Information
-
Patent Grant
-
6811103
-
Patent Number
6,811,103
-
Date Filed
Monday, September 30, 200222 years ago
-
Date Issued
Tuesday, November 2, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
- Venable LLP
- Voorhees; Catherine M.
-
CPC
-
US Classifications
Field of Search
US
- 239 88
- 239 89
- 239 90
- 239 91
- 239 95
- 239 96
- 239 5332
- 239 5851
- 239 5852
- 239 5855
- 123 467
- 123 506
- 123 60114
-
International Classifications
-
Abstract
The invention relates to a fuel injection device for a reciprocating internal combustion engine, comprising a nozzle part (5) with an injection nozzle (13), said nozzle part having a pressure chamber (10) in which a nozzle needle (9) that closes the injection nozzle (13) is guided. Said nozzle needle can be moved into the opening position when subjected to pressure by the fuel to be injected. The pressure chamber (10) is connected to a control part (7) by a connecting channel (6), this control part having a valve chamber (21) into which the connecting channel (6) and a high pressure channel (8) that is connected to a fuel supply (4) open, and in which a valve body (23) is guided. Said valve body (23) acts as a piston system and is held in the closing position by a valve spring and a valve seat (22). The nozzle part also comprises an actuator part (20) which is functionally connected to the valve body (23) and which when activated, moves said valve body in the opening direction and releases the through-flow from the high pressure channel (8) into the connecting channel (6).
Description
Fuel injection devices embodied as so-called common rail systems, for a reciprocating internal combustion engine with direct fuel injection, essentially comprise a nozzle part with an injection nozzle, which part has a nozzle needle that closes the injection nozzle and that is movable in the opening position via servo hydraulics upon imposition of pressure by the fuel to be injected. The requisite pilot pressure is taken from the high-pressure part of the fuel supply, that is, the common rail. Via the pressure specification in the common rail, the injection pressure can be varied quite flexibly, and via the triggering of a servo valve, and thus of the nozzle needle, the instant of injection and duration of injection can also be adjusted with great flexibility.
However, if with the known systems not only the injection quantity is to be dimensioned, by a suitable control of the opening time, but the injection rate is also to be formed, that is, the injection quantity per unit of time is to be varied during the opening time, then the stroke of the nozzle needle must be controlled. However, the hydraulic energy of the flowing fuel is set to turbulence immediately upstream of the injection port of the injection nozzle by the so-called seat throttling, which occurs especially at a relatively short needle stroke, since the free flow cross section between the nozzle needle and the nozzle needle seat, which varies as a function of the stroke, acts as a throttle. The resultant increased turbulence in the flowing fuel in the region of the injection port affects the mixture formation, so there is no “genuine” rate control. In direct fuel injection, that is, injection of the fuel directly into the cylinder chamber, this is disadvantageous. As a consequence of this increase in turbulence, at small injection quantities, for instance, [injection quantities, for instance,] (sic) combustion near the nozzle of the injected fuel quantity has been found, which adversely affects the course of the combustion process.
From U.S. Pat. No. 5,526,791, German Patent Disclosure DE-A 43 41 546, and German Utility Model DE-U 297 17 649, fuel injection devices are known that each have a valve body which can be displaced into the open position by an activated actuator and allows the inflow of fuel at high pressure. If the actuator is inactivated, a restoring spring pushes the valve body back into the closing position.
The object of the invention is to create a fuel injection device for direct fuel injection that makes it possible during the applicable injection time to vary the injection quantity, or in other words to shape the injection rate.
This object is attained by a fuel injection device for a reciprocating internal combustion engine, having a nozzle part with an injection nozzle, which part has a pressure chamber in which a nozzle needle that closes the injection nozzle is guided, which needle is movable in the opening position upon imposition of pressure by the fuel to be injected, wherein the pressure chamber communicates via a connecting channel with a control part which has a valve chamber, into which the connecting channel on the one hand and a high-pressure channel, communicating with a fuel supply, on the other discharges, and in which a valve body acting as a piston system is guided, which body is kept in the closing position on a valve seat by a valve spring, and having an actuator, which is operatively connected to the valve body and which moves the valve body in the opening direction upon activation and enables the flow from the high-pressure channel into the connecting channel, and having a compensation piston, which can be acted upon via the pressure in the connecting channel in the opposite direction from the exertion of force by the actuator.
