Information
-
Patent Grant
-
6209525
-
Patent Number
6,209,525
-
Date Filed
Tuesday, October 26, 199925 years ago
-
Date Issued
Tuesday, April 3, 200123 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
- Sughrue, Mion Zinn, Macpeak & Seas, PLLC
-
CPC
-
US Classifications
Field of Search
US
- 123 456
- 123 467
- 123 457
- 123 458
- 123 506
- 123 4467
-
International Classifications
-
Abstract
A fuel supply system for a direct injection gasoline engine can be used in a variable fuel pressure system without using a large pulsation absorber and, as a result, is inexpensive and can be easily reduced in size. The fuel supply system for a direct injection gasoline engine includes a single-cylinder high-pressure pump, a resonator for suppressing the pressure pulsation of high-pressure fuel supplied from the high-pressure fuel pump, and a high-pressure variable regulator for variably changing the pressure of the high-pressure fuel. The fuel-supply system directly injects the high-pressure fuel into the cylinders of the engine through injectors.
Description
FIELD OF THE INVENTION
The present invention relates to fuel supply equipment used in a variable fuel pressure system and, particularly, to fuel supply equipment for a direct injection gasoline engine, which comprises a single-cylinder high-pressure fuel pump and directly injects high-pressure fuel into the cylinders of an engine.
BACKGROUND OF THE INVENTION
Diesel engine technology is widely known as an example of an engine technology where the fuel is injected into its cylinders, which is so called “in-cylinder injection engine” or “direct injection engine”. For spark ignition (gasoline) engine also, in-cylinder injection type has recently been proposed. For such in-cylinder injection engines, it is required that the fuel pressure pulsation should be small enough to achieve stable injection as well as the fuel injection pressure should be sufficiently high.
Therefore, a single-cylinder high-pressure fuel pump which is simple in structure, produced at a low cost and compact is already known.
Since the single-cylinder high-pressure fuel pump has only one plunger, it generates a larger pulsation width in the fuel pressure than a multi-cylinder high-pressure fuel pump does. Therefore, a metal bellows type or metal diaphragm type pulsation absorber is provided in a fuel supply system to absorb the pulsation.
FIG. 8
is a diagram showing the configuration of a fuel supply system for a direct injection gasoline engine disclosed by Japanese Laid-open Patent Application No. 9-310661, for example. In this fuel supply system for a direct injection gasoline engine, the pressure of fuel (gasoline) stored in a fuel tank
70
is increased to a low level by a low-pressure fuel pump
71
and then the fuel is supplied to a high-pressure fuel pump
73
by a low-pressure pipe
72
. The high-pressure fuel pump
73
further increases the pressure of the fuel to a high level by the reciprocating motion of a plunger
75
driven by the cam shaft
74
of an unshown engine and discharges the fuel from an outlet port
76
. This outlet port
76
is connected to a common rail
79
through a high-pressure check valve
77
and a high-pressure pipe
78
. High-pressure fuel stored in the common rail
79
is supplied to injectors
81
attached to the respective cylinders
80
of the engine through branch passages
82
.
This common rail
79
is connected to a metal bellows type pulsation absorber
85
. This metal bellows type pulsation absorber
85
is constituted such that a barrel portion is composed of metal bellows
85
a,
an opening at one end of the metal bellows
85
a
is closed by an end plate
85
b,
a peripheral portion at the other end of the metal bellows
85
a
is connected to the end surface
85
c
of the absorber by welding or the like, a closed space is formed inside the metal bellows
85
a,
and gas such as nitrogen or argon is charged into this closed space. The pressure pulsation of high-pressure fuel to be applied to the end plate
85
b
is absorbed by the expansion and contraction of the metal bellows
85
a
so that the pressure pulsation of the high-pressure fuel supplied into the common rail
79
is absorbed.
