A fuel injector is referred to in German Patent Application No. 42 31 448, in which the fuel injector is provided with helical grooves arranged in a guide bore above the valve-sealing seat to generate a swirl. The helical grooves, which are open toward the valve-closure member, are closed by the valve-closure body guided in the guide bore to form swirl channels. A circumferential groove swirl chamber is arranged downstream from the guide bore, into which the helical grooves discharge with a slight tangential component. Due to the tangential component, the fuel flowing into the swirl chamber obtains a circumferential velocity that fans out a jet of fuel when it exits from the fuel injector, thereby providing an improved atomization.
The helical grooves are introduced into the valve-seat member by machining. Afterwards, burrs produced by the introduction of the helical grooves are removed from the transitions of the helical grooves to the guide bore, and the guide bore and the valve-seat surface are ground. Once the valve-seat member has been cleaned of all work-related residue, such as shavings, coolants and abrasives, the valve-seat member is hardened to ensure a long service life.
It is believed that machining processes are disadvantageous in that they involve additional processing. The burrs, which may be produced by the introduction of the helical grooves, may form in the transition between the helical grooves and the guide bore. These burrs are removed in an additional processing step. Moreover, resulting shavings are removed to prevent early wear of the fuel injector in the guide area and the valve seat.
Furthermore, it is believed to be disadvantageous in that the machining introduces heat into the workpiece, which may be unavoidable, even when coolants are used during the machining. Therefore, a cooling phase may be required prior to checking the valve-seat member for dimensional accuracy.
It is believed that an exemplary method according to the present invention has an advantage in that the helical grooves are introduced in a non-cutting manner. In this manner, the formation of burrs may be prevented, and additional work may be reduced during further processing. By omitting one working step, the production costs may be reduced.
The grinding of the guide bore and the valve seat is performed before the helical grooves are introduced into the uninterrupted inner surface of the guide bore of the valve-seat member. The number and geometry of the helical grooves may thus be freely chosen, without having to consider resonant vibrations of the grinding tools, which may occur, such as in the case of grooves already introduced and evenly distributed over the circumference.
Furthermore, it is believed to be advantageous in that the valve seat may be hardened before the helical grooves are introduced. As a result, the circumference of the guide of the valve-closure member may be evenly hardened, since no undesired effects occur, such as those which may occur at the edges of the transition from the helical grooves to the guide bore.
Electro-mechanical metal processing may not cause thermal distortion during the introduction of the grooves. In this manner, the valve-seat member may be checked using a suitable method, such as a template. No cooling of the valve-seat member, which may be warm from the machining, may be required.
Referring to
Fuel injector 1 includes a nozzle body 2, in which a valve needle 3 is positioned. Valve needle 3 is connected in operative connection to a valve-closure member 4 that cooperates with a valve-seat surface 6, arranged on a valve-seat member 5, to form a sealing seat. Fuel injector 1, in the exemplary embodiment shown in
Valve needle 3 is guided in a valve needle guide 14, which may be designed, for example, as a disk. A paired adjustment disk 15 adjusts the (valve) lift. An armature 20 is positioned on the other side of adjustment disk 15 and connected by force-locking to valve needle 3 via a first flange 21, and valve needle 3 is connected to first flange 21 by a welded seam 22. Braced against first flange 21 is a return spring 23, which receives an initial stress from a sleeve 24.
A second flange 31, which is connected to valve needle 3 via a welded seam 33, forms a lower armature stop. An elastic intermediate ring 32, which lies upon second flange 31, avoids bounce when fuel injector 1 is closed.
Fuel channels 30a, 30b and grooves 36, respectively, extend through valve needle guide 14, armature 20 and valve seat member 5, which conduct the fuel, supplied via central fuel supply 16 and filtered by a filter element 25, to spray-discharge orifice 7 in valve-seat member 5. Fuel injector 1 is sealed by seal 28 from a distributor line (not shown).
In the neutral position of fuel injector 1, return spring 23, via first flange 21 at valve needle 3, acts upon armature 20 counter to its lift direction, so that valve-closure member 4 is retained in sealing contact against valve-seat surface 6. Upon excitation of magnetic coil 10, the latter generates a magnetic field that moves armature 20 in the lift direction, counter to the spring force of return spring 23, the lift being predefined by a working gap 27 existing in the neutral position between internal pole 13 and armature 20. Armature 20 also carries along, in the lift direction, first flange 21, which is welded to valve needle 3. Valve-closure member 4, being operatively connected to valve needle 3, lifts off from valve seat surface 6, and fuel guided to spray-discharge orifice 7 via fuel channels 30a, 30b and grooves 36, respectively, is sprayed off.
When the coil current is switched off, after sufficient decay of the magnetic field, armature 20 falls away from internal pole 13 due to the pressure of return spring 23 on first flange 21, whereupon valve needle 3 moves in a direction counter to the lift. In this manner, valve-closure member 4 rests on valve-seat surface 6 and fuel injector 1 is closed.
When manufacturing valve-seat member 5 according to the present invention, a blank is first produced, into which a central cut-out 35 for guiding valve-closure member 4, a swirl chamber 37, a valve-seat surface 6 and a spray-discharge orifice 7 are introduced by machining. The shavings produced during processing and any left-over residue from coolants used in machining, are then completely removed.
In a subsequent method step, helical grooves 36 are introduced into valve-seat member 5. Helical grooves 36 may differ in their cross-section and extension, as shown in
In the exemplary embodiment according to the present invention shown in
According to another exemplary embodiment of the present invention, cut-out 35 and valve-seat surface 6 are jointly ground in a manufacturing method according to the present invention, before the helical grooves are introduced. In this manner, valve-seat surface 6 and central cut-out 35 of valve-seat member 5 obtain their final shape and surface properties. Valve-closure member 4 sealingly cooperates with cut-out 35 and valve-seat surface 6. The removed material and the left-over abrasive are removed in one cleaning step. Then, the hardening of valve-seat member 5 occurs. Valve-seat surface 6 and the surface of cut-out 35 for guiding valve-closure member 4 are exposed to strong stresses over the course of their service life. To prevent premature wear of the fuel injector 1, the surfaces are hardened. The rotational symmetry of valve-seat member 5, which as yet does not have any helical grooves 36, facilitates the even grinding and hardening of the surface in cut-out 35.
Helical grooves 36 may be introduced into valve-seat member 5 by electro-chemical metal cutting, as illustrated in
Helical grooves 36 may be introduced in valve-seat member 5 by eroding the helical grooves 36.
As a final method step, the introduced helical grooves are checked for form and position. If compliance with the predefined setpoint values is ascertained, by checking with a template, for example, valve-closure member 5 is supplied to the further installation process of fuel injector 1.
Number | Date | Country | Kind |
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100 46 304.5 | Sep 2000 | DE | national |
Filing Document | Filing Date | Country | Kind |
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PCT/DE01/03265 | 8/25/2001 | WO |