WO2013117841A1 - Pendular shock-absorbing device - Google Patents

Pendular shock-absorbing device Download PDF

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Publication number
WO2013117841A1
WO2013117841A1 PCT/FR2013/050173 FR2013050173W WO2013117841A1 WO 2013117841 A1 WO2013117841 A1 WO 2013117841A1 FR 2013050173 W FR2013050173 W FR 2013050173W WO 2013117841 A1 WO2013117841 A1 WO 2013117841A1
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WO
WIPO (PCT)
Prior art keywords
roller
pendulum
central
mass
diameter
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Application number
PCT/FR2013/050173
Other languages
French (fr)
Inventor
Jonathan ROST
Clément TONDELLIER
Original Assignee
Valeo Embrayages
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Publication date
Application filed by Valeo Embrayages filed Critical Valeo Embrayages
Publication of WO2013117841A1 publication Critical patent/WO2013117841A1/en

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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
    • F16F15/14Suppression 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 present invention relates to a pendulum damping device in a torque transmission for a motor vehicle, in particular in a double damping flywheel.
  • the document FR 2 826 079 describes a double damping flywheel for a motor vehicle, comprising a primary flywheel intended to be coupled to a motor shaft, such as for example a crankshaft, and a secondary flywheel, intended to be coupled to a drive shaft. input of a gearbox via a clutch.
  • the primary flywheel comprises two elements, a flywheel and a cover, welded to one another at their radially outer periphery, so as to delimit a sealed internal volume in which are mounted curved elastic members such as coil springs. helical.
  • the elastic members extend circumferentially and bear, at a first end, on the flywheel and / or on the cover and, at a second end, on an annular web connected to the secondary flywheel.
  • the elastic members are pressed against chutes disposed at the outer periphery of the aforementioned volume under the effect of centrifugal forces.
  • This volume includes grease to ensure the proper functioning of the elastic members.
  • the double damping flywheel further comprises pendular damping means, housed in the aforementioned internal volume, and comprising pendular masses mounted movably on the annular web, in particular by means of guide rollers. These masses are arranged radially inside or outside the curved elastic members.
  • the ends of the guide rollers are mounted in arcuate elongated holes of the annular web.
  • the edges of the holes oblongs thus form raceways for the ends of the rollers.
  • Document DE 10 2010 054 556 describes an annular web for a double damping flywheel equipped with pendular damping means.
  • the annular web consists of two annular parts attached to each other and defining between them a space housing pendular masses.
  • Each mass comprises two elongated arc-shaped holes, the concavity of which is turned radially outwards, serving for assembly with a set of two rollers.
  • the ends of the rollers are engaged in recesses of the aforementioned parts of the annular web, each recess having a generally arcuate oblong shape, with a concavity turned radially inwardly.
  • the rollers comprise radial flanges extending between the pendular masses and the portions of the annular web.
  • flanges are for example formed by elastic rings mounted in grooves cylindrical rollers.
  • assembly of the assembly is carried out in the following manner.
  • rollers are engaged in the oblong holes of the masses.
  • the elastic rings are then mounted on either side of the masses, in the corresponding grooves of the pendular masses.
  • First ends of the rollers are then engaged in the recesses of a first portion of the annular web, the second portion of the annular web then being mounted on the first, so that the second ends of the rollers engage in the corresponding recesses. of the second part.
  • the two parts of the annular web are then fixed to each other, for example by welding.
  • Guide rollers are movably mounted in the elongated holes of the aforesaid portions, the ends of the rollers being mounted in arcuate elongated holes of two supports attached to one another and forming a phasing washer.
  • the rollers comprise an enlarged central cylindrical zone, of diameter smaller than the radial dimension of the oblong holes formed in the central parts of the masses, but of diameter greater than the radial dimension of the oblong holes formed in the lateral parts of the masses.
  • the mounting of the pendular damping means is carried out as follows.
  • the rollers are engaged in the central parts of the masses, so that the central areas of the rollers are located in the oblong holes of the central parts of the masses.
  • the side portions are then disposed on either side of the central portions, so that the rollers extend through the oblong holes of said side portions.
  • the central part and the corresponding lateral parts of each mass are then fixed to each other by rivets.
  • the rollers are thus mounted captively in the masses. Indeed, after assembly, the widened central areas of the rollers abut against the lateral parts of the masses, which prevents the rollers from escaping axially.
  • the invention aims in particular to provide a simple, effective and economical solution to this problem.
  • a pendular damping device comprising at least one pendulum mass comprising a central part and at least two lateral parts, arranged on either side of the central part, each of said parts comprising at least one oblong hole. in an arc, and at least one guide roller movably mounted in the oblong holes of said parts, the roller being intended to be mounted in oblong holes in a circular arc of two supports, at two end zones.
  • cylindrical roller the roller having a central cylindrical zone, housed in the oblong hole of the central portion of the pendulum mass, characterized in that the roller comprises two cylindrical intermediate zones, housed in the oblong holes of the lateral parts of the pendulum mass , extending between the central zone and each of the end zones, the intermediate zones having a diameter different from the diameter of e the central zone, so as to form shoulders preventing the axial withdrawal of the roller from the oblong holes of the pendulum mass, the end zones having a diameter smaller than the diameter of the adjacent intermediate zones, so as to form a shoulder intended to come to bear against the corresponding supports.
  • the diameter of the central zone is greater than the diameter of the intermediate zones, the lateral parts of the mass forming axial stops for the shoulders provided between the central zone and the intermediate zones of the roll, so as to prevent the axial withdrawal of said roll from said mass.
  • the pendulum mass may, in this embodiment, have a large mass.
  • the diameter of the central zone is smaller than the diameter of the intermediate zones, the shoulders provided between the central zone and the intermediate zones of the roller being intended to come axially in abutment on the central part of the mass, in order to prevent axial removal of said roll from said mass.
  • This embodiment makes it possible to reduce the Hertz pressures between the roll and the mass, and between the roll and the supports.
  • the arc-shaped oblong hole of the central portion may have an enlarged end, allowing insertion of the roll into said oblong hole.
  • the enlarged end thus allows the passage of the widest areas of the roll, namely the intermediate areas.
  • At least some of the roll shoulders and / or some of the abutment surfaces of said shoulders are frustoconical or extend obliquely to the radial plane.
  • the central zone of the roll is intended to bear on the edges of the oblong hole of the central part of the pendulum mass.
  • the rolling of the rollers is only on the central part.
  • the realization of the masses is therefore easy because the lateral parts of the pendular masses do not have to be aligned very precisely.
  • the intermediate zones of the roller are intended to bear on the edges of the oblong holes of the lateral parts of the roller. pendulum mass. This has the advantage of preventing the tilting of the masses in operation.
  • the invention also relates, according to a second aspect of the invention, to a torque transmission device for a motor vehicle, comprising a torque input member and a torque output member rotatable with respect to the other, and resilient members mounted between the input and torque output members, the torque output member, or respectively the torque input member, having an annular web, the elastic members being mounted between the annular web and the torque entry element, or respectively between the annular web and the torque output member, characterized in that two annular supports extend radially on either side of the annular web and are fixed to said annular web, the torque transmission device further comprising a pendulum damping device according to the first aspect of the invention, the pendulum masses being arranged axially between the annular supports, the end regions of the rollers being movably mounted in arcuate oblong holes of the annular supports.
  • the torque transmitted by the annular web during operation can cause a deformation thereof and thus a deformation of the edges of the oblong holes forming the raceways. This can have an impact on the trajectory and, more generally, on the displacement of the pendular masses, which can affect the efficiency of the pendulum damping device.
  • the pendular masses are not mounted on the annular web, but on independent supports which do not provide the torque transmission function and which are therefore not deformed in operation.
  • the trajectory of the pendular masses is thus not affected by any deformation of the annular web, so that the efficiency of the pendular damping device is preserved.
  • the invention finally relates to a method for mounting a pendular damping device of the aforementioned type, characterized in that it comprises the steps of:
  • FIG. 1 is an exploded view, in perspective, of a double damping flywheel according to the invention
  • FIG. 2 is a view in axial section of the double damping flywheel of FIG. 1,
  • FIG. 3 is an exploded view, in perspective, of the annular web, the supports and the pendular damping means of the double damping flywheel of FIGS. 1 and 2,
  • FIGS. 4 to 6 are side views and in partial radial section, the double damping flywheel of Figures 1 to 3, in three different positions of the pendular masses,
  • FIG. 7 is a perspective view of a pendulum mass
  • FIG. 8 is an exploded perspective view of the pendulum mass of FIG. 7
  • FIGS. 9 and 10 are views respectively corresponding to FIGS. 7 and 8, illustrating a pendulum mass according to another embodiment of the invention
  • FIG. 11 is a detailed view of part of the double damping flywheel, in which the guide roller has been removed,
  • FIG. 12 is a view of a guide roller
  • FIG. 13 is a view corresponding to FIG. 11, in which the guide roller is represented,
  • FIG. 14 is a view corresponding to FIG. 13, illustrating another embodiment of the invention.
  • FIGS. 15, 16 and 17 are views respectively corresponding to FIGS. 13, 11 and 12, illustrating yet another embodiment of the invention.
  • FIG. 18 is a front view of the pendulum mass of FIGS. 15 and 16,
  • FIG. 19 is a perspective view of the annular web, supports and pendular damping means, according to another embodiment
  • FIG. 20 is a front view of the assembly of FIG. 19,
  • FIG. 21 is a sectional view along the line A-A of FIG. 20,
  • FIG. 22 and 23 are views respectively corresponding to Figures 20 and 21, an alternative embodiment of the invention.
  • a double damping flywheel according to a first embodiment of the invention is shown in Figures 1 and 2. It comprises a primary flywheel 1 comprising a central hub 2, called primary hub 2, comprising a cylindrical tubular portion 3 from which a radial portion 4 extends radially outwardly.
  • the radial portion 4 of the primary hub 2 is fixed to the end of a crankshaft 5 (FIG. 2) of an internal combustion engine by means of screws 6.
  • This part radial 4 is also fixed to the radially inner periphery of an annular plate 7, axially flexible or not, This sheet 7 has holes 8 in the middle part, whose function will be described later.
  • a primary annular mass of inertia 9 is fixed to the radially outer periphery of the annular plate 7.
  • the primary mass of inertia 9 comprises a radially extending annular portion 10 (FIG. 2) whose radially outer periphery is extended forward by a cylindrical rim January 1.
  • the front face of the annular portion 10 comprises two projecting elements 12 (Figure 1) diametrically opposed, intended to form bearing faces.
  • the free edge of the cylindrical flange 1 1 is fixed, for example by welding, to the radially outer periphery of another annular sheet 13, more particularly to the rear radial face of this sheet 13.
  • a ring gear 14, intended to mesh with a starter belt is fixed on the front face of the sheet 13.
  • the sheet 13 comprises two elements 13a reference already used for the ring gear protruding axially rearward, diametrically opposed, arranged facing the projecting elements 12 of the primary mass of inertia and each forming two bearing faces.
  • the primary mass of inertia 9 and the annular plate 13 define an internal space, intended to be filled with grease and serving to accommodate curved elastic members 15.
  • These elastic members 15 are helical compression springs, mounted in the aforementioned internal space. More particularly, during assembly, the ends 16, 17 of the curved elastic members bear against the bearing faces defined by the projecting members 12, 13a. The primary mass of inertia 9 and the annular plate 13 thus form guide washers.
  • a secondary flywheel 19 is centered and guided in rotation on the primary flywheel 1.
  • the secondary flywheel 19 comprises a secondary mass of inertia 20, comprising in its center a bore 21 for mounting and centering the secondary mass of inertia 20 on the cylindrical portion 3 of the primary hub 2, by the intermediate ball bearing 22 ( Figure 2).
  • the secondary mass of inertia 20 has holes 23 (FIG. 1) serving for the passage of a tool for screwing or unscrewing the fastening screws 6 of the primary flywheel 1 on the end of the crankshaft 5, and holes 24 for These rivets 25 make it possible in particular to fix an annular web 26 to the second mass of inertia 20.
  • the annular web 26 has an annular portion 27 from which two diametrically opposed legs 28 extend radially outwardly.
  • Each lug 28 comprises two opposite bearing faces 29 of the resilient members located radially on the outside, and two opposite bearing faces 30, the function of which will be described later, located radially inward with respect to the faces of FIG. support 29.
  • the bearing faces 29 of the elastic members 15 form an angle relative to each other and diverge from each other outwardly.
  • the faces 30 also form an angle relative to each other and diverge radially inwardly.
  • the elastic members 15 In operation, when a torque is transmitted from the primary flywheel 1 to the secondary flywheel 19, the elastic members 15 bear, at a first end 16 or 17, against the bearing faces 12, 13a of the primary flywheel 1, and at a second end 17 or 16 against the bearing faces 29 of the tabs 28 of the annular web 26, belonging to the secondary flywheel 19.
  • the resilient members 15 can dampen and absorb vibrations and motor rotation acyclisms, as is known per se.
  • the elastic members 15 are associated with friction means for dissipating energy by friction.
  • Supports 33 in the form of annular sheets are mounted on either side of the annular web 26.
