WO2008019641A1 - Drehschwingungsdämpfer - Google Patents

Drehschwingungsdämpfer Download PDF

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Publication number
WO2008019641A1
WO2008019641A1 PCT/DE2007/001242 DE2007001242W WO2008019641A1 WO 2008019641 A1 WO2008019641 A1 WO 2008019641A1 DE 2007001242 W DE2007001242 W DE 2007001242W WO 2008019641 A1 WO2008019641 A1 WO 2008019641A1
Authority
WO
WIPO (PCT)
Prior art keywords
vibration damper
torsional vibration
parts
damper according
spring
Prior art date
Application number
PCT/DE2007/001242
Other languages
German (de)
English (en)
French (fr)
Inventor
Steffen Lehmann
Uwe Weller
Original Assignee
Luk Lamellen Und Kupplungsbau Beteiligungs 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=38626252&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=WO2008019641(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Luk Lamellen Und Kupplungsbau Beteiligungs Kg filed Critical Luk Lamellen Und Kupplungsbau Beteiligungs Kg
Priority to CN200780030049XA priority Critical patent/CN101501362B/zh
Priority to DE112007001663.9T priority patent/DE112007001663B4/de
Priority to BRPI0715128-4A priority patent/BRPI0715128B1/pt
Publication of WO2008019641A1 publication Critical patent/WO2008019641A1/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
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/121Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon using springs as elastic members, e.g. metallic springs
    • F16F15/123Wound springs
    • F16F15/1232Wound springs characterised by the spring mounting
    • F16F15/12346Set of springs, e.g. springs within springs
    • 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
    • F16F15/12Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon
    • F16F15/121Suppression of vibrations in rotating systems by making use of members moving with the system using elastic members or friction-damping members, e.g. between a rotating shaft and a gyratory mass mounted thereon using springs as elastic members, e.g. metallic springs
    • F16F15/123Wound springs
    • F16F15/12313Wound springs characterised by the dimension or shape of spring-containing windows

