The present disclosure relates generally to pumps and, more specifically, to a high-pressure fuel pump and/or an engine valve for pressurizing a fuel.
Both in the case of engine valves and in the case, for example, of piston pumps that are used as high-pressure fuel pumps for the pumping of fuel, a rod is commonly provided which is driven by a plunger. The plunger itself is driven, for example in the case of a piston pump as a high-pressure fuel pump, by a camshaft of an internal combustion engine.
In the case of the piston pump 14, fuel is pressurized by way of the movement of the piston 20 along a piston axis 24.
In the case of an engine valve 18, the movement of the rod 12 along a rod axis 26 causes the engine valve 18 to be opened and closed, and thus, upon opening, a pressure is discharged, and upon closing of the engine valve 18, pressure is built up. Altogether, therefore, the arrangement shown in
The pressure-influencing device 28 in
Also schematically illustrated in
In general, in the case of a rod 12 driven by the plunger 10—for example in engine valves 18 or in piston pumps 14—considerable contact forces are generated at a contact point 46 between a rod end 48 in the second end region 42 of the rod 12 and the traverse 36 of the plunger 10. This is caused firstly by the axial load Fa but also by way of geometrical tolerances of the individual components of the pressure-influencing device 28 and the respective play of the individual elements in the pressure-influencing device 28.
In detail, the following forces act:
All of these forces lead to considerable bearing reaction forces both in the plunger guide 32 and in the rod guide 30, which bearing reaction forces can lead to wear and ultimately to abrasion of the linear or sliding guides. The maximum admissible bearing reaction forces in the guides 50, 52 determine the maximum admissible errors of the overall system.
Until now, to improve the system, close tolerances, and associated high production costs, and/or an increase of the guide lengths, have/has been implemented. Here, the individual forces are influenced as follows:
Altogether, therefore, the considerable contact forces that prevail in a construction according to the prior art as per
In accordance with the teachings of the present disclosure, a high-pressure fuel pump for pressurizing a fuel has a piston which is arranged so as to be movable along a piston axis between a first, top dead center and a second, bottom dead center, and a plunger with a traverse which is arranged substantially perpendicular to a plunger axis and which serves for transmitting kinetic energy from a plunger drive to the piston in a contact region between a traverse surface and an end region of the piston. In the contact region, the piston has a calotte-shaped end region, and the traverse has a likewise calotte-shaped recess.
The “top dead center” is to be understood to mean a position of the rod in which the rod is, by a drive, for example a camshaft, pushed to its highest deflection point along the rod axis relative to an axis of, for example, the camshaft. Analogously, the expression “bottom dead center” is to be understood to mean the point at which the rod is situated closest to the axis of, for example, the camshaft.
Correspondingly, a pressure-influencing device for influencing a pressure in a medium has a rod with a first end region for delimiting a space which has the medium, wherein the rod is arranged so as to be movable along a rod axis between a first, top dead center and a second, bottom dead center. Also provided is a plunger with a traverse which is arranged substantially perpendicular to a plunger axis and which serves for transmitting kinetic energy from a plunger drive to the rod in a contact region between a traverse surface and a second end region of the rod, said second end region being arranged opposite the first end region. In the contact region, the rod has a calotte-shaped end region, and the traverse has a likewise calotte-shaped recess.
Thus, the second end region of the rod is formed by the calotte-shaped end region.
Here, the pressure-influencing device may be a high-pressure fuel pump or an engine valve. In the case of the high-pressure fuel pump, the rod is then formed by the piston.
By way of the described arrangement, it is now the case that the rod, by way of its calotte-shaped rod end, moves no longer on a planar traverse but in a calotte-shaped depression, that is to say the previous “calotte/surface contact” is replaced with “calotte/calotte contact”. Here, a calotte, in particular a spherical calotte, is formed into the previously planar surface of the traverse. In this way, for the same Hertzian stress, it is possible to select a smaller radius on the calotte-shaped end region of the rod. The angle error y is thereby eliminated entirely. Only a slight concentricity error remains between a rod axis and a central point of the calotte shape. This has a positive effect on the transverse forces and the resulting moments, because the contact angles β1 and β2, and the lever arms al and a2, are reduced.
This is because, owing to the calotte-shaped recess in the traverse, a contact point K between the traverse and the rod is shifted from an outer edge region of the calotte-shaped end region of the rod toward the rod axis. In this way, the described lever arms a1 and a2, which define spacings between the contact point K and a plunger guide axis and rod guide axis respectively, and the contact angles β1, β2, which define angles in each case of a normal to the traverse at the contact point K with respect to a rod axis and a plunger axis respectively, are considerably reduced.
In this way, the contact forces acting between the elements can be considerably reduced, but without changing tolerances and guide lengths to an excessive extent, such that altogether, an improved transmission of kinetic energy from the plunger to the rod can be achieved, without the production costs being excessively increased in the process. The traverse preferably has, in regions adjoining the calotte-shaped recess, a traverse surface which is of planar form substantially perpendicular to the plunger axis. Thus, that region of the traverse surface which comes into contact with the calotte-shaped end region of the rod is preferably not entirely of calotte-shaped form but additionally still has planar sub-regions. This is advantageously conducive to reinforcing the traverse overall. Furthermore, it may however also be advantageous for further measures to be implemented for stiffening the traverse, for example if the traverse is of thicker form parallel to the plunger axis, or is formed from a stiffer material, in relation to a traverse from the prior art.
