WO2012062239A1 - Fliehkraftpendeleinrichtung - Google Patents

Fliehkraftpendeleinrichtung Download PDF

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Publication number
WO2012062239A1
WO2012062239A1 PCT/DE2011/001057 DE2011001057W WO2012062239A1 WO 2012062239 A1 WO2012062239 A1 WO 2012062239A1 DE 2011001057 W DE2011001057 W DE 2011001057W WO 2012062239 A1 WO2012062239 A1 WO 2012062239A1
Authority
WO
WIPO (PCT)
Prior art keywords
axial
pendulum
pendulum mass
rolling element
axial point
Prior art date
Application number
PCT/DE2011/001057
Other languages
German (de)
English (en)
French (fr)
Inventor
Florian Baral
David SCHNÄDELBACH
Original Assignee
Schaeffler Technologies AG & Co. KG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Schaeffler Technologies AG & Co. KG filed Critical Schaeffler Technologies AG & Co. KG
Priority to CN201180040237.7A priority Critical patent/CN103180635B/zh
Priority to DE112011102751.6T priority patent/DE112011102751B4/de
Publication of WO2012062239A1 publication Critical patent/WO2012062239A1/de

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • F16F15/14Suppression 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
    • F16F15/1407Suppression 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
    • F16F15/145Masses mounted with play with respect to driving means thus enabling free movement over a limited range

