WO2012062276A1 - Fliehkraftpendel - Google Patents
Fliehkraftpendel Download PDFInfo
- Publication number
- WO2012062276A1 WO2012062276A1 PCT/DE2011/001908 DE2011001908W WO2012062276A1 WO 2012062276 A1 WO2012062276 A1 WO 2012062276A1 DE 2011001908 W DE2011001908 W DE 2011001908W WO 2012062276 A1 WO2012062276 A1 WO 2012062276A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- pendulum
- cutout
- mass
- absorber
- absorber mass
- Prior art date
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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2121—Flywheel, motion smoothing-type
- Y10T74/2128—Damping using swinging masses, e.g., pendulum type, etc.
Definitions
- the invention relates to a centrifugal pendulum, in particular a centrifugal pendulum for damping torsional vibrations of a buoyancy strand, for example, a buoyancy strand of vehicles with an internal combustion engine.
- a speed-adaptive vibration damper for a shaft rotating about an axis.
- an inertial mass of the vibration absorber performs a purely translational movement relative to a hub part. This is achieved by a so-called parallel bifilar suspension storage.
- each point associated with the inertial mass performs an identical motion along the trajectory B passing through the respective point P.
- speed-adaptive centrifugal pendulum for a shaft rotatable about an axis, comprising: a pendulum flange on which at least two axially opposing absorber masses connected to one another via a spacer are arranged, the absorber masses and / or the pendulum flange of the centrifugal pendulum having at least one cutout, in which the spacer element and thus the absorber mass is guided, wherein the cutout is formed from a neutral position by a deviating from a circle or a circle segment curve, by increasing the radius of the cutout in a range from the neutral position and a radius reduction of the cutout in the other range from the neutral position, wherein the neutral position is the position in which the spacer element of the absorber mass at a swing angle! of the centrifugal pendulum of 0 ° touches the cutout.
- the radius of the outer contour and / or inner contour of the eruption is increased in at least one section and / or reduced in at least one section formed, wherein the radius of the outer contour and / or inner contour increases in particular at one or both ends of the cutout or reduced in size.
- the outer contour and the inner contour of the cutout can have the same course or contour or a different contour.
- the radius of the outer contour and / or inner contour of the cutout is formed enlarged and / or reduced from a neutral position or point in at least one section.
- the cutout is designed in such a way that a translatory and a rotational movement can be carried out with the absorber mass, the at least one cutout in particular having a non-symmetrical course or trajectory.
- the absorber mass does not follow a symmetrical trajectory, but a non-symmetrical trajectory, as described below, for example. is shown in Figs. 2 and 4.
- Fig. 1 is a schematic representation of the principle of a centrifugal pendulum according to the invention
- Fig. 2 shows a first embodiment of the centrifugal pendulum according to the invention
- Fig. 3 is a sectional view AA of the centrifugal pendulum of FIG. 1; 4 shows a second embodiment of the centrifugal pendulum according to the invention. 5 shows a sectional view AA of the centrifugal pendulum pendulum according to FIG. 4;
- Fig. 6 shows a roll neck of a pendulum flange of the centrifugal pendulum according to the invention, as shown in Fig. 4, and
- FIG. 7 shows an associated rolling cut-out of an absorber mass of the centrifugal pendulum pendulum according to the invention according to FIG. 4.
- the basic principle of a centrifugal pendulum pendulum is based on the fact that an absorber mass pair is linked as a pendulum to a pendulum flange. Since the absorber mass pair is located in the centrifugal force field, its natural frequency increases in proportion to the speed. An interpretation of the pendulum geometry makes it possible to keep the natural frequency of the pendulum always the same engine speed order.
- Tilgeraku is used.
- FIG. 1 shows a schematic representation of the principle of a centrifugal pendulum 10 according to the invention.
- the invention relates to a Fiiehkraftpendel for damping torsional vibrations of a buoyancy strand, in particular a buoyancy strand in a vehicle, such. a vehicle with an internal combustion engine.