In the fuel injection device of the invention, the nozzle part is embodied such that upon pressure imposition, the nozzle needle opens the flow cross section to the nozzle openings as completely as possible; no intermediate positions are provided. The control of the volumetric flow is effected via the valve body, provided in the control part, whose stroke is variable by means of suitable triggering of the actuator. The valve body is preferably embodied as a seat valve, to assure tightness in the closed state. The actuator is expediently embodied such that in terms of its adjustment travel, it is embodied adjustingly in proportion to the adjustment energy applied. Electrical actuators which are embodied adjustingly in proportion to voltage in terms of their adjustment travel, of the kind embodied by so-called solid-state actuators, are especially suitable for this purpose. As solid-body actuators, piezoelectric actuators can be considered in particular, but also magnetostrictive actuators. Electromagnetically functioning actuators can also be used. It is advantageous to dispose a compensation piston of suitable diameter, which can be acted upon via the pressure in the connecting channel toward the nozzle part and accordingly acts counter to the force of the actuator. This produces a so-called pressure feedback, which enables good regulability of the volumetric flow flowing from the high-pressure side to the connecting channel, and thus enables good shaping of the injection rate.
It is especially expedient if in one embodiment, the valve body is provided, on an end remote from the actuator, with a compensation piston which can be acted upon via the pressure in the connecting channel.
In a feature of the invention, it is provided that the control part has a relief valve, opening toward the low-pressure side of the fuel supply, which is associated with the connecting channel and closes upon activation of the actuator. By the disposition of a relief valve of this kind, care is taken to assure that immediately upon seating of the valve body in the control part on its valve seat, the pressure in the connecting channel toward the nozzle part is rapidly decreased, so that the nozzle needle is also guided very quickly into its closing direction.
In an especially advantageous feature of the invention, it is also provided that the control part has a pressure divider, which communicates on the one hand with the high-pressure channel and on the other with the valve body with a compensation piston, forming a piston system, and which is adjustable via the actuator. Disposing a pressure divider in the control part in this way enables dynamic adjustment of whatever injection pressure is desired. Depending on the embodiment, the arrangement can be such that depending on the type of actuator used, the injection pressure can be adjusted upstream of a pressure-controlled injection nozzle, either via the adjustment travel of the actuator or via the force of the actuator.
Further characteristics and features of the invention can be learned from the claims and the ensuing description of exemplary embodiments.
The invention will be explained in further detail in terms of schematic drawings of exemplary embodiments. Shown are:
FIG. 1
, a circuit diagram of a fuel injection device;
FIG. 2
, an exemplary embodiment of a fuel injection valve with a nozzle part and control part;
FIG. 3
, a modified embodiment of the control part;
FIG. 4
, a further modification of the control part;
FIG. 5
, the detail A in
FIG. 4
on a larger scale;
FIG. 6
, a modified embodiment with a pressure divider integrated with the control part;
FIG. 7
, the pressure divider of
FIG. 6
on a larger scale;
FIG. 8
, an embodiment of the pressure divider with a support piston;
FIG. 9
, an embodiment of the pressure divider with a hydraulic travel booster;
FIG. 10
, an embodiment of the fuel injection nozzle with a two-spring support;
FIG. 11
, an embodiment of the fuel injection nozzle with an escape piston.
In
FIG. 1
, a fuel injection device for direct injection of the fuel into the individual cylinders of a reciprocating internal combustion engine is shown in the form of a flow chart. The fuel injection device has a fuel supply
1
, which is essentially formed by a fuel tank
2
, a high-pressure pump
3
, and a high-pressure chamber
4
or so-called common rail.
Each cylinder of the reciprocating internal combustion engine is provided with a nozzle part
5
, which communicates with the fuel supply
1
via a connecting channel
6
, a control part
7
, and a high-pressure channel
8
. The control part
7
further communicates with an engine controller, not shown in detail here, by which the control part
7
, acting as a control valve, can be triggered such that at the instant of injection, the communication between the high-pressure channel
8
and the connecting channel is opened, and the fuel that is at high pressure can act on the nozzle part
5
. The special mode of operation will be described in further detail hereinafter.
