WO2015162491A2 - Driven plate with intermediate plate centering guide - Google Patents

Driven plate with intermediate plate centering guide Download PDF

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Publication number
WO2015162491A2
WO2015162491A2 PCT/IB2015/000640 IB2015000640W WO2015162491A2 WO 2015162491 A2 WO2015162491 A2 WO 2015162491A2 IB 2015000640 W IB2015000640 W IB 2015000640W WO 2015162491 A2 WO2015162491 A2 WO 2015162491A2
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WO
WIPO (PCT)
Prior art keywords
plate
driven
intermediate plate
driven plate
tabs
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.)
Ceased
Application number
PCT/IB2015/000640
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French (fr)
Other versions
WO2015162491A3 (en
Inventor
Rabah Arhab
Alfonso Medellin
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Valeo Embrayages SAS
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Valeo Embrayages SAS
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 Valeo Embrayages SAS filed Critical Valeo Embrayages SAS
Priority to CN201580021815.0A priority Critical patent/CN106255844B/en
Priority to DE112015002014.4T priority patent/DE112015002014B4/en
Publication of WO2015162491A2 publication Critical patent/WO2015162491A2/en
Publication of WO2015162491A3 publication Critical patent/WO2015162491A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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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
    • F16F15/131Suppression 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 the rotating system comprising two or more gyratory masses
    • F16F15/133Suppression 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 the rotating system comprising two or more gyratory masses using springs as elastic members, e.g. metallic springs
    • F16F15/134Wound springs
    • F16F15/1343Wound springs characterised by the spring mounting
    • 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
    • F16HGEARING
    • F16H45/00Combinations of fluid gearings for conveying rotary motion with couplings or clutches 
    • F16H45/02Combinations of fluid gearings for conveying rotary motion with couplings or clutches  with mechanical clutches for bridging a fluid gearing of the hydrokinetic type
    • 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
    • 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
    • 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
    • F16HGEARING
    • F16H45/00Combinations of fluid gearings for conveying rotary motion with couplings or clutches 
    • F16H45/02Combinations of fluid gearings for conveying rotary motion with couplings or clutches  with mechanical clutches for bridging a fluid gearing of the hydrokinetic type
    • F16H2045/0221Combinations of fluid gearings for conveying rotary motion with couplings or clutches  with mechanical clutches for bridging a fluid gearing of the hydrokinetic type with damping means
    • 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
    • F16HGEARING
    • F16H45/00Combinations of fluid gearings for conveying rotary motion with couplings or clutches 
    • F16H45/02Combinations of fluid gearings for conveying rotary motion with couplings or clutches  with mechanical clutches for bridging a fluid gearing of the hydrokinetic type
    • F16H2045/0221Combinations of fluid gearings for conveying rotary motion with couplings or clutches  with mechanical clutches for bridging a fluid gearing of the hydrokinetic type with damping means
    • F16H2045/0226Combinations of fluid gearings for conveying rotary motion with couplings or clutches  with mechanical clutches for bridging a fluid gearing of the hydrokinetic type with damping means comprising two or more vibration dampers