FIG. 9
is a sectional view showing the configuration of a high-pressure fuel supply system
10
D equipped with a metal diaphragm type pulsation absorber. The high-pressure fuel supply system
10
D comprises a high-pressure fuel pump
11
, a low-pressure damper
14
provided in an inlet passage
12
connected to an inlet port side of the high-pressure fuel pump
11
and equipped with metal bellows
14
a,
a high-pressure damper
90
provided in an outlet passage
15
connected to an outlet port side of the high-pressure fuel pump
11
and equipped with a metal diaphragm
90
m,
and a high-pressure check valve
17
arranged on a downstream side of the high-pressure damper
90
, all of which are integrally arranged in a casing
100
.
The high-pressure pump
11
pressurizes the low pressure fuel supplied from the unshown fuel inlet port through the inlet passage to a high pressure level and discharges it to the outlet passage
15
by utilizing the plunger
112
which is arranged in a cylinder
111
in such a manner it can reciprocate and is driven by a cam
19
whose rotational speed is a half of an unshown engine's crank speed.
The metal diaphragm type pulsation absorber
90
is provided to suppress the pressure pulsation of this discharged high-pressure fuel. As shown in FIG.
9
and
FIG. 10
, the metal diaphragm type pulsation absorber
90
comprises a case
91
constituting one part of a high-pressure container, a plate
92
constituting the other part of the high-pressure container, and a flexible thin metal disk-like diaphragm
90
m
forming a first high-pressure chamber
93
with the above case
91
and a second high-pressure chamber
94
with the above plate
92
. The above second high pressure chamber
94
is connected via multiple through holes
96
with a recess
95
which constitutes a path between the first passage
15
P to an outlet of the high-pressure fuel pump located in the casing
100
and the second passage
15
Q to a check valve
17
. The above first high-pressure chamber
93
is filled with unshown gas from a gas filling port
97
formed in the case
91
at a predetermined pressure. This predetermined pressure is required to absorb the pulsation of the high-pressure fuel running through the second passage portion
15
Q from the first passage portion
15
P through the recessed portion
95
.
When pulsation occurs in the above fuel while the first high-pressure chamber
93
is filled with gas and the second high-pressure chamber
94
is filled with fuel, the diaphragm
90
m
absorbs the pressure pulsation by bending towards the case
91
and towards the plate
92
from the balance point (for example, a position having no deflection shown by a bold line in
FIG. 10
) where the total of the gas pressure in the first high-pressure chamber
93
and the spring force of the diaphragm
90
m
itself becomes equivalent to the average pressure of the fuel.
However, in the metal diaphragm type pulsation absorber
90
, since the metal diaphragm which is an expansion member expands and contracts repeatedly by an amount equivalent to the pressure pulsation of fuel with the balance point at an average fuel pressure as a center, when this fuel supply system for a direct injection gasoline engine is used in a fuel pressure variable system, the balance point changes, whereby average stress generated in the diaphragm alters, thereby causing a problem with durability.
For instance, when the variable range of fuel supply pressure of the fuel supply system is 5 to 10 MPa and the balance point of the metal diaphragm
90
m
is set to P
0
=7.5 MPa which is the center of the above variable range, as shown in
FIG. 10
, if P
0
=10 MPa, the metal diaphragm
90
m
vibrates with the balance point greatly displaced to the first high-pressure chamber
93
side and if P
0
=5 MPa, the metal diaphragm
90
m
vibrates with the balance point greatly displaced to the second high-pressure chamber
94
side. Since average stress applied to the metal diaphragm
90
m
becomes larger as the balance point displaces more from the center of the variable range, the durability of the metal diaphragm
90
m
deteriorates.
To prevent deterioration in the durability of the metal diaphragm, it is conceivable, for example, to reduce the volume of the first high-pressure chamber
93
so as to lessen the amount of charged gas. In this case, pulsation absorption capability becomes less. It is also possible to improve the durability of the metal diaphragm by reducing average stress to be applied to the metal diaphragm by increasing the diameter. However, in this case, the pulsation absorber becomes large in size.
Even when a metal bellows type pulsation absorber is used as a high-pressure damper, if fuel supply pressure is made variable, the gas charging pressure must be reduced to achieve the minimum fuel pressure and the number of pleats of the metal bellows must be increased to obtain the large expansion width of the metal bellows with the result that the system becomes large in size.
