Crankshaft Arrangement Comprising a Torsional Vibration Damper

Abstract

A crankshaft arrangement for an internal combustion engine includes a crankshaft, a torsional vibration damper having a primary mass and a flywheel, wherein the primary mass is connected fixedly to the crankshaft, and the flywheel and the primary mass are coupled via a viscous fluid. The torsional vibration damper is attached to an output end of the crankshaft. The primary mass is coupled to a secondary coupling via an elastomer coupling ring. The torsional vibration damper is coupled to the secondary coupling via a feedback device. The feedback device has a negative stiffness.

Claims

1-14. (canceled)

15. A crankshaft arrangement for an internal combustion engine, comprising: a crankshaft; a torsional vibration damper with a primary mass and a vibration damper ring, wherein the primary mass is connected fixedly to the crankshaft, and the vibration damper ring and the primary mass are coupled via a viscous fluid, wherein the torsional vibration damper is attached to an output end of the crankshaft; an elastomer coupling ring by which the primary mass is coupled to a secondary coupling; a feedback device by which the torsional vibration damper is coupled to the secondary coupling, wherein the feedback device has a negative rigidity.

16. The crankshaft arrangement as claimed in claim 15, wherein the vibration damper ring of the torsional vibration damper is an outer vibration damper ring, to which the feedback device is coupled.

17. The crankshaft arrangement as claimed in claim 16, wherein the feedback device with the negative rigidity has spring elements.

18. The crankshaft arrangement as claimed in claim 17, wherein the spring elements are attached in a manner which is distributed uniformly on a circumference of an outer ring of the secondary coupling and on an opposite edge of the vibration damper ring of the torsional vibration damper, and extend in a radial direction.

19. The crankshaft arrangement as claimed in claim 17, wherein the spring elements in each case comprise at least one prestressed helical spring.

20. The crankshaft arrangement as claimed in claim 17, wherein the feedback device with the negative rigidity has four or more spring elements.

21. The crankshaft arrangement as claimed in claim 15, wherein the feedback device with the negative rigidity has magnetic elements.

22. The crankshaft arrangement as claimed in claim 21, wherein first magnetic elements are attached in a manner which is distributed uniformly on a circumference of an edge of the vibration damper ring, and second magnetic elements are attached in a manner which is distributed uniformly on a circumference of an outer ring of the secondary coupling.

23. The crankshaft arrangement as claimed in claim 21, wherein the feedback device with the negative rigidity has at least four or more first magnetic elements and at least four or more second magnetic elements.

24. The crankshaft arrangement as claimed in claim 23, wherein an angle between in each case two adjacent first magnetic elements and an angle between in each case two adjacent second magnetic elements about a rotational axis is 90°, and an angle in each case between a first magnetic element and a second magnetic element about the rotational axis is 45°.

25. The crankshaft arrangement as claimed in claim 22, wherein the first magnetic elements point with a north pole toward the rotational axis, and the second magnetic elements point with a north pole toward the rotational axis.

26. The crankshaft arrangement as claimed in claim 21, wherein the magnetic elements are permanent magnets.

27. The crankshaft arrangement as claimed in claim 21, wherein that the magnetic elements are configured as electromagnets.

28. A method for damping torsional vibrations of a crankshaft of a crankshaft arrangement, comprising: in a first method step, providing an apparatus which has a torsional vibration damper comprising a primary mass and an outer vibration damper ring, and comprising a secondary coupling with an elastomer coupling ring, in a second method step, torsional vibration damping taking place by way of coupling of the outer vibration damper ring to the primary mass, further damping being carried out by way of coupling of the primary mass for its part to the secondary coupling, and in a third method step, damping of the torsional vibrations and at a same time isolating a drive train is carried out by way of a negative rigidity which brings about feedback of the secondary coupling to the outer vibration damper ring.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0035] FIG. 1 shows a crankshaft arrangement according to the prior art;

[0036] FIG. 2 shows a section of a further crankshaft arrangement and an apparatus for damping torsional vibrations according to the prior art;

[0037] FIG. 3 shows a section of a crankshaft arrangement according to the invention with one exemplary embodiment of the apparatus according to the invention for damping torsional vibrations;

[0038] FIGS. 4-5 show diagrammatic views of exemplary embodiments of a feedback device with negative rigidities;

[0039] FIGS. 6-7 show graphical representations of torsional vibration curves; and

[0040] FIG. 8 shows a diagrammatic flow chart of a method according to the invention.

