Information
-
Patent Grant
-
6726128
-
Patent Number
6,726,128
-
Date Filed
Thursday, January 16, 200322 years ago
-
Date Issued
Tuesday, April 27, 200420 years ago
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Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 239 5332
- 239 90
- 239 92
- 239 88
- 239 1022
- 123 506
- 123 503
- 123 458
- 123 500
- 123 446
- 123 479
- 123 501
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International Classifications
-
Abstract
A unite injector a unit injector for injecting fuel into the combustion chamber of a self-igniting internal combustion engine, including a pump part a nozzle part and an final control element that is followed downstream by a hydraulic coupler which actuates a valve needle of a 2/2-way valve inside a nozzle body. The final control element includes a piezoelectric crystal array. The hydraulic coupler acts on the face end of the valve needle in such a way that it can be put into a first position that enables a pressure buildup, and a further position of the valve needle that enables the opening of a nozzle needle, with the pressure buildup and the valve opening being separately adjustable.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
In injection systems of the UIS (unit injector system) type, a final control element, via a hydraulic coupler, closes the high-pressure chamber of a fuel injection pump. In the UI systems, the pressure is built up by means of a piston. When a certain value is reached, the pressure opens the injection valve.
2. Description of the Prior Art
With pump-nozzle systems (UIS or unit injector systems), mechanically-hydraulically controlled injection phases are presently generated in self-igniting internal combustion engines, and these phases contribute on the one hand to noise abatement and on the other to minimizing pollution. In unit injection systems, a distinction is made among four operating states. A pump piston is moved upward via a restoring spring. The fuel, which is under constant overpressure, flows out of the low-pressure part of the fuel supply via the inlet bores, integrated with the engine block, and the inlet conduit into a valve chamber of a magnet valve. The magnet valve is opened. Via a connecting bore, the fuel enters the high-pressure chamber.
Upon a rotation of the drive cam, the pump piston moves downward. The magnet valve remains in its open position, and the fuel is pressed by the pump piston, via the return conduit, into the low-pressure part of the fuel supply.
In a third phase of the injection event, when an electromagnetic valve is used, the coil of the electromagnet is supplied with current at a certain instant by the control unit, so that the magnet valve needle is pulled into a seat, and the communication between the high-pressure chamber and the low-pressure part is closed. This instant is also known as the “electrical injection onset”. The fuel pressure in the high-pressure chamber rises continuously as a result of the motion of the pump piston, and as a result a rising pressure is also established at the injection nozzle. When a nozzle opening pressure of approximately 300 bar is reached, a lifting of the nozzle needle occurs, causing fuel to be injected into the combustion chamber. This instant is also called the “actual injection onset”, or as the supply onset. Because of the high pumping rate of the pump piston, the pressure continues to rise further during the entire injection event. In a concluding operating state, the coil of the electromagnet is switched off again, after which, after a slight delay time, the magnet valve opens, and the communication between the high-pressure chamber and the low-pressure part is again opened. In this transition phase, the peak pressure is reached, which depending on the pump type varies between a maximum of 1800 and a maximum of 2050 bar. After that, the pressure collapses very quickly. When it falls below the nozzle closing pressure, the injection nozzle closes and terminates the injection event. The remaining fuel pumped by the pump element until the apex point of the drive cam is forced into the low-pressure part of the fuel system via the return conduit.
As a rule, such unit injector systems, used for instance in injection systems for trucks, include two final control elements embodied as electromagnets. When there are two final control elements, the unit injector system requires more space, which when such injection systems are used in utility vehicles is available. It is therefore easily possible to accommodate the final control elements embodied as magnet valves in Diesel engines for trucks. In passenger cars, however, there is only limited space available in the engine compartment, especially in the upper region of the cylinder block, and this codetermines the outer dimensions of a unit injector system. If instead of final control elements in the form of two electromagnet valves, only one electromagnet valve is used, then there is the disadvantage that the valve can be kept in an intermediate position only highly imprecisely and at high effort and expense in terms of regulation.