Definitions

  • the invention relates to a torsional vibration damper with two side parts which are rotatably connected to each other and between which two intermediate parts are arranged, which are rotatable relative to the side members against the spring action of spring means limited, which are arranged within windows, both in the side panels and in the intermediate parts are recessed.
  • the object of the invention is to improve a torsional vibration damper according to the preamble of claim 1, in particular with regard to wear.
  • the object is in a torsional vibration damper with two side parts which are rotatably connected to each other and between which two intermediate parts are arranged, which are rotatable relative to the side members against the spring action of spring means limited, which are arranged within windows, both in the side panels and are recessed in the intermediate parts, achieved in that the windows with the intermediate parts in the circumferential direction on one side each have a guide nose and on the other side in each case a recess in which a guide lug of the respective other intermediate part is arranged.
  • the guide lugs unfold their guiding effect only in one load direction, that is to say under tensile or shear loading.
  • the recesses allow a simple way a movement of the intermediate parts with the guide lugs relative to each other.
  • a preferred embodiment of the torsional vibration damper is characterized in that in each case a spacer pin, which is fixedly connected to the side parts, extends through the recesses of the window.
  • the spacer bolts serve to arrange the side parts in the axial direction at a defined distance from each other. About the standoffs torque is transmitted from the side parts depending on the load direction on one of the intermediate parts.
  • the spacer bolts form a stop for each intermediate part in the circumferential direction.
  • the shape of the recesses is adapted to the shape of the spacer bolts.
  • the intermediate parts each comprise a hub flange which is coupled to a hub.
  • the hub is non-rotatably connected to a transmission input shaft.
  • a further preferred embodiment of the torsional vibration damper is characterized in that the hub is provided with an external toothing, which cooperates with an internal toothing of the intermediate parts. This allows the transmission of torque from the intermediate parts to the hub.
  • a further preferred embodiment of the torsional vibration damper is characterized in that between the outer toothing of the hub and the internal teeth of the intermediate parts in the circumferential direction a defined game is present.
  • the hub is rotatably connected with its outer teeth with one or the other intermediate part.
  • a further preferred embodiment of the torsional vibration damper is characterized in that the guide projections each extend from a plane in which the associated intermediate part expands in the direction of a longitudinal axis of the associated spring device.
  • a further preferred exemplary embodiment of the torsional vibration damper is characterized in that the spring devices each comprise at least one helical spring element with two ends, in each of which one of the guide lugs engages.
  • the coil spring element can also be encompassed externally by a guide element.
  • a further preferred embodiment of the torsional vibration damper is characterized in that the spring means each comprise an outer and an inner helical spring element with two ends, in each of which one of the guide lugs engages. The outer coil spring element is guided over the inner coil spring element by the guide lugs.
  • a further preferred embodiment of the torsional vibration damper is characterized in that the guide lugs are integrally connected to the associated intermediate part.
  • the intermediate part is preferably a sheet metal part from which the guide lugs are stamped out.
  • Figure 1 is a half of a torsional vibration damper according to the invention in the
  • Figure 2 shows the torsional vibration damper of Figure 1 in section
  • Figure 3 is an enlarged detail of Figure 2;
  • FIG. 4 shows the representation of a section through an intermediate component plane of the torsional vibration damper from FIGS. 1 to 3;
  • FIG. 5 shows the illustration of a section through a helical spring plane of the torsional vibration damper from FIGS. 1 to 4;
  • Figure 6 is a schematic representation of the torsional vibration damper from the
  • Figure 7 is an exploded view of the torsional vibration damper of Figures 1 to 6;
  • Figure 8 is a perspective view of an intermediate part of the torsional vibration damper of Figures 1 to 7;
  • Figure 9 shows the intermediate part of Figure 8 in section and Figure 10 shows the intermediate part of Figure 8 in plan view.
  • FIGS. 1 to 7 show a torsional vibration damper 1 in various views and sections.
  • the torsional vibration damper 1 comprises a hub 4, which is provided with an internal toothing 5.
  • the internal toothing 5 serves to non-rotatably connect the hub 4 to a transmission input shaft (not shown) of a transmission of a motor vehicle.
  • the hub 4 is provided with external teeth 6, by which the hub 4 with two intermediate parts 11, 12 rotatably connected.
  • the intermediate parts 11, 12 extend in the radial direction in the manner of a flange and are therefore also referred to as hub flanges.
  • the terms radial, axial and in the circumferential direction in the context of the present invention refer to a rotational axis 13 of the torsional vibration damper 1.
  • bearing means 14, 15 are two side parts 21, 22 relative to the intermediate parts 11, 12 against the spring action of spring means 24, 25, 26 limited rotatable.
  • the twist angle is limited by standoffs 28 which are secured to the side members 21, 22 and extend through the intermediate members 11, 12.