DETAILED DESCRIPTION OF THE DRAWINGS

[0041] FIG. 1 shows a crankshaft arrangement according to the prior art.

[0042] FIG. 2 illustrates a section of a further crankshaft arrangement and an apparatus 100′ for damping torsional vibrations according to the prior art.

[0043] The crankshaft arrangement 1 is particularly suitable for a reciprocating piston engine, in particular for an internal combustion engine. A crankshaft 2 with a rotational axis 2a is connected at a drive end 6 to a torsional vibration damper 3. Therefore, the torsional vibration damper 3 is situated at an original position of the flywheel (not shown).

[0044] Since the torsional vibration damper 3 also assumes the task of the reduction of the torsional non-uniformity of the engine, to which the crankshaft 2 is assigned, it requires suitable tuning between a primary mass 4 which is connected fixedly to the crankshaft 2 and a secondary mass 5 which is attached on the primary mass 4 in a seismically, elastically damping manner.

[0045] The suitable tuning brings it about that, at a low rotational speed, that is to say at low frequencies, the connection between the primary mass 4 and the secondary mass 5 can be considered to be rigid. The two masses 4, 5 form, as it were, one unit and act as a flywheel at low rotational speeds. In this situation, torsional vibrations play a subordinate role in an engine. A further flywheel is not necessary in the case of a crankshaft arrangement 1 of this type.

[0046] At a relatively high rotational speed, that is to say at relatively high frequencies, the larger secondary mass 5 comes into play and damps the torsional vibrations. The torsional vibration damper 3 operates in its original form. In this operating state, that is to say at high rotational speeds, the torsional non-uniformity plays a subordinate role.

[0047] The crankshaft arrangement 1 shown in the example shows an outline sketch for a four-cylinder engine. The invention is not to be restricted hereto; it can also be used as a crankshaft arrangement of engines with a lower or higher number of cylinders, in particular with six, eight, ten, twelve or more cylinders or else of V-engines with up to 20 cylinders.

[0048] The torsional vibration damper 3 in FIG. 2 is, for example, a viscosity damper and has the primary mass 4 which is connected fixedly to the crankshaft and the secondary mass 5 which is configured here as a ring which can rotate in a chamber of the primary mass 4, a gap between these two masses being filled with a viscous medium, for example silicone oil. Suitable tuning also brings it about here that, at a low rotational speed, that is to say at low frequencies, the primary mass 4 and the secondary mass 5 can be considered to be one unit.

[0049] A coupling functional section with an elastomer coupling ring 8 is also integrated directly into the torsional vibration damper 3 and forms a secondary coupling 9. The elastomer coupling ring 8 is connected on one side to a hub-like inner ring 7 of the primary mass 4 and on the other side to an outer ring 8 of the secondary coupling 9. The outer ring 8 is coupled via a connecting section 9b to an output 10, for example an input element of a transmission (otherwise not shown) which belongs to a drive train (likewise not shown but contemplated).

[0050] This embodiment is also called a “Flywheel Integrated Damper and Coupling” (FIDC).

[0051] FIG. 3 shows a section of a crankshaft arrangement 1 according to the invention with one exemplary embodiment of the apparatus 100 according to the invention for damping torsional vibrations.

[0052] The apparatus 100 comprises a primary coupling 11 as viscosity torsional vibration damper 3 with a primary mass 4 and a vibration damper ring 12, a secondary coupling 9 with an elastomer coupling ring 8, and a feedback device 13.

[0053] A vibration damper ring 12 is coupled to the primary mass 4. This is shown in FIG. 3 by way of example as a primary coupling 11.

[0054] The primary coupling 11 comprises the primary mass 4 which is connected to the crankshaft 2 and has a damper element 11 a which is disk-shaped here with a circumferential collar, and the vibration damper ring 12 with a chamber 12a, in which the damper element 11a is received with a fluid which is not described in greater detail. The chamber 12a is sealed by means of seals 12b which are not described in greater detail with respect to the shaft of the primary mass 4. This construction has a certain rigidity and damping action.

