Patent Application
20080251612
The invention relates to a unit fuel injector (UFI) and to a pump-line-nozzle unit (PLNU) for an internal combustion engine, with a pump element, the pump element having a pump chamber, and with a magnet valve, the magnet valve having a valve member and an armature; the magnet valve opens or closes a hydraulic connection between the pump chamber and a low-pressure region of the unit fuel injector.
In connection with the invention, the following discussion will refer only to the unit fuel injector (UFI), although pump-line-nozzle units (PLNUs) are always intended as well. The most essential distinction between unit fuel injectors and pump-line-nozzle units is that a pump-line-nozzle unit has a short high-pressure line between the pump element and the injection nozzle. For the present invention, this distinction does not matter, and hence patent protection is claimed equally for unit fuel injectors and pump-line-nozzle units.
A unit fuel injector is known for instance from German Patent Disclosure DE 198 37 333 A1. In this unit fuel injector, the valve and the armature of the magnet valve are connected to one another nonpositively by a compression spring. Because the valve member and the armature are coupled only nonpositively, the dynamic performance of the magnet valve is difficult to control, and it is hardly avoidable that during operation, the armature and the valve member will repeatedly briefly separate from one another and after that collide again. This process is known as “bouncing”. The bouncing is unwanted, since it has an adverse effect on the precision with which the magnet valve opens and closes. Moreover, the bouncing causes high wear to the armature, which is of a soft material, so that the valve stroke and thus also the operating performance of the magnet valve vary over the course of time. Finally, it should also be mentioned that the armature must be guided in a capsule, and for structural reasons this guide can only be relatively short. As a consequence, the armature has a tendency to tilting, and the armature guide wears down relatively quickly.
In a unit fuel injector and a pump-line-nozzle unit according to the invention for an internal combustion engine, with a pump element, the pump element having a pump chamber, and with a magnet valve, the magnet valve having a valve member and an armature, and in which the magnet valve opens or closes a hydraulic connection between the pump chamber and a low-pressure region, it is provided that the armature is fixedly connected to the valve member.
As a result of this structural provision, the bouncing of the armature on the valve member can be effectively averted. Because of the rigid, fixed connected between the armature and the valve member, a separate guide of the armature can be omitted, since the armature is guided by the valve member. Tipping or tilting of the armature in its guide during operation and the resultant functional problems of the unit fuel injector therefore no longer occur.
An especially advantageous aspect of the embodiment according to the invention is also that the number of components needed is reduced, since a separate compression spring that keeps the armature in contact with the valve member can be omitted. As a result, the manufacturing and installation costs are reduced, and less installation space is required.
In an advantageous feature of the invention, it is provided that a receiving mandrel is embodied on the valve member, and that the armature is fixedly connected to the receiving mandrel. In particular, it is advantageous if the armature is connected to the receiving mandrel by nonpositive engagement, in particular by pressing. As a result of this structural embodiment of the connection between the valve member and the armature, a secure and economical connection between the armature and the valve member can be made in a simple way. It is also possible to position the armature with high precision relative to the valve seat of the valve member. As a result, production tolerances in mass production can be compensated for by a suitable mounting of the armature on the receiving mandrel. The operating performance of various individual examples in a large-scale series is consequently virtually identical. This advantage is of considerable significance, since controlling the unit fuel injector of the invention is based on a certain predetermined, programmed-in operating performance of the unit fuel injector. Any deviation of the unit fuel injector from this programmed-in, predetermined operating performance makes the operating performance of the engine worse.
The range of deviation in operating performance of the unit fuel injector of the invention can be further improved by providing that a sealing face and a stroke stop are embodied on the valve member, and that the maximum stroke of the valve member is defined by the spacing in the axial direction between the sealing face and the stroke stop. This means that even during production of the valve member of the invention, the maximum stroke of the valve member is predetermined. Since the spacing in the axial direction between the sealing face and the stroke stop is easy to accomplish in production and can also be well monitored by measuring instruments, the deviation in the valve stroke from one example to another in a series is virtually zero.
As with other magnet valves as well, it has proved advantageous to embody the sealing face frustoconically, so that with a likewise frustoconical valve seat embodied in the valve housing, it forms a conical sealing seat.
To improve the operating performance of the magnet valve of the invention, a magnet plate cooperating with a coil of the magnet valve is provided between the armature and the stroke stop, and the receiving mandrel of the valve member protrudes through a bore in the magnet plate. With the aid of the magnet plate, it is possible to optimize the magnetic flux of the coil, so that the magnetic forces exerted on the armature of the magnet valve as a consequence of an electric current flowing through the coil are maximized, and the electrical power loss is minimized.