  • Each support 33 has a radially inner portion 34, intended to be fixed to the annular web 26, to the opposite support 33 and to the secondary mass of inertia 20, via the rivets 25.
  • rivets 35 serve to fix the subassembly consisting of the supports 33 and the annular web 27 ( Figure 2).
  • the holes 8 formed in the sheet 7 of the primary flywheel 1 are arranged opposite the rivets 25 and allow the passage of a riveting tool.
  • Each support 33 further includes a radially outer portion 36, connected to the radially inner portion by a generally frustoconical portion 37 ( Figure 3).
  • the radially outer portion 36 is axially offset from the radially inner portion 34, opposite the web 26.
  • the radially inner portions 34 of the supports 33 are pressed against the annular web 26 while the radially outer portions 36 are spaced apart, of a determined axial distance, for example between 7 and 20 mm.
  • Some areas of the frustoconical portions 37 are perforated, so that the radially outer portions 36 are connected to the radially inner portions 34 by radial tabs 38.
  • the radially inner portions have fastening tabs 34a extending into the perforated areas and in which are formed holes 34b for mounting the rivets 25.
  • This embodiment provides a flat area for the support of the secondary flywheel 20 and the rivet head 25 while reducing the diameter of the axial offset, that for the purpose of enlarge the internal radial space for the implantation of pendulum masses.
  • Four pendular masses 39 are mounted between the radially outer portions 36 of the supports 33, around the annular web 26. More particularly, each mass 39 is mounted circumferentially between a tab 28 and a stop 31.
  • each support 33 has four pairs of elongated arc-shaped holes 40, the concavity of which is turned radially inwards. Each pair of oblong holes 40 is intended for mounting a mass 39.
  • the oblong holes 40 of one of the supports 33 are arranged facing the oblong holes 40 of the other support 33.
  • Each pendulum mass 39 has three parts 39a, 39b of the same general arc-shaped shape, respectively a central portion 39a and two side portions 39b, disposed on either side of the central portion 39a.
  • the different parts 39a, 39b are fixed to each other by means of three rivets 41, the rivet heads 41 resting on countersinks 42 formed in the side portions 39b.
  • each of the parts 39a, 39b has two circumferential ends. 43, 44 substantially radial, connected by a curved outer peripheral edge 45 and an inner peripheral edge 46.
  • the inner peripheral edge 46 is composed of two parts 46a, 46b each extending over one half of said edge 46, each portion 46a, 46b being curved and having a radius of curvature substantially equal to the radius of the outer periphery 47 of the annular web 26.
  • the inner peripheral edge 46 thus has two adjacent concave zones 46a, 46b, in contrast to the outer peripheral edge 47 which is continuous.
  • Each of the portions 39a, 39b further has two arcuate oblong holes 48a, 48b whose concavity faces outwards, and each disposed between two rivets 41.
  • the radially inner edges 49a oblong holes 48a of the central portion 39a are located radially inwardly relative to the radially inner edges 49b of the oblong holes 48b of the side portions 39b.
  • the radially outer edges 50a of the oblong holes 48a of the central portion 39a are located radially outwardly with respect to the radially outer edges 50b of the oblong holes 48b of the side portions 39b.
  • Guide rolls 51 are mounted loosely in the arcuate oblong holes 48a, 48b, 40 of the masses 39 and supports 33.
  • each roll 51 comprises a central cylindrical zone 51a of diameter D1, bordered on both sides by two cylindrical intermediate zones 51b, of diameter D2, and two end zones.
  • cylindrical 51 c of diameter D3.
  • the diameter D1 is greater than the diameter D2, itself greater than the diameter D3.
  • E1 denotes the radial dimension of the oblong holes 48a of the central portions 39a of the masses 39, that is to say the distance from the inner peripheral edge 49a to the corresponding outer peripheral edge 49b.
  • E2 denotes the radial dimension of the oblong holes 48b of the parts Lateral 39b of the masses 39.
  • e3 designates the radial dimension of the oblong holes 40 of the supports 33.
  • the assembly with play of the rollers 51 in the masses 39 and in the supports 33 implies that e1 is greater than D1, that e2 is greater than D2 and that e3 is greater than D3.
  • D1 is greater than e2 and D2 may possibly be greater than e3.
  • the axial length of the central zone 51a of each roller 51 is slightly less than the axial thickness of the central portion 39a of the corresponding mass 39.
  • the radial shoulders 52 formed between the central zone 39a and the intermediate zones of the rollers are able to abut against radial shoulders 53, situated radially inwards, formed between the oblong holes 49a of the central portion 39a and the oblong holes 49b of the lateral parts 39b of the masses 39.
  • the shoulders 53a located radially outward facing the internal shoulders 53 have a greater clearance chamfer angle than that of the internal shoulders 53, so as to avoid the friction of the rollers 51 on the outer shoulders 53a.
  • the radial shoulders 54 formed between the intermediate zones 51b and the end zones 51c of the rollers 51 are designed to bear, in operation, respectively against the front face of the rear support 33 and against the rear face of the front support 33, which ensures the correct axial positioning of the masses 39 between the supports 33.
  • the distance between the two shoulders 54 is slightly smaller than the distance between the two radially outer portions 36 of the supports 33.
  • at least some of the aforementioned shoulders may be frustoconical, in particular the shoulders 52 and 53, so as to ensure the centering of the masses 39 during the rapid rotation of the rollers 51 inside the oblong holes 48a, 48b of the masses. 39.
  • the radial dimensions of the different shoulders are relatively small, so as to limit friction.
  • the embodiment of FIG. 13 has the advantage of preventing the masses 39 from tilting.
  • the rolling of the rollers 51 is only performed on the part 49a.
  • the realization of the masses 39 is easier because the two parts 39b do not need a very precise alignment of the inner peripheral edges 49b with respect to each other.
  • the rollers 51 bear on the outer peripheral edges of the oblong holes 40 of the supports 33.
  • each mass 39 may comprise resiliently deformable damping means at its circumferential ends 46, 44 and its radially inner edge 46 intended to bear against the faces of support 29 of the lugs 28 or against the bearing faces 32 of the stops 31, and against the radially outer edge 47 of the annular web 26.
  • these damping means are formed by an elastomer strip 55 extending continuously from one circumferential end 43 to another 44, passing through the radially inner edge 46. of the central portion 39a of the corresponding mass 39.
  • This strip 55 comprises pads 56 dovetail on its side facing the central portion 39a, inserted and locked in openings 57 of complementary shape of the central portion 39a, opening at the circumferential ends 43, 44 and the radially inner edge 46.
  • the shape of the strip 55 follows the profile of the inner peripheral edge 46 of the central portion 39a, so that this strip 55 also has two adjacent concave zones 58a, 58b (FIG.
  • each zone 58a, 58b having a radius of curvature substantially equal to the radius of the outer periphery 47 of the annular web 26.
  • the radially inner edge 46 of the central portion 39a is located radially outwardly relative to the radially inner edges 46 of the side portions 39b, so that trapping the band 55 between the lateral parts 39b after assembly.
  • the mounting of the masses 39 is carried out as follows. First, the dovetail pads 56 are mounted in the openings 57 so as to position the elastomeric strip along the circumferential ends 43, 44 and the corresponding edge 46 of the central portion 39a. The central zones 51 with rollers 51 are also engaged with clearance in the oblong holes 48a of the central portions 39a of the masses 39. The lateral portions 39b of the masses 39 are then pressed on either side of the central portion 39a, the zones intermediate 51 b rollers 51 being housed with clearance in the oblong holes 48b of said side portions 39b. The different portions 39a, 39b of the masses 39 are then fixed to each other by the rivets 41.
  • rollers 51 are then mounted captively on the corresponding masses 39 and the elastomeric strip 55 is also fixed on the central portion 39a, between the lateral parts 39b, which allows easy handling of the assembly before assembly of the masses 39 between the The elastomer strip 55 is thus held radially and axially.
  • the damping means are formed by four cylindrical studs 59 made of elastomer, housed in holes 57 in the form of a cylinder portion.
  • a hole 57 opens at each of the circumferential ends 43, 44 of the central portion 39a, two other holes 47 opening at each of the concave portions 46a, 46b of the inner edge 46 of the central portion 39a of the mass 39 corresponding.
  • holes 47 extend over more than 180 °, so that, once the cylindrical studs 59 are housed in these holes 47, they can not escape to the outside.
  • the dimensions of the holes 47 and the pads 59 are adapted so that a sufficient portion of the pads (for example between 0.5 and 5 mm) protrudes outwardly from the central portion 39a, in order to come into bearing against the bearing faces 30 of the tabs 28 and / or against the outer peripheral edge 47 of the annular web 26.
  • the lateral portions 39b are fixed on either side of the central portion 39a, by means of rivets 41, so as to maintain the cylindrical studs 59 in the holes 47 mentioned above.
  • the masses 39 are movable between two extreme positions shown in FIGS. 4 and 6, an intermediate position being represented in FIG.
  • the masses 39 are positioned obliquely to the circumferential direction.
  • One 44 of the circumferential ends 43, 44 abuts against the corresponding bearing face 32 of the abutment 31, the concave zone 58a of the elastomeric strip 55 which is opposite the aforementioned circumferential end 44 bearing against the outer periphery 47 of the annular web 26.
  • the masses 39 are also positioned obliquely to the circumferential direction.
  • One 43 of the circumferential ends 43, 44 abuts against the corresponding bearing surface 30 of the tab 28, the concave zone 58b of the elastomer strip 55 which is opposite the end circumferential 43 being in abutment against the outer periphery 47 of the annular web 26.
  • the masses 39 are intended to oscillate pendulously from one end position to another, through the intermediate position shown in Figure 5 in which the masses 39 are spaced apart from the annular web 26, tabs 28 and stops 31.
  • This pendulum movement of the masses 39 makes it possible to dampen and absorb vibrations and motor rotation acyclisms.
  • the masses 39 can bear only at a circumferential end 43, 44 or a concave zone 58a, 58b.
  • the support can be carried out, at first, at a circumferential end 43, 44 or respectively of a concave zone 58a, 58b and then, in a second step, the support can be furthermore achieved at the concave zone 58a, 58b or respective circumferential end 43, 44. This makes it possible to obtain progressive damping of the masses 39, with stiffness constants which change over time.
  • the deformable means equipping the circumferential ends 43, 44, on the one hand, and the radially inner edge 46, on the other hand have different stiffnesses, the deformable means bearing in a first place presenting a lower stiffness than the deformable means bearing in a second time.
  • the rollers 51 do not come into contact with the ends of the oblong holes 40, 48a, 48b of the supports 33 and masses 39, which makes it possible to limit the noise during operation.
  • the pendular damping means also contribute to reducing the noise in operation.
  • FIGS. 15 to 18 illustrate another embodiment in which the radial dimension e2 of the oblong holes 49b of the lateral portions 39b of the masses 39 is greater than the radial dimension e3 of the holes oblongs 40 of the supports 33 and greater than the radial dimension e1 of the oblong holes 49a of the central portions 39a of the masses 39.
  • the diameter D2 of the intermediate zones 51b of the rollers 51 is greater than the diameter D3 of the end zones 51c, itself greater than the diameter D1 of the central zone 51a.
  • the shoulders 52, 53 and / or 54 may have a frustoconical shape.
  • the oblong holes 49a of the central portions 39a of the masses 39 have enlarged ends 63, visible in dashed lines in FIG. 18, so as to allow the passage of the intermediate zones 51b of the rollers 51 through said enlarged ends 63.
  • This embodiment makes it possible to reduce the Hertz pressures between the rollers 51 and the masses 39, and between the rollers 51 and the supports 33 since it makes it possible to increase the diameter of the zones 51b of the rollers 51 intended to roll.
  • the intermediate zones 51b of the rollers 51 are intended to roll against the edges of the oblong holes 49b of the lateral portions 39b of the masses 39.
  • the central zones 51a are, in turn, not intended to roll directly. at the edges of the oblong holes 49a of the central portions 39a of the masses 39.
  • a variant could consist in providing the opposite.
  • Figures 21 to 23 show another embodiment of the invention, in which the radially outer portions 36 of the supports 33 comprise tabs 61 made of material with the supports 33 and made by cutting and deformation of said supports.
  • Each tongue 61 extends radially, the two ends of the tongue being attached to the corresponding support 33.
  • Each tongue 61 is further deformed axially, so as to extend axially towards the annular web 26.
  • Each tongue 61 thus has a zone 62 bearing on the annular web 26, more particularly on one of the tabs 28 or on one of the stops 31 of the annular web 26.
  • the tongues 61 may be prestressed by bearing on the annular web 26, the prestressing force exerted by each tongue 61 then being less than 200 N.
  • the tongues 61 may also comprise a single end connected to the corresponding support 33, the other end bearing against the annular web 26.
  • the tongues 61 in particular provide a bracing function. These tongues 61 may be elastically deformable, so as to compensate for any deformation of the annular web 26 and prevent such deformation has an effect on the geometry or flatness of the support 33.
  • FIGS. 24 and 25 illustrate an embodiment variant in which rivets 65 provide the spacer function between the supports 33, more particularly between the radially outer portions 36 of said supports 33.