The nozzle part
5
is essentially formed by a nozzle needle
9
, which is guided in a pressure chamber
10
into which the connecting channel
6
discharges. The nozzle needle
9
has a needle tip
11
, which cooperates with a corresponding seat
12
of the injection nozzle
13
and acts as a valve. The injection nozzle
13
is provided with corresponding nozzle openings
14
. On the side remote from the needle tip
11
, the nozzle needle
9
is provided with a piston body
15
, on which a closing spring
16
acts in the closing direction. If the communication between the high-pressure channel
8
and the connecting channel
6
is opened via the control part
7
and the pressure chamber
10
and thus the piston body
15
are acted upon by pressure, then the nozzle needle
9
lifts from its valve seat
12
, so that the fuel from the pressure chamber
10
can emerge through the nozzle openings
14
into the combustion chamber of the applicable cylinder of the reciprocating internal combustion engine, in the form of a fine mist. As soon as the communication with the high-pressure chamber
4
is closed via the control part
7
, the nozzle needle
9
is pressed back onto its valve seat via the closing spring
16
, and the fuel delivery is terminated.
Upon the return of the control part
7
to its closing direction, a communication between the connecting channel
6
and a low-pressure channel
17
is opened, so that the pressure chamber
10
is pressure-relieved and the nozzle needle can rapidly be returned to its closing direction. The nozzle part
5
acting as an injection valve is conceived of in the exemplary embodiment such that upon imposition of pressure, it opens the injection nozzle
13
completely and closes it upon pressure relief, so that depending on the triggering via the control part
7
, opening and closure of the injection nozzle at precise times is assured. In the arrangement shown in
FIG. 10
of two closing springs
16
.
1
and
16
.
2
with different spring stiffness, the goal is for the nozzle needle
9
to be capable of assuming two opening positions as a function of pressure.
The closing spring
16
is disposed in a leakage chamber
18
, which communicates via a leakage line
19
with the low-pressure line
17
, so that the amounts of leakage collecting in the leakage chamber
18
can be diverted into the fuel tank
2
.
The actuator
20
is preferably embodied such that in terms of its adjustment travel, it is embodied adjustingly in proportion to the adjustment energy applied. In an embodiment of the control part
7
, for instance as a throttle valve, the possibility thus exists of varying the volumetric flow, flowing out of the high-pressure channel
8
into the connecting channel
6
, by suitably adjusting the opening cross section in the control part
7
. Since upon pressure imposition, the nozzle part
5
embodied as an injection valve opens completely, in the schematic example shown, it is possible via a suitable change in the adjustment of the control part
7
for the volumetric flow delivered to the nozzle part
5
to be varied during the duration of opening of the injection nozzle
13
.
The structure and function of the control part
7
will now be described in further detail in terms of various exemplary embodiments.
The actuator
20
is advantageously embodied as a so-called solid-state actuator. Preferably, an actuator functioning piezoelectrically is used, which in terms of its adjustment travel, or because of its mechanical resilience, is embodied as adjusting its adjusting force in proportion to voltage. Instead of a piezoelectric actuator, the use of a magnetostrictive actuator is also possible, which is embodied as adjusting in proportion to current in terms of its adjustment travel. Since such solid-state actuators are distinguished by high switching speed, good regulability of the adjustment travel, and also high adjusting forces and moreover act directly, or optionally via a hydraulic stroke boost, on the adjusting part in the control part
7
, the possibility is obtained, even at only short opening times for the nozzle part
5
embodied as an injection valve, of purposeful shaping of the injection rate, that is, a purposeful change in the volumetric flow introduced into the combustion chamber of the applicable cylinder during the opening time of the injection valve.
While it is possible in principle to use the nozzle part
5
and the control part
7
as separate component units, in
FIG. 2
an embodiment is shown in which the nozzle part
5
and control part
7
are embodied together with the actuator
20
as a structural unit. From the description of this exemplary embodiment, the special features of the embodiment of the control part
7
indicated above can also be found. Reference numerals used in
FIG. 1
for components described above are also adopted in
FIG. 2
, so that the above description can be referred to.
As can be seen from
FIG. 2
, the entire arrangement comprises a carrier body, constructed in multiple parts for production reasons, which is characterized by a coaxial relationship among the nozzle part
5
, control part
7
and actuator
20
.
The control part
7
has a valve assembly
21
.
0
with a valve chamber
21
.
1
, into which the high-pressure channel
8
on the one hand and the connecting channel
6
on the other discharge. The valve chamber
21
.