- the invention is not limited to this application.
- a centrifugal pendulum 10 is provided, the Tilger glovessverlauf is structurally adjustable depending on a swing angle.
- the centrifugal pendulum 10 at the same time the advantages of a Tra ezaniser, ie the space can be optimally used.
- the centrifugal pendulum 10 has a pendulum flange 12 and a plurality of absorber masses 14 arranged in pairs.
- the pendulum length, the pendulum distance and the angle of rotation of the absorber masses are dependent on the oscillation angle, whereby influencing the Tilgerowski (constant or variable) is possible.
- a twist angle of the absorber mass 14 is provided.
- any desired track shape 18 for the mass center of gravity can be achieved with a corresponding rotation of the absorber mass pair and thus the desired erosion course.
- the absorber mass 14 will perform superimposed translational and rotational movements, ie the absorber mass 14 will move with its center of gravity along a path 18 and at the same time rotate about its own center of gravity.
- the movements of the absorber mass 14 can be achieved by the trajectories of two points 20, 22 of the absorber mass 14 whose position (x u , yu; XRI, y TM) is determined by the geometry quantities H and B.
- H is the distance of the first or second point 20, 22 of the absorber mass 14 of the vibrating center 24, here the axis of rotation of the pendulum disc or the pendulum flange 12 (in Fig. 1 center of the disc).
- B is the distance between the two points 20, 22 from each other.
- the points 20, 22 in FIG. 1 each have the same distance to the central axis 26, which runs through the oscillation center 24, or in other words, the two points 20, 22 are symmetrical to the central axis 26 30 of the point 20 or 22 is not symmetrical or does not run symmetrically.
- the absorber mass 14 performs superimposed translational and rotational movements.
- the cutouts or roll cutouts in a damping mass 14 and / or a pendulum flange 12 trace the non-symmetrical course of the movement path. This also applies to the cutouts or roll cutouts shown in FIG. 4.
- the mass torsion ß depends on the oscillation angle ⁇ :
- This special case provides a constant order of death.
- FIG. 2 shows a detail of a centrifugal pendulum pendulum 10 according to a first embodiment of the invention. As shown in Fig. 2, a pendulum flange 12 is shown, on which at least one or more pairs of absorber masses 14 are arranged.
- a damping mass 14 is arranged on the pendulum flange 12.
- the movements of the damping mass 14 can be achieved by the movement paths 28, 30 of two points 20, 22 of the absorber mass 14 whose position is determined by the geometry quantities H and B.
- the trajectories 28, 30 corresponding cutouts or rolling cutouts 32 are now formed in the pendulum flange 12.
- a respective absorber mass 14 is arranged on opposite sides of the pendulum flange 12.
- the two absorber masses 14 are suspended by means of two pins 34 and bearings 36 mounted thereon in rolling cutouts of the pendulum flange.
- a pin 34 and its bearing 36 thereby form a spacer element for suspending and guiding the absorber mass 14 in the respective cutout 32.
- the bearings 36 have the advantage that they essentially cause rolling friction instead of sliding friction.
- the provision of the bearings 36 is an optional feature.
- the pins 34 connect the two absorber masses to a Tilgermassencru. As described above, the cutouts 32 or recesses on the pendulum flange 12 have the shape or shape of the movement frame.
- NEN 28, 30 for two points 20, 22 of the absorber mass 14, as previously described with reference to FIG. 1.
- the course of the movement path 18 of the center of mass of the absorber mass 14 is also shown in FIG. 1, as well as the central axis 26, through which the oscillation center 24 extends.
- the spacer or here a combination of pin and bearing preferably has a smaller diameter than the width of the respective cutout 32 in which it is received, as this could otherwise lead to undesirable friction.
- Fig. 3 is a section A-A through the centrifugal pendulum 10 shown in FIG. 2.
- a respective absorber mass 14 is provided on both sides of the pendulum flange 12 or the pendulum disk.