  • the invention thus proposes a torque transmission device, of the double damping flywheel type, in which the torque transmission functions of the annular web 26 and support of the pendulum masses 39 have been dissociated, so as to ensure that the deformation of the annular web 26 has no influence on the displacement or the trajectory of the annular masses 39. This ensures the efficiency of the pendulum damping means.

Abstract

The invention relates to a pendular shock-absorbing device comprising pendular bodies (39), each having a central portion (39a) and two side portions (39b). Each portion (39a, 39b) includes two arcuate oblong holes (48a, 48b) in which guide rollers (51) are mounted. Each roller (51) comprises a cylindrical central area (51a), two cylindrical intermediate areas (51b), and two cylindrical end areas (51c). The intermediate areas (51b) have a diameter (D2) that is different than the diameter (D1) of the central area (51a) so as to form shoulders (52) that prevent the roller (51) from being axially removed from the oblong holes (48a, 48b) of the pendular body (39). Further, the end areas (51c) have a diameter (D3) that is smaller than the diameter (D2) of the adjacent intermediate areas (51b) so as to form a shoulder (54) which is engage with mountings (33).

Description

Dispositif d'amortissement pendulaire  Pendulum damping device
La présente invention concerne un dispositif d'amortissement pendulaire dans une transmission de couple pour véhicule automobile, notamment dans un double volant amortisseur. The present invention relates to a pendulum damping device in a torque transmission for a motor vehicle, in particular in a double damping flywheel.
Le document FR 2 826 079 décrit un double volant amortisseur pour véhicule automobile, comportant un volant primaire destiné à être couplé à un arbre moteur, tel par exemple qu'un vilebrequin, et un volant secondaire, destiné à être couplé à un arbre d'entrée d'une boîte de vitesses par l'intermédiaire d'un embrayage.  The document FR 2 826 079 describes a double damping flywheel for a motor vehicle, comprising a primary flywheel intended to be coupled to a motor shaft, such as for example a crankshaft, and a secondary flywheel, intended to be coupled to a drive shaft. input of a gearbox via a clutch.
Le volant primaire comprend deux éléments, un volant moteur et un couvercle, soudées l'un à l'autre à leur périphérie radialement externe, de manière à délimiter un volume interne étanche dans lequel sont montés des organes élastiques courbes tels que des ressorts à spires hélicoïdales.  The primary flywheel comprises two elements, a flywheel and a cover, welded to one another at their radially outer periphery, so as to delimit a sealed internal volume in which are mounted curved elastic members such as coil springs. helical.
Les organes élastiques s'étendent circonférentiellement et prennent appui, à une première extrémité, sur le volant moteur et/ou sur le couvercle et, à une seconde extrémité, sur un voile annulaire lié au volant secondaire.  The elastic members extend circumferentially and bear, at a first end, on the flywheel and / or on the cover and, at a second end, on an annular web connected to the secondary flywheel.
En fonctionnement, les organes élastiques sont plaqués contre des goulottes disposées en périphérie externe du volume précité sous l'effet des forces centrifuges. Ce volume comporte de la graisse permettant de garantir le bon fonctionnement des organes élastiques.  In operation, the elastic members are pressed against chutes disposed at the outer periphery of the aforementioned volume under the effect of centrifugal forces. This volume includes grease to ensure the proper functioning of the elastic members.
Le double volant amortisseur comporte en outre des moyens d'amortissement pendulaires, logés dans le volume interne précité, et comportant des masses pendulaires montées de façon mobile sur le voile annulaire, notamment par l'intermédiaire de rouleaux de guidage. Ces masses sont disposées radialement à intérieur ou à l'extérieur des organes élastiques courbes.  The double damping flywheel further comprises pendular damping means, housed in the aforementioned internal volume, and comprising pendular masses mounted movably on the annular web, in particular by means of guide rollers. These masses are arranged radially inside or outside the curved elastic members.
Les extrémités des rouleaux de guidage sont montées dans des trous oblongs en forme d'arc du voile annulaire. Les bords des trous oblongs forment ainsi des chemins de roulement pour les extrémités des rouleaux. The ends of the guide rollers are mounted in arcuate elongated holes of the annular web. The edges of the holes oblongs thus form raceways for the ends of the rollers.
Le document DE 10 2010 054 556 décrit un voile annulaire pour un double volant amortisseur, équipé de moyens d'amortissement pendulaires.  Document DE 10 2010 054 556 describes an annular web for a double damping flywheel equipped with pendular damping means.
Le voile annulaire est constitué de deux parties annulaires fixées l'une à l'autre et délimitant entre elles un espace logeant des masses pendulaires. Chaque masse comprend deux trous oblongs en forme d'arc, dont la concavité est tournée radialement vers l'extérieur, servant au montage avec jeu de deux rouleaux. Les extrémités des rouleaux sont engagées dans des renfoncements des parties précitées du voile annulaire, chaque renfoncement présentant une forme générale oblongue en forme d'arc, avec une concavité tournée radialement vers l'intérieur.  The annular web consists of two annular parts attached to each other and defining between them a space housing pendular masses. Each mass comprises two elongated arc-shaped holes, the concavity of which is turned radially outwards, serving for assembly with a set of two rollers. The ends of the rollers are engaged in recesses of the aforementioned parts of the annular web, each recess having a generally arcuate oblong shape, with a concavity turned radially inwardly.
Les rouleaux comportent des collerettes radiales s'étendant entre les masses pendulaires et les parties du voile annulaire.  The rollers comprise radial flanges extending between the pendular masses and the portions of the annular web.
Ces collerettes sont par exemple formées par des anneaux élastiques montés dans des gorges des rouleaux cylindriques. Dans ce cas, le montage de l'ensemble est réalisé de la manière suivante.  These flanges are for example formed by elastic rings mounted in grooves cylindrical rollers. In this case, assembly of the assembly is carried out in the following manner.
Tout d'abord les rouleaux sont engagés dans les trous oblongs des masses. Les anneaux élastiques sont ensuite montés de part et d'autre des masses, dans les gorges correspondantes des masses pendulaires. Des premières extrémités des rouleaux sont alors engagées dans les évidements d'une première partie du voile annulaire, la seconde partie du voile annulaire étant ensuite montée sur la première, de façon à ce que les secondes extrémités des rouleaux s'engagent dans les évidements correspondants de la seconde partie. Les deux parties du voile annulaire sont alors fixées l'une à l'autre, par exemple par soudage.  First the rollers are engaged in the oblong holes of the masses. The elastic rings are then mounted on either side of the masses, in the corresponding grooves of the pendular masses. First ends of the rollers are then engaged in the recesses of a first portion of the annular web, the second portion of the annular web then being mounted on the first, so that the second ends of the rollers engage in the corresponding recesses. of the second part. The two parts of the annular web are then fixed to each other, for example by welding.
Un tel montage est relativement complexe. En particulier, le montage d'anneaux élastiques dans des gorges des rouleaux est fastidieux.  Such an arrangement is relatively complex. In particular, the mounting of elastic rings in grooves of the rollers is tedious.
La demande de brevet FR 1 153794, déposée par la Demanderesse et non encore publiée, propose un dispositif d'amortissement de torsion équipé de moyens d'amortissement pendulaires comportant des masses formées chacune d'une partie centrale et d'au moins deux parties latérales, disposées de part et d'autre de la partie centrale, chacune desdites parties comprenant des trous oblongs en forme d'arc. The patent application FR 1 153794, filed by the Applicant and not yet published, proposes a torsion damping device equipped with pendulum damping means comprising masses each formed of a central portion and at least two lateral portions, disposed on either side of the central portion, each of said portions comprising arcuate oblong holes .
Des rouleaux de guidage sont montés de façon mobile dans les trous oblongs des parties précitées, les extrémités des rouleaux étant montées dans des trous oblongs en forme d'arc de deux supports fixés l'un à l'autre et formant une rondelle de phasage.  Guide rollers are movably mounted in the elongated holes of the aforesaid portions, the ends of the rollers being mounted in arcuate elongated holes of two supports attached to one another and forming a phasing washer.
Les rouleaux comportent une zone centrale cylindrique élargie, de diamètre inférieur à la dimension radiale des trous oblongs ménagés dans les parties centrales des masses, mais de diamètre supérieur à la dimension radiale des trous oblongs ménagés dans les parties latérales des masses.  The rollers comprise an enlarged central cylindrical zone, of diameter smaller than the radial dimension of the oblong holes formed in the central parts of the masses, but of diameter greater than the radial dimension of the oblong holes formed in the lateral parts of the masses.
Le montage des moyens d'amortissement pendulaires est réalisé de la façon suivante.  The mounting of the pendular damping means is carried out as follows.
Tout d'abord, les rouleaux sont engagés dans les parties centrales des masses, de manière à ce que les zones centrales des rouleaux soient situées dans les trous oblongs des parties centrales des masses. Les parties latérales sont alors disposées de part et d'autre des parties centrales, de façon à ce que les rouleaux s'étendent au travers des trous oblongs desdites parties latérales. La partie centrale et les parties latérales correspondantes de chaque masse sont alors fixées les unes aux autres par des rivets. Les rouleaux sont ainsi montés de façon imperdable dans les masses. En effet, après montage, les zones centrales élargies des rouleaux viennent en butée contre les parties latérales des masses, ce qui empêche les rouleaux de s'échapper axialement.  First, the rollers are engaged in the central parts of the masses, so that the central areas of the rollers are located in the oblong holes of the central parts of the masses. The side portions are then disposed on either side of the central portions, so that the rollers extend through the oblong holes of said side portions. The central part and the corresponding lateral parts of each mass are then fixed to each other by rivets. The rollers are thus mounted captively in the masses. Indeed, after assembly, the widened central areas of the rollers abut against the lateral parts of the masses, which prevents the rollers from escaping axially.
Dans ce cas toutefois, le centrage axial des masses entre les supports n'est pas assuré, les masses pouvant frotter contre les supports en fonctionnement, ce qui réduit l'efficacité des moyens d'amortissement pendulaires. L'invention a notamment pour but d'apporter une solution simple, efficace et économique à ce problème. In this case, however, the axial centering of the masses between the supports is not ensured, the masses being able to rub against the supports in operation, which reduces the efficiency of the pendular damping means. The invention aims in particular to provide a simple, effective and economical solution to this problem.
A cet effet, elle propose un dispositif d'amortissement pendulaire comprenant au moins une masse pendulaire comportant une partie centrale et au moins deux parties latérales, disposées de part et d'autre de la partie centrale, chacune desdites parties comprenant au moins un trou oblong en arc de cercle, et au moins un rouleau de guidage monté de façon mobile dans les trous oblongs desdites parties, le rouleau étant destiné à être monté dans des trous oblongs en arc de cercle de deux supports, au niveau de deux zones d'extrémité cylindriques du rouleau, le rouleau comportant une zone centrale cylindrique, logée dans le trou oblong de la partie centrale de la masse pendulaire, caractérisé en ce que le rouleau comporte deux zones intermédiaires cylindriques, logées dans les trous oblongs des parties latérales de la masse pendulaire, s'étendant entre la zone centrale et chacune des zones d'extrémité, les zones intermédiaires ayant un diamètre différent du diamètre de la zone centrale, de façon à former des épaulements empêchant le retrait axial du rouleau hors des trous oblongs de la masse pendulaire, les zones d'extrémité ayant un diamètre inférieur au diamètre des zones intermédiaires adjacentes, de manière à former un épaulement destiné à venir en appui contre les supports correspondants.  For this purpose, it proposes a pendular damping device comprising at least one pendulum mass comprising a central part and at least two lateral parts, arranged on either side of the central part, each of said parts comprising at least one oblong hole. in an arc, and at least one guide roller movably mounted in the oblong holes of said parts, the roller being intended to be mounted in oblong holes in a circular arc of two supports, at two end zones. cylindrical roller, the roller having a central cylindrical zone, housed in the oblong hole of the central portion of the pendulum mass, characterized in that the roller comprises two cylindrical intermediate zones, housed in the oblong holes of the lateral parts of the pendulum mass , extending between the central zone and each of the end zones, the intermediate zones having a diameter different from the diameter of e the central zone, so as to form shoulders preventing the axial withdrawal of the roller from the oblong holes of the pendulum mass, the end zones having a diameter smaller than the diameter of the adjacent intermediate zones, so as to form a shoulder intended to come to bear against the corresponding supports.
On immobilise ainsi axialement le rouleau à l'intérieur de la masse pendulaire, ce qui facilite le montage du dispositif d'amortissement sur les supports. En outre, les différents épaulements assurent le centrage des masses entre les supports, ce qui permet d'éviter tout frottement des masses sur les supports en fonctionnement. L'efficacité du dispositif d'amortissement pendulaire est donc garantie.  This axially immobilizes the roller inside the pendulum mass, which facilitates the mounting of the damping device on the supports. In addition, the different shoulders ensure the centering of the masses between the supports, which makes it possible to avoid any friction of the masses on the supports in operation. The efficiency of the pendulum damping device is therefore guaranteed.
