1. Field of the Invention
The invention relates to an improved fuel injection system for internal combustion engines.
2. Description of the Prior Art
A fuel injection system for internal combustion engines of the type with which this invention is concerned is known from European Patent Disclosure EP 1 176 306 A2, in which, for triggering a fuel injection valve, a servo control circuit is provided, having a control valve which has a control piston which is longitudinally displaceable in a bore and which being triggered by an electromagnetic valve as a switching valve realizes the pressure control of the fuel injection valve. The control valve has a first valve seat, which defines a first pressure chamber, and a second valve seat, embodied as a slide seal, which defines a second pressure chamber. The fuel injection system is embodied without a pressure booster interposed between the pressure reservoir and the fuel injection valve.
From German Patent Disclosure DE 101 23 913 A1, a fuel injection system for internal combustion engines with a pressure boosting device for pressure boosting is known in which a 3-way valve is used to control the injector. Such 3-way valves, embodied as servo valves, as a rule have both an electromagnetically or piezoelectrically triggered switching valve and a control valve with a control piston, which is triggered by the switching valve. Control valves of this kind, which are constructed in a seat-slide embodiment, must control a large return quantity of the pressure boosting device. Various pressure chambers for connection to control lines are necessary on the control piston of the control valve here and are subjected from the inside to system pressure (rail pressure, or the pressure to be switched). This pressure burden causes the leakage gaps in high-pressure-tight guides to widen and causes deformation and widening of the control edges of slide seats and high notch tensions at bore intersections. These effects occurring because of the pressure burden impair the function and hence the durability of the servo valve.
The fuel injection system of the invention has the advantage that a force proportional to the pressure to be switched is exerted from outside on the valve body, so that the pressure forces acting on the critical parts of the control piston and the valve body are compensated for, and as a result the forces of deformation operative in the control valve can be kept slight. The proportional force is generated by the pressure prevailing in the fuel line; it is furnished by a fuel pump, for example, and is present as the system pressure. As a result, high notch tensions do not occur at the bore intersections of the valve body. Moreover, wear at the control edges of slide seats is reduced. The incident tensions remain markedly below the fatigue strength values, and as a result the production methods to be employed can be simplified, and more-economical materials can be used. This makes it possible to furnish a more-economical fuel injection system.
It is especially expedient to insert the bush in pressuretight fashion into a receptacle of the valve body and surround it by an annular chamber. An expedient embodiment moreover comprises having a transverse bore lead from the annular chamber into the valve pressure chamber that cooperates with the control piston. Via this transverse bore, the pressure equalization is accomplished between the inner chambers of the control valve and an outer chamber formed by an annular chamber. The invention is especially suitable for triggering fuel injection systems that have a pressure booster; the control edges of the control piston make it possible in alternation to connect a differential pressure chamber of the pressure booster to a high-pressure chamber that communicates with the high-pressure line, or to connect it to a low-pressure system connected to a return line.
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:
In
The fuel injector 1 in
The fuel injector 1 also has an electrohydraulic servo valve 90, which includes a hydraulic control valve 30 and an electrically triggerable switching valve 40; the triggering is effected by an electromagnetic or piezoelectric actuator 41. The switching valve 40 has an actuator piston 42, which is connected to the actuator 41 and is guided in an actuator bore 43. The actuator piston 42, with a sealing seat 44 on the actuator side, separates a leak fuel chamber 45 on the actuator side from an annular chamber 46 on the actuator side in fluid-tight fashion. However, it is equally possible for the control valve 30 to be embodied as a directly controlled valve. To that end, the actuator 41 is connected directly to the control piston 70, so that the switching motion of the actuator 41 is transmitted directly to the control piston 70, and the switching motion of the actuator 41 carries out the reciprocating motion of the control piston 70.