Definitions

  • the invention generally relates to a turbine damper assembly of a torque converter. Specifically, this invention relates to a turbine damper assembly of a torque converter turbine comprising a driven piate including . an axiai!y and circumferential driven plate flange that ensures intermediate plate to driven plate centering and also helps contain elastic drive elements.
  • a contemporary torque converter includes a friction clutch assembly associated wit a driven member of the torque converter which, at preset loads and speeds, eliminates the fluid transmission of torque and replaces the fluid coupling with a direct mechanical friction coupling. This feature is commonly -referred to as a lock-up clutch.
  • the present invention is a turbine damper assembly comprising a torque converter turbine associated driven plate that includes a shaped, axially extending, driven plate flange -that functions as a guide and centering element for an associated driven intermediate plate.
  • the driven plate flange helps contain the elastic torque transmitting dri ve elements in position in the turbine damper assembly. This containment feature eases assembly and reduces the onset of rattles between the component following wear and sudden torque transitions.
  • the turbine damper assembly includes a driven plate non-rotatably attached on a surface opposed to a turbine portion of the torque converter.
  • the driven plate i turn, rotationaliy engages the overlying and
  • the driven plate includes an axially extended, circumferentially oriented, driven plate flange that is, preferably, stamped into, the driven plate.
  • the intermediate piate is driven via radially extendin driven plate tabs associated with the driven plate, as these tabs push against the elastic spring elements in a circumferential rotational direction against compleme tary torque receiving intermediate plate tabs on the intermediate plate.
  • the torque receiving tabs on the intermediate plate overlie the driven plate flange profile so as to center the respective driven and intermediate plates one with Driven Plate with intermediate Plate Centering Guide respect to the other, hi such a structure, once the torque converter is placed in a lock-up mode, the torque path of the drive system is through the elastic drive elements of the intermed ate plate.
  • the driven plate flange stamped into the driven plate preferably supports the elastic torque transmitting drive elements as they rest in cooperating aligned windows, stamped into the driven plate, and a circumferential inwardly directed tab equipped groove in the intermediat plate.
  • the elastic- drive elements compress and decompress at. various levels of torque transmission, they are suspended against axial and radial movement in a series of circumferential curved cavities which Include the driven plate flange and the intermediate plate groove forming at least a portion of the circumferential curved cavity.
  • FIG. 1 is a partial perspective view of turbine driven plate and associated overlying intermediate plate of a turbine damper assembly in accordance ith an exemplary embodiment of the present invention.
  • FIG. 2 is a sectional view of the turbine damper assembly in accordance w th the exemplary embodiment of the present invention. Driven Plate with intermediate Plate Centering Guide
  • Fig, 1 shows a turbine damper assembly 10 of a torque converter including a turbine 14.
  • the turbine damper assembly 10 comprises a substantially annular turbine driven plate 12 and a substantially -annular .intermediate plate 16, wherein the turbine driven plate 12 is provided with a eirc-umferentia!ly and axial i-y extending driven plate flange 24 in accordance with the present invention.
  • the turbine 14 and the associated driven plate 12 rotate as an integral unit about a turbine hub 30. in other words, both the turbine driven plate 12 and the turbine 14 are non- roiatably secured to a turbine hub 30.
  • the turbine driven plate 12, the turbine 14 and the turbine hub 28 may be non-rotaiably secured to one another using any appropriate technique, such as, for example, welding or fasteners, such as rivets.
  • the turbine driven plate 12 includes radially outwardly extending driven plate (or first) tabs 22 that rotational ly urge springs seats 19 against elastic drive elements (springs) 18 that, in turn, urge against radially inwardly directed, torque receiving intermediate plate (or second) tabs 20, so as to rotate the intermediate plate 16,
  • the intermediate plate 16 is, for example, then associated rotationaily with a friction clutch element (not shown) for transmitting, torque thereafter through an associated vehicle drive system,
  • the intermediate plate 16 further includes an inwardly directed circumferential (or annular) groove 17 that also include the intermediate plate tabs 20.
  • the intermediate plate tabs 20 overlie and rest on the driven plate flange 24 when the intermediate plate 1 and the driven plate 12 are assembled as shown.
  • the driven plate flange 24 the intermediate plate tab 20 interface serves to center the Intermediate- plate 16 with respect to the driven plate 12.
  • the elastic drive elements I S are contained within w indows 21 stamped into the driven plate 12 hat cooperate with the complementary intermediate plate tab 20 locations on the overlying intermediate plate- 16.
  • the radially inward portions of the elastic drive elements 18 are contained, Driven Plate with intermediate Plate Centering Guide in part, by the driven plate flange 24.
  • FIG. L shows a sectional view of the turbine damper assembly 10 shown in Fig. L
  • the intermediate plate 16 overlies -and is centered with respect to the driven plate 12 via cooperating sliding contact between the torque receiving intermediate plate tab.20 and the driven plate flange 24.
  • the radius Rl of the driven plate flange 24 is shown to be smaller than an outer radius R2 of the intermediate plate 16 and an inner surface of the associated intermediate plate tab 20.
  • the intermediate plate tab 20 has a reversed tl -shape profile, wherein an inward portion of the U rests along a radially outer surface of the driven plate flange 24.
  • the intermediate plate 16 and the driven plate 12 remain respectively centered and the elastic drive elements 18 remain confined in their locations.
  • the respective driven plate 12 and intermediate plate 16. along with their associated tabs 22 and 20. are stamped from suitable steei or other resilient metal useful for forming torque eon verier and drive system elements.
  • the e lastic drive elements 18 are preferably wound steel springs with sufficient capacity to transfer the torque for which the overall system is designed to transmit.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Operated Clutches (AREA)
  • Motor Power Transmission Devices (AREA)

Abstract

A turbine damper assembly, for a torque converter, includes a driven plate and an intermediate plate. The driven plate engages and drives the intermediate piate through elastic drive elements. The driven plate includes an axially extended, circumferentially oriented, driven plate flange that both centers the intermediate plate with respect to the drive plate and also assists in containing the elastic drive elements in circumferential curved cavities during and after assembly of the turbine damper assembly.