Selon une forme de réalisation, le diamètre de la zone centrale est supérieur au diamètre des zones intermédiaires, les parties latérales de la masse formant des butées axiales pour les épaulements ménagés entre la zone centrale et les zones intermédiaires du rouleau, de façon à empêcher le retrait axial dudit rouleau hors de ladite masse. According to one embodiment, the diameter of the central zone is greater than the diameter of the intermediate zones, the lateral parts of the mass forming axial stops for the shoulders provided between the central zone and the intermediate zones of the roll, so as to prevent the axial withdrawal of said roll from said mass.
La masse pendulaire peut, dans cette forme de réalisation, présenter une masse importante.  The pendulum mass may, in this embodiment, have a large mass.
Selon une autre forme de réalisation, le diamètre de la zone centrale est inférieur au diamètre des zones intermédiaires, les épaulements ménagés entre la zone centrale et les zones intermédiaires du rouleau étant destinés à venir axialement en butée sur la partie centrale de la masse, de façon à empêcher le retrait axial dudit rouleau hors de ladite masse.  According to another embodiment, the diameter of the central zone is smaller than the diameter of the intermediate zones, the shoulders provided between the central zone and the intermediate zones of the roller being intended to come axially in abutment on the central part of the mass, in order to prevent axial removal of said roll from said mass.
Cette forme de réalisation permet de réduire les pressions de Hertz entre le rouleau et la masse, et entre le rouleau et les supports.  This embodiment makes it possible to reduce the Hertz pressures between the roll and the mass, and between the roll and the supports.
Dans cette forme de réalisation également, le trou oblong en forme d'arc de la partie centrale peut comporter une extrémité élargie, permettant l'insertion du rouleau dans ledit trou oblong.  In this embodiment also, the arc-shaped oblong hole of the central portion may have an enlarged end, allowing insertion of the roll into said oblong hole.
L'extrémité élargie permet ainsi le passage des zones les plus larges du rouleau, à savoir les zones intermédiaires.  The enlarged end thus allows the passage of the widest areas of the roll, namely the intermediate areas.
De préférence, au moins certains des épaulements du rouleau et/ou certaines des surfaces de butée desdits épaulements sont tronconiques ou s'étendent de façon oblique par rapport au plan radial.  Preferably, at least some of the roll shoulders and / or some of the abutment surfaces of said shoulders are frustoconical or extend obliquely to the radial plane.
Cette caractéristique permet de garantir le bon centrage de la masse lors de la rotation rapide du rouleau à l'intérieur des trous oblongs.  This characteristic makes it possible to guarantee the proper centering of the mass during the rapid rotation of the roller inside the oblong holes.
La zone centrale du rouleau est destinée à venir en appui sur les bords du trou oblong de la partie centrale de la masse pendulaire.  The central zone of the roll is intended to bear on the edges of the oblong hole of the central part of the pendulum mass.
Dans cette réalisation, le roulement des rouleaux ne se fait que sur la partie centrale. La réalisation des masses est donc aisée car les parties latérales des masses pendulaires n'ont pas à être alignées de manière très précise.  In this embodiment, the rolling of the rollers is only on the central part. The realization of the masses is therefore easy because the lateral parts of the pendular masses do not have to be aligned very precisely.
En variante, les zones intermédiaires du rouleau sont destinées à venir en appui sur les bords des trous oblongs des parties latérales de la masse pendulaire. Ceci a pour avantage d'éviter le basculement des masses en fonctionnement. In a variant, the intermediate zones of the roller are intended to bear on the edges of the oblong holes of the lateral parts of the roller. pendulum mass. This has the advantage of preventing the tilting of the masses in operation.
L'invention concerne également, selon un deuxième aspect de l'invention, un dispositif de transmission de couple pour un véhicule automobile, comportant un élément d'entrée de couple et un élément de sortie de couple mobiles en rotation l'un par rapport à l'autre, et des organes élastiques montés entre les éléments d'entrée et de sortie de couple, l'élément de sortie de couple, ou respectivement l'élément d'entrée de couple, comportant un voile annulaire, les organes élastiques étant montés entre le voile annulaire et l'élément d'entrée de couple, ou respectivement entre le voile annulaire et l'élément de sortie de couple, caractérisé en ce que deux supports annulaires s'étendent radialement de part et d'autre du voile annulaire et sont fixés audit voile annulaire, le dispositif de transmission de couple comportant en outre un dispositif d'amortissement pendulaire selon le premier aspect de l'invention, les masses pendulaires étant disposées axialement entre les supports annulaires, les zones d'extrémité des rouleaux étant montées de façon mobile dans des trous oblongs en forme d'arc des supports annulaires.  The invention also relates, according to a second aspect of the invention, to a torque transmission device for a motor vehicle, comprising a torque input member and a torque output member rotatable with respect to the other, and resilient members mounted between the input and torque output members, the torque output member, or respectively the torque input member, having an annular web, the elastic members being mounted between the annular web and the torque entry element, or respectively between the annular web and the torque output member, characterized in that two annular supports extend radially on either side of the annular web and are fixed to said annular web, the torque transmission device further comprising a pendulum damping device according to the first aspect of the invention, the pendulum masses being arranged axially between the annular supports, the end regions of the rollers being movably mounted in arcuate oblong holes of the annular supports.
Dans le document FR 2 826 079 notamment, le couple transmis par le voile annulaire en fonctionnement peut provoquer une déformation de celui-ci et donc une déformation des bords des trous oblongs formant les chemins de roulement. Ceci peut avoir un impact sur la trajectoire et, plus généralement, sur le déplacement des masses pendulaires, ce qui peut affecter l'efficacité du dispositif d'amortissement pendulaire.  In the document FR 2 826 079 in particular, the torque transmitted by the annular web during operation can cause a deformation thereof and thus a deformation of the edges of the oblong holes forming the raceways. This can have an impact on the trajectory and, more generally, on the displacement of the pendular masses, which can affect the efficiency of the pendulum damping device.
Dans le dispositif de transmission de couple selon l'invention, les masses pendulaires ne sont pas montées sur le voile annulaire, mais sur des supports indépendants qui n'assurent pas la fonction de transmission de couple et qui ne sont donc pas déformés en fonctionnement.  In the torque transmission device according to the invention, the pendular masses are not mounted on the annular web, but on independent supports which do not provide the torque transmission function and which are therefore not deformed in operation.
La trajectoire des masses pendulaires n'est donc pas affectée par une éventuelle déformation du voile annulaire, de sorte que l'efficacité du dispositif d'amortissement pendulaire est préservée. L'invention concerne enfin un procédé de montage d'un dispositif d'amortissement pendulaire du type précité, caractérisé en ce qu'il comporte les étapes consistant à : The trajectory of the pendular masses is thus not affected by any deformation of the annular web, so that the efficiency of the pendular damping device is preserved. The invention finally relates to a method for mounting a pendular damping device of the aforementioned type, characterized in that it comprises the steps of:
- insérer le rouleau dans la partie centrale de la masse pendulaire, de façon à ce que la zone centrale dudit rouleau soit située dans le trou oblong de la partie centrale,  - insert the roll in the central part of the pendulum mass, so that the central zone of said roll is located in the oblong hole of the central part,
- disposer les parties latérales de part et d'autre de la partie centrale de la masse pendulaire, de façon à ce que les zones intermédiaires du rouleau soient situées dans les trous oblongs des parties latérales,  - arrange the lateral parts on either side of the central part of the pendulum mass, so that the intermediate areas of the roller are located in the oblong holes of the lateral parts,
- fixer la partie centrale et les parties latérales les unes aux autres, par exemple par l'intermédiaire de rivets, de façon à ce que le rouleau soit maintenu axialement en position dans les trous oblongs de la masse pendulaire.  - Fix the central portion and the side portions to each other, for example by means of rivets, so that the roller is held axially in position in the oblong holes of the pendulum mass.
L'invention sera mieux comprise et d'autres détails, caractéristiques et avantages de l'invention apparaîtront à la lecture de la description suivante faite à titre d'exemple non limitatif en référence aux dessins annexés dans lesquels :  The invention will be better understood and other details, characteristics and advantages of the invention will appear on reading the following description given by way of non-limiting example with reference to the accompanying drawings in which:
- la figure 1 est une vue éclatée, en perspective, d'un double volant amortisseur selon l'invention,  FIG. 1 is an exploded view, in perspective, of a double damping flywheel according to the invention,
- la figure 2 est une vue en coupe axiale du double volant amortisseur de la figure 1 ,  FIG. 2 is a view in axial section of the double damping flywheel of FIG. 1,
- la figure 3 est une vue éclatée, en perspective, du voile annulaire, des supports et des moyens d'amortissement pendulaires du double volant amortisseur des figures 1 et 2, FIG. 3 is an exploded view, in perspective, of the annular web, the supports and the pendular damping means of the double damping flywheel of FIGS. 1 and 2,
- les figures 4 à 6 sont des vues de côté et en coupe radiale partielle, du double volant amortisseur des figures 1 à 3, dans trois positions différentes des masses pendulaires, - Figures 4 to 6 are side views and in partial radial section, the double damping flywheel of Figures 1 to 3, in three different positions of the pendular masses,
- la figure 7 est une vue en perspective d'une masse pendulaire, - la figure 8 est une vue éclatée, en perspective, de la masse pendulaire de la figure 7, - les figures 9 et 10 sont des vues correspondant respectivement aux figures 7 et 8, illustrant une masse pendulaire selon une autre forme de réalisation de l'invention, FIG. 7 is a perspective view of a pendulum mass; FIG. 8 is an exploded perspective view of the pendulum mass of FIG. 7; FIGS. 9 and 10 are views respectively corresponding to FIGS. 7 and 8, illustrating a pendulum mass according to another embodiment of the invention,
- la figure 1 1 est une vue de détail d'une partie du double volant amortisseur, dans laquelle le rouleau de guidage a été retiré, FIG. 11 is a detailed view of part of the double damping flywheel, in which the guide roller has been removed,
- la figure 12 est une vue d'un rouleau de guidage, FIG. 12 is a view of a guide roller,
- la figure 13 est une vue correspondant à la figure 1 1 , dans laquelle le rouleau de guidage est représenté,  FIG. 13 is a view corresponding to FIG. 11, in which the guide roller is represented,
- la figure 14 est une vue correspondant à la figure 13, illustrant une autre forme de réalisation de l'invention,  FIG. 14 is a view corresponding to FIG. 13, illustrating another embodiment of the invention,
- les figures 15, 16 et 17 sont des vues correspondant respectivement aux figures 13, 1 1 et 12, illustrant une encore une autre forme de réalisation de l'invention,  FIGS. 15, 16 and 17 are views respectively corresponding to FIGS. 13, 11 and 12, illustrating yet another embodiment of the invention,
- la figure 18 est une vue de face de la masse pendulaire des figures 15 et 16,  FIG. 18 is a front view of the pendulum mass of FIGS. 15 and 16,
- la figure 19 est une vue en perspective du voile annulaire, des supports et des moyens d'amortissement pendulaires, selon une autre forme de réalisation,  FIG. 19 is a perspective view of the annular web, supports and pendular damping means, according to another embodiment,
- la figure 20 est une vue de face de l'ensemble de la figure 19, FIG. 20 is a front view of the assembly of FIG. 19,
- la figure 21 est une vue en coupe selon la ligne A-A de la figure 20, FIG. 21 is a sectional view along the line A-A of FIG. 20,
- les figures 22 et 23 sont des vues correspondant respectivement aux figures 20 et 21 , d'une variante de réalisation de l'invention.  - Figures 22 and 23 are views respectively corresponding to Figures 20 and 21, an alternative embodiment of the invention.
Un double volant amortisseur selon une première forme de réalisation de l'invention est représenté aux figures 1 et 2. Il comporte un volant primaire 1 comprenant un moyeu central 2, appelé moyeu primaire 2, comprenant une partie tubulaire cylindrique 3 à partir de laquelle une partie radiale 4 s'étend radialement vers l'extérieur. La partie radiale 4 du moyeu primaire 2 est fixée à l'extrémité d'un vilebrequin 5 (figure 2) d'un moteur à combustion interne, par l'intermédiaire de vis 6. Cette partie radiale 4 est également fixée à la périphérie radialement interne d'une tôle annulaire 7, flexible axialement ou non, Cette tôle 7 comporte des trous 8 en partie médiane, dont la fonction sera décrite plus loin. A double damping flywheel according to a first embodiment of the invention is shown in Figures 1 and 2. It comprises a primary flywheel 1 comprising a central hub 2, called primary hub 2, comprising a cylindrical tubular portion 3 from which a radial portion 4 extends radially outwardly. The radial portion 4 of the primary hub 2 is fixed to the end of a crankshaft 5 (FIG. 2) of an internal combustion engine by means of screws 6. This part radial 4 is also fixed to the radially inner periphery of an annular plate 7, axially flexible or not, This sheet 7 has holes 8 in the middle part, whose function will be described later.
Une masse d'inertie primaire 9 de forme annulaire est fixée à la périphérie radialement externe de la tôle annulaire 7.  A primary annular mass of inertia 9 is fixed to the radially outer periphery of the annular plate 7.