SUMMARY OF THE INVENTION
It is an object of the present invention which has been made in view of the above problems of the prior art to provide a fuel supply system for a direct injection gasoline engine which can be used in a fuel pressure variable system without using a large pulsation absorber, is inexpensive and can be reduced in size.
According to a first aspect of the present invention, there is provided a fuel supply system for a direct injection gasoline engine, which comprises a single-cylinder high-pressure fuel pump, a resonator for suppressing the pressure pulsation of high-pressure fuel supplied from the high-pressure fuel pump and a high-pressure variable regulator for controlling the pressure of high-pressure fuel, wherein the pressure of fuel to be injected into the cylinders of an engine from injectors is made variable, and the pressure pulsation of the fuel is suppressed.
According to a second aspect of the present invention, there is provided a fuel supply system for a direct injection gasoline engine, wherein the high-pressure variable regulator and the resonator are integrated with the high-pressure fuel pump.
The above and other objects, features and advantages of the invention will become more apparent from the following description when taken in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE ACCOMPANYING DRAWINGS
FIG. 1
is a diagram showing the configuration of a fuel supply system for a direct injection gasoline engine according to Embodiment 1 of the present invention;
FIG. 2
is a sectional view of a high-pressure fuel supplier according to Embodiment 1 of the present invention;
FIG. 3
is a diagram showing the configuration of a high-pressure variable regulator;
FIG. 4
is a diagram showing the configuration of another fuel supply system for a direct injection gasoline engine according to Embodiment 1 of the present invention;
FIG. 5
is a diagram showing the configuration of a fuel supply system for a direct injection gasoline engine according to Embodiment 2 of the present invention;
FIG. 6
is a sectional view of a high-pressure fuel supplier according to Embodiment 2 of the present invention;
FIG. 7
is a diagram showing the configuration of another fuel supply system for a direct injection gasoline engine according to Embodiment 2 of the present invention;
FIG. 8
is a diagram showing the configuration of a fuel supply system for a direct injection gasoline engine of the prior art;
FIG. 9
is a sectional view showing the configuration of another fuel supply system for a direct injection gasoline engine of the prior art; and
FIG. 10
is a diagram for explaining the operation of a pulsation absorber.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
Preferred embodiments of the present invention will be described with reference to the accompanying drawings.
Embodiment 1
FIG. 1
shows the configuration of a fuel supply system for a direct injection gasoline engine according to Embodiment 1 of the present invention. In
FIG. 1
, reference numeral
10
denotes a high-pressure fuel supplier equipped with a high-pressure fuel pump
11
,
20
a fuel tank equipped with a low-pressure fuel pump
21
,
30
a common rail storing the fuel supplied from the fuel tank
20
and pressurized by the high-pressure pump
11
,
31
injectors attached to the respective cylinders of an unshown engine and connected to the common rail
30
,
40
a high-pressure fuel passage for connecting the common rail
30
to the high-pressure fuel pump
11
, and
50
a low-pressure fuel passage for connecting the high-pressure pump
11
to the fuel tank
20
. The high-pressure fuel passage
40
and the low-pressure fuel passage
50
form a fuel passage for connecting the injectors
31
of the cylinders to the fuel tank
20
. Letter F is fuel stored in the fuel tank
20
.
As shown in FIG.
