GB2354055A - Speed-adaptive vibration damper - Google Patents
Speed-adaptive vibration damper Download PDFInfo
- Publication number
- GB2354055A GB2354055A GB0025338A GB0025338A GB2354055A GB 2354055 A GB2354055 A GB 2354055A GB 0025338 A GB0025338 A GB 0025338A GB 0025338 A GB0025338 A GB 0025338A GB 2354055 A GB2354055 A GB 2354055A
- Authority
- GB
- United Kingdom
- Prior art keywords
- speed
- vibration damper
- pin
- curved
- adaptive vibration
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
- F16F15/14—Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers
- F16F15/1407—Suppression of vibrations in rotating systems by making use of members moving with the system using masses freely rotating with the system, i.e. uninvolved in transmitting driveline torque, e.g. rotative dynamic dampers the rotation being limited with respect to the driving means
- F16F15/145—Masses mounted with play with respect to driving means thus enabling free movement over a limited range
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Abstract
A speed-adaptive vibration damper for a shaft rotatable about an axis (15) comprises a hub part (17), on which a number of inertia masses (19) adjacent in the peripheral direction are in each case mounted in two holders (21), which are adjacent in the peripheral direction and which comprise pins (1) which can roll on curved tracks (27, 29), curved in opposite directions, of the inertia masses (19) and the hub part (17) in such a way that, when torsional vibrations superimposed on a rotational movement are initiated, the distance of the inertia masses (19) from the axis (15) is reduced in the course of curved paths of movement. The curved tracks (27, 29) are lubricated with a traction fluid.
Description
2354055 Speed-adaptive vibration damper The invention relates to a
speed-adaptive vibration damper for a shaft rotatable about an axis, comprising a hub part, on which a number of inertia masses adjacent in the peripheral direction are in each case mounted in two holders, which are adjacent in the peripheral direction and which comprise pins which can roll on curved tracks, curved in opposite directions, of the inertia-mass elements and the hub part in such a way that, when torsional vibrations superimposed on a rotational movement are initiated, the distance of the inertia-mass elements from the axis is reduced in the course of curved paths of movement.
DE 196 31 989 Cl discloses such a speed-adaptive vibration damper.
On shafts of machines working in a periodic manner, for example on the crankshaft of an internal combustion engine, torsional vibrations superimposed on the rotational movement occur, and the frequency of these torsional vibrations varies with the speed of the shaft. Vibration dampers may be provided in order to reduce these torsional vibrations. These vibration dampers are designated as speed adaptive if they can dampen torsional vibrations over a larger speed range, ideally over the entire speed range of the machine.
The principle underlying the torsional-vibration dampers is that the inertia masses,, due to centrifugal force, attempt to revolve around the axis at the greatest possible distance when a rotary movement is initiated.
Torsional vibrations which are superimposed on the rotary movement lead to a relative movement of the inertia-mass elements inwards in the radial direction, which leads to a vibration-damping effect. The vibration damper has a natural frequency proportional to the speed, so that torsional vibrations which have frequencies which are proportional to the speed can be damped over a large speed range. A disadvantage of the known speed-adaptive vibration damper, however, is that the desired long service life is not reached on account of wear on the rolling combination of pin/curved tracks.
one aim of the invention is to develop a known 5 speed-adaptive damper in such a way that an especially long service life and operational reliability can be achieved.
The present invention provides a speed-adaptive vibration damper according to claim 1.
The pins can roll on rolling tracks which are lubricated with a traction fluid. The use of traction fluids is known in friction drives. By the use of such a lubricant in a vibration damper, the service life of the vibration damper is increased in a surprising manner. on the one hand, it provides for sufficient lubrication of the rolling combination of pin/curved track, yet sliding of the pin on the curved tracks is reliably avoided.
A further improvement is achieved owing to the fact that the viscosity of the traction fluid increases sharply under pressure. As a result, a coefficient of friction which ensures that the pin performs a rolling movement is achieved at the rolling combination of pin/curved track, where a high pressure prevails during operation.
It has proved to be especially advantageous if the traction fluid contains a synthetic oil of the cycloaliphatic hydrocarbon type.
An especially advantageous refinement of the invention may also be achieved by the pins being provided with first auxiliary means, which can be brought into engagement with appropriately shaped second auxiliary means of the curved tracks in order to prevent peripheral slip and/or axially directed relative displacements. The interengaging auxiliary means ensure that the pin performs a rotary movement.
