ROTOR FOR A HYDRAULIC CAMSHAFT ADJUSTER AND MANUFACTURING METHOD FOR A ROTOR FOR A CAMSHAFT ADJUSTER

Abstract

A rotor for a hydraulic camshaft adjuster. The rotor includes a first rotor element and a second rotor element. At least one of the rotor elements has oil channels separated from each other by radially arranged elevations. Each elevation of the first rotor element has a first joining profile and the second rotor element forms a complementary-shaped second joining profile corresponding to the position of each first joining profile, wherein the first and the second joining profile engage with each other in the assembled rotor. The first joining profile of the first rotor element has a notch and an elevation and the second joining profile of the second rotor element has a notch and an elevation formed in such a way that prior to the joining of the two rotor elements, a height of the elevation of the second joining profile, which engages in a notch of the first joining profile, is less than a height of the notch of the first joining profile, and a height of the elevation of the first joining profile, which engages in a notch-of the second joining profile, is less than a height of the notch of the second joining profile.

Claims

1-10. (canceled)

11. A rotor for a hydraulic camshaft adjuster, the rotor being rotatably movable around an axis and comprising: a first rotor element; and a second rotor element, at least one of the first and second rotor elements having a plurality of oil channels separated from each other by radially arranged elevations, the first rotor element having a first joining profile having a first notch and a first elevation, and the second rotor element having formed a complementarily shaped second joining profile corresponding to the position of each first joining profile, the second joining profile having a second notch and a second elevation, the first and the second joining profiles engaging with each other when joined when the rotor is assembled, and prior to the joining of the first and second rotor elements, a second elevation height of the second elevation, which engages with the first notch, is less than a first notch height of the first notch, and a first elevation height of the first elevation, which engages with the second notch, is less than a second notch height of the second notch.

12. The rotor as recited in claim 11 wherein a clearance is formed between the first and second elevations and the respective second and first notches prior to the joining of the first and second rotor elements.

13. The rotor as recited in claim 11 wherein each of the first and second notches has a rounded area, and each of the first and second elevations has a flattened area 29.

14. The rotor as recited in claim 11 wherein a base width of the first and second elevations and of the first and second notch of the first and second joining profiles is 0.5 mm to 10.0 mm.

15. The rotor as recited in claim 11 the first and second elevation heights and the first and second notch height are 0.5 mm to 5.0 mm.

16. The rotor as recited in claim 11 wherein the first and second joining profiles are designed in an elastically resilient manner in such a way that the first and second elevations in the respective second and first notches each form an overlap on each lateral edge of the first and second joining profiles in the rotor when assembled, and each clearance in the assembled rotor is at least partially filled with the material from the first and second joining profiles.

17. The rotor as recited in claim 16 wherein the first and second elevations in the second and first notches each have two lateral edges enclosing an acute angle with respect to each other.

18. The rotor as recited in claim 11 wherein the plurality of the oil channels of the first rotor element and the second rotor element run in a radial direction, and are each separated from each other by radially arranged elevations, and each elevation of the first rotor element has formed the first joining profile, and each elevation of the second rotor element has formed the second and complementarily shaped joining profile.

19. The rotor as recited in claim 11 wherein the first joining profile is provided on each first elevation, and the second joining profile is provided on each second elevation of the second rotor element in such a way that the first and second joining profiles each run from an inner area to an outer area of the first and second rotor elements.

20. A manufacturing method for the rotor as recited in claim 11, the method comprising: joining the first rotor element and the second rotor element by their particular contact side in such a way that multiple first joining profiles of the first rotor element and corresponding second joining profiles of the second rotor element engage with each other in such a way that a clearance is formed between each second elevation of the multiple second joining profiles and each first notch of the first joining profiles as well as between each first elevation of the multiple first joining profiles and each second notch of the second joining profiles prior to the assembly of the first and second rotor elements.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Exemplary embodiments of the present invention and their advantages are explained in greater detail below on the basis of the attached figures. The proportions in the figures do not always correspond to the real proportions, since some shapes have been simplified and other shapes have been enlarged in relation to other elements for the purpose of better clarification.