1
and
FIG. 2
, the high-pressure fuel supplier
10
comprises the high-pressure fuel pump
11
, an inlet passage
12
constituting part of the low-pressure fuel passage
50
and connected to an inlet port side of the high-pressure fuel pump
11
, a filter
13
arranged in the inlet passage
12
, a low-pressure damper
14
provided between the high-pressure fuel pump
11
and the filter
13
and equipped with metal bellows
14
a,
an outlet passage
15
constituting part of the high-pressure fuel passage
40
and connected to an outlet port side of the high-pressure fuel pump
11
, a resonator
16
which is a means of suppressing the pulsation of high-pressure fuel discharged from the high-pressure fuel pump
11
and communicates with a buffer chamber
15
S provided in the outlet passage
15
, a high-pressure check valve
17
arranged on a downstream side of the resonator
16
for maintaining the pressure of fuel in the common rail
30
to an appropriate level when the engine is suspended, a high-pressure variable regulator
18
arranged on a downstream side of the high-pressure check valve
17
for controlling the pressure of fuel to be supplied to the injectors
31
of the cylinders, a drain passage
18
D for the high-pressure variable regulator
18
and a drain passage
11
D for the high-pressure fuel pump
11
.
The high-pressure pump
11
pressurizes the low pressure fuel supplied from the unshown fuel inlet port through the inlet passage to a high pressure level and discharges it to the outlet passage
15
by utilizing the plunger
112
which is arranged in a cylinder
111
in such a manner it can reciprocate and is driven by a cam
19
whose rotational speed is a half of an unshown engine's crank speed.
Denoted by
113
and
114
are reed valves for sucking and discharging fuel, respectively.
A filter
22
is provided on an inlet side of the low-pressure fuel pump
21
arranged in the fuel tank
20
, and a low-pressure check valve
23
is provided on an outlet side of the low-pressure fuel pump
21
. The outlet side of the low-pressure fuel pump
21
is connected to the fuel inlet port
101
of the high-pressure fuel supplier
10
by a low-pressure pipe
24
. A filter
25
is provided in the low-pressure pipe
24
. Reference numeral
26
denotes a low-pressure regulator provided on the low-pressure pipe
24
, and
27
a low-pressure fuel return pipe for the low-pressure regulator. Reference numeral
28
represents a drain pipe for connecting the drain passage
11
D of the high-pressure fuel pump
11
to the fuel tank
20
, which is connected to a regulator drain pipe
29
for connecting the drain passage
18
D of the high-pressure variable regulator
18
to the fuel tank
20
.
Meanwhile, the fuel outlet port
102
of the high-pressure fuel supplier
10
and the common rail
30
are connected to each other by a high-pressure pipe
32
. Denoted by
33
is a fuel pressure sensor provided on the common rail
30
. A current to be applied to the coil of the above high-pressure variable regulator
18
is controlled by an unshown electronic control unit (ECU) based on the output signal of the fuel pressure sensor
33
.
As shown in
FIG. 3
, the high-pressure variable regulator
18
for controlling the pressure of fuel comprises a needle valve
1
consisting of a valve sheet
1
b
having an orifice
1
a
which is opened to a branch passage
15
K branching off from the outlet passage
15
and a needle
1
c
for opening and closing the orifice
1
a
by contacting to and separating from the valve sheet
1
b,
an unshown magnetic armature connected to the needle valve
1
integrally, an unshown spring for urging this armature downward (direction for closing the needle valve
1
) and a coil
5
for generating a magnetic flux in a magnetic circuit comprising the armature and an unshown magnetic core, and controls the pressure of fuel discharged from the high-pressure fuel pump
11
.
This high-pressure variable regulator
18
urges the needle valve
1
downward by the spring, changes the magnetic flux in the magnetic circuit comprising the magnetic core and the armature corresponding to the current applied to the coil
5
based on a required pressure of the fuel, assists the spring by controlling force for urging the armature downward and adjusts the opening of the needle valve
1
. When the variable range of fuel supply pressure of the fuel supplier is 5 to 10 MPa, for example, a state having zero current applied to the coil
5
is a state where the needle valve
1
is opened most. At this point, the pressure of fuel becomes minimum at 5 MPa. When a current to be applied to the coil
5
is gradually increased, the needle valve
1
is gradually closed, and the pressure of fuel rises. When the supply current is maximum, fuel pressure is controlled to the maximum pressure of 10 MPa by urging the needle valve
1
.
The high-pressure variable regulator may also be of such a type that sets the pressure of the spring to a level corresponding to the maximum pressure of fuel and controls the pressure of fuel by urging the armature upward by the coil
5
.