The first and second auxiliary means may be formed by the interengaging of the projections and grooves. These may be designed, for example, as a tooth system between pin and curved tracks.
An especially advantageous refinement is achieved by the projections contacting the grooves in the region of conical surfaces.
A distinctly longer service life and operational reliability of the speedadaptive vibration damper are achieved by a design in which the pins each have a shell, which encloses a cavity, whichis empty or is filled with a material having a density which is lower than that of the shell. During relative movement of the inertia mass with respect to the hub part, the pin rolls on the curved tracks of hub part and inertia mass. The applied pressure on the rolling combination of pin/curved track is essentially determined by the speed of the rotating shaft. Due to the design according to the invention, the pin is able to follow the relative movement of inertia mass and hub mass more easily, so that a situation in which the pin performs a sliding movement, instead of a rolling movement, relative to the curved tracks is avoided. A surprising advantage is that this design makes it possible to use lubricants between pin and curved tracks in order to further increase the service life, which lubricants reduce the coefficient of friction at the rolling combination of pin/curved tracks. Such a low coefficient of friction in principle increases the risk of the pin sliding, since the tangential force at the contact points of pin/curved tracks is reduced by the use of the lubricant. However, this can be compensated for in an advantageous manner by the present invention.
The durability of the speed-adaptive vibration damper is further increased if the shell is enclosed by a wear-resistant coating.
30. The manufacture of the pin is simplified in particular if the shell of the pin is formed by a tube.
In a further advantageous refinement, provision is made for stiffening ribs projecting into the cavity to be provided. The stability of the pin, with a low pin weight at the same time ', is increased by these stiffening ribs.
In a development of this idea, provision may be made for the stiffening ribs to extend parallel to the longitudinal direction of the pin. Such a pin can be manufactured in an especially simple and cost-effective manner.
On the other hand, especially high stability is achieved by the stiffening ribs extending transversely to 5 the longitudinal direction of the pin.
In particular, the manufacture is further simplified if the stiffening ribs form a component of at least one stiffening element fitted into the cavity. In this refinement, a further increase in the stability of the pin can be achieved by the stiffening element being arranged under prestress in the cavity of the pin, so that the stiffening element exerts a force directed radially outwards on the shell of the pin.
In an advantageous refinement, provision is made for the stiffening element to be formed by at least one ring or a helix.
Especially high stability, with low pin weight at the same time, is also achieved by the ring or the helix, in at least one section, having a rectangular profile arranged transversely to the longitudinal direction of the pin.
The resistance of the pin to pressure loading is further improved if the material in the cavity is essentially non-deformable. Suitable materials are, in particular, epoxy resin, a sintered body of metal, expanded aluminium, phenolic resin, porcelain and industrial ceramics. Compared with the shell, which may be made of high-strength steel, for example, these materials have a low density and, due to their high dimensional stability, increase the strength of the pin. Materials having similar coefficients of thermal expansion are preferably used, so that stresses in the pin which are induced by temperature fluctuations are reduced.
Embodiments of the invention will now be described in more detail, by way of example only, with reference to the accompanying drawings, in which:
Fig. 1-i's a plan view of a pin which may be used with the present invention, Fig. 2 is a longitudinal section through the pin shown in Fig. 1, Fig. 3 is a plan view of a further embodiment of a pin which may be used with the invention, Fig. 4 is a longitudinal section through a further 5 embodiment of a pin which may be used with the invention, Fig. 5 is a front view of a speed-adaptive vibration damper, Fig. 6 is a cross section through the speed-adaptive vibration damper shown in Fig. 5, and Fig. 7 is a cross section through a pin which may be used with the invention in a further embodiment.
Shown in Figures 1 and 2 is a pin 1 having a shell 3, which encloses a cavity 5.
The shell 3 is a tube made of high-strength steel and having a circular cross section. The interior of the tubular shell 3, which is open on both sides, defines the cavity 5.
