Patent Application
20170067376
The present disclosure relates to a hydraulic camshaft adjuster having an at least two-piece rotor. The at least two-piece rotor can rotate about an axis, and is composed of a first rotor element and a second rotor element.
The present disclosure also relates to an at least two-piece rotor for a hydraulic camshaft adjuster.
The disclosure furthermore relates to a method for the production of a rotor for a hydraulic camshaft adjuster.
It is generally known that camshaft adjusters enable optimal valve control times over a broad load and rotational rate range for a motor. In this manner, significant reductions in emissions and fuel consumption have been achieved. Furthermore, by optimizing the torque and the performance, the driving enjoyment is increased significantly. A distinction is made in the prior art between electric camshaft adjusters and the hydraulic camshaft adjusters specified in the introduction.
Rotors are known from the field of hydraulic camshaft adjusters, which are composed of a first rotor element and a second rotor element. This is disclosed, for example, in the German patent application DE 10 2009 053 600 A1. Two rotor elements are connected with pins or sintered therein. The disadvantage with this is that additional connecting parts such as pins are required. As a result, there are additional costs for parts and installation.
Another embodiment for joining two rotor elements of a rotor is described in the German patent application DE 10 2008 028 640 A1. Two rotor elements are designed therein, such that they can be joined due to their respective “distinct” geometries. Two rotor elements that seal oil channels through sinter facets, and are thus connected to one another, is disclosed in the German patent application DE 10 2011 117 856 A1. The European patent application EP 2 300 693 B1 furthermore describes two identical rotor elements, joined by means of a form fit and press fit to form the oil channels. In the documents specified in this paragraph, the form-fitting and sealing elements extend beyond sealing surfaces, and can be produced either by additional separating planes in the sintering tool or by an excess pressure applied to the entire surface of the flange on the rotor elements. The negative consequences here are the additional tool costs, larger pressing machines and a reduction in quality of the sealing surfaces in the interstice subjected to excess pressure, e.g. the degradation of the evenness and parallel alignment of the end surfaces of the rotor, and an increase in the internal leakage between the oil channels as a result of irregularities in the interstice.
The rotor designed in the form of a composite system, wherein the rotor core plus the cover form the oil channels, is disclosed in the European patent application EP 1 731 722 B1. The separating plane is not in the sintered part thereby, because the complete width of the rotor is produced using sintering technology, as is the case with the single-piece rotors known from the prior art. As a result, it is not possible to obtain a cost reduction in relation to a single-piece rotor, because a larger compression machine having a higher pressure force must be used, as is the case with a single-piece rotor. A cost reduction first obtained by reducing the width of the rotor, e.g. by means of the division of the rotor described in the introduction, can be realized as a result of lower cost factors for the smaller compression machine.
One objective of the present disclosure is thus to further develop a hydraulic camshaft adjuster, having an at least two-piece rotor, such that it is constructed in a cost-effective manner, with higher quality, and is furthermore functionally reliable when in operation.
This objective is achieved by means of a hydraulic camshaft adjuster having an at least two-piece rotor, comprising the features described herein.
Another objective of the present disclosure is to create an at least two-piece rotor for a hydraulic camshaft adjustor, that is produced simply and economically.
This objective is achieved by means of an at least two-piece rotor for a hydraulic camshaft adjuster comprising the features of described herein.
Another objective of the present disclosure is to provide a simple, quality-improving and economical method for producing a rotor for a hydraulic camshaft adjuster.
This objective is achieved by means of a method for producing a rotor for a hydraulic camshaft adjuster comprising the features described herein.
With the hydraulic camshaft adjuster according to the disclosure, having an at least two-piece rotor, which can rotate about an axis and is composed of a first rotor element and a second rotor element, the first rotor element has at least one first bore-hole, which is aligned with at least one second bore-hole of the second rotor element. A joinable connecting element is located thereby in the at least one first bore-hole and the at least one second bore-hole, such that the first rotor element is connected to the second rotor element in a form-fitting, force-fitting and/or material bonded manner. The first rotor element and the second rotor element may be connected to one another via four connecting elements, such that the first rotor element therefore has four first bore-holes, and the second rotor element has four second bore-holes. As a matter of course, other embodiments, having more or fewer connecting elements, first bore-holes and second bore-holes, are also conceivable.
In a first embodiment of the hydraulic camshaft adjuster according to the present disclosure, a first free end of the joinable connecting element is secured in place by means of a sintered connection or a laser-welded seam on a bore-hole wall of the at least first bore-hole and/or a second free end of the joinable connecting element is secured in place by means of a sintered connection or laser-welded seam on a bore-hole wall of the at least second bore-hole.
