DEVICE FOR REDUCING TORSIONAL VIBRATIONS IN A DRIVE TRAIN
20210341020 · 2021-11-04
Inventors
- Stefan HERZOG (Coburg, DE)
- Laura RÖDER (Prosselsheim, DE)
- Marcel WINKLER (Rodewisch, DE)
- Miroslav CIZEK (Plzen 3, CZ)
- Jakub SKLENICKA (Plzen 3, CZ)
- Monika Rößner (Donnersdorf, DE)
- Gerald Viernekes (Hassfurt, DE)
- Manfred ZIMMER (Zeil, DE)
Cpc classification
F16D3/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D3/843
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D2200/0004
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F15/121
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F2230/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F15/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F2224/0208
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D2300/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F2236/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F2230/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D2300/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D2300/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D2250/0084
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F2226/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F2232/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F15/1213
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16D3/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D3/84
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An apparatus for damping torsional vibrations in a drivetrain, including a drive device and an output device, which drive device and output device are arranged so as to be rotatable around a common axis, a damping device that connects the drive device and the output device to one another, and a thrust bearing device for axial support of drive device and the output device. The drive device, cover device, and thrust bearing device are arranged such that a partially enclosed spatial region is formed, and at least one damping element of the damping device is arranged in the spatial region. Elements of the drive device, the cover device, the output device and the thrust bearing device are arranged to inhibit liquid entry into the spatial region.
Claims
1-12. (canceled)
13. An apparatus configured to damp torsional vibrations in a drivetrain, comprising: a drive device; an output device, wherein the drive device and the output device are arranged to be rotatable around a common axis; a damping device that connects the drive device and the output device to one another; a thrust bearing device configured to axially support the drive device and the output device; a cover device; a partially enclosed spatial region is formed by an arrangement of the drive device, the cover device, and the thrust bearing device relative to one another; and at least one damping element of the damping device is arranged in the partially enclosed spatial region, wherein elements of the drive device, the cover device, the output device, and the thrust bearing device are arranged relative to one another to inhibit liquid entry, and/or configured to reduce liquid entry into the partially enclosed the partially enclosed spatial region.
14. The apparatus according to claim 13, wherein the damping device comprises at least one damping element configured to be liquid-repellent.
15. The apparatus according to claim 14, wherein the at least one damping element is provided with a liquid-repellent coating and/or an anti-corrosion coating.
16. The apparatus according to claim 13, wherein at least one of the drive device, the output device, the cover device, and the thrust bearing device are acted upon by a liquid-repellent lubricant.
17. The apparatus according to claim 13, wherein at least one element of the drive device, the output device and/or the cover device which outwardly defines the partially enclosed spatial region is at least one of: formed without holes and is provided with at least one hole that is closed.
18. The apparatus according to claim 13, further comprising: a spring device is arranged to provide a predeterminable axial preloading on at least one thrust bearing element of the thrust bearing device so that a determined preloading force on is maintained above a certain value.
19. The apparatus according to claim 18, wherein the spring device is arranged at the cover device.
20. The apparatus according to claim 19, wherein the spring device is arranged between cover device and thrust bearing device such that it outwardly limits the partially enclosed spatial region.
21. The apparatus according to claim 18, wherein the at least one thrust bearing element with which the spring device cooperates is arranged on a radial inner side of the spring device.
22. The apparatus according to claim 13, wherein the thrust bearing device comprises at least one thrust bearing element that has a larger extension in axial direction than an element of the output device adjoining in radial direction, and wherein the at least one thrust bearing element of the thrust bearing device abuts an element of the output device without axial intermediate space.
23. The apparatus according to claim 13, further comprising: a spacer element arranged between an inner side of the drive device and a thrust bearing element, the spacer element is formed such that the spacer element at least partially wraps around the thrust bearing element in radial and axial direction.
24. A method for producing an apparatus for damping torsional vibrations in a drivetrain, comprising: providing a drive device and an output device such that the drive device and the output device are rotatable around a common axis; providing a damping device that connects the drive device and the output device to one another; providing a thrust bearing device for axial support of the drive device and the output device; providing a cover device; arranging the drive device, the output device, the cover device, and the thrust bearing device relative to one another such that a partially enclosed spatial region is formed; and arranging at least one damping element of the damping device in the partially enclosed spatial region, wherein elements of the drive device, the cover device, the output device, and the thrust bearing device are arranged relative to one another to inhibit liquid entry and/or configured to reduce liquid entry into the partially enclosed spatial region.
25. The apparatus according to claim 13, wherein elements of the drive device, the cover device, the output device, and the thrust bearing device are arranged relative to one another to inhibit water entry.
26. The apparatus according to claim 16, wherein the liquid-repellent lubricant is a grease.
27. The apparatus according to claim 26, wherein the liquid is water.
28. The apparatus according to claim 22, wherein the at least one thrust bearing element is a thrust ring.
29. The apparatus according to claim 23, wherein the spacer element is formed as sheet metal.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0038] Preferred constructions and embodiment forms of the invention are shown in the drawings and described more fully in the following description Like reference characters designate like or similar or functionally like component parts or elements.