Definitions

  • the invention relates to a centrifugal pendulum device with the features according to the preamble of claim 1.
  • the torsional vibration damper allows transmission of a torque coming from a drive side, for example, from an internal combustion engine to an output side, such as a transmission and beyond a dusk can tion of torsional vibrations as they can be caused by the internal combustion engine, cause.
  • the torsional vibration damper on a drive part and on the effect of at least one energy storage element with respect to the drive part limited rotatable output part.
  • the torsional vibration damper comprises a centrifugal pendulum device for further damping and / or Ti Igung the torsional vibrations in the drive train.
  • the centrifugal pendulum device comprises a rotatable about an axis of rotation pendulum mass carrier and at least one arranged Pendelmassencru consisting of two axially on both sides of the pendulum mass carrier s opposite Pendelm asses, which are interconnected by means of cutouts in the pendulum mass carrier by cross-fasteners.
  • the pendulum pair is limited relative to the pendulum mass carrier via two rolling elements pivotally limited.
  • the rolling element comprises an outer surface which can be unrolled along an inner surface of a career in the pendulum mass carrier Supremebil Deten career and whereby the rolling element against the pendulum mass carrier limited t is 29enkbar.
  • the inner surface is flat along its axial extent, that is along the axial extent of the inner surface is a first axial point and a second axial point in the rolling surface and the first and second axial point have a same radial distance from the Drehachs e. Under certain circumstances, it can lead to an axial displacement of the rolling element in the career of the pendulum mass carrier.
  • the object of the invention is to improve the leadership of a pendulum mass carrier on a pendulum, in particular to improve the axial guidance. This object is achieved by a centrifugal pendulum device with the features of claim 1.
  • a centrifugal pendulum with m axially arranged on both sides of a rotatable about an axis pendulum mass carrier and a pendulum mass pair forming pendulum masses proposed, the pendulum masses are formed to form the pendulum mass pair with the help of at least one by a cutout in the pendulum mass carrier fastening element together and wherein the pendulum mass pair with the help of at least one with an outer surface along an inner surface of a career formed in the pendulum mass carrier rolling element limited 29enkbar limited to the pendulum mass carrier and wherein at a first circumferential position along the axial extent of the inner surface, a first axial point and a second axial point in the Inner surface is located.
  • the first and the second axial point for forming an axial course of the inner surface are radially spaced from each other, wherein the outer surface of the rolling element on a the inner surface of the raceway axially overlapping portion at least two different and axially spaced-apart diameter.
  • the centrifugal pendulum device is preferably arranged on a torsional vibration damper and / or on a dual-mass flywheel and / or in a hydrodynamic torque converter.
  • the rolling element is advantageously designed as a rolling element or as a roller bearing. Also, the rolling element may be formed as a stepped bolt.
  • the axial course of the outer surface of the Abroiielements is wedge-shaped, convex, triangular or rectangular. Also, a paragraph may be provided in the outer surface.
  • the axial course between the first and second axial point is continuous and / or unsteady.
  • a shoulder, a groove or the like may be incorporated in the inner surface.
  • the axial course of the inner surface L-shaped and / or be formed as a continuous curvature.
  • the inner surface has a third axial point at the first circumferential position along the axial extent of the inner surface. at the third axial point has a radial distance to the second axial point and wherein the second axial point is located axially between the first axial point and the third axial point.
  • the inner surface between the first and third axial point is concave or convex.
  • the axial course may be pointed and / or have a plurality of deflection points and / or be formed wave-shaped. Also, a rectangular course can be provided.
  • the rolling element on a complementary to the axial course of the inner surface formed on the outer surface may be concave and the outer surface may be convex or spherical.
  • the axial course of the inner surface on the circumferential side in sections, that is formed over a portion of the circumference of the inner surface is formed circumferentially along the during operation of the centrifugal pendulum device by the rolling movement of the rolling element on the track ü coated inner surface.
  • the axial course over the entire circumference of the inner surface may be formed.
  • further complementary raceways are formed in the pendulum masses of the pendulum mass pair complementary to the track in the pendulum mass carrier, in which the rolling element is received and unrolled.
  • the rolling element is preferably received and unrolled in the raceways of the pendulum masses with an axially central portion in the raceway of the pendulum mass carrier and mounted on both sides of the central portion axially outer portions.
  • FIG. 1 side view of a centrifugal pendulum device according to the prior art.
  • FIG. 2 Spatial cross-sectional view of a section of the centrifugal pendulum device from FIG. 1.
  • Figure 3 Spatial cross-sectional view of a section of a centrifugal pendulum device in a specific embodiment of the invention.
  • Figure 4 cross section through egg nen section of the centrifugal pendulum device of Figure 3.
  • Figure 5 cross section through egg nen section of a centrifugal pendulum device in a further specific embodiment of the invention.