In another embodiment of the present disclosure, the joinable connecting element is a powder column or a sintering core. The advantages of the connecting element in the form of a powder column or a sintering core shall be described below in reference to the method according to the present disclosure for producing a rotor for a hydraulic camshaft adjuster.
Another embodiment of the hydraulic camshaft adjuster according to the present disclosure provides that the first rotor element and the second rotor element of the at least two-piece rotor has numerous blades, each of which have the at least first bore-hole, or the at least second bore-hole, formed therein, and in each case a joinable connecting element extends from the first bore-hole into the second bore-hole. In this embodiment as well, the first rotor element and the second rotor element are connected to one another via four connecting elements.
It should furthermore be noted that the at least two-piece rotor can also be designed such that the same connecting technology, i.e. a joinable connecting element in at least a first and second bore-hole, can also be used for other parts of the hydraulic camshaft adjuster according to the present disclosure, e.g. in the stator.
With the at least two-piece rotor for a hydraulic camshaft adjuster according to the present disclosure, a first rotor element has, according to the present disclosure, at least a first bore-hole, and a second rotor element has, according to the present disclosure, at least a second bore-hole, wherein a powder column or a sintering core is pressed and/or sintered into the at least first bore-hole or the at least second bore-hole. Advantageously, the powder column or the sintering core is pressed into and/or sintered to a bore-hole end or the middle of a bore-hole, i.e. a blind bore-hole, or optionally, two separate, opposing, coaxial blind bore-holes, is/are formed.
The method for producing a rotor for a hydraulic camshaft adjuster is distinguished according to the present disclosure by the following steps: in a first step, at least one first bore-hole in a first rotor element and at least one second bore-hole in a second rotor element can be formed by means of sintering, or optionally, drilled. It should be ensured thereby that a diameter of the at least second bore-hole, which is can be produced by means of a sintering shaping process, is the same as, or slightly smaller than, a diameter of the at least first bore-hole. The nominal diameter thereof is 2.0 to 5 mm in one embodiment.
In a subsequent step, a connecting element is formed at an end or in the middle of the at least first bore-hole. If a connecting element is formed at the end of the bore-hole, then the first rotor element has a blind bore-hole. If a connecting element is formed in the middle of the bore-hole, then the first rotor element has two separate, coaxially opposing blind bore-holes.
A subsequent step provides that the first rotor element and the second rotor element are place on top of one another, such that the at least first bore-hole is aligned with the at least second bore-hole.
In a further step, the joinable connecting element is axially sheared off from a bore- hole wall of the at least first bore-hole by means of a pressing element, such that the joinable connecting element is at least partially joined into the at least second bore-hole. In particular, the joining of the joinable connecting element occurs by means of a longitudinal press-fit into the at least second bore-hole, by means of a pressure mandrel for example. The joinable connecting element may be inserted halfway thereby, in terms of its axial length, into the at least second bore-hole, i.e. the connecting element is placed between the at least first and at least second rotor elements. The length of the sheared off and joined connecting element is 3 to 20 mm in an embodiment, depending on the thickness of the assembled, at least two-piece rotor.
The joined rotor is subsequently sintered and calibrated.
Alternatively, already pre-sintered rotor parts can be joined to one another in an assembly tool by means of shear-joining, and calibrated in the same tool.
As a result, two different sequences with respect to the sintering and calibration procedures can be used in the production of the rotor. In brief, these are: the first embodiment provides that the two rotor elements, including their bore-holes, are pressed from sintering powder, subsequently both rotor elements are joined by means of shear-joining, and subsequently sintered and calibrated. The alternative embodiment provides that, likewise, the two rotor elements, including their bore-holes, are pressed from sintering powder, subsequently already sintered, however, and then joined by means of a shear-joining (optionally here, sintering core laser-welding), and subsequently calibrated.
It should be noted at this point that the calibration of the sintered part comprises locally repressing sintered surfaces having sintering pores, with the aim of evening out the distortions in the sintering process, thus to increase the dimensional precision and also the surface density, surface hardness, surface quality of the relevant functional surfaces or functional elements, as well as the durability of the component, such that this step can be used here. The repressing can be increased depending on the pore density and pore size in the starting material, the compressing process (shaping in a compression mold or rollers) and the deformation degree of up to 100% of the possible packing density. As a result, the calibrated surfaces are nearly pore-less, and the material density in the surface region is nearly identical to the density of the solid base material (e.g. steel, at ca. 7.8 g/cm3).