1
is provided with a valve seat
22
, on which a valve body
23
embodied as a piston system is held in the closing direction by its valve part
23
.
1
via a valve spring
24
, so that the high-pressure channel
8
is blocked off from the connecting channel
6
. The structural space required for the valve spring
24
communicates with the leakage line
19
. Some of the portions
23
.
1
,
23
.
2
,
23
.
3
and
23
.
4
have different diameters here.
On the side remote from the valve spring
24
, the actuator
20
acts on the valve body
23
; in the exemplary embodiment shown here, it is embodied as a piezoelectric actuator. The piezoelectric actuator
20
is essentially formed by a stack of piezoelectric bodies
20
.
1
, which are connected to a controllable voltage source, not shown here, and are braced on one end on a housing part
20
.
2
and on the other act on a transmission piston
20
.
3
. The transmission piston
20
.
3
is assigned a hydraulic chamber
20
.
4
, which is filled in a known manner with a fluid, in this case fuel.
On the side toward the control part, the hydraulic chamber
20
.
4
is assigned a pressure piston
23
.
1
, which communicates with the valve body
23
. If the piezoelectric body
20
.
1
is subjected to a voltage, then the transmission piston is moved forward in the direction of the hydraulic chamber
20
.
4
, and then under the influence of the fluid contained in the hydraulic chamber
20
.
4
, the pressure piston
23
.
1
is displaced as well. Because the pressure piston
23
.
1
has a smaller diameter than the transmission piston
20
.
3
, a stroke boost is obtained; that is, depending on the diameter ratio, the valve body
23
is displaced over a correspondingly longer path relative to the voltage-proportional lengthening of the piezoelectric body
20
.
1
.
The change in length of the piezoelectric body
20
.
1
takes place in proportion to voltage, so that depending on the voltage applied, the valve body
23
lifts with its valve part
23
.
1
from the valve seat
22
and thus opens a corresponding flow cross section, so that a volumetric flow corresponding to the throttling between the valve seat
22
and the valve part
23
.
1
can flow out of the high-pressure channel
8
into the connecting channel
6
and then lift the nozzle needle
9
and open the injection nozzle
13
. Depending on the opening cross section uncovered at the valve part
23
.
1
and depending on the duration of the opening, fuel then flows via the nozzle openings
14
into the combustion chamber of the applicable cylinder. If the voltage at the piezoelectric body
20
.
1
is reduced, then via the valve spring
24
, the valve part
23
.
1
is pressed against the valve seat
22
, thus preventing fuel delivery.
On the nozzle end of the valve body
23
, a compensation piston
25
is provided, which has a smaller diameter than the valve part
23
.
2
. The compensation piston
25
can be connected to the valve body, as shown, or can be separate from the valve body. This compensation piston
25
is acted upon the pressure prevailing in the connecting channel
6
via a branch line
26
branching off from the connecting channel
6
. The result is a force feedback via the pressure in the closing direction of the valve body
23
, or in other words counter to the force of the actuator
20
. The effect is that the valve body
23
does not act solely counter to the force of the actuator
20
by means of the valve spring
24
; instead, the force feedback assures that the valve body
23
, during its longitudinal motion, both in the opening direction and the closing direction adapts without play and without delay to any change in length of the actuator, and hence an energy-dependent, or in the case of a piezoelectric actuator a voltage-dependent, change in length can be transmitted exactly to the motion of the valve body
23
. Pivoting motions are suppressed. As a result of the adaptation of the various diameters or surface areas exposed to the pressure imposition, such as the diameter of the guide parts
23
.
3
and
23
.
4
of the valve body and the diameter of the compensation piston
25
, the degree of the force feedback can be dimensioned. For a high degree of feedback, the regulability becomes better but requires more-powerful actuators.
This force feedback makes it possible to use a simple electromagnetic actuator, instead of a piezoelectric actuator; in an electromagnetic actuator, the adjusting force is proportional to the energy input, and thus a more precisely defined action on the injection nozzle is possible.
The low-pressure channel
17
, which continues with part of its length
17
.
1
inside the valve body
23
and connects the low-pressure channel
17
to the connecting channel
6
, is provided with a relief valve
27
, shown here as a simple ball valve. Since a tension spring
20
.
5
is disposed between the transmission piston
20
.
3
and the pressure piston
23
.
1
in the hydraulic chamber
20
.
