in Fig. 17 executed when CNIRQ = 5.
[0079] Description is made primarily on the difference from the first embodiment with the
same processes being designated with the same reference numerals in the figure.
[0080] In this embodiment, step S601 for checking the pump power-on period TF in the first
embodiment is skipped, and only step S602 is executed. The control conditions for
preventing opening of the electromagnetic valves 6a and 6b are limited to only that
the common rail pressure PC is higher than the target common rail pressure PF + tolerance
value. If affirmative at step S602, the power-on flag TFON is set to 0.
[0081] The excessive pressure-feeding of fuel arising from admixed air can also be prevented
in this control method.
[0082] Further, the present invention may be applied to not only the above variable discharge-type
high pressure pump which is constructed to have a control valve and a suction valve
for each of a plurality of pressure chambers, but also other types in which low pressure
fuel is fed to a pressure chamber through a control valve and a suction valve.
[0083] For example, as shown in Fig. 17, the pump may be so constructed that low pressure
fuel fed out from a feed pump and passing through a common control valve 6 flows into
a suction valve 4a through a flow passage 71a and into a suction valve 4b through
a flow passage 71b. The pump may also be so constructed that the control valve and
the suction valve are provided singly for a single pressure chamber as shown in Fig.
18.
[0084] In the above embodiments, the opening period of a control valve is controlled to
control the amount of fuel flowing between a feed pump and a suction valve. However,
the control valve is not limited to the above type, but may be a linear solenoid valve
type which controls its opening area proportionally. The present invention may also
be applied to a system in which the amount of fuel is controlled by varying the opening
area of the control valve.
[0085] A control valve (6a) and a check valve (4a) are provided from the upstream side in
the middle of a flow passage leading from a low pressure pump (P1) to a pressure chamber
(23a) which sucks low pressure fuel and pressure-feed it by its expansion and contraction
of displacement. A variable discharge-type high pressure pump sucks fuel into the
pressure chamber (23a) during a period until the control valve (6a) and the check
valve (4a) are closed, when the displacement of the pressure chamber (23a) expands.
The opening of the control valve (6a) is disabled if the pressure in an accumulation
chamber is higher than a target pressure by more than a tolerance, so that air admixed
in fuel from the low pressure pump (P1) is not allowed to flow into the upstream side
of the check valve (4a). Thus, fuel excess condition in the pressure chamber (23a)
which will be caused when the air expands due to lowering of pressure from a feed
pressure after closing of the control valve (6a) and forces out fuel into the pressure
chamber 23a is avoided, so that excessive pressure-feeding of fuel is prevented.