The control valve 30 has a valve body 31 with a receptacle 39 for a bush 80. In the bush 80, a stepped bore 32 is embodied, which discharges into a control chamber 33 and, on the opposite end, into a connecting chamber 36. Between the control chamber 33 and the connecting chamber 36, the stepped bore 32 forms a valve chamber 34 and a valve pressure chamber 35. In the stepped bore 32 of the control valve 30, a control piston 70 is guided axially displaceably. The control piston 70 is likewise embodied in graduated form, with a first piston portion 71 and a second piston portion 72; the first piston portion 71 has a larger piston diameter than the second piston portion 72. The end face of the first piston portion 71 forms a first pressure face 78. Because of the graduated embodiment of the control piston 70, an annular face is created between the first piston portion 71 and the second piston portion 72 and acts as a second pressure face 79. The first pressure face 78 is larger than the second pressure face 79. A first control edge 73 and a second control edge 74 are also embodied on the control piston 70.
The bush 80 is surrounded in the receptacle 39 by an annular chamber 82, which is closed in pressuretight fashion with a cap 83 and a seal 84 on the valve body 31. The annular chamber 82 is in communication with the fuel line 3 (rail), so that the pressure furnished by the fuel pump 5 prevails as the system pressure in the annular chamber 82, and as a result the bush 80 is acted upon by the system pressure prevailing in the fuel line 3. A transverse bore 85 is made in the bush 80 and connects the annular chamber 82 to the valve pressure chamber 35. From the annular chamber 82, a connecting bore 55 also leads to the pressure boosting chamber 27. A further connecting line 57 leads through the first piston portion 71 and connects the control chamber 33 to the valve pressure chamber 35 via an inlet throttle 56. The fuel line 3 acted upon by system pressure is connected to the annular chamber 82.
A connecting conduit 37 is embodied on the second piston portion 72 and, in the switching position shown, it connects the valve pressure chamber 35 with the valve chamber 34 located upstream of the first control edge 73. A sealing edge 75, which cooperates with the second control edge 74 and together with it, in a second switching position, to be described hereinafter, of the control valve 30, forms a sealing face is embodied on the stepped bore 32.
For connecting the various components, that is, the injection valve 10, pressure boosting device 20, control valve 30 and switching valve 40, pressure lines are used, which are for instance integrated with the fuel injector 1. The pressure chamber 14 of the fuel injection valve 10 communicates, by a first pressure line 51, with the high-pressure chamber 25 of the pressure boosting device 20. From the closing pressure chamber 16 of the injection valve 10, a second pressure line 52 leads to the return chamber 26 of the pressure boosting device 20. In addition, there is a connecting line 53 with a throttle between the closing pressure chamber 16 and the high-pressure chamber 25. The hydraulic pressure of the high-pressure fuel source 5 is carried via the high-pressure line 3 and the connecting bore 55 into the pressure boosting chamber 27 of the pressure boosting device 20. The pressure boosting chamber 27 thus communicates via the transverse bore 85 with the valve pressure chamber 35 of the control valve 30. A return chamber line 58 connects the return chamber 26 of the pressure boosting device 20 with the valve chamber 34 of the control valve 30.
From the connecting chamber 36 of the control valve 30, a first return line 61 leads, via a low-pressure system not shown in the drawing, back into a fuel tank, also not shown. The control chamber 33 of the control valve 30 communicates by means of a control line 59, via an outlet throttle 64, with the annular chamber 46 on the actuator side of the switching valve 40. Finally, a second return line 62 leads out of the leak fuel chamber 45 toward the actuator of the switching valve 40 into the low-pressure or return system. The return lines 61, 62 may, however, be embodied as one common return system instead.
