Information
-
Patent Grant
-
6764027
-
Patent Number
6,764,027
-
Date Filed
Tuesday, September 24, 200222 years ago
-
Date Issued
Tuesday, July 20, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Mar; Michael
- Gorman; Darren
Agents
-
CPC
-
US Classifications
Field of Search
US
- 239 53312
- 239 5332
- 239 5339
- 239 5851
- 239 489
- 239 5333
- 239 53311
- 239 53314
- 239 5852
- 239 5853
- 239 5854
- 239 5855
-
International Classifications
- F02M6100
- F02M5900
- F02M6300
- F02M6120
- B05B134
-
Abstract
A fuel injector for fuel injection systems of internal combustion engines includes a valve needle and a valve-closure member mechanically linked to it, which cooperates with a valve-seat surface situated in a valve-seat member to form a sealing seat, and at least one swirl-producing element which is situated upstream from the sealing seat in the valve-seat member. One or more swirl channels which are open toward the upstream side of the valve-seat member are incorporated into the upstream side of the valve-seat member as a swirl-producing element.
Description
FIELD OF THE INVENTION
The present invention relates to a fuel injector.
BACKGROUND INFORMATION
Fuel injectors in which swirl-producing elements are incorporated into a valve-seat member are referred to in German Patent No. 41 31 499. The swirl-producing element is implemented in the form of grooves which are incorporated into the valve-seat member and discharge into an injection orifice. The metering of the volume of fuel to be injected is accomplished by the cross section of the injection orifice. The injection orifice is located either in the valve-seat member or in a perforated disk which is situated at the downstream end of the fuel injector.
An additional fuel injector in which the swirl is produced by grooves is referred to in German Patent No. 42 31 448. The swirl-producing elements are located upstream from the sealing seat and are incorporated in the form of grooves in a central recess of the valve-seat member which is used to guide the valve-closure member. The swirl grooves, which are open toward the center line of the fuel injector, are closed by the valve-closure member, which is spherical, to form channels. This defines a cross section within the swirl channels through which the fuel is metered.
One disadvantage of the fuel injector referred to in German Patent No. 41 31 499 is the position of the swirl-creating element downstream from the sealing seat. The danger of contamination from coking is great, especially in the case of directly injecting fuel injectors. Particular attention must paid in the configuration to ruggedness of the swirl-producing elements; this limits the configuration options for the component, since minimum requirements for material thickness for example must be adhered to.
A further disadvantage is that the location downstream from the sealing seat causes a dead volume to be formed, from which fuel may escape after the injection operation ends. This afterdripping results in incomplete and uncontrolled combustion, which produces a large amount of pollutants. In addition, the one-piece configuration of nozzle body and valve-seat member makes it difficult to produce the grooves. Exceeding of component tolerances which may occur during manufacturing thus result in the rejection of an expensive component.
In the fuel injector referred to in German Patent No. 42 31 448, completing the grooves into swirl channels by the spherical valve-closure member is disadvantageous. The spherical geometry of the valve-closure member causes the swirl grooves to be closed to form swirl channels only at the circumference of the valve-closure member. This makes it difficult to prevent leakage, since the tolerances of several components are cumulative. This is particularly critically apparent because the sealing gap is in the form of a line. The result is a wide range of variation in the metered fuel volume.
Also disadvantageous is the necessary strong deflection of the fuel stream. This results from the arrangement of the swirl channels on the cylindrical wall of the recess which guides the valve-closure member. The adjacent swirl chamber is necessary to produce a uniformly turbulent stream. However, the associated deflection of the stream leads to severe losses of flow, which are evident in a poorer injection pattern. In addition, during the process of opening the fuel injector a pre-jet is formed, which includes no swirl. The resulting poor atomization causes deficient combustion.
SUMMARY OF THE INVENTION
The exemplary fuel injector according to the present invention may provide that the swirling fuel stream reaches the injection orifice without strong deflection. At the same time the swirl-producing elements are in a protected arrangement upstream from the sealing seat. The separation of the swirl production from the metering of the fuel to be injected is a further advantage for manufacturing. Relatively rough dimensional tolerances may be chosen for the swirl-producing elements, this may allow the use of more economical production methods.
Adaptation of the fuel injector to customer requirements in regard to the volume of fuel to be injected and injection pattern is simple. This is done by modifying only one component, which is able to influence both the swirl production and fuel metering. The swirl production may be varied by influencing the axial component of the fuel stream. This results in modification of the envelope of the cone on which the fuel is injected.
The metered volume is also adjusted while retaining the valve-seat member unchanged, by modifying an annular gap which is produced by an offset in the valve-closure member. In addition to the definition of a metered volume with the fuel injector completely open, the opening and closing response may be influenced by modifying the contour of the offset.