[0039] The drawings show schematically and in cross section:
[0040]
[0041]
[0042]
[0043]
[0044]
[0045]
[0046]
[0047]
DETAILED DESCRIPTION OF THE PRESENTLY PREFERRED EMBODIMENTS
[0048]
[0049] A torsion damper 1 is shown in detail in
[0050] On the axial side remote of the primary flywheel 2, i.e., a secondary side, a cover plate 7 is arranged at the primary flywheel 2 such that the compression springs 6 substantially in a U-shaped spatial region 100, which is formed by the primary flywheel 2, which is substantially L-shaped in cross section, and the cover device which adjoins the primary flywheel 2 and extends substantially inward in radial direction in the form of a cover plate 7. Further, a spring device extending substantially in radial direction in the form of a plate spring 8 is arranged. On the one hand, the spring device is connected to the cover plate 7 or is supported at the latter and, on the other hand, exerts a preloading force on a supporting ring 9 which is located farther radially inward and arranged on the radial outer side of the hub 3. As an alternative to the plate spring 8, it is also conceivable to correspondingly arrange a sealing plate or the like arranged in particular at the hub 3 so as to be fixed with respect to rotation relative to it. To limit the spatial region 100 radially inward on the primary side, a spacer element in the form of a washer 5, which is axially and radially angled multiple times, is first arranged between the primary flywheel 2 in the region of the hub 3 from left to right in axial direction. A thrust ring 4 is arranged on the radial inner side of the washer 5. The thrust ring 4 has a larger axial extension than the flywheel masses 14 that are connected to the hub 3 and that are arranged radially outwardly of the thrust ring 4 or supporting ring 9 on both sides of the radially outer region 3′ of the hub 3. This minimizes intermediate spaces and accordingly reduces the probability of a possible intrusion of water. The washer 5 is formed in such a way that, on the one hand, it covers the clearance between the primary flywheel 2 and the thrust ring 4 in axial direction and, on the other hand, projects over the thrust ring 4 in axial direction on the radial outer side of the thrust ring 4 such that through-openings toward region 100 are also minimized in this case. The thrust ring 4, washer 5, plate spring 8 and supporting ring 9 are elements of a thrust bearing device of the torsion damper 1.
[0051] On the output side, that is, on the right-hand side of hub 3 referring to
[0052] The compression springs 6 further have a liquid-repellent coating 6a as well as a corrosion-inhibiting coating. Beyond this, a lubricant 20, particularly in the form of a grease which, in particular, is not water-soluble and does not absorb water, is used between at least two of the above-mentioned component parts of the torsion damper.
[0053]
[0054] In contrast to the torsion damper 1 according to
[0055]
[0056] It should also be noted here that the mounting openings 35 depicted in this instance are provided in an output element 45 connected to the hub 3 by riveting, and further mounting openings which are distributed around the rotational axis A are sealed by an individual sealing disk 37. As is shown in
[0057]
[0058]
[0059]
[0060] Steps of a method for producing an apparatus for damping torsional vibrations in a drivetrain are shown in
[0061] The method comprises the following:
[0062] In step S1, a drive device and an output device are provided in such a way that the drive device and output device are rotatable around a common axis.
[0063] In S2, a damping device, which connects the drive device and output device to one another, is provided.
[0064] In S3, a thrust bearing device is provided for axial support of drive device and output device.
[0065] In S4, a cover device is provided.
[0066] In S5, the drive device, the output device, the cover device, and the thrust bearing device are arranged relative to one another such that a partially enclosed spatial region is formed.
[0067] In S6, at least one damping element of the damping device is arranged in the spatial region.
[0068] In S7, elements of the drive the device, the cover device, the output device, and the thrust bearing device are arranged relative to one another so as to inhibit liquid entry, particularly water entry and/or are configured to reduce liquid entry into the spatial region.
[0069] In summary, at least one of the embodiment forms of the invention provides at least one of the following features: [0070] Removal of all, in particular unnecessary, openings, holes or the like in an outer shell of a torsional vibration damper. [0071] Optimization of axial support with respect to geometry and preloading for forming a closed sealing plane. [0072] Water-insoluble or water-repellent lubricant, in particular grease. [0073] Water-repellent coating of component parts, particularly of the damping elements.
[0074] In summary, at least one of the embodiment forms of the invention has at least one of the following advantages: [0075] torsion damper with fording capability [0076] simple production [0077] cost-effective production [0078] longer life [0079] protection against external environmental influences, particularly against an intrusion of liquid, particularly water
[0080] Although the present invention has been described in terms of preferred exemplary embodiments, it is not limited thereto and may be modified in various ways.
[0081] Thus, while there have shown and described and pointed out fundamental novel features of the invention as applied to a preferred embodiment thereof, it will be understood that various omissions and substitutions and changes in the form and details of the devices illustrated, and in their operation, may be made by those skilled in the art without departing from the spirit of the invention. For example, it is expressly intended that all combinations of those elements and/or method steps which perform substantially the same function in substantially the same way to achieve the same results are within the scope of the invention. Moreover, it should be recognized that structures and/or elements and/or method steps shown and/or described in connection with any disclosed form or embodiment of the invention may be incorporated in any other disclosed or described or suggested form or embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.