- the pendulum flange 12 has two cutouts 32, which have the shape of the movement paths 28, 30 for two points 20, 22 of the absorber mass 14 or follow their course.
- a pin 34 is received in the respective cutout 32 and has a bearing 36.
- the bearing 36 may be, for example, a rolling bearing, a roller bearing or a plain bearing, to name three examples.
- the pins 34 are each connected to an absorber mass 14 on both sides.
- FIG. 4 shows a section of a centrifugal pendulum pendulum 10 according to a second embodiment.
- a pendulum flange 12 is shown, on which at least one or more pairs of absorber masses 4 are arranged.
- the absorber masses 14 are suspended in cutouts 32 or recesses on the respective absorber mass 14 and the pendulum flange 12 by means of rollers 38 as spacers.
- the spacers or rollers 38 preferably have a smaller diameter than the width of the respective cutout 32 in which they are received.
- a cutout 32 of the absorber mass 14 is assigned a cutout 32 of the pendulum flange 12, wherein both cutouts 32 are arranged above one another. As shown in FIG. 4, the respective cutout 32 on the pendulum flange 12 and the associated cutout 32 on the absorber mass 14 are arranged relative to one another such that the respective roller 38, which is guided in the two cutouts 32, the respective cutout 32 of the Pendulum 12 and the absorber mass 14 in a neutral position or position 33, ie at a
- FIG. 4 there is likewise an absorber mass 14 on both sides of the pendulum flange 12, wherein in FIG. 4 the absorber mass 14 is shown on the front side of the pendulum flange 12.
- the absorber mass with its two cutouts on the back of the pendulum flange 12 is arranged corresponding to the absorber mass 12 and their cutouts on the front.
- centrifugal pendulum or the vibration damper assembly 10 with adjustable Tilgerord- ubensverlauf can be realized both with simple roles and, for example, with step rollers.
- the cutouts or rolling cutouts 32 on the respective absorber mass 14 and the pendulum flange 12 are formed by curves deviating from a circle segment or a circular shape.
- the rolling cutouts 32 on the mass 14 and the pendulum flange 12 are formed, for example, from the neutral position or from the neutral position 33, by radius increases and radius reductions R m & or Rs & by a curve deviating from a circle or circle segment, as in the following 6 and 7 is shown.
- an area 40 or a side of the cutout 32 of the pendulum flange 12 or the absorber mass 14 from the neutral position 33 formed by a radius reduction of a curve deviating from a circle or circle segment and in the other area 39 or on the other side of the Section 32 of the pendulum flange 12 and the absorber mass 14 from the neutral position 33, formed by an increase in radius of a deviating from a circle or circle segment curve.
- the side contour is, for example, a straight line portion which is parallel to the pitch axis ⁇ and at a distance c, as shown in Fig. 4, where, for example, c is 0.
- FIGS. 6 and 7 show an exemplary embodiment of a cutout 32 or roll cutout 32 for a damping mass 14 and a pendulum flange 12. More specifically, Fig. 6 shows the respective cutout 32 of the pendulum flange of the centrifugal pendulum in Fig. 4 and Fig. 7, the respective associated cutout 32 of the absorber mass of the centrifugal pendulum in Fig. 4. As previously described, the sliding on the pairs of rollers To minimize or avoid roll cuttings 32 are formed by curves deviating from a circle.
- a radius reduction or radius enlargement is meant, for example, a linear increase or decrease of the radius with the distance from the neutral position.
- another behavior can be selected, with which the radius becomes larger or smaller with the distance from the neutral position.
- the cutouts 32 of the pendulum flange 12 can be arranged in mirror image to each other.
- the two cutouts 32 of the pendulum flange can be arranged in mirror image to the center axis 26 by the swing center 24. Accordingly, the two cutouts 32 of the respective absorber mass 14 can be arranged in mirror image to each other, ie mirror image of the central axis 26 through the swing center 24th
- the radius or external radius R S of the rolling cutout 32 is increased, here by an amount R s t, so that R S + R 1 - on the other Side or in the other area 40 is reduced from the neutral position 33 of the radius or here outer radius R s of the rolling cutout 32, thereby by an amount S AI, so that applies R s - R S ⁇ 1 .