  • the spacer bolts 28 are designed as stepped bolts and riveted to the side parts 21, 22.
  • the intermediate parts 11, 12 are arranged in the axial direction between the side parts 21, 22.
  • a clutch disc 30 with two friction lining halves 31, 32 is attached radially on the outside.
  • the spring means 24 comprises an outer coil spring 34 and an inner coil spring 35. .
  • the intermediate part 11 has an internal toothing 39, in which the external toothing 6 of the hub 4 engages.
  • a defined game 40 is provided in the circumferential direction between the internal teeth 39 of the intermediate part 11 and the external teeth 6 of the hub 4.
  • the angle of rotation of the intermediate part 11 is limited relative to the hub 4.
  • four windows 41, 42, 43 and 44 are recessed in the intermediate part 11, in each of which a spring device 24, 45, 46, 47 is arranged.
  • the spring devices 45, 46 in FIG. 4 correspond to the spring devices 25, 26 in FIG. 1.
  • the spring devices 45 to 47 like the spring device 24, respectively comprise an inner helical spring and an outer helical spring.
  • the longitudinal axis of the spring device 24 is designated 50 in FIGS. 4 and 5.
  • the longitudinal axis 50 is simultaneously the longitudinal axis of the coil springs 34 and 35.
  • the spring means 24, 45, 46, 47 each engage a guide nose 51 to 54, which extends in the direction of the longitudinal axis 50 of the associated spring means 24, 45 extends to 47.
  • the windows 41 to 44 each have a recess 55 to 58 on. The recesses 55 to 58 extend beyond the space required for receiving the spring means in the circumferential direction addition.
  • a guide nose 61 to 64 is arranged in each case, which emanates from the intermediate part 12.
  • the outgoing from the intermediate part 12 guide lugs 61 to 64 engage in the other end of the inner coil springs of the spring means 24, 45 to 47 a.
  • the shape of the recesses is at the end in each case adapted to the shape of spacer bolts 28, 65, 66, 67, which extend in the region of the recesses through the intermediate parts 11, 12.
  • the intermediate parts 11, 12 are identical.
  • the guide lugs 51, 61 are each integrally connected to the associated intermediate part 11, 12.
  • the intermediate parts are designed as sheet metal parts from which the guide lugs 51, 61 are stamped out.
  • the complete shape of the intermediate part 11 and the spring engaging portion of the second intermediate part 12 can be seen.
  • the recessed in the intermediate parts 11, 12 windows at the ends of the spacer bolts 66, 67 abut and thus initiate the moment.
  • the hub (4 in Figure 4) sits with its external teeth in the internal teeth of the intermediate elements 11, 12 and is connected depending on the load direction with one or the other intermediate part 11,12 on flanking the teeth.
  • FIG. 5 shows a section through the longitudinal axis 50 of the spring device 24 parallel to the axis of rotation (13 in FIG. 2) of the torsional vibration damper 1.
  • the guide lugs 51, 61 of the intermediate parts 11, 12, which are also referred to as intermediate elements axially stamped out so that they are approximately in the spring center axis 50.
  • the guide lugs 51, 61 protrude into the width B between the two intermediate parts 11, 12 for lateral guidance of the spring device 24 in all operating states.
  • the moment flux in the torsional vibration damper 1 is indicated schematically.
  • an arrow 70 the normal direction of rotation of the torsional vibration damper 1 is indicated.
  • hatched arrows 71 to 74 of the torque flow or power flow in the train operation of a equipped with the torsional vibration damper 1 motor vehicle is indicated.
  • Arrows 75 to 78 indicate the torque flow or force flow in the overrun operation of the motor vehicle.
  • the torque is transmitted via the spacing bolt 67 as a circumferential force to the intermediate part 12, as indicated by the arrow 71.
  • the intermediate part 12 transmits the force to the spring devices 24 via the guide lugs 61.
  • the spring devices 24 in turn transmit the force or the torque to the guide lugs 54 of the intermediate part 11, as indicated by the arrow 72.
  • the arrows 73 and 74 indicate that the force or the torque is transmitted via the internal toothing of the intermediate part 11 to the external toothing of the hub 4.
  • the abutment torque and thus the Endverduswinkel are reached when the internal teeth of the intermediate part 12 also abuts the outer toothing of the hub 4.
  • the conditions are analogous, as indicated by the arrows 75 to 78.
  • FIG. 7 shows an exploded view of the torsional vibration damper 1.
  • window wings 81, 82 are provided on the side parts 21, 22.
  • the sashes 81, 82 are not the side guide of the spring means 24, 45 to 47, but have to these in each position a minimum distance.
  • the sashes 81, 82 serve only for additional security, and should prevent the emergence of the spring means 24, 45 to 47 from the torsional vibration damper 1 in case of malfunction. Since the side guide is effected solely by the intermediate parts 11, 12, the window sash 81, 82 on the side parts 21, 22 can also be omitted.
  • FIGS. 8 to 10 it can be seen that the two intermediate parts or intermediate elements 11, 12 are of identical construction.
  • the identical intermediate elements 11, 12 are installed rotated by 180 degrees.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Mechanical Operated Clutches (AREA)
PCT/DE2007/001242 2006-08-12 2007-07-12 Drehschwingungsdämpfer WO2008019641A1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN200780030049XA CN101501362B (zh) 2006-08-12 2007-07-12 扭转振动减振器
DE112007001663.9T DE112007001663B4 (de) 2006-08-12 2007-07-12 Drehschwingungsdämpfer
BRPI0715128-4A BRPI0715128B1 (pt) 2006-08-12 2007-07-12 Amortecedor de vibrações torsionais