Description

DRIVEN PLATE WITH INTERMEDIATE PLATE CENTERING .GUIDE
Field of the Invention;
J O lj The invention generally relates to a turbine damper assembly of a torque converter. Specifically, this invention relates to a turbine damper assembly of a torque converter turbine comprising a driven piate including. an axiai!y and circumferential driven plate flange that ensures intermediate plate to driven plate centering and also helps contain elastic drive elements.
Background of the invention:
[0002) In the evolution of automobiles from motorized carriages to highly regulated devices for mass transportation, there has been a continuous pursuit of refinement of the basic combination of elements that comprise the automobile. One aspect of this refinement has been the
transmission of torque from an internal combustion engine to a drive system of the automobile. This transmission of torque has, throughout, been -accomplished by various gear or chain dri ven transmission systems alternatively dnvingly connected to, or disconnected from, -a source of motive power, such as the internal combustion engine. The connection/disconnection- feature of the drive system is accomplished by means of a clutch- Sinc the mid- 1950\s, especially in the United States, this clutch has been a fluid clutch or a torque converter. Owing to the inclusion of this fluid torque transmitting coupling, enhanced refinement of the driving experience was obtained, but this refinement came at the expense of lost, efficiency. To address this lost efficiency, the torque converter has become, itself,, an object of greater refinement and recaptured Driven Plate with intermediate Plate Centering Guide efficiency. Often times, a contemporary torque converter includes a friction clutch assembly associated wit a driven member of the torque converter which, at preset loads and speeds, eliminates the fluid transmission of torque and replaces the fluid coupling with a direct mechanical friction coupling. This feature is commonly -referred to as a lock-up clutch.
(0003] .In. the current lock-up clutch equipped torque converter, efficiency has been recaptured, but a loss of refinement has also occurred when the clutch is in lock-up mode and when it is transitioning into and out of lock-up mode. This is especially true when lock-up clutch elements become worn and tolerances between various rotating and fixed elements increase/decrease in accord with their respective wear patterns. To al leviate some of the mechanical coarseness created by the incorporation of lock-up clutches onto torque converters, the clutch systems, themselves, have increased in complexity. For example, the inclusion of a driven intermediate plate, and the further inclusion of elastic damping members- to keep driveline torque oscillations within acceptable parameters, adds rotational mass and complexity to the torque converter subassemblies. This added complexity creates the potential for a loss refinement through vibration caused, in part, b unbalanced de-centered rotation of the various components. In -addition, it is common for the elastic torque transmitting member equipped devices to, over time and wear, develop rattles and other noises that, create a perception of low integrity of the torque converter device. In addition, the assembly of these increasingly complex clinch and damper systems requires more time, patience, and precision. An example of such a torque converter with a lockup clutch and elastic torque transmission element through an intermediate plate is shown in US Patent 6,571 ,929. Driven Plate with intermediate Plate Centering Guide
[0004} Therefore, the torque converters are susceptible to improvements that may enhance their performance, refinement and cost. With this in mind, a need exists to develop an improved turbine damper assembly for a torque converter with improved performance and refinement.
BRIEF SUMMARY OF THE INVENTION
(OQOSJ The present invention is a turbine damper assembly comprising a torque converter turbine associated driven plate that includes a shaped, axially extending, driven plate flange -that functions as a guide and centering element for an associated driven intermediate plate. In addition, during and after assembly of the driven plate and intermediate plate, the driven plate flange helps contain the elastic torque transmitting dri ve elements in position in the turbine damper assembly. This containment feature eases assembly and reduces the onset of rattles between the component following wear and sudden torque transitions.
[OO06J The turbine damper assembly according with an exemplary embodiment of the present invention includes a driven plate non-rotatably attached on a surface opposed to a turbine portion of the torque converter. The driven plate, i turn, rotationaliy engages the overlying and