The resonator
16
is a Helmholtz resonator comprising an orifice
16
a
which is opened to the buffer chamber
15
S of the outlet passage
15
at one end and a fuel control chamber
16
b
connected to an opening portion at the other end of the orifice
16
a
(see FIG.
2
). The amplitude of fuel pressure pulsation at the resonance frequency in the outlet passage
15
that is caused by the discharge pulsation of the high-pressure pump
11
can be reduced by controlling the resonance characteristics of the resonator
16
which are determined by the volume of the fuel control chamber
16
b
and the size of the orifice
16
a.
The resonator
16
has a simple structure consisting of the orifice
16
a
and the fuel control chamber
16
b
and has no expansion member such as a metal diaphragm or metal bellows. Therefore, even when the range of variable fuel supply pressure of the fuel supplier is large, unlike the conventional pulsation absorber, a durability problem does not arise.
A description is subsequently given of the operation of the above fuel supply system for a direct injection gasoline engine. The low-pressure fuel pump
21
sucks fuel through the filter
22
, increases the pressure of the fuel to a low level and discharges the fuel. This low-pressure fuel is supplied to the fuel inlet port
101
of the high-pressure fuel supplier
10
through the low-pressure check valve
23
and the filter
25
by the low-pressure pipe
24
. At this point, when the pressure of the fuel running through the low-pressure pipe
24
exceeds a predetermined low value set by the low-pressure regulator
26
, part of the fuel in the low-pressure pipe
24
is returned to the fuel tank
20
through the low-pressure regulator
26
by the low-pressure fuel return pipe
27
, thereby controlling the pressure of fuel supplied to the high-pressure fuel supplier
10
from the fuel tank
20
to a predetermined value.
The fuel supplied to the inlet passage
12
of the high-pressure fuel supplier
10
is sucked by the high-pressure fuel pump
11
through the filter
13
and the low-pressure damper
14
. The high-pressure fuel pump
11
increases the pressure of the above sucked fuel to a high level, discharges the fuel from the outlet passage
15
and drains fuel leaking from a space between the plunger
112
and the cylinder
111
of the high-pressure pump
11
to the drain passage
11
D. The fuel flowing into the drain passage
11
D is returned to the fuel tank
20
through the drain pipe
29
.
The pulsation of the fuel supplied to the outlet passage
15
is suppressed by the resonator
16
in the buffer chamber
15
S, and then the fuel passes through the high-pressure check valve
17
and is supplied to the common rail
30
from the fuel outlet port
102
through the high-pressure pipe
32
. At this point, the pressure of the fuel running through the outlet passage
15
is controlled to a value set by the high-pressure variable regulator
18
. When the pressure of the fuel exceeds the above set value, part of the fuel in the outlet passage
15
is returned to the fuel tank
20
by the drain passage
18
D and the regulator drain pipe
29
. In this state, the injectors
31
connected to the common rail
30
inject high-pressure fuel into the respective cylinders at a fuel injection timing for each cylinder of the engine.
According to this Embodiment 1, the pressure pulsation of high-pressure fuel discharged from the single-cylinder high-pressure fuel pump
11
is suppressed by the resonator
16
, and the high-pressure variable regulator
18
for controlling the pressure of the high-pressure fuel is provided to control the pressure of high-pressure fuel to be supplied to the injectors
31
connected to the common rail
30
. Therefore, a fuel pressure variable type fuel supply system for a direct injection gasoline engine which is small in size and has durability can be obtained.
In this Embodiment 1, when the pressure of fuel in the outlet passage
15
exceeds the above value set by the high-pressure variable regulator
18
, part of the fuel in the outlet passage
15
(to be referred to as “regulator return” hereinafter) is returned to the fuel tank
20
by the drain passage
18
D and the regulator drain pipe
29
. As shown in
FIG. 4
, the drain passage
18
D may be connected to the inlet passage
12
to return fuel to the inlet side of the high-pressure fuel pump
11
.