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006037841.5 2006-08-12
DE102006037841 2006-08-12

Publications (1)

Publication Number Publication Date
WO2008019641A1 true WO2008019641A1 (de) 2008-02-21

Family

ID=38626252

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE2007/001242 WO2008019641A1 (de) 2006-08-12 2007-07-12 Drehschwingungsdämpfer

Country Status (4)

Country Link
CN (1) CN101501362B (zh)
BR (1) BRPI0715128B1 (zh)
DE (1) DE112007001663B4 (zh)
WO (1) WO2008019641A1 (zh)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015172785A1 (de) 2014-05-16 2015-11-19 Schaeffler Technologies AG & Co. KG Kupplungsscheibe mit torsionsschwingungsdämpfer
WO2015185271A1 (de) * 2014-06-05 2015-12-10 Zf Friedrichshafen Ag Drehschwingungsdämpfer
DE102015211899A1 (de) 2015-06-26 2016-12-29 Schaeffler Technologies AG & Co. KG Torsionsschwingungsdämpfer
DE102016205512A1 (de) 2016-04-04 2017-10-05 Schaeffler Technologies AG & Co. KG Flügelantriebselement eines Drehschwingungsdämpfers mit symmetrisch angeordnetem Bolzen
DE102017123768A1 (de) 2017-08-04 2019-02-07 Schaeffler Technologies AG & Co. KG Torsionsschwingungsdämpfer mit radial angeordneter Reihenschaltung zwei Dämpfungseinheiten und Kupplung mit Torsionsschwingungsdämpfer
DE202019106749U1 (de) 2018-12-07 2019-12-16 Schaeffler Technologies AG & Co. KG Drehmomentbegrenzer
DE102018131319B3 (de) * 2018-12-07 2020-02-27 Schaeffler Technologies AG & Co. KG Drehmomentbegrenzer mit zumindest einem Abstandsblech und/oder Abstandsbolzen zur Zentrierung einer daran angrenzenden Komponente des Drehmomentbegrenzers
DE202020102033U1 (de) 2019-06-26 2020-04-20 Schaeffler Technologies AG & Co. KG Torsionsschwingungsdämpfer im Zweiflansch-Design mit zwei in einer Schwungscheibe integrierten Flanschelementen und gestapelten Blechsegmenten; sowie Antriebsstrang
DE102018131348A1 (de) 2018-12-07 2020-06-10 Schaeffler Technologies AG & Co. KG Drehmomentbegrenzer mit über den Umfang des Drehmomentbegrenzers asymmetrisch verteilten Montagebohrungen
DE102018131346A1 (de) 2018-12-07 2020-06-10 Schaeffler Technologies AG & Co. KG Mehrflanschdämpfer für eine lösbare Drehmomentübertragungseinheit
DE102018131322A1 (de) 2018-12-07 2020-06-10 Schaeffler Technologies AG & Co. KG Mehrflanschtorsionsschwingungsdämpfer mit zumindest zwei gleichteilig ausgebildeten Nabenflanschen und einem Drehmomentbegrenzer
DE102018131318A1 (de) 2018-12-07 2020-06-10 Schaeffler Technologies AG & Co. KG Abstandselement für einen Torsionsschwingungsdämpfer
DE102019105836A1 (de) * 2019-03-07 2020-09-10 Schaeffler Technologies AG & Co. KG Drehschwingungsdämpfer
DE102019204374A1 (de) * 2019-03-28 2020-10-01 Zf Friedrichshafen Ag Fliehkraftausgleichselement zur Ansteuerung von Torsionsfedern in einer Kupplungsscheibe
WO2020228899A1 (de) 2019-05-10 2020-11-19 Schaeffler Technologies AG & Co. KG Drehschwingungsdämpfer mit mehrflanschdämpfer und vordämpfer sowie system und kupplungsscheibe mit drehschwingungsdämpfer
WO2021052529A1 (de) 2019-09-19 2021-03-25 Schaeffler Technologies AG & Co. KG Torsionsdämpfer mit mehrstufiger hauptdämpferkennlinie
US20220228642A1 (en) * 2019-06-26 2022-07-21 Lord Corporation Dual rate torsional coupling
DE102022105340B3 (de) 2022-03-08 2023-04-20 Schaeffler Technologies AG & Co. KG Kupplungsscheibe

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101852783B (zh) * 2010-05-21 2011-08-03 重庆市计量质量检测研究院 顶空固相微萃取-气相色谱质谱联用检测潲水油的方法
CN104653702B (zh) * 2013-11-25 2017-10-31 上海汽车集团股份有限公司 双质量飞轮
DE102020202178A1 (de) 2020-02-20 2021-08-26 Zf Friedrichshafen Ag Torsionsschwingungsdämpfer und Schraubenfeder für einen Torsionsschwingungsdämpfer

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4613029A (en) * 1980-12-16 1986-09-23 Valeo Torsion damping device for an automobile clutch friction disc
DE3840615A1 (de) * 1987-12-08 1989-06-22 Valeo Drehschwingungsdaempfer mit grossem verschiebungswinkel, insbesondere reibungskupplung, besonders fuer ein kraftfahrzeug
DE4332936A1 (de) * 1992-10-14 1994-04-21 Luk Lamellen & Kupplungsbau Torsionsschwingungsdämpfer

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2619182B2 (fr) * 1987-04-02 1992-06-12 Valeo Dispositif amortisseur de torsion a organe de transmission de mouvement
EP1394440B1 (en) * 1995-07-24 2005-05-25 Exedy Corporation Damper disc assembly having a friction mechanism with improved friction elements
CN2301575Y (zh) * 1997-09-10 1998-12-23 上海离合器总厂 扭转减振机构
DE10209409A1 (de) * 2001-03-08 2002-09-12 Luk Lamellen & Kupplungsbau Drehschwingungsdämpfer
ATE370352T1 (de) * 2004-11-30 2007-09-15 Luk Lamellen & Kupplungsbau Drehschwingungsdämpfer