Placed in the cavity 5 is a material 7 which has a lower density than the shell 3. The material 7 used in the cavity 5 is an essentially non-deformable material. According to the invention, in particular epoxy resin, a sintered body of metal, expanded aluminium, phenolic resin, porcelain and industrial ceramics are suitable. The shell 3 of the pin 1 can be supported in the radial direction of the pin 1 by these materials, as a result of which the stability of the pin 1 can be increased. At the same time, the weight of the pin 1 is reduced owing to the fact that the material 7 has a lower density than the shell 3.
The pin 1 filled with the incompressible material 7 can be produced by the material 7, for example epoxy resin, being poured into the cavity 5. However, it is also possible to shrink the tubular shell 3 of the pin 1 onto a prepared piece of material, for example made of porcelain or ceramic. In this way, a prestress, which has a positive effect on the service life of the pin 1, can be produced in the pin 1.
A wdar-resistant coating 9 is provided on the outside of the shell 3. Wear on the pin 1 can be reduced to a minimum by this coating 9. The coating may comprise for - 6 example, a hardness layer.
In the embodiment of a pin 1 shown in Figure 3, stiffening ribs 110, which project into the cavity 5, are provided on the inside of the tubular shell 3. The stiffening ribs 1 increase the loading capacity of the pin 1 under compression and bending stress. The stiffening pins 11 extend parallel to the longitudinal direction of the pin 1 over its entire length. However, the stiffening ribs 11 may also be oriented transversely to the longitudinal direction of the pin 1.
In the semilateral longitudinal section through a pin I shown in Figure 4, the shell 3 is likewise of tubular design. A number of stiffening ribs 13, which increase the loading capacity of the shell 3 in the radial direction, are fitted in the cavity 5. Like the cavity 5, the stiffening ribs 13 have a circular cross section and are of pot-shaped design. The stiffening elements 13 are held in the cavity 5 by virtue of the fact that they bear against the shell 3 in an elastically deformed manner. However, they may also be designed as a ring or as a helix. Such a ring or helix, in at least one section, advantageously has a rectangular profile arranged transversely to the longitudinal direction of the pin 1.
Figure 5 shows a speed-adaptive vibration damper for a shaft (not shown) rotatable about an axis 15, the vibration damper having a hub part 17 and a number of inertia masses 19 adjacent in the peripheral direction. For each inertia mass 19, the hub part 17 has in each case two holders 21, adjacent in the peripheral direction, in order to mount the inertia masses 19 on the hub part 17.
Each holder 21 is formed by a recess 23 in the hub part 17 and a pin 1 accommodated therein. In this case, the pin 1, whose longitudinal axis runs parallel to the axis 15 of the hub part 17, extends into a recess 25, formed as an aperture, in the inertia mass 19.
The hub part 17-has a curved track 27 defining the recess 23, and the inertia-mass element 19 has a curved track 29 defining the recess 25. The curved tracks 27, 29 and the pin 1 are designed and arranged in such a way that the inertia masses 19 can move relative to the hub part 17 while performing a pendulum motion. In the process, the pins 1 roll on the curved tracks 27, 29, which are curved in opposite directions. In this case, the curved track 27 in the hub part 17 points in the direction of the axis 15, whereas the curved track 29 in the inertia mass 19 points outwards away from the axis 15.
When a torsional vibration superimposed on a rotational movement of the shaft occurs, the inertia masses 19 are moved out of their centre position shown in Figure 5 relative to the hub part 17 along a curved path of movement, which is determined by the curved tracks 27, 29 and the pin 1. In this way, the distance of the centre of gravity of the inertia masses 19 from the axis 15 is reduced. The forces exerted in the process on the hub part 17 by the inertia masses 19 via the curved tracks 27, 29 dampen the vibrations. This vibration damping is optimal if the exciting frequency at a given speed corresponds to the natural frequency of the damper. In this case, the natural frequency of the damper changes in proportion to the speed of the shaft.
In addition, the inertia masses 19 have guide tracks 31 opposite the curved tracks 29 in the recess 25, so that the recess 25 is given the shape of a U, which is directed away from the axis 15. Corresponding guide tracks 33 opposite the curved tracks 27 are also formed in the holder 21 of the hub part 17 (cf. Fig. 6).
The curved tracks 27, 29 and the guide tracks 31, 33 form components of insert parts 41, 43, which are captively accommodated in the hub part 17 and the inertia masses 19 respectively. The insert parts 41, 43 may also be inserted loosely to begin with and, by subsequent shaping of the layer 45, 47 carrying the guide tracks 31, 33, may be adhesively bonded to the hub part 17 and the inertia masses 19 respectively.