Embodiment 2
FIG. 5
is a diagram showing the configuration of a fuel supply system for a direct injection gasoline engine according to Embodiment 2 of the present invention. The high-pressure variable regulator is constructed separately from the high-pressure fuel supplier. Reference numeral
60
denotes a regulator unit which is connected to the high-pressure pipe
32
for connecting the fuel outlet port
102
of a high-pressure fuel supplier
10
A having no high-pressure variable regulator to the common rail
30
and comprises a high-pressure variable regulator
61
and a filter
62
provided on an upstream side of the high-pressure variable regulator
61
. Denoted by
61
D is a drain passage for the high-pressure variable regulator
61
, and
64
a regulator drain pipe for returning regulator return to the fuel tank
20
.
FIG. 6
is a sectional view of the high-pressure fuel supplier
10
A according to Embodiment 2 and diagram typically showing connection between the high-pressure fuel supplier
10
A and the high-pressure variable regulator
61
. The high-pressure fuel is supplied to the high-pressure pipe
32
from the fuel outlet port
102
of the high-pressure fuel supplier
10
A, its pressure is controlled by the high-pressure variable regulator
61
provided in the high-pressure pipe
32
, and the fuel is supplied to the common rail
30
.
As the constituent elements of the high-pressure fuel supplier
10
A and the high-pressure variable regulator
61
are the same as those of Embodiment 1 shown in FIG.
2
and
FIG. 3
, their descriptions are omitted, here.
In this Embodiment 2, regulator return is returned to the fuel tank
20
. As shown in
FIG. 7
, regulator return may be returned to the fuel inlet port
101
of the high-pressure fuel supplier
10
A by a regulator drain pipe
65
.
As having been described above, according to the first aspect of the present invention, a single-cylinder high-pressure fuel pump, a resonator for suppressing the pressure pulsation of high-pressure fuel supplied from the high-pressure fuel pump and a high-pressure variable regulator for controlling the pressure of the high-pressure fuel are provided, the pressure of fuel to be injected into the cylinders of the engine from the injectors can be changed, and the pressure pulsation of the fuel is suppressed. Therefore, a fuel pressure variable type fuel supply system for a direction injection gasoline engine which is small in size and has durability can be obtained.
According to the second aspect of the present invention, since the high-pressure variable regulator and the resonator are integrated with the high-pressure pump, the system can be further reduced in size.
Claims
- 1. A fuel supply system for a direct injection gasoline engine, comprising:a single-cylinder high-pressure fuel pump that supplies high-pressure fuel; a resonator for suppressing pressure pulsation of the high-pressure fuel supplied from the high-pressure fuel pump; and a high-pressure variable regulator for variably changing the pressure of the high-pressure fuel supplied by the high-pressure fuel pump, wherein the system outputs variably regulated high-pressure fuel for being directly injected into cylinders of the engine.
- 2. The fuel supply system for a direct injection gasoline engine according to claim 1, wherein the high-pressure variable regulator and the resonator are integrated with the high-pressure fuel pump.
- 3. The fuel supply system for a direct injection gasoline engine according to claim 1, further comprising a high-pressure check valve disposed between the high-pressure fuel pump and the high-pressure variable regulator.
- 4. The fuel supply system for a direct injection gasoline engine according to claim 1, further comprising a low-pressure fuel pump for supplying low-pressure fuel to an inlet of the high-pressure fuel pump.
- 5. The fuel supply system for a direct injection gasoline engine according to claim 1, wherein the high-pressure variable regulator is electrically-controllable for effecting the variable changing of pressure.
- 6. The fuel supply system for a direct injection gasoline engine according to claim 5, further comprising an electrical control unit (ECU) operative to provide electrical control of the high-pressure variable regulator.
Priority Claims (1)
Number |
Date |
Country |
Kind |
11-094741 |
Apr 1999 |
JP |
|
US Referenced Citations (19)
Foreign Referenced Citations (2)
Number |
Date |
Country |
9-310661 |
Dec 1997 |
JP |
10-299609 |
Nov 1998 |
JP |