- the inner radius R si of the rolling cutout 32 is enlarged by the same amount as the outer radius R s from a neutral position 33 in one area 39 and in the other area 40 from the neutral position 33 the outer radius R s by the same amount (in Fig. 6 - R s ) reduced.
- the respective roller cutout 32 on the pendulum flange 12 and the associated roller cutout 32 on the absorber mass 14 are arranged relative to one another in such a way that the roller 38, which is guided in the two roller cutouts 32, the respective rolling cutout of the pendulum flange or 6 and 7) .
- the regions 40 of the rolling cutouts 32 of the pendulum flange 12 and the absorber mass 14 are their radius R s or R m in this region hen 40 from the neutral position or position 33 is reduced, opposite each other.
- a Schwingungstilgeran extract or a centrifugal pendulum can, for example. preferably characterized by at least one of the following:
- the swing length is variable or constant depending on swing angle
- the distance of the vibration center is variable or constant depending on swing angle
- the angle of rotation of the absorber mass is variable or constant depending on swing angle
- the desired Tilger alssverlauf corresponds to a particular track shape of the center of gravity with a certain twist course of the absorber mass;
- the track shape and the rotation of the center of mass is achieved by tracks of, for example, two points of the absorber mass;
- the absorber masses are e.g. by means of two pins and bearings mounted thereon in the roller cut-outs e.g. suspended the pendulum disk or the pendulum, wherein the cutouts in the pendulum disc or in the pendulum have the shape or the course of the web shapes of the two points of the absorber mass.
- the absorber masses are e.g. suspended by means of rollers in the rolling cutouts of the pendulum disc or of the pendulum flange, for example by means of two rollers;
- the cutouts or roll cutouts are e.g. formed by a respective deviating from a circle or circle segments curves.
- the respective cutout or roll cutout is in each case not symmetrical or runs along a non-symmetrical path or trajectory.
- centrifugal pendulum or a vibrator damping device or arrangement in which the desired absorber order curve is achieved by a specific path shape and a rotation profile of the center of mass, and this in turn by the variation of geometry variables over the oscillation angle.
- the present embodiments as described above with reference to FIGS. 1 to 7, can also be combined with each other, in particular individual features thereof.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2013538064A JP5916745B2 (ja) | 2010-11-08 | 2011-10-28 | 遠心振り子 |
DE112011103700.7T DE112011103700B4 (de) | 2010-11-08 | 2011-10-28 | Fliehkraftpendel |
US13/888,717 US20130239746A1 (en) | 2010-11-08 | 2013-05-07 | Centrifugal pendulum |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102010050715.6 | 2010-11-08 | ||
DE102010050715 | 2010-11-08 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/888,717 Continuation US20130239746A1 (en) | 2010-11-08 | 2013-05-07 | Centrifugal pendulum |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2012062276A1 true WO2012062276A1 (de) | 2012-05-18 |