OBJECT AND SUMMARY OF THE INVENTION
The advantage of the embodiment proposed according to the invention is above all that the closure of the high-pressure chamber of the unit injector system can be controlled separately for the pressure buildup and for the opening of the nozzle needle. Thus the injection pressure, that is, the pressure at which the nozzle needle opens, can be varied freely.
If a piezoelectric actuator is used, then its stroke length can be varied arbitrarily by varying the voltage at the piezoelectric actuator. The final control element, embodied as a piezoelectric actuator, of the unit injector can be followed downstream by a hydraulic pressure booster, in order to achieve the requisite stroke lengths within the housing of the unit injector. An final control element embodied as a piezoelectric actuator can be switched to various switching positions by means of supplying suitable current. In the voltage-free state of the piezoelectric actuator without any current, the nozzle needle assumes an open position; that is, fuel is pumped at low pressure by the fuel feed pump through the unit injector. In this position of the nozzle needle, the low-pressure side inlet and the inlet to a high-pressure side pump chamber communicate with one another by a short circuit, since the openings corresponding to them inside the housing of the unit injector are uncovered by the nozzle needle.
At maximum current supply to the piezoelectric final control element, the nozzle needle is moved downward; that is, the low-pressure side inlet and the high-pressure side inlet to the pump chamber are both closed. The pressure buildup begins in this phase, without the nozzle needle being opened by the steadily rising pressure. Conversely, once the desired injection pressure has been built up in the unit injector, the current supply to the piezoelectric final control element is withdrawn, as a result of which the nozzle needle opens with pressure reinforcement.
The end of the injection is brought about by opening the return, which causes the closure of the nozzle needle. With this provision, with an final control element embodied as a piezoelectric actuator, the pressure buildup and the opening of the nozzle needle can be controlled separately from one another in a unit injector, which allows freedom of choice in terms of the injection pressure built up.
BRIEF DESCRIPTION OF THE DRAWING
The invention will be better understood and further objects and advantages thereof will become more apparent from the ensuing detailed description of preferred embodiments taken in conjunction with the drawings, in which:
FIG. 1
shows a unit injector that is actuatable by means of a magnet valve;
FIG. 2.1
shows a piezoelectric actuator with a hydraulic coupling chamber in a first switching position;
FIG. 2.2
shows the piezoelectric final control element with a downstream hydraulic coupling chamber, with the nozzle needle fully closed;
FIG. 2.3
shows the piezoelectric final control element with the downstream hydraulic coupling chamber in an intermediate position that is triggered with pressure reinforcement; and
FIG. 3
shows the voltage profile with which the piezoelectric actuator can be triggered.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
FIG. 1
shows a unit injector, which is actuatable with an final control element embodied as a piezoelectric actuator.
It can be seen from the illustration in
FIG. 1
that the unit injector
1
shown there includes both a pump part
2
and a nozzle part
3
. The nozzle part
3
of the unit injector
1
is let into the cylinder head
4
of a self-igniting internal combustion engine not shown in further detail. The nozzle part
3
of the unit injector
1
is screwed into a cylinder head bore
22
and is received sealingly in the cylinder head bore
22
by means of both a spacer disk
32
and O-rings
33
.
An final control element
5
, which is embodied as a piezoelectric final control element and which includes a piezoelectric crystal array in stacked form, is received laterally on the pump part
2
of the unit injector
1
. The electrical triggering of the piezoelectric crystal stack
7
is effected via a plug connection
6
received laterally on the final control element
5
. The final control element
5
is received laterally on the pump housing
8
of the pump part
2
of the unit injector
1
and acts upon a hydraulic coupler
38
, which via a coupler line
39
acts on the end face of a valve needle
24
disposed displaceably in a nozzle body
23
of the nozzle part
3
. A pump piston
9
is let into the pump housing
8
of the pump part
2
of the unit injector
1
and is actuated under camshaft control via a tilt lever
17
. The face end
11
of the pump piston
9
defines a pressure chamber
10
in the pump housing
8
.