It is possible for the calotte-shaped recess to be generated in the traverse surface by being formed into a planar traverse surface by stamping. An inexpensive realization of the traverse surface geometry is possible in this way.
In some embodiments, the calotte-shaped recess is arranged symmetrically about an axis which bisects the traverse perpendicularly to the longitudinal axis thereof. This means that the calotte-shaped recess is arranged, overall, symmetrically on that side of the traverse which comes into contact with the calotte-shaped end region of the rod. In this way, it is possible for a defined position of a central point of the calotte-shaped recess on the traverse to be generated, which in turn leads to defined guidance of the rod by the traverse.
The traverse may be arranged so as to be movable radially with respect to the plunger axis, wherein the traverse is inserted into the plunger without radial fastening. In this way, it is possible for the concentricity errors to be compensated by way of the radially movable traverse. This is because the concentricity errors constitute only a very small fraction of the lever arms a1 and a2; they constitute a static position error of the calotte shape. In the case of an traverse that is movable radially with respect to the plunger axis, it is thus the case that the traverse finds its position within the initial strokes of the rod, and can thus compensate the static position error.
A recess radius of the calotte-shaped recess of the traverse is greater than a rod radius of the calotte-shaped end region of the rod. This yields the advantage that the rod is, in all operating states, reliably situated with its calotte-shaped end region in the calotte-shaped recess of the traverse.
Some embodiments include a rod guide having a rod guide axis, wherein a rod end radius of the calotte-shaped end region of the rod is smaller than or equal to a spacing, which exists at the top dead center of the rod, between a tangent to a rod calotte surface at the rod axis and an intersection point of the plunger axis and the rod guide axis.
The spacing between the tangent to the calotte-shaped end region of the rod, at the point at which the rod axis intersects an outer surface of the rod, and an intersection point of the plunger axis with the rod guide axis changes during the operation of the rod. The spacing is smaller at the top dead center of the rod than at the bottom dead center and in all operating states in between. This means that the radius of the calotte-shaped end region of the rod is selected to be smaller than or equal to the smallest spacing between the intersection point of the guide axes and a smallest protrusion of the rod end—in the position at top dead center. This has the effect that the contact angles β1 and β2 are smaller than or equal to the angle error α, and it is thus the case that only low transverse forces act.
If, for construction-related reasons, it is not possible for the rod end radius of the calotte-shaped end region of the rod to be designed to be smaller than the described minimum spacing at top dead center, the recess radius of the calotte-shaped recess may b considerably greater than the radius of the calotte-shaped end region. Here, a rod guide having a rod guide axis is provided, wherein a rod end radius of the calotte-shaped end region of the rod is greater than a spacing, which exists at the top dead center of the rod, between a tangent to a rod calotte surface at the rod axis to an intersection point of the plunger axis and the rod guide axis, wherein a recess radius of the calotte-shaped recess of the traverse is greater than a rod end radius of the calotte-shaped end region of the rod, to such an extent, in the case of identical materials being used, that the Hertzian stress is situated in the region of contact between a planar traverse surface and a calotte-shaped end region of the rod.
This means that, if the radius of the calotte-shaped end region of the rod cannot be realized for example owing to Hertzian stress values having increased to too great an extent owing to the very small radius of the end region, the values of the Hertzian stress should be compensated by way of a larger radius of the calotte-shaped recess. This is because, the greater the radius of the calotte-shaped recess of the traverse is, the smaller the contact surface between the end region of the rod and traverse surface becomes, owing to the Hertzian stress. In relation to an arrangement in which no calotte-shaped recess is provided in the traverse, it should be the case that at least similar values for the Hertzian stress are realized.
The pressure-influencing device may be a high-pressure fuel pump, though may alternatively also be an engine valve. An example embodiment of the invention will be discussed in more detail below on the basis of the appended drawings.
In the drawings:
Below, the expressions “rod” and “piston” are synonymous with one another. The same applies to the expressions “pressure-influencing device”, “engine valve” and “high-pressure fuel pump”.
The roller 38 and the camshaft 65 thus jointly form a plunger drive 66.
In the idealized illustration in
As can also be seen in
In the ideal embodiment of the pressure-influencing device 28, the traverse 36 and the rod 12 make punctiform contact in a contact region 68 of a traverse surface 70 and of a second end region 42, which is situated opposite a first end region 22, of the rod 12. In the contact region 68, the traverse has a calotte-shaped recess 72, and the rod 12 has a calotte-shaped end region 74. The calotte-shaped recess 72 does not span the entire traverse surface 70, but rather the traverse 36 has, adjacent to the calotte-shaped recess 72, a traverse surface which is of planar form perpendicular to the plunger axis 40. The calotte-shaped recess 72 may be formed into the traverse surface 70 for example by stamping. The calotte-shaped recess 72 is arranged symmetrically on the traverse surface 70, such that the lowest point of the calotte-shaped recess 72 is intersected by the plunger axis 40, which runs perpendicular to a longitudinal axis 76 of the traverse 36.