Family
ID=45463131
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DE2011/001908 WO2012062276A1 (de) | 2010-11-08 | 2011-10-28 | Fliehkraftpendel |
Country Status (4)
Country | Link |
---|---|
US (1) | US20130239746A1 (de) |
JP (1) | JP5916745B2 (de) |
DE (2) | DE102011085400A1 (de) |
WO (1) | WO2012062276A1 (de) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2652355B1 (de) | 2010-12-15 | 2016-11-09 | Schaeffler Technologies AG & Co. KG | Fliehkraftpendel und kupplungsscheibe mit demselben |
CN106326561A (zh) * | 2016-08-25 | 2017-01-11 | 同济大学 | 一种新型外旋轮线型离心摆吸振器设计方法 |
FR3077858A1 (fr) * | 2018-02-14 | 2019-08-16 | Valeo Embrayages | Dispositif d'amortissement pendulaire |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104471278B (zh) * | 2012-07-12 | 2016-04-20 | 舍弗勒技术股份两合公司 | 转速适配式减振器和带有该减振器的扭转振动减振器 |
FR3014519B1 (fr) * | 2013-12-09 | 2016-10-07 | Valeo Embrayages | Dispositif d'amortissement de torsion a pendule d'efficacite de filtration amelioree |
DE112015000246T9 (de) * | 2014-01-17 | 2016-12-01 | Aisin Aw Co., Ltd. | Zentrifugalpendelartige schwingungsabsorbierende Vorrichtung und Ordnungsfestlegungsverfahren für dieselbe |
DE102015201504A1 (de) * | 2014-02-12 | 2015-08-13 | Schaeffler Technologies AG & Co. KG | Fliehkraftpendel und Drehmomentübertragungseinrichtung mit solch einem Fliehkraftpendel |
JP6237414B2 (ja) * | 2014-03-31 | 2017-11-29 | アイシン・エィ・ダブリュ株式会社 | 遠心振子式吸振装置 |
DE102014214534A1 (de) * | 2014-07-24 | 2016-01-28 | Schaeffler Technologies AG & Co. KG | Fliehkraftpendel und Antriebssystem mit Fliehkraftpendel |
WO2016026494A1 (de) * | 2014-08-22 | 2016-02-25 | Schaeffler Technologies AG & Co. KG | Fliehkraftpendel und antriebssystem mit solch einem fliehkraftpendel |
KR101708035B1 (ko) * | 2015-04-21 | 2017-02-17 | 한국파워트레인 주식회사 | 평 베어링 진자를 이용한 차량용 토크 컨버터의 진동 저감 장치 |
FR3037114B1 (fr) * | 2015-06-02 | 2017-06-02 | Valeo Embrayages | Dispositif d'amortissement d'oscillations de torsion |
FR3038682B1 (fr) * | 2015-07-06 | 2017-07-28 | Valeo Embrayages | Dispositif d'amortissement d'oscillations de torsion |
FR3038953B1 (fr) * | 2015-07-17 | 2018-03-02 | Valeo Embrayages | Dispositif d'amortissement d'oscillations de torsion |
DE102015220419A1 (de) * | 2015-10-20 | 2017-04-20 | Zf Friedrichshafen Ag | Tilgersystem mit Führungsbahnen und Verfahren zur Auslegung von Führungsbahnen an einem Tilgersystem |
JP2017129271A (ja) * | 2016-01-14 | 2017-07-27 | 日本精工株式会社 | 遠心振り子ダンパ及びトルク伝達装置 |
DE102016206500A1 (de) | 2016-04-18 | 2017-10-19 | Zf Friedrichshafen Ag | Tilgersystem |
FR3052520B1 (fr) * | 2016-06-08 | 2019-05-10 | Valeo Embrayages | Procede de realisation d'un dispositif d'amortissement pendulaire |
FR3052835B1 (fr) * | 2016-06-16 | 2018-06-08 | Valeo Embrayages | Dispositif d'amortissement pendulaire |
JP6733506B2 (ja) * | 2016-11-07 | 2020-08-05 | トヨタ自動車株式会社 | 捩り振動低減装置 |
FR3059749B1 (fr) * | 2016-12-06 | 2020-02-21 | Valeo Embrayages | Dispositif d'amortissement pendulaire |
JP2019100523A (ja) * | 2017-12-07 | 2019-06-24 | アイシン精機株式会社 | ダンパ装置 |
