The invention relates to a method for producing a fuel injection valve.
A method of said type for producing a fuel injection valve (hereinafter also referred to, in part, as “injector”) is already generally known and is used in particular for fuel injection valves in so-called common rail injection systems. Here, lift-controlled common rail injectors are known in which the nozzle needle is servo-driven. As pressure setting means, use is made of piezo valves and magnet valves by means of which the servo circuit is controlled. For fast closure of the valve needle, a permanent low-pressure stage is often installed which exerts a permanent closing force on the valve needle. The disadvantage here is however the relatively large amount of leakage that occurs between the high-pressure side and the low-pressure side. Leakage inevitably leads to the requirement for a higher pump power in the common rail injection system, and therefore to losses in the efficiency of the system. This is a problem particularly at relatively high pressures.
For this reason, the most modern injectors for extremely high injection pressures (this means pressures in the region of approximately 2000 bar) are designed to exhibit low leakage by virtue of the low-pressure stage being dispensed with. As a result of the lack of the low-pressure stage, however, only small closing forces are available for the valve needle. As a result, the response time between the actuation of the valve needle and the start of injection is relatively short. The response time is dependent primarily on the stiffness of the valve needle. Specifically because said response time is short in the case of an injector without a low-pressure stage, even an extremely small change in needle stiffness leads to a significant shift in the start of injection and change in the injected fuel quantity. The stiffness of the valve needle is dependent on the diameter and the length of the valve needle. If it is sought to design injectors of different structural length to have equal response times, it is necessary to realize corresponding waisting or diameter variation of the valve needle for each type or each length of injector. In this way, it is possible for the stiffness of the valve needles to be made consistent for all injectors. This however results in relatively long machine set-up times. A variation of only the needle length, with the needle diameter being equal for all injector structural lengths, would be ideal. This is however not possible owing to the resulting differences in the stiffness of the valve needle.
Taking the presented prior art as a starting point, it is the object of the invention to further develop a method for producing a fuel injection valve such that the response time is at least substantially constant in fuel valves of different structural length or with different lengths of valve needle. Said object is achieved with a method for producing a fuel injection valve. Here, the invention is based on the concept of compensating for the different mechanical stiffness owing to different lengths of the valve needles by means of a variation of the “hydraulic stiffness” of the control chamber which is operatively connected to the valve needle. The underlying knowledge here is that, the larger the volume in the control chamber, the longer the delay or the response time until the opening of the injection orifices. In other words, this means that a relatively short and therefore stiff valve needle is compensated for by virtue of said valve needle being placed in operative connection with a control chamber which has a relatively large storage volume for fuel, and vice versa.
To permit particularly economical production of the fuel injection valve in which always the same valve piece with always the same recess for the control chamber can be used, it is proposed in one embodiment of the invention, which is particularly advantageous from a construction aspect, that the geometry of the control chamber in the region in which the valve needle is guided is in the form of a cylindrical bore with always the same diameter and always the same depth, and that the volume of the control chamber is adapted by means of a shortening or lengthening of that portion of the valve needle which is guided in the control chamber.
If a variation of the length of that portion of the valve needle which is guided in the control chamber is not sufficient to obtain the desired actuation time of the fuel injection valve, it is provided in a further refinement, which is particularly advantageous from a construction aspect, that the valve needle is composed of at least a standardized first portion arranged in the control chamber, which first portion is connected, on the side facing away from the control chamber, to a second cylindrical portion, and that the diameter of the second portion of the valve needle is varied such that, to shorten the delay time, the diameter of the valve needle is increased and, to lengthen the delay time, the diameter of the valve needle is decreased.
Here, to limit the number of possible different diameters of the valve needles, it is particularly advantageous if the diameter of the valve needle is varied in diameter steps, and if fine adjustment of the delay time is carried out by means of an adaptation of the volume of the control chamber by means of a variation of the length of the second cylindrical portion. A combination of a valve needle of a certain diameter with a valve needle of a certain length hereby takes place, in such a way that that portion of the standardized first portion which projects into the control chamber forms a certain control volume.
Furthermore, it is particularly advantageous if, taking into consideration the minimum and maximum possible volume of the control chamber and the available diameter steps of the valve needle, that valve needle diameter is selected which leads to a minimum volume of the control chamber. This means that always that valve needle which has the smallest diameter is selected. The further adaptation of the delay time is thereby realized by means of a lengthening or shortening of the valve needle.
Furthermore, the fuel valves can be produced particularly economically if the second portion of the valve needle is connected, on the opposite side from the standardized first portion, to a standardized third portion.
The connection between at least the second portion of the valve needle and the standardized first portion and if appropriate between the second portion of the valve needle and the third portion is realized preferably by laser welding. In this way it is possible to produce high-strength connections in a relatively economical manner.
Fuel valves produced in accordance with the method according to the invention can be produced particularly economically with regard to their structural length if the injector housing of the fuel injection valve has a standardized upper part with the closing element, with an actuating mechanism for the closing element and if appropriate with the valve piece, and a standardized lower part with a nozzle body, and if a central part which determines the overall structural length of the injector housing is arranged between the upper part and the lower part.
Further advantages of the method according to the invention for producing a fuel injection valve, and of the fuel injection valve, will emerge from the following description of preferred exemplary embodiments and on the basis of the drawings, in which:
Identical components or components of identical function are provided with the same reference numerals in the figures.
A fuel injection system 7 as described has a separate fuel injection valve 10 for each cylinder of an internal combustion engine, which fuel injection valves are all connected to the rail 2.