The method according to the present disclosure thus connects the first and the second rotor elements by means of an interstice and shear-joint. This interstice and shear joint technology can be used, in particular, for sintered steel, steel, sintered aluminum, aluminum, or plastic parts, such that this type of connection is suitable for use not only for the rotor parts of the camshaft adjuster, but also for other parts, such as those in the stator or in the blade region of the camshaft adjuster. As a result, a rotor can be connected multiple times in a method step with this technology in the base body as well as in the blade region.
In an embodiment of the method according to the present disclosure, the formation of the joinable connecting element is carried out by means of a compression technology or sintering technology, such that a powder column or a sintering core is pressed into and/or sintered in the at least one first bore-hole.
In another embodiment of the method according to the present disclosure, a first free end and a second free end of the joinable connecting element is clamped, optionally by means of a compression device, and then axially sheared off by means of the pressing element. In this manner, a better separation of the joinable connecting element from the bore-hole wall is obtained. In addition, material blow-outs on the sheared surfaces are avoided.
In another optional embodiment of the method according to the present disclosure, the first free end of the joinable connecting element is secured in place, by means of a sintering technology connection or laser-welding seams, to the bore-hole wall of the at least first bore-hole and/or the second free end of the joinable connecting element is secured in place, by means of a sintering technology connection or laser-welding seams, to a bore-hole wall of the at least second bore-hole.
Directly after the assembly, an outer casing of the assembled rotor is calibrated, potentially in the same joining tool, i.e. the pressing element, or in the compression device, in order to close the interstice, seal oil channels, and to obtain the necessary tolerance precision on an axial and/or radial bearing, as well as on other functional surfaces such as locking bore-holes, etc.
One advantage of the present disclosure is that with the method and under the aspect of “the interstice and shear-joint,” both rotor elements are joined to one another through a combination of form-fitting, force-fitting and/or material bonding. The result thereby is a simple and economical hydraulic camshaft adjuster, having an at least two-piece rotor, which also results in there no longer being any leakage of oil during operation (the connecting element is located in bore-holes).
Exemplary embodiments of the present disclosure and the advantages thereof shall be explained in greater detail below, with reference to the attached Figures. The proportions in the figures do not always correspond to the actual proportions, because some shapes are simplified, and other shapes are enlarged for the sake of a better illustration, in relation other elements.
Identical reference symbols are used for identical elements, or elements having the same function. Furthermore, for purposes of clarity, only those reference symbols that are necessary for the description of the respective Figure are depicted in the individual Figures. The depicted embodiments only represent examples of how the hydraulic camshaft adjuster according to the present disclosure, the at least two-piece rotor for a hydraulic camshaft adjuster, and the method according to the present disclosure for producing a rotor for a hydraulic camshaft adjuster, could be designed, and thus do not represent a closed delimiting of the present disclosure.
According to the present disclosure, the first rotor element 4 has four first bore-holes 8, which are aligned with four second bore-holes 10 of the second rotor element 6. A joinable connecting element 12, such as a powder column or a sintering core 12, is located thereby in each first bore-hole 8 and second bore-hole 10, such that the first rotor element 4 is connected to the second rotor element 6 in a form-fitting, force-fitting and/or material bonded manner. As a matter of course, it is also conceivable that the first rotor element 4 is connected to the second rotor element 6 using more or fewer than four connecting elements 12.
In this case, the first rotor element 4 and the second rotor element 6 of the rotor 2 have numerous blades 24, each of which have formed four first bore-holes 8 or four second bore-holes 10, respectively, and in each case, a joinable connecting element 12 extends from the first bore-hole 8 into the second bore-hole 10. It is also conceivable here, however, that the first rotor element 4 is connected to the second rotor element 6 by means of more or fewer than four connecting elements 12 in the blades 24.
In a subsequent step, likewise shown in
Another step, depicted in
Optionally, as shown here in
As shown in
The starting position is shown in
Because the reference symbols depicted in
| Number | Date | Country | Kind |
|---|---|---|---|
| 10 2014 205 237.8 | Mar 2014 | DE | national |
This application is the U.S. National Phase of PCT Appln. No. PCT/DE2015/200080 filed Feb. 16, 2015, which claims priority to DE 10 2014 205 237.8 filed Mar. 20, 2014, the entire disclosures of which are incorporated by reference herein.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/DE2015/200080 | 2/16/2015 | WO | 00 |