La masse d'inertie primaire 9 comporte une partie annulaire 10 (figure 2) s'étendant radialement dont la périphérie radialement externe est prolongée vers l'avant par un rebord cylindrique 1 1 . La face avant de la partie annulaire 10 comporte deux éléments en saillie 12 (figure 1 ) diamétralement opposés, destinées à former des faces d'appui.  The primary mass of inertia 9 comprises a radially extending annular portion 10 (FIG. 2) whose radially outer periphery is extended forward by a cylindrical rim January 1. The front face of the annular portion 10 comprises two projecting elements 12 (Figure 1) diametrically opposed, intended to form bearing faces.
Le bord libre du rebord cylindrique 1 1 est fixé, par exemple par soudage, à la périphérie radialement externe d'une autre tôle annulaire 13, plus particulièrement à la face radiale arrière de cette tôle 13. Une couronne dentée 14, destinée à engrener avec une courroie de démarreur, est fixée sur la face avant de la tôle 13.  The free edge of the cylindrical flange 1 1 is fixed, for example by welding, to the radially outer periphery of another annular sheet 13, more particularly to the rear radial face of this sheet 13. A ring gear 14, intended to mesh with a starter belt is fixed on the front face of the sheet 13.
La tôle 13 comporte deux éléments 13a référence déjà utilisée pour la couronne dentée en saillie axialement vers l'arrière, diamétralement opposés, disposés en regard des éléments en saillie 12 de la masse d'inertie primaire et formant chacun deux faces d'appui.  The sheet 13 comprises two elements 13a reference already used for the ring gear protruding axially rearward, diametrically opposed, arranged facing the projecting elements 12 of the primary mass of inertia and each forming two bearing faces.
La masse d'inertie primaire 9 et la tôle annulaire 13 délimitent un espace interne, destiné à être rempli de graisse et servant au logement d'organes élastiques courbes 15.  The primary mass of inertia 9 and the annular plate 13 define an internal space, intended to be filled with grease and serving to accommodate curved elastic members 15.
Ces organes élastiques 15 sont des ressorts de compression hélicoïdaux, montés dans l'espace interne précité. Plus particulièrement, lors du montage, les extrémités 16, 17 des organes élastiques courbes viennent en appui contre les faces d'appui définies par les organes en saillie 12, 13a. La masse d'inertie primaire 9 et la tôle annulaire 13 forment ainsi des rondelles de guidage.  These elastic members 15 are helical compression springs, mounted in the aforementioned internal space. More particularly, during assembly, the ends 16, 17 of the curved elastic members bear against the bearing faces defined by the projecting members 12, 13a. The primary mass of inertia 9 and the annular plate 13 thus form guide washers.
Des goulottes 18 sont montées entre la paroi interne du rebord cylindrique 1 1 et les organes élastiques 15, ces goulottes 18 servant à l'appui des organes élastiques 15 lorsque ceux-ci se déforment par centrifugation en fonctionnement. Chutes 18 are mounted between the inner wall of the cylindrical rim January 1 and the elastic members 15, these chutes 18 serving to the support of the elastic members 15 when they deform by centrifugation in operation.
Un volant d'inertie secondaire 19 est centré et guidé en rotation sur le volant d'inertie primaire 1 .  A secondary flywheel 19 is centered and guided in rotation on the primary flywheel 1.
Le volant d'inertie secondaire 19 comporte une masse d'inertie secondaire 20, comportant en son centre un alésage 21 servant au montage et au centrage de la masse d'inertie secondaire 20 sur la partie cylindrique 3 du moyeu primaire 2, par l'intermédiaire d'un roulement à billes 22 (figure 2).  The secondary flywheel 19 comprises a secondary mass of inertia 20, comprising in its center a bore 21 for mounting and centering the secondary mass of inertia 20 on the cylindrical portion 3 of the primary hub 2, by the intermediate ball bearing 22 (Figure 2).
La masse d'inertie secondaire 20 comporte des trous 23 (figure 1 ) servant au passage d'un outil de vissage ou de dévissage des vis de fixation 6 du volant primaire 1 sur l'extrémité du vilebrequin 5, et des trous 24 servant au montage de rivets 25. Ces rivets 25 permettent notamment de fixer un voile annulaire 26 à la seconde masse d'inertie 20.  The secondary mass of inertia 20 has holes 23 (FIG. 1) serving for the passage of a tool for screwing or unscrewing the fastening screws 6 of the primary flywheel 1 on the end of the crankshaft 5, and holes 24 for These rivets 25 make it possible in particular to fix an annular web 26 to the second mass of inertia 20.
Comme cela est mieux visible à la figure 3, le voile annulaire 26 comporte une partie annulaire 27 à partir de laquelle deux pattes diamétralement opposées 28 s'étendent radialement vers l'extérieur.  As best seen in Figure 3, the annular web 26 has an annular portion 27 from which two diametrically opposed legs 28 extend radially outwardly.
Chaque patte 28 comporte deux faces 29 opposées d'appui des organes élastiques, situées radialement à l'extérieur, et deux faces 30 opposées d'appui, dont la fonction sera décrite après, situées radialement à l'intérieur par rapport aux faces d'appui 29.  Each lug 28 comprises two opposite bearing faces 29 of the resilient members located radially on the outside, and two opposite bearing faces 30, the function of which will be described later, located radially inward with respect to the faces of FIG. support 29.
Les faces 29 d'appui des organes élastiques 15 forment un angle l'une par rapport à l'autre et divergent l'une de l'autre vers l'extérieur. Les faces 30 forment également un angle l'une par rapport à l'autre et divergent radialement vers l'intérieur.  The bearing faces 29 of the elastic members 15 form an angle relative to each other and diverge from each other outwardly. The faces 30 also form an angle relative to each other and diverge radially inwardly.
En fonctionnement, lorsqu'un couple est transmis du volant primaire 1 au volant secondaire 19, les organes élastiques 15 prennent appui, à une première extrémité 16 ou 17, contre les faces d'appui 12, 13a du volant primaire 1 , et à une seconde extrémité 17 ou 16 contre les faces d'appui 29 des pattes 28 du voile annulaire 26, appartenant au volant secondaire 19. Les organes élastiques 15 permettent d'amortir et d'absorber les vibrations et les acyclismes de rotation du moteur, comme cela est connu en soi. In operation, when a torque is transmitted from the primary flywheel 1 to the secondary flywheel 19, the elastic members 15 bear, at a first end 16 or 17, against the bearing faces 12, 13a of the primary flywheel 1, and at a second end 17 or 16 against the bearing faces 29 of the tabs 28 of the annular web 26, belonging to the secondary flywheel 19. The resilient members 15 can dampen and absorb vibrations and motor rotation acyclisms, as is known per se.
_Dans un mode de réalisation non représenté, les organes élastiques 15 sont associés à des moyens de friction permettant de dissiper l'énergie par frottement.  _In an embodiment not shown, the elastic members 15 are associated with friction means for dissipating energy by friction.
Au contraire, dans le mode de réalisation représenté, aucun moyen de friction supplémentaire n'est ajouté, l'énergie étant dissipée par le frottement naturel entre la masse primaire 9 et la masse secondaire 19, en grande partie du au frottement des organes élastiques 15. Deux butées 31 diamétralement opposées s'étendent en outre radialement vers l'extérieur depuis le voile annulaire 26. Chaque butée 31 présente deux faces latérales d'appui 32 opposées, formant un angle l'une avec l'autre et divergeant l'une de l'autre radialement vers l'intérieur.  On the contrary, in the embodiment shown, no additional friction means is added, the energy being dissipated by the natural friction between the primary mass 9 and the secondary mass 19, largely due to the friction of the elastic members 15 Two diametrically opposite stops 31 extend radially outwardly from the annular web 26. Each stop 31 has two opposite lateral bearing faces 32 forming an angle with each other and diverging one from the other. on the other side radially inwards.
Des supports 33 se présentant sous la forme de tôles annulaires sont montés de part et d'autre du voile annulaire 26.  Supports 33 in the form of annular sheets are mounted on either side of the annular web 26.
Chaque support 33 comporte une partie radialement interne 34, destinée à être fixée au voile annulaire 26, au support opposé 33 et à la masse d'inertie secondaire 20, par l'intermédiaire des rivets 25.  Each support 33 has a radially inner portion 34, intended to be fixed to the annular web 26, to the opposite support 33 and to the secondary mass of inertia 20, via the rivets 25.
D'autres rivets 35 servent à la fixation du sous-ensemble constitué des supports 33 et du voile annulaire 27 (figure 2).  Other rivets 35 serve to fix the subassembly consisting of the supports 33 and the annular web 27 (Figure 2).
Les trous 8 formés dans la tôle 7 du volant d'inertie primaire 1 sont ménagés en regard des rivets 25 et permettent le passage d'un outil de rivetage.  The holes 8 formed in the sheet 7 of the primary flywheel 1 are arranged opposite the rivets 25 and allow the passage of a riveting tool.
Chaque support 33 comporte en outre une partie radialement externe 36, reliée à la partie radialement interne par une partie globalement tronconique 37 (figure 3). La partie radialement externe 36 est décalée axialement de la partie radialement interne 34, à l'opposé du voile 26. Ainsi, les parties radialement internes 34 des supports 33 sont plaquées contre le voile annulaire 26 alors que les parties radialement externes 36 en sont écartées, d'une distance axiale déterminée, par exemple comprise entre 7 et 20 mm. Each support 33 further includes a radially outer portion 36, connected to the radially inner portion by a generally frustoconical portion 37 (Figure 3). The radially outer portion 36 is axially offset from the radially inner portion 34, opposite the web 26. Thus, the radially inner portions 34 of the supports 33 are pressed against the annular web 26 while the radially outer portions 36 are spaced apart, of a determined axial distance, for example between 7 and 20 mm.
Certaines zones des parties tronconiques 37 sont ajourées, de sorte que les parties radialement externes 36 sont reliées aux parties radialement internes 34 par des pattes radiales 38. Les parties radialement internes portent des pattes de fixation 34a s'étendant dans les zones ajourées et dans lesquelles sont formés des trous 34b servant au montages des rivets 25. Cette réalisation permet d'obtenir une zone plane pour le support du volant secondaire 20 et de la tête de rivet 25 tout en réduisant le diamètre du décalage axial, cela dans le but d'agrandir l'espace radial interne pour l'implantation des masses pendulaires. Quatre masses pendulaires 39 sont montées entre les parties radialement externes 36 des supports 33, autour du voile annulaire 26. Plus particulièrement, chaque masse 39 est montée circonférentiellement entre une patte 28 et une butée 31 .  Some areas of the frustoconical portions 37 are perforated, so that the radially outer portions 36 are connected to the radially inner portions 34 by radial tabs 38. The radially inner portions have fastening tabs 34a extending into the perforated areas and in which are formed holes 34b for mounting the rivets 25. This embodiment provides a flat area for the support of the secondary flywheel 20 and the rivet head 25 while reducing the diameter of the axial offset, that for the purpose of enlarge the internal radial space for the implantation of pendulum masses. Four pendular masses 39 are mounted between the radially outer portions 36 of the supports 33, around the annular web 26. More particularly, each mass 39 is mounted circumferentially between a tab 28 and a stop 31.
La partie radialement externe 36 de chaque support 33 comporte quatre paires de trous oblongs en forme d'arc 40, dont la concavité est tournée radialement vers l'intérieur. Chaque paire de trous oblongs 40 est destinée au montage d'une masse 39. Les trous oblongs 40 de l'un des supports 33 sont disposés en regard des trous oblongs 40 de l'autre support 33.  The radially outer portion 36 of each support 33 has four pairs of elongated arc-shaped holes 40, the concavity of which is turned radially inwards. Each pair of oblong holes 40 is intended for mounting a mass 39. The oblong holes 40 of one of the supports 33 are arranged facing the oblong holes 40 of the other support 33.
Chaque masse pendulaire 39 comporte trois parties 39a, 39b de même forme générale en forme d'arc, respectivement une partie centrale 39a et deux parties latérales 39b, disposées de part et d'autre de la partie centrale 39a. Les différentes parties 39a, 39b sont fixées les unes aux autres par l'intermédiaire de trois rivets 41 , les têtes des rivets 41 s'appuyant sur des lamages 42 ménagés dans les parties latérales 39b. De manière alternative, il est possible de fixer les trois parties 39a, 39b et 39c par collage ou par soudage.  Each pendulum mass 39 has three parts 39a, 39b of the same general arc-shaped shape, respectively a central portion 39a and two side portions 39b, disposed on either side of the central portion 39a. The different parts 39a, 39b are fixed to each other by means of three rivets 41, the rivet heads 41 resting on countersinks 42 formed in the side portions 39b. Alternatively, it is possible to fix the three parts 39a, 39b and 39c by gluing or welding.