4
, the pressure piston
23
.
1
is pressed in the state of repose via a tension spring
20
.
5
against the ball acting as a relief valve
27
, thus keeping the latter in the closing position.
If the actuator
20
is acted upon and the valve body
23
is displaced in the opening direction (arrow
28
), the relief valve
27
is kept in the closing direction. When the electrical voltage at the actuator
20
is shut off, the actuator abruptly shortens its length, so that because of inertia and the injection pressure prevailing in the connecting channel
6
, the transmission piston
23
.
1
is lifted from the ball, and the flow cross section is thus opened. Thus the injection pressure still prevailing in the connecting channel
6
can be decreased quickly via the low-pressure channel
17
to the fuel tank
2
, so that the nozzle needle
9
is likewise put with precise timing in the closing direction via the closing spring
16
.
By a suitable adaptation of the relief valve, it can be attained that the pressure upstream of the nozzle is not reduced to nothing; instead, a residual pressure remains, which prevents the development of vapor bubbles.
In
FIG. 3
, a modified embodiment of the control part
7
described in conjunction with
FIG. 2
is shown. Identical components are identified by the same reference numerals. The structure of the embodiment of
FIG. 3
is essentially equivalent to that described in conjunction with FIG.
2
. The distinction is first that the valve body
23
is embodied in one piece, and on the side toward the actuator, the pressure piston
23
.
1
is solidly connected to the valve body
23
. The pressure piston
23
.
1
has a smaller diameter than the piston parts
23
.
2
and
23
.
3
.
In the embodiment of
FIG. 3
, a hydraulic seat valve is provided as the relief valve
27
; its piston part
27
.
1
presses a valve needle
27
.
2
against its sealing seat, so that the connecting line
6
is blocked off from the low-pressure channel
17
. Upon actuation of the valve, via the pressure buildup in the hydraulic chamber
20
.
4
, the closing force of the relief valve
27
is increased in proportion to pressure, and the relief valve
27
is thus reliably kept in the closing direction in the presence of the injection pressure in the connecting channel
6
. If the actuator is deprived of voltage and shortens its length, then the pressure reduction in the hydraulic chamber
20
.
4
as well as the fuel still at injection pressure in the connecting channel
6
suffice to open the relief valve
27
briefly, counter to the force of a closing spring
27
.
3
embodied as a cup spring, so as to assure the pressure reduction in the connecting channel
6
via the low-pressure channel
17
as well.
In
FIG. 4
, a further embodiment of the control part
7
is shown. The structure is essentially equivalent to the structure of the embodiment described in conjunction with
FIG. 3
, which can therefore be referred to in this respect. The difference here is solely that a separate relief valve is not provided; instead, the valve body
23
is designed, in the region of its end acting as a pressure piston
23
.
1
, as a relief valve
27
and to that end is embodied as a slide valve. As can be seen from the enlarged view in
FIG. 5
, the end of the valve body
23
acting as a pressure piston
23
.
1
is shaped so as to taper conically on its end toward the valve chamber
21
, or is provided with an oblique flat face or a groove, specifically in such a way that in the closing direction of the valve body
23
, the end toward the actuator of the conical part
27
.
4
protrudes into an annular chamber
27
.
5
communicating with the low-pressure channel
17
and thus leaves a flow cross section open.
As soon as the valve body
23
is displaced via the actuator
20
in the opening direction (arrow
28
), the annular chamber
27
.
5
is closed off from the valve chamber
21
, so that in accordance with the opening of the flow cross section at the valve seat
22
, fuel can flow from the high-pressure channel
8
into the connecting channel
6
and build up the injection pressure.
If the actuator
20
is deprived of voltage, then the valve body
23
, under the influence of the force of the closing spring
24
and the pressure imposition via the compensation piston
25
, moves in the direction of the valve seat
22
. The flow cross section at the annular chamber
27
.
5
is uncovered in the process, so that the pressure in the connecting channel
6
can be reduced. The arrangement here is dimensioned such that the opening of the flow cross section to the annular chamber
27
.
5
is enabled practically simultaneously with the seating of the blocking part
23
.
2
on the valve seat
22
.
In the embodiment of the relief valve
27
described in conjunction with
FIG. 3
as well, by suitable dimensioning, the pressure reduction at the injection valve can be conducted such that vapor bubble formation is avoided. In the embodiment described in conjunction with
FIG. 4
, this can be achieved by means of an additional pressure limiting valve, connected to the line
17
.