[0055] In contrast to the vibration damper ring 5 from the prior art as shown in FIG. 2, the vibration damper ring 12 is configured here as an outer vibration damper ring 12. The vibration damper ring 12 additionally has a circumferential edge 12c which points toward the output 10. The edge 12c will be described further below.

[0056] The primary mass 4 for its part is additionally coupled to the secondary coupling 9. This coupling is shown in FIG. 3 by way of example by way of the elastomer coupling ring 8 with its connections on one side to the hub-like inner ring 7 of the primary mass 4 and on the other side to the outer ring 8 of the secondary coupling 9.

[0057] In contrast to the prior art, the vibration damper ring 12 is coupled via a rigidity to the secondary coupling 9. This rigidity is configured here as what is known as a negative rigidity of the feedback device 13. The feedback device 13 connects the edge 12c of the vibration damper ring 12 to the outer ring 9a of the secondary coupling 9.

[0058] The feedback device 13 forms an additional coupling of the components which are already present in the case of the FIDC (see FIG. 2), and leads to it being possible for the isolation of the drive train to be improved decisively. This additional coupling is the coupling of the vibration damper ring 12 (the absorber mass) to the secondary side of the secondary coupling 9, that is to say to the outer ring 9a. It is decisive here that this additional coupling has to have a negative rigidity, in order that the desired behavior is configured. Mechanical components with a negative rigidity individually behave in an unstable manner, and the stability of the overall system is achieved by way of the further couplings which are already present.

[0059] The coupling of the vibration damper ring 12 to the secondary coupling 9 by means of a negative rigidity can take place via various technical approaches, for example via correspondingly arranged magnets or via prestressed springs or via an active system with a positive feedback booster.

[0060] FIG. 4 shows a diagrammatic view of a first exemplary embodiment of the feedback device 13 with a negative rigidity with spring elements 14.

[0061] FIG. 5 illustrates a diagrammatic view of a second exemplary embodiment of the feedback device 13 with a negative rigidity with magnetic elements 15, 16.

[0062] In this first exemplary embodiment, the feedback device 13 has four spring elements 14-1, 14-2, 14-3 and 14-4 which are attached in a uniformly distributed manner on the circumference of the outer ring 9a of the secondary coupling 9 and on the opposite edge 12c of the vibration damper ring 12, and extend in the radial direction. Here, an angle between in each case two adjacent spring elements 14-1, 14-2, 14-3, 14-4 about the rotational axis 2a is 90°.

[0063] Each spring element 14-1, 14-2, 14-3, 14-4 consists here of at least one prestressed helical spring. More than four spring elements 14 can of course also be used.

[0064] In the second exemplary embodiment of the feedback device 13, four first magnetic elements 15-1, 15-2, 15-3, 15-4 are attached uniformly on the circumference of the edge 12c of the vibration damper ring 12 in such a way that their respective north pole (denoted here by “+”) points toward the rotational axis 2a. Here, an angle between in each case two adjacent first magnetic elements 15-1, 15-2, 15-3, 15-4 about the rotational axis 2a is 90°.

[0065] In addition, four second magnetic elements 16-1, 16-2, 16-3, 16-4 are attached on the circumference of the outer ring 9a of the secondary coupling 9, in a uniform manner on the circumference of the outer ring 9a of the secondary coupling 9. Here, an angle between in each case two adjacent second magnetic elements 16-1, 16-2, 16-3, 16-4 about the rotational axis 2a is 90°, an angle between in each case a first magnetic element 15-1, 15-2, 15-3, 15-4 and a second magnetic element 16-1, 16-2, 16-3, 16-4 about the rotational axis 2a having a value of 45°.

[0066] The second magnetic elements 16-1, 16-2, 16-3, 16-4 are arranged in such a way that their south pole (denoted here by “−”) points radially to the outside away from the rotational axis 2a, or their north pole points toward the rotational axis 2a.

[0067] Here, the magnetic elements 15-1, 15-2, 15-3, 15-4 and 16-1, 16-2, 16-3, 16-4 are arranged in such a way that the annular region between the outer ring 9a of the secondary coupling 9 and that inner side of the edge 12c which points toward the rotational axis 2a remains free.