The pump piston
9
is moved in the axial direction in the pump housing
8
and is prestressed by a spring element
12
, embodied here as a spiral spring. The spring element embodied as a spiral spring
12
is braced on one end on a collar
13
of the pump housing
8
and on the other on a spring plate
14
that is penetrated by a pressure bolt
15
. The pressure bolt
15
is braced on one end on a ball-socketlike element
16
and acts upon the face end, remote from the pump chamber
10
, of the pump piston
9
. The pressure bolt
15
, which is received with its lower end in a bolt socket
16
, is surrounded, on its end facing the bolt socket
16
, by a tilt lever
17
that is rotatable about a tilt lever shaft
18
. On the end of the tilt lever
17
opposite the pressure bolt
15
, a tilt lever roller
19
is rotatably supported, which with its outer circumferential face rolls on an eccentric cam
21
that is embodied on a camshaft
20
. By means of the outer circumferential contour of the eccentric cam
21
, the axial motion of the pump piston
9
, transmitted via the tilt lever
17
, is generated inside the pump housing
8
.
The nozzle body
23
of the nozzle part
3
is let into the cylinder head bore
22
and includes a valve needle
24
, which is moved in the axial direction inside the nozzle body
23
. The upper face end
40
of the valve needle
24
communicates via the coupler line
39
with the hydraulic coupler
38
, which in turn is acted upon by the piezoelectric crystal stack array
7
of the final control element
5
. Moreover, the valve needle
24
of the 2/2-way valve in the nozzle body
23
is acted upon a restoring spring. The restoring spring, which is associated with the face end of the valve needle
24
remote from the face end
40
, is braced in turn on a disklike element, which is acted upon by a nozzle needle spring
35
. A high-pressure line branches off from the pump chamber
11
in the pump housing
8
of the pump part
2
and via the control chamber inlet
26
acts upon the control chamber
25
of the valve needle
24
, and at the same time, via the nozzle chamber inlet
27
, it acts with fuel that is at high pressure upon the nozzle chamber
28
in the nozzle body
23
, which chamber receives the nozzle needle
29
that is received displaceably in the nozzle body
23
. From the nozzle chamber
28
, the fuel that is at high pressure flows via an annular gap
30
in the direction of the nozzle tip, where at least one injection opening
31
is embodied that protrudes into a combustion chamber, not shown in
FIG. 1
, of a self-igniting internal combustion engine. The nozzle needle
29
is guided in the end toward the combustion chamber of the nozzle body
23
and is prestressed by the nozzle needle spring
35
. The axial position of the nozzle body
23
in the cylinder head
4
is determined by the thickness of a spacer disk
32
. The sealing function between the combustion chamber and the cylinder head
4
is performed by the spacer disk
32
and by a number of O-rings
33
.
Located laterally of the nozzle body
23
inside the cylinder head
4
is a fuel return, identified by reference numeral
36
, that is disposed above a fuel inlet, identified by reference numeral
37
, to the nozzle body
23
. The nozzle body
23
communicates with the part oriented toward the combustion chamber of the self-igniting internal combustion engine via a nozzle lock nut
34
. This nut tightens the two parts of the nozzle body
23
against one another and creates a fuel-tight connection between the pump chamber
10
of the pump part
2
and the high-pressure inlets
26
,
27
to the control chamber
25
and nozzle chamber
28
, respectively.
FIG. 2.1
shows a piezoelectric final control element with a hydraulic coupling chamber, which is put into a first switching position.
In the first position
41
, shown in
FIG. 2.1
, of the valve needle
24
in the nozzle body
23
, the piezoelectric crystal stack array
7
of the final control element
5
is not being supplied with current. Accordingly, the hydraulic coupler
38
is not acted upon. The valve needle
24
in the nozzle part
3
of the unit injector
1
has moved upward by a first stroke length
45
, relative to its seat toward the nozzle body. In this switching position, the inlet
37
, which is schematically shown in
FIGS. 2.1
,
2
.
2
and
2
.
3
as disposed above the return
36
in the nozzle body
23
, and the return
36
are both open. In the voltage-free state, shown in
FIG. 2.1
, of the final control element
5
, the valve needle
24
is open; the fuel is pumped by the fuel feed pump at low pressure through the nozzle part
2
of the unit injector
1
. In this first position
41
of the valve needle
24
, the final control element
5
, or in other words its piezoelectric crystal stack array
7
, is not being supplied with current, which corresponds to the voltage level shown in
FIG. 3
before the ascending edge
50
of the voltage.