To enable adjusting the operating performance of the magnet valve in the installed state, a compression spring acting on the valve member is provided, whose prestressing force is very easily adjustable with the aid of an adjusting disk. By replacing this adjusting disk with another adjusting disk of a different thickness, the operating performance of different examples of magnet valves of the invention can be further improved, and the variations from one another among various examples in a series can be further reduced.
So that no fuel can reach the coil, the armature is embodied in encapsulated form. This can be done especially advantageously according to the invention by providing that the armature is surrounded by a capsule; that a spacer ring of a nonmagnetic material, in particular stainless steel, is provided between the capsule and the magnet plate; and that the capsule, spacer ring, and magnet plate are connected in sealing fashion to one another. Especially preferably, the capsule, spacer ring and magnet plate are welded or soldered to one another.
To assure high functional reliability and a long service life, the valve member is guided at least one point, but preferably at two points, in a housing. As a result, it is assured that the sealing face of the valve member always strikes the valve seat in the valve housing parallel to the valve seat, and moreover the armature does not rest on the capsule, which does not move relative to the valve housing, and as a result the armature does not wear down.
So that the magnet valve of the invention will assume its open position when the coil is made currentless, a compression spring is provided between the valve member and the valve housing.
The magnet valve of the invention can be installed especially advantageously by means of a method in which the fully machined valve member is locked in a receptacle of a fixed installation device; the magnet plate and the spacer plate are mounted on the receiving mandrel; the magnet plate, spacer plate and valve member are pressed against the receptacle; next, the magnet plate and the spacer plate are displaced by an amount A relative to the valve member; and the armature is secured to the receiving mandrel of the valve member in such a way that the armature rests on the magnet plate.
By means of this method, it is easily possible, despite the production tolerances that occur in every mass production, to adjust the valve stroke exactly and with very great repeatability. In the process, production tolerances among individual components do not adversely affect the precision of the adjusted valve stroke.
It has proved advantageous if the magnet plate and the spacer plate are displaced by an amount A that corresponds to the sum of the valve stroke and a desired remanent air gap between the armature and the magnet plate in the closed state of the magnet valve.
To prevent fuel from being able to reach the coil of the magnet valve, a spacer ring and a capsule are then slipped onto the magnet plate and tightly welded to one another.
For calibrating the magnet valve, the compression spring and the valve member are then inserted into the valve housing; a coil of the magnet is triggered with a current which is selected such that the magnetic force exerted on the armature is greater than the spring force that is to be exerted by the compression spring on the valve member; the spring force exerted by the compression spring on the valve member is recorded as a function of the position of the magnet valve in the housing; the recorded spring force and travel graph is evaluated; and if needed, a correction is made in the thickness of the adjusting disk.
By means of this method for calibrating the magnet valve of the invention, it can be assured in a simple way that the current with which the coil must be triggered for closing the magnet valve will be virtually identical in all examples in a series. As a result, there is a very uniform operating performance of the magnet valve of the invention. Once the initial tension of the compression spring has been adjusted, function monitoring can be performed, and if needed, another correction of the thickness of the adjusting plate is made. This step is done until such time as the function of the unit fuel injector is in accordance with the required demands.
Further advantages and advantageous features of the invention can be learned from the ensuing drawings, their description, and the claims. All the characteristics described in the drawings, their description, and the claims can be essential to the invention both individually and in arbitrary combination with one another.
Shown are:
In
The unit fuel injector 1 is controlled by a 2/2-way control valve 5 which is shown in the form of a block circuit diagram.
The control valve 5 is triggered by an actuator, not shown in
As in every unit fuel injector, the pump element 2 and the injection nozzle 3 form a unit. For each cylinder of the engine, one unit fuel injector 1 is built into the cylinder head 7 of the engine and driven, either directly via a tappet or indirectly via tilt levers, by a camshaft of the engine (not shown) via an actuating element 8.
A pump chamber 9 of the pump element 2 communicates, via a fuel inlet 11, with a low-pressure fuel supply 12. The low-pressure fuel supply 12 may for instance comprise an electrically driven prefeed pump 15 and a fuel filter (not shown), which aspirate fuel from a fuel tank 13 via a line.