The fuel injection valve 10 has an injector housing denoted as a whole by 11. Here, the elongate injector housing 11 is composed of three assemblies: a standardized upper part 12, a central part 13 which is dependent on the structural length of the fuel injection valve 10 and which is in particular of annular design and formed if appropriate with different diameters, and a likewise standardized lower part 14. Between the upper part 12 and the central part 13 there is inserted into a seal groove a sealing ring 15, wherein the pressure-tight connection between the central part 13 and the upper part 12 is realized for example by means of an encircling laser weld or by means of an encircling flanged portion. In contrast, between the central part 13 and the lower part 14, with the interposition of a sealing ring 17, there is formed for example a screw connection 18 for connecting the central part 13 to the lower part 14 in a pressure-tight manner.
A pressure-balanced magnet valve 20 is inserted or arranged in the upper part 12, which magnet valve has a magnet core 21 and also a magnet coil 22 arranged in the magnet core 21. The magnet valve 20 furthermore has a magnet armature 23 which acts as a closing element and which is guided in an axially movable manner in a pin-shaped guide member 24. The guide member 24 is arranged in a through bore 25 of the magnet core 21 and has a step 26 between which and the facing side of the magnet armature 23 is supported a compression spring 28. Here, the compression spring 28 is arranged in a spring chamber 29 which, like the region of the upper part 12, in which the magnet core 21 is situated, is connected at least indirectly to the return line 5 and therefore to low pressure.
In the de-energized state of the magnet coil 22, the magnet armature 23 is pressed against a seat 30 of a valve piece 32. Here, the valve piece 32 is screwed into an upper portion of the central part 13, and here, is seated on a step 33 of the central part 13. A through bore 34 with an outflow throttle 35 is arranged in the longitudinal axis of the valve piece 32. The outflow throttle 35 is connected to a control chamber 37 which is formed as a blind bore 38 on the opposite side of the valve piece 32 from the magnet armature 23. On the open end side opposite from the outflow throttle 35, there projects into the blind bore 38 a first guide portion 39 of a valve needle 40.
The valve needle 40, which is of substantially cylindrical design, has on its opposite end from the valve piece 32 a second guide portion 41 which adjoins a valve tip 42. The valve tip 42 is pressed against a seat 46 of a nozzle body 47 by means of a compression spring 43 which is supported between a collar 44 of the valve needle 40 and the facing end surface of the valve piece 32. The seat 46 delimits a nozzle chamber 48 into which opens at least one through bore which serves as a fuel outlet orifice 49. Here, the nozzle body 47 is inserted into the lower part 14 of the injector housing 11.
The function of the fuel injection valve 10 as described is generally known and will therefore be explained only briefly, as follows: in the de-energized state of the magnet valve 20, the magnet armature 23 is pressed by the force of the compression spring 28 against the seat 30, such that the control chamber 37 is closed. Furthermore, the valve needle 40 is pressed by means of the compression spring 43 against the seat 46, such that the fuel outlet orifice 49 is also closed. When the magnet valve 20 or the magnet coil 22 is energized, the magnet armature 23 is raised from the seat 30, such that a passage is created from the control chamber 37, which is under high fuel pressure, to an armature chamber 51 which is connected to the return line 5. The flow of the fuel out of the control chamber 37 has the effect that the valve needle 40 is raised from its seat 46, and fuel flows from the high-pressure chamber 52, which is subjected to high pressure via the supply line 1, and from the nozzle chamber 48 out of the fuel injection valve 10 through the fuel outlet orifice 49, and is discharged into the combustion chamber of the internal combustion engine.
The valve needle 40 has a certain stiffness based on its length L1, its material and therefore its modulus of elasticity, and its cross-sectional area A. In the de-energized state of the magnet valve 20, the valve needle 40 is pressed against the seat 46, wherein an elastic deformation of the valve needle 40 occurs owing to the above-described material properties and the geometry of the valve needle 40. When the magnet coil 20 is energized, and upon the associated pressure drop in the control chamber 37, the lifting of the valve needle 40 from the seat 46 takes place only when the pressure prevailing at the upper end surface 53 of the valve needle 40 or the corresponding axial force has decreased to such an extent that the valve needle 40 assumes its original length again. It is at the same time pointed out that the pressure drop in the control chamber 37, that is to say the period of time between the lifting of the magnet armature 23 from the seat 30 and the reduction in the axial force at the end surface 53, takes a certain period of time which is dependent on the size of the volume of the control chamber 37. The sum of the delays, resulting firstly from the pressure drop in the control chamber 37 and secondly from the elastic deformation of the valve needle 40, is referred to as the delay time or actuation time t.
As can be seen from a juxtaposition of
Here, the ratio of the enlargement of the valve needle stroke ΔH owing to the enlargement of the volume of the control chamber 37 to the shortening of the needle stroke owing to the shortening of the valve needle ΔL can be calculated as follows:
ΔH/ΔL=(E(37)×A(37))/(E(65; 65a)×A(65; 65a)),
Where E(37) is the modulus of elasticity of the fuel in the region of the control chamber 37,
A(37) is the cross-sectional area A in the region of the control chamber 37,
E(65; 65a) is the modulus of elasticity of the portion 65; 65a,
A(65; 65a) is the cross-sectional area A in the region of the portion 65; 65a,
and where, according to the invention, the ratio ΔH/ΔL lies between 100 and 500.
The fuel injection valves 10, 10a and 60, 60a as described may be changed or modified in a variety of ways. In particular, the magnet assembly or the magnet valve 20 may be constructed differently or replaced with a piezo. It is also additionally mentioned that the fuel injection valves 10, 10a, 60, 60a may be designed such that the magnet valve 20 can be closed again already before the injection begins or the through bore 34 is opened up. Variations between successive injections and back pressure dependencies can be reduced in this way.
Number | Date | Country | Kind |
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102009046582.0 | Nov 2009 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2010/064647 | 10/1/2010 | WO | 00 | 4/24/2012 |