The cross section along the axis 15 shown in Figure 6 illustrates the arrangement and mounting of the inertia masses 19 on the hub part 17. In the embodiment shown in Figure 6, the inertia masses 19 are arranged in an axially adjacent position in pairs on both sides in the hub part. However, it is also possible to arrange the inertia masses 19 in such a way that the hub part 17 axially encloses the inertia masses 19 on both sides.
The outer hub part 17 forming the holders 21 is enclosed by caps 35 sealed off from the hub part 17, so that a chamber 37 is obtained.
A lubricant is accommodated in the chamber 37. This lubricant passes in particular through the passages 39 formed in the inertia masses 19 to the pins 1 and the curved tracks 27 and 29, on which the pin 1 rolls. Only a small amount of lubricant is contained in the chamber 37 in order not to hinder the pendulum movement of the inertia masses 19 relative to the hub part 17 to such an extent that the vibration-damping effect would be considerably impaired as a result.
The lubricant used for the curved tracks 27, 29 is a traction fluid, the viscosity of which increases sharply under pressure. This ensures that the pin performs no sliding movement, which leads to premature wear, on the curved tracks. The traction fluid used may be a synthetic oil of the cyclo-aliphatic hydrocarbon type. The service life of the speed-adaptive vibration damper is considerably increased by this use, according to the invention, of the lubricant.
Figure 7 schematically shows a further embodiment of a pin 1 according to the invention with a detail of the curved track 29. The pin 1 is provided with first auxiliary means 49, which can be brought into engagement with appropriately shaped second auxiliary means 51 of the curved tracks 27, 29 in order to prevent peripheral slip and/or axially directed relative displacements. The first and second auxiliary means 49, 51 are designed as interengaging projections'- and grooves. These may be designed, for example, as an interengaging tooth system of curved tracks 27, 29 and pin 1, this tooth system being shown by chain-dotted lines in Figure 7. In this case, the pins I and the curved tracks 27, 29 may be designed in such a way that the projections contact the grooves in the region of conical surfaces.
--1
Claims (7)
1. A speed-adaptive vibration damper for a shaft rotatable about an axis, comprising a hub part, on which a number of inertia masses adjacent in the peripheral direction are in each case mounted in two holders, which are adjacent in the peripheral direction and which comprise pins which can roll on curved tracks, curved in opposite directions, of the inertia masse and the hub part in such a way that, when torsional vibrations superimposed on a rotational movement are initiated, the distance of the inertia masses from the axis is reduced in the course of curved paths of movement, wherein the pins can roll on curved tracks which are lubricated with a traction fluid.
2. A speed-adaptive vibration damper according to claim 1, wherein the viscosity of the traction fluid increases sharply under pressure.
3. A speed-adaptive vibration damper according to claim 1 or 2, wherein the traction fluid contains a synthetic oil of the cyclo-aliphatic hydrocarbon type.
4. A speed-adaptive vibration damper according to claim 1, 2 or 3, wherein the pins are provided with first auxiliary means, which can be brought into engagement with appropriately shaped second auxiliary means of the curved tracks in order to prevent peripheral slip and/or axially directed relative displacements.
5. A speed-adaptive vibration damper according to claim 4, wherein the first and second auxiliary means are formed by interengaging projections and grooves.
6. A speed-adaptive vibration damper according to claim 5, wherein the projections contact the grooves in the region of conical surfaces.
7. A speed-adaptive vibration damper substantially as described herein with reference to Figures 5 and 6 of the accompanying drawings.