Comme cela est mieux visible aux figures 7 et 8 notamment, chacune des parties 39a, 39b comporte deux extrémités circonférentielles 43, 44 sensiblement radiales, reliées par un bord périphérique externe courbe 45 et un bord périphérique interne 46. Le bord périphérique interne 46 est composé de deux parties 46a, 46b s'étendant chacune sur une moitié dudit bord 46, chaque partie 46a, 46b étant courbe et présentant un rayon de courbure sensiblement égal au rayon de la périphérie externe 47 du voile annulaire 26. Le bord périphérique interne 46 présente ainsi deux zones concaves adjacentes 46a, 46b, contrairement au bord périphérique externe 47 qui est continu. As can be seen more clearly in FIGS. 7 and 8, each of the parts 39a, 39b has two circumferential ends. 43, 44 substantially radial, connected by a curved outer peripheral edge 45 and an inner peripheral edge 46. The inner peripheral edge 46 is composed of two parts 46a, 46b each extending over one half of said edge 46, each portion 46a, 46b being curved and having a radius of curvature substantially equal to the radius of the outer periphery 47 of the annular web 26. The inner peripheral edge 46 thus has two adjacent concave zones 46a, 46b, in contrast to the outer peripheral edge 47 which is continuous.
Chacune des parties 39a, 39b présente en outre deux trous oblongs 48a, 48b en forme d'arc dont la concavité est tournée vers l'extérieur, et disposés chacun entre deux rivets 41 .  Each of the portions 39a, 39b further has two arcuate oblong holes 48a, 48b whose concavity faces outwards, and each disposed between two rivets 41.
Comme cela est mieux visible aux figures 1 1 et 13, les bords radialement internes 49a des trous oblongs 48a de la partie centrale 39a sont situés radialement à l'intérieur par rapport aux bords radialement internes 49b des trous oblongs 48b des parties latérales 39b. En outre, les bords radialement externes 50a des trous oblongs 48a de la partie centrale 39a sont situés radialement à l'extérieur par rapport aux bords radialement externes 50b des trous oblongs 48b des parties latérales 39b.  As best seen in Figures 1 1 and 13, the radially inner edges 49a oblong holes 48a of the central portion 39a are located radially inwardly relative to the radially inner edges 49b of the oblong holes 48b of the side portions 39b. In addition, the radially outer edges 50a of the oblong holes 48a of the central portion 39a are located radially outwardly with respect to the radially outer edges 50b of the oblong holes 48b of the side portions 39b.
Des rouleaux de guidage 51 sont montés avec jeu dans les trous oblongs 48a, 48b, 40 en forme d'arc des masses 39 et des supports 33.  Guide rolls 51 are mounted loosely in the arcuate oblong holes 48a, 48b, 40 of the masses 39 and supports 33.
Comme cela est mieux visible aux figures 12 et 13, chaque rouleau 51 comporte une zone centrale cylindrique 51 a de diamètre D1 , bordée de part et d'autre par deux zones intermédiaires cylindriques 51 b , de diamètre D2, et deux zones d'extrémité cylindriques 51 c, de diamètre D3. Le diamètre D1 est supérieur au diamètre D2, lui-même supérieur au diamètre D3.  As can be seen more clearly in FIGS. 12 and 13, each roll 51 comprises a central cylindrical zone 51a of diameter D1, bordered on both sides by two cylindrical intermediate zones 51b, of diameter D2, and two end zones. cylindrical 51 c, of diameter D3. The diameter D1 is greater than the diameter D2, itself greater than the diameter D3.
On désigne par e1 la dimension radiale des trous oblongs 48a des parties centrales 39a des masses 39, c'est-à-dire la distance du bord périphérique interne 49a au bord périphérique externe 49b correspondant. On désigne par e2 la dimension radiale des trous oblongs 48b des parties latérales 39b des masses 39. On désigne enfin par e3 la dimension radiale des trous oblongs 40 des supports 33. E1 denotes the radial dimension of the oblong holes 48a of the central portions 39a of the masses 39, that is to say the distance from the inner peripheral edge 49a to the corresponding outer peripheral edge 49b. E2 denotes the radial dimension of the oblong holes 48b of the parts Lateral 39b of the masses 39. Finally, e3 designates the radial dimension of the oblong holes 40 of the supports 33.
Le montage avec jeu des rouleaux 51 dans les masses 39 et dans les supports 33 implique que e1 est supérieur à D1 , que e2 est supérieur à D2 et que e3 est supérieur à D3.  The assembly with play of the rollers 51 in the masses 39 and in the supports 33 implies that e1 is greater than D1, that e2 is greater than D2 and that e3 is greater than D3.
Par ailleurs, D1 est supérieur à e2 et D2 peut éventuellement être supérieur à e3. La longueur axiale de la zone centrale 51 a de chaque rouleau 51 est légèrement inférieure à l'épaisseur axiale de la partie centrale 39a de la masse 39 correspondante.  Moreover, D1 is greater than e2 and D2 may possibly be greater than e3. The axial length of the central zone 51a of each roller 51 is slightly less than the axial thickness of the central portion 39a of the corresponding mass 39.
Le fait que D1 soit supérieur à e2 implique que, quand les rouleaux The fact that D1 is greater than e2 implies that when the rollers
51 sont montés dans les masses 39, ils sont logés de façon imperdable dans les trous oblongs 49a, 49b correspondants. En effet, les épaulements radiaux 52 formés entre la zone centrale 39a et les zones intermédiaires des rouleaux sont aptes à venir en butée contre les épaulements radiaux 53, situés radialement à l'intérieur, formés entre les trous oblongs 49a de la partie centrale 39a et les trous oblongs 49b des parties latérales 39b des masses 39. 51 are mounted in the masses 39, they are housed captively in the corresponding oblong holes 49a, 49b. Indeed, the radial shoulders 52 formed between the central zone 39a and the intermediate zones of the rollers are able to abut against radial shoulders 53, situated radially inwards, formed between the oblong holes 49a of the central portion 39a and the oblong holes 49b of the lateral parts 39b of the masses 39.
Les épaulements 53a situés radialement à l'extérieur, situés en regard des épaulements internes 53, présentent un angle de chanfrein de dégagement plus important que celui des épaulements internes 53, de manière à éviter le frottement des rouleaux 51 sur les épaulements externes 53a.  The shoulders 53a located radially outward facing the internal shoulders 53, have a greater clearance chamfer angle than that of the internal shoulders 53, so as to avoid the friction of the rollers 51 on the outer shoulders 53a.
De même, les épaulements radiaux 54 formés entre les zones intermédiaires 51 b et les zones d'extrémité 51 c des rouleaux 51 (figure 1 1 ) sont destinés à venir en appui, en fonctionnement, respectivement contre la face avant du support arrière 33 et contre la face arrière du support avant 33, ce qui assure le bon positionnement axial des masses 39 entre les supports 33. La distance entre les deux épaulements 54 est légèrement inférieure à la distance entre les deux parties radialement externes 36 des supports 33. De préférence, certains au moins des épaulements précités peuvent être tronconiques, en particulier les épaulements 52 et 53, de façon à assurer le centrage des masses 39 lors de la rotation rapide des rouleaux 51 à l'intérieur des trous oblongs 48a, 48b des masses 39. Les dimensions radiales des différents épaulements sont relativement réduites, de manière à limiter les frottements. Likewise, the radial shoulders 54 formed between the intermediate zones 51b and the end zones 51c of the rollers 51 (FIG. 11) are designed to bear, in operation, respectively against the front face of the rear support 33 and against the rear face of the front support 33, which ensures the correct axial positioning of the masses 39 between the supports 33. The distance between the two shoulders 54 is slightly smaller than the distance between the two radially outer portions 36 of the supports 33. Preferably, at least some of the aforementioned shoulders may be frustoconical, in particular the shoulders 52 and 53, so as to ensure the centering of the masses 39 during the rapid rotation of the rollers 51 inside the oblong holes 48a, 48b of the masses. 39. The radial dimensions of the different shoulders are relatively small, so as to limit friction.
On rappelle qu'en fonctionnement, les masses 39 et les rouleaux 51 sont poussés radialement vers l'extérieur par les forces centrifuges. Ainsi, en fonctionnement, les rouleaux 51 sont en appui sur les bords périphériques internes 49b des trous oblongs 48b des parties latérales 39b des masses 39 (figure 13) ou sur les bords périphériques internes 49a des trous oblongs 48a des parties centrales 39a des masses 39 (figure 14).  It is recalled that in operation, the masses 39 and the rollers 51 are pushed radially outwards by the centrifugal forces. Thus, in operation, the rollers 51 bear on the inner peripheral edges 49b of the oblong holes 48b of the lateral portions 39b of the masses 39 (FIG. 13) or on the inner peripheral edges 49a of the oblong holes 48a of the central portions 39a of the masses 39 (Figure 14).
La forme de réalisation de la figure 13 a pour avantage d'éviter le basculement des masses 39. Dans la forme de réalisation de la figure 14, le roulement des rouleaux 51 ne se fait que sur la partie 49a. La réalisation des masses 39 est donc plus aisée car les deux pièces 39b n'ont pas besoin d'un alignement très précis des bords périphériques internes 49b l'un par rapport à l'autre. En outre, en fonctionnement, les rouleaux 51 sont en appui sur les bords périphériques externes des trous oblongs 40 des supports 33.  The embodiment of FIG. 13 has the advantage of preventing the masses 39 from tilting. In the embodiment of FIG. 14, the rolling of the rollers 51 is only performed on the part 49a. The realization of the masses 39 is easier because the two parts 39b do not need a very precise alignment of the inner peripheral edges 49b with respect to each other. In addition, in operation, the rollers 51 bear on the outer peripheral edges of the oblong holes 40 of the supports 33.
Comme cela est mieux visible aux figures 7 à 10, chaque masse 39 peut comporter des moyens d'amortissement élastiquement déformables au niveau de ses extrémités circonférentielles 46, 44 et de son bord radialement interne 46, destinées à venir en appui contre les faces d'appui 29 des pattes 28 ou contre les faces d'appui 32 des butées 31 , et contre le bord radialement externe 47 du voile annulaire 26.  As can be seen more clearly in FIGS. 7 to 10, each mass 39 may comprise resiliently deformable damping means at its circumferential ends 46, 44 and its radially inner edge 46 intended to bear against the faces of support 29 of the lugs 28 or against the bearing faces 32 of the stops 31, and against the radially outer edge 47 of the annular web 26.
Dans la forme de réalisation des figures 7 et 8 notamment, ces moyens d'amortissement sont formés par une bande en élastomère 55 s'étendant de manière continue d'une extrémité circonférentielle 43 à une autre 44, en passant par le bord radialement interne 46 de la partie centrale 39a de la masse correspondante 39. Cette bande 55 comporte des plots 56 en queue d'aronde sur sa face tournée vers la partie centrale 39a, insérés et bloqués dans des ouvertures 57 de forme complémentaire de la partie centrale 39a, débouchant au niveau des extrémités circonférentielles 43, 44 et du bord radialement interne 46. En outre, la forme de la bande 55 suit le profil du bord périphérique interne 46 de la partie centrale 39a, de sorte que cette bande 55 présente également deux zones concaves adjacentes 58a, 58b (figure 7), chaque zone 58a, 58b ayant un rayon de courbure sensiblement égal au rayon de la périphérie externe 47 du voile annulaire 26. De préférence, le bord radialement interne 46 de la partie centrale 39a est situé radialement à l'extérieur par rapport aux bords radialement interne 46 des parties latérales 39b, de manière à bien emprisonner la bande 55 entre les parties latérales 39b après montage. In the embodiment of FIGS. 7 and 8 in particular, these damping means are formed by an elastomer strip 55 extending continuously from one circumferential end 43 to another 44, passing through the radially inner edge 46. of the central portion 39a of the corresponding mass 39. This strip 55 comprises pads 56 dovetail on its side facing the central portion 39a, inserted and locked in openings 57 of complementary shape of the central portion 39a, opening at the circumferential ends 43, 44 and the radially inner edge 46. In addition, the shape of the strip 55 follows the profile of the inner peripheral edge 46 of the central portion 39a, so that this strip 55 also has two adjacent concave zones 58a, 58b (FIG. 7), each zone 58a, 58b having a radius of curvature substantially equal to the radius of the outer periphery 47 of the annular web 26. Preferably, the radially inner edge 46 of the central portion 39a is located radially outwardly relative to the radially inner edges 46 of the side portions 39b, so that trapping the band 55 between the lateral parts 39b after assembly.
Le montage des masses 39 est réalisé de la manière suivante. Tout d'abord, les plots 56 en queue d'aronde sont montés dans les ouvertures 57 de manière à positionner la bande élastomère le long des extrémités circonférentielles 43, 44 et du bord correspondant 46 de la partie centrale 39a. Les zones centrales 51 a des rouleaux 51 sont également engagées avec jeu dans les trous oblongs 48a des parties centrales 39a des masses 39. Les parties latérales 39b des masses 39 sont ensuite plaquées de part et d'autre de la partie centrale 39a, les zones intermédiaires 51 b des rouleaux 51 venant se loger avec jeu dans les trous oblongs 48b desdites parties latérales 39b. Les différentes parties 39a, 39b des masses 39 sont ensuite fixées les unes aux autres par les rivets 41 . Les rouleaux 51 sont alors montés de façon imperdable sur les masses correspondantes 39 et la bande élastomère 55 est également fixée sur la partie centrale 39a, entre les parties latérales 39b, ce qui permet de manipuler facilement l'ensemble avant montage des masses 39 entre les supports 33. La bande élastomère 55 est ainsi maintenue radialement et axialement.  The mounting of the masses 39 is carried out as follows. First, the dovetail pads 56 are mounted in the openings 57 so as to position the elastomeric strip along the circumferential ends 43, 44 and the corresponding edge 46 of the central portion 39a. The central zones 51 with rollers 51 are also engaged with clearance in the oblong holes 48a of the central portions 39a of the masses 39. The lateral portions 39b of the masses 39 are then pressed on either side of the central portion 39a, the zones intermediate 51 b rollers 51 being housed with clearance in the oblong holes 48b of said side portions 39b. The different portions 39a, 39b of the masses 39 are then fixed to each other by the rivets 41. The rollers 51 are then mounted captively on the corresponding masses 39 and the elastomeric strip 55 is also fixed on the central portion 39a, between the lateral parts 39b, which allows easy handling of the assembly before assembly of the masses 39 between the The elastomer strip 55 is thus held radially and axially.