A further advantage is an arrangement of the swirl channels on a cone envelope whose angle is identical to the angle of the valve seat surface. Because of the resulting elimination of strong flow deflection downstream from the production of the swirl there is no loss in circumferential speed of the fuel on the way to the injection orifice.
This results in the further advantage of the elimination of a dead volume downstream from the production of swirl. Consequently a swirl is formed in the fuel stream as early as during the process of opening the fuel injector. In the final analysis, the improved swirl conditioning during opening and closing ensures improved combustion and thus results in lower emission of pollutants.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
shows a schematic partial section through an exemplary embodiment of a fuel injector according to the present invention.
FIG. 2
shows a schematic partial section in detail II of
FIG. 1
of the exemplary embodiment of a fuel injector according to the present invention.
FIG. 3
shows a schematic section along the line III—III in FIG.
2
.
DETAILED DESCRIPTION
Before discussing an exemplary embodiment of a fuel injector
1
according to the present invention with reference to
FIGS. 2 and 3
, the essential components of the exemplary fuel injector
1
according to the present invention will now be explained briefly in an overall view for a better understanding of the presentation with reference to FIG.
1
.
Fuel injector
1
is configured in the form of a fuel injector
1
for fuel injection systems of engines having fuel mixture compression and spark ignition. Fuel injector
1
is suitable in particular for direct injection of fuel into the combustion chamber (not shown) of an engine.
Fuel injector
1
includes a nozzle body
2
in which a valve needle
3
is situated. Valve needle
3
is mechanically linked to a valve-closure member
4
, which cooperates with a valve-seat surface
6
on a valve-seat member
5
to form a sealing seat. In this exemplary embodiment, fuel injector
1
is an electromagnetically operated fuel injector
1
which includes an injection orifice
7
. Nozzle body
2
is sealed by a gasket
8
from a stationary pole
9
of a solenoid
10
. Solenoid
10
is encapsulated in a coil housing
11
and wound onto a field spool
12
, which is in contact with an internal pole
13
of solenoid
10
. Internal pole
13
and stationary pole
9
are separated from one another by a gap
26
and are supported on a connecting component
29
. Solenoid
10
is energized by an electric current that may be supplied through an electric plug-in contact
17
via a line
19
. Plug-in contact
17
is enclosed by plastic sheathing
18
, which may be integrally molded on internal pole
13
.
Valve needle
3
is guided in a disk-shaped valve needle guide
14
. Matched to the latter is an adjusting disk
15
which is used to adjust the lift of the valve needle. An armature
20
is situated on the upstream side of adjusting disk
15
. Via a flange
21
, the armature is frictionally engaged with valve needle
3
, which is joined by a weld
22
to flange
21
. A restoring spring
23
, which is pre-stressed by a sleeve
24
pressed into internal pole
13
in the present configuration of fuel injector
1
, is supported on flange
21
.
Fuel channels
30
a
,
30
b
run in valve needle guide
14
and armature
20
. A filter element
25
is provided in a central fuel feed
16
. Fuel injector
1
is sealed from a fuel line (not shown) by a gasket
28
.
In the resting state of fuel injector
1
, armature
20
is acted upon by restoring spring
23
via flange
21
on valve needle
3
against its direction of lift, so that valve-closure member
4
is held in sealing contact on valve seat
6
. When solenoid
10
is energized, it builds up a magnetic field which moves armature
20
in the direction of lift against the elastic force of restoring spring
23
, the lift being predetermined by a working gap
27
between internal pole
13
and armature
20
in the resting position. Armature
20
also entrains flange
21
, which is welded to valve needle
3
, and with it valve needle
3
, in the direction of lift. Valve-closure member
4
, which is connected to valve needle
3
, is lifted up from valve-seat surface
6
, and the fuel conveyed through swirl channels
36
and an adjacent annular gap
37
to injection orifice
7
is injected.
When the coil current is turned off, armature
20
drops back due to the pressure of restoring spring
23
onto flange
21
of internal pole
13
, so that valve needle
3
moves against the direction of lift. That causes valve-closure member
4
to drop onto valve-seat surface
6
, and fuel injector
1
is closed.
FIG. 2
shows the swirl-producing module of an exemplary fuel injector
1
according to the present invention in a sectional detail. The swirl-producing module is made of valve-seat member
5
, valve needle
3
and valve-closure member
4
, which is mechanically linked to valve needle
3
.
On its upstream side
33
, valve-seat member
5
includes a guide recess
38
which is used to guide valve needle
3
in the axial direction. Adjacent to it downstream is a tapering, which is cone-shaped, on which valve-seat surface
6
is situated. Adjacent to the narrowing on the downstream side is injection orifice
7
. On the upstream side
33
of valve-seat member
5
, swirl channels
36
are incorporated into valve-seat member
5
. They are open toward the upstream surface
33
of valve body
5
, and discharge, e.g., tangentially, into guide recess
38
. The swirl channels are configured as grooves in valve-seat member
5
. Bottom
39
of the grooves forms the downstream limiting surface of swirl channels
36
, and is situated on the envelope of a cone whose apex angle α is identical to apex angle β enclosed by cone-shaped valve-seat surface
6
with center line
35
of fuel injector
1
.