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4613029A (en) * 1980-12-16 1986-09-23 Valeo Torsion damping device for an automobile clutch friction disc
DE3840615A1 (de) * 1987-12-08 1989-06-22 Valeo Drehschwingungsdaempfer mit grossem verschiebungswinkel, insbesondere reibungskupplung, besonders fuer ein kraftfahrzeug
DE4332936A1 (de) * 1992-10-14 1994-04-21 Luk Lamellen & Kupplungsbau Torsionsschwingungsdämpfer

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015172785A1 (de) 2014-05-16 2015-11-19 Schaeffler Technologies AG & Co. KG Kupplungsscheibe mit torsionsschwingungsdämpfer
WO2015185271A1 (de) * 2014-06-05 2015-12-10 Zf Friedrichshafen Ag Drehschwingungsdämpfer
DE102015211899A1 (de) 2015-06-26 2016-12-29 Schaeffler Technologies AG & Co. KG Torsionsschwingungsdämpfer
DE102016205512A1 (de) 2016-04-04 2017-10-05 Schaeffler Technologies AG & Co. KG Flügelantriebselement eines Drehschwingungsdämpfers mit symmetrisch angeordnetem Bolzen
DE102017123768A1 (de) 2017-08-04 2019-02-07 Schaeffler Technologies AG & Co. KG Torsionsschwingungsdämpfer mit radial angeordneter Reihenschaltung zwei Dämpfungseinheiten und Kupplung mit Torsionsschwingungsdämpfer
DE102018131348A1 (de) 2018-12-07 2020-06-10 Schaeffler Technologies AG & Co. KG Drehmomentbegrenzer mit über den Umfang des Drehmomentbegrenzers asymmetrisch verteilten Montagebohrungen
DE102018131319B3 (de) * 2018-12-07 2020-02-27 Schaeffler Technologies AG & Co. KG Drehmomentbegrenzer mit zumindest einem Abstandsblech und/oder Abstandsbolzen zur Zentrierung einer daran angrenzenden Komponente des Drehmomentbegrenzers
DE202019106749U1 (de) 2018-12-07 2019-12-16 Schaeffler Technologies AG & Co. KG Drehmomentbegrenzer
DE102018131346A1 (de) 2018-12-07 2020-06-10 Schaeffler Technologies AG & Co. KG Mehrflanschdämpfer für eine lösbare Drehmomentübertragungseinheit
DE102018131322A1 (de) 2018-12-07 2020-06-10 Schaeffler Technologies AG & Co. KG Mehrflanschtorsionsschwingungsdämpfer mit zumindest zwei gleichteilig ausgebildeten Nabenflanschen und einem Drehmomentbegrenzer
DE102018131318A1 (de) 2018-12-07 2020-06-10 Schaeffler Technologies AG & Co. KG Abstandselement für einen Torsionsschwingungsdämpfer
DE102019105836A1 (de) * 2019-03-07 2020-09-10 Schaeffler Technologies AG & Co. KG Drehschwingungsdämpfer
DE102019204374A1 (de) * 2019-03-28 2020-10-01 Zf Friedrichshafen Ag Fliehkraftausgleichselement zur Ansteuerung von Torsionsfedern in einer Kupplungsscheibe
WO2020228899A1 (de) 2019-05-10 2020-11-19 Schaeffler Technologies AG & Co. KG Drehschwingungsdämpfer mit mehrflanschdämpfer und vordämpfer sowie system und kupplungsscheibe mit drehschwingungsdämpfer
DE202020102033U1 (de) 2019-06-26 2020-04-20 Schaeffler Technologies AG & Co. KG Torsionsschwingungsdämpfer im Zweiflansch-Design mit zwei in einer Schwungscheibe integrierten Flanschelementen und gestapelten Blechsegmenten; sowie Antriebsstrang
US20220228642A1 (en) * 2019-06-26 2022-07-21 Lord Corporation Dual rate torsional coupling
WO2021052529A1 (de) 2019-09-19 2021-03-25 Schaeffler Technologies AG & Co. KG Torsionsdämpfer mit mehrstufiger hauptdämpferkennlinie
DE102022105340B3 (de) 2022-03-08 2023-04-20 Schaeffler Technologies AG & Co. KG Kupplungsscheibe

Also Published As

Publication number Publication date
CN101501362A (zh) 2009-08-05
BRPI0715128A8 (pt) 2016-12-27
BRPI0715128A2 (pt) 2013-04-02
DE112007001663B4 (de) 2017-09-07
DE112007001663A5 (de) 2009-04-16
BRPI0715128B1 (pt) 2019-04-30
CN101501362B (zh) 2011-06-08

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