Dans la forme de réalisation des figures 9 et 10, les moyens d'amortissement sont formés par quatre plots cylindriques 59 en élastomère, logés dans des trous 57 en forme de portion de cylindre. Un trou 57 débouche au niveau de chacune des extrémités circonférentielles 43, 44 de la partie centrale 39a, deux autres trous 47 débouchant au niveau de chacune des parties concave 46a, 46b du bord interne 46 de la partie centrale 39a de la masse 39 correspondante. In the embodiment of Figures 9 and 10, the damping means are formed by four cylindrical studs 59 made of elastomer, housed in holes 57 in the form of a cylinder portion. A hole 57 opens at each of the circumferential ends 43, 44 of the central portion 39a, two other holes 47 opening at each of the concave portions 46a, 46b of the inner edge 46 of the central portion 39a of the mass 39 corresponding.
Les bords de ces trous 47 s'étendent sur plus de 180°, de manière à ce que, une fois que les plots cylindriques 59 sont logés dans ces trous 47, ils ne peuvent pas s'échapper vers l'extérieur. Bien entendu, les dimensions des trous 47 et des plots 59 sont adaptées pour qu'une partie suffisante des plots (comprise par exemple entre 0,5 et 5 mm) fasse saillie vers l'extérieur de la partie centrale 39a, afin de venir en appui contre les faces d'appui 30 des pattes 28 et/ou contre le bord périphérique externe 47 du voile annulaire 26.  The edges of these holes 47 extend over more than 180 °, so that, once the cylindrical studs 59 are housed in these holes 47, they can not escape to the outside. Of course, the dimensions of the holes 47 and the pads 59 are adapted so that a sufficient portion of the pads (for example between 0.5 and 5 mm) protrudes outwardly from the central portion 39a, in order to come into bearing against the bearing faces 30 of the tabs 28 and / or against the outer peripheral edge 47 of the annular web 26.
Comme précédemment, les parties latérales 39b sont fixées de part et d'autre de la partie centrale 39a, par l'intermédiaire de rivets 41 , de façon à maintenir les plots cylindriques 59 dans les trous 47 précités.  As previously, the lateral portions 39b are fixed on either side of the central portion 39a, by means of rivets 41, so as to maintain the cylindrical studs 59 in the holes 47 mentioned above.
En fonctionnement, les masses 39 sont mobiles entre deux positions extrêmes représentées aux figures 4 et 6, une position intermédiaire étant représentée à la figure 5.  In operation, the masses 39 are movable between two extreme positions shown in FIGS. 4 and 6, an intermediate position being represented in FIG.
Dans la position extrême représentée à la figure 4, les masses 39 sont positionnées de manière oblique par rapport à la direction circonférentielle. L'une 44 des extrémités circonférentielles 43, 44 vient en appui contre la face d'appui 32 correspondante de la butée 31 , la zone concave 58a de la bande élastomère 55 qui est opposée à l'extrémité circonférentielle 44 précitée étant en appui contre la périphérie externe 47 du voile annulaire 26.  In the extreme position shown in Figure 4, the masses 39 are positioned obliquely to the circumferential direction. One 44 of the circumferential ends 43, 44 abuts against the corresponding bearing face 32 of the abutment 31, the concave zone 58a of the elastomeric strip 55 which is opposite the aforementioned circumferential end 44 bearing against the outer periphery 47 of the annular web 26.
Dans la position extrême représentée à la figure 6, les masses 39 sont également positionnées de manière oblique par rapport à la direction circonférentielle. L'une 43 des extrémités circonférentielles 43, 44 vient en appui contre la face d'appui 30 correspondante de la patte 28, la zone concave 58b de la bande élastomère 55 qui est opposée à l'extrémité circonférentielle 43 précitée étant en appui contre la périphérie externe 47 du voile annulaire 26. In the extreme position shown in Figure 6, the masses 39 are also positioned obliquely to the circumferential direction. One 43 of the circumferential ends 43, 44 abuts against the corresponding bearing surface 30 of the tab 28, the concave zone 58b of the elastomer strip 55 which is opposite the end circumferential 43 being in abutment against the outer periphery 47 of the annular web 26.
En fonctionnement, les masses 39 sont destinées à osciller de manière pendulaire d'une position extrême à une autre, en passant par la position intermédiaire représentée à la figure 5 dans laquelle les masses 39 sont écartées du voile annulaire 26, des pattes 28 et des butées 31 .  In operation, the masses 39 are intended to oscillate pendulously from one end position to another, through the intermediate position shown in Figure 5 in which the masses 39 are spaced apart from the annular web 26, tabs 28 and stops 31.
Ce mouvement pendulaire des masses 39 permet d'amortir et d'absorber les vibrations et les acyclismes de rotation du moteur.  This pendulum movement of the masses 39 makes it possible to dampen and absorb vibrations and motor rotation acyclisms.
En variante, les masses 39 peuvent venir en appui uniquement au niveau d'une extrémité circonférentielle 43, 44 ou d'une zone concave 58a, 58b. En variante également, l'appui peut être réalisé, dans un premier temps, au niveau d'une extrémité circonférentielle 43, 44 ou respectivement d'une zone concave 58a, 58b puis, dans un second temps, l'appui peut en outre être réalisé au niveau de la zone concave 58a, 58b ou respectivement de l'extrémité circonférentielle 43, 44 correspondante. Ceci permet d'obtenir un amortissement progressif des masses 39, avec des constantes de raideur qui évoluent dans le temps.  As a variant, the masses 39 can bear only at a circumferential end 43, 44 or a concave zone 58a, 58b. As a variant also, the support can be carried out, at first, at a circumferential end 43, 44 or respectively of a concave zone 58a, 58b and then, in a second step, the support can be furthermore achieved at the concave zone 58a, 58b or respective circumferential end 43, 44. This makes it possible to obtain progressive damping of the masses 39, with stiffness constants which change over time.
Dans une variante de réalisation, les moyens déformables équipant les extrémités circonférentielles 43, 44, d'une part, et le bord radialement interne 46, d'autre part, présentent des raideurs différentes, les moyens déformables venant en appui dans un premier temps présentant une raideur plus faible que les moyens déformable venant en appui dans un second temps.  In an alternative embodiment, the deformable means equipping the circumferential ends 43, 44, on the one hand, and the radially inner edge 46, on the other hand, have different stiffnesses, the deformable means bearing in a first place presenting a lower stiffness than the deformable means bearing in a second time.
Dans les positions extrêmes des figures 4 et 6, les rouleaux 51 ne viennent pas en contact avec les extrémités des trous oblongs 40, 48a, 48b des supports 33 et des masses 39, ce qui permet de limiter les bruits en fonctionnement. De manière générale, les moyens d'amortissement pendulaires participent également à réduire le bruit en fonctionnement.  In the extreme positions of FIGS. 4 and 6, the rollers 51 do not come into contact with the ends of the oblong holes 40, 48a, 48b of the supports 33 and masses 39, which makes it possible to limit the noise during operation. In general, the pendular damping means also contribute to reducing the noise in operation.
Les figures 15 à 18 illustrent une autre forme de réalisation dans laquelle la dimension radiale e2 des trous oblongs 49b des parties latérales 39b des masses 39 est supérieure à la dimension radiale e3 des trous oblongs 40 des supports 33 et supérieure à la dimension radiale e1 des trous oblongs 49a des parties centrales 39a des masses 39. FIGS. 15 to 18 illustrate another embodiment in which the radial dimension e2 of the oblong holes 49b of the lateral portions 39b of the masses 39 is greater than the radial dimension e3 of the holes oblongs 40 of the supports 33 and greater than the radial dimension e1 of the oblong holes 49a of the central portions 39a of the masses 39.
De même, le diamètre D2 des zones intermédiaires 51 b des rouleaux 51 est supérieur au diamètre D3 des zones d'extrémité 51 c, lui- même supérieur au diamètre D1 de la zone centrale 51 a.  Similarly, the diameter D2 of the intermediate zones 51b of the rollers 51 is greater than the diameter D3 of the end zones 51c, itself greater than the diameter D1 of the central zone 51a.
Comme précédemment, les épaulements 52, 53 et/ou 54 peuvent présenter une forme tronconique.  As before, the shoulders 52, 53 and / or 54 may have a frustoconical shape.
Les trous oblongs 49a des parties centrales 39a des masses 39 comportent des extrémités élargies 63, visibles en pointillés à la figure 18, de manière à autoriser le passage des zones intermédiaires 51 b des rouleaux 51 au travers desdites extrémités élargies 63.  The oblong holes 49a of the central portions 39a of the masses 39 have enlarged ends 63, visible in dashed lines in FIG. 18, so as to allow the passage of the intermediate zones 51b of the rollers 51 through said enlarged ends 63.
Cette forme de réalisation permet de réduire les pressions de Hertz entre les rouleaux 51 et les masses 39, et entre les rouleaux 51 et les supports 33 puisqu'elle permet d'augmenter le diamètre des zones 51 b des rouleaux 51 destinées à rouler.  This embodiment makes it possible to reduce the Hertz pressures between the rollers 51 and the masses 39, and between the rollers 51 and the supports 33 since it makes it possible to increase the diameter of the zones 51b of the rollers 51 intended to roll.
Dans cette forme de réalisation, les zones intermédiaires 51 b des rouleaux 51 sont destinées à rouler contre les bords des trous oblongs 49b des parties latérales 39b des masses 39. Les zones centrales 51 a ne sont, quant à elles, pas destinées à rouler directement sur les bords des trous oblongs 49a des parties centrales 39a des masses 39. Bien entendu, une variante pourrait consister à prévoir l'inverse.  In this embodiment, the intermediate zones 51b of the rollers 51 are intended to roll against the edges of the oblong holes 49b of the lateral portions 39b of the masses 39. The central zones 51a are, in turn, not intended to roll directly. at the edges of the oblong holes 49a of the central portions 39a of the masses 39. Of course, a variant could consist in providing the opposite.
Les figures 21 à 23 présentent une autre forme de réalisation de l'invention, dans laquelle les parties radialement externes 36 des supports 33 comportent des languettes 61 venant de matière avec les supports 33 et réalisées par découpage et déformation desdits supports.  Figures 21 to 23 show another embodiment of the invention, in which the radially outer portions 36 of the supports 33 comprise tabs 61 made of material with the supports 33 and made by cutting and deformation of said supports.
Chaque languette 61 s'étend radialement, les deux extrémités de la languette étant rattachées au support 33 correspondant.  Each tongue 61 extends radially, the two ends of the tongue being attached to the corresponding support 33.
Chaque languette 61 est en outre déformée axialement, de manière à s'étendre axialement en direction du voile annulaire 26. Chaque languette 61 présente ainsi une zone 62 en appui sur le voile annulaire 26, plus particulièrement sur l'une des pattes 28 ou sur l'une des butées 31 du voile annulaire 26. Each tongue 61 is further deformed axially, so as to extend axially towards the annular web 26. Each tongue 61 thus has a zone 62 bearing on the annular web 26, more particularly on one of the tabs 28 or on one of the stops 31 of the annular web 26.
Les languettes 61 peuvent être précontraintes par appui sur le voile annulaire 26, l'effort de précontrainte exercé par chaque languette 61 étant alors inférieur à 200 N.  The tongues 61 may be prestressed by bearing on the annular web 26, the prestressing force exerted by each tongue 61 then being less than 200 N.
Bien entendu, les languettes 61 peuvent également comporter une seule extrémité reliée au support 33 correspondant, l'autre extrémité venant en appui contre le voile annulaire 26.  Of course, the tongues 61 may also comprise a single end connected to the corresponding support 33, the other end bearing against the annular web 26.
Les languettes 61 assurent notamment une fonction d'entretoisement. Ces languettes 61 peuvent être déformables élastiquement, de façon à compenser toute déformation du voile annulaire 26 et éviter qu'une telle déformation ait un effet sur la géométrie ou la planéité du support 33.  The tongues 61 in particular provide a bracing function. These tongues 61 may be elastically deformable, so as to compensate for any deformation of the annular web 26 and prevent such deformation has an effect on the geometry or flatness of the support 33.