This is shown by a comparison between a pressure-influencing device according to the prior art, as shown in
As can be seen in
This means that the angle error γ may, in expedient situations, hereinafter referred to as “best case”, compensate the angle error α, depending on sign. Said angle error γ may however also further increase the angle error α, this being referred to hereinafter as “worst case”.
The sum of α and γ results in the contact points, illustrated in
Altogether, this yields considerably lower transverse forces acting on the pressure-influencing device 28, which leads to considerably lower loads and considerably less wear of the pressure-influencing device 28.
In some embodiments, the Hertzian stresses may be kept constant without restriction of the production tolerances. This can be realized through selection of the radius relationships of calotte-shaped recess 72 and calotte-shaped end region 74. Here, a distinction is made between two cases. The distinguishing criterion is the condition that the Hertzian stress should not be increased in relation to an arrangement of the pressure-influencing device 28 as shown in
In the first case, it is possible for the rod end radius 84 to be designed to be smaller than the spacing amin, as illustrated in
Owing to Hertzian stresses becoming too large, however, it may also not be expedient to design the rod end radius 84 to be smaller than the spacing amin. Said situation—second case—is illustrated in
In all operating states, however, it is advantageous for a recess radius 88 of the calotte-shaped recess 72 of the traverse 36 to be greater than the rod end radius 84.
In some embodiments, the dimensions ensure adequate stiffness of the traverse 36. In this way, the contact point K is always situated between the axes 50, 52 and a very small variance between “worst case” and “best case” tolerances can be realized.
Owing to the Hertzian stresses, it may however also be expedient for the rod end radius 84 to be selected to be greater than amin, This configuration also constitutes a significant improvement in relation to the situation in
The situation—second case—is illustrated in
By contrast, the Diagram C illustrates the situation for a pressure-influencing device 28 without calotte-shaped recess 72 for the “worst case” scenario—contact point 78 in
Diagram B shows the force conditions for a pressure-influencing device 28 which has a calotte-shaped recess 72 in the traverse 36. In the diagram B, the traverse 36 exhibits radial mobility relative to the plunger axis 40.
Diagram D shows the situation of a pressure-influencing device 28 with the calotte-shaped recess 72, but in the case of the traverse 36 being fixed and not being radially movable relative to the plunger axis 40.
It can be clearly seen that the arrangement with calotte-shaped recess 72 and movable traverse 36 provides considerably better force conditions than the “worst case” scenario of the pressure-influencing device 28 without calotte-shaped recess 72. Since the achievement of “worst case” and “best case” cannot be controlled, and the force profile in Diagram B closely resembles the “best case” situation, more effectively controllable force conditions are obtained in a pressure-influencing device 28 with calotte-shaped recess 72. At the same time, the differences between Diagrams B and D show that a radially movable 36 may be very much favored.
Altogether, the calotte-shaped recess 72 generates direction-independent transverse forces which lie at a low level between “best case” and “worst case” of the pressure-influencing device 28 according to the prior art. This corresponds to a general reduction of the acting transverse forces.
Altogether, the transverse forces arising from the axial forces Fa owing to geometrical discontinuities of the components can be reduced by up to 40% in relation to the “worst case” configuration from the prior art. The detrimental influences of the transverse forces owing to the contact angles β1, β2 can be largely eliminated, leading to a reduction of the transverse forces. At the same time, the perpendicularity of the traverse 36 with respect to the plunger axis 40 is virtually irrelevant, which leads to a reduction in production costs. The calotte-shaped recess 72 of the traverse 36 can be generated by way of simple stamping, which is particularly inexpensive. Altogether, the angle error γ is eliminated entirely, and the variance and magnitude of the overall angle error β1 and β2 is considerably reduced, such that, for the design process, virtually constant loads can be expected, and the “best case” and “worst case” advantageously lie close together. Additionally, with skilled pairing of the rod radius 84 and of the recess radius 88, it is even possible for β1 and β2 to be kept smaller than the inevitable angle error α between the axes 50, 52 of the guides.
These advantages can be utilized in order to increase the axial load Fa overall, to improve the service life of the guides 30, 32, that is to say increase robustness, to reduce the required guide lengths, which is associated with a reduction in costs and reduction in size of structural space, and, altogether, to increase the tolerances of the components, which likewise contributes to a reduction in costs in the production process.
In some embodiments, the calotte-shaped recess 72 may be provided in a separate slide shoe which is arranged in the plunger 10.
Number | Date | Country | Kind |
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10 2014 216 173.8 | Aug 2014 | DE | national |
This application is a U.S. National Stage Application of International Application No. PCT/EP2015/064309 filed Jun. 24, 2015, which designates the United States of America, and claims priority to DE Application No. 10 2014 216 173.8 filed Aug. 14, 2014, the contents of which are hereby incorporated by reference in their entirety.
Filing Document | Filing Date | Country | Kind |
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PCT/EP2015/064309 | 6/24/2015 | WO | 00 |