  • Figure 6 cross section through egg nen section of a centrifugal pendulum device in a further specific embodiment of the invention.
  • a centrifugal pendulum device 10 according to the prior art is shown in side view.
  • the centrifugal pendulum device 10 includes a rotatable around a Drehachs e 100 Pen delmassenvic 12 m it in a radially inner region introduced spring windows 14 for receiving energy storage elements, such as coil springs.
  • the energy storage elements are connected to the pendulum mass carrier 12 and a damper component of a Torsionsschwingungsdäm not shown here pfers in operative connection to allow a rotation of the damper member relative to the pendulum mass carrier 12 cherimplantation under the effect of Energyspei.
  • an output hub 16 is fixed to the pendulum mass carrier 12, in particular riveted, wherein the output hub 16 via a toothing 18 m with a transmission gear effetshaft rotatably connected.
  • pendulum masses 18 Radial outside of the pendulum mass carrier 12 four pendulum masses 18 are arranged with it not shown here axially gege lying on the other Be te of the pendulum mass carrier 12 pendulum masses connected to four pendulum masses si nd.
  • the connection is made with the help of three fasteners 20th per pendulum mass pair, wherein the fastening elements 20 are fixedly connected to the pendulum masses 18 and pass through cutouts 22 in the pendulum mass carrier 12 through n.
  • the cutouts 22 are shaped such that a pivoting of the pendulum masses 18 can be made possible over the pendulum mass carrier 12 along a pendulum track.
  • the cutouts 22 are kidney-shaped.
  • the actual pivotal movement of the pendulum masses 18 relative to the pendulum mass carrier 12 is made possible by rolling elements 24 and correspondingly in the pendulum mass carrier 12 and in the pendulum masses 18 shaped raceways 26, 28.
  • rolling elements 24 for example rolling elements, in particular stepped bolts in the respective raceways 26, 28 are arranged per pendulum mass pair.
  • the La ufbahnen 28 in the P endelmassen 18 of a pendulum mass pair are kom plementär to the track 26 in the pendulum mass carrier 12aded det.
  • the Lau is fbahn 26 in the pendulum mass carrier 12 ni erenförmig and the raceways 28 in the pendulum masses 18 curved in opposite directions.
  • FIG. 2 shows a spatial cross-sectional view of a section of the centrifugal pendulum device 10 from FIG. 1.
  • the roller elements 24 each have an outer surface 30 with which they can be unrolled along an inner surface 32 of the track 26 in the pendulum mass carrier 12.
  • the inner surface 32 is flat along its axial extension with respect to an axial direction 102, that is, along the axial extent of the inner surface 32, a first axial point 34 and a second axial point 36 have an equal radial distance in the inner surface with respect to a radial direction 104 from the axis of rotation 100.
  • FIG. 3 shows a spatial cross-sectional view of a section of a centrifugal pendulum device 10 in a specific embodiment of the invention.
  • the rolling element 24 is preferably formed as a rolling element and in particular as a stepped bolt, the axially central portion 38 which axially overlaps the raceway 26 of the pendulum mass carrier 12 has a larger diameter as the two adjacent axially outer Bereic he 40, 42.
  • the peripheral surfaces 42 of two axially outer portions 40, 42 which sroll in the raceways 28 of the pendulum masses 18 of the pendulum mass pair si nd are cylindrical.
  • the rolling element 24 at a circumferential position of the circumference of the raceway forming inner surface 32 along the axial direction 102 has a first ax ial point 34 and a second axial point 36 wherein the second axial point 36 is axially spaced from the first axial point 34.
  • the first and second axial points 34, 36 are also in relation to each other for forming an axial course of the inner surface 32 the radial direction 104 is radially spaced from the rolling element.
  • the axial course of the inner surface 32 is continuous and curved between the first and second axial points 34, 36.
  • the inner surface 32 at the first and second axial point 34, 36 associated circumferential position along the axial extent of the inner surface 32 has a third axial point 44, wherein the third axial P is 44 a radial distance from the second axial point 36 and in particular has a sliding surfaces radial distance as the first axial point 34.
  • the second axial point 36 lies axially between the first axial point 34 and the third axial point 44.
  • the inner surface 32 is formed concave as a whole between the first and the third axial point 34, 44.
  • the outer surface 30 of the rolling element 24 is formed such that at least one of the inner surface 32 of the race 26 axially overlapping portion 46 at least two different and axially spaced diameter 8, 50 has.
  • a mean diameter 50 is greater than the axial outer diameter 48 and the outer surface 30 is generally spherical and formed as in the concave axial course of the inner surface 32 of the raceway 26 inserting surface.
  • the axial course of the inner surface 32 is circumferentially formed in sections, in particular over a peripheral portion of the inner surface 32 is swept over during operation of the centrifugal pendulum device 10 by the Abrol Iamba of the rolling element 24 on the track 26.
  • FIG. 5 shows a cross section through a section of a centrifugal pendulum device 10 in a further specific embodiment of the invention.
  • Figure 6 shows a cross section through a section of a centrifugal pendulum device 10 in a further specific embodiment of the invention.
  • the axial course of the outer surface 30 of the rolling element 24 and, correspondingly, the shape of the track of the pendulum mass carrier 12 is formed triangularly with a kink 52.
PCT/DE2011/001057 2010-08-19 2011-05-11 Fliehkraftpendeleinrichtung WO2012062239A1 (de)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201180040237.7A CN103180635B (zh) 2010-08-19 2011-05-11 离心力摆装置
DE112011102751.6T DE112011102751B4 (de) 2010-08-19 2011-05-11 Fliehkraftpendeleinrichtung