The control valve 5 splits the fuel inlet into two portions 11a and 11b. The control valve 5 is triggered by a control unit, not shown, and opens the hydraulic connection between the pump chamber 9 and the tank 13, as shown in
When the control valve 5 is opened, fuel can flow into the pump chamber 9 during the intake stroke of the pump piston 10. In the ensuing pumping stroke of the pump piston 10, the fuel previously pumped into the pump chamber 9 is pumped back into the tank 13, as long as the control valve 5 is open. This also means that a pressure sufficient to open the injection nozzle 3 does not build up in the pump chamber 9.
When fuel is to be injected via the injection nozzle 3 into the combustion chamber, not shown, of the engine, the control valve 5 is closed during the pumping stroke of the pump piston 10. As a result, the fuel can no longer be pumped out of the pump chamber 9 back into the tank 13, and in the pump chamber 9 a high pressure builds up, which finally leads to the opening of the injection nozzle 3 and hence to the injection of fuel into the combustion chamber (not shown) of the engine. The onset of the injection of fuel into the combustion chamber can be determined by the closing time of the control valve 5. The injection of fuel into the combustion chamber is terminated by opening the control valve 5 again.
In
The magnet valve 5 comprises a 2/2-way valve with a valve member 21. The valve member 21 has a frustoconical portion, on which a sealing face 23 is located. The valve member 21 is guided in a bore 25 of the housing 17. On its lower end in terms of
As needed, a second guide portion 29 may also be embodied on the valve member 21, in the vicinity of the sealing face 23. In this second guide portion 29, there is a plurality of flat faces 31, distributed over the circumference of the valve member 21. The flat faces 31 may for instance be distributed over the circumference at intervals of 120° or 90°. The flat faces 31 serve to establish a hydraulic connection between the portion 11a of the fuel inlet 11 and the portion 11b of the fuel inlet 11 when the magnet valve 5 is open. Above the second guide portion 29 in the housing 17, a valve seat 33 is provided. When the valve member 21 moves downward in terms of
In the lower portion of the bore 25, there is a closure element 28, which is secured in the housing 17. On the lower end of the valve member 21, a compression spring 54 is provided in the bore 25; this spring is braced on one end against an adjusting disk 26 for adjusting the spring force and on the other against the valve member 21 and lifts the valve member from the valve seat 33 when a coil 37 is made currentless. The adjusting disk 26 in turn rests on the closure element 28, and if the needs arises, it can be very easily replaced.
The coil 37 has two electrical terminals 39, by way of which the coil 37 can be supplied with electric current. The delivery of current to the coil 37 is controlled by a control unit, not shown, of the unit fuel injector or of the engine.
In the interior of the toroidal coil 37, there is an armature 41. The armature 41 is pressed onto a receiving mandrel 43 of the valve member 21. Below the coil 37, a magnet plate 45 is provided, which comprises a material which is a good conductor of the magnetic field lines of the coil 37. By means of the magnet plate 45, the heat generated in the coil 37 is dissipated, and the magnetic force exerted by the coil 37 on the armature 41 is increased. A spacer ring 47 of a nonmagnetic material, such as stainless steel, and a capsule 49 are slipped onto on the magnet plate 45. The capsule 49 and the spacer ring 47, like the spacer ring 47 and the magnet plate 45, are joined together in fluid-tight fashion by weld seams 51.
The armature 41 does not rest with its outer diameter on the capsule 49, so that it can move freely in the axial direction of the valve member 21. In the middle, the magnet plate 45 has a through bore 53, through which the receiving mandrel 43 protrudes into the chamber (not identified by reference numeral) that is defined by the capsule 49 and the magnet plate 45.
Between the magnet plate 45 and a stroke stop 55 embodied on the valve member 21, a spacer plate 57 is provided. The spacer plate 57 has a hole 59. The hole 59 may also be embodied as an oblong slot, which extends radially outward from the center point of the spacer plate 57 as far as its outer diameter. As a result, it is possible as needed to replace the spacer plate 57 with another spacer plate 57 of a slightly different thickness D, and as a result, by way of the remanent air gap, to adjust the resultant magnetic force of the magnet valve 5 in a simple way.
The magnet valve 5 functions as follows:
When the coil 37 is made currentless, the compression spring 54 opens the magnet valve 5, by lifting the sealing face 23 of the valve member 21 from the sealing seat 33. As a result, a hydraulic connection is made between the portions 11a and 11b of the fuel inlet. As soon as current is flowing through the coil 37, a magnetic force exerted by the coil 37 on the armature 41 pulls the valve member 21 downward counter to the force of the compression spring 54, so that the sealing face 23 of the valve member 21 rests on the valve seat 33 of the magnet valve 5. As a consequence, the hydraulic connection between the portions 11a and 11b of the fuel inlet 11 is interrupted, so that a pressure buildup can take place in the pump chamber 9 of the pump element 2 (see
The connection of the armature 41 to the receiving mandrel 43 by means of a cylindrical press fit has the advantage that the armature 41 can be pressed onto the receiving mandrel 43 far enough until it has reached the desired position relative to the stroke stop 55 of the valve member 21.