Les figures 24 et 25 illustrent une variante de réalisation dans laquelle des rivets 65 assurent la fonction d'entretoise entre les supports 33, plus particulièrement entre les parties radialement externes 36 desdits supports 33. L'invention propose ainsi un dispositif de transmission de couple, de type double volant amortisseur, dans lequel les fonctions de transmission de couple du voile annulaire 26 et de support des masses pendulaires 39 ont été dissociées, de manière à garantir que la déformation du voile annulaire 26 n'a pas d'influence sur le déplacement ou la trajectoire des masses annulaires 39. On garantit ainsi l'efficacité des moyens d'amortissement pendulaires.  FIGS. 24 and 25 illustrate an embodiment variant in which rivets 65 provide the spacer function between the supports 33, more particularly between the radially outer portions 36 of said supports 33. The invention thus proposes a torque transmission device, of the double damping flywheel type, in which the torque transmission functions of the annular web 26 and support of the pendulum masses 39 have been dissociated, so as to ensure that the deformation of the annular web 26 has no influence on the displacement or the trajectory of the annular masses 39. This ensures the efficiency of the pendulum damping means.

Claims

REVENDICATIONS
1 . Dispositif d'amortissement pendulaire comprenant au moins une masse pendulaire (39) comportant une partie centrale (39a) et au moins deux parties latérales (39b), disposées de part et d'autre de la partie centrale (39a), chacune desdites parties (39a, 39b) comprenant au moins un trou oblong (48a, 48b) en forme d'arc, et au moins un rouleau de guidage (51 ) monté de façon mobile dans les trous oblongs (48a, 48b) desdites parties (39a, 39b), le rouleau (51 ) étant destiné à être monté dans des trous oblongs (40) en forme d'arc de deux supports (33), au niveau de deux zones d'extrémité cylindriques (51 c) du rouleau (51 ), le rouleau (51 ) comportant une zone centrale cylindrique (51 a), logée dans le trou oblong (48a) de la partie centrale (39a) de la masse pendulaire (39), caractérisé en ce que le rouleau (51 ) comporte deux zones intermédiaires cylindriques (51 b), logées dans les trous oblongs (48b) des parties latérales (39b) de la masse pendulaire (39), s'étendant entre la zone centrale (51 a) et chacune des zones d'extrémité (51 c), les zones intermédiaires (51 b) ayant un diamètre (D2) différent du diamètre (D1 ) de la zone centrale (51 a), de façon à former des épaulements (52) empêchant le retrait axial du rouleau (51 ) hors des trous oblongs (48a, 48b) de la masse pendulaire (39), les zones d'extrémité (51 c) ayant un diamètre (D3) inférieur au diamètre (D2) des zones intermédiaires (51 b) adjacentes, de manière à former un épaulement (54) destiné à venir en appui contre les supports (33) correspondants. 1. Pendulum damping device comprising at least one pendulum mass (39) comprising a central part (39a) and at least two lateral parts (39b), arranged on either side of the central part (39a), each of said parts ( 39a, 39b) comprising at least one elongated arc-shaped hole (48a, 48b) and at least one guide roller (51) movably mounted in the oblong holes (48a, 48b) of said portions (39a, 39b) ), the roller (51) being adapted to be mounted in arcuate elongated holes (40) of two supports (33), at two cylindrical end regions (51c) of the roller (51), the roller (51) having a central cylindrical zone (51a), housed in the oblong hole (48a) of the central portion (39a) of the pendulum mass (39), characterized in that the roller (51) has two zones cylindrical intermediates (51b), housed in the oblong holes (48b) of the lateral parts (39b) of the pendulum mass (39), extending between the central zone (51 a) and each of the end zones (51 c), the intermediate zones (51 b) having a diameter (D2) different from the diameter (D1) of the central zone (51 a), so forming shoulders (52) preventing the axial withdrawal of the roller (51) from the oblong holes (48a, 48b) of the pendulum mass (39), the end zones (51c) having a diameter (D3) less than diameter (D2) of the intermediate zones (51b) adjacent, so as to form a shoulder (54) intended to bear against the corresponding supports (33).
2. Dispositif d'amortissement pendulaire selon la revendication 1 , caractérisé en ce que le diamètre (D1 ) de la zone centrale (51 a) est supérieur au diamètre (D2) des zones intermédiaires (51 b), les parties latérales (39b) de la masse (39) formant des butées axiales pour les épaulements (52) ménagés entre la zone centrale (51 a) et les zones intermédiaires (51 b) du rouleau (51 ), de façon à empêcher le retrait axial dudit rouleau (51 ) hors de ladite masse (39). 2. Pendulum damping device according to claim 1, characterized in that the diameter (D1) of the central zone (51 a) is greater than the diameter (D2) of the intermediate zones (51 b), the lateral parts (39b). mass (39) forming axial stops for the shoulders (52) formed between the central zone (51a) and the intermediate zones (51b) of the roller (51), so as to prevent the axial withdrawal of said roller (51); ) out of said mass (39).
3. Dispositif d'amortissement pendulaire selon la revendication 1 , caractérisé en ce que le diamètre (D1 ) de la zone centrale (51 a) est inférieur au diamètre (D2) des zones intermédiaires (51 b), les épaulements (52) ménagés entre la zone centrale (51 a) et les zones intermédiaires (51 b) du rouleau (51 ) étant destinés à venir axialement en butée sur la partie centrale (39a) de la masse (39), de façon à empêcher le retrait axial dudit rouleau (51 ) hors de ladite masse (39). 3. A pendulum damping device according to claim 1, characterized in that the diameter (D1) of the central zone (51 a) is smaller than the diameter (D2) of the intermediate zones (51 b), the shoulders (52) arranged between the central zone (51 a) and the intermediate zones (51 b) of the roller (51) being intended to come axially in abutment with the central part (39a) of the mass (39), so as to prevent the axial withdrawal of said roll (51) out of said mass (39).
4. Dispositif d'amortissement pendulaire selon la revendication 3, caractérisé en ce que le trou oblong (48a) en forme d'arc de la partie centrale (39a) comporte une extrémité élargie (63), permettant l'insertion du rouleau (51 ) dans ledit trou oblong (48a).  Pendulum damping device according to claim 3, characterized in that the elongated arc-shaped hole (48a) of the central portion (39a) has an enlarged end (63) for insertion of the roller (51). ) in said oblong hole (48a).
5. Dispositif d'amortissement pendulaire selon l'une des revendications 1 à 4, caractérisé en ce que au moins certains des épaulements (52, 54) du rouleau et/ou certaines des surfaces de butée (53) desdits épaulements (52, 54) sont tronconiques ou s'étendent de façon oblique par rapport au plan radial.  Pendulum damping device according to one of claims 1 to 4, characterized in that at least some of the shoulders (52, 54) of the roller and / or some of the abutment surfaces (53) of said shoulders (52, 54 ) are frustoconical or extend obliquely to the radial plane.
6. Dispositif d'amortissement pendulaire selon l'une des revendications 1 à 5, caractérisé en ce que la zone centrale (51 a) du rouleau (51 ) est destinée à venir en appui sur les bords du trou oblong (48a) de la partie centrale (39a) de la masse pendulaire (39).  6. pendular damping device according to one of claims 1 to 5, characterized in that the central region (51 a) of the roller (51) is intended to bear on the edges of the oblong hole (48a) of the central portion (39a) of the pendulum mass (39).
7. Dispositif d'amortissement pendulaire selon l'une des revendications 1 à 5, caractérisé en ce que les zones intermédiaires (51 b) du rouleau (51 ) sont destinées à venir en appui sur les bords des trous oblongs (48b) des parties latérales (39b) de la masse pendulaire (39).  7. Pendulum damping device according to one of claims 1 to 5, characterized in that the intermediate zones (51 b) of the roller (51) are intended to bear against the edges of the oblong holes (48b) of the parts laterals (39b) of the pendulum mass (39).
8. Dispositif de transmission de couple pour véhicule automobile, comportant un élément d'entrée de couple (1 ) et un élément de sortie de couple (19) mobiles en rotation l'un par rapport à l'autre, et des organes élastiques (15) montés entre les éléments d'entrée et de sortie de couple (1 , 19), l'élément de sortie de couple (19), ou respectivement l'élément d'entrée de couple (1 ), comportant un voile annulaire (26), les organes élastiques (15) étant montés entre le voile annulaire (26) et l'élément d'entrée de couple (1 ), ou respectivement entre le voile annulaire (26) et l'élément de sortie de couple (19), caractérisé en ce que deux supports annulaires (33) s'étendent radialement de part et d'autre du voile annulaire (26) et sont fixés audit voile annulaire (26), le dispositif de transmission de couple comportant en outre un dispositif d'amortissement pendulaire selon l'une des revendications 1 à 7, les masses pendulaires (39) étant disposées axialement entre les supports annulaires (33), les zones d'extrémité (51 c) des rouleaux (51 ) étant montées de façon mobile dans des trous oblongs (40) en forme d'arc des supports annulaires (33). A torque transmission device for a motor vehicle having a torque input member (1) and a torque output member (19) rotatable relative to each other and resilient members ( 15) mounted between the torque input and output members (1, 19), the torque output member (19), or the torque input member (1), respectively, having an annular web ( 26), the resilient members (15) being mounted between the annular web (26) and the element torque inlet (1), or respectively between the annular web (26) and the torque output member (19), characterized in that two annular supports (33) extend radially on either side of the annular web (26) and are fixed to said annular web (26), the torque transmission device further comprising a pendulum damping device according to one of claims 1 to 7, the pendulum masses (39) being arranged axially between the annular supports (33), the end regions (51c) of the rollers (51) being movably mounted in arcuate elongated holes (40) of the annular supports (33).
9. Procédé de montage d'un dispositif d'amortissement pendulaire selon l'une des revendications 1 à 7, caractérisé en ce qu'il comporte les étapes consistant à :  9. A method of mounting a pendulum damping device according to one of claims 1 to 7, characterized in that it comprises the steps of:
- insérer le rouleau (51 ) dans la partie centrale (39a) de la masse pendulaire (39), de façon à ce que la zone centrale (51 a) dudit rouleau (51 ) soit située dans le trou oblong (48a) de la partie centrale (39a),  - insert the roller (51) in the central part (39a) of the pendulum mass (39), so that the central zone (51a) of said roller (51) is located in the oblong hole (48a) of the central portion (39a),
- disposer les parties latérales (39b) de part et d'autre de la partie centrale (39a) de la masse pendulaire (39), de façon à ce que les zones intermédiaires (51 b) du rouleau (51 ) soient situées dans les trous oblongs (48b) des parties latérales (39b),  arranging the lateral parts (39b) on either side of the central portion (39a) of the pendulum mass (39), so that the intermediate zones (51b) of the roll (51) are located in the oblong holes (48b) of the lateral parts (39b),
- fixer la partie centrale (39a) et les parties latérales (39b) les unes aux autres, par exemple par l'intermédiaire de rivets (41 ), de façon à ce que le rouleau (51 ) soit maintenu axialement en position dans les trous oblongs (48a, 48b) de la masse pendulaire (39).  - fixing the central portion (39a) and the side portions (39b) to each other, for example by means of rivets (41), so that the roller (51) is held axially in position in the holes oblong (48a, 48b) of the pendulum mass (39).
PCT/FR2013/050173 2012-02-07 2013-01-28 Pendular shock-absorbing device WO2013117841A1 (en)

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CN105658992B (en) * 2013-10-24 2019-08-06 舍弗勒技术股份两合公司 Torsional vibration damper
WO2015144169A1 (en) 2014-03-27 2015-10-01 Schaeffler Technologies AG & Co. KG Centrifugal force pendulum comprising a spring arrangement
DE102014211597A1 (en) 2014-06-17 2015-12-17 Schaeffler Technologies AG & Co. KG centrifugal pendulum
WO2015192840A1 (en) 2014-06-17 2015-12-23 Schaeffler Technologies AG & Co. KG Centrifugal force pendulum
DE102014212172A1 (en) * 2014-06-25 2016-01-14 Schaeffler Technologies AG & Co. KG centrifugal pendulum
DE102014212172B4 (en) * 2014-06-25 2016-06-23 Schaeffler Technologies AG & Co. KG centrifugal pendulum
WO2016000711A1 (en) 2014-07-02 2016-01-07 Schaeffler Technologies AG & Co. KG Centrifugal pendulum
DE102014212813A1 (en) 2014-07-02 2016-01-07 Schaeffler Technologies AG & Co. KG centrifugal pendulum
CN106468330A (en) * 2015-08-20 2017-03-01 舍弗勒技术股份两合公司 Centrifugal force pendulum and the fluid torque-converter with centrifugal force pendulum
CN108027011A (en) * 2015-09-10 2018-05-11 舍弗勒技术股份两合公司 Torsional vibration damper
CN107795636A (en) * 2016-09-06 2018-03-13 福特全球技术公司 Bent axle pendulum with the fully integrated buffer for improving NVH
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CN110382909A (en) * 2017-03-31 2019-10-25 日本Tmt机械株式会社 Vibration absorber and coil holder system
CN110382909B (en) * 2017-03-31 2021-05-25 日本Tmt机械株式会社 Vibration damper and bobbin holder system
CN112963502A (en) * 2017-03-31 2021-06-15 日本Tmt机械株式会社 Rotating body system
CN112963502B (en) * 2017-03-31 2022-05-10 日本Tmt机械株式会社 Rotating body system
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