surrounding intermediate plate through the elastic drive elements. The driven plate includes an axially extended, circumferentially oriented, driven plate flange that is, preferably, stamped into, the driven plate. The intermediate piate is driven via radially extendin driven plate tabs associated with the driven plate, as these tabs push against the elastic spring elements in a circumferential rotational direction against compleme tary torque receiving intermediate plate tabs on the intermediate plate. The torque receiving tabs on the intermediate plate overlie the driven plate flange profile so as to center the respective driven and intermediate plates one with Driven Plate with intermediate Plate Centering Guide respect to the other, hi such a structure,, once the torque converter is placed in a lock-up mode, the torque path of the drive system is through the elastic drive elements of the intermed ate plate.
[0007] Also, in accordance with the exemplary embodiment of the present invention, the driven plate flange stamped into the driven plate preferably supports the elastic torque transmitting drive elements as they rest in cooperating aligned windows, stamped into the driven plate, and a circumferential inwardly directed tab equipped groove in the intermediat plate. As the elastic- drive elements compress and decompress at. various levels of torque transmission, they are suspended against axial and radial movement in a series of circumferential curved cavities which Include the driven plate flange and the intermediate plate groove forming at least a portion of the circumferential curved cavity.
BRIEF PES.CRIFn.ON OF THE SEVERAL VIEWS OP THE DRAWING(S)
[0008] The accompanying drawings are incorporated in and constitute a pari of the specification. The drawings, together with the general description given above and the detailed description of the exemplary embodiments and methods given below, serve to explain the principles of the invention. In such drawings:
|0009] FIG. 1 is a partial perspective view of turbine driven plate and associated overlying intermediate plate of a turbine damper assembly in accordance ith an exemplary embodiment of the present invention; and
[.00.1.0] FIG. 2 is a sectional view of the turbine damper assembly in accordance w th the exemplary embodiment of the present invention. Driven Plate with intermediate Plate Centering Guide
DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS AND EMBODIED
METHODS OF THE INVENTION
(0011 ] Reference will now be made in detail to exemplar embodiments and methods of the invention as illustrated in the accompanying drawings, in which like reference characters designate like or corresponding parts throughout the drawings, ft. should be noted, however, that the invention in its broader aspects is not limited to the specific details, representative devices and methods, and illustrative examples shown and described in connection with the exemplary embodiments and methods.
|0 I2] This description of exemplary embodiments is intended to be read in connection with the accompanying drawings, which are to be considered part of the entire written description. In the description, relative terras such as "horizontal" "vertical." "up," "down." "upper", "lower", "right*, "left", "top" and "bottom" as well as derivatives (.hereof (e.g., "horizontally,"
"downwardly," "upwardly," etc.) should be construed to refer to the orientation as then described or as shown in the drawing figure under discussion. These relative terms are for convenience of description and normally are not intended to require a particular orientation. Terms concerning attachments, coupling and the like, such as "connected" and "interconnected," 'refer to a
relationship wherein structures are secured or attached to one another either directl or indirectly through intervening structures, as well as both movable or rigid attachments or relationships, unless expressly described otherwise. The term "operatively connected" is such an attachment, coupling or connection that allows the pertinent structures to operate as intended by virtue of that relationship. Additionally, the word "a" and "an" as used in the claims means " t least one" and the word " wo" as used in the claims means "a least two". Driven Plate with ntermediate Plate Centering Guide
{0613] Fig, 1 shows a turbine damper assembly 10 of a torque converter including a turbine 14. The turbine damper assembly 10 comprises a substantially annular turbine driven plate 12 and a substantially -annular .intermediate plate 16, wherein the turbine driven plate 12 is provided with a eirc-umferentia!ly and axial i-y extending driven plate flange 24 in accordance with the present invention. The turbine 14 and the associated driven plate 12 rotate as an integral unit about a turbine hub 30. in other words,, both the turbine driven plate 12 and the turbine 14 are non- roiatably secured to a turbine hub 30. It should be understood that the turbine driven plate 12, the turbine 14 and the turbine hub 28 may be non-rotaiably secured to one another using any appropriate technique, such as, for example, welding or fasteners, such as rivets.