In
FIG. 2.2
, the piezoelectric final control element with the downstream hydraulic coupler
38
is being supplied with maximum voltage, corresponding to the first voltage level
54
shown in FIG.
3
. As a result, the piezoelectric crystal stack array
7
of the final control element
5
moves into the hydraulic coupler
38
in such a way that via the coupler line
39
, shown in
FIG. 1
, the face end
40
of the valve needle
24
is acted upon by high pressure. As a result, the valve needle
24
of the 2/2-way valve moves downward all the way inside the needle guide
44
and closes both the inlet
37
and the return
36
. In the second position
42
, shown in
FIG. 2.2
, of the valve needle
24
, the pressure buildup takes place in the high-pressure chamber, that is, in the pump chamber
10
of the pump part
2
. The second position
42
of the valve needle
24
is maintained during the pressure buildup phase
52
. During the pressure buildup phase
52
(see the voltage profile in FIG.
3
), the pressure buildup takes place in the high-pressure chamber, that is, in the pump chamber
10
inside the pump housing
8
, until a desired pressure level is reached.
FIG. 2.3
shows the piezoelectric final control element with the downstream hydraulic coupler in a further, third position
43
.
For attaining a switching state of the valve needle
24
corresponding to the third position of the valve needle
24
, the current supply to the piezoelectric crystal stack array
7
of the final control element
5
is withdrawn to a second voltage level
56
(see FIG.
3
). The voltage drops along a first descending voltage edge
55
from the first voltage level
54
, which is maintained during the second position
42
of the valve needle
24
, back to a second, lower voltage level
56
(see FIG.
3
).
Because of this, the pressure in the hydraulic coupler
38
and in the coupler line
39
drops, so that the valve needle
24
, whose face end
40
is acted upon by the high pressure, moves upward by a second stroke length
46
in the vertical direction relative to the nozzle body
23
. In the third position
43
of the valve needle
24
, the return
36
is opened, while the inlet
37
remains closed by the valve needle
24
, analogously to what is shown in
FIG. 2.2
. The nozzle needle
29
(see
FIG. 1
) is as a result opened with pressure reinforcement. The injection ends by opening of the return
36
, since the opening of the return
36
has the effect of an immediate pressure reduction and the closure of the nozzle needle
29
.
FIG. 3
shows the voltage profile with which the piezoelectric final control element, in the form of a piezoelectric actuator, that double-switches the 2/2-way valve is triggered.
In the state of the piezoelectric final control element
5
when it is not being supplied with current, the voltage is equivalent to the level that prevails in
FIG. 3
before the ascending edge
50
of the voltage. The pressure buildup phase
52
is generated by the ascending edge
50
of the voltage up to a first voltage level
54
. The supply onset is indicated by reference numeral
51
. The pressure buildup phase
52
can be kept variable and is independent, that is, separate, from the triggering of the nozzle needle
29
by actuation of the valve needle
24
. During the pressure buildup phase, the piezoelectric final control element
5
is supplied with current at the first voltage level
54
. The pressure buildup takes place without the unit injector being opened by the nozzle needle
29
as a result of the pressure being built up in the pump chamber
10
. As soon as the desired injection pressure level and the desired instant for the injection onset
53
is reached, the first voltage level
54
is lowered to a second voltage level
56
. While the first voltage level
54
prevails, the valve needle
24
of the 2/2-way valve of the unit injector
1
is in the second position, which is marked
42
in the
FIG. 2.2
; that is, both the inlet
37
and the return
36
to the pump chamber
11
are closed. If the first voltage level
54
is lowered along the first, descending voltage edge
55
to the second voltage level
56
, a relief of the hydraulic coupler
38
takes place, since the piezoelectric crystal array
7
contracts upon the application of a low voltage level corresponding to the second voltage level
56
. Accordingly, the valve needle
24
moves by the second stroke length
46
, shown in
FIG. 2.3
, into its third position. In the third position, the inlet
37
is still closed, while the return
36
to the pump chamber
11
remains open. The second voltage level
56
prevails until the end of supply
57
by the fuel pump and then drops along a further, second, descending voltage edge
58
to the 0 level. At the 0 level of the voltage V, the valve needle
24
again assumes the first position
41
shown in
FIG. 2.1
, in which the nozzle needle traverses a first stroke length
45
inside the nozzle body
23
, and in which the inlet
37
and the return
36
are short-circuited to one another. By means of the valve needle
24
of the 2/2-way valve inside the nozzle body
23
, the closure of the high-pressure chamber, that is, of the pump chamber
10
of the pump part
2
, is controlled separately from one another for the pressure buildup and for the opening of the nozzle needle
29
. The injection pressure can be controlled freely in accordance with the instant of triggering of the final control element
5
, at which the first voltage level
54
is lowered to the second voltage level
56
, and the pressure buildup phase remains unaffected.