Upstream from upstream face
33
of valve-seat member
5
, valve needle
3
includes a radial extension
31
, so that swirl channels
36
, which are open on the upstream side, are at least partly covered in the radial direction. Depending on the radial dimension of radial extension
31
and on the distance from upstream face
32
of radial extension
31
to upstream face
33
of valve-seat member
5
, the axial component of the fuel stream may thus be varied when fuel injector
1
is open. The dimension of radial extension
31
is smaller than the inside diameter of nozzle body
2
. The changes in the axial components of the fuel stream during opening and closing of fuel injector
1
may be influenced selectively for example by a cone-shaped or funnel-shaped configuration of upstream face
33
of valve-seat member
5
. It may also be influenced via the corresponding face
32
of radial extension
31
.
Valve-closure member
4
, which is connected to valve needle
3
, includes a radial extension which is smaller than guide recess
38
of valve-seat member
5
. The cross sectional area of annular gap
37
thus formed between valve-closure member
4
and valve-seat member
5
determines the metering of the fuel to be injected. The height of annular gap
37
established by valve needle
3
should be chosen such that swirl channels
36
are in contact with annular gap
37
, at least when fuel injector
1
is open. If valve needle
3
together with valve-closure member
4
are in their open stop position when solenoid
10
is energized, the cross sectional area of annular gap
37
is the smallest cross section through which the fuel stream must flow on the way to injection orifice
7
.
FIG. 3
shows a sectional detail of the exemplary embodiment of a fuel injector according to the present invention shown in FIG.
2
. Here swirl channels
36
discharge tangentially into annular gap
37
, which is formed between valve-closure member
4
and guide recess
38
of valve-seat member
5
. The sum of the cross sectional areas of the discharge holes of swirl channels
36
is greater than the cross sectional area of annular gap
37
formed between guide recess
38
of valve-seat member
5
and valve-closure member
4
. The cross sectional areas of the discharge holes may be adjusted by increasing the axial dimension of valve-closure member
4
in the area of annular gap
37
.
Claims
- 1. A fuel injector for a fuel injection system of an internal combustion engine, comprising:a valve needle; a valve-seat member; a valve-seat surface arranged in the valve-seat member; a valve-closure member connected to the valve needle, the valve-closure member cooperating with the valve-seat surface to form a sealing seat; and at least one swirl-producing element positioned upstream from the sealing seat in the valve-seat member; wherein at least one swirl channel is open toward an upstream side of the valve-seat member, and is incorporated into the upstream side of the valve-seat member; and wherein the at least one swirl channel includes a groove-incorporated into the valve-seat member, and is open toward the upstream side.
- 2. The fuel injector of claim 1, wherein the valve needle includes a radial extension upstream from the upstream side of the valve-seat member.
- 3. The fuel injector of claim 2, wherein the radial extension has a geometry on its upstream side corresponding to the upstream side of the valve-seat member.
- 4. The fuel injector of claim 1, wherein the valve-closure member includes a radial extension that is smaller than another radial extension of the valve needle.
- 5. The fuel injector of claim 1, wherein an annular gap is formed downstream from the at least one swirl channel between the valve-closure member and a recess in the valve-seat member, a cross-sectional area of the annular gap forming a smallest cross-sectional area through which fuel flows.
- 6. The fuel injector of claim 5, wherein the annular gap separates the sealing seat from the at least one swirl channel.
- 7. The fuel injector of claim 1, wherein a bottom of the at least one swirl channel faces away from the upstream side, and lies on a first conical surface.
- 8. The fuel injector of claim 7, wherein the valve-seat surface forms a second conical surface and a first apex angle of the first conical surface essentially matches a second apex angle of the second conical surface, the first apex angle and the second apex angle being with respect to a center line of the fuel injector.
Priority Claims (1)
Number |
Date |
Country |
Kind |
100 50 752 |
Oct 2000 |
DE |
|
PCT Information
Filing Document |
Filing Date |
Country |
Kind |
PCT/DE01/03913 |
|
WO |
00 |
Publishing Document |
Publishing Date |
Country |
Kind |
WO02/31352 |
4/18/2002 |
WO |
A |
US Referenced Citations (6)
Foreign Referenced Citations (6)
Number |
Date |
Country |
41 31 499 |
Apr 1993 |
DE |
42 31 448 |
Oct 1993 |
DE |
199 07 860 |
Mar 2000 |
DE |
1 026 393 |
Aug 2000 |
EP |
1 036 933 |
Sep 2000 |
EP |
2 170 269 |
Jul 1986 |
GB |