10014) The turbine driven plate 12 includes radially outwardly extending driven plate (or first) tabs 22 that rotational ly urge springs seats 19 against elastic drive elements (springs) 18 that, in turn, urge against radially inwardly directed, torque receiving intermediate plate (or second) tabs 20, so as to rotate the intermediate plate 16, The intermediate plate 16 is, for example, then associated rotationaily with a friction clutch element (not shown) for transmitting, torque thereafter through an associated vehicle drive system,
}M15J The intermediate plate 16 further includes an inwardly directed circumferential (or annular) groove 17 that also include the intermediate plate tabs 20. The intermediate plate tabs 20 overlie and rest on the driven plate flange 24 when the intermediate plate 1 and the driven plate 12 are assembled as shown. The driven plate flange 24 the intermediate plate tab 20 interface serves to center the Intermediate- plate 16 with respect to the driven plate 12. The elastic drive elements I S are contained within w indows 21 stamped into the driven plate 12 hat cooperate with the complementary intermediate plate tab 20 locations on the overlying intermediate plate- 16. The radially inward portions of the elastic drive elements 18 are contained, Driven Plate with intermediate Plate Centering Guide in part, by the driven plate flange 24. This containment via the driven' plate flange 24 eases assembly of the intermediate plate 16 and the driven plate 12, and also lessens the development of rattles as- the assembled clearances of the turbine damper assembly 10 alter with wear. The elastic drive elements 18 remain confined with a series of circumferential curved' cavities 23 defined, respectively, between the inwardly directed groove 17 of the intermediate plate 16, and the axial and circumferential driven plate flange 24 of the driven plate 12, and respective driv tabs 22 and 20, and spring seats 19,
(0016) Fig, 2 shows a sectional view of the turbine damper assembly 10 shown in Fig. L The intermediate plate 16 overlies -and is centered with respect to the driven plate 12 via cooperating sliding contact between the torque receiving intermediate plate tab.20 and the driven plate flange 24. The radius Rl of the driven plate flange 24 is shown to be smaller than an outer radius R2 of the intermediate plate 16 and an inner surface of the associated intermediate plate tab 20.
Preferably, the intermediate plate tab 20 has a reversed tl -shape profile, wherein an inward portion of the U rests along a radially outer surface of the driven plate flange 24. Thus, when assembled and, thereafter, in use. the intermediate plate 16 and the driven plate 12 remain respectively centered and the elastic drive elements 18 remain confined in their locations.
10017] The respective driven plate 12 and intermediate plate 16. along with their associated tabs 22 and 20. are stamped from suitable steei or other resilient metal useful for forming torque eon verier and drive system elements. The e lastic drive elements 18 are preferably wound steel springs with sufficient capacity to transfer the torque for which the overall system is designed to transmit.
[0018} The foregoing description of the exemplary embodimen t(s) of the present invention has been presented for the purpose of illustration in accordance with the provisions of the Patent Driven Plate with Intermediate Plate Centering Guide
Statutes, ft is not intended to be exhaustive or to limit the invention TO the precise forms disclosed. The embodiments disclosed hereinabove were chosen in order to best illustrate the principles of the present invention and its practical application to thereby enable those of ordinary skill in the art to best utilize the invention in various embodiments and with various modifications as suited to the particular use contemplated, as long as the principles described herein are followed. This application is iherefbre intended to cover any variations, uses, or adaptations of the invention using its general principles. Further, this application is intended to cover such departures from the present, disclosure as come within known or customary practice in the art to which this invention pertains. Thus, changes can be made in the above-described invention without departing from the intent and scope thereof it is also intended that the scope of the present invention be defined by the claims appended thereto.