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102010034808 2010-08-19
DE102010034808.2 2010-08-19

Publications (1)

Publication Number Publication Date
WO2012062239A1 true WO2012062239A1 (de) 2012-05-18

Family

ID=44581858

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE2011/001057 WO2012062239A1 (de) 2010-08-19 2011-05-11 Fliehkraftpendeleinrichtung

Country Status (3)

Country Link
CN (1) CN103180635B (zh)
DE (3) DE202011004695U1 (zh)
WO (1) WO2012062239A1 (zh)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150369334A1 (en) * 2013-02-12 2015-12-24 Schaeffler Technologies AG & Co. KG Centrifugal force pendulum device
WO2018006905A1 (de) * 2016-07-05 2018-01-11 Schaeffler Technologies AG & Co. KG Pendelrolle für fliehkraftpendeleinrichtung

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2991739B1 (fr) * 2012-06-12 2018-01-26 Valeo Embrayages Dispositif d'amortissement pendulaire a element de roulement stabilise
DE112014003716A5 (de) * 2013-08-12 2016-04-28 Schaeffler Technologies AG & Co. KG Fliehkraftpendel
DE102015209871A1 (de) 2014-05-30 2015-12-03 Schaeffler Technologies AG & Co. KG Fliehkraftpendel
DE102015201801B4 (de) * 2015-02-03 2017-07-06 Schaeffler Technologies AG & Co. KG Fliehkraftpendeleinrichtung und Drehschwingungsdämpfer
DE102015215903A1 (de) * 2015-08-20 2017-02-23 Schaeffler Technologies AG & Co. KG Fliehkraftpendel und hydrodynamischer Drehmomentwandler mit Fliehkraftpendel
FR3067080B1 (fr) * 2017-06-06 2020-06-26 Valeo Embrayages Dispositif d'amortissement pendulaire

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006028556A1 (de) 2005-07-11 2007-01-18 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Drehmomentübertragungseinrichtung
EP1780434A2 (de) * 2005-10-29 2007-05-02 LuK Lamellen und Kupplungsbau Beteiligungs KG Kupplungseinrichtung
DE102006028552A1 (de) * 2005-10-29 2007-05-03 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Kupplungseinrichtung
DE102009042825A1 (de) * 2008-10-30 2010-05-12 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Drehmomentübertragungseinrichtung
DE102009042836A1 (de) * 2008-11-24 2010-05-27 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Fliehkraftpendel
DE102010005599A1 (de) * 2009-02-09 2010-08-12 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Fliehkraftpendel

Family Cites Families (3)

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Publication number Priority date Publication date Assignee Title
EP1865222A1 (de) * 2006-06-10 2007-12-12 LuK Lamellen und Kupplungsbau Beteiligungs KG Fliehkraftpendeleinrichtung
DE102009042812A1 (de) * 2008-11-24 2010-05-27 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Torsionsdämpfungseinrichtung
DE102010029464A1 (de) * 2010-05-28 2011-12-01 Zf Friedrichshafen Ag Torsionsschwingungsdämpferanordnung und Schwingungsdämpfereinrichtung, insbesondere in einer Torsionsschwingungsdämpferanordnung

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006028556A1 (de) 2005-07-11 2007-01-18 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Drehmomentübertragungseinrichtung
EP1780434A2 (de) * 2005-10-29 2007-05-02 LuK Lamellen und Kupplungsbau Beteiligungs KG Kupplungseinrichtung
DE102006028552A1 (de) * 2005-10-29 2007-05-03 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Kupplungseinrichtung
DE102009042825A1 (de) * 2008-10-30 2010-05-12 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Drehmomentübertragungseinrichtung
DE102009042836A1 (de) * 2008-11-24 2010-05-27 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Fliehkraftpendel
DE102010005599A1 (de) * 2009-02-09 2010-08-12 Luk Lamellen Und Kupplungsbau Beteiligungs Kg Fliehkraftpendel

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150369334A1 (en) * 2013-02-12 2015-12-24 Schaeffler Technologies AG & Co. KG Centrifugal force pendulum device
WO2018006905A1 (de) * 2016-07-05 2018-01-11 Schaeffler Technologies AG & Co. KG Pendelrolle für fliehkraftpendeleinrichtung

Also Published As

Publication number Publication date
DE112011102751B4 (de) 2019-02-21
DE202011004695U1 (de) 2011-09-26
DE102011101162A1 (de) 2012-02-23
DE112011102751A5 (de) 2013-07-04
CN103180635A (zh) 2013-06-26
CN103180635B (zh) 2015-04-01

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