[0021] FIG. 1 shows a top view of a rotor for a hydraulic camshaft adjuster, which is known from the prior art;

[0022] FIG. 2 shows a side view of the rotor from FIG. 1, a vane being represented in the sectional view along line A-A from FIG. 1;

[0023] FIG. 3 shows an enlarged detail of the area marked D in FIG. 2;

[0024] FIG. 4 also shows an enlarged detail of the area marked D in FIG. 2;

[0025] FIG. 5 shows an exploded view of the rotor according to the present invention for a hydraulic camshaft adjuster, including a first and a second rotor element;

[0026] FIG. 6 shows an enlarged perspective view of a contact side of the first rotor element from FIG. 5;

[0027] FIG. 7 shows an enlarged detail of the area marked E in FIG. 6;

[0028] FIG. 8 shows a top view of the rotor according to the present invention for a hydraulic camshaft adjuster;

[0029] FIG. 9 shows a side view of the rotor according to the present invention from FIG. 8, a vane being represented in the sectional view along line B-B from FIG. 8;

[0030] FIG. 10 shows an enlarged detail of the area marked F in FIG. 9; and

[0031] FIG. 11 also shows an enlarged detail of the area marked F in FIG. 9.

DETAILED DESCRIPTION

[0032] Identical reference numerals are used for the same elements or elements having the same function. Furthermore, for the sake of clarity, only reference numerals which are necessary for describing the particular figure are shown in the individual figures. The illustrated specific embodiments represent only examples of how the rotor according to the present invention for a hydraulic camshaft adjuster and the manufacturing method according to the present invention for a rotor for a hydraulic camshaft adjuster may be designed, and they thus do not represent a final limitation of the present invention. The designations of the first rotor element and the second rotor element may be used interchangeably.

[0033] FIG. 1 shows a top view and FIG. 2 a side view of rotor 2, a vane 42 being represented in the sectional view along line A-A from FIG. 1. Rotor 2 is known from the prior art to be suitable for a hydraulic camshaft adjuster (not illustrated). Rotor 2 is rotatably movable around an axis A and includes a first rotor element 4 and a second rotor element 6. At least one of rotor elements 4, 6 also has a plurality of oil channels 10, which are separated from each other by radially arranged elevations 12.

[0034] Each elevation 12 or each contact side 8 of first and second rotor elements 4, 6 includes multiple joining profiles 14, 15, as illustrated in FIGS. 3 and 4 in an enlarged detail of the area marked D in FIG. 2. Each elevation 12 of first rotor element 4 forms a first joining profile 14, and second rotor element 6 forms a complementarily shaped second joining profile 15 corresponding to the position of each first joining profile 14. First and second joining profiles 14, 15 engage with each other in assembled rotor 2 made up of the first and second rotor elements 4, 6. However, it is problematic in this case that an overlap 33 is shared by first and second joining profiles 14, 15, so that both of elastically resilient joining profiles 14, 15 have a rebound effect. This is schematically illustrated, in particular, on the basis of the area marked Z in FIG. 4. Oppositely oriented forces F1, F2, which induce an unnecessary driving apart of first and second rotor elements 4, 6 during operation, occur at first and second joining profiles 14, 15. Oppositely oriented forces F1, F2 thus have a rebound effect.

[0035] FIG. 5 shows an exploded view of rotor 2 according to the present invention for a hydraulic camshaft adjuster, including a first and a second rotor element 4, 6. The structure of oil channels 10 and elevations 12 of first and second rotor elements 4, 6 is similar to the preceding description of FIGS. 1 through 4. Likewise, first joining profiles 14 in this case also engage with complementarily shaped second joining profiles 15 (see FIGS. 10 and 11) in assembled rotor 2 according to the present invention, as illustrated in an enlarged perspective view in FIG. 6 and in an enlarged detail of the area in FIG. 7 marked E in FIG. 6. For example, as also illustrated in FIG. 5, first and second rotor elements 4, 6 are connected to each other via pins 35 and/or with the aid of an oil distribution and centering sleeve 37. Pins 35 also represent an anti-rotation mechanism. However, it is also self-evident that the two rotor elements 4, 6 are also connectable to each other with the aid of other known connecting systems.

[0036] As is also apparent from the specific embodiment in FIGS. 5 and 6, the plurality of oil channels 10 of first rotor element 4 and second rotor element 6 running in a radial direction R1 are each separated from each other by radially arranged elevations 12. Likewise, oil channels 10 may run radially and axially in other specific embodiments, even if this is not illustrated herein. Each elevation 12 of first rotor element 4 forms first joining profile 14, and each elevation 12 of second rotor element 6 forms second and complementarily shaped joining profile 15. In particular, first joining profile 14 is provided on each elevation 12 of first rotor element 4, and second joining profile 15 is provided on each elevation 12 of second rotor element 6 in such a way that first and second joining profiles 14, 15 each run from an inner area 38 to an outer area 40 of first and second rotor elements 4, 6. Likewise, first and second rotor elements 4, 6 include multiple vanes 42, each of which includes elevation 12. In this case as well, the two joining profiles 14, 15 thus run from inner area 38 to outer area 40 on elevations 12 of first rotor element 4 and second rotor element 6.