Claims

Driven Plate with intermediate Plate Centering Guide What' is claimed is:
\ . A torque converter turbine damper assembly, comprising:
a turbine mounted driven plate including a eireumferenttaiiy and axially extended driven plate flange having a first radius, and torque transmitting, radially extending, driven plate tabs extending beyond said first radius;
an intermediate plate including a radially in wardly directed groove formed around a circumference of said intermediate plate, said intermediaie plate having a second radius exceeding said first radius, said groove further including radially inwardly directed torque receiving intermediate plate tabs; and
elastic drive elements interposed rotaiiona!ly between said driven plate and said intermediate plate, and residing in a series of circumferential cavities .defined, in part, by said driven plate flange and said inward iy directed groove, respectively;
said driven plate tabs, provided on said drive plate, drive said intermediate plate tabs, provided on said intermediate plate, through said interposed elastic drive elements, and said intermediate plate tabs radially overhe said driven plate flange and rotationally center said intermediate plate with respect to said driven plate.
2. The turbine damper assembly as in claim I , wherein each of said driven plate and said intermediaie plate comprises a stamped metallic construction. Driven Piste with intermediate Plate Centering Guide
3. The turbine dampe assembl , a in claim 1 , wherein each of said intermediate plate tabs has an inwardly directed U-shaped profile; and wherein a bottom portion of said U- shaped profile contacts said driven plate flange.
4. 'The turbine damper assembly, as In claim 1 , wherein said elastic drive elements comprise wound springs.
5. A turbine damper assembly comprising:
a stamped, turbine mounted driven plate including a stamped circumferenUally and axially extended driven plate flange having a first radius, and torque transmitting, radially extending, stamped driven plate tabs extending beyond said first radius;
a stamped intermediate plate including a radially inwardly directed groove formed around a circumference of said intermediate plate, said intermediate plate having a second radius exceeding said first radius, said groove further including radially inwardly directed torque receiving U-shaped intermediate plate tabs; and
elastic drive elements interposed roiationai!y between said driven plate and said
intermediate plate and residing in a series of circum erential cavities defined, in part, by said driven plate flange and said inwardly directed groove, respectively;
said driven plate tabs, formed on said driven plate, drive said intermediate plate tabs, formed on said intermediate plate, through spring seats associated with each of said interposed elastic drive elements, and said U-shaped intermediate plate tabs radially overlie said driven plate flange and rotational iy center said intermediate plate with respect to said driven plate. Driven Plate with intermediate Plate Centering Guide
6, The turbine damper assembly, as in claim 5, wherein said elastic drive elements comprise wound springs,
7, The turbine assembly, as in claim 5, wherein said U-shaped intermediate plate tabs contact said driven plate flange along a bottom -portion of said U-shaped intermediate plate- tabs.
8, The turbine damper assembly s in claim 5-, wherein each of said driven plate and said intermediate plate comprises a stamped metallic construction,
9, A turbine damper assembly, comprising:
a substantially annular turbine mounted driven, plate including a cireumferentiafly and axia!Iy extended driven plate flange having a first radius, and torque transmitting, radially extending, driven plate tabs extending beyond said first radius;
substantially annular intermediate plate including a radially inwardly directed groove formed around a circumference of said intermediate plate, said intermediate plate having a second radius exceeding said first radius, said groove further including radially inwardly directed torque receiving intermediate plate tabs; and
wound spring elastic drive elements interposed rotationally between said driven, plate and said intermediate plate, and residing in a series of circumferential cavities defined, in part by said driven plate flange and said inwardly directed groove, respectively;
said driven plate tabs, provided on said drive plate, drive said intermediate- plate tabs, provided on said intermediate plate, through said interposed wound spring elastic drive elements. Driven Plate with intermediate Plate Centering Guide and said intermediate plate tabs radially overlie said driven fate flange and rotationailv center said intermediate plate with respect to said driven plate.
10. The damper assembly, as in claim 9, wherein said second tabs have .U-shaped profiles and wherein a bottom portion of said U-shaped profiles contacts said driven plate flange.
1 1 . The turbine damper assembly as .in claim wherein each of said driven plate and said intermediate plate comprises a stamped metallic construction.
PCT/IB2015/000640 2014-04-25 2015-04-17 Driven plate with intermediate plate centering guide Ceased WO2015162491A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201580021815.0A CN106255844B (en) 2014-04-25 2015-04-17 Drive plate with mid-plate centering guide
DE112015002014.4T DE112015002014B4 (en) 2014-04-25 2015-04-17 DRIVEN PLATE TURBINE DAMPER ASSEMBLY WITH INTERMEDIATE CENTERING GUIDE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/262,286 2014-04-25
US14/262,286 US9732825B2 (en) 2014-04-25 2014-04-25 Driven plate with intermediate plate centering guide

Publications (2)

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WO2015162491A2 true WO2015162491A2 (en) 2015-10-29
WO2015162491A3 WO2015162491A3 (en) 2016-01-07

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US (1) US9732825B2 (en)
CN (1) CN106255844B (en)
DE (1) DE112015002014B4 (en)
WO (1) WO2015162491A2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
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WO2017176743A1 (en) * 2016-04-06 2017-10-12 Schaeffler Technologies AG & Co. KG Damper assembly including spring support plate configured for receiving arc springs after assembly

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CN106255844B (en) 2019-09-06
US20150308539A1 (en) 2015-10-29
DE112015002014T5 (en) 2017-02-09
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WO2015162491A3 (en) 2016-01-07
CN106255844A (en) 2016-12-21
US9732825B2 (en) 2017-08-15

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