In
From
The installation and calibration of the magnet valve 5 are done in an installation device 61. This installation device 61 includes a cylindrical receptacle 63, in which the valve member 21 is received. The valve member 21 rests with the underside of the stroke stop 55 on one end of the receptacle 63. Next, the spacer plate 57, which may be of simple steel, and the magnet plate 45 are placed on the valve member 21 in such a way that the spacer plate 57 rests on the stroke stop 55, and with the aid of a pressing sleeve 65, the magnet plate 45 and the spacer plate 57 are pressed against the stroke stop 55.
In a further step, an installation sleeve 67 is driven from below against the spacer plate 57. Once the installation sleeve 67 has been driven from below against the spacer plate 57, without the spacer plate 57 lifting from the stroke stop 55 as a result, the position of the installation sleeve 67 is detected. Next, the installation sleeve 67 in
The spacer plate 57 and the magnet plate 45 move away from the stroke stop 55 by an amount A relative to the valve member 21. This position of the spacer plate 57 and magnet plate 45 is shown in
The installation sleeve 67 is locked in the position shown in
A plurality of longitudinal bores 42 are provided in the armature 41, so that the motion of the armature 41 in the capsule 49 is not hindered by the fuel (not shown) located in the capsule. At the same time, the design of these longitudinal bores 42 is utilized to achieve the optimal damping of the motion of the armature 41 and the valve member 21 at the end of the stroke. To that end, the longitudinal bores 41 may have one or more throttle restrictions, not shown.
In
Since the compression spring 54 has a certain variation in terms of its dimensions and spring rate, it is advantageous to calibrate the magnet valve when the valve member 21 and the compression spring 54 are built into the housing 17. To that end, in a first step, the coil 37 is supplied with a predetermined current. This current is so great that the coil 37 exerts a magnetic force on the armature 41 that is greater than the desired prestressing force of the compression spring 54. In a second step, the structural group, together with the compression spring 54, is pushed into its installed position in the housing 17, and the spring force exerted in the process on the valve member 21 by the compression spring 54 is measured and recorded as a function of the position of the valve member 21 in the housing 17. Next, the current supply to the coil 37 is interrupted. By evaluating the previously ascertained spring force and travel graph, it can be found whether, in the desired installed position, the spring force exerted by the compression spring 54 is correct.
If that proves not to be the case, then the spring force of the compression spring 35 can be adjusted by replacing the adjusting disk 26 with an adjusting disk 26 (see
Next, it is checked whether the magnet valve 5 closes when the coil 37 is supplied with the desired current intensity Iset. If the function of the magnet valve 5 proves not to be satisfactory, then the desired closing performance and opening performance of the magnet valve 5 can be adjusted by means of a further replacement of the adjusting disk 26. This operation is repeated until such time as the magnet valve 5 functions correctly.
By means of the magnet valve 5 of the invention, essentially the following advantages are obtained:
The bouncing between the armature 41 and the valve member 21 is entirely avoided.
There is therefore now only one compression spring 54 that acts on the valve member 21, with a favorable effect on the manufacturing costs and on the space required for the compression spring 54. In the prior art, two compression springs are necessary, one of which acts on the armature 41 and keeps it in contact with the valve member 21.
The adjusting disk 26 is a component that is relatively unproblematic to manufacture, and there is no need, as in the prior art, to pair different components in order to adjust the magnet valve 5. The desired opening and closing performance of the magnet valve 5 can be adjusted merely by replacing the adjusting disk 26. Moreover, adjusting the magnet valve 5 is made markedly simpler by the provision that the armature 41 and the valve member 21 form a component that is solidly joined together and whose dynamic performance is comparatively simple to control.
The armature 41 is guided by the valve member 21, so that in the region of the armature 41 and the capsule 49, separate guidance of the armature is no longer necessary, which reduces the costs and increases the functional reliability of the unit fuel injector of the invention.
Moreover, the advantage, known from the prior art, of a dry coil 37 can also be retained in the magnet valve 5 of the invention.
| Number | Date | Country | Kind |
|---|---|---|---|
| 102004015362.0 | Mar 2004 | DE | national |
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/EP2005/050210 | 1/19/2005 | WO | 00 | 9/22/2006 |