The embodiments of the control part
7
described in conjunction with
FIGS. 3 and 4
can be employed in the same way as described in conjunction with
FIG. 2
, namely as a structural unit combined with a nozzle part
5
. However, as can be seen from the basic illustration in
FIG. 1
, it is also possible for all forms of the control part
7
to provide an arrangement in which the control part
7
is disposed separately from the nozzle part
5
. Accordingly, in the schematic illustration in
FIG. 1
, the branch line
26
leading to the control part
7
is indicated by dot-dashed lines.
In the ensuing
FIGS. 6-9
, a modified embodiment of the injection nozzle of
FIG. 2
is shown in the form of a flow chart, in which only the parts essential to the function are shown in detail. Identical components are again provided with the same reference numerals, so that the above description of the other exemplary embodiments can be referred to for both the structure and the function.
In the embodiment of
FIG. 6
, the valve assembly
21
.
0
is preceded by a so-called pressure divider
30
. In
FIG. 7
, one embodiment of the pressure divider
30
is shown on a larger scale. The pressure divider essentially comprises a piston body
31
, which is operatively connected (arrow
20
in
FIG. 7
) by its upper end to the actuator
20
and on its lower end is braced on a restoring spring
33
via a spring plate
32
. The piston body
31
is provided with a valve body
34
, which cooperates with a first valve seat
35
.
1
. In the pressure relieved state, the valve body
34
is pressed onto the first valve seat
35
.
1
by the restoring spring
33
.
Associated with the valve body
34
, on its side toward the restoring spring, is a second valve seat
35
.
2
, which connects the annular chamber
37
with the outflow chamber
39
, and which the valve body
34
closes to a greater extent, the farther it moves in the direction of the arrow
20
. The valve body
34
together with the valve seats
35
.
1
and
35
.
2
thus forms a 3/2-way proportional valve with 100% negative overlap. As a result of this arrangement, the pressure in the annular chamber
37
rises approximately linearly with the adjustment travel of the valve body
34
, from 0 bar when the valve body is in contact with the valve seat
35
.
1
up to the pressure prevailing in the line
8
, when the valve body is in contact with the valve seat
35
.
2
. Depending on the diameter of the valve seat
35
.
2
, a feedback of the pressure in the annular chamber
37
to the actuator
20
takes place, so that even an electromagnetic actuator can be used. The valve seat
35
.
2
can be embodied as a flat seat, in order to minimize the demands made in terms of production precision.
Also associated with the valve body
34
is a first annular chamber
36
, into which a branch line
8
.
1
of the high-pressure line discharges, and which is closed off by the closing direction defined by the valve seat
35
.
1
. The valve body
35
is disposed in a second annular chamber
37
, which communicates via an overflow line
8
.
2
with a pressure chamber
38
, which is defined by the valve body
23
on its side remote from the restoring spring
24
. The valve body
34
is also associated, in the region of the restoring spring
33
, with an outflow chamber
39
, which communicates with the low-pressure channel
17
via an outflow line
40
.
Via a line, the pressure chamber
38
communicates with a pressure chamber
41
, the latter being associated with the piston part
27
.
1
of the relief valve
27
.
If the valve body
34
is lifted from its valve seat
35
.
1
by the amount predetermined by the energy imposed via a piezoelectric actuator, then fuel at a correspondingly high pressure flows out of the high-pressure channel
8
via the connecting line
8
.
1
into the annular chamber
36
and on into the pressure chamber
38
via the connecting line
8
.
2
. As a result, the valve body
23
is displaced in proportion to pressure counter to the force of the restoring spring
24
, and the flow to the connecting channel
6
to the injection valve
5
is opened accordingly. The injection pressure prevailing in the connecting channel
6
also acts on the side of the valve body
23
toward the spring
24
, the pressure-loaded surface of which valve body is precisely the same size as the pressure-loaded surface of the side of the valve body oriented toward the chamber
38
. Since the force of the spring
24
is slight in comparison with the pressure forces applied, the valve body
23
always opens widely enough that the pressures in the chamber
38
and the connecting channel
6
are equal.
On the basis of the above-described function of the pressure divider
30
, the injection pressure can be modulated during the injection, by triggering the actuator
20
precisely far enough that it moves the valve body
34
into a position between the two valve seats
35
.