111
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1998131153 DE19831153A1 (en) | 1998-07-11 | 1998-07-11 | Speed adaptive vibration damper for a rotating shaft |
GB9916043A GB2339460B (en) | 1998-07-11 | 1999-07-08 | Speed-adaptive vibration damper |
Publications (3)
Publication Number | Publication Date |
---|---|
GB0025338D0 GB0025338D0 (en) | 2000-11-29 |
GB2354055A true GB2354055A (en) | 2001-03-14 |
GB2354055B GB2354055B (en) | 2001-08-08 |
Family
ID=26047365
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0025338A Expired - Fee Related GB2354055B (en) | 1998-07-11 | 1999-07-08 | Speed-adaptive vibration damper |
Country Status (1)
Country | Link |
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GB (1) | GB2354055B (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2413614A (en) * | 2004-05-01 | 2005-11-02 | Safe Developments Ltd | A flywheel with pendulum masses tracking an order of vibration across engine speeds |
WO2013057441A1 (en) * | 2011-10-19 | 2013-04-25 | Valeo Embrayages | Pendulum-oscillator-type damping system comprising an improved guiding device |
WO2014012835A1 (en) * | 2012-07-20 | 2014-01-23 | Valeo Embrayages | Damping system of pendular oscillator type comprising an inbuilt guidance device |
CN104813063A (en) * | 2012-11-26 | 2015-07-29 | 本田技研工业株式会社 | Centrifugal pendulum damping device |
EP2916033A4 (en) * | 2012-11-01 | 2016-07-13 | Toyota Motor Co Ltd | Torsional vibration damping device |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1023912A (en) * | 1963-03-06 | 1966-03-30 | Jarmuefejlesztesi Intezet | A device acting with silicone oil for damping torsional vibrations,principally for motors |
-
1999
- 1999-07-08 GB GB0025338A patent/GB2354055B/en not_active Expired - Fee Related
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1023912A (en) * | 1963-03-06 | 1966-03-30 | Jarmuefejlesztesi Intezet | A device acting with silicone oil for damping torsional vibrations,principally for motors |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2413614A (en) * | 2004-05-01 | 2005-11-02 | Safe Developments Ltd | A flywheel with pendulum masses tracking an order of vibration across engine speeds |
CN103890447B (en) * | 2011-10-19 | 2016-07-06 | Valeo离合器公司 | Shock mitigation system including the pendulum-type oscillator type of modified form guider |
WO2013057441A1 (en) * | 2011-10-19 | 2013-04-25 | Valeo Embrayages | Pendulum-oscillator-type damping system comprising an improved guiding device |
FR2981715A1 (en) * | 2011-10-19 | 2013-04-26 | Valeo Embrayages | PENDULUM OSCILLATOR TYPE DAMPING SYSTEM WITH IMPROVED GUIDE DEVICE |
US9551397B2 (en) | 2011-10-19 | 2017-01-24 | Valeo Embrayages | Pendulum-oscillator-type damping system comprising an improved guiding device |
CN103890447A (en) * | 2011-10-19 | 2014-06-25 | Valeo离合器公司 | Pendulum-oscillator-type damping system comprising an improved guiding device |
CN103890448A (en) * | 2011-10-19 | 2014-06-25 | Valeo离合器公司 | Pendulum-oscillator-type damping system comprising an improved guiding device |
US9506525B2 (en) | 2011-10-19 | 2016-11-29 | Valeo Embrayages | Pendulum-oscillator-type damping system comprising an improved guiding device |
CN103890448B (en) * | 2011-10-19 | 2016-02-10 | Valeo离合器公司 | Comprise the shock mitigation system of the pendulum-type oscillator type of improved type guiding device |
FR2993625A1 (en) * | 2012-07-20 | 2014-01-24 | Valeo Embrayages | PENDULUM OSCILLATOR TYPE DAMPING SYSTEM WITH INTEGRATED GUIDE DEVICE |
WO2014012835A1 (en) * | 2012-07-20 | 2014-01-23 | Valeo Embrayages | Damping system of pendular oscillator type comprising an inbuilt guidance device |
EP2916033A4 (en) * | 2012-11-01 | 2016-07-13 | Toyota Motor Co Ltd | Torsional vibration damping device |
US9435397B2 (en) | 2012-11-01 | 2016-09-06 | Toyota Jidosha Kabushiki Kaisha | Torsional vibration damping device |
US9404555B2 (en) | 2012-11-26 | 2016-08-02 | Honda Motor Co., Ltd. | Centrifugal pendulum damping device |
CN104813063B (en) * | 2012-11-26 | 2016-08-17 | 本田技研工业株式会社 | Centrifugal vibrator type vibration absorber |
CN104813063A (en) * | 2012-11-26 | 2015-07-29 | 本田技研工业株式会社 | Centrifugal pendulum damping device |
Also Published As
Publication number | Publication date |
---|---|
GB2354055B (en) | 2001-08-08 |
GB0025338D0 (en) | 2000-11-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20030708 |