JP7087947B2 (ja) * | 2018-11-20 | 2022-06-21 | 株式会社アイシン | 振動減衰装置およびその設計方法 |
FR3094769B1 (fr) * | 2019-04-03 | 2021-04-02 | Valeo Embrayages | Dispositif d’amortissement pendulaire |
JP2021060052A (ja) * | 2019-10-03 | 2021-04-15 | 日本精工株式会社 | 遠心振り子ダンパ |
DE102019215909A1 (de) * | 2019-10-16 | 2021-04-22 | Zf Friedrichshafen Ag | Tilgersystem |
DE102021129063A1 (de) | 2021-11-09 | 2023-05-11 | Schaeffler Technologies AG & Co. KG | Fliehkraftpendel |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2318169A (en) * | 1996-06-12 | 1998-04-15 | Mannesmann Sachs Ag | Torsional vibration damper |
DE19752667A1 (de) * | 1997-11-27 | 1999-06-02 | Mannesmann Sachs Ag | Drehschwingungsdämpfer |
DE19831160A1 (de) | 1998-07-11 | 2000-01-13 | Freudenberg Carl Fa | Drehzahladaptiver Schwingungstilger |
DE102009035909A1 (de) * | 2008-08-21 | 2010-02-25 | Luk Lamellen Und Kupplungsbau Beteiligungs Kg | Drehschwingungstilger |
DE102010005599A1 (de) * | 2009-02-09 | 2010-08-12 | Luk Lamellen Und Kupplungsbau Beteiligungs Kg | Fliehkraftpendel |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2272189A (en) * | 1939-06-29 | 1942-02-10 | Ranger Engineering Corp | Dynamic damper for engines |
US2332072A (en) * | 1942-08-06 | 1943-10-19 | Fairchild Engine & Airplane | Vibration damping device |
JPH01312245A (ja) * | 1988-06-13 | 1989-12-18 | Nissan Motor Co Ltd | 定次数形ダイナミックダンパ |
DE19604160C1 (de) * | 1996-02-06 | 1997-05-28 | Freudenberg Carl Fa | Drehzahladaptiver Tilger |
JP4797176B2 (ja) * | 2001-06-12 | 2011-10-19 | シェフラー テクノロジーズ ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト | トルク伝達装置 |
DE10238194A1 (de) * | 2002-08-21 | 2004-03-04 | Carl Freudenberg Kg | Drehzahladaptiver Schwingungstilger |
WO2008098536A2 (de) * | 2007-02-12 | 2008-08-21 | Luk Lamellen Und Kupplungsbau Beteiligungs Kg | Fliehkraftpendeleinrichtung |
DE102008059297B4 (de) * | 2007-12-10 | 2019-07-25 | Schaeffler Technologies AG & Co. KG | Kupplungseinrichtung |
JP5602832B2 (ja) * | 2009-04-14 | 2014-10-08 | シェフラー テクノロジーズ アクチエンゲゼルシャフト ウント コンパニー コマンディートゲゼルシャフト | 遠心力振り子 |
DE102011016568B4 (de) * | 2010-04-29 | 2019-02-21 | Schaeffler Technologies AG & Co. KG | Fliehkraftpendel |
WO2012095072A1 (de) * | 2010-12-24 | 2012-07-19 | Schaeffler Technologies AG & Co. KG | Fliehkraftpendeleinrichtung |
-
2011
- 2011-10-28 WO PCT/DE2011/001908 patent/WO2012062276A1/de active Application Filing
- 2011-10-28 DE DE102011085400A patent/DE102011085400A1/de not_active Withdrawn
- 2011-10-28 DE DE112011103700.7T patent/DE112011103700B4/de active Active
- 2011-10-28 JP JP2013538064A patent/JP5916745B2/ja active Active
-
2013
- 2013-05-07 US US13/888,717 patent/US20130239746A1/en not_active Abandoned
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2318169A (en) * | 1996-06-12 | 1998-04-15 | Mannesmann Sachs Ag | Torsional vibration damper |
DE19752667A1 (de) * | 1997-11-27 | 1999-06-02 | Mannesmann Sachs Ag | Drehschwingungsdämpfer |
DE19831160A1 (de) | 1998-07-11 | 2000-01-13 | Freudenberg Carl Fa | Drehzahladaptiver Schwingungstilger |
DE102009035909A1 (de) * | 2008-08-21 | 2010-02-25 | Luk Lamellen Und Kupplungsbau Beteiligungs Kg | Drehschwingungstilger |