1
and
35
.
2
, which position adjusts the pressure that is desired as the injection pressure in the annular chamber
37
and thus also in the chamber
38
. The pressure in the annular chamber
3
also prevails in the pressure chamber
41
at the piston body
27
.
1
of the relief valve
27
, so that this pressure acts, reinforcing the closing spring
27
.
3
, in the closing direction against the valve body
27
.
2
.
If the actuator
20
is deactivated, then the valve body
34
of the pressure divider
30
takes it seat on its valve seat
35
.
1
, so that the pressure chambers
41
and
38
are pressure-relieved, and the valve assembly
21
.
0
thus closes. The pressure still prevailing in the connecting channel
6
can be reduced quite rapidly via the line
17
.
1
and the relief valve
27
, so that the valve spring
16
very quickly puts the nozzle needle
9
in the closing direction; the valve spring
27
.
3
is designed such that on the one hand the fastest possible pressure reduction takes place, but on the other, a residual pressure remains, so that vapor bubble formation is avoided.
The embodiment of
FIG. 8
is identical in function, with regard to the control part
7
, to the embodiment described above for
FIGS. 6 and 7
. The difference is only that the piston body
31
of the pressure divider
30
is provided, on its end toward the restoring spring
33
, with a compensation piston
42
, which can be subjected to the partial pressure via a branch line branching off from the overflow line
8
.
2
, and a pressure feedback can thus be effected. This makes it possible to actuate the pressure divider
30
in the direction of the arrow via an electromagnetic actuator.
The modification shown in
FIG. 9
is essentially equivalent to the above-described structure of
FIGS. 6 and 7
. The control part
7
is merely modified here in such a way that the pressure chamber
41
of the relief valve communicates directly, via a throttle
43
, with the low-pressure channel
17
, and the pressure divider
30
here can be embodied as a 2/2-way valve.
In the embodiment of
FIG. 9
, the pressure divider
30
is not acted upon directly via the actuator
20
, but instead via a hydraulic travel booster
43
, of the kind already described in conjunction with the embodiment of
FIGS. 2 and 3
. Via a feed line
44
, the unavoidable leakage losses in the hydraulic chamber of the hydraulic travel booster are compensated for. The travel booster described can be combined with all the variants described for the injection system.
In
FIG. 10
, an embodiment of the injection valve with a nozzle needle
9
that can be opened in two stages is shown. The nozzle needle
9
is braced here on the housing, via a first, soft closing spring
16
.
1
. A slide body
16
.
3
is also provided, which is braced with its side remote from the nozzle needle
9
against a second, harder closing spring
16
.
2
. The slide body
16
.
3
has a support extension
16
.
4
, which ends a slight distance a upstream, in terms of the closing direction of the nozzle needle
9
, of the end of the piston body
15
of the nozzle needle
9
.
If via the connecting channel
6
the pressure chamber
10
is subjected to a pressure that is less than the restoring force of the restoring spring
16
.
2
, then the injection valve opens only by a stroke corresponding to the amount a. If the pressure chamber
10
is acted upon by a pressure that is greater than the restoring force of the closing spring
16
.
2
, then the nozzle needle
9
is displaced backward correspondingly far, and the injection valve opens completely.
In
FIG. 11
, a modification of the embodiment of
FIG. 10
is shown. In this embodiment, the closing spring
16
is braced on an escape piston
16
.
5
, which on its side remote from the closing spring has a pressure chamber
16
.
6
, which is connected to the connecting channel
6
via a throttle
16
.
7
. A pressure-dependent, dynamic guidance of the opening motion of the nozzle needle
9
is possible via this arrangement.
With a fuel injection device of the type according to the invention, it is possible, even in high-speed Diesel engines, in particular Diesel engines for passenger cars, which under full load can have rotary speeds of 4000 to 4500 rpm and in which high injection pressures of approximately 1500 to 2000 bar exist, to achieve short injection times, for instance of 1.5 milliseconds, specifically by means of direct triggering of the control part.