A second exemplary embodiment is shown in FIG. 2. In this exemplary embodiment, the same components of the fuel injector 1 are identified by the same reference numerals. The special feature of the exemplary embodiment of
The mode of operation of the fuel injector 1 is as follows: At the onset of the injection event, because of the constant pressure in the high-pressure reservoir 5, the pressure prevailing in the pressure boosting chamber 27 also prevails, via the return chamber line 58, in the return chamber 26 and, via the second pressure line 52 and the connecting line 53, in the high-pressure chamber 25 and from there, via the first pressure line 51, in the pressure chamber 14. The actuator 41 of the switching valve 40, which in the present exemplary embodiment is an electromagnetic valve is supplied with current such that the actuator piston 42 closes the control line 59, which communicates with the control chamber 33 of the control valve 30, off against the leak fuel chamber 45 on the actuator side that communicates with the second return line 62. As a result, the same pressure prevails in the control chamber 33 as in the annular chamber 82, which communicates with the pressure boosting chamber 27 via the further connecting line 57. Because of the high pressure acting on the first pressure face 78, the first control edge 73 is pressed against the sealing seat. As a result, the valve chamber 36 and with it the first return line 61 are decoupled from the high pressure or system pressure. The injection valve 10 is closed.
The opening stroke motion of the closing piston 12 of the injection valve 10 is initiated by the lifting of the actuator piston 42 from the sealing seat 44 on the actuator side, which occurs with suitable delivery of current to the actuator 41, so that the control chamber 33 is made to communicate with the annular chamber 46 toward the actuator and with the connecting bore 55 toward the pressure booster. The flow resistances of the inlet throttle 56 and outlet throttle 64 should be dimensioned such that the pressure in the control chamber 33 drops, and the control piston 70 lifts from the sealing seat of the first control edge 73. Simultaneously, the pressure in the pressure boosting chamber 27 acts on the second, smaller pressure face 79, causing it to continue its opening motion and, with the second control edge 74, closing the valve pressure chamber 35 toward the valve chamber 34 and blocking off the high pressure from the connecting chamber 36. As a result, the return chamber 26 is made to communicate with the first return line 61, via the return chamber line 58, the valve chamber 34, and the connecting chamber 36. Accordingly, the high pressure prevailing in the return chamber 26 of the pressure boosting device 20 is depressurized via the return line 61, and the pressure in the return chamber 26 drops. As a result, the pressure boosting chamber 27e is activated, and the second partial piston 23, which has the smaller effective surface area, compresses the fuel in the high-pressure chamber 25, so that in the pressure chamber 14 communicating with the high-pressure chamber 25, the pressure force engaging the pressure shoulder 13 in the opening direction rises, and the closing piston 12 uncovers the injection openings 11. As long as the return chamber 26 is pressure-relieved, the pressure boosting device 20 remains activated and compresses the fuel in the high-pressure chamber 25.
For terminating the injection event, the switching valve 40 is returned to its outset position. This disconnects the return chamber 26 from the first return line 61 and connects it to the supply pressure of the high-pressure fuel source 5 again. As a result, the pressure in the high-pressure chamber 25 drops to system pressure, so that system pressure prevails again in the pressure chamber 14 as well. The restoration of the closing piston 12 is reinforced by the closing spring 17 disposed in the closing pressure chamber 16 and is realized by the system pressure also prevailing via the second pressure line 52. After the pressure equilibrium, the pressure booster piston 21 is returned to its outset position by the restoring spring 18, and the high-pressure chamber 25 is filled from the high-pressure fuel source 5 via the connecting line 53.
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.
Number | Date | Country | Kind |
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103 37 574 | Aug 2003 | DE | national |
Number | Name | Date | Kind |
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5687693 | Chen et al. | Nov 1997 | A |
6283441 | Tian | Sep 2001 | B1 |
6637409 | Brenk et al. | Oct 2003 | B2 |
6655602 | Shafer et al. | Dec 2003 | B2 |
6745952 | Hlousek | Jun 2004 | B1 |
20040099246 | Gould | May 2004 | A1 |
Number | Date | Country |
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1176306 | Jan 2002 | EP |
Number | Date | Country | |
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20050035212 A1 | Feb 2005 | US |