DE102010005599A1 (de) * | 2009-02-09 | 2010-08-12 | Luk Lamellen Und Kupplungsbau Beteiligungs Kg | Fliehkraftpendel |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2652355B1 (de) | 2010-12-15 | 2016-11-09 | Schaeffler Technologies AG & Co. KG | Fliehkraftpendel und kupplungsscheibe mit demselben |
CN106326561A (zh) * | 2016-08-25 | 2017-01-11 | 同济大学 | 一种新型外旋轮线型离心摆吸振器设计方法 |
FR3077858A1 (fr) * | 2018-02-14 | 2019-08-16 | Valeo Embrayages | Dispositif d'amortissement pendulaire |
Also Published As
Publication number | Publication date |
---|---|
JP5916745B2 (ja) | 2016-05-11 |
DE102011085400A1 (de) | 2012-05-10 |
JP2013542387A (ja) | 2013-11-21 |
DE112011103700B4 (de) | 2020-10-15 |
US20130239746A1 (en) | 2013-09-19 |
DE112011103700A5 (de) | 2013-08-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2012062276A1 (de) | Fliehkraftpendel | |
DE112011100859B4 (de) | Torsionsschwingungsdämpfer | |
DE102014210489B4 (de) | Fliehkraftpendel | |
EP2976547B1 (de) | Tilgerschwingungsdämpfer | |
DE102013109583B4 (de) | Zentrallager-Buchseneinheit für eine Antriebswelle | |
DE102010054254A1 (de) | Fliehkraftpendeleinrichtung | |
DE102013213373A1 (de) | Tilgerschwingungsdämpfer | |
DE112013006159T5 (de) | Dämpfungsvorrichtung vom Typ Pendeloszillator | |
DE102019106343A1 (de) | Fliehkraftpendeleinrichtung mit einer an einen Randabschnitt herangeführten Kulissenbahn und Verfahren zur Herstellung einer Fliehkraftpendeleinrichtung | |
DE102014218268B4 (de) | Asymmetrische Fliehkraftpendeleinrichtung | |
DE112015001362T5 (de) | Dämpfungsvorrichtung für einen Antriebsstrang eines Fahrzeugs | |
WO2016015725A1 (de) | Fliehkraftpendel | |
DE10325116A1 (de) | Gleichlaufdrehgelenk | |
DE112016002681T5 (de) | Dämpfervorrichtung | |
DE102020206724B4 (de) | Semiaktive stabilisatorvorrichtung | |
DE10331391B4 (de) | Schwungrad | |
EP3475595B1 (de) | Fliehkraftpendeleinrichtung | |
DE102014214534A1 (de) | Fliehkraftpendel und Antriebssystem mit Fliehkraftpendel | |
DE102014217007A1 (de) | Drehschwingungsdämpfer | |
DE102016215145A1 (de) | Fliehkraftpendel | |
DE102019100359A1 (de) | Ringtilgereinrichtung | |
DE102014214539A1 (de) | Pendelflansch und Fliehkraftpendel mit solch einem Pendelflansch | |
DE102019110796A1 (de) | Wälzlagerkäfig und Verfahren zur Herstellung eines Wälzlagerkäfigs | |
DE102014208777A1 (de) | Fliehkraftpendeleinrichtung | |
WO2018171829A1 (de) | Fliehkraftpendeleinrichtung |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 11805384 Country of ref document: EP Kind code of ref document: A1 |
|
ENP | Entry into the national phase |
Ref document number: 2013538064 Country of ref document: JP Kind code of ref document: A |
|
WWE | Wipo information: entry into national phase |
Ref document number: 1120111037007 Country of ref document: DE Ref document number: 112011103700 Country of ref document: DE |
|
REG | Reference to national code |
Ref country code: DE Ref legal event code: R225 Ref document number: 112011103700 Country of ref document: DE Effective date: 20130808 |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 11805384 Country of ref document: EP Kind code of ref document: A1 |