Claims
- 1. A fuel injection device for a reciprocating internal combustion engine, having a nozzle part (5) with an injection nozzle (13), which part has a pressure chamber (10) in which the nozzle needle (9) that closes the injection nozzle (13) is guided, which needle is movable in the opening position upon imposition of pressure by the fuel to be injected, wherein the pressure chamber (10) communicates via a connecting channel (6) with a control part (7) which has a valve chamber (21), into which the connection to channel (6) on the one hand and a high-pressure channel (8), communicating with a fuel supply (4), on the other hand for discharging, and in which a valve body (23) acting as a piston system is guided, which body is kept in the closing position on a valve seat (22) by a valve spring (24), and having an actuator (20), which is operatively connected to the valve body (23) and which moves the valve body in the opening direction upon activation and enables the flow from the high-pressure channel (8) into the connecting channel (6), and having a compensation piston (25; 42) which is acted upon counter to the force action of the actuator via the pressure in the connecting channel (6).
- 2. The fuel injection device of claim 1, characterized in that the compensation piston (26), which can be acted upon via the pressure in the connecting channel (6), is disposed on the valve body, on its end (25) remote from the actuator (20).
- 3. The fuel injection device of claim 1, characterized in that the connecting channel (6) is provided with a relief valve (27), which opens toward the low-pressure side (17) of the fuel supply (14), and which is closed upon activation of the actuator (20).
- 4. The fuel injection device of claim 1, characterized in that a tension spring (20.5) is disposed between the actuator (20) and the valve body (23).
- 5. The fuel injection device of claim 1, characterized in that the actuator (20) has a transmission piston (20.3), and the end of the valve body (23) oriented toward the actuator (20) has a pressure piston (23.1), and that between the two pistons, a hydraulic chamber (20.4) is disposed, and the diameter of the pressure piston (23.1) is less than the diameter of the transmission piston (20.3).
- 6. The fuel injection device of claim 1, characterized in that the diameter of the compensation piston (25), depending on the desired force feedback is less than, equal to, or greater than the diameter of the part of the piston system of the valve body (23) that acts in the opening direction upon imposition of pressure.
- 7. The fuel injection device of claim 1, characterized in that the actuator (20), with respect to its adjustment travel, is embodied adjustingly in proportion to the adjustment energy applied.
- 8. The fuel injection device of claim 1, characterized in that an electrical actuator (20) is provided, which is embodied adjustingly in proportion to voltage with respect to its adjustment travel.
- 9. The fuel injection device of claim 1, characterized in that an electrical actuator (20) is provided, which is embodied adjustingly in proportion to current with respect to its adjustment travel.
- 10. The fuel injection device of claim 1, characterized in that the control part (7) has a pressure divider (30), which communicates on the one hand with the high-pressure channel (6) and on the other with the valve body (23) forming a piston system, the valve body having a pressure compensation piston (23.1; 42) acting as a compensation piston, which can be acted upon by the pressure acting in the connecting channel (6), counter to the actuator force, and which is adjustable via the actuator.
- 11. The fuel injection device of claim 1, characterized in that a pressure divider (30) is operatively connected to a relief valve (27).
- 12. The fuel injection device of claim 11, characterized in that the relief valve (27) has a valve spring (27.3), acting on a valve body (27.2) in the closing direction, and a piston (27.1) which can additionally be acted upon in the closing direction via the pressure divider (30).
- 13. The fuel injection device of claim 1, characterized in that a pressure divider (30) is embodied as a 3/2-way valve, and the two valve seats of the 3/2-way valve represent two throttle restrictions of the pressure divider (30).
- 14. The fuel injection device of claim 1, characterized in that a valve seat (35.2) of a pressure divider (30) is embodied as a flat seat.
Priority Claims (1)
Number |
Date |
Country |
Kind |
100 01 828 |
Jan 2000 |
DE |
|
PCT Information
Filing Document |
Filing Date |
Country |
Kind |
PCT/EP00/12777 |
|
WO |
00 |
Publishing Document |
Publishing Date |
Country |
Kind |
WO01/53688 |
7/26/2001 |
WO |
A |
US Referenced Citations (3)
Number |
Name |
Date |
Kind |
5526791 |
Timmer et al. |
Jun 1996 |
A |
5893350 |
Timms |
Apr 1999 |
A |
5979790 |
Gurich et al. |
Nov 1999 |
A |
Foreign Referenced Citations (3)
Number |
Date |
Country |
43.41 546 |
Jun 1995 |
DE |
297 17 649 |
Nov 1997 |
DE |
197 06 647 |
Mar 1998 |
DE |