The foregoing relates to preferred exemplary embodiments of the invention, it being understood that other variants and embodiments thereof are possible within the spirit and scope of the invention, the latter being defined by the appended claims.
Claims
- 1. In a unit injector (1) for injecting fuel into the combustion chamber of a self-igniting internal combustion engine, having a pump part (2), a nozzle part (3) and a final control element (5) that is followed downstream by a hydraulic coupler (38, 39) by way of which a valve needle (24) of a 2/2-way valve inside a nozzle body (23) is actuatable, the improvement wherein the final control element (5) comprises a piezoelectric crystal array (7) acting on the hydraulic coupler (38, 39) which acts upon one face end (40) of the valve needle (24) to put the valve needle (24) into a first position (41) that enables a pressure buildup, and a second position (42) of the valve needle (24) that enables the opening of a nozzle needle (29), whereby the pressure buildup and the valve opening are adjustable independently.
- 2. The unit injector in accordance with claim 1, wherein the hydraulic coupler (38, 39) in the nozzle body (23) changes over into a needle guide (44) that guides the valve needle (24).
- 3. The unit injector in accordance with claim 1, further comprising a control chamber inlet (26) and a nozzle chamber inlet (27) branching off from the pump chamber (10) of the pump part (2) and simultaneous act upon a control chamber (25) of the valve needle (24) and a nozzle chamber (28) surrounding the nozzle needle (29).
- 4. The unit injector in accordance with claim 1, wherein, viewed in the longitudinal direction of the nozzle needle (29) in the nozzle body (23), a fuel inlet (37) is disposed above a return (36).
- 5. The unit injector in accordance with claim 4, wherein in the first position (41) of the valve needle (24), with no current being supplied to the final control element (5), the fuel inlet (37) and the return (36) in the nozzle body (23) are open.
- 6. The unit injector in accordance with claim 5, wherein in the first position (41) of the valve needle (24), a first stroke length (45) of the valve needle (24) is established, at which the fuel inlet (37) and the fuel return (36) are open.
- 7. The unit injector in accordance with claim 4, wherein when current at a first voltage level (54) is supplied to the final control element (5), the inlet (37) and the return (36) are closed by the valve needle (24), and a pressure buildup phase (52) takes place in the pump chamber (10) of the pump part (2).
- 8. The unit injector in accordance with claim 4, wherein after a pressure buildup phase (52) in the pump chamber (10) of the pump part (2) has elapsed, at an injection onset (53), the final control element (5) is subjected to a second voltage level (56), and the nozzle needle (29) opens, with pressure reinforcement.
- 9. The unit injector in accordance with claim 8, wherein the injection onset (53) and the pressure buildup phase (52) are controllable separately from one another by means of closure of the pump chamber (10).
- 10. The unit injector in accordance with claim 8, wherein in a third position (43) of the valve needle (24), a second stroke length (46) of the valve needle (24) is established, at which the fuel return (36) to the pump chamber (10) is opened.
Priority Claims (1)
Number |
Date |
Country |
Kind |
102 01 470 |
Jan 2002 |
DE |
|
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A |
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A |
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