[0037] FIG. 8 shows a top view and FIG. 9 a side view of rotor 2 according to the present invention, a vane 42 being represented in the sectional view of rotor 2 according to the present invention described above, along line B-B from FIG. 8. The essential advantages of the present invention over the prior art are properly illustrated only in the enlarged details of the area in FIGS. 10 and 11 marked F in FIG. 9, namely that first joining profile 14 of first rotor element 4 has a notch 17 and an elevation 18, and second joining profile 15 of second rotor element 6 has a notch 19 and an elevation 16 in such a way that a height H.sub.6 of elevation 16 of second joining profile 15, which engages with a notch 17 of first joining profile 14, is less than a height H.sub.4 of notch 17 of first joining profile 14, and a height H.sub.14 of elevation 18 of first joining profile 14, which engages with a notch 19 of second joining profile 15, is less than a height H.sub.16 of notch 19 of second joining profile 15.

[0038] With the aid of heights H.sub.6, H.sub.14 of elevations 16, 18 of first and second joining profiles 14, 15, which are less than heights H.sub.4, H.sub.16 of notches 17, 19 of first and second joining profiles 14, 15, a clearance 21 is thus formed between particular elevations 16, 18 and particular notches 17, 19 of first and second rotor elements 4, 6. This clearance 21 formed thereby thus prevents the two rotor elements 4, 6 from being driven apart during operation. As a result, no forces occur which would drive first and second rotor elements 4, 6 apart. As is also illustrated herein, each notch 17, 19 of first and second joining profiles 14, 15 advantageously provides a rounded area 27, each elevation 16, 18 of first and second joining profiles 14, 15 then preferably providing a flattened area 29, so that clearance 21 is formed thereby. Thus, a basic width 23 of elevations 16, 18 and a basic width 25 of notches 17, 19 of first and second joining profiles 14, 15 are preferably 0.5 mm to 2.0 mm.

[0039] It is preferably also provided in the present invention that first and second joining profiles 14, 15 are designed in an elastically resilient manner in such a way that elevations 16, 18 in notches 17, 19 of first and second joining profiles 14, 15 each form an overlap 33 on each lateral edge 31 of first and second joining profiles 14, 15 in assembled rotor 2, and each clearance 21 in an assembled rotor 2 is at least partially filled with the material from first and second joining profiles 14, 15. Overlap 33 on each lateral edge 31 is thus preferably 0.005 mm to 1.0 mm. This means that the two rotor elements 4, 6 have a slight negative allowance (not illustrated) for forming an overlap 33 on each of lateral edges 31 of first and second joining profiles 14, 15, so that edges 31 engage with each other in an elastically resilient manner during the joining of the two rotor elements 4, 6 and thereby create an axial longitudinal interference fit. In particular, clearances 21 described above accommodate material deformations of first and second joining profiles 14, 15 of the two rotor elements 4, 6 from the longitudinal interference fit during operation.

[0040] As is also illustrated herein, elevations 16, 18 in notches 17, 19 of first and second joining profiles 14, 15 each have two lateral edges 31, which enclose an acute angle α with respect to each other. This acute angle α is preferably from 0° to 35°, since this inclination is suitable for better demolding with the aid of the compression mold.

LIST OF REFERENCE NUMERALS

[0041] 2 rotor [0042] 4 first rotor element [0043] 6 second rotor element [0044] 8 contact side [0045] 10 oil channel [0046] 12 elevation [0047] 14 first joining profile [0048] 15 second joining profile [0049] 16 elevation of the second joining profile [0050] 17 notch of the first joining profile [0051] 18 elevation of the first joining profile [0052] 19 notch of the second joining profile [0053] 21 clearance [0054] 23 basic width of the elevation [0055] 25 basic width of the notch [0056] 27 rounded area [0057] 29 flattened area [0058] 31 edge [0059] 33 overlap [0060] 35 pin [0061] 37 oil distribution and centering sleeve [0062] 38 inner area [0063] 40 outer area [0064] 42 vane [0065] A axis [0066] F1 force [0067] F2 force [0068] H.sub.4 height of the notch of the first joining profile [0069] H.sub.6 height of the elevation of the second joining profile [0070] H.sub.14 height of the elevation of the first joining profile [0071] H.sub.16 height of the notch of the second joining profile [0072] R1 radial direction [0073] α angle