[0068] Here, the magnetic elements 15-1, 15-2, 15-3, 15-4 and 16-1, 16-2, 16-3, 16-4 are configured as permanent magnets. It is also contemplated, however, that they can be configured as electromagnets. In this case, open-loop control of the feedback device 13 which is formed in this way is contemplated. Closed-loop control is also contemplated in a manner which is dependent on different parameters, for example rotational speed, engine load, etc. In this way, the above-indicated active system can be realized with a positive feedback booster.

[0069] More than four magnetic elements 15, 16 can also be used in each case.

[0070] FIG. 6 shows a graphical representation of a torsional vibration curve 20′ with a torsional vibration damper 3 of the apparatus 100′ from the prior art.

[0071] FIG. 7 shows a graphical representation of a torsional vibration curve 20 with the apparatus 100 according to the invention.

[0072] Tests have resulted in the torsional vibration curves 20′, 20 in FIGS. 6 and 7.

[0073] The torsional vibration curve 20′ is plotted with its amplitude A against a rotational speed n. At a rotational speed n of approximately 1050 1/min, an amplitude maximum which lies approximately in the middle of a range 21′ between 900 and 1200 1/min at an amplitude value of approximately A=0.2 is shown in the prior art.

[0074] A reduction of torsional non-uniformities by approximately 75% can be possible by means of the apparatus 100 according to the invention. This is shown clearly by the torsional vibration curve 20 in FIG. 7. The amplitude A lies in the range 21 substantially below the amplitude maximum which occurs in the range 21′ in FIG. 6. In addition, extreme amplitude maxima are no longer to be registered, and the amplitude A remains constantly below a value A=0.05 and runs without exceeding this value.

[0075] FIG. 8 shows a diagrammatic flow chart of a method according to the invention for damping torsional vibrations of a crankshaft 2.

[0076] In a first method step S1, an apparatus 100 is provided which has a torsional vibration damper 3 with a primary coupling 11 with a primary mass 4 and a vibration damper ring 12, and a secondary coupling 9 with an elastomer coupling ring 8.

[0077] A second method step S2 provides that torsional vibration damping takes place by means of a coupling of the vibration damper ring 12 to the primary mass 4, further damping being carried out by means of a coupling of the primary mass 4 to the secondary coupling 9.

[0078] Finally, in a third method step S3, damping of the torsional vibrations and simultaneous isolating of a drive train take place by means of a negative rigidity which brings about feedback of the secondary coupling 9 to the vibration damper ring 12.

[0079] In this way, the torsional non-uniformities or torsional vibrations can be reduced considerably, and there is improved isolation of the drive train. In addition, lower loading of the components of the drive train can be achieved, such as, for example, lower transmission wear. In the case of a generator, the “cleanness” of a sine wave of the generated alternating current can be increased, that is to say frequency stability and amplitude stability can be improved.

[0080] The invention is not restricted by way of the above-specified exemplary embodiment, but rather can be modified within the scope of the claims.

[0081] It is contemplated that the feedback device 13 has a combination of spring elements 14 and magnetic elements 15, 16.

[0082] The magnetic elements 15, 16 can also be combined as permanent magnets and electromagnets.

LIST OF DESIGNATIONS

[0083] 1 Crankshaft arrangement [0084] 2 Crankshaft [0085] 2a Rotational axis [0086] 3 Torsional vibration damper [0087] 4 Primary mass [0088] 5 Secondary mass [0089] 6 Drive end, crankshaft [0090] 7 Inner ring [0091] 8 Elastomer coupling ring [0092] 9 Secondary coupling [0093] 9a Outer ring [0094] 9b Connecting section [0095] 10 Output [0096] 11 Primary coupling [0097] 11a Damper element [0098] 12 Vibration damper ring [0099] 12a Chamber [0100] 12b Sealing element [0101] 12c Edge [0102] 13 Feedback device [0103] 14-1; 14-2; 14-3; 14-4 Spring element [0104] 15-1; 15-2; 15-3; 15-4 First magnetic element [0105] 16-1; 16-2; 16-3; 16-4 Second magnetic element [0106] 17, 18, 19 Characteristic curve [0107] 20, 20′ Torsional vibration curve [0108] 21, 21′ Range [0109] 0100, 100′ Apparatus [0110] A Amplitude [0111] F Force [0112] S1; S2